A318/A319/A320 NORMAL CHECKLIST BEFORE START
APPROACH (BELOW FL 180)
Log Book/S Book/Secu ecurit rityy Check. Check. . . . . . . . .Checke .Checked/E d/Ente ntered red
(CR) (CR)
Appro Approach ach Brief Brief . . . . . . . . . . . . . . . . . . . . . . .Complet .Completed ed
(CR) (CR)
Departu Departure re Brie Brieff . . . . . . . . . . . . . . . . . . . . . . Comple Complete ted d
(CR) (CR)
ECAM Status. Status. . . . . . . . . . . . . . . . . . . . . . . . . . .Checked .Checked
(CR)
Cockpi Cockpitt Prep Prep . . . . . . . . . . . . . . . . . . . . . . . . Comple Complete ted d
(CR) (CR)
Baro Baro & MDA MDA/DH. /DH. . . . . . . . . . . . . . . . . . . . . . . . .___ .___ Set Set
(CR) (CR)
Cabi Cabin n Sig Signs ns . . . . . . . . . . . . . . . . . . . .On, Auto Auto & Arm Armed ed
(C) (C)
Seat Belt Signs. . . . . . . . . . . . . . . . . . . . . . . . . . . . . On
(PNF)
ADIR ADIRS. S. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Nav Nav
(C) (C)
Autobrak Autobrake e . . . . . . . . . . . . . . . . . . . . . . Low / Med / Off
(PNF)
Fuel Fuel . . . . . . . . . . . . . . .Rlsd .Rlsd With With __ , __ __ Lbs Lbs On Boar Board d
(C) (C)
Baro Baro R Ref. ef. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .___Set .___Set
(CR) (CR)
Park Parkin ing g Bra Brake ke . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . On
(C) (C)
Takeoff akeoff Data Data . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Set
(CR) (CR)
Beac Beacon on . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . On
(C) (C)
NW Strg Strg Disc. Disc. . . . . . . . . . . . . . . . . . . . . . . . . . Check Checked ed
(C) (C)
Windo Windows, ws, Doors Doors & Slides. Slides. . . . . . . . . . Clos Closed ed & Armed Armed
(CR) (CR)
Cock Cockpi pitt Doo Doorr . . . . . . . . . . . . . . . . . . . Clos Closed ed & Loc Locke ked d
(F) (F)
AFTER START
LANDING Cabin Signal Signal . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Given Given
(PNF)
A/Thr A/Thr . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Spee Speed d / Off Off
(PF) (PF)
Landin Landing g Gear Gear . . . . . . . . . . . . . . . Down Down & Three Three Green Green
(CR) (CR)
ECAM ECAM Memo. Memo. . . . . . . . . . . . . . . . . . . . . . . .Ldg No No Blue Blue
(CR) (CR)
AFTER LANDING (SILENT) Flap Flaps s . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Retr .Retrac acte ted d
(F) (F)
Land Landin ing g Lig Light hts s . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Off
(F) (F)
Spoi Spoile lers. rs. . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Disa .Disarm rmed ed
(F) (F)
Anti Anti-i -ice. ce. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .On / Off
(C) (C)
Rada Radarr & Pred Predic icti tive ve W/S. W/S. . . . . . . . . . . . . . . . . . . . . . Off
(F) (F)
Pitch Pitch Trim Trim.. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .___Set .___Set
(CR) (CR)
TCAS TCAS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Stby Stby
(F) (F)
Rudd Rudder er Trim rim . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Zero .Zero
(F) (F)
APU APU . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . On On / Off Off
(F) (F)
ECAM ECAM Stat Status us (two (two-en -engin gine e start start only only)) . . . . . . . Check Checked ed
(CR) (CR)
Yellow Yellow Electric Pump . . . . . . . . . . . . . . . . . . . . . . . On
(F)
Engine 2 Generator Generator . . . . . . . . . . . . . . . . . . . . . . . . Off
(F)
SINGLE ENGINE TAXI IN APU (if required at gate) gate) . . . . . . . . . . . . . . . . . . . Start
(F)
Ensure APU AVAIL light on prior to shutting down #2 engine.
