AHM560 737-500 Rev9 Trim UTair

Airport Handling Manual

AHM-560 A HM-560

Boeing 737-500 VP-BVL VP-BVN VP-BVZ VQ-BAC VQ-BAE VP-BXQ VP-BXV VP-BXY

VP-BYK VP-BYL VP-BYM VQ-BAD VP-BXO VP-BXR VP-BXU VP-BXZ

AHM560 B 737-500 737-500

Rev. 9

02-Oct-2009 02-Oct-200 9

Air A ir po r t Handl Han dl in g Manu al

A HM 560

COMMUNICATION ADDRESSES

EDP-SYSTEM SEMI-PERMANENT SEMI-PERMANENT DATA

A Sheet 1 Carrier UT

1.

SUPPLIERS’ SUPPLIERS’ CONTACT ADDRESS Completed Completed sheets and changes of b asic data and procedure must be forw arded arded to:

MAILING ADDRESS:

TELETYPE ADDRESS:

E-MAIL ADDRESS:

REMARKS:

2.

CARRIER’S CONTACT ADDRESS MAILING ADDRESS:

UTair Aviation, Khanty-Mansiysk Khanty-Mansiysk airport, Khanty-Mansiysk Khanty-Mansiysk autonomous district, Tyumen region, 628012, Russia

TELETYPE ADDRESS:

E-MAIL ADDRESS:

[email protected] [email protected] .ru

REMARKS:

Completed by: (Signature)

A.Nutretsov

AHM 560 B737-500

Issue No.: A1/1.0 Date: 21-Feb-2008

Air A ir po r t Handl Han dl in g Manu al

A HM 560

COMMUNICATION ADDRESSES

EDP-SYSTEM SEMI-PERMANENT SEMI-PERMANENT DATA


1.

SUPPLIERS’ SUPPLIERS’ CONTACT ADDRESS Completed Completed sheets and changes of b asic data and procedure must be forw arded arded to:

MAILING ADDRESS:

TELETYPE ADDRESS:

E-MAIL ADDRESS:

REMARKS:

2.

CARRIER’S CONTACT ADDRESS MAILING ADDRESS:

UTair Aviation, Khanty-Mansiysk Khanty-Mansiysk airport, Khanty-Mansiysk Khanty-Mansiysk autonomous district, Tyumen region, 628012, Russia

TELETYPE ADDRESS:

E-MAIL ADDRESS:

[email protected] [email protected] .ru

REMARKS:


A.Nutretsov

AHM 560 B737-500

Issue No.: A1/1.0 Date: 21-Feb-2008

Air A ir po r t Handl Han dl in g Manu al COMMUNICATION ADDRESSES

EDP-SYSTEM SEMI-PERMANENT SEMI-PERMANENT DATA 3.

A HM 560

AUTOMATICALL Y PRODUCED PRODUCED DOCUMENTS DOCUMENTS (tick (ti ck as requ ir ed)


NOTOC SEATPLAN LOADPLAN PASSENGER INFO LIST LOADSHEET LOADING INSTRUCTION/REPORT INSTRUCTION/REPORT

4.

MESSAGE REQUIREME REQUIREMENTS NTS (tick (ti ck as requ ired) ir ed) LDM Load Message AHM 583 ALI Abbreviated Load Load Information Message Message AHM 584 CPM Container/Pallet Distribution Message AHM 587 UCM ULD Control Message AHM 424 (dispatch only) MVT Movement Messages AHM 730 and 780 DIV Diversion Message AHM 781 SOM Seats Occupied Message Recommended Practice 1712 PTM Passenger Transfer Message Recommended Practice 1718 PSM Passenger Service Message Recommended Practice 1715 (dispatch only) TPM Teletype Passenger Manifest Recommended Practice 1717 (dispatch only) PFS Passenger Final Sales Message Recommended Practice 1719 (dispatch only) IDM Industry Discount Message Recommended Practice 1714 RQL Request List Message Recommended Practice 1709 (dispatch only) PNL/ ADL Passenger Name List and Additions And Deletions List (Recommended Practice 1708)(acceptance only) SAL Seats Available List Recommended Practice 1713 (acceptance only) SLS Statistical Load Summary AHM 588 FMM Fuel Monitoring Message AHM 782 RQM Request Information Message AHM 783 UWS ULD/ Bulk Load Weight Signal AHM 581 (acceptance only)

5.

