Engine Fault Code

CF34-10E (GEK112081) ENGINE MANUAL

Revision No. 29

Dated 05/31/2013

ESM 72-00-00, FAULT ISOLATION 001 GENERAL

* * * FOR ALL -10E MODELS TASK 72-00-00-810-801 1.

Ge ne ral . A. The Fault Fault Isolation Isolation Manual Manual contains contains procedures procedures that provide provide instructions instructions to isolate fault conditions that result in a fault message being sent by the FADEC. B. The document document is divided divided into into seven seven fault isolati isolation on procedur procedures: es: (1) Fault Isolation 001: Provides Provides general scope on the whole procedure and explains how to use it when a fault message appears, provides a description of six fault message categories, provides some general fault isolation instructions, specifies tools, equipment and consumable materials utilized during a fault isolation, and contains two tables of all FADEC faults listed both ways: in Fault Code order - Table 101, and CMC Message alphabetical order - Table 102. (2) Fault Isolation 002-007: 002-007: Deal with fault isolation procedures procedures corresponding to six categories of FADEC faults. Each fault isolation procedure contains general information on its contents, how-to-use instructions, two tables of faults, listed the same way as in this procedure: in Fault Code order - Table 101, and CMC Message alphabetical order - Table 102, and troubleshooting procedures relevant to the faults. (3) Fault Isolation 008: Deal with "Non-FADEC" "Non-FADEC" fault isolation procedures. procedures. C. FADEC FADEC Fault Fault Mess Message age Cate Categor gories ies: : (1) In-Flight Warning: Warning: Indicates fault that requires pilot action or notification. Sent to the cockpit CAS messages or icons on the EICAS displays. Refer to TASK 72-00-00-810-802 (72-00-00, Fault Isolation 002). (2) No Dispatch: Dispatch is not permitted with message message present. Message can be caused by a single indicated fault or a combination of short and/or long-term faults. Refer to TASK 72-00-00-810-803 (72-00-00, Fault Isolation 003). (3) Short-Term Dispatch: Dispatch: Dispatch is permitted with a short-term fault(s) fault(s) present. The permitted dispatch interval for these faults is 150 flight hours. The indicated fault must be fixed/cleared before 150 flight hours expires. Message is displayed on EICAS. Refer to TASK 72-00-00-810-804 (72-00-00, Fault Isolation 004). (4) Long-Term Dispatch: Dispatch: Dispatch is permitted with long-term long-term fault(s) present. Correct all long-term faults on a periodic basis. The time interval approved for this periodic maintenance is less than or equal to 750 flight hours. Refer to TASK 72-00-00-810-805 (72-00-00, Fault Isolation 005). (5) Economic Dispatch: Dispatch: Dispatch is permitted with no time limit. Refer to TASK 72-00-00-810-806 (72-00-00, Fault Isolation 006). (6) Maintenance Information Information Messages: Can only be seen on the CMC. Refer to TASK 72-00-00-810-807 (72-00-00, Fault Isolation 007). D. Special troubleshooting troubleshooting procedures corresponding corresponding to the Fault Fault Message Message Categories are defined as subtasks in TASK 72-00-00-810-802 (72-00-00, Fault Isolation 002) thru TASK 72-00-00-810-807 (72-00-00, Fault Isolation 007). (1) Each subtask concerning concerning the fault isolation procedure may consist of the

GE PROPRIETARY INFORMATION - Not to be used, disclosed to others or reproduced without the express written consent of GE. Technical Date Printed: data is considered ITAR and/or EAR controlled; transfer of this Aug 28, 2016 data to a Non-US Person, without USG authorization, is strictly

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following parts: (a) Maintenance Maintenance Messages. This part gives the CMC message and the fault code information for the fault isolation procedure. (b) Descript Description. ion. This part describes the nature and possible causes of the fault. (c) Initial Evaluation Evaluation Procedure. Procedure. This part provides preliminary procedure that, in some circumstances, releases the maintenance crew from performing further troubleshooting steps provided in the Fault Isolation Procedure specific for the subtask. (d) Fault Isolation Isolation Procedure. Procedure. This part defines the procedure to isolate and correct the fault. (e) Repair Confirmation. Confirmation. This part defines the steps necessary to prove that the fault has been corrected. 2. How-to How-to-Us -Use e Inst Instru ructi ctions ons. . A. Read and follow General Fault Isolation Isolation Instructions Instructions described described in in paragraph paragraph 3. B. Having the Fault Code and/or CMC Message of of the fault fault under investigation investigation find appropriate Fault Message Category and Fault Isolation Subtask number in Table 101 - using the Fault Code, or in Table 102 - using the CMC Message. C. Go to the appropriate appropriate Fault Isolation Isolation corresponding corresponding to the Fault Fault Message Message Category and find the Fault Isolation Procedure that describes actions to isolate and correct the fault. D. Follow the instructions instructions in each each procedure procedure to isolate isolate the the fault. Each fault message includes instructions that can vary depending on which FADEC channel sent the message. Make sure that you follow the instructions for the FADEC channel (A or B) that sent the fault message when applicable. 3. General General Fault Fault Isolat Isolation ion Instruct Instructions ions. . A. Record all fault messages messages before before you do maintenance maintenance on the engine, engine, or before before you remove the engine from the aircraft. Refer to the AMM for operation of the EICAS and the CMC. Note the engine and FADEC designations. B. Some troubleshootin troubleshooting g procedures procedures require require special special evaluation engine runs in addition to the initial evaluation provided in particular subtasks. If the special evaluation engine run is required, the run procedure will be provided within the Fault Isolation Procedure. C. Some faults faults may require checking of electrical electrical characterist characteristics ics of possible defective components. D. Replace all all components components that fail a required check. Turn Turn off the the appropriate appropriate aircraft circuit breakers, refer to the AMM, and then re-power the FADEC and clear the faults. If faults are no longer present, do the necessary engine checks for replacement of that component. (1) Because some fault messages are only sent during engine operation, operation, a confirmation that a fault has been corrected can require engine operation, as instructed in the specific isolation procedure, to do the GE PROPRIETARY INFORMATION - Not to be used, disclosed to others or reproduced without the express written consent of GE. Technical Date Printed: data is considered ITAR and/or EAR controlled; transfer of this Aug 28, 2016 data to a Non-US Person, without USG authorization, is strictly

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check. (2) Because the FADEC channel channel and the igniters change change with each engine start, more than one engine start can be necessary to confirm that an engine start fault has been corrected. Refer to the engine operational check procedure. (3) Because some test faults (i.e., overspeed overspeed and EDP relay test faults) are stored to FADEC memory until the test is passed, multiple starts, as instructed in the specific isolation procedure, can be necessary to clear the fault after replacement of the component. E. Swapping of the FADEC harnesses for "XXX "XXX SENSOR SENSOR RANGE FAULT" faults. (1) The first step for "XXX SENSOR SENSOR RANGE FAULT" faults in the Fault Fault Isolation Procedure is to decide, using your judgment, whether the probability of a FADEC fault is significant enough to be taken into account as an actual fault cause. If so, perform the swapping of the FADEC harnesses according to the following procedure: (a) Turn off 400 Hz power to the FADEC by pulling pulling the appropriate aircraft circuit breakers. Refer to the AMM. (b) Disconnect the FA FADEC-side DEC-side P3 and P4 connectors connectors and swap the W3 (yellow) cable and the W4 (blue) cable. (c) Re-power the FADEC. 1

If the the fault fault is now now detec detected ted on the the oppos opposite ite channel channel (the fault fault switches channels), the defect is in the component or the cable associated with the original fault channel. Continue with the Fault Isolation Procedure at the subsequent step.

2

If the the fault fault remai remains ns on the the same same chan channel nel (th (the e fault fault does does not not switch channels), the defective component is the FADEC. Replace the FADEC. Refer to: FADEC Removal, AMM TASK 73-21-01-000-801-A. 73-21-01-000-801-A. FADEC Installation, AMM TASK 73-21-01-400-801-A.

F. If a fault message message is still still present, present, contin continue ue the fault fault isolation isolation. . 4. Tools, Tools, Equi Equipm pment ent, , and Mater Material ials. s. NOTE

You can use equivalent alternatives for tools, equipment, and consumable materials. A. Tool Tools s and and Equi Equipm pmen ent. t. (1) Special Tools. None. None. (2) Standard Tools Tools and Equipment. Equipment. D

r

M

r r

Digital Multimeter (4-1/2 digit readout, accuracy of not less than 0.5 percent, minimum impedance of one megohm)

Hewlett-Packard Corp. 1501 Page Mill Rd. Palo Alto, CA 94304 U.S.A.

Sho r tin g/ u mpe r Pi ns

L oc al P urc ha se

(3) Locally Manufactured Manufactured Tools. Tools. None. (4) Consumable Materials. None. (5) Referenced Procedures. GE PROPRIETARY INFORMATION - Not to be used, disclosed to others or reproduced without the express written consent of GE. Technical Date Printed: data is considered ITAR and/or EAR controlled; transfer of this Aug 28, 2016 data to a Non-US Person, without USG authorization, is strictly

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Revision No. 29

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ATA N

D r 

7 2- 00 -0 0

F au lt I so lat io n 00 2

7 2- 00 -0 0


7 2- 00 -0 0


7 2- 00 -0 0


7 2- 00 -0 0


7 2- 00 -0 0


7 2- 00 -0 0


--

Air cra f t M a int ena n ce M anu al ( AMM )

(6) Expendable Parts. None. 5. Index Index of all all FADEC FADEC Fault Faults. s.

TABLE 101. FAULT MESSAGE DISPATCH - MASTER INDEX (Fault Code Order) F

 C d

C MC M

D

r

(CAS M)

F

 I

S (D L)

73215214E1A 73215214E1B 73215214E2A 73215214E2B

T/R DEPLOY COMMAND OFF FAULT (ENG X REV PROT FAULT)

No affect on TRAS operation but the sense of deployment command has failed to OFF

72-00-00-810-258 (IN FLIGHT WARNING)

73215215E1A 73215215E1B 73215215E2A 73215215E2B

T/R DCU CMD MONITOR FAILED ON (ENG X REV PROT FAULT)

No affect on TRAS operation but the DCU command monitor has failed to ON


73215216E1A 73215216E1B 73215216E2A 73215216E2B

T/R DCU CMD MON FAILED Off (ENG X REV PROT FAULT)

No affect on TRAS operation but the DCU command monitor has failed to OFF


73215217E1A 73215217E1B 73215217E2A 73215217E2B

T/R COWL LK CMD MON FAILED ON (ENG X REV PROT FAULT)

No affect on TRAS operation, a sensor of the cowl lock operation has failed to ON


73215218E1A 73215218E1B 73215218E2A 73215218E2B

T/R COWL LK CMD MON FAILED OFF (ENG X REV PROT FAULT)

No affect on TRAS operation, a sensor of the cowl lock operation has failed to OFF


73215219E1A 73215219E1B 73215219E2A 73215219E2B

T/R ICU RELAY FAILED CLOSED (ENG X REV PROT FAULT)

One (or both) ICU control relay contact has failed in the pressure (CLOSED) state


73215220E1A

T/R ICU RELAY FAILED

Reverser does not

72-00-00-810-2 64


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73215220E1B 73215220E2A 73215220E2B

OPEN (ENG X REV FAIL)

DEPLOY when commanded. Both ICU control relay contacts have failed in the non-pressure (OPEN) state

(IN FLIGHT WARNING)

73215221E1A 73215221E1B 73215221E2A 73215221E2B

T/R ICU CMD MON FAILED OPEN (ENG X REV PROT FAULT)

No affect on reverser operation. The ICU command monitor has failed to OFF, reducing the test ability


73215222E1A 73215222E1B 73215222E2A 73215222E2B

T/R ICU CMD MON FAILED CLOSED (ENG X REV PROT FAULT)

No affect on reverser operation. The ICU command monitor has failed to ON, reducing the test ability


73215223E1A 73215223E1B 73215223E2A 73215223E2B

T/R 1 POWER SUPPLY FAULT(ENG X REV FAIL)

The SPDA is not sending 28 VDC power to the TRAS system when the engine 1 is running on ground or GMO state is true. This fault is ACTIVE only on engine 1


73215224E1A 73215224E1B 73215224E2A 73215224E2B

T/R 2 POWER SUPPLY FAULT (ENG X REV FAIL)



73215225E1A 73215225E1B 73215225E2A 73215225E2B

T/R 1 HYDRAULIC PRESSURE LOW (NONE)

The ARINC input of the TRAS hydraulic pressure for engine 1 is lower than 1800 PSIA

72-00-00-810-269 (LONG DISPATCH)

73215226E1A 73215226E1B 73215226E2A 73215226E2B



72-00-00-810-270 (LONG DISPATCH)

73215227E1A 73215227E1B 73215227E2A 73215227E2B

T/R POSITION SENSOR DISAGREE (NONE)

The two TRAS LVDT signals are in range but differ by more than 3.75 stroke for 5.3 seconds or more

72-00-00-810-271 (LONG DISPATCH)

73215228E1A 73215228E1B 73215228E2A

T/R COWL LK SLND FAULT (ENG X REV FAIL)

The TRAS cowl lock has CLOSED before it was expected to close



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7 321 5 228 E2B

a ft er a st ow . Th is condition may prevent TRAS operation during the next flight

73215229E1A 73215229E1B 73215229E2A 73215229E2B

MULTIPLE T/R PROT FAULTS (ENG X NO DISPATCH)

Two or more Thrust Reverser protection faults have been set

72-00-00-810-726 (NO DISPATCH)

73215321E1A 73215321E1B 73215321E2A 73215321E2B

LPT CMD - POSITION DISAGREE (NONE) NOTE: For v5.20 and below this fault is a "SHORT DISPATCH" fault

The LPT position is more than 5 percent from the demanded position. The sensor and torque motor values are OK, the sensor has been valid for more than 2.0 seconds

72-00-00-810-247 (LONG DISPATCH)

73215322E1A 73215322E1B 73215322E2A 73215322E2B

LPT SENSOR RANGE FAULT (NONE)

Local channel LPT position feedback sensor is out of the range of -8.6 to 108.6% stroke or the voltage sum is out of the range of 3.0 to 13.0 volts. Cross channel sensor is used

72-00-00-810-248 (ECONOMIC DISPATCH)

73215323E1A 73215323E1B 73215323E2A 73215323E2B

LPT DUAL CMD-CURRENT DISAGREE (NONE) NOTE: For v5.20 and below this fault is a "SHORT DISPATCH" fault

Dual channel failure in the torque motor driver circuits. LPT will slew to the FAIL SAFE position

72-00-00-810-249 (LONG DISPATCH)

73215324E1A 73215324E1B 73215324E2A 73215324E2B

LPT LPT CMD CMD - CURR CURREN ENT T DISAGREE (NONE)

Single channel failure in the LPT torque motor driver circuit


73215325E1A 73215325E1B 73215325E2A 73215325E2B

LPT DUAL SENSOR RANGE FAULT (NONE) NOTE: For v5.20 and below this fault is a "SHORT DISPATCH" fault

Both LPT position feedback sensors have failed. LPT position is set to 100 percent CLOSED. LPT will slew to the FAIL SAFE position

72-00-00-810-251 (LONG DISPATCH)

73215326E1A 73215326E1B 73215326E2A 73215326E2B

LPT CHAN A-B SENSORS DISAGREE (NONE)

The two LPT position feedback sensors are in range but disagree by more than 5 percent stroke. Sensor is selected based on rate of change and previously



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failed sensor 73215327E1A 73215327E1B 73215327E2A 73215327E2B

ECU TEMP SENSORS Sensors that monitor DISAGREE the FADEC internal (NONE) temperature differs NOTE: For v5.32 and by more than 50F below, this fault is a (10C) from the "SHORT DISPATCH" fault average FADEC internal temperature. Indicates the failure of the ECU temperature sensor

72-00-00-810-738 (LONG DISPATCH)

73215328E1A 73215328E1B 73215328E2A 73215328E2B

ECU TEMP SENSOR DUAL FAILURE (ENG X SHORT DISPATCH) NOTE: For v5.32 and below, this fault is a "NO DISPATCH" fault

Both FADEC internal temperature sensors are out of the range of T2-11C to T2-33C (varying lower limit) to 340F (171C)

72-00-00-810-720 (SHORT DISPATCH)

73215329E1A 73215329E1B 73215329E2A 73215329E2B

ECU TEMP SENSOR FAULT (NONE) NOTE: For v5.20 and below this fault is a "SHORT DISPATCH" fault

Sensor that monitors the FADEC internal temperature has failed out of the range of T2-11C to T2-33C (varying lower limit) to 340F (171C)

72-00-00-810-209 (LONG DISPATCH)

73215414E1A 73215414E1B 73215414E2A 73215414E2B

S CMD CMD - POSI POSITI TION ON DISAGREE (ENG X CONTROL FAULT) NOTE: For v5.20 and below software CAS Message is "IN FLIGHT ARNING"

The S position is more than 5 percent from the demanded position. The sensor and torque motor values are OK, the sensor has been valid for more than 2.0 seconds

72-00-00-810-210 (NO DISPATCH)

73215415E1A 73215415E1B 73215415E2A 73215415E2B

S SENSOR RANGE FAULT Local channel S (ENG X SHORT DISPATCH) position feedback NOTE: For v5.32 and sensor is out of the below, this fault is a range of -10 to 110 "LONG DISPATCH" fault percent stroke or the voltage sum is out of the range of 6.9-9.3 volts. Cross channel sensor is used

72-00-00-810-721 (SHORT DISPATCH)

73215416E1A 73215416E1B 73215416E2A 73215416E2B

S DUAL DUAL CMD - CURREN CURRENT T DISAGREE (ENG X NO DISPATCH) NOTE: For v5.32 and below, this fault is a "IN FLIGHT ARNING" fault

Dual channel failure in the torque motor driver circuits. S will slew to the FAIL SAFE position

72-00-00-810-727 (NO DISPATCH)

73215417E1A 73215417E1B

S CMD CMD - CURR CURREN ENT T DISAGREE

Single channel failure in the torque

72-00-00-810-213 (SHORT DISPATCH)


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73215417E2A 73215417E2B

(ENG X SHORT SHORT DISPATCH DISPATCH) )

motor motor driver driver circuit circuit

73215418E1A 73215418E1B 73215418E2A 73215418E2B

S DUAL SENSOR RANGE FAULT (ENG X CONTROL FAULT)

Both S position feedback sensors have failed. S position is set to 100 percent CLOSED. S will slew to the FAIL SAFE position

72-00-00-810-214 (IN FLIGHT ARNING)

73215419E1A 73215419E1B 73215419E2A 73215419E2B

S CHAN A-B SENSORS DISAGREE (ENG X NO DISPATCH)

The two S position feedback sensors are in range but disagree by more than 5 percent stroke. Sensor is selected based on rate of change and previously failed sensor

72-00-00-810-215 (NO DISPATCH)

73215420E1A 73215420E1B 73215420E2A 73215420E2B

B CMD - POSITION The B position is DISAG more than 5 percent (ENG X SHORT DISPATCH) from the demanded position. The sensor and torque motor values are OK, the sensor has been valid for more than 2.0 seconds

72-00-00-810-219 (SHORT DISPATCH)

73215421E1A 73215421E1B 73215421E2A 73215421E2B

B SENSOR RANGE FAULT Local channel B (ENG X SHORT DISPATCH) position feedback NOTE: For v5.32 and sensor is out of the below, this fault is a range of -10 to 110 "LONG DISPATCH" fault percent stroke or the voltage sum is out of the range of 6.9-9.3 volts. Cross channel sensor is used

72-00-00-810-722 (SHORT DISPATCH)

73215422E1A 73215422E1B 73215422E2A 73215422E2B

B DUAL CMD - CURRENT Dual channel failure DISAG in the torque motor (ENG X CONTROL FAULT) driver circuits. B will slew to the FAIL SAFE position

72-00-00-810-221 (IN FLIGHT ARNING)

73215423E1A 73215423E1B 73215423E2A 73215423E2B

B CMD - CURRENT Single channel DISAG failure in the torque (ENG X SHORT DISPATCH) motor driver circuit

72-00-00-810-222 (SHORT DISPATCH)

73215424E1A 73215424E1B 73215424E2A 73215424E2B

B DUAL SENSOR RANGE FAULT (ENG X CONTROL FAULT) Note: For v5.20 and below this fault is a "NO DISPATCH" fault