SECOND ENGINE START
Yellow Yellow Electric Pump. . . . . . . . . . . . . . . . . . . . . . . . On
(F)
Yellow Yellow Electric Pump . . . . . . . . . . . . . . . . . . . . . . . Off
(F)
Challenge . . . . . . . . . “Off the Steering and and Brakes”
(F)
Engine 2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Start
(F)
Engine 2 Master . . . . . . . . . . . . . . . . . . . . . . . . . . . Off
(F)
Anti-ice . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . On / Off
(F)
SINGLE ENGINE APU START
Challenge . . . . . . . . . “Of f the Steering and Brakes” Brakes”
(F)
If the APU is required after Engine 2 is shutdown
Engine 2 Generator Generator . . . . . . . . . . . . . . . . . . . . . . . . On
(F)
APU Generator. . . . . . . . . . . . . . . . . . . . . . . . . . . . . Off
(F)
APU Bleed/APU Master. . . . . . . . . . . . . . . . . . On/Off
(F)
APU . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Start
(F)
ECAM Status. . . . . . . . . . . . . . . . . . . . . . . . . Checked
(CR)
BEFORE TAKEOFF
When APU AVAIL light is illuminated: Challenge . . . . . . . . . “Off the Steering and and Brakes”
(F)
APU Generator Generator . . . . . . . . . . . . . . . . . . . . . . . . . . . . . On
(F)
Takeoff akeoff Brie Brieff . . . . . . . . . . . . . . . . . . . . . . . . Compl Complet eted ed
(CR) (CR)
Flight Flight Contro Controls. ls. . . . . . . . . . . . . . . . . . . . . . . . . Check Checked ed
(CR) (CR)
Flight Flight Instru Instrumen ments ts . . . . . . . . . . . . . . . . . . . . . Check Checked ed
(CR) (CR)
Park Park Brk Brk & Cho Chock cks s . . . . . . . . . . . . . . . . . . . . . . .On & In In
(C) (C)
Flaps Flaps . . . . . . . . . . . . . . . . . . . . . . . ___Planne ___Planned d __ ___Se _Sett
(CR) (CR)
Engi Engine ne(s (s). ). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Off
(C) (C)
ECAM ECAM Memo Memo . . . . . . . . . . . . . . . . . . . . . . . T.O. No Blue Blue
(CR) (CR)
Beac Beacon on . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Off
(C) (C)
Seat Seat Bel Beltt Sig Signs. ns. . . . . . . . . . . . . . . . . . . . . . . . . . . . . Off
(C) (C)
Cabi Cabin n Sig Signa nall . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Given .Given
(F) (F)
Emer Emerg g Exi Exitt Lig Light hts s . . . . . . . . . . . . . . . . . . . . . Arme Armed/ d/Off Off
(C) (C)
TCAS TCAS.. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . TA/RA A/RA
(F) (F)
Yellow Electric Pump . . . . . . . . . . . . . . . . . . . . . . . . Off
(C)
Pack Packs s . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Off Off
(F) (F)
Fuel Fuel Pump Pumps. s. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Off
(C) (C)
AFTER TAKEOFF (SILENT)
PARKING
SECURING
Ldg Gear . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Up
(PNF)
Parking Parking Brake Brake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . On
(F/C)
Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Retract Retracted ed
(PNF) (PNF)
ADIRS ADI RS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Off
(F/C) (F/C)
Packs. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . On
(PNF) (PNF)
Oxygen Oxygen . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Off
(F/C) (F/C)
ECAM Memo . . . . . . . . . . . . . . . . . . . . . . . . . . Checked Checked
(PNF) (PNF)
Exterior Exterior Lights. Lights. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Off
(F/C)
Cabin Cabin Signs Signs & Emerg Emerg Exit Exit Light Lights s . . . . . . . . . . . . . . . Off
(F/C) (F/C)
APU & BAT. BAT. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Off
(F/C)
NOTE: Checklist items presented in BOLD type repre sent Single Engine Taxi Taxi procedures and are “Read and Do” items.