MESSAGE ADDRESSES Attach a complete address list for all all messages mentioned mentioned under paragraph 4 above. above.

6.

DEFINITION OF CLA SS CODES The following class naming convention convention shall be used throughout the document. Class codes: (e.g. F, Y, C, M, etc.)

Class 1 Class 2 Class 3 Class 4 Class 5

7.

Y

DEFINITION DEFINITION OF UNITS OF MEASURE (tick (ti ck as appr opri op ri ate) Weight Length Volume Liquid Volume

8.

C

Kg Meters Cu. mtr Liter

Lbs Inches Cu. ft US Gallon

MULTIPLE MULTIPL E SHEETS NUMBERING In the event of the requirements to produce multiple copies of the same sheets (e.g. C5, C9) establish an additional sequence identifier while keeping the original sheet number. E.g. C5a, C5b, etc, or C5.1, C5.2, etc.


A.Nutretsov

AHM 560 B737-500

Issue No.: A2/1.6 Date: 11-Aug-2009

Air A ir po r t Handl Han dl in g Manu al EDP-SYSTEM SEMI-PERMANENT SEMI-PERMANENT DATA

A HM 560

LIST OF REVISIONS


Document issue number

Revision number

Reason

Changes overview

1

9

02-Oct-2009

A.Nutretsov A.Nutrets ov

New aircraft was added (VP-BXZ).

25-S 25-Sep eptt-20 2009 09

A.Nu A.Nutr tret etso sov v

New New airc aircra raft ft was was added (VP-BXY).

7

17-Sep 17-Sept-2 t-200 009 9

A.Nutr A.Nutrets etsov ov

New New aircra aircraft ft was added (VP-BXU).

1

6

11-Aug-2009

A.Nutretsov A.Nutret sov

1

5

24-Feb-2009


Class Code for Class 1 is changed. New aircraft were added (VP-BXO, VP-BXQ, VP-BXV, VP-BXR). New aircraft was added (VQ-BAE).

Update complete document Update complete document Update complete document Update complete document

1

8

1

1

4

02-Feb-2009

A.Nutretsov A.Nutrets ov

1

3

12-Nov-2008


1

2

01-S 01-Sep eptt-20 2008 08

S.Za S.Zaku kute tenk nkov ov

1

1

10-Au 10-Aug-2 g-2008 008

S.Zaku S.Zakuten tenkov kov

1

0

21-Fe 21-Feb-2 b-200 008 8

S.Zaku S.Zakuten tenkov kov


Release date

Completed by

A.Nutretsov

AHM 560 B737-500

New aircraft were added (VQ-BAC, VQ-BAD). Data (upper limits for TO and Flight) for a/c VP-BVN is corrected. New New WB info inform rmat atio ion n were added. Data in Pantry tables is corrected. New aircra aircraft ft were were added.

Update complete document Update complete document Update complete document Update complete document Update complete document

Initia Initiall issue issue

Issue No.: A3/1.9 Date: 02-Oct-2009

Air A ir po r t Handl Han dl in g Manu al EDP-SYSTEM SEMI-PERMANENT SEMI-PERMANENT DATA

A HM 560

LIST OF EFFECTIVE SHEETS

A Sheet 4.1 Carrier UT

Section

Sheet

A

1 2 3 4

B

Multiple page identifier

1 2

1 2 3 1 2 3 4 5

1 2

6 7 C

8

1 2

9 10 11 12

D


1 2

13 14 1 2 3

A.Nutretsov

AHM 560 B737-500

Sheet issue No.

Date

A1/1.0 A2/1.6 A3/1.8 A4.1/1.8 A4.2/1.8 B1/1.0 B2/1.0 B3/1.0 C1/1.0 C2/1.0 C3/1.0 C4/1.8 C5.1/1.0 C5.2/1.8 C6/1.8 C7/1.0 C8.1/1.2 C8.2/1.2 C9/1.0 C10/1.0 C11/1.0 C12.1/1.2 C12.2/1.8 C13/1.0 C14/1.0 D1/1.0 D2/1.0 D3/1.0

21-Feb-2008 11-Aug-2009 02-Oct-2009 02-Oct-2009 02-Oct-2009 21-Feb-2008 21-Feb-2008 21-Feb-2008 21-Feb-2008 21-Feb-2008 21-Feb-2008 02-Oct-2009 21-Feb-2008 02-Oct-2009 25-Sept-2009 21-Feb-2008 01-Sept-2008 01-Sept-2008 21-Feb-2008 21-Feb-2008 21-Feb-2008 01-Sept-2008 02-Oct-2009 21-Feb-2008 21-Feb-2008 21-Feb-2008 21-Feb-2008 21-Feb-2008