72-00-00-810-223 (IN FLIGHT ARNING)

Both B position feedback sensors have failed. B position is set to 100 percent OPEN. B will slew to the FAIL SAFE position


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73215425E1A 73215425E1B 73215425E2A 73215425E2B

B CHAN A-B SENSORS DISAG (ENG X NO DISPATCH)

The two B position feedback sensors are in range but disagree by more than 10 percent stroke. Sensor is selected based on rate of change and previously failed sensor

72-00-00-810-224 (NO DISPATCH)

73215426E1A 73215426E1B 73215426E2A 73215426E2B

T25 OUT OF RANGE (ENG X NO DISPATCH) NOTE: For v5.32 and below, this fault is a "SHORT DISPATCH" fault

T25 sensor is outside expected limits

72-00-00-810-728 (NO DISPATCH)

73215427E1A 73215427E1B 73215427E2A 73215427E2B

T25 DUAL OUT OF RANGE (ENG X NO DISPATCH)

Both channels of the T25 sensors are out of range

72-00-00-810-217 (NO DISPATCH)

73215428E1A 73215428E1B 73215428E2A 73215428E2B

T25 CHAN A-B INPUTS DISAGREE (ENG X NO DISPATCH)

The two T25 signals differ by more than 50F (10C). Default signal is one closest to T25 model. Fault may be due to single channel fault if occurs at low subidle engine speeds

72-00-00-810-218 (NO DISPATCH)

73215514E1A 73215514E1B 73215514E2A 73215514E2B

HPT CMD - POSIT POSITION ION DISAGREE (NONE)

The HPT position is more than 5 percent from the demanded position. The sensor and torque motor values are OK, the sensor has been valid for more than 2.0 seconds

72-00-00-810-225 (LONG DISPATCH)

73215515E1A 73215515E1B 73215515E2A 73215515E2B

HPT SENSOR RANGE FAULT (NONE)

Local channel HPT position feedback sensor is out of the range of -10 to 110 percent stroke or the voltage sum is out of the range of 4.0 to 6.7 volts. Cross channel sensor is used


73215516E1A 73215516E1B 73215516E2A 73215516E2B

HPT DUAL DUAL CMD CMD - CURREN CURRENT T Dual channel failure DISAG in the torque motor (NONE) driver circuits. HPT will slew to the FAIL SAFE position


73215517E1A

HPT CMD - CURRENT

72-00-00-810 -228

Single channel


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73215517E1B 73215517E2A 73215517E2B

DISAG (NONE)

failure in the HPT torque motor driver circuit

(ECONOMIC DISPATCH)

73215518E1A 73215518E1B 73215518E2A 73215518E2B

HPT DUAL SENSOR RANGE FAULT (NONE)

Both HPT position feedback sensors have failed. HPT position is set to 0.0 percent OPEN. HPT will slew to the FAIL SAFE position

72-00-00-810-229 (LONG DISPATCH)

73215519E1A 73215519E1B 73215519E2A 73215519E2B

HPT SENSORS CHAN A-B DISAGREE (NONE)

The two HPT position feedback sensors are in range but disagree by more than 5 percent stroke. Sensor is selected based on rate of change and previously failed sensor


73215520E1A 73215520E1B 73215520E2A 73215520E2B

TB CMD - POSITION The TB position is DISAGREE more than 5 percent (ENG X NO DISPATCH) from the demanded NOTE: For v5.32 and position. The sensor below, this fault is a and torque motor "SHORT DISPATCH" fault values are OK, the sensor has been valid for more than 2.0 seconds

72-00-00-810-729 (NO DISPATCH)

73215521E1A 73215521E1B 73215521E2A 73215521E2B

TB SENSOR RANGE FAULT (NONE)

Local channel TB position feedback sensor is out of the range of -10 to 110 percent stroke or the voltage sum is out of the range of 4.0-6.7 volts. Cross channel sensor is used

72-00-00-810-232 (LONG DISPATCH)

73215522E1A 73215522E1B 73215522E2A 73215522E2B

TB DUAL CMD - CURRENT DISAGREE (ENG X NO DISPATCH) NOTE: For v5.32 and below, this fault is a "SHORT DISPATCH" fault

Dual channel failure in the torque motor driver circuits. TB will slew to the FAIL SAFE position

72-00-00-810-730 (NO DISPATCH)

73215523E1A 73215523E1B 73215523E2A 73215523E2B

TB CMD - CURRENT DISAGREE (NONE)

Single channel failure in the torque motor driver circuit

72-00-00-810-234 (LONG DISPTACH)

73215524E1A 73215524E1B 73215524E2A 73215524E2B

TB DUAL SENSOR RANGE Both TB position FAULT feedback sensors have (ENG X NO DISPATCH) failed. Default TB NOTE: For v5.32 and position of 100 below, this fault is a percent is assigned.

72-00-00-810-731 (NO DISPATCH)


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"SHORT "SHORT DISPA DISPATCH" TCH" fault fault

TBV will slew to the the FAIL SAFE position

73215525E1A 73215525E1B 73215525E2A 73215525E2B

TBV SENSORS CHAN A-B DISAGREE (ENG X SHORT DISPATCH)

The two TBV position feedback sensors are in range but disagree by more than 5 percent stroke. Sensor is selected based on rate of change and previously failed sensor

72-00-00-810-236 (SHORT DISPATCH)

73215526E1A 73215526E1B 73215526E2A 73215526E2B

T3 OUT OF RANGE (NONE)

T3 sensor is outside expected limits. Fault inhibited when engine not running or subidle

72-00-00-810-237 (LONG DISPTACH)

73215527E1A 73215527E1B 73215527E2A 73215527E2B


Both of the T3 sensors are out of range. Fault is inhibited until the engine is close to idle or above

72-00-00-810-238 (NO DISPATCH)

73215528E1A 73215528E1B 73215528E2A 73215528E2B

T3 CHAN A-B INPUTS DISAGREE (ENG X SHORT DISPATCH)

The two T3 signals differ by more than 132.1ºF (55.6ºC). Weighted averaging starts at 27.8º delta. Default signal is one closest to T3 model. Fault inhibited when engine not running or subidle

72-00-00-810-239 (SHORT DISPATCH)

73215614E1A 73215614E1B 73215614E2A 73215614E2B

HPTACC TC OUT OF RANGE (NONE)

HPTACC TC sensor is outside expected limits


73215615E1A 73215615E1B 73215615E2A 73215615E2B

HPTACC TC DUAL OUT OF RANGE (NONE)

Both of the HPTACC TC sensors are out of range

72-00-00-810-241 (LONG DISPATCH)

73215616E1A 73215616E1B 73215616E2A 73215616E2B

HPTACC TC CHAN A-B DISAGREE (NONE)

The two HPTACC TC signals differ by more than 40.0ºC. Weighted averaging starts at 30.0º delta. Minimum sensor value is used as default


73215617E1A 73215617E1B 73215617E2A

DP3 SENSOR OUT OF RANGE (NONE)

DP3 sensor is outside expected limits. Fault inhibited when

72-00-00-810-243 (LONG DISPATCH)


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7 321 5 617 E2B

H PS OV is C LO SE D and DP3 is less than 0.0 PSID

73215618E1A 73215618E1B 73215618E2A 73215618E2B

DP3 SENSOR DUAL OUT OF RANGE (ENG X NO DISPATCH)

Both of the DP3 sensors are out of range. Fault inhibited when HPSOV is CLOSED and DP3 less than 0.0 PSID

72-00-00-810-244 (NO DISPATCH)

73215619E1A 73215619E1B 73215619E2A 73215619E2B

DP3 CHAN A-B SENSORS DISAGREE (ENG X NO DISPATCH) NOTE: For v5.32 and below, this fault is a "SHORT DISPATCH" fault

The two DP3 signals differ by more than 8.0 PSID (55.2 kPa). Default signal is one closest to DP3 model. Fault inhibited when HPSOV is CLOSED

72-00-00-810-732 (NO DISPATCH)

73215620E1A 73215620E1B 73215620E2A 73215620E2B

FMU NULL BIAS SHIFT (NONE)

The FMU null biases for both the VSV and FMV have drifted from nominal such that an engine overspeed condition may occur if the FADEC were to lose electrical power while the engine was running at full thrust

72-00-00-810-246 (LONG DISPATCH)

73216014E1A 73216014E1B 73216014E2A 73216014E2B

NO.1 BEARING ACCEL FAULT (NONE) NOTES: For v5.32 this fault is an "ECONOMIC DISPATCH" fault For v5.20 and below, this fault is a "SHORT DISPATCH" fault

Both IEVM outputs for the front accelerometer are invalid. ARINC communications communications is O and at least 1 rear accelerometer signal is O

72-00-00-810-739 (LONG DISPATCH)

73216015E1A 73216015E1B 73216015E2A 73216015E2B

REAR ACCELEROMETER Both IEVM outputs for FAULT the rear (ENG X SHORT DISPATCH) accelerometer are invalid. ARINC communications communications is O and at least 1 front accelerometer signal is O

72-00-00-810-020 (SHORT DISPATCH)

73216016E1A 73216016E1B 73216016E2A 73216016E2B

ADS 1-2 INPUT FAULT (NONE)

All inputs from ADS 1 and ADS 2 are faulted or are out of range. Other ARINC inputs are being received

72-00-00-810-021 (LONG DISPATCH)

73216017E1A 73216017E1B

ADS 1 INPUT FAULT (NONE)

All inputs from ADS 1 are faulted or are

72-00-00-810-022 (LONG DISPATCH)


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73216017E2A 73216017E2B

out of range. Other ARINC inputs are being received

73216018E1A 73216018E1B 73216018E2A 73216018E2B


All inputs from ADS 2 are faulted or are out of range. Other ARINC inputs are being received

72-00-00-810-023 (LONG DISPATCH)

73216019E1A 73216019E1B 73216019E2A 73216019E2B

NO.1 BEARING ACCEL OFF DUE TO ECP CONFIG (NONE)

ECP Configuration for defective front accelerometer is in use. Scaled rear accelerometer will be used.


73216020E1A 73216020E1B 73216020E2A 73216020E2B

MULTIPLE FAILURES DETECTED (ENG X NO DISPATCH)

Combination of faults were detected on FADEC channel A and B. Clear multiple short time dispatch faults to clear this fault

72-00-00-810-024 (NO DISPATCH)

73216021E1A 73216021E1B 73216021E2A 73216021E2B

RADIO ALTIMETER 1 INPUT FAULT (NONE)

The radio altimeter input No. 1 is invalid (on receiver 1 and 3), but other ARINC inputs are being received

72-00-00-810-025 (LONG DISPATCH)

73216024E1A 73216024E1B 73216024E2A 73216024E2B

ATS SPDA 2 CIRCUIT FAULT (ENG X START VLV OPEN)

SPDA is supplying power to the ATS unexpectedly


73216026E1A 73216026E1B 73216026E2A 73216026E2B

ATS SPDA 2 MONITOR OFF FAULT (NONE)

ATS solenoid voltage monitor indicates no voltage and N2 indicates the engine is starting

72-00-00-810-029 (LONG DISPATCH)

73216027E1A 73216027E1B 73216027E2A 73216027E2B

ATS SPDA 2 MONITOR ON FAULT (NONE)

The ATS solenoid voltage monitor (monitored in SPDA 2) is always detecting that voltage is being sent to the starter

72-00-00-810-030 (LONG DISPATCH)

73216028E1A 73216028E1B 73216028E2A 73216028E2B

ATS VALVE FAILD OPEN (ENG X START VLV OPEN)

Air Turbine Starter valve is stuck OPEN, as the feedback switch is O and it indicates that the valve has not CLOSED when commanded


73216029E1A 73216029E1B

ICE DETECTOR INPUTS FAULT

ARINC inputs to the FADEC indicate that



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73216029E2A 73216029E2B

( NON E )

the en g ine has reached idle and both of the ice detectors have failed for this engine

73216114E1A 73216114E1B 73216114E2A 73216114E2B

ATS SWITCH FAILED CLOSED (NONE)

The ATS switch is detected as failed CLOSED as the starter is energized and the engine is starting, but the switch is indicating the valve is CLOSED

72-00-00-810-033 (LONG DISPATCH)

73216115E1A 73216115E1B 73216115E2A 73216115E2B

ECS BLEED ON FAULT The FADEC has (ENG X SHORT DISPATCH) requested the ECS to be off, but FADEC inputs indicate that bleed air is flowing. Aircraft must be airborne and be below 15,000 feet

72-00-00-810-034 (SHORT DISPATCH)

73216116E1A 73216116E1B 73216116E2A 73216116E2B

BCM INPUT FAULT (NONE)

The Brake Control Module inputs have failed, the wheel speed is unknown but other ARINC inputs are being received and the engine is running

72-00-00-810-035 (LONG DISPATCH)

73216117E1A 73216117E1B 73216117E2A 73216117E2B

FADEC INTERNAL XTAL FAULT (ENG X NO DISPATCH)

The local FADEC channel cannot receive serial data from the other FADEC channel

72-00-00-810-036 (NO DISPATCH)

73216118E1A 73216118E1B 73216118E2A 73216118E2B

FADEC CHANNEL ID FAULT (ENG X NO DISPATCH)

The channel ID inputs disagree, cannot determine if the local channel is A or B. Interferes with channel-in-control selection logic, CMC interactions

72-00-00-810-037 (NO DISPATCH)

73216119E1A 73216119E1B 73216119E2A 73216119E2B

CMC INPUT FAULT (NONE)

Loss of the CMC input has been detected. The CMC will not report maintenance faults. No CMC initiated tests can be performed


73216120E1A 73216120E1B 73216120E2A

IGNITION A MONITOR FAULT (NONE)

The EICC output ("Ignition A Rly Status" on SPDA)

72-00-00-810-039 (LONG DISPATCH)


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7 321 6 120 E2B

i nd ic ate s th e ig nit or was not energized, but the engine lit off

73216121E1A 73216121E1B 73216121E2A 73216121E2B

ROLLBAC (ENG X FAIL)

The engine has been running, but core speed (N2) has dropped below idle unexpectedly

72-00-00-810-040 IN FLIGHT WARNING

73216122E1A 73216122E1B 73216122E2A 73216122E2B

IGNITION B MONITOR FAULT (NONE)

The SPDA output indicates the ignitor was not energized (SPDA monitors the output voltage supplied to the igniters), but the engine lit off

72-00-00-810-041 (LONG DISPATCH)

73216123E1A 73216123E1B 73216123E2A 73216123E2B

ENGINE ID INPUTS DISAGREE (ENG X NO DISPATCH)

Hardwired engine id inputs disagree, local channel is invalid

72-00-00-810-042 (NO DISPATCH)

73216124E1A 73216124E1B 73216124E2A 73216124E2B

ENGINE ENGINE ID ARIN ARINC C - HWRE HWRE Hardwired engine id DISAG inputs agree, but (ENG X NO DISPATCH) disagree with the ARINC input

72-00-00-810-043 (NO DISPATCH)

73216125E1A 73216125E1B 73216125E2A 73216125E2B

ETTS N1 TRIM INPUTS INVALID (NONE)

The N1 TRIM input from the ETTS is invalid and the engine is running. N1 trim function is not available, ARINC is otherwise O

72-00-00-810-044 (LONG DISPATCH)

73216126E1A 73216126E1B 73216126E2A 73216126E2B

FADEC INTERNAL FAULT A FADEC internal (ENG X NO DISPATCH) fault has been NOTE: For v5.32 and detected. Set by: below, this fault is a FADEC Interlock, PSU "SHORT DISPATCH" fault High Voltage ShutDown, AIP Local channel processor, High Side Relay Fault, Basic Computer Fault, Channel ID Fault, ARINC internal wrap fault

72-00-00-810-733 (NO DISPATCH)

73216127E1A 73216127E1B 73216127E2A 73216127E2B

FADEC CPU FAULT (ENG X NO DISPATCH)

72-00-00-810-046 (NO DISPATCH)

Set for FADEC internal failures that cause incorrect results, but the channel is healthy enough to transmit ARINC. (Caused by AIP or CPU failures of:


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Dated 05/31/2013


WDM, CPU Instruction Test, Scratchpad Memory, Program Memory, NVM Adjustments, Adjustments, Dual Port RAM.) 73216128E1A 73216128E1B 73216128E2A 73216128E2B

FADEC INTERLOCK FAULT (NONE)

One or both of the FADEC reprogramming reprogramming lockouts have failed

72-00-00-810-047 (LONG DISPATCH)

73216129E1A 73216129E1B 73216129E2A 73216129E2B

FADEC DUAL CHANNEL FADEC internal OVTMP temperature has (ENG X FADEC OVERTEMP) exceeded 248ºF (120ºC)


73216214E1A 73216214E1B 73216214E2A 73216214E2B

FADEC SINGLE CHANNEL OVTMP (ENG X NO DISPATCH)

FADEC internal temperature has exceeded 248ºF (120ºC) on a single channel only

72-00-00-810-049 (NO DISPATCH)

73216215E1A 73216215E1B 73216215E2A 73216215E2B

FADEC HI VOLT SHUTDOWN FAULT (ENG X SHORT DISPATCH)

Power supply's high voltage disconnect has failed Built In Test (BIT) test

72-00-00-810-054 (SHORT DISPATCH)

73216216E1A 73216216E1B 73216216E2A 73216216E2B

GMO SW INPUTS CHAN A-B The two inputs from DISAG the GMO (for thrust (NONE) reverser test) switch NOTE: For v5.32 and disagree below, this fault is a "LONG DISPATCH" fault


73216218E1A 73216218E1B 73216218E2A 73216218E2B

START ABORT (HOT) (NONE)

Engine start has aborted due to an ITT over temperature condition

72-00-00-810-056 (MAINT. INF. MSGS)

73216219E1A 73216219E1B 73216219E2A 73216219E2B

FADEC DUAL CTRL RELAY FAULT (ENG X NO DISPATCH)

The FADECs high side relays have failed OPEN on both channels. Fault is set if the over current fault is set or if both the TR DCU and ICU relays were detected OPEN during the ground start BIT test. The FADEC cannot energize the overspeed solenoid, hardwired ignitor, and reverser

72-00-00-810-057 (NO DISPATCH)

73216220E1A 73216220E1B 73216220E2A 73216220E2B

FADEC CTRL RELAY OPEN FAULT (ENG X SHORT DISPATCH)

The relay source (high side) contacts have been detected as failed OPEN on the

72-00-00-810-058 (SHORT DISPATCH)


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local channel. Fault is set if the over current fault is set or if both the TR DCU and ICU relays were detected OPEN during the ground start BIT testing 73216221E1A 73216221E1B 73216221E2A 73216221E2B

START ABORT (HUNG) (NONE)

The engine has failed to accelerate to idle in the allotted time. May be due to low starter air pressure, worn starter or engine problems

72-00-00-810-050 (MAINT. INF. MSGS)

73216222E1A 73216222E1B 73216222E2A 73216222E2B

IEVM INPUT FAULT (ENG X NO DISPATCH)

The ARINC input labels carrying the vibration signals for exceedance checking are all invalid

72-00-00-810-051 NO DISPATCH

73216223E1A 73216223E1B 73216223E2A 73216223E2B

IGNITION A DISCRETE FAULT (NONE)

The hardwired ignition connection between the FADEC channel A and the SPDA is OPEN circuit

72-00-00-810-052 (LONG DISPATCH)

73216224E1A 73216224E1B 73216224E2A 73216224E2B

IGNITION B DISCRETE FAULT (NONE)

The hardwired ignition connection between the FADEC channel B and the SPDA is OPEN circuit

72-00-00-810-053 (LONG DISPATCH)

73216225E1A 73216225E1B 73216225E2A 73216225E2B

IGNITION A-B DISCRETE The hardwired FAULT ignition connections (ENG X SHORT DISPATCH) between the FADEC and the SPDA are OPEN circuit

72-00-00-810-059 (SHORT DISPATCH)

73216226E1A 73216226E1B 73216226E2A 73216226E2B

IGNITION SW OFF INPUTS DISAG (NONE)

The two inputs for cockpit ignition switch being "OFF" disagree

72-00-00-810-060 (LONG DISPATCH)

73216227E1A 73216227E1B 73216227E2A 73216227E2B

IGNITION SW ON INPUTS DISAG (NONE)

The two inputs for cockpit ignition switch being ON disagree

72-00-00-810-061 (LONG DISPATCH)