676011 Rev. 12
FAA Approved 04/17/06
A318/A319/A320 SUPPLEMENTAL CHECKLIST Refer to FOM Volume II, Chapter 5.10 for expanded information.
NOTE: In the following procedures, the F/O should read and the captain should execute the actions.
MANUAL ENGINE START Thr Levers . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Idle Eng Mode Selector . . . . . . . . . . . . . . . . . . . . . . . Norm then Ign Eng Man Start . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . On When N2 reaches max motoring speed (min 20%) Master Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . On ECAM Displays . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Check When N2 reaches 50% ECAM Displays . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Check Eng Idle Parameters . . . . . . . . . . . . . . . . . . . . . . Check Normal Man Start . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Off Eng Mode Selector . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Norm In the event of a start malfunction Man Start (affected) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Off Eng Master (affected). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Off
Crossbleed Engine Start Adjust thrust of supplying engine to obtain 30 PSI at start valve prior to (and at least 25 PSI during) crossbleed start. If Starting Prior to Taxi Before Start Checklist . . . . . . . . . . . . . . . . . . . . . . . . Complete APU Bleed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Off Eng Bleed (running engine) . . . . . . . . . . . . . . . . . . . . . . . . . . On Eng Bleed (receiving engine). . . . . . . . . . . . . . . . . . . . . . . . .Off X Bleed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Open If Starting Af ter Single Engine Taxi: Yellow Electric Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Off APU Bleed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Off Eng Bleed (running engine) . . . . . . . . . . . . . . . . . . . . . . . . . . On Eng Bleed (receiving engine). . . . . . . . . . . . . . . . . . . . . . . . .Off X Bleed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Open After start Thrust Lever (supplying engine) . . . . . . . . . . . . . . . . . . . . . Idle X Bleed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Auto Eng Bleed (receiving engine). . . . . . . . . . . . . . . . . . . . . . . . . On Packs. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Check On After Start Checklist. . . . . . . . . . . . . . . . . . . . . . . . .Accomplish
– Mode Sel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Crank – Man Start (affected) . . . . . . . . . . . . . . . . . . . . . . . . . . . . .On
Crosswind Component
NOTE: The last two lines are not displayed on the ECAM. Dry crank the engine for 30 seconds. The start valve automatically reopens when N2 is below 20%. The pilot must decide whether to attempt a new start, or to report the no start condition for appropriate maintenance action.
Start Valve Manual Operation Audio Control Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Cab When ground crew member is ready, order “START 1(2)” Eng Mode Sel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Ign Eng Master . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . On Start Valve. . . . . . . . . . . . . . . . . Order “Open and Keep Open” When N2 at 50% Start Valve. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Order “Close”
Engine Start w/Ext Pneumatic Power Before connecting external pneumatic power Packs 1 and 2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Off Before start APU Bleed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Off Eng Bleed (both engines). . . . . . . . . . . . . . . . . . . . . . . . . . . Off X Bleed (if starting engine 2) . . . . . . . . . . . . . . . . . . . . . . Open Cleared to start Brake Accum Press. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Check Engine 1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Start Normal Engine Start Procedures. . . . . . . . . . . . . . . . . . . Apply NOTE: Consider using manual engine start procedure in case of low air pressure. See FOM II, Chapter 5.10. After Engine 1 (2) is started External Power . . . . . . . . . . . . . . . . . . . . . . . . . . . Off/Removed Packs 1 and 2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . On Eng Bleed (running engine) . . . . . . . . . . . . . . . . . . . . . . . . . .On
676011 Rev. 12
Enter the graph by following the “Wind Direction Relative to Runway” radial li ne until it intersects the windspeed. From the point of intersection, determine the headwind/tailwind component by moving horizontally to the left, and the crosswind component by moving vertically down.