Issue No.: A4.1/1.9 Date: 02-Oct-2009

Air po rt Handl in g Manu al EDP-SYSTEM SEMI-PERMANENT DATA

AHM 560

LIST OF EFFECTIVE SHEETS

A Sheet 4.2 Carrier UT

Weight and Balance Information

Trim Sheet


Additional and supplemental information VP-BVL VP-BVN VP-BVZ VP-BYK VP-BYL VP-BYM VQ-BAC VQ-BAD VQ-BAE VP-BXO VP-BXQ VP-BXR VP-BXV VP-BXU VP-BVL VP-BVZ VP-BYK VP-BYL VP-BYM VP-BVN VQ-BAC VQ-BAD VQ-BAE VP-BXO VP-BXQ VP-BXR VP-BXV VP-BXU VP-BXY VP-BXZ

A.Nutretsov

AHM 560 B737-500

10-Aug-2008 10-Aug-2008 01-Sept-2008 10-Aug-2008 01-Sept-2008 01-Sept-2008 02-Feb-2009 02-Feb-2009 24-Feb-2009 11-Aug-2009 11-Aug-2009 11-Aug-2009 11-Aug-2009 02-Oct-2009

10-Aug-2008

10-Aug-2008

02-Oct-2009

Issue No.: A4.2/1.9 Date: 02-Oct-2009

Air po rt Handl in g Manu al

AHM 560

GENERAL INFORMATION

EDP-SYSTEM SEMI-PERMANENT DATA

B Sheet 1 Carrier UT

1.

PASSANGER AND BAGGAGE WEIGHTS

1.1

Standard / default passenger / cabin baggage weigh ts

Standard / variations*

Average adult Adult male Adult female Child Infant Cabin Baggage

Standard Standard Winter Summer Weight Weight 80 kg 75 kg

30 kg 15 kg

*

*

*

*

*

30 kg 15 kg Yes

No

Cabin baggage weight is included in the above mentioned passenger weights If No: Actual cabin or standard baggage weight must be used. Remarks: Standard Winter and Summer Weights in accordance with airport schedule.

1.2

If passenger / cabin baggage weights vary by class, use the following table:

Class as appropriate Average adult Adult male Adult female Child Infant Cabin Baggage

Class 1

Class 2

Class 3

Class 4

Class 5

Remarks:

1.3

Checked baggage weight

Standard / variations* Standard Weight per piece ACTUAL Weight per ------passenger

*

*

*

*

* Variations may include domestic, international, charter, route, etc. Enter “actual” if standard weight not permitted. Remarks (condition for Oversize etc.):


A.Nutretsov

AHM 560 B737-500

Issue No.: B1/1.0 Date: 21-Feb-08

*


AHM 560

GENERAL INFORMATION



2. CREW AND CREW BA GGAGE WEIGHTS 2.1 Crew weight s

Cockpit Cabin

Standard 80 kg 75 kg

Male

Female

Crew hand baggage shall be included in the above crew weights. Remarks:

2.2 Crew baggage weight s (other than hand baggage) Cockpit

Cabin

Shorthaul Longhaul Others* *Specify conditions as appropriate Remarks: Average Crew Baggage Weight – 30 kg, is included into DOW & DOI. Recommended Place – Forward Part of FWD Cargo Compartment (CPT 1)


A.Nutretsov

AHM 560 B737-500



AHM 560

GENERAL INFORMATION



3.

DRY OPERATING WEIGHT AND DRY OPERATING INDEX SPECIFICATIONS (tick as appropriate)

DOW Item

Incl.

Excl.

DOI Incl.

Remarks

Excl.

Basic Weight Cockpit Crew Cabin Crew Forward part of FWD Cargo CPT

Crew baggage Pantry Containers

Not applicable

Pallets

Not applicable

Potable Water Items for Service Emergency Equipment Specific Aircraft Items*

Remarks: * Specific Aircraft Items include such items as Unusable Fuel, Engine Oil, Galley Structure, Toilet Fluids and Set of Necessary Documentation.