73216228E1A 73216228E1B 73216228E2A 73216228E2B

IGN SW ON AND OFF INPUTS ON (ENG X SHORT DISPATCH)

The cockpit switch for ignition inputs are set to OFF and ON at the same time

72-00-00-810-062 (SHORT DISPATCH)

73216229E1A 73216229E1B 73216229E2A 73216229E2B

IGNITION A POWER FAULT The SPDA 1 has (ENGINE X NO DISPATCH) reported a loss of power supplied to ignitor A. Ignitor A

72-00-00-810-063 (NO DISPATCH)


Page 17 of 72


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was commanded to be energized. This fault could be set by a failure of the SPDA 1 excitor monitor sensor 73216314E1A 73216314E1B 73216314E2A 73216314E2B

IGNITOR A NO LIGHT OFF (ENG X NO DISPATCH)

The engine did not start while using ignitor A (it will then use ignitor B.). There were no other detected contributing ignition faults. The ignition system is the probable cause (excitor, ignitor)

72-00-00-810-064 (NO DISPATCH)

73216315E1A 73216315E1B 73216315E2A 73216315E2B

IGNITORS A-B NO LIGHT OFF (ENG X NO DISPATCH)

The engine did not start when both ignition systems were tried. There were no other detected contributing contributing ignition or fuel system faults. The ignition system is the probable cause (excitor, ignitor)

72-00-00-810-065 (NO DISPATCH)

73216316E1A 73216316E1B 73216316E2A 73216316E2B

ARINC T/R COMM FAULT (ENG X NO DISPATCH)

Either FADEC input ARINC label 244 or label 250 is missing. The FADEC is receiving other ARINC inputs OK

72-00-00-810-273 (NO DISPATCH)

73216317E1A 73216317E1B 73216317E2A 73216317E2B

IGNITION B POWER FAULT The SPDA 2 has (ENG X SHORT DISPATCH) reported a loss of power supplied to ignitor B. Ignitor B was commanded to be energized. This fault could be set by a failure of the SPDA 2 excitor monitor sensor

72-00-00-810-067 (SHORT DISPATCH)

73216318E1A 73216318E1B 73216318E2A 73216318E2B

IGNITOR B NO LIGHT OFF (ENG X SHORT DISPATCH)

72-00-00-810-068 (SHORT DISPATCH)

The engine did not start while using ignitor B (it will then use ignitor A). There were no other detected contributing ignition faults. The ignition system is the probable cause (excitor, ignitor)


Page 18 of 72


Revision No. 29

Dated 05/31/2013


73216319E1A 73216319E1B 73216319E2A 73216319E2B

MACH OUT OF RANGE (ADS1) (NONE)

The mach number inputted from ARINC from ADS1 has not been received or is out of range. Ground, the limits are -0.12 to 0.409 (altitude dependant). Airborne, the limits are 0.0 to 0.97 (altitude dependant) for 5 seconds

72-00-00-810-069 (LONG DISPATCH)

73216320E1A 73216320E1B 73216320E2A 73216320E2B



72-00-00-810-070 (LONG DISPATCH)

73216321E1A 73216321E1B 73216321E2A 73216321E2B

MACH INPUT FAULT (ADS1-2) (NONE)

Both mach numbers inputted from ARINC from ADS1 and ADS2 have not been received or are out of range. Ground, the limits are -0.12 to 0.409 (altitude dependant). Airborne, the limits are 0.0 to 0.97 (altitude dependant) for 30 seconds

72-00-00-810-071 (LONG DISPATCH)

73216322E1A 73216322E1B 73216322E2A 73216322E2B

T/R SPDA (COWL LOCK) OUTPUT (ENG X REV FAIL)

The SPDA output to energize the TRAS cowl lock is not being turned on


73216323E1A 73216323E1B 73216323E2A 73216323E2B

INTERNAL FADEC FAULT The FADEC is unable (ENG X CONTROL FAULT) to process the local NOTE: For v5.20 and and cross channel below, this fault is a sensor inputs "LONG TIME DISPATCH" fault


73216324E1A 73216324E1B 73216324E2A 73216324E2B

N1 OUT OF RANGE (ENG X SHORT DISPATCH) NOTE: For v5.32 and below, this fault is a "LONG DISPATCH" fault

72-00-00-810-723 (SHORT DISPATCH)

Local channel N1 sensor is invalid or out of range of 10 to 125 percent when N1 should be more than 10 percent based on


Page 19 of 72


Revision No. 29

Dated 05/31/2013


other parameters. Fault inhibited when engine not running or subidle 73216325E1A 73216325E1B 73216325E2A 73216325E2B

N1 DUAL OUT OF RANGE (ENG X CONTROL FAULT) NOTE: For v5.20 and below, this fault is a "NO DISPATCH" fault

Both N1 sensors are invalid or out of range. A computed value is used that is calculated from N2, T12, Mach Number


73216326E1A 73216326E1B 73216326E2A 73216326E2B

N1 CHAN A-B INPUTS DISAGREE (ENG X NO DISPATCH)

The N1 sensor inputs are valid but disagree by more than 5 percent. Rate of change and result of previous range tests are used to isolate the invalid signal. Fault inhibited when engine not running or subidle

72-00-00-810-075 (NO DISPATCH)

73216327E1A 73216327E1B 73216327E2A 73216327E2B

N2 PMA DUAL OUT OF No valid N2 signals RANGE exist from the (ENG X CONTROL FAULT) alternator NOTE: For v5.20 and below, this fault is a "NO DISPATCH" fault


73216328E1A 73216328E1B 73216328E2A 73216328E2B

N2 ALTERNATOR OUT OF The local channel N2 RANGE alternator signal is (ENG X SHORT DISPATCH) out of the allowable range of 5-130 percent when N2 should be more than 5 percent based on other parameters. Fault inhibited when engine not running or subidle

72-00-00-810-077 (SHORT DISPATCH)

73216329E1A 73216329E1B 73216329E2A 73216329E2B

N2 ALTERNATOR INPUTS The two N2 alternator DISAGREE inputs from the (ENG X SHORT DISPATCH) alternator are valid but disagree by more than 1.2 percent. Rate of change and result of previous range tests are used to isolate the invalid signal. Fault inhibited when engine not running or subidle

72-00-00-810-078 (SHORT DISPATCH)

73216414E1A 73216414E1B

THRUST CONTROL MALFUNCTION


The measured fan speed exceeds the


Page 20 of 72


Revision No. 29

Dated 05/31/2013


73216414E2A 73216414E2B

( E N G X F A IL )

com man d ed f an spe e d plus 6 percent margin. An engine shutdown occurs for this condition when on the ground and not at take-off

73216415E1A 73216415E1B 73216415E2A 73216415E2B

N2 ALTERNATOR-FUEL PUMP DISAG (ENG X NO DISPATCH)

The N2 inputs from the fuel pump are valid but disagree with the valid N2 inputs from the alternator by more than 1.2 percent

72-00-00-810-079 (NO DISPATCH)

73216416E1A 73216416E1B 73216416E2A 73216416E2B

N2 FUEL PUMP DUAL OUT OF RNG (ENG X NO DISPATCH)

Both N2 signals from the main fuel pump are invalid or out of the allowable range of 5-130 percent when N2 should be more than 5 percent based on other parameters

72-00-00-810-080 (NO DISPATCH)

73216417E1A 73216417E1B 73216417E2A 73216417E2B

N2 FUEL PUMP OUT OF RANGE (ENG X SHORT DISPATCH)

The local channel N2 signal from the main fuel pump is out of the allowable range of 5-130 percent when N2 should be more then 5 percent based on other parameters. Fault inhibited when engine not running or subidle

72-00-00-810-081 (SHORT DISPATCH)

73216418E1A 73216418E1B 73216418E2A 73216418E2B

N2 FUEL PUMP INPUTS The two N2 inputs DISAGREE from the fuel pump (ENG X SHORT DISPATCH) are valid but disagree by more than 1.2 percent. Rate of change and result of previous range tests are used to isolate the invalid signal. Fault inhibited when engine not running or subidle

72-00-00-810-082 (SHORT DISPATCH)

73216425E1A 73216425E1B 73216425E2A 73216425E2B

OVERSPEED TEST FAULT (ENG X SHORT DISPATCH)

72-00-00-810-083 (SHORT DISPATCH)

Overspeed system failed electrical test. Test is performed at idle and again when TLA is advanced from ground idle and 40 sec. after landing


Page 21 of 72


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Dated 05/31/2013


73216426E1A 73216426E1B 73216426E2A 73216426E2B

OVERSPEED DUAL TEST FAULT (ENG X NO DISPATCH) Note: For v5.20 and below software, this fault is a "Maintenance Information Message" fault

Combination of faults 72-00-00-810-343 were detected on (NO DISPATCH) FADEC channel A and B resulting in dual channel loss of overspeed protection. Clear short term N2 ore overspeed electrical test faults to clear this fault

73216427E1A 73216427E1B 73216427E2A 73216427E2B

OVERSPEED SHUTDON TEST FAULT (ENG X NO DISPATCH)

Overspeed system failed engine shutdown test, the engine has not flamed out after 2 seconds of commanding the overspeed solenoid to shut off fuel

72-00-00-810-084 (NO DISPATCH)

73216428E1A 73216428E1B 73216428E2A 73216428E2B

N2 OVERSPEED (ENG X FAIL)

N2 has exceeded the overspeed trip limit of 102 percent (Aircraft ) engine shutdown is commanded

72-00-00-810-085 (IN FLIGHT ARNING)

73216429E1A 73216429E1B 73216429E2A 73216429E2B

P0 OUT OF RANGE (ADS 1-2) (NONE)

Both ADS P0 inputs have failed

72-00-00-810-086 (LONG DISPATCH)

73216515E1A 73216515E1B 73216515E2A 73216515E2B

PO ALL INPUTS FAULT (ENG X CONTROL FAULT)

All PO signals have failed

72-00-00-810-087 (IN FLIGHT ARNING)

73216516E1A 73216516E1B 73216516E2A 73216516E2B

PO OUT OF RANGE (FADEC) (ENG X NO DISPATCH)

Local channel PO engine sensor is out of the range of 1.816.8 PSIA (12.4-115.8 kPa)

72-00-00-810-088 (NO DISPATCH)

73216517E1A 73216517E1B 73216517E2A 73216517E2B

PO DUAL OUT OF RANGE (FADEC) (ENG X NO DISPATCH)

Both engine P0 sensors are out of the range of 1.8-16.8 PSIA (12.4-115.8 kPa)

72-00-00-810-089 (NO DISPATCH)

73216518E1A 73216518E1B 73216518E2A 73216518E2B

PO - ADS DISAGREE (NONE)

ADS P0 inputs disagree with the ENGINE P0 inputs

72-00-00-810-090 (LONG DISPATCH)

73216519E1A 73216519E1B 73216519E2A 73216519E2B

PO INPUTS DISAGREE (FADEC) (ENG X NO DISPATCH)

The two FADEC P0 sensors disagree by more than 0.4 PSIA (2.8 kPa)

72-00-00-810-091 (NO DISPATCH)

73216520E1A 73216520E1B

PO OUT OF RANGE (ADS1) (NONE)

P0 from the ADS1 sensor is out of the

72-00-00-810-092 (LONG DISPATCH)


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73216520E2A 73216520E2B

range of 3.88 to 34.2 inches of mercury (1.8 to 16.8 PSIA)

73216521E1A 73216521E1B 73216521E2A 73216521E2B

PO OUT OF RANGE (ADS2) (NONE)

P0 from the ADS2 sensor is out of the range of 3.88 to 34.2 inches of mercury (1.8 to 16.8 PSIA)

72-00-00-810-093 (LONG DISPATCH)

73216522E1A 73216522E1B 73216522E2A 73216522E2B

TLA DUAL SIGNAL OUT OF RANGE (ENG X TLA FAIL)

Both of the Thrust Lever Angle (TLA) sensors are invalid or signals are out of range of -4.5 to 88 degrees or the RVDT sum voltages are out of allowable range of 6.65 to 8.06 volts. A variable default value is used for TLA after 0.096 seconds of failure

72-00-00-810-094 (IN FLIGHT ARNING)

73216523E1A 73216523E1B 73216523E2A 73216523E2B

TLA SIGNALS OUT OF RANGE (ENG X NO DISPATCH)

Local channel Thrust Lever Angle (TLA) sensor is invalid or out of range of -4.5 to 88 degrees or the RVDT sum voltage is out of allowable range of 6.65 to 8.06 volts

72-00-00-810-095 (NO DISPATCH)

73216524E1A 73216524E1B 73216524E2A 73216524E2B

TLA SIGNALS DISAGREE (ENG X NO DISPATCH)

The TLA sensor inputs disagree by more than 3.75 Degrees. Rate of change (160 Deg/0.016 second interaction) interaction) and result of previous range tests are used to isolate the invalid signal

72-00-00-810-096 (NO DISPATCH)

73216526E1A 73216526E1B 73216526E2A 73216526E2B

PMA LO POER OUTUP (ENG X SHORT DISPATCH)

N2 from the pump is O and more than 75 percent and power is being drawn from the aircraft (28V) OR N2 from the pump is O and more than 50 percent and at least one PMA phase has been detected as OPEN circuit

72-00-00-810-097 (SHORT DISPATCH)

73216527E1A 73216527E1B 73216527E2A

PS3 DUAL SENSORS FAULT Dual channel PS3 (ENG X CONTROL FAULT) sensor failure detected

72-00-00-810-098 (IN FLIGHT ARNING)


Page 23 of 72


Revision No. 29

Dated 05/31/2013


73216527E2B 73216528E1A 73216528E1B 73216528E2A 73216528E2B

FADEC PS3 OUT OF RANGE (ENG X SHORT DISPATCH) NOTE: For v5.32 and below, this fault is a "LONG DISPATCH" fault

PS3 sensor is failed if the value is outside the computed range. Minimum limit is 1.0 or P0-4.0 PSIA (whichever is greater). Maximum limit is PS3 more than 520 (N2 is more than 90) or 620 (N2 is more than 91) PSIA. Engine is operating where parameters should be within limits

72-00-00-810-724 (SHORT DISPATCH)

73216529E1A 73216529E1B 73216529E2A 73216529E2B

FADEC PS3 LINE BROEN FAULT (NONE)

The PS3 line is detected as broken

72-00-00-810-362

73216614E1A 73216614E1B 73216614E2A 73216614E2B

PS3 INPUTS DISAGREE (ENG X NO DISPATCH) NOTE: For v5.32 and below, this fault is a "SHORT DISPATCH" fault

The two PS3 sensors disagree by more than 16 PSIA (110 kPa). PS3 is weighted averaged starting at 8 PSIA (55 kPa) delta. Failsafe value is 47.0 PSIA (324.1 kPa). Fault isolation is based on past failure and excitation faults

72-00-00-810-734 (NO DISPATCH)

73216615E1A 73216615E1B 73216615E2A 73216615E2B

PSEM DUAL INPUTS FAULT (NONE) NOTE: For v5.20 and below this fault is a "SHORT TIME DISPATCH" fault

Both of the landing gear proximity sensor computers have failed with the engine running, no Os signal is available

72-00-00-810-101 (LONG DISPATCH)

73216616E1A 73216616E1B 73216616E2A 73216616E2B

PSEM 1 INPUT FAULT (NONE)

Landing gear proximity sensor computer 1 has failed with the engine running

72-00-00-810-102 (LONG DISPATCH)

73216617E1A 73216617E1B 73216617E2A 73216617E2B



72-00-00-810-103 (LONG DISPATCH)

73216618E1A 73216618E1B 73216618E2A 73216618E2B

MAU ARINC INPUTS FAULT (ENG X SHORT DISPATCH)

This channel has no ARINC inputs from the aircraft

72-00-00-810-104 (SHORT DISPATCH)


Page 24 of 72


Revision No. 29

Dated 05/31/2013


73216619E1A 73216619E1B 73216619E2A 73216619E2B

MAU ARINC BUS RX 1 FAULT (NONE)

ARINC receiver 1 (supplies aircraft data) has failed. N2 must be more than 10 percent

72-00-00-810-105 (LONG DISPATCH)

73216620E1A 73216620E1B 73216620E2A 73216620E2B

FADEC ARINC XENG FAULT (ENG X NO DISPATCH)

This channel has no ARINC inputs from the opposite (cross) engine. N2 must be more than 10 percent

72-00-00-810-106 (NO DISPATCH)

73216621E1A 73216621E1B 73216621E2A 73216621E2B

FADEC ARINC BUS RX 2 FAULT (NONE)

ARINC receiver 2 (supplies cross engine data) has failed. N2 must be more than 10 percent

72-00-00-810-107 (LONG DISPATCH)

73216622E1A 73216622E1B 73216622E2A 73216622E2B



72-00-00-810-108 (LONG DISPATCH)

73216623E1A 73216623E1B 73216623E2A 73216623E2B



72-00-00-810-109 (LONG DISPATCH)

73216624E1A 73216624E1B 73216624E2A 73216624E2B

SLAT/FLAP - ACE INPUT FAULT (NONE)

The ARINC input from the slat/flap angle computer is invalid and the engine is running

72-00-00-810-110 (LONG DISPATCH)

73216714E1A 73216714E1B 73216714E2A 73216714E2B

START AND STOP S INPUTS ON (NONE)

Both start switch and stop switch inputs are on at the same time

72-00-00-810-111 (LONG DISPATCH)

73216716E1A 73216716E1B 73216716E2A 73216716E2B

START S ON INPUTS DISAGREE (NONE)

The start switch inputs disagree

72-00-00-810-112 (LONG DISPATCH)

73216717E1A 73216717E1B 73216717E2A 73216717E2B

START S ON AT POER The start switch was UP in the "start" (ENG X SHORT DISPATCH) position when the FADEC powered up

72-00-00-810-113 (SHORT DISPATCH)

73216718E1A 73216718E1B 73216718E2A 73216718E2B

FADEC SOFTARE VERSIONS DISAG (ENG X NO DISPATCH)

72-00-00-810-114 (NO DISPATCH)

The software versions on the two channels in the FADEC are different, giving different control functionality depending on the channel in control. Possibly due to an


Page 25 of 72


Revision No. 29

Dated 05/31/2013


aborted reprogramming procedure 73216721E1AN 73216721E1B 73216721E2A 73216721E2B

T12 ALL INPUTS FAULT All T12 signals have (ENG X CONTROL FAULT) failed. The TAT NOTE: For v5.20 and inputs and T12 engine below, this fault is a sensors failed "NO DISPATCH" fault


73216722E1A 73216722E1B 73216722E2A 73216722E2B


The local channel engine T12 sensor is out of the range of 100 to 199ºF (-73 to 93ºC)

72-00-00-810-116 (LONG DISPATCH)

73216723E1A 73216723E1B 73216723E2A 73216723E2B


Both of the engine T12 sensors are out of the range of -99.4 to 199.4ºF (-73 to 93ºC)

72-00-00-810-117 (NO DISPATCH)

73216724E1A 73216724E1B 73216724E2A 73216724E2B

T12 T12 ADS ADS - FADE FADEC C DISAGREE (NONE)

T12 engine sensors disagree with the aircraft TAT sensors when the aircraft is in flight or the speed is greater than 0.2 MN. Fault inhibited when engine not running or subdile

72-00-00-810-118 (LONG DISPATCH)

73216725E1A 73216725E1B 73216725E2A 73216725E2B

T12 CHAN A-B INPUTS DISAGREE (ENGINE X SHORT DISPATCH)

The channels A and B T12 sensors disagree by more than 5.56ºC. Signal selection is based on rate of change of T12 and any previous range fault. NOTE: Do not convert 5.56ºC to ºF because in this case, the temperature conversion is not a direct ratio from ºC to ºF

72-00-00-810-119 (SHORT DISPATCH)

73217017E1A 73217017E1B 73217017E2A 73217017E2B

ITT DUAL OUT OF RANGE (ENG X NO DISPATCH)

Both of the ITT sensors are out of range. The default value is 2001.2ºF (1094ºC). Fault is inhibited until the engine is close to idle or above

72-00-00-810-120 (NO DISPATCH)

73217018E1A 73217018E1B 73217018E2A

ITT OUT OF RANGE (NONE)

ITT is less than 300ºF (149ºC) or more than 2540.3ºF

72-00-00-810-121 (LONG DISPATCH)