FAA Approved 04/17/06
A318/A319/A320 LANDING DATA A318 LANDING DISTANCE (WITHOUT AUTOBRAKE) – CONF FULL (FEET) WEIGHT (1000 LB) n o i t i d n o C y a w n u R
80
90
100
110
120
130
140
150
Dry
2180
2180
2170
2260
2370
2480
2620
2810
Wet
2820
2850
2860
3040
3260
3480
3710
3950
1/4 in Water
3870
3950
4010
4290
4640
5010
5400
5800
1/2 in Water
3700
3790
3860
4120
4450
4790
5150
5510
1/4 in Slush
3780
3850
3920
4180
4490
4780
5110
5480
1/2 in Slush
3640
3720
3790
4050
4340
4620
4930
5280
Compact Snow
3750
3790
3830
4050
4300
4540
4800
5060
Ice
7860
7940
8040
8410
8860
9280
9760
10230
A318 CORRECTIONS ON ACTUAL LANDING DISTANCE – CONF FULL Rwy Condition 1000 ft above SL r e P
Dry
Wet
1/4 in Water
1/2 in Water
1/4 in Slush
1/2 in Slush
Compact Snow
Ice
+ 3%
+ 3%
+ 4%
+ 3%
+ 4%
+ 4%
+ 3%
+ 3%
10 kt headwind 10 kt tailwind
No correction for headwind due to wind correction on approach speed + 19%
+ 23%
+ 25%
+ 23%
+ 23%
+ 21%
+ 19%
+ 38%
5 kt speed increment (and no failure) add 8% (all runways)
A319 LANDING DISTANCE (WITHOUT AUTOBRAKE) – CONF FULL (FEET) WEIGHT (1000 LB) n o i t i d n o C y a w n u R
90
100
110
120
130
140
150
160
170
Dry
2280
2270
2330
2440
2540
2650
2800
3110
3380
Wet
2980
2990
3140
3360
3540
3750
3990
4240
4410
1/4 in Water
4040
4110
4330
4670
5000
5330
5730
6130
6390
1/2 in Water
3870
3940
4150
4470
4770
5080
5440
5780
6060
1/4 in Slush
3950
4010
4230
4520
4770
5040
5400
5780
6030
1/2 in Slush
3800
3870
4080
4360
4600
4860
5190
5550
5780
Compact Snow
3890
3920
4090
4330
4530
4740
4990
5240
5380
Ice
8200
8290
8610
9030
9380
9770
10240
10730
11010
CORRECTIONS ON ACTUAL LANDING DISTANCE – CONF FULL Rwy Condition 1000 ft above SL r e P
Dry
Wet
1/4 in Water
1/2 in Water
1/4 in Slush
1/2 in Slush
Compact Snow
Ice
+ 3%
+ 3%
+ 4%
+ 4%
+ 5%
+ 4%
+ 3%
+ 3%
No correction for headwind due to wind correction on approach speed
10 kt headwind 10 kt tailwind
+ 20%
+ 23%
+ 25%
+ 23%
+ 24%
+ 21%
+ 19%
+ 35%
Per 5 kt speed increment (and no failure) add 8% (all runways)
A320 LANDING DISTANCE (WITHOUT AUTOBRAKE) – CONF FULL (FEET) WEIGHT (1000 LB) n o i t i d n o C y a w n u R
100
110
120
130
140
150
160
170
180
Dry
TBD
TBD
TBD
TBD
TBD
TBD
TBD
TBD
TBD
Wet
TBD
TBD
TBD
TBD
TBD
TBD
TBD
TBD
TBD
1/4 in Water
TBD
TBD
TBD
TBD
TBD
TBD
TBD
TBD
TBD
1/2 in Water
TBD
TBD
TBD
TBD
TBD
TBD
TBD
TBD
TBD
1/4 in Slush
TBD
TBD
TBD
TBD
TBD
TBD
TBD
TBD
TBD
1/2 in Slush
TBD
TBD
TBD
TBD
TBD
TBD
TBD
TBD
TBD
Compact Snow
TBD
TBD
TBD
TBD
TBD
TBD
TBD
TBD
TBD
Ice
TBD
TBD
TBD
TBD
TBD
TBD
TBD
TBD
TBD