A.Nutretsov

AHM 560 B737-500



AHM 560

AIRCRAFT DATA


Sheet 1 A/C Type B737-500

1. 1.1

C Carrier UT

BALANCE AND SPECIAL INFORMATION – OUTPUT ON LOADSHEET Balance output (Reference AHM 517)

Please mark your requirements in respective box . Basic Index

Remarks

BI

Dry Operating Index

DOI

Deadload Index

DLI

Deadload MAC

MACDLW

Loaded Index at zero fuel weight

LIZFW

Loaded Index at take-off weight

LITOW

Loaded Index at landing weight

LILAW

MAC – at zero fuel weight

MACZFW

MAC – at take-off weight

MACTOW

MAC – at landing weight

MACLAW

Stabilizer trim setting at take-off

STABTO*

* Specify ANU or AND as appropriate.

1.1.1 Passenger trim output Please mark your requirements in respective box.

Remarks*

Class trim Cabin area trim Seat row trim

* Remarks: Indicate any other terminology to be printed on the loadsheet (Ref. AHM 517,6.2 item 44). 1.2

Special information Specify the information to be entered in the lower parts of the EDP Loadsheet.

1.2.1 Captain’s information/notes, Center of Gravity limits, Ramp weight, etc. (give examples). (Ref. AHM 517, 6.2, item 45).

1.2.2 Load message before LMC, if required, to be shown. (Ref. AHM 517, 6.2, item 46).


A.Nutretsov

AHM 560 B737-500

Issue No.: C1/1.0 Date: 21-Feb-2008


AHM 560

AIRCRAFT DATA


Sheet 2.1 A/C Type B737-500

2.

BASIC INDEX AND MAC/RC FORMULA

2.1

Examples and definitions

Index

W · (Sta. – Ref.Sta.)

=

С

2.2

= = = = = = = =

Index formula : = =

648.5 40 30000

inches from zero

134.5 625.6

inches inches from zero

MAC/RC Information Length of MAC/RC LEMAC at

2.4

+ K

Weight, actual. Station, horizontal distance in length units from station zero to the location. Reference station/axis. Selected station around which all index values are calculated. Constant used as a plus value to avoid negative index figures. Constant used as a denominator to convert moment values into index values. Index value corresponding to respective weight. Length of Mean Aerodynamic Chord / Reference Chord in length units. Horizontal distance in length units from the station zero to location of the Leading Edge of the MAC / RC

Ref.Sta. at K (constant) C (constant)

2.3

Carrier UT

C·(I - K) + Ref.Sta. – LEMAC W MAC / RC 100

% MAC/RC = W Sta. Ref. Sta. K C I MAC / RC LEMAC

C

= :

Stabilizer trim setting (see additional page C2.2) For each required Flap setting, supply the following data: Flaps setting (Specify stabilizer settings for at least one weight if setting doesn’t change at different weights). (Specify at least minimum and maximum MAC/RC values).


A.Nutretsov

AHM 560 B737-500

Issue No.: C2.1/1.0 Date: 21-Feb-2008


AHM 560

AIRCRAFT DATA


C Sheet 2.2

A/C Type B737-500

Carrier UT

2.4.1 Takeoff horizontal stabilizer trim setting The following diagram provides Takeoff Trim Settings versus Airplane Center of Gravity for Flaps 5 and 15 in Kilograms. AIRPLANE NOSE

1

DOWN

FLAPS 5 & 15 2

S T I N U M I R T R E Z I L I B A T S

3

D N A B N E E R G

4

9 * 3 . 5 5 1 * 4 3 < 4 4. 5 9 * * . 3 5 3 1 . 4 4 5 4 > 5

5

6 *GROSS WEIGHT - 1000 KG AIRPLANE NOSE UP

7 0

5

10

15

20

25

30

35

CENT ER OF G RAVITY - %MAC

The following table provides inflection point data for the Takeoff Trim Settings versus Airplane Center of Gravity diagram. TAKEOFF TRIM SETTING INFLECTION POINTS (Gross Weight - 1000 KG) <45.359 C.G.

STAB. TRIM

45.35 9-54.431

C.G.

STAB. TRIM

>54.431

C.G.

STAB. TRIM

5.0

6.8

5.0

5.9

5.0

6.4

5.6

6.8

30.0

2.0

30.0

2.5

30.0

3.0

A tolerance of plus or minus 0.75 trim units is acceptable when determining takeoff trim as a function of airplane takeoff weight and center of gravity. This is approximately equivalent to plus or minus 4.8% MAC. This allowable tolerance between “actual” and “calculated” takeoff center of gravity must be adhered to in the development of simplified loading devices or manifests.