Page 26 of 72


Revision No. 29

Dated 05/31/2013


7 321 7 018 E2B

( 1 3 9 3 . 5 º C ) . F au l t inhibited when engine not running or subidle

73217019E1A 73217019E1B 73217019E2A 73217019E2B

ITT CHAN A-B INPUTS The two ITT signals DISAGREE differ by  55.6ºC. (ENG X SHORT DISPATCH) Weighted averaging starts at 27.8ºC delta. The failsafe value is 1093.5ºC. Fault can be due to single channel fault if occurs at low engine speeds. Fault inhibited when engine not running or subidle. NOTE: Do not convert 55.6ºC to ºF because in this case, the temperature conversion is not a direct ratio from ºC to ºF

72-00-00-810-122 (SHORT DISPATCH)

73217020E1A 73217020E1B 73217020E2A 73217020E2B

TAT OUT OF RANGE (ADS1) (NONE)

TAT from ADS1 is invalid or is out of the range of -99.4ºF to 200.3ºF (-73 to 93.5ºC) when the aircraft is in flight or the speed is more than 0.2 MN

72-00-00-810-123 (LONG DISPATCH)

73217021E1A 73217021E1B 73217021E2A 73217021E2B


TAT from ADS2 is invalid or is out of the range of -99.4ºF to 200.3ºF(-73 to 93.5ºC) when the aircraft is in flight or the speed is more than 0.2 MN

72-00-00-810-124 (LONG DISPATCH)

73217022E1A 73217022E1B 73217022E2A 73217022E2B

TAT OUT OF RANGE (ADS1-2) (NONE)

ADS1 and ADS2 TAT signals are invalid or are out of -99.4ºF to 200.3ºF (-73 to 93.5ºC) when the aircraft is in flight or the speed is more than 0.2 MN

72-00-00-810-125 (LONG DISPATCH)

73217023E1A 73217023E1B 73217023E2A 73217023E2B

T/R MECHANICAL FAIL (ENG X RE FAIL) (ENG X RE DEPLOYED) NOTE: The CAS message displayed will depend

The thrust reverser has a mechanical failure. It has failed somewhere between stowed and



Page 27 of 72


Revision No. 29

Dated 05/31/2013


on whether or not the fault occurred when the T/R was stowed or deployed

deployed

73217024E1A 73217024E1B 73217024E2A 73217024E2B

T/R ACTUATOR DUAL LDT FAULT (ENG X NO DISPATCH)

Both TRAS LDTs are failed, position is nown only by the loc switches TRAS LDT position is set at 50

72-00-00-810-275 (NO DISPATCH)

73217026E1A 73217026E1B 73217026E2A 73217026E2B

T/R ACTUATOR 3 LDT FAULT (NONE)

TRAS actuator 3 LDT is out of the range of -10 to 110 or the voltage sum is not in the range of 4 to 6 volts

72-00-00-810-276 (LONG DISPATCH)

73217027E1A 73217027E1B 73217027E2A 73217027E2B

T/R ACTUATOR 4 LDT FAULT (NONE)

TRAS actuator 4 LDT is out of the range of -10 to 110 or the voltage sum is not in the range of 4 to 6 volts

72-00-00-810-277 (LONG DISPATCH)

73217028E1A 73217028E1B 73217028E2A 73217028E2B

T/R DCU RELAY A FAULT (NONE)

Channel A TRAS DCU relay coil has failed

72-00-00-810-278 (LONG DISPATCH)

73217029E1A 73217029E1B 73217029E2A 73217029E2B

T/R DCU DUAL RELAYS FAULT (ENG X RE FAIL)

The reverser is unavailable due to loss of both DCU control relays


73217114E1A 73217114E1B 73217114E2A 73217114E2B

T/R DCU RELAY B FAULT (NONE)

Channel B TRAS DCU relay coil has failed

72-00-00-810-280 (LONG DISPATCH)

73217115E1A 73217115E1B 73217115E2A 73217115E2B

GMO INPUTS INALID (NONE)

Thrust reverser GMO switches have been detected as being in the wrong state. Set if the GMO was selected at power up for selected (pushed) for more than 2 minutes


73217116E1A 73217116E1B 73217116E2A 73217116E2B

T/R ICU RELAY A FAULT (NONE)

Channel A TRAS ICU relay coil has failed

72-00-00-810-281 (LONG DISPATCH)

73217117E1A 73217117E1B 73217117E2A 73217117E2B

T/R ICU DUAL RELAYS FAULT (ENG X RE FAIL)

The reverser is unavailable due to loss of both ICU control relays



Page 28 of 72


Revision No. 29

Dated 05/31/2013


73217118E1A 73217118E1B 73217118E2A 73217118E2B

T/R ICU RELAY B FAULT (NONE)

Channel B TRAS ICU relay coil has failed

73217119E1A 73217119E1B 73217119E2A 73217119E2B

T/R STOWED LOC SW 1 T/R is stowed, but he FAULT loc switch 1 (ENG X RE PROT FAULT) indicates UNLOCED


73217120E1A 73217120E1B 73217120E2A 73217120E2B

T/R LOC SWITCH DUAL DISAGREE (ENG X NO DISPATCH)

Both reverser locs that the FADEC monitors are OPEN after the reverser is stowed as indicated by the TRAS LDT position sensors

72-00-00-810-285 (NO DISPATCH)

73217121E1A 73217121E1B 73217121E2A 73217121E2B

T/R LOC SWITCH DUAL FAULT (ENG X NO DISPATCH)

Both of the TR loc switches indicate LOCED when the reverser is deployed as indicated by the TRAS LDT position sensors

72-00-00-810-286 (NO DISPATCH)

73217122E1A 73217122E1B 73217122E2A 73217122E2B

T/R DEPLOYED LOC SW 1 The T/R loc 1 FAULT indicates LOCED when (ENG X RE PROT FAULT) the reverser is deployed as indicated by the TRAS LDT position sensors


73217123E1A 73217123E1B 73217123E2A 73217123E2B

T/R STOW LOC SW 2 FAULT (ENG X RE PROT FAULT)


73217124E1A 73217124E1B 73217124E2A 73217124E2B

T/R DEPLOYED LOC WS 2 The T/R loc 2 FAULT indicates LOCED when (ENG X RE PROT FAULT) the reverser is deployed as indicated by the TRAS LDT position sensors


73217125E1A 73217125E1B 73217125E2A 73217125E2B

NLG WOW - WHSPD FAIL TRAS is unavailable (ENG X RE FAIL) due to combination of NOTE: For v5.20 and bad NLG and wheel below, this fault is a speed signals "SHORT DISPATCH" fault


73217126E1A 73217126E1B 73217126E2A 73217126E2B

FADEC MINOR HEALTH The serial and the FAULT parallel versions of (ENG X NO DISPATCH) the cross channel NOTE: For v5.32 and engine health below, this fault is a parameter disagree "SHORT DISPATCH" fault

72-00-00-810-735 (NO DISPATCH)

73217127E1A 73217127E1B

FADEC ECP NM FAULT (ENG X SHORT DISPATCH)

72-00-00-810-146 (SHORT DISPATCH)

T/R is stowed, but the loc switch 2 indicates UNLOCED

A checsum fault in the engine thrust

72-00-00-810-283 (LONG DISPATCH)


Page 29 of 72


Revision No. 29

Dated 05/31/2013


73217127E2A 73217127E2B

rating (NM version) exists

73217128E1A 73217128E1B 73217128E2A 73217128E2B

FADEC GENERAL NM FAULT (ENG X NO DISPATCH)

NM fault has been detected at power up or during GSBIT

72-00-00-810-147 (NO DISPATCH)

73217220E1A 73217220E1B 73217220E2A 73217220E2B

FMU CMD - POSITION DISAGREE (ENG X FAIL) (ENG X NO DISPATCH)

The FMU Metering alve position is more than 5 percent from the demanded position (when NG is greater than 20 percent) or the WF loop position is more than 20 percent from the demanded position. The sensor and torue motor values are valid, the sensor has been valid for more than 2.0 seconds

72-00-00-810-148 (NO DISPATCH)

73217221E1A 73217221E1B 73217221E2A 73217221E2B

FMU SENSOR RANGE FAULT Local channel FMU (ENG X SHORT DISPATCH) Metering alve NOTE: For v5.32 and position feedbac below, this fault is a sensor is out of the "LONG DISPATCH" fault range of -50 to 140 percent stroe or the voltage sum is out of the range of 8.6-12.0 volts. Cross channel sensor is used

72-00-00-810-725 (SHORT DISPATCH)

73217222E1A 73217222E1B 73217222E2A 73217222E2B

FMU DUAL CMD - CURRENT DISAG (ENG X FAIL) (ENG X NO DISPATCH)

Dual channel failure in the torue motor driver circuits. FMU Metering alve will slew to the FAIL SAFE position. ARINC output will be set until the engine drops below 30 percent N2

72-00-00-810-150 (NO DISPATCH)

73217223E1A 73217223E1B 73217223E2A 73217223E2B

FMU CMD - CURRENT Single channel DISAGREE failure in the torue (ENG X SHORT DISPATCH) motor driver circuit

72-00-00-810-151 (SHORT DISPATCH)

73217224E1A 73217224E1B 73217224E2A 73217224E2B

FMU DUAL SENSOR RANGE FAULT (ENG X FAIL)


Both FMU Metering alve position feedbac sensors are out of the range of 50 to 140 percent stroe or the voltage sums are out of the


Page 30 of 72


Revision No. 29

Dated 05/31/2013


range of 8.6 to 12.0 volts. Default value of 100 percent stroke is used. FMU Metering Valve will slew to the FAIL SAFE position 73217225E1A 73217225E1B 73217225E2A 73217225E2B

FMU SENSOR CHAN A-B DISAGREE (ENG X NO DISPATCH)

The two position feedback sensors are in range but disagree by more than 10 percent stroke. Sensor is selected based on rate of change and previously failed sensor

72-00-00-810-153 (NO DISPATCH)

73217226E1A 73217226E1B 73217226E2A 73217226E2B

WOW HARDWIRE - ARINC FAULT (ENG X NO DISPATCH)

All MLG WOW inputs are invalid

72-00-00-810-154 (NO DISPATCH)

73217227E1A 73217227E1B 73217227E2A 73217227E2B

WOW DUAL ARINC FAULT (NONE) NOTE: For v5.20 and below this fault is a "SHORT DISPATCH" fault

Both MLG WOW inputs on ARINC are invalid and the engine is running

72-00-00-810-155 (LONG DISPATCH)

73217228E1A 73217228E1B 73217228E2A 73217228E2B

WOW ARINC DISAGREE (NONE) NOTE: For v5.20 and below this fault is a "SHORT DISPATCH" fault

The two MLG WOW inputs on ARINC are valid, but differ with the engine running

72-00-00-810-156 (LONG DISPATCH)

73217314E1A 73217314E1B 73217314E2A 73217314E2B

WOW HARDWIRE DISAGREE (ENG X NO DISPATCH)

The two MLG WOW inputs from hardware discretes are valid, but differ

72-00-00-810-157 (NO DISPATCH)

73217315E1A 73217315E1B 73217315E2A 73217315E2B

WOW MLG-NLG DISAGREE (NONE)

The WOW inputs from the MLG are valid and agree, and the WOW inputs from the NLG are valid and agree, but the selected MLG and NLG values disagree with the engine running

72-00-00-810-158 (LONG DISPATCH)

73217316E1A 73217316E1B 73217316E2A 73217316E2B

WOW HARDWIRE - ARINC DISAGREE (ENG X NO DISPATCH)

The WOW inputs on ARINC agree and the WOW hardwired inputs are valid and agree, but the ARINC and hardwired inputs differ

72-00-00-810-159 (NO DISPATCH)

73217317E1A 73217317E1B

WOW PSEM 1 ARINC FAULT (NONE)

The WOW input on the ARINC input from PSEM

72-00-00-810-160 (LONG DISPATCH)


Page 31 of 72


Revision No. 29

Dated 05/31/2013


73217317E2A 73217317E2B

1 is invalid and the engine is running

73217318E1A 73217318E1B 73217318E2A 73217318E2B

T/R T/R LVDT LVDT - LOC LOC SW SW DISAGREE (ENG X NO DISPATCH)

One TRAS LVDT has failed out of range. The other TRAS LVDT does not agree with the 2 lock switches when they both indicate that the TRAS is stowed

72-00-00-810-290 (NO DISPATCH)

73217319E1A 73217319E1B 73217319E2A 73217319E2B


The WOW input on the ARINC input from PSEM 2 is invalid and the engine is running

72-00-00-810-162 LONG DISPATCH

73217320E1A 73217320E1B 73217320E2A 73217320E2B

FADEC TCPL SENSOR The local cold FAULT unction temperature (ENG X NO DISPATCH) from the local NOTE: For v5.32 and channel and cross below, this fault is a channel disagree by "SHORT DISPATCH" fault more than 100R (50.5C)

72-00-00-810-736 (NO DISPATCH)

73217321E1A 73217321E1B 73217321E2A 73217321E2B

WOW DUAL NLG FAULT (NONE)

Both NLG WOW inputs on ARINC are invalid and the engine is running

72-00-00-810-164 (LONG DISPATCH)

73217322E1A 73217322E1B 73217322E2A 73217322E2B

WOW NLG1 FAULT (NONE)

The local channel WOW input on ARINC for the NLG 1 sensor is invalid with the engine running

72-00-00-810-165 (LONG DISPATCH)

73217323E1A 73217323E1B 73217323E2A 73217323E2B

WOW NLG DISAGREE (NONE)

The two NLG WOW inputs on ARINC are valid, but differ with the engine running

72-00-00-810-166 (LONG DISPATCH)

73217324E1A 73217324E1B 73217324E2A 73217324E2B

FADEC OTHER CHANNEL FAULT (ENG X SHORT DISPATCH)

The other FADEC channel has been detected as not being able to control the engine

72-00-00-810-167 (SHORT DISPATCH)

73217325E1A 73217325E1B 73217325E2A 73217325E2B



72-00-00-810-168 (LONG DISPATCH)

73217326E1A 73217326E1B 73217326E2A 73217326E2B

IGNITOR A POWER FAILED ON (ENG X SHORT DISPATCH)

Ignition A feedback indicates the Ignitor power is commanded on when the signal selector multiplexer is selecting Ignition

72-00-00-810-169 (SHORT DISPATCH)


Page 32 of 72


Revision No. 29

Dated 05/31/2013


A command via ARINC or ALL. The ignition A power is not commanded on 73217327E1A 73217327E1B 73217327E2A 73217327E2B

IGN A SPDA CMD FEEDBAC FAULT (NONE)

Ignition feedback indicates ignitor A is off when commanding ignition A power on. Fault is set when commanding via ARINC

72-00-00-810-170 (LONG DISPATCH)

73217328E1A 73217328E1B 73217328E2A 73217328E2B

IGNITION A RELAY FAIL ON (NONE)

Ignition A feedback indicates the Ignitor power is on when the signal selector multiplexer is selecting relay power for A. The ignition A power is not commanded on

72-00-00-810-171 (LONG DISPATCH)

73217329E1A 73217329E1B 73217329E2A 73217329E2B

IGNITOR B POWER FAILED ON (ENG X SHORT DISPATCH)

Ignition B feedback indicates the Ignitor power is commanded on when the signal selector multiplexer is selecting Ignition B command via ARINC or ALL. The ignition B power is not commanded on

72-00-00-810-172 (SHORT DISPATCH)

73217414E1A 73217414E1B 73217414E2A 73217414E2B

IGN B SPDA CMD FEEDBAC FAULT (NONE)

Ignition feedback indicates ignitor B is off when commanding ignition B power on. Fault is set when commanding via ARINC

72-00-00-810-173 (LONG DISPATCH)

73217415E1A 73217415E1B 73217415E2A 73217415E2B

IGNITION B NOT POWERED (NONE)

Indicates no power at 115V bus 1 (left engine) or 115V Bus 2 (right engine)


73217416E1A 73217416E1B 73217416E2A 73217416E2B

IGNITION B RELAY FAIL ON (NONE)

Ignition B feedback indicates the Ignitor power is on when the signal selector multiplexer is selecting relay power for B. The ignition B power is not commanded on

72-00-00-810-175 (LONG DISPATCH)

73217417E1A 73217417E1B

DISCRETE STOP SW INPUT DISAG

The valid hardwired signals disagree

72-00-00-810-176 (SHORT DISPATCH)


Page 33 of 72


Revision No. 29

Dated 05/31/2013


73217417E2A 73217417E2B

(ENG X SHORT DISPATCH)

73217418E1A 73217418E1B 73217418E2A 73217418E2B

ARINC ARINC - HWRE HWRE STOP STOP SW SW DISAGREE (ENG X SHORT DISPATCH)

The valid hardwired signals agree, but disagree with the valid ARINC input signals

72-00-00-810-177 (SHORT DISPATCH)

73217422E1A 73217422E1B 73217422E2A 73217422E2B

FADEC TCPL REFERENCE FAULT (NONE) NOTE: For v5.20 and below this fault is a "SHORT DISPATCH" fault

Sensor that monitors the FADEC thermocouple thermocouple cold unction has failed out of the range of T2-11C to T2-33C (varying lower limit) to 340F (171C)

72-00-00-810-178 (LONG DISPATCH)

73217423E1A 73217423E1B 73217423E2A 73217423E2B

FADEC TCPL REF DUAL FAULT (ENG X NO DISPATCH)

Both FADEC thermocouple thermocouple unction temperature sensors are out of the range of T2-11C to T2-33C (varying lower limit) to 340F (171C)

72-00-00-810-179 (NO DISPATCH)

73217424E1A 73217424E1B 73217424E2A 73217424E2B

HYD PRESSUER INPUT FAULT (NONE)

Hydraulic pressure ARINC label is not received or is faulted when the engine is running, or the GMO switch is pushed. Other ARINC labels are received


73217425E1A 73217425E1B 73217425E2A 73217425E2B

FADEC ARINC TX 1 FAULT (NONE)

The FADEC internal test of the T1 transmitter, transmitter, receiver pair has failed. Indicates a partial or total failure of the pair. Complete loss of both T transmitters transmitters will cause the loss of cross engine data to the other engine

72-00-00-810-181 (LONG DISPATCH)

73217426E1AN 73217426E1B 73217426E2A 73217426E2B


The FADEC internal test of the T12 transmitter, transmitter, receiver pair has failed. Indicates a partial or total failure of the pair. Complete loss of both T12 transmitters transmitters will cause the loss of engine data display

72-00-00-810-182 (LONG DISPATCH)


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on the EICAS 73217427E1A 73217427E1B 73217427E2A 73217427E2B

XENG SOFTWARE VERSION DISAGREE (ENG X NO DISPATCH) NOTE: Deleted

The local engine and cross engine AS software versions disagree

72-00-00-810-344 (NO DISPATCH)

73217514E1A 73217514E1B 73217514E2A 73217514E2B

T/R ICU PRESS SWITHC FAULT (ENG X REV PROT FAULT) NOTE: For v5.20 and below software, this fault is a "Long Time Dispatch" fault

Pressure switch CLOSED when system is not pressurized above switch threshold


73217515E1A 73217515E1B 73217515E2A 73217515E2B

TR ICU VALVE FAILED OPEN (ENG X NO DISPATCH) NOTE: For v5.20 and below software, this fault is a "Long Time Dispatch" fault

System pressurized, pressurized, but ICU indicated T/R is inhibited

72-00-00-810-345 (NO DISPATCH)

73217516E1A 73217516E1B 73217516E2A 73217516E2B

T/R DCU RELAY A TEST FAULT (ENG X REV FAIL)

TRAS DCU control relay contact on channel A is invalid. Tested during the pre-engine start test of the TRAS DCU relay. Test is performed after a reset only if the aircraft is on ground, N2 is less than 9.5 , TLA is at idle, MAU is transmitting to the FADEC


73217517E1A 73217517E1B 73217517E2A 73217517E2B

T/R DCU RELAY B TEST FAULT (ENG X REV FAIL)

TRAS DCU control relay contact on channel B is invalid. Tested during the pre-engine start test of the TRAS DCU relay. Test is performed after a reset only if the aircraft is on ground, N2 is less than 9.5 , TLA is at idle, MAU is transmitting to the FADEC


73217519E1A 73217519E1B 73217519E2A 73217519E2B

MACH NUMBER INPUTS DISAGREE (NONE)

Mach Number inputs disagree by more than 0.34 to 0.113, depending on N2, MN

72-00-00-810-185 (LONG DISPATCH)