CORRECTIONS ON ACTUAL LANDING DISTANCE – CONF FULL Rwy Condition 1000 ft above SL r e P
Dry
Wet
1/4 in Water
1/2 in Water
1/4 in Slush
1/2 in Slush
Compact Snow
Ice
TBD
TBD
TBD
TBD
TBD
TBD
TBD
TBD
10 kt headwind 10 kt tailwind
No correction for headwind due to wind correction on approach speed TBD
TBD
TBD
TBD
TBD
Per 5 kt speed increment (and no failure) TBD 676011 Rev. 12
TBD
TBD
TBD
°C
°F
-40 -39 -38 -37 -36 -35 -34 -33 -32 -31 -30 -29 -28 -27 -26 -25 -24 -23 -22 -21 -25 -20 -19 -18 -17 -16 -15 -14 -13 -12 -11 -10 -9 -8 -7 -6 -5 -4 -3 -2 -1 0 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 49
-40 -38 -36 -35 -33 -31 -29 -27 -26 -24 -22 -20 -18 -17 -15 -13 -11 -9 -8 -6 -13 -4 -2 0 1 3 5 7 9 10 12 14 16 18 19 21 23 25 27 28 30 32 34 36 37 39 41 43 45 46 48 50 52 54 55 57 59 61 63 64 66 68 70 72 73 75 77 79 81 82 84 86 88 90 91 93 95 97 99 100 102 104 106 108 109 111 113 115 117 118 120
FAA Approved 04/17/06
A318/A319/A320 EMERGENCY QUICK REFERENCE CHECKLIST ENGINE TAILPIPE FIRE
ENGINE FAIL AT CRUISE STRATEGY
CAUTION External fire agents can cause severe corrosive damage and therefore should only be considered after having applied the following procedure. – – – – – •
MAN START . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF ENG MASTER (affected). . . . . . . . . . . . . . . . . . . . . . . . . . OFF AIR BLEED PRESS . . . . . . . . . . . . . . . . . . . . . . . .ESTABLISH ENG MODE SEL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CRANK MAN START . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON When burning stopped: – MAN START . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF – ENG MODE SEL. . . . . . . . . . . . . . . . . . . . . . . . . . . .NORM End of Procedure
– – – – – –
ECAM ACTIONS / MCT (Simultaneously) . . . . . INITIATE / SET AUTOTHRUST . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF CRUISE FL (PROG Page) . . . . . . . . . . . . . . . . . . DETERMINE ATC . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NOTIFY SPEED ON FCU . . . . . M.78, 300 KT / GREEN DOT – PULL ALTITUDE ON FCU . . . . . . . . . . . . CRUISE FL – SET & PULL
Refer to FOM II, Chapter 9 – Additional Procedural Techniques
EMERGENCY DESCENT – OXYGEN MASKS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON – CREW COMMUNICATION . . . . . . . . . . . . . . . . . ESTABLISH
NOTE: Set the oxygen diluter selector to the N position. With the oxygen diluter selector left at 100%, oxygen quantity may be insufficient to cover the entire emer gency descent profile.