A.Nutretsov

AHM 560 B737-500



AHM 560

AIRCRAFT DATA


C Sheet 3

A/C Type B737-500

3.

Carrier UT

AIRCRAFT REGISTRATIONS, WEIGHT AND INDEX DETAILS DRY OPERATING WEIGHT

BASIC WEIGHT

(tick as appropriate)

Provide full list of registrations/tail numbers and adjustments to fleet weight/index Fleet Weight : Registration/ tail number

________ Weight Adjustment

Index Adjustment

Fleet Index :

____

Registration/ tail number

Weight Adjustment

.

Index Adjustment

*

* Aircraft Weights and Indices are shown in Attachment – Weight and Balance Information for appropriate aircraft. Note: Notification for data changes at short notice may also be made by means of data exchange message (AHM 562).


A.Nutretsov

AHM 560 B737-500

Issue No.: C3/1.1 Date: 10-Aug-2008


AHM 560

AIRCRAFT DATA


C Sheet 4

A/C Type B737-500

4.

LIMITATIONS

4.1

Aircraft weight limitations

Carrier UT

Operator defined maximum weights for: Aircraft Reg./ Tail Number

Ramp/Taxi /kg/

Take-off /kg/

Zero fuel /kg/

Landing /kg/

VP-BVL

60 781

60 554

46 720

49 895

VP-BVZ

60 781

60 554

46 720

49 895

VP-BYK

60 781

60 554

46 720

49 895

VP-BYL

60 781

60 554

46 720

49 895

VP-BYM

60 781

60 554

46 720

49 895

VP-BVN

58 967

58 740

46 720

49 895

VQ-BAC

58 967

58 740

46 720

49 895

VQ-BAD

58 967

58 740

46 720

49 895

VQ-BAE

58 967

58 740

46 720

49 895

VP-BXO

58 967

58 740

46 720

49 895

VP-BXQ

58 967

58 740

46 720

49 895

VP-BXR

58 967

58 740

46 720

49 895

VP-BXV

58 967

58 740

46 720

49 895

VP-BXU

58 967

58 740

46 720

49 895

VP-BXY

58 967

58 740

46 720

49 895

VP-BXZ

58 967

58 740

46 720

49 895


A.Nutretsov

AHM 560 B737-500

Issue No.: C4/1.9 Date: 02-Oct-2009

Airport Handling Manual AIRCRAFT DATA


4.2

VP-BVZ VP-BYM

C Sheet 5.1

Configuration(s) VP-BVL VP-BYL

AHM 560

A/C Type B737-500

VP-BYK

Carrier UT

CG – Limits for Loadsheet Purposes Enter the forward and the aft balance limits in the boxes, commencing at the lowest possible operating weight and terminating at the highest possible operating weight to b е checked. IMPORTANT: If limits are affected and/or determined by passenger/ fuel/ version other conditions, specify each set of limits on а separate sheet, entering the special condition(s) in the box.

FORWARD

AFT

Special condition if applicable Specify applicability*

Zero Fuel Check

Take-Off Check

Weight /kg/

MZFW

MTOW

In-flight Check

Landing Check

MLW

25 000 46 720

Special condition if applicable Index

32.2 19.5

25 000 50 859

26.5 12.6

60 554

25.9

25 000 49 411

25.4 11.1

60 554

25.9

25 000 49 895

26.5 13.1

Specify applicability*

Zero Fuel Check

Take-Off Check

Weight /kg/

MZFW

MTOW

In-flight Check

Landing Check

MLW

Index

25 000 36 287

45.3 59.2

46 720

62.6

25 000 40 823

47.8 65.6

60 554

71.5

25 000 36 287

49.6 63.5

60 554

71.5

25 000 36 287

49.6 63.5

49 895

68.8

*Zero fuel, taxi, take-off, in-flight, landing Note: A balance chart/trim sheet must be attached for c heck purp oses as per AHM519. Stat e tr im met hod (i .e. cabin area tri m, c pt tr im etc .) Remarks:


A.Nutretsov

AHM 560 B737-500



EDP-SYSTEM SEMI-PERMANENT DATA Configuration(s) VP-BVN VQ-BAD VP-BXV

4.2

VQ-BAE VP-BXU

VP-BXO VP-BXY

AHM 560

C Sheet 5.2

VQ-BAC VP-BXQ VP-BXR VP-BXZ

A/C Type B737-500

Carrier UT

CG – Limits for Loadsheet Purposes Enter the forward and the aft balance limits in the boxes, commencing at the lowest possible operating weight and terminating at the highest possible operating weight to b е checked. IMPORTANT: If limits are affected and/or determined by passenger/ fuel/ version other conditions, specify each set of limits on а separate sheet, entering the special condition(s) in the box.