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Dated 05/31/2013


(inverse relationship) 73217521E1A 73217521E1B 73217521E2A 73217521E2B

ECP APPLICATION ID PLUG DISAG (ENG X NO DISPATCH)

Selected engine rating from ECP disagrees with selected application ID

72-00-00-810-737 (NO DISPATCH)

73217522E1A 73217522E1B 73217522E2A 73217522E2B

APPLICATION ID PLUG SOFT FAULT (NONE) NOTE: For v5.20 and below this fault is a "Maintenance Information Message" fault

Data from both channel's aircraft application plug disagree (APPID NVM and one of APPID channel inputs are invalid). The correct Application ID is selected based on comparison to last valid NVM

72-00-00-810-346 (LONG DISPATCH)

73217523E1A 73217523E1B 73217523E2A 73217523E2B

ECP LOCAL CHANNEL FAULT (NONE) NOTE: For v5.20 and below this fault is a "SHORT DISPATCH" fault

Data from one channel ECP is missing or invalid

72-00-00-810-186 (LONG DISPATCH)

73217524E1A 73217524E1B 73217524E2A 73217524E2B

ECP LOCAL CHAN DATA Data from both INVALID channel's ECPs is (ENG X SHORT DISPATCH) valid, but 1 is not correct, perhaps from a programming error of the ECP

72-00-00-810-187 (SHORT DISPATCH)

73217525E1A 73217525E1B 73217525E2A 73217525E2B

ECP DATA INVALID (ENG X NO DISPATCH)

Data from both channel's ECPs is valid, but both are not correct, perhaps from a programming error of the ECP

72-00-00-810-188 (NO DISPATCH)

73217526E1A 73217526E1B 73217526E2A 73217526E2B

ECP FAULT (ENG X NO DISPATCH)

Data from both channel's ECPs is missing or invalid

72-00-00-810-189 (NO DISPATCH)

73217527E1A 73217527E1B 73217527E2A 73217527E2B

ECP RATING FAULT (ENG X NO DISPATCH)

The ECP selected rating data is incompatible incompatible with the FADEC software

72-00-00-810-190 (NO DISPATCH)

73217528E1A 73217528E1B 73217528E2A 73217528E2B

APPLICATION ID PLUG FAULT (ENG X NO DISPATCH)

The aircraft application plug is incorrect for the FADEC software (both APPID and NVM disagree or both APPID are invalid or only one APPID is

72-00-00-810-191 (NO DISPATCH)


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valid but it disagrees with NVM) 73217529E1A 73217529E1B 73217529E2A 73217529E2B

IGNITOR B NOT USED (NONE) NOTE: For v5.20 and below this fault is a "SHORT DISPATCH" fault

Ignitor B was not tested within consecutive times permitted

72-00-00-810-254 (MAINT. INF MSGS)

73217614E1A 73217614E1B 73217614E2A 73217614E2B

T/R ACTUATOR 1 LOC FAULT (ENG X REV FAIL)

System commanded to DEPLOY, but held by No. 1 Actuator Lock


73217615E1A 73217615E1B 73217615E2A 73217615E2B


System commanded to DEPLOY, but held by No. 2 Actuator Lock


73217617E1A 73217617E1B 73217617E2A 73217617E2B

T/R COWL LOC /SWITCH OPEN (ENG X REV PROT FAULT)

System stowed and unpressurized but Cowl Lock Switch indicates UNLOC ED


73217618E1A 73217618E1B 73217618E2A 73217618E2B

T/R COWL LOC FAILED CLOSED (ENG X REV FAIL)

System fails to DEPLOY when commanded, the cowl lock and actuator locks remain CLOSED


73217619E1A 73217619E1B 73217619E2A 73217619E2B

T/R COWL LOC SWITCH MONITOR (ENG X REV PROT FAULT)

System deployed, but Cowl Lock Switch indicates LOC ED


73217620E1A 73217620E1B 73217620E2A 73217620E2B

T/R ICU PRESSURE FAULT System indicates (ENG X REV PROT FAULT) pressure when there NOTE: For v5.20 and is NO PRESSURE below this fault is a command "NO DISPATCH" fault


73217621E1A 73217621E1B 73217621E2A 73217621E2B

T/R ICU NO PRESSURE FAULT (ENG X REV FAIL)

ICU signal commands power, but there is NO PRESSURE indication


73217622E1A 73217622E1B 73217622E2A 73217622E2B

T/R ICU PRESSURE SWITCH FAULT (ENG X REV PROT FAULT)



73217623E1A 73217623E1B 73217623E2A 73217623E2B

T/R DCU OPEN STATE FAULT (ENG X REV DEPLOYED)

Reverser fails to stow because the DCU remains in the stow position when DEPLOY is commanded


73217624E1A 73217624E1B 73217624E2A 73217624E2B

T/R DCU CLOSED STATE FAULT (ENG X REV FAIL)

The TRAS will not DEPLOY when commanded and the actuator locks remain CLOSED.



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Cowl lock solenoid valve mounted on the DCU Failed to OPEN 73217625E1A 73217625E1B 73217625E2A 73217625E2B

T/R TLA DCU SW FAILED OPEN (ENG X REV FAIL)

TLA switch fails OPEN so that TRAS will not DEPLOY when commanded. The DCU solenoid will not be energized. The TLA switch is in series with FADEC controlled DCU control (ground) relay


73217626E1A 73217626E1B 73217626E2A 73217626E2B

T/R TLA DCU SW FAILED CLOSED (ENG X REV PROT FAULT)

TLA switch fails CLOSED. System will operate normally, but has lost part of one line of defense. Switch is in serried with FADEC controlled DCU control (ground) relay


73217627E1A 73217627E1B 73217627E2A 73217627E2B

T/R TLA COWL L SW OPEN (ENG X REV FAIL)

TLA switch fails OPEN so that the TRAS will not DEPLOY, the cowl lock will not OPEN


73217628E1A 73217628E1B 73217628E2A 73217628E2B

T/R TLA COWL L SW CLOSED (ENG X REV PROT FAULT)

System will operate normally, but has lost part of one line of defense. Switch is in series with FADEC controlled DCU control (ground) relay


73217629E1A 73217629E1B 73217629E2A 73217629E2B

T/R DCU RELAY FAILED CLOSED (ENG X REV PROT FAULT)

A DCU relay contact has failed CLOSED, or the ADLEN signal is failed to voltage sensed


TABLE 102. FAULT MESSAGE DISPATCH - MASTER INDEX (CMC Message Alphabetical Order) F

 C d

CMC M (CAS M)



r

F  I S (  L)

73216017E1A 73216017E1B 73216017E2A 73216017E2B



72-00-00-810-022 (LONG DISPATCH)

73216016E1A 73216016E1B

ADS 1-2 INPUT FAULT (NONE)

All inputs from ADS 1 and ADS 2 are faulted

72-00-00-810-021 (LONG DISPATCH)


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Dated 05/31/2013


73216016E2A 73216016E2B

or are out of range. Other ARINC inputs are being received

73216018E1A 73216018E1B 73216018E2A 73216018E2B



72-00-00-810-023 (LONG DISPATCH)

73217528E1A 73217528E1B 73217528E2A 73217528E2B

APPLICATION ID PLUG FAULT (ENG X NO DISPATCH)

The aircraft application plug is incorrect for the FADEC software (both APPID and NVM disagree or both APPID are invalid or only one APPID is valid but it disagrees with NVM)

72-00-00-810-191 (NO DISPATCH)

73217522E1A 73217522E1B 73217522E2A 73217522E2B

APPLICATION ID PLUG SOFT FAULT (NONE) NOTE:For v5.20 and below this fault is a "Maintenance Information Message" fault

Data from both channel's aircraft application plug disagree (APPID NVM and one of APPID channel inputs are invalid). The correct Application ID is selected based on comparison to last valid NVM

72-00-00-810-346 (LONG DISPATCH)

73217418E1A 73217418E1B 73217418E2A 73217418E2B

ARINC - HWRE STOP SW DISAGREE (ENG X SHORT DISPATCH)

The valid hardwired signals agree, but disagree with the valid ARINC input signals

72-00-00-810-177 (SHORT DISPATCH)

73216316E1A 73216316E1B 73216316E2A 73216315E2B

ARINC T/R COMM FAULT (ENG X NO DISPATCH)

Either FADEC input ARINC label 244 or label 250 is missing. The FADEC is receiving other ARINC inputs O

72-00-00-810-273 (NO DISPATCH)

73216024E1A 73216024E1B 73216024E2A 73216024E2B

ATS SPDA 2 CIRCUIT FAULT (ENG X START VLV OPEN)

SPDA is supplying power to the ATS unexpectedly


73216026E1A 73216026E1B 73216026E2A 73216026E2B

ATS SPDA 2 MONITOR OFF FAULT (NONE)

ATS solenoid voltage monitor indicates no voltage and N2 indicates the engine is starting

72-00-00-810-029 (LONG DISPATCH)

73216027E1A 73216027E1B 73216027E2A 73216027E2B

ATS SPDA 2 MONITOR ON FAULT (NONE)

The ATS solenoid voltage monitor (monitored in SPDA 2) is always detecting that voltage is being

72-00-00-810-030 (LONG DISPATCH)


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sent to the starter 73216114E1A 73216114E1B 73216114E2A 73216114E2B

ATS SWITCH FAILED CLOSED (NONE)

The ATS switch is detected as failed CLOSED as the starter is energized and the engine is starting, but the switch is indicating the valve is CLOSED

72-00-00-810-033 (LONG DISPATCH)

73216028E1A 73216028E1B 73216028E2A 73216028E2B

ATS VALVE FAILD OPEN (ENG X START VLV OPEN)

Air Turbine Starter valve is stuck OPEN, as the feedback switch is O and it indicates that the valve has not CLOSED when commanded


73216116E1A 73216116E1B 73216116E2A 73216116E2B

BCM INPUT FAULT (NONE)

The Brake Control Module inputs have failed, the wheel speed is unknown but other ARINC inputs are being received and the engine is running

72-00-00-810-035 (LONG DISPATCH)

73216119E1A 73216119E1B 73216119E2A 73216119E2B

CMC INPUT FAULT (NONE)

Loss of the CMC input has been detected. The CMC will not report maintenance faults. No CMC initiated tests can be performed


73217417E1A 73217417E1B 73217417E2A 73217417E2B

DISCRETE STOP SW INPUT DISAG (ENG X SHORT DISPATCH)

The valid hardwired signals disagree

72-00-00-810-176 (SHORT DISPATCH)

73215619E1A 73215619E1B 73215619E2A 73215619E2B

DP3 CHAN A-B SENSORS DISAGREE (ENG X NO DISPATCH) NOTE: For v5.32 and below, this fault is a "SHORT DISPATCH" fault

The two DP3 signals differ by more than 8.0 PSID (55.2 kPa). Default signal is one closest to DP3 model. Fault inhibited when HPSOV is CLOSED

72-00-00-810-732 (NO DISPATCH)

73215618E1A 73215618E1B 73215618E2A 73215618E2B

DP3 SENSOR DUAL OUT OF RANGE (ENG X NO DISPATCH)

Both of the DP3 sensors are out of range. Fault inhibited when HPSOV is CLOSED and DP3 less than 0.0 PSID

72-00-00-810-244 (NO DISPATCH)

73215617E1A 73215617E1B 73215617E2A 73215617E2B

DP3 SENSOR OUT OF RANGE (NONE)

DP3 sensor is outside expected limits. Fault inhibited when HPSOV is CLOSED and DP3 is less than 0.0 PSID

72-00-00-810-243 (LONG DISPATCH)

7321 732175 7525 25E1 E1A A

ECP ECP DATA DATA INVA INVALI LID D

Data ata from from both both

72-0 72-000-00 00-8 -810 10-1 -188 88


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Dated 05/31/2013


73217525E1B 73217525E2A 73217525E2B

(ENG (ENG X NO NO DIS DISPAT PATCH) CH)

channe channel's l's ECPs ECPs is is valid, but both are not correct, perhaps from a programming error of the ECP

(NO DISPATCH)

73217521E1A 73217521E1B 73217521E2A 73217521E2B

ECP APPLICATION ID PLUG DISAG (ENG X NO DISPATCH)

Selected engine rating 72-00-00-810-737 from ECP disagrees (NO DISPATCH) with selected application ID

73217526E1A 73217526E1B 73217526E2A 73217526E2B

ECP FAULT (ENG X NO DISPATCH)

Data from both channel's ECPs is missing or invalid

72-00-00-810-189 (NO DISPATCH)

73217524E1A 73217524E1B 73217524E2A 73217524E2B

ECP LOCAL CHAN DATA INVALID (ENG X SHORT DISPATCH)

Data from both channel's ECPs is valid, but 1 is not correct, perhaps from a programming error of the ECP

72-00-00-810-187 (SHORT DISPATCH)

73217523E1A 73217523E1B 73217523E2A 73217523E2B

ECP LOCAL CHANNEL FAULT (NONE) NOTE:For v5.20 and below this fault is a "SHORT DISPATCH" fault

Data from one channel ECP is missing or invalid

72-00-00-810-186 (LONG DISPATCH)

73217527E1A 73217527E1B 73217527E2A 73217527E2B

ECP RATING FAULT (ENG X NO DISPATCH)

The ECP selected rating data is incompatible incompatible with the FADEC software

72-00-00-810-190 (NO DISPATCH)

73216115E1A 73216115E1B 73216115E2A 73216115E2B

ECS BLEED ON FAULT (ENG X SHORT DISPATCH)

The FADEC has requested the ECS to be off, but FADEC inputs indicate that bleed air is flowing. Aircraft must be airborne and be below 15,000 feet

72-00-00-810-034 (SHORT DISPATCH)

73215328E1A 73215328E1B 73215328E2A 73215328E2B

ECU TEMP SENSOR DUAL FAILURE (ENG X SHORT DISPATCH) NOTE: For v5.32 and below, this fault is a "NO DISPATCH" fault

Both FADEC internal temperature sensors are out of the range of T2-11ºC to T2-33ºC (varying lower limit) to 340ºF (171ºC)

72-00-00-810-720 (SHORT DISPATCH)

73215329E1A 73215329E1B 73215329E2A 73215329E2B

ECU TEMP SENSOR FAULT (NONE) NOTE:For v5.20 and below this fault is a "SHORT DISPATCH"

Sensor that monitors the FADEC internal temperature has failed out of the range of T2-11ºC to T2-33ºC (varying lower limit)

72-00-00-810-209 (LONG DISPATCH)


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fau l t

t o 3 4 0º F ( 17 1º C)

73215327E1A 73215327E1B 73215327E2A 73215327E2B

ECU TEMP SENSORS DISAGREE (NONE) NOTE: For v5.32 and below, this fault is a "SHORT DISPATCH" fault

Sensors that monitor the FADEC internal temperature differ by more than 50ºF (10ºC) from the average FADEC internal temperature. Indicates the failure of the ECU temperature sensor

72-00-00-810-738 (LONG DISPATCH)

73216124E1A 73216124E1B 73216124E2A 73216124E2B

ENGINE ID ARINC HWRE DISAG (ENG X NO DISPATCH)

Hardwired engine id inputs agree, but disagree with the ARINC input

72-00-00-810-043 (NO DISPATCH)

73216123E1A 73216123E1B 73216123E2A 73216123E2B

ENGINE ID INPUTS DISAGREE (ENG X NO DISPATCH)

Hardwired engine id inputs disagree, local channel is invalid

72-00-00-810-042 (NO DISPATCH)

73216125E1A 73216125E1B 73216125E2A 73216125E2B

ETTS N1 TRIM INPUTS INVALID (NONE)

The N1 TRIM input from the ETTS is invalid and the engine is running. N1 trim function is not available, ARINC is otherwise O

72-00-00-810-044 (LONG DISPATCH)

73216621E1A 73216621E1B 73216621E2A 73216621E2B



72-00-00-810-107 (LONG DISPATCH)

73216623E1A 73216623E1B 73216623E2A 73216623E2B



72-00-00-810-109 (LONG DISPATCH)

73217425E1A 73217425E1B 73217425E2A 73217425E2B


The FADEC internal test of the T1 transmitter, transmitter, receiver pair has failed. Indicates a partial or total failure of the pair. Complete loss of both T transmitters will cause the loss of cross engine data to the other engine

72-00-00-810-181 (LONG DISPATCH)

73217426E1A 73217426E1B 73217426E2A 73217426E2B


The FADEC internal test of the T12 transmitter, transmitter, receiver pair has failed. Indicates a partial or total failure of the

72-00-00-810-182 (LONG DISPATCH)


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pair. Complete loss of both T12 transmitters will cause the loss of engine data display on the EICAS 73216620E1A 73216620E1B 73216620E2A 73216620E2B

FADEC ARINC XENG FAULT (ENG X NO DISPATCH)

This channel has no ARINC inputs from the opposite (cross) engine. N2 must be more than 10 percent

72-00-00-810-106 (NO DISPATCH)

73216118E1A 73216118E1B 73216118E2A 73216118E2B

FADEC CHANNEL ID FAULT (ENG X NO DISPATCH)

The channel ID inputs disagree, cannot determine if the local channel is A or B. Interferes with channel-in-control selection logic, CMC interactions

72-00-00-810-037 (NO DISPATCH)

73216127E1A 73216127E1B 73216127E2A 73216127E2B

FADEC CPU FAULT (ENG X NO DISPATCH)

Set for FADEC internal 72-00-00-810-046 failures that cause (NO DISPATCH) incorrect results, but the channel is healthy enough to transmit ARINC. (Caused by AIP or CPU failures of: WDM, CPU Instruction Test, Scratchpad Memory, Program Memory, NVM Adjustments, Adjustments, Dual Port RAM.)