SMOKE/FUMES IF PERCEPTIBLE SMOKE APPLY IMMEDIATELY: – OXYGEN MASKS. . . . . . . . . . . . . . . . ON / 100% / EMERG – CREW COMMUNICATION . . . . . . . . . . . . . . . . .ESTABLISH – LAND ASAP – CAB FANS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF – BLOWER . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OVRD – EXTRACT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OVRD – GALLEY & CAB . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF – CABIN SIGNS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON – CABIN COMMUNICATION . . . . . . . . . . . . . . . . . . .ESTABLISH – FAULT EQUIP (if identified). . . . . . . . . . . . . . . . . . . . ISOLATE IF DENSE SMOKE, at any time of the procedure: – EMER EXIT LIGHTS. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON – SMOKE/TOXIC FUMES REMOVAL . . . . . . . . . . . . . . . . APPLY – EMER ELEC CONFIG. . . . . . . . . . . . . . . . . . . . . . . CONSIDER Refer to FOM Volume II, Chapter 4.10
The recommendation is to descend with the AP engaged: – Turn the ALT selector knob and pull. – Turn the HDG selector knob and pull. – Adjust the target SPD/MACH. – Use of the autopilot is also permitted in EXPEDITE mode. – THRUST LEVERS (If A/THR not engaged). . . . . . . . . . . IDLE – SPD BRK . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL – Extension of the speedbrakes will significantly increase VLS. – In order to avoid AP disconnection and automatic retraction of speedbrakes due to possible activation of angle of attack protection, allow the speed to increase before starting to use speedbrakes – SPEED . . . . . . . . . . . . . . . . . . . . . . . . . . MAX APPROPRIATE Refer to FOM Volume II, Chapter 4.10
LOSS OF BRAKING • IF – • IF –
UNRELIABLE SPEED INDICATION Unreliable speed indication may be caused by radome destruction or frozen pitots. CAUTION If the failure is due to radome destruction, the drag will increase and therefore N1 must be increased 5%. Fuel flow will increase by about 27%. – CROSSCHECK INSTRUMENTS
AUTOBRAKE IS SELECTED: BRAKE PEDALS. . . . . . . . . . . . . . . . . . . . . . . . . . . . PRESS NO BRAKING AVAILABLE: REV . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .MAX
– BRAKE PEDALS . . . . . . . . . . . . . . . . . . . . . . . . .RELEASE – A /SKID & NW STRG . . . . . . . . . . . . . . . . . . . . . . . . . OFF – BRAKE PEDALS . . . . . . . . . . . . . . . . . . . . . . . . . . . PRESS – MAX BRAKE PRESS . . . . . . . . . . . . . . . . . . . . . 1000 PSI • IF STILL NO BRAKING: – PARKING BRAKE . . . . . . . . . . SHORT AND SUCCESSIVE APPLICATIONS
• If unable to establish reliable source, perform the following action items: – THRUST/PITCH – Below THR RED ALT . . . . . . . . . . . . . . . . . . . . 15 /TOGA – Above THR RED ALT and Below FL 100 . . . . . . . .10 /CL – Above THR RED ALT and Above FL 100 . . . . . . . . . 5 /CL – AP/FD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF – A/THR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF – FLAPS . . . . . . . . . . . . . . . . . . . MAINTAIN CURRENT CONFIG – SPEEDBRAKES. . . . . . . . . . . . . . . . . . . . . .CHECK RETRACT If failure is detected while in CONF FULL and go-around is initiated, select CONF 3. – LANDING GEAR . . . . . . . . . . . . . . . . . UP WHEN AIRBORNE Refer to FOM Volume II, Chapter 4.10
End of Procedure
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ON GROUND EMERGENCY / EVACUATION – AIRCRAFT / PARKING BRK . . . . . . . . . . . . . . . . . STOP / ON – ATC (VHF) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NOTIFY – P . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK ZERO If not zero, MODE SEL on MAN, V/S CTL FULL UP. – ENGINE MASTER 1 AND 2 . . . . . . . . . . . . . . . . . . . . . . . OFF – NOTIFY CABIN CREW. . . . . . . . . . . . (PA) “REMAIN SEATED” – FIRE P/Bs (ENG and APU). . . . . . . . . . . . . . . . . . . . . . PUSH – AGENTS (ENG and APU) . . . . . . . . . . . . . . . . . . . . .AS RQRD – EVACUATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . INITIATE End of Procedure
NOTE: Shaded checklist items (presented in BOLD ITALIC type) represent memory items. These should be accomplished from memory prior to consulting this Emergency QRC.
676011 Rev. 12
FAA Approved 04/17/06