FORWARD

AFT

Special condition if applicable Specify applicability*

Zero Fuel Check

Take-Off Check

Weight /kg/

MZFW

MTOW

In-flight Check

Landing Check

MLW

25 000 46 720

Special condition if applicable Index

32.2 19.5

25 000 50 859

26.5 12.6

58 740

23.1

25 000 49 411

25.4 11.1

58 740

23.1

25 000 49 895

26.5 13.1

Specify applicability*

Zero Fuel Check

Take-Off Check

Weight /kg/

MZFW

MTOW

In-flight Check

Landing Check

MLW

Index

25 000 36 287

45.3 59.2

46 720

62.6

25 000 40 823

47.8 65.6

58 740

71.0

25 000 36 287

49.6 63.5

58 740

71.0

25 000 36 287

49.6 63.5

49 895

68.8

*Zero fuel, taxi, take-off, in-flight, landing Note: A balance chart/trim sheet must be attached for c heck purp oses as per AHM519. Stat e tr im met hod (i .e. cabin area tri m, c pt tr im etc .) Remarks:


A.Nutretsov

AHM 560 B737-500

Issue No.: C5.2/1.9 Date: 02-Oct-2009


AHM 560

AIRCRAFT DATA



5.

C Carrier UT

EFFECT OF FUEL (tick as appropriate) Remarks/ Procedure Name Standard Procedure Non-standard Procedure

FUEL DENSITY:

Fuel Weight /kg/ 1000 2000 3000 4000 5000 6000 7000 8000 9000 9078 *

+ +

Index + 1.20 2.09 2.72 3.16 3.55 3.72 3.57 2.08 0.42 0.67

0.8 kg/L___

Fuel Weight /kg/ 10000 11000 12000 13000 14000 15000 16100 ** Standard Taxi Fuel Weight

-

Index + 0.79 2.33 3.86 5.40 6.94 8.48 10.57 Index +

227 Note: *

TANKS No 1 & No 2 – FULL (9 078 kg)

** TANKS No 1, No 2 & Central – FULL (16 100 kg)

Note 1: Use additional sheets for other fuel densities or state correction factors. Note 2: Specify maximum capacity. Note 3: Use additional sheets for each fuel condition/procedure.


A.Nutretsov

AHM 560 B737-500

Issue No.: C6/1.8 Date: 25-Sept-2009


AHM 560

AIRCRAFT DATA



6. 6.1

C Carrier UT

CREW Number of cockpit crew seats and average location

Maximum number of cockpit seats Captain & First Officer (2) First Observer (1) Second Observer (1)

+

Length of arm from reference station, in

+

Index influence per 1 kg

-

444.5 413.0 413.0

-

0.01482 0.01377 0.01377

NOTE: First and second observers normally are not included in DOW

6.2

6.3

Number of cabin crew seats and location Length of arm from reference station

Crew seats

Maximum No.

location

of seats

+

inches

+

per 1 kg

FWD

2

360,5

3

+

0.01202

AFT

+

370,5

Index influence

0.01235

Crew Distribution/Crew Code Crew Code Captain First Officer

Cockpit Crew Cabin Crew

Cockpit Cockpit

Location of Crew Hand Luggage Cockpit Cockpit

Location *

1 1

Attendant

2

FWD entry area

UNDER-BIN C1

Attendant

3

AFT entry area

UNDER-BIN C1

*Use the locations as under paragraph 6.2

Remarks: For additional information about Crew Distribution see Weight and Balance Information for the a/c.


A.Nutretsov

AHM 560 B737-500




A/C Type B737-500

All

GALLEY AND PANTRY

7.1

Galleys

Galley locations

C Sheet 8.1

Configuration(s)

7.