73216220E1A 73216220E1B 73216220E2A 73216220E2B

FADEC CTRL RELAY OPEN FAULT (ENG X SHORT DISPATCH)

The relay source (high side) contacts have been detected as failed OPEN on the local channel. Fault is set if the over current fault is set or if both the TR DCU and ICU relays were detected "OPEN" during the ground start BIT testing

72-00-00-810-058 (SHORT DISPATCH)

73216129E1A 73216129E1B 73216129E2A 73216129E2B

FADEC DUAL CHANNEL OVTMP (ENG X FADEC OVERTEMP)

FADEC internal temperature has exceeded 248ºF (120ºC)


73216219E1A 73216219E1B 73216219E2A 73216219E2B

FADEC DUAL CTRL RELAY FAULT (ENG X NO DISPATCH)

The FADECs high side relays have failed OPEN on both channels. Fault is set if the over current fault is set or if both the TR

72-00-00-810-057 (NO DISPATCH)


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DCU and ICU relays were detected "OPEN" during the ground start BIT test. The FADEC cannot energize the overspeed solenoid, hardwired ignitor, and reverser 73217127E1A 73217127E1B 73217127E2A 73217127E2B

FADEC ECP NVM FAULT (ENG X SHORT DISPATCH)

A checksum fault in the engine thrust rating (NVM version) exists

72-00-00-810-146 (SHORT DISPATCH)

73217128E1A 73217128E1B 73217128E2A 73217128E2B

FADEC GENERAL NVM FAULT (ENG X NO DISPATCH)

NVM fault has been detected at power up or during GSBIT

72-00-00-810-147 (NO DISPATCH)

73216215E1A 73216215E1B 73216215E2A 73216215E2B

FADEC HI VOLT SHUTDOWN FAULT (ENG X SHORT DISPATCH)

Power supply's high voltage disconnect has failed Built In Test (BIT) test

72-00-00-810-054 (SHORT DISPATCH)

73216128E1A 73216128E1B 73216128E2A 73216128E2B

FADEC INTERLOC FAULT (NONE)

One or both of the FADEC reprogramming reprogramming lockouts have failed

72-00-00-810-047 (LONG DISPATCH)

73216126E1A 73216126E1B 73216126E2A 73216126E2B

FADEC INTERNAL FAULT (ENG X NO DISPATCH) NOTE: For v5.32 and below, this fault is a "SHORT DISPATCH" fault

A FADEC internal fault has been detected. Set by: FADEC Interlock, PSU High Voltage ShutDown, AIP Local channel processor, High Side Relay Fault, Basic Computer Fault, Channel ID Fault, ARINC internal wrap fault

72-00-00-810-733 (NO DISPATCH)

73216117E1A 73216117E1B 73216117E2A 73216117E2B

FADEC INTERNAL XTAL FAULT (ENG X NO DISPATCH)

The local FADEC 72-00-00-810-036 channel cannot receive (NO DISPATCH) serial data from the other FADEC channel

73217126E1A 73217126E1B 73217126E2A 73217126E2B

FADEC MINOR HEALTH FAULT (ENG X NO DISPATCH) NOTE: For v5.32 and below, this fault is a "SHORT DISPATCH" fault

The serial and the parallel versions of the cross channel engine health parameter disagree

72-00-00-810-735 (NO DISPATCH)

73217324E1A 73217324E1B 73217324E2A 73217324E2B

FADEC OTHER CHANNEL FAULT (ENG X SHORT DISPATCH)

The other FADEC channel has been detected as not being able to control the engine

72-00-00-810-167 (SHORT DISPATCH)


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73216529E1A 73216529E1B 73216529E2A 73216529E2B

FADEC PS3 LINE BRO EN FAULT (NONE)

The PS3 line is detected as broken

72-00-00-810-362

73216528E1A 73216528E1B 73216528E2A 73216528E2B

FADEC PS3 OUT OF RANGE (ENG X SHORT DISPATCH) NOTE: For v5.32 and below, this fault is a "LONG DISPATCH" fault

PS3 sensor is failed if the value is outside the computed range. Minimum limit is 1.0 or P0-4.0 PSIA (whichever is greater). Maximum limit is PS3 more than 520 (N2 is more than 90) or 620 (N2 is more than 91) PSIA. Engine is operating where parameters should be within limits

72-00-00-810-724 (SHORT DISPATCH)

73216214E1A 73216214E1B 73216214E2A 73216214E2B

FADEC SINGLE CHANNEL OVTMP (ENG X NO DISPATCH)

FADEC internal 72-00-00-810-049 temperature has (NO DISPATCH) exceeded 248ºF (120ºC) on a single channel only

73216718E1A 73216718E1B 73216718E2A 73216718E2B

FADEC SOFTWARE VERSIONS DISAG (ENG X NO DISPATCH)

The software versions on the two channels in the FADEC are different, giving different control functionality depending on the channel in control. Possibly due to an aborted reprogramming procedure

72-00-00-810-114 (NO DISPATCH)

73217423E1A 73217423E1B 73217423E2A 73217423E2B

FADEC TCPL REF DUAL FAULT (ENG X NO DISPATCH)

Both FADEC thermocouple thermocouple junction temperature sensors are out of the range of T2-11ºC to T2-33ºC (varying lower limit) to 340ºF (171ºC)

72-00-00-810-179 (NO DISPATCH)

73217422E1A 73217422E1B 73217422E2A 73217422E2B

FADEC TCPL REFERENCE FAULT (NONE) NOTE:For v5.20 and below this fault is a "SHORT DISPATCH" fault

Sensor that monitors 72-00-00-810-178 the FADEC thermocouple thermocouple (LONG DISPATCH) cold junction has failed out of the range of T2-11ºC to T2-33ºC (varying lower limit) to 340ºF (171ºC)

73217320E1A 73217320E1B 73217320E2A 73217320E2B

FADEC TCPL SENSOR FAULT (ENG X NO DISPATCH) NOTE: For v5.32 and

The local cold junction temperature from the local channel and cross channel

72-00-00-810-736 (NO DISPATCH)


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Dated 05/31/2013


below,this fault is a "SHORT DISPATCH" fault

disagree by more than 100ºR (50.5ºC)

73217223E1A 73217223E1B 73217223E2A 73217223E2B

FMU FMU CMD CMD - CURR CURREN ENT T DISAGREE (ENG X SHORT DISPATCH)


73217220E1A 73217220E1B 73217220E2A 73217220E2B

FMU FMU CMD CMD - POSITI POSITION ON DISAGREE (ENG X FAIL) (ENG X NO DISPATCH)

The FMU Metering Valve 72-00-00-810-148 position is more than (NO DISPATCH) 5 percent from the demanded position (when NG is greater than 20 percent) or the WF loop position is more than 20 percent from the demanded position. The sensor and torque motor values are valid, the sensor has been valid for more than 2.0 seconds.

73217222E1A 73217222E1B 73217222E2A 73217222E2B

FMU DUAL CMD CURRENT DISAG (ENG X FAIL) (ENG X NO DISPATCH)

Dual channel failure 72-00-00-810-150 in the torque motor (NO DISPATCH) driver circuits. FMU Metering Valve will slew to the FAIL SAFE position. ARINC output will be set until the engine drops below 30 percent N2

73217224E1A 73217224E1B 73217224E2A 73217224E2B

FMU DUAL SENSOR RANGE FAULT (ENG X FAIL)

Both FMU Metering Valve position feedback sensors are out of the range of 50 to 140 percent stroke or the voltage sums are out of the range of 8.6 to 12.0 volts. Default value of 100 percent stroke is used. FMU Metering Valve will slew to the FAIL SAFE position


73215620E1A 73215620E1B 73215620E2A 73215620E2B

FMU NULL BIAS SHIFT (NONE)

The FMU null biases for both the VSV and FMV have drifted from nominal such that an engine overspeed condition may occur if the FADEC were to lose electrical power while the engine was running

72-00-00-810-246 (LONG DISPATCH)

72-00-00-810-151 (SHORT DISPATCH)


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Revision No. 29

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at full thrust 73217221E1A 73217221E1B 73217221E2A 73217221E2B

FMU SENSOR RANGE FAULT (ENG X SHORT DISPATCH) NOTE: For v5.32 and below, this fault is a "LONG DISPATCH" fault

Local channel FMU Metering Valve position feedback sensor is out of the range of -50 to 140 percent stroke or the voltage sum is out of the range of 8.6-12.0 volts. Cross channel sensor is used

72-00-00-810-725 (SHORT DISPATCH)

73217225E1A 73217225E1B 73217225E2A 73217225E2B

FMU SENSORS CHAN AB DISAGREE (ENG X NO DISPATCH)

The two position 72-00-00-810-153 feedback sensors are (NO DISPATCH) in range but disagree by more than 10 percent stroke. Sensor is selected based on rate of change and previously failed sensor

73216014E1A 73216014E1B 73216014E2A 73216014E2B

NO.1 BEARING ACCEL FAULT (NONE) NOTES: For v5.32 this fault is an "ECONOMIC DISPATCH" fault For v5.20 and below, this fault is a "SHORT DISPATCH" fault

Both IEVM outputs for the front accelerometer are invalid. ARINC communications communications is O and at least 1 rear accelerometer signal is O

72-00-00-810-739 (LONG DISPATCH)

73217115E1A 73217115E1B 73217115E2A 73217115E2B

GMO INPUTS INVALID (NONE)

Thrust reverser GMO switches have been detected as being in the wrong state. Set if the GMO was selected at power up for selected (pushed) for more than 2 minutes


73216216E1A 73216216E1B 73216216E2A 73216216E2B

GMO SW INPUTS CHAN A-B DISAG NOTE: For v5.32 and below, this fault is a "LONG DISPATCH" fault

The two inputs from the GMO (for thrust reverser test) switch disagree


73215517E1A 73215517E1B 73215517E2A 73215517E2B

HPT CMD - CURRENT DISAGREE (NONE)

Single channel failure in the HPT torque motor driver circuit


73215514E1A 73215514E1A

HPT CMD - POSITION

The HPT position is

72-00-00-810-225 72-00-00-810-225


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Dated 05/31/2013


73215514E1B 73215514E2A 73215514E2B

DISAG (NONE)

more than 5 percent from the demanded position. The sensor and torque motor values are O , the sensor has been valid for more than 2.0 seconds

(LONG DISPATCH)

73215516E1A 73215516E1B 73215516E2A 73215516E2B

HPT DUAL CMD CURRENT DISAG (NONE)

Dual channel failure in the torque motor driver circuits. HPT will slew to the FAIL SAFE position


73215518E1A 73215518E1B 73215518E2A 73215518E2B

HPT DUAL SENSOR RANGE FAULT (NONE)

Both HPT position feedback sensors have failed. HPT position is set to 0.0 percent OPEN. HPT will slew to the FAIL SAFE position

72-00-00-810-229 (LONG DISPATCH)

73215515E1A 73215515E1B 73215515E2A 73215515E2B

HPT SENSOR RANGE FAULT (NONE)

Local channel HPT position feedback sensor is out of the range of -10 to 110 percent stroke or the voltage sum is out of the range of 4.0 to 6.7 volts. Cross channel sensor is used


73215519E1A 73215519E1B 73215519E2A 73215519E2B

HPT SENSORS CHAN AB DISAGREE (NONE)

The two HPT position feedback sensors are in range but disagree by more than 5 percent stroke. Sensor is selected based on rate of change and previously failed sensor


73215616E1A 73215616E1B 73215616E2A 73215616E2B

HPTACC TC CHAN A-B DISAGREE (NONE)

The two HPTACC TC signals differ by more than 40.0ºC. Weighted averaging starts at 30.0º 30.0º delta. delta. Minimu Minimum m sensor value is used as default


73215615E1A 73215615E1B 73215615E2A 73215615E2B

HPTACC TC DUAL OUT OF RANGE (NONE)

Both of the HPTACC TC sensors are out of range

72-00-00-810-241 (LONG DISPATCH)

73215614E1A 73215614E1B 73215614E2A 73215614E2B

HPTACC TC OUT OF RANGE (NONE)

HPTACC TC sensor is outside expected limits



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73217424E1A 73217424E1B 73217424E2A 73217424E2B

HYD PRESSURE INPUT FAULT (NONE)

Hydraulic pressure ARINC label is not received or is faulted when the engine is running, or the GMO switch is pushed. Other ARINC labels are received


73216029E1A 73216029E1B 73216029E2A 73216029E2B

ICE DETECTOR INPUTS FAULT (NONE)

ARINC inputs to the FADEC indicate that the engine has reached idle and both of the ice detectors have failed for this engine


73216222E1A 73216222E1B 73216222E2A 73216222E2B

IEVM INPUT FAULT (ENG X NO DISPATCH)

The ARINC input labels 72-00-00-810-051 carrying the vibration (NO DISPATCH) signals for exceedance checking are all invalid

73217327E1A 73217327E1B 73217327E2A 73217327E2B

IGN A SPDA CMD FEEDBAC FAULT (NONE)

Ignition feedback indicates ignitor A is off when commanding ignition A power on. Fault is set when commanding via ARINC

72-00-00-810-170 (LONG DISPATCH)

73217414E1A 73217414E1B 73217414E2A 73217414E2B

IGN B SPDA CMD FEEDBAC FAULT (NONE)

Ignition feedback indicates ignitor B is off when commanding ignition B power on. Fault is set when commanding via ARINC

72-00-00-810-173 (LONG DISPATCH)

73216228E1A 73216228E1B 73216228E2A 73216228E2B

IGN SW ON AND OFF INPUTS ON (ENG X SHORT DISPATCH)

The cockpit switch for ignition inputs are set to OFF and ON at the same time

72-00-00-810-062 (SHORT DISPATCH)

73216223E1A 73216223E1B 73216223E2A 73216223E2B

IGNITION A DISCRETE FAULT (NONE)

The hardwired ignition connection between the FADEC channel A and the SPDA is OPEN circuit

72-00-00-810-052 (LONG DISPATCH)

73216120E1A 73216120E1B 73216120E2A 73216120E2B

IGNITION A MONITOR FAULT (NONE)

The EICC output ("Ignition A Rly Status" on SPDA) indicates the ignitor was not energized, but the engine lit off

72-00-00-810-039 (LONG DISPATCH)

73216229E1A 73216229E1B 73216229E2A 73216229E2B

IGNITION A POWER (ENG X NO DISPATCH)

The SPDA 1 has reported a loss of power supplied to ignitor A. Ignitor A was commanded to be energized. This fault

72-00-00-810-063


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could be set by a failure of the SPDA 1 excitor monitor sensor 73217328E1A 73217328E1B 73217328E2A 73217328E2B

IGNITION A RELAY FAIL ON (NONE)

Ignition A feedback indicates the Ignitor power is on when the signal selector multiplexer is selecting relay power for A. The ignition A power is not commanded on

72-00-00-810-171 (LONG DISPATCH)

73216225E1A 73216225E1B 73216225E2A 73216225E2B

IGNITION A-B DISCRETE FAULT (ENG X SHORT DISPATCH)

The hardwired ignition connections between the FADEC and the SPDA are OPEN circuit

72-00-00-810-059 (SHORT DISPATCH)

73216224E1A 73216224E1B 73216224E2A 73216224E2B

IGNITION B DISCRETE FAULT (NONE)

The hardwired ignition connection between the FADEC channel B and the SPDA is OPEN circuit

72-00-00-810-053 (LONG DISPATCH)

73216122E1A 73216122E1B 73216122E2A 73216122E2B

IGNITION B MONITOR FAULT (NONE)

The SPDA output indicates the ignitor was not energized (SPDA monitors the output voltage supplied to the igniters), but the engine lit off

72-00-00-810-041 (LONG DISPATCH)

73217415E1A 73217415E1B 73217415E2A 73217415E2B

IGNITION B NOT POWERED (NONE)

Indicates no power at 115V bus 1 (left engine) or 115V Bus 2 (right engine)


73216317E1A 73216317E1B 73216317E2A 73216317E2B

IGNITION B POWER FAULT (ENG X SHORT DISPATCH)

The SPDA 2 has reported a loss of power supplied to ignitor B. Ignitor B was commanded to be energized. This fault could be set by a failure of the SPDA 2 excitor monitor sensor

72-00-00-810-067 (SHORT DISPATCH)

73217416E1A 73217416E1B 73217416E2A 73217416E2B

IGNITION B RELAY FAIL ON (NONE)

Ignition B feedback indicates the Ignitor power is on when the signal selector multiplexer is selecting relay power for B. The ignition B power is not commanded on

72-00-00-810-175 (LONG DISPATCH)

73216226E1A

IGNITION SW OFF

The two inputs for

72-00-00-810 -060


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73216226E1B 73216226E2A 73216226E2B

INPUTS DISAG (NONE)

cockpit ignition switch being "OFF" disagree

(LONG DISPATCH)

73216227E1A 73216227E1B 73216227E2A 73216227E2B

IGNITION SW ON INPUTS DISAG (NONE)

The two inputs for cockpit ignition switch being ON disagree

72-00-00-810-061 (LONG DISPATCH)

73216314E1A 73216314E1B 73216314E2A 73216314E2B

IGNITOR A NO LIGHT OFF (ENG X NO DISPATCH)

The engine did not start while using ignitor A (it will then use ignitor B). There were no other detected contributing ignition faults. The ignition system is the probable cause (excitor, ignitor)

72-00-00-810-064 (NO DISPATCH)

73217326E1A 73217326E1B 73217326E2A 73217326E2B

IGNITOR A POWER FAILED ON (ENG X SHORT DISPATCH)

Ignition A feedback indicates the Ignitor power is commanded on when the signal selector multiplexer is selecting Ignition A command via ARINC or ALL. The ignition A power is not commanded on

72-00-00-810-169 (SHORT DISPATCH)

73216318E1A 73216318E1B 73216318E2A 73216318E2B

IGNITOR B NO LIGHT OFF (ENG X SHORT DISPATCH)

The engine did not start while using ignitor B (it will then use ignitor A). There were no other detected contributing ignition faults. The ignition system is the probable cause (excitor, ignitor)

72-00-00-810-068 (SHORT DISPATCH)

73217529E1A 73217529E1B 73217529E2A 73217529E2B

IGNITOR B NOT USED (NONE) NOTE:For v5.20 and below this fault is a "SHORT DISPATCH" fault

Ignitor B was not tested within consecutive times permitted

72-00-00-810-254 (MAINT. INF. MSGS)

73217329E1A 73217329E1B 73217329E2A 73217329E2B

IGNITOR B POWER FAILED ON (ENG X SHORT DISPATCH)

Ignition B feedback indicates the Ignitor power is commanded on when the signal selector multiplexer is selecting Ignition B command via ARINC or ALL. The ignition B power is not commanded on

72-00-00-810-172 (SHORT DISPATCH)


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73216315E1A 73216315E1B 73216315E2A 73216315E2B

IGNITORS A-B NO LIGHT OFF (ENG X NO DISPATCH)

The engine did not start when both ignition systems were tried. There were no other detected contributing contributing ignition or fuel system faults. The ignition system is the probable cause (excitor, ignitor)

72-00-00-810-065 (NO DISPATCH)

73216323E1A 73216323E1B 73216323E2A 73216323E2B

INTERNAL FADEC FAULT (ENG X CONTROL FAULT) NOTE:For v5.20 and below, this fault is a "LONG TIME DISPATCH" fault

The FADEC is unable to process the local and cross channel sensor inputs


73217019E1A 73217019E1B 73217019E2A 73217019E2B

ITT CHAN A-B INPUTS DISAGREE (ENG X SHORT DISPATCH)

The two ITT signals differ by  55.6C. Weighted averaging starts at 27.8C delta. The failsafe value is 1093.5C. Fault can be due to single channel fault if occurs at low engine speeds. Fault inhibited when engine not running or subidle. NOTE: Do not convert 55.6C to F because in this case, the temperature conversion is not a direct ratio from C to F

72-00-00-810-122 (SHORT DISPATCH)

73217017E1A 73217017E1B 73217017E2A 73217017E2B

ITT DUAL OUT OF RANGE (ENG X NO DISPATCH)

Both of the ITT sensors are out of range. The default value is 2001.2F (1094C). Fault is inhibited until the engine is close to idle or above

72-00-00-810-120 (NO DISPATCH)

73217018E1A 73217018E1B 73217018E2A 73217018E2B

ITT OUT OF RANGE (NONE)

ITT is less than 300F (149C) or more than 2540.3F (1393.5C). Fault inhibited when engine not running or subidle

72-00-00-810-121 (LONG DISPATCH)

73215326E1A 73215326E1B

LPT CHAN A-B SENSORS DISAGREE

The two LPT position feedback sensors are



Page 52 of 72


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73215326E2A 73215326E2B

(NO N E)

i n r a nge but di s agr e e by more than 5 percent stroke. Sensor is selected based on rate of change and previously failed sensor

73215324E1A 73215324E1B 73215324E2A 73215324E2B

LPT LPT CMD CMD - CURR CURREN ENT T DISAGREE (NONE)

Single channel failure in the LPT torue motor driver circuit


73215321E1A 73215321E1B 73215321E2A 73215321E2B

LPT LPT CMD CMD - POSITI POSITION ON DISAGREE (NONE) NOTE:For v5.20 and below this fault is a "SHORT DISPATCH" fault

The LPT position is more than 5 percent from the demanded position. The sensor and torue motor values are O, the sensor has been valid for more than 2.0 seconds

72-00-00-810-247 (LONG DISPATCH)

73215323E1A 73215323E1B 73215323E2A 73215323E2B

LPT DUAL CMD CURRENT DISAGREE (NONE) NOTE:For v5.20 and below this fault is a "SHORT DISPATCH" fault

Dual channel failure in the torue motor driver circuits. LPT will slew to the FAIL SAFE position

72-00-00-810-249 (LONG DISPATCH)

73215325E1A 73215325E1B 73215325E2A 73215325E2B

LPT DUAL SENSOR RANGE FAULT (NONE) NOTE:For v5.20 and below this fault is a "SHORT DISPATCH" fault

Both LPT position feedback sensors have failed. LPT position is set to 100 percent CLOSED. LPT will slew to the FAIL SAFE position

72-00-00-810-251 (LONG DISPATCH)

73215322E1A 73215322E1B 73215322E2A 73215322E2B

LPT SENSOR RANGE FAULT (NONE)

Local channel LPT position feedback sensor is out of the range of -8.6 to 108.6 stroke or the voltage sum is out of the range of 3.0 to 13.0 volts. Cross channel sensor is used


73216321E1A 73216321E1B 73216321E2A 73216321E2B

MACH INPUT FAULT (ADS1-2) (NONE)

Both mach numbers inputted from ARINC from ADS1 and ADS2 have not been received or are out of range. Ground, the limits are -0.12 to 0.409 (altitude dependant). Airborne, the limits are 0.0 to 0.97

72-00-00-810-071 (LONG DISPATCH)


Page 53 of 72


Revision No. 29

Dated 05/31/2013


(altitude dependant) for 30 seconds 73217519E1A 73217519E1B 73217519E2A 73217519E2B

MACH NUMBER INPUTS DISAGREE (NONE)

Mach Number inputs disagree by more than 0.34 to 0.113, depending on N2, MN (inverse relationship)

72-00-00-810-185 (LONG DISPATCH)

73216319E1A 73216319E1B 73216319E2A 73216319E2B



72-00-00-810-069 (LONG DISPATCH)

73216320E1A 73216320E1B 73216320E2A 73216320E2B



72-00-00-810-070 (LONG DISPATCH)

73216619E1A 73216619E1B 73216619E2A 73216619E2B



72-00-00-810-105 (LONG DISPATCH)

73216622E1A 73216622E1B 73216622E2A 73216622E2B



72-00-00-810-108 (LONG DISPATCH)

73216618E1A 73216618E1B 73216618E2A 73216618E2B

MAU ARINC INPUTS FAULT (ENG X SHORT DISPATCH)

This channel has no ARINC inputs from the aircraft

72-00-00-810-104 (SHORT DISPATCH)

73216020E1A 73216020E1B 73216020E2A 73216020E2B

MULTIPLE FAILURES DETECTED (ENG X NO DISPATCH)

Combination of faults were detected on FADEC channel A and B. Clear multiple short time dispatch faults to clear this fault

72-00-00-810-024 (NO DISPATCH)

73215229E1A

MULTIPLE T/R PROT

Two or more Thrust

72-00-00-810 -726


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Revision No. 29

Dated 05/31/2013


73215229E1B 73215229E2A 73215229E2B

FAULTS (ENG X NO DISPATCH)

Reverser protection faults have been set

(NO DISPATCH)

73216019E1A 73216019E1B 73216019E2A 73216019E2B

NO.1 BEARING ACCEL OFF DUE TO ECP CONFIG (NONE)

ECP Configuration for defective front accelerometer is in use. Scaled rear accelerometer will be used


73216326E1A 73216326E1B 73216326E2A 73216326E2B

N1 CHAN A-B INPUTS DISAGREE (ENG X NO DISPATCH)

The N1 sensor inputs are valid but disagree by more than 5 percent. Rate of change and result of previous range tests are used to isolate the invalid signal. Fault inhibited when engine not running or subidle

72-00-00-810-075 (NO DISPATCH)

73216325E1A 73216325E1B 73216325E2A 73216325E2B

N1 DUAL OUT OF RANGE (ENG X CONTROL FAULT) NOTE:For v5.20 and below, this fault is a "NO DISPATCH" fault

Both N1 sensors are invalid or out of range. A computed value is used that is calculated from N2, T12, Mach Number


73216324E1A 73216324E1B 73216324E2A 73216324E2B

N1 OUT OF RANGE (ENG X SHORT DISPATCH) NOTE: For v5.32 and below, this fault is a "LONG DISPATCH" fault

Local channel N1 sensor is invalid or out of range of 10 to 125 percent when N1 should be more than 10 percent based on other parameters. Fault inhibited when engine not running or subidle

72-00-00-810-723 (SHORT DISPATCH)

73216329E1A 73216329E1B 73216329E2A 73216329E2B

N2 ALTERNATOR INPUTS DISAGREE (ENG X SHORT DISPATCH)

The two N2 alternator inputs from the alternator are valid but disagree by more than 1.2 percent. Rate of change and result of previous range tests are used to isolate the invalid signal. Fault inhibited when engine not running or subidle

72-00-00-810-078 (SHORT DISPATCH)

73216328E1A 73216328E1B 73216328E2A 73216328E2B

N2 ALTERNATOR OUT OF RANGE (ENG X SHORT DISPATCH)

The local channel N2 alternator signal is out of the allowable range of 5-130 percent

72-00-00-810-077 (SHORT DISPATCH)


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when N2 should be more than 5 percent based on other parameters. Fault inhibited when engine not running or subidle 73216415E1A 73216415E1B 73216415E2A 73216415E2B

N2 ALTERNATOR-FUEL PUMP DISAG (ENG X NO DISPATCH)

The N2 inputs from the fuel pump are valid but disagree with the valid N2 inputs from the alternator by more than 1.2 percent

72-00-00-810-079 (NO DISPATCH)

73216416E1A 73216416E1B 73216416E2A 73216416E2B

N2 FUEL PUMP DUAL OUT OF RNG (ENG X NO DISPATCH)

Both N2 signals from the main fuel pump are invalid or out of the allowable range of 5130 percent when N2 should be more than 5 percent based on other parameters

72-00-00-810-080 (NO DISPATCH)

73216418E1A 73216418E1B 73216418E2A 73216418E2B

N2 FUEL PUMP INPUTS DISAGREE (ENG X SHORT DISPATCH)

The two N2 inputs from the fuel pump are valid but disagree by more than 1.2 percent. Rate of change and result of previous range tests are used to isolate the invalid signal. Fault inhibited when engine not running or subidle

72-00-00-810-082 (SHORT DISPATCH)

73216417E1A 73216417E1B 73216417E2A 73216417E2B

N2 FUEL PUMP OUT OF RANGE (ENG X SHORT DISPATCH)

The local channel N2 signal from the main fuel pump is out of the allowable range of 5-130 percent when N2 should be more than 5 percent based on other parameters. Fault inhibited when engine not running or subidle

72-00-00-810-081 (SHORT DISPATCH)

73216428E1A 73216428E1B 73216428E2A 73216428E2B

N2 OVERSPEED (ENG X FAIL)

N2 has exceeded the overspeed trip limit of 102 percent (Aircraft %) engine shutdown is commanded


73216327E1A 73216327E1B 73216327E2A 73216327E2B

N2 PMA DUAL OUT OF RANGE (ENG X CONTROL FAULT) NOTE:For v5.20 and below, this fault is a "NO DISPATCH"

No valid N2 signals exist from the alternator



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fault 73217125E1A 73217125E1B 73217125E2A 73217125E2B

NLG WOW - WHSPD FAIL (ENG X REV FAIL) NOTE:For v5.20 and below, this fault is a "SHORT DISPATCH" fault

TRAS is unavailable due to combination of bad NLG and wheel speed signals


73216426E1A 73216426E1B 73216426E2A 73216426E2B

OVERSPEED DUAL TEST FAULT (ENG X NO DISPATCH) NOTE:For v5.20 and below software, this fault is a "Maintenance Information Message" fault

Combination of faults 72-00-00-810-343 were detected on FADEC (NO DISPATCH) channel A and B resulting in dual channel loss of overspeed protection. Clear short term N2 core overspeed electrical test faults to clear this fault

73216427E1A 73216427E1B 73216427E2A 73216427E2B

OVERSPEED SHUTDOWN TEST FAULT (ENG X NO DISPATCH)

Overspeed system 72-00-00-810-084 failed engine shutdown (NO DISPATCH) test, the engine has not flamed out after 2 seconds of commanding the overspeed solenoid to shut off fuel

73216425E1A 73216425E1B 73216425E2A 73216425E2B

OVERSPEED TEST FAULT (ENG X SHORT DISPATCH)

Overspeed system failed electrical test. Test is performed at idle and again when TLA is advanced from ground idle and 40 sec. after landing

72-00-00-810-083 (SHORT DISPATCH)

73216518E1A 73216518E1B 73216518E2A 73216518E2B

P0 - ADS DISAGREE (NONE)

ADS P0 inputs disagree with the ENGINE P0 inputs

72-00-00-810-090 (LONG DISPATCH)

73216515E1A 73216515E1B 73216515E2A 73216515E2B

P0 ALL INPUTS FAULT (ENG X CONTROL FAULT)

All P0 signals have failed


73216517E1A 73216517E1B 73216517E2A 73216517E2B

P0 DUAL OUT OF RANGE (FADEC) (ENG X NO DISPATCH)

Both engine P0 sensors are out of the range of 1.8-16.8 PSIA (12.4-115.8 Pa)

72-00-00-810-089 (NO DISPATCH)

73216519E1A 73216519E1B 73216519E2A 73216519E2B

P0 INPUTS DISAGREE (FADEC) (ENG X NO DISPATCH)

The two FADEC P0 sensors disagree by more than 0.4 PSIA (2.8 Pa)

72-00-00-810-091 (NO DISPATCH)

73216429E1A 73216429E1B

P0 OUT OF RANGE (ADS 1-2)

Both ADS P0 inputs have failed

72-00-00-810-086 (LONG DISPATCH)


Page 57 of 72


Revision No. 29

Dated 05/31/2013


73216429E2A 73216429E2B

(NONE)

73216520E1A 73216520E1B 73216520E2A 73216520E2B

P0 OUT OF RANGE (ADS1) (NONE)


72-00-00-810-092 (LONG DISPATCH)

73216521E1A 73216521E1B 73216521E2A 73216521E2B

P0 OUT OF RANGE (ADS2) (NONE)


72-00-00-810-093 (LONG DISPATCH)

73216516E1A 73216516E1B 73216516E2A 73216516E2B

P0 OUT OF RANGE (FADEC) (ENG X NO DISPATCH)

Local channel P0 engine sensor is out of the range of 1.816.8 PSIA (12.4-115.8 Pa)

72-00-00-810-088 (NO DISPATCH)

73216526E1A 73216526E1B 73216526E2A 73216526E2B

PMA LOW POWER OUTPUT (ENG X SHORT DISPATCH)

N2 from the pump is O and more than 75 percent and power is being drawn from the aircraft (28V) OR N2 from the pump is O and more than 50 percent and at least one PMA phase has been detected as OPEN circuit

72-00-00-810-097 (SHORT DISPATCH)

73216527E1A 73216527E1B 73216527E2A 73216527E2B

PS3 DUAL SENSORS FAULT (ENG X CONTROL FAULT)

Dual channel PS3 sensor failure detected


73216614E1A 73216614E1B 73216614E2A 73216614E2B

PS3 INPUTS DISAGREE (ENG X NO DISPATCH) NOTE: For v5.32 and below, this fault is a "SHORT DISPATCH" fault

The two PS3 sensors disagree by more than 16 PSIA (110 Pa). PS3 is weighted averaged starting at 8 PSIA (55Pa) delta. Failsafe value is 47.0 PSIA (324.1 Pa). Fault isolation is based on past failure and excitation faults

72-00-00-810-734 (NO DISPATCH)

73216616E1A 73216616E1B 73216616E2A 73216616E2B



72-00-00-810-102 (LONG DISPATCH)

73216617E1A 73216617E1B 73216617E2A 73216617E2B


Landing gear proximity sensor computer 2 has failed with engine running

72-00-00-810-103 (LONG DISPATCH)


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73216615E1A 73216615E1B 73216615E2A 73216615E2B

PSEM DUAL INPUTS FAULT (NONE) NOTE:For v5.20 and below this fault is a "SHORT TIME DISPATCH" fault

Both of the landing gear proximity sensor computers have failed with the engine running, no WOWs signal is available

72-00-00-810-101 (LONG DISPATCH)

73216021E1A 73216021E1B 73216021E2A 73216021E2B

RADIO ALTIMETER 1 INPUT FAULT (NONE)

The radio altimeter input No. 1 is invalid (on receiver 1 and 3), but other ARINC inputs are being received

72-00-00-810-025 (LONG DISPATCH)

73216015E1A 73216015E1B 73216015E2A 73216015E2B

REAR ACCELEROMETER FAULT (ENG X SHORT DISPATCH)

Both IEVM outputs for the rear accelerometer are invalid. ARINC communications communications is O and at least 1 front accelerometer signal is O

72-00-00-810-020 (SHORT DISPATCH)

73216121E1A 73216121E1B 73216121E2A 73216121E2B

ROLLBAC (ENG X FAIL)

The engine has been running, but core speed (N2) has dropped below idle unexpectedly


73216624E1A 73216624E1B 73216624E2A 73216624E2B

SLAT/FLAP - ACE INPUT FAULT (NONE)

The ARINC input from the slat/flap angle computer is invalid and the engine is running

72-00-00-810-110 (LONG DISPATCH)

73216218E1A 73216218E1B 73216218E2A 73216218E2B

START ABORT (HOT) (NONE)

Engine start has aborted due to an ITT over temperature condition

72-00-00-810-056 (MAINT. INF. MSGS)

73216221E1A 73216221E1B 73216221E2A 73216221E2B

START ABORT (HUNG) (NONE)

The engine has failed to accelerate to idle in the allotted time. May be due to low starter air pressure, worn starter or engine problems

72-00-00-810-050 (MAINT. INF. MSGS)

73216714E1A 73216714E1B 73216714E2A 73216714E2B

START AND STOP SW INPUTS ON (NONE)

Both start switch and stop switch inputs are on at the same time

72-00-00-810-111 (LONG DISPATCH)

73216717E1A 73216717E1B 73216717E2A 73216717E2B

START SW ON AT POWER UP (ENG X SHORT DISPATCH)

The start switch was in the "start" position when the FADEC powered up

72-00-00-810-113 (SHORT DISPATCH)

73216716E1A 73216716E1B 73216716E2A

START SW ON INPUTS DISAGREE (NONE)

The start switch inputs disagree

72-00-00-810-112 (LONG DISPATCH)


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Dated 05/31/2013


73216716E2B 73217621E1A 73217621E1B 73217621E2A 73217621E2B

T/R ICU NO PRESSURE FAULT (ENG X REV FAIL)



73215225E1A 73215225E1B 73215225E2A 73215225E2B



72-00-00-810-269 (LONG DISPATCH)

73215223E1A 73215223E1B 73215223E2A 73215223E2B




73215226E1A 73215226E1B 73215226E2A 73215226E2B



72-00-00-810-270 (LONG DISPATCH)

73215224E1A 73215224E1B 73215224E2A 73215224E2B




73217614E1A 73217614E1B 73217614E2A 73217614E2B


System commanded to DEPLOY, but held by No. 1 Actuator Loc


73217615E1A 73217615E1B 73217615E2A 73217615E2B


System commanded to DEPLOY, but held by No. 2 Actuator Loc


73217026E1A 73217026E1B 73217026E2A 73217026E2B

T/R ACTUATOR 3 LVDT FAULT (NONE)

TRAS actuator 3 LVDT is out of the range of -10% to 110% or the voltage sum is not in the range of 4 to 6 volts

72-00-00-810-276 (LONG DISPATCH)

73217027E1A 73217027E1B 73217027E2A 73217027E2B

T/R ACTUATOR 4 LVDT FAULT (NONE)

TRAS actuator 4 LVDT is out of the range of -10% to 110% or the voltage sum is not in the range of 4 to 6 volts

72-00-00-810-277 (LONG DISPATCH)


Page 60 of 72


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Dated 05/31/2013


73217024E1A 73217024E1B 73217024E2A 73217024E2B

T/R ACTUATOR DUAL LVDT FAULT (ENG X NO DISPATCH)

Both TRAS LVDTs are failed, position is known only by the lock switches TRAS LVDT position is set at 50%

72-00-00-810-275 (NO DISPATCH)

73215218E1A 73215218E1B 73215218E2A 73215218E2B

T/R COWL LK CMD MON FAILED OFF (ENG X REV PROT FAULT)

No affect on TRAS operation, a sensor of the cowl lock operation has failed to off


73215217E1A 73215217E1B 73215217E2A 73215217E2B

T/R COWL LK CMD MON FAILED ON (ENG X REV PROT FAULT)

No affect on TRAS operation, a sensor of the cowl lock operation has failed to on


73215228E1A 73215228E1B 73215228E2A 73215228E2B

T/R COWL LK SLND FAULT (ENG X REV FAIL)

The TRAS cowl lock has CLOSED before it was expected to close after a stow. This condition may prevent TRAS operation during the next flight


73217618E1A 73217618E1B 73217618E2A 73217618E2B

T/R COWL LOCK FAILED CLOSED (ENG X REV FAIL)

System fails to DEPLOY when commanded, the cowl lock and actuator locks remain CLOSED


73217619E1A 73217619E1B 73217619E2A 73217619E2B

T/R COWL LOCK SWITCH MONITOR (ENG X REV PROT FAULT)

System deployed, but Cowl Lock Switch indicates LOCKED


73217617E1A 73217617E1B 73217617E2A 73217617E2B

T/R COWL LOCK/SWITCH LOCK/SWITCH OPEN (ENG X REV PROT FAULT)

System stowed and unpressurized but Cowl Lock Switch indicates UNLOCKED


73217624E1A 73217624E1B 73217624E2A 73217624E2B

T/R DCU CLOSED STATE FAULT (ENG X REV FAIL)

The TRAS will not DEPLOY when commanded and the actuator locks remain CLOSED. Cowl lock solenoid valve mounted on the DCU Failed to OPEN


73215216E1A 73215216E1B 73215216E2A 73215216E2B

T/R DCU CMD MON FAILED OFF (ENG X REV PROT FAULT)

No affect on TRAS operation but the DCU command monitor has failed to "OFF"


73215215E1A 73215215E1B 73215215E2A 73215215E2B

T/R DCU CMD MONITOR FAILED ON (ENG X REV PROT FAULT)

No affect on TRAS operation but the DCU command monitor has failed to "ON"


73217029E1A 73217029E1B

T/R DCU DUAL RELAYS FAULT

The reverser is unavailable due to



Page 61 of 72


Revision No. 29

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73217029E2A 73217029E2B

(EN G X R EV FAI L )

l oss of b oth DC U control relays

73217623E1A 73217623E1B 73217623E2A 73217623E2B

T/R DCU OPEN STATE FAULT (ENG X REV DEPLOYED)

Reverser fails to stow because the DCU remains in the stow position when DEPLOY is commanded


73217028E1A 73217028E1B 73217028E2A 73217028E2B

T/R DCU RELAY A FAULT (NONE)

Channel A TRAS DCU relay coil has failed

72-00-00-810-278 (LONG DISPATCH)

73217516E1A 73217516E1B 73217516E2A 73217516E2B

T/R DCU RELAY A TEST FAULT (ENG X REV FAIL)

TRAS DCU control relay contact on channel A is invalid. Tested during the pre-engine start test of the TRAS DCU relay. Test is performed after a reset only if the aircraft is on ground, N2 is less than 9.5%, TLA is at idle, MAU is transmitting to the FADEC


73217114E1A 73217114E1B 73217114E2A 73217114E2B

T/R DCU RELAY B FAULT (NONE)

Channel B TRAS DCU relay coil has failed

72-00-00-810-280 (LONG DISPATCH)

73217517E1A 73217517E1B 73217517E2A 73217517E2B

T/R DCU RELAY B TEST FAULT (ENG X REV FAIL)

TRAS DCU control relay contact on channel B is invalid. Tested during the pre-engine start test of the TRAS DCU relay. Test is performed after a reset only if the aircraft is on ground, N2 is less than 9.5%, TLA is at idle, MAU is transmitting to the FADEC


73217629E1A 73217629E1B 73217629E2A 73217629E2B

T/R DCU RELAY FAILED CLOSED (ENG X REV PROT FAULT)

A DCU relay contact has failed CLOSED, or the ADLEN signal is failed to voltage sensed


73215214E1A 73215214E1B 73215214E2A 73215214E2B

T/R DEPLOY COMMAND OFF FAULT (ENG X REV PROT FAULT)

No affect on TRAS operation but the sense of deployment command has failed to "OFF"


73217122E1A

T/R DEPLOYED LOCK

The T/R lock 1

72-00-00-810 -287


Page 62 of 72


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Dated 05/31/2013


73217122E1B 73217122E2A 73217122E2B

SW 1 FAULT (ENG X REV PROT FAULT)

indicates LOCKED when the reverser is deployed as indicated by the TRAS LVDT position sensors

(IN FLIGHT WARNING)

73217124E1A 73217124E1B 73217124E2A 73217124E2B

T/R DEPLOYED LOCK SW 2 FAULT (ENG X REV PROT FAULT)

The T/R lock 2 indicates LOCKED when the reverser is deployed as indicated by the TRAS LVDT position sensors


73215222E1A 73215222E1B 73215222E2A 73215222E2B

T/R ICU CMD MON FAILED CLOSED (ENG X REV PROT FAULT)

No affect on reverser operation. The ICU command monitor has failed to "ON", reducing the test ability


73215221E1A 73215221E1B 73215221E2A 73215221E2B

T/R ICU CMD MON FAILED OPEN (ENG X REV PROT FAULT)

No affect on reverser operation. The ICU command monitor has failed to "OFF", reducing the test ability


73217117E1A 73217117E1B 73217117E2A 73217117E2B

T/R ICU DUAL RELAYS FAULT (ENG X REV FAIL)