AHM 560

Length of arm from reference station inches +/-

Carrier UT

Index influence +/-

per 1 kg

G1 (FWD)

-

392.50

-

0.01308

G2 (FWD)

-

334.50

-

0.01115

G4B (AFT)

+

418.50

+

0.01395

Remarks:

Pantry Weight/Pantry Code (normally used for above mentioned cabin configurations) a)

Pantry Code “A”: Normal flight, included in DOW-DOI (maximum capacity of pantry)

Pantry Code Galley G1+G2 (FWD)

Pantry Weight /kg/ 165

Index

Location*

- 1.97

FWD AFT

Galley G4B (AFT)

361

+ 5.04

TOTAL

526 kg

+ 3.07


A.Nutretsov

AHM 560 B737-500

Issue No.: C8.1/1.2 Date: 01-Sept-2008



A/C Type B737-500

All


Index

Location*

- 1.90

FWD AFT

Galley G4B (AFT)

305

+ 4.26

TOTAL

463 kg

+ 2.36

Pantry Code “S”: Short flight (half capacity of pantry)


d)

Carrier UT

Pantry Code “R”: Reduced flight (3/4 of full pantry capacity)


c)

C Sheet 8.2

Configuration(s)

b)

AHM 560


Index

Location*

- 1.73

FWD AFT

Galley G4B (AFT)

249

+ 3.47

TOTAL

392 kg

+ 1.73

Pantry Code “O”: Training or ferry flight only



Index

Location*

- 0.92

FWD AFT

Galley G4B (AFT)

212

+ 2.95

TOTAL

288 kg

+ 2.03

*Use the locations as under paragraph 7.1.

Remarks:


A.Nutretsov

AHM 560 B737-500



AHM 560

AIRCRAFT DATA


C Sheet 9

Configuration(s) 114 Pax (8C + 106Y)

8.

PASSENGER CABIN

8.1

Passenger seats

A/C Type B737-500

Carrier UT

Note: Fill in one table for each cabin configuration code. Name of cabin section

8.2

Number of seats Class 1

OA OB OC OD

8

Total per class

8

Class 2

Class 3

Class 4

Class 5

Total per cabin section

36 46 24

8 36 46 24

106

Total 114

Class / Cabin Sections Class/Cabin Section

OA OB OC OD


Length of arm from reference station inches +/-

+ +

267.00 129.00 92.72 274.00

A.Nutretsov

AHM 560 B737-500

Index influence

+/-

+ +

per 1kg 0,00890 0,00430 0,00309 0,00913




C Sheet 10

Configuration(s)

A/C Type B737-500

All

8.3

AHM 560

Carrier UT

Seating Layout Show the passenger seating layout for the configuration given in the box at the top by inserting the seat row numbers and letters in the following table. For special seats use the description codes listed below. B = Bassinet Position С = Crew seat E = Emergency Exit G = Groups H = Incapacitated passenger I = Infant preference row / seats J = Rear facing seats K = Near galley L = Leg space seat M = Wheel chair N = No smoking O = Over wing seat

P = Stretcher location Q = Quiet zone S = Smoking T = Near toilet U = Unaccompanied minor V = Seat left vacant / offered last W = No movie X = No facility seat, e.g. no distinction between smoking and non-smoking Y = Not fitted Z = Buffer zone A = Aisle

Alfa / Characters – D, F, R, Blank, not used


A.Nutretsov

AHM 560 B737-500




C Sheet 11

Configuration(s)

A/C Type B737-500

All

8.3.1

AHM 560

Carrier UT

Seatplan Layout / Facilities and Row Index Influence

N O I T C E S

OA OB

OC

OD

Seat Identifier

. e o ) i N d s

H

R W / H O ( R L

1 2 5 6 7 8 9 10 12 14 15 16 17 18 19 20 21 22 23 24

A

W W W W W W W W W W W W W W W W W W W

B

A A X X X X X X E X X X X X X X X X X X

C

A A A A A A A A A A A A A A A A A A

D

A A A A A A A A A A A A A A A A A A

E

A A X X X X X X E X X X X X X X X X X X

F

W W W W W W W W W W W W W W W W W W W

Length of arm from reference station, in

- 285.50 - 248.50 - 206.50 - 175.50 - 144.50 - 113.50 - 82.50 - 51.50 - 20.50 + 10.50 + 41 .50 + 72.50 + 103.50 + 134.50 + 165.50 + 196.50 + 227.50 + 258.50 + 289.50 + 320.50

Index influence per 1 kg

+/+ + + + + + + + + + +

0. 0. 0. 0. 0. 0. 0. 0. 0. 0. 0. 0. 0. 0. 0. 0. 0. 0. 0. 