The reverser is unavailable due to loss of both ICU control relays


73217514E1A 73217514E1B 73217514E2A 73217514E2B

T/R ICU PRESS SWITCH FAULT (ENG X REV PROT FAULT) NOTE:For v5.20 and below software, this fault is a "Long Time Dispatch" fault

Pressure switch CLOSED when system is not pressurized above switch threshold


73217620E1A 73217620E1B 73217620E2A 73217620E2B

T/R ICU PRESSURE FAULT (ENG X REV PROT FAULT) NOTE:For v5.20 and below this fault is a "NO DISPATCH" fault

System indicates pressure when there is NO PRESSURE command


73217622E1A 73217622E1B 73217622E2A 73217622E2B

T/R ICU PRESSURE SWITCH FAULT (ENG X REV PROT FAULT)



73217116E1A 73217116E1B 73217116E2A 73217116E2B

T/R ICU RELAY A FAULT (NONE)

Channel A TRAS ICU relay coil has failed

72-00-00-810-281 (LONG DISPATCH)


Page 63 of 72


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Dated 05/31/2013


73217118E1A 73217118E1B 73217118E2A 73217118E2B

T/R ICU RELAY B FAULT (NONE)

Channel B TRAS ICU relay coil has failed

72-00-00-810-283 (LONG DISPATCH)

73215219E1A 73215219E1B 73215219E2A 73215219E2B

T/R ICU RELAY FAILED CLOSED (ENG X REV PROT FAULT)

One (or both) ICU control relay contact has failed in the pressure (CLOSED) state


73215220E1A 73215220E1B 73215220E2A 73215220E2B

T/R ICU RELAY FAILED OPEN (ENG X REV FAIL)

Reverser does not DEPLOY when commanded. Both ICU control relay contacts have failed in the non-pressure (OPEN) state


73217121E1A 73217121E1B 73217121E2A 73217121E2B

T/R LOCK SWITCH DUAL FAULT (ENG X NO DISPATCH)

Both of the TR lock switches indicate LOCKED when the reverser is deployed as indicated by the TRAS LVDT position sensors

72-00-00-810-286 (NO DISPATCH)

73217120E1A 73217120E1B 73217120E2A 73217120E2B

T/R LOCK SWITCH DUAL DISAGREE (ENG X NO DISPATCH)

Both reverser locks that the FADEC monitors are OPEN after the reverser is stowed as indicated by the TRAS LVDT position sensors

72-00-00-810-285 (NO DISPATCH)

73217318E1A 73217318E1B 73217318E2A 73217318E2B

T/R LVDT - LOCK SW DISAGREE (ENG X NO DISPATCH)

One TRAS LVDT has failed out of range. The other TRAS LVDT does not agree with the 2 lock switches when they both indicate that the TRAS is stowed

72-00-00-810-090 (NO DISPATCH)

73217023E1A 73217023E1B 73217023E2A 73217023E2B

T/R MECHANICAL FAIL (ENG X REV FAIL) (ENG X REV DEPLOYED) NOTE:The CAS message displayed will depend on whether or not the fault occurred when the T/R was stowed or deployed

The thrust reverser has a mechanical failure. It is failed somewhere between stowed and deployed


73215227E1A 73215227E1B 73215227E2A 73215227E2B

T/R POSITION SENSOR DISAGREE (NONE)

The two TRAS LVDT signals are in range but differ by more than 3.75% stroke for

72-00-00-810-271 (LONG DISPATCH)


Page 64 of 72


Revision No. 29

Dated 05/31/2013


5.3 seconds or more 73216322E1A 73216322E1B 73216322E2A 73216322E2B

T/R SPDA (COWL LOCK) OUTPUT (ENG X REV FAIL)

The SPDA output to energize the TRAS cowl lock is not being turned on


73217123E1A 73217123E1B 73217123E2A 73217123E2B

T/R STOW LOCK SW 2 FAULT (ENG X REV PROT FAULT)

T/R is stowed, but he lock switch 2 indicates UNLOCKED


73217119E1A 73217119E1B 73217119E2A 73217119E2B

T/R STOWED LOCK SW 1 FAULT ENG X REV PROT FAULT)

T/R is stowed, but he lock switch 1 indicates UNLOCKED


73217626E1A 73217626E1B 73217626E2A 73217626E2B

T/R TLA DCU SW FAILED CLOSED (ENG X REV PROT FAULT)

TLA switch fails CLOSED. System will operate normally, but has lost part of one line of defense. Switch is in serried with FADEC controlled DCU control (ground) relay


73217625E1A 73217625E1B 73217625E2A 73217625E2B

T/R TLA DCU SW FAILED OPEN (ENG X REV FAIL)

TLA switch fails OPEN so that TRAS will not DEPLOY when commanded. The DCU solenoid will not be energized. The TLA switch is in series with FADEC controlled DCU control (ground) relay


73217628E1A 73217628E1B 73217628E2A 73217628E2B

T/R TLA COWL LK SW CLOSED (ENG X REV PROT FAULT)

System will operate normally, but has lost part of one line of defense. Switch is in series with FADEC controlled DCU control (ground) relay


73217627E1A 73217627E1B 73217627E2A 73217627E2B

T/R TLA COWL LK SW OPEN (ENG X REV FAIL)

TLA switch fails OPEN so that the TRAS will not DEPLOY, the cowl lock will not OPEN


73216724E1A 73216724E1B 73216724E2A 73216724E2B

T12 T12 ADS ADS - FADE FADEC C DISAGREE (NONE)

T12 engine sensors disagree with the aircraft TAT sensors when the aircraft is in flight or the speed is more than 0.2 MN. Fault inhibited when engine not running or subidle

72-00-00-810-118 (LONG DISPATCH)


Page 65 of 72


Revision No. 29

Dated 05/31/2013


73216721E1A 73216721E1B 73216721E2A 73216721E2B

T12 ALL INPUTS FAULT (ENG X CONTROL FAULT) NOTE:For v5.20 and below, this fault is a "NO DISPATCH" fault

All T12 signals have failed. The TAT inputs and T12 engine sensors failed


73216725E1A 73216725E1B 73216725E2A 73216725E2B

T12 CHAN A-B INPUTS DISAGREE (ENG X SHORT DISPATCH)

The channels A and B T2 sensors disagree by more than 5.56ºC. Signal selection is based on rate of change of T12 and any previous range fault. NOTE: Do not convert 5.56ºC to ºF because in this case, the temperature conversion is not a direct ratio from ºC to ºF

72-00-00-810-119 (SHORT DISPATCH)

73216723E1A 73216723E1B 73216723E2A 73216723E2B


Both of the engine T12 sensors are out of the range of -99.4 to 199.4ºF (-73 to 93ºC)

72-00-00-810-117 (NO DISPATCH)

73216722E1A 73216722E1B 73216722E2A 73216722E2B


The local channel engine T12 sensor is out of the range of 100 to 199ºF (-73 to 93ºC)

72-00-00-810-116 (LONG DISPATCH)

73215428E1A 73215428E1B 73215428E2A 73215428E2B

T25 CHAN A-B INPUTS DISAGREE (ENG X NO DISPATCH)

The two T25 signals differ by more than 50ºF (10ºC). Default signal is one closest to T25 model. Fault may be due to single channel fault if occurs at low sub-idle engine speeds

72-00-00-810-218 (NO DISPATCH)

73215427E1A 73215427E1B 73215427E2A 73215427E2B


Both channels of the T25 sensors are out of range

72-00-00-810-217 (NO DISPATCH)

73215426E1A 73215426E1B 73215426E2A 73215426E2B

T25 OUT OF RANGE (ENG X NO DISPATCH) NOTE: For v5.32 and below, this fault is a "SHORT DISPATCH" fault

T25 sensor is outside expected limits

72-00-00-810-728 (NO DISPATCH)

73215528E1A 73215528E1B 73215528E2A

T3 CHAN A-B INPUTS DISAGREE (ENG X SHORT

The two T3 signals differ by more than 132.1ºF (55.6ºC).

72-00-00-810-239 (SHORT DISPATCH)


Page 66 of 72


Revision No. 29

Dated 05/31/2013


7 321 5 528 E2B

D I SPA T CH)

We i g h t e d a v er a g i n g starts starts at 27.8 27.8º º delta delta. . Default signal is one closest to T3 model. Fault inhibited when engine not running or subidle

73215527E1A 73215527E1B 73215527E2A 73215527E2B


Both of the T3 sensors are out of range. Fault is inhibited until the engine is close to idle or above

72-00-00-810-238 (NO DISPATCH)

73215526E1A 73215526E1B 73215526E2A 73215526E2B


T3 sensor is outside expected limits. Fault inhibited when engine not running or subidle

72-00-00-810-237 (LONG DISPATCH)

73217020E1A 73217020E1B 73217020E2A 73217020E2B



72-00-00-810-123 (LONG DISPATCH)

73217022E1A 73217022E1B 73217022E2A 73217022E2B

TAT OUT OF RANGE (ADS1-2) (NONE)

ADS1 and ADS2 TAT signals are invalid or are out of -99.4ºF to 200.3ºF (-73 to 93.5ºC) when the aircraft is in flight or the speed is more than 0.2 MN

72-00-00-810-125 (LONG DISPATCH)

73217021E1A 73217021E1B 73217021E2A 73217021E2B



72-00-00-810-124 (LONG DISPATCH)

73215523E1A 73215523E1B 73215523E2A 73215523E2B

TBV TBV CMD CMD - CURR CURREN ENT T DISAGREE (NONE)


72-00-00-810-234 (LONG DISPATCH)

73215520E1A 73215520E1B 73215520E2A 73215520E2B

TBV TBV CMD CMD - POSITI POSITION ON DISAGREE (ENG X NO DISPATCH) NOTE: For v5.32 and below, this fault is a "SHORT DISPATCH" fault

The TBV position is more than 5 percent from the demanded position. The sensor and torque motor values are O , the sensor has been valid for more than 2.0

72-00-00-810-729 (NO DISPATCH)


Page 67 of 72


Revision No. 29

Dated 05/31/2013


seconds 73215522E1A 73215522E1B 73215522E2A 73215522E2B

TBV DUAL CMD CURRENT DISAGREE (ENG X NO DISPATCH) NOTE: For v5.32 and below, this fault is a "SHORT DISPATCH" fault

Dual channel failure in the torque motor driver circuits. TBV will slew to the FAIL SAFE position

72-00-00-810-730 (NO DISPATCH)

73215524E1A 73215524E1B 73215524E2A 73215524E2B

TBV DUAL SENSOR RANGE FAULT (ENG X NO DISPATCH) NOTE: For v5.32 and below, this fault is a "SHORT DISPATCH" fault

Both TBV position feedback sensors have failed. Default TBV position of 100 percent is assigned. TBV will slew to the FAIL SAFE position

72-00-00-810-731 (NO DISPATCH)

73215521E1A 73215521E1B 73215521E2A 73215521E2B

TBV SENSOR RANGE FAULT (NONE)

Local channel TBV position feedback sensor is out of the range of -10 to 110 percent stroke or the voltage sum is out of the range of 4.0-6.7 volts. Cross channel sensor is used

72-00-00-810-232 (LONG DISPATCH)

73215525E1A 73215525E1B 73215525E2A 73215525E2B

TBV SENSORS CHAN AB DISAGREE (ENG X SHORT DISPATCH)

The two TBV position feedback sensors are in range but disagree by more than 5 percent stroke. Sensor is selected based on rate of change and previously failed sensor

72-00-00-810-236 (SHORT DISPATCH)

73216414E1A 73216414E1B 73216414E2A 73216414E2B

THRUST CONTROL MALFUNCTION (ENG X FAIL)

The measured fan speed exceeds the commanded fan speed plus 6 percent margin. An engine shutdown occurs for this condition when on the ground and not at take-off


73216522E1A 73216522E1B 73216522E2A 73216522E2B

TLA DUAL SIGNAL OUT OF RANGE (ENG X TLA FAIL)

Both of the Thrust Lever Angle (TLA) sensors are invalid or signals are out of range of -4.5 to 88 degrees or the RVDT sum voltages are out of allowable range of 6.65 to 8.06 volts. A variable default value is used for TLA after 0.096 seconds of



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failure 73216523E1A 73216523E1B 73216523E2A 73216523E2B

TLA SIGNAL OUT OF RANGE (ENG X NO DISPATCH)

Local channel Thrust Lever Angle (TLA) sensor is invalid or out of range of -4.5 to 88 degrees or the RVDT sum voltage is out of allowable range of 6.65 to 8.06 volts

72-00-00-810-095 (NO DISPATCH)

73216524E1A 73216524E1B 73216524E2A 73216524E2B

TLA SIGNALS DISAGREE (ENG X NO DISPATCH)

The TLA sensor inputs disagree by more than 3.75 Degrees. Rate of change (160 Deg/0.016 second interaction) interaction) and result of previous range tests are used to isolate the invalid signal

72-00-00-810-096 (NO DISPATCH)

73217515E1A 73217515E1B 73217515E2A 73217515E2B

TR ICU VALVE FAILED OPEN (ENG X NO DISPATCH) NOTE:For v5.20 and below software, this fault is a "Long Time Dispatch" fault

System pressurized, pressurized, but ICU indicated T/R is inhibited

72-00-00-810-345 (NO DISPATCH)

73215425E1A 73215425E1B 73215425E2A 73215425E2B

VBV CHAN A-B SENSORS DISAGREE (ENG X NO DISPATCH)

The two VBV position 72-00-00-810-224 feedback sensors are (NO DISPATCH) in range but disagree by more than 10 percent stroke. Sensor is selected based on rate of change and previously failed sensor

73215423E1A 73215423E1B 73215423E2A 73215423E2B

VBV CMD - CURRENT DISAGREE (ENG X SHORT DISPATCH)


72-00-00-810-222 (SHORT DISPATCH)

73215420E1A 73215420E1B 73215420E2A 73215420E2B

VBV CMD - POSITION DISAGREE (ENG X SHORT DISPATCH)

The VBV position is more than 5 percent from the demanded position. The sensor and torque motor values are O , the sensor has been valid for more than 2.0 seconds

72-00-00-810-219 (SHORT DISPATCH)

73215422E1A 73215422E1B 73215422E2A 73215422E2B

VBV DUAL CMD CURRENT DISAG (ENG X CONTROL FAULT)

Dual channel failure in the torque motor driver circuits. VBV will slew to the FAIL



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Dated 05/31/2013


SAFE position 73215424E1A 73215424E1B 73215424E2A 73215424E2B

VBV DUAL SENSOR RANGE FAULT (ENG X CONTROL FAULT) NOTE:For v5.20 and below this fault is a "NO DISPATCH" fault

Both VBV position feedback sensors have failed. VBV position is set to 100 percent OPEN. VBV will slew to the FAIL SAFE position


73215421E1A 73215421E1B 73215421E2A 73215421E2B

VBV SENSOR RANGE FAULT (ENG X SHORT DISPATCH) NOTE: For v5.32 and below, this fault is a "LONG DISPATCH" fault

Local channel VBV position feedback sensor is out of the range of -10 to 110 percent stroke or the voltage sum is out of the range of 6.9-9.3 volts. Cross channel sensor is used

72-00-00-810-722 (SHORT DISPATCH)

73215419E1A 73215419E1B 73215419E2A 73215419E2B

VSV CHAN A-B SENSORS DISAGREE (ENG X NO DISPATCH)

The two VSV position feedback sensors are in range but disagree by more than 5 percent stroke. Sensor is selected based on rate of change and previously failed sensor

72-00-00-810-215 (NO DISPATCH)

73215417E1A 73215417E1B 73215417E2A 73215417E2B

VSV CMD - CURRENT DISAGREE (ENG X SHORT DISPATCH)


72-00-00-810-213 (SHORT DISPATCH)

73215414E1A 73215414E1B 73215414E2A 73215414E2B

VSV CMD - POSITION DISAGREE (ENG X CONTROL FAULT) NOTE:For v5.20 and below software CAS Message is "IN FLIGHT WARNING"

The VSV position is more than 5 percent from the demanded position. The sensor and torque motor values are O , the sensor has been valid for more than 2.0 seconds

72-00-00-810-210 (NO DISPATCH)

73215416E1A 73215416E1B 73215416E2A 73215416E2B

VSV DUAL CMD CURRENT DISAGREE (ENG X NO DISPATCH) NOTE: For v5.32 and below, this fault is an "IN FLIGHT WARNING" fault

Dual channel failure in the torque motor driver circuits. VSV will slew to the FAIL SAFE position

72-00-00-810-727 (NO DISPATCH)

73215418E1A 73215418E1B 73215418E2A 73215418E2B

VSV DUAL SENSOR RANGE FAULT (ENG X CONTROL FAULT)

Both VSV position feedback sensors have failed. VSV position is set to 100 percent CLOSED. VSV will slew



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to the FAIL SAFE position 73215415E1A 73215415E1B 73215415E2A 73215415E2B

VSV SENSOR RANGE FAULT (ENG X SHORT DISPATCH) NOTE: For v5.32 and below, this fault is an "LONG DISPATCH" fault

Local channel VSV position feedback sensor is out of the range of -10 to 110 percent stroke or the voltage sum is out of the range of 6.9-9.3 volts. Cross channel sensor is used

72-00-00-810-721 (SHORT DISPATCH)

73217228E1A 73217228E1B 73217228E2A 73217228E2B

WOW ARINC DISAGREE (NONE) NOTE:For v5.20 and below this fault is a "SHORT DISPATCH" fault

The two MLG WOW inputs on ARINC are valid, but differ with the engine running

72-00-00-810-156 (LONG DISPATCH)

73217227E1A 73217227E1B 73217227E2A 73217227E2B

WOW DUAL ARINC FAULT (NONE) NOTE:For v5.20 and below this fault is a "SHORT DISPATCH" fault

Both MLG WOW inputs on ARINC are invalid and the engine is running

72-00-00-810-155 (LONG DISPATCH)

73217321E1A 73217321E1B 73217321E2A 73217321E2B

WOW DUAL NLG FAULT (NONE)

Both NLG WOW inputs on ARINC are invalid and the engine is running

72-00-00-810-164 (LONG DISPATCH)

73217316E1A 73217316E1B 73217316E2A 73217316E2B

WOW HARDWIRE ARINC DISAGREE (ENG X NO DISPATCH)

The WOW inputs on ARINC agree and the WOW hardwired inputs are valid and agree, but the ARINC and hardwired inputs differ

72-00-00-810-159 (NO DISPATCH)

73217226E1A 73217226E1B 73217226E2A 73217226E2B

WOW HARDWIRE ARINC FAULT (ENG X NO DISPATCH)

All MLG WOW inputs are invalid

72-00-00-810-154 (NO DISPATCH)

73217314E1A 73217314E1B 73217314E2A 73217314E2B

WOW HARDWIRE DISAGREE (ENG X NO DISPATCH)

The two MLG WOW inputs from hardware discretes are valid, but differ

72-00-00-810-157 (NO DISPATCH)

73217315E1A 73217315E1B 73217315E2A 73217315E2B

WOW MLG-NLG DISAGREE (NONE)

The WOW inputs from the MLG are valid and agree, and the WOW inputs from the NLG are valid and agree, but the selected MLG and NLG values disagree with the engine running

72-00-00-810-158 (LONG DISPATCH)


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Dated 05/31/2013


73217323E1A 73217323E1B 73217323E2A 73217323E2B

WOW NLG DISAGREE (NONE)

The two NLG WOW inputs on ARINC are valid, but differ with the engine running

72-00-00-810-166 (LONG DISPATCH)

73217322E1A 73217322E1B 73217322E2A 73217322E2B



72-00-00-810-165 (LONG DISPATCH)

73217325E1A 73217325E1B 73217325E2A 73217325E2B



72-00-00-810-168 (LONG DISPATCH)

73217317E1A 73217317E1B 73217317E2A 73217317E2B



72-00-00-810-160 (LONG DISPATCH)

73217319E1A 73217319E1B 73217319E2A 73217319E2B



72-00-00-810-162 (LONG DISPATCH)

73217427E1A 73217427E1B 73217427E2A 73217427E2B

XENG SOFTWARE VERSION DISAGREE (ENG X NO DISPATCH) NOTE: Deleted

The local engine and cross engine AS software versions disagree

72-00-00-810-344 (NO DISPATCH)


Page 72 of 72

Engine Fault Code

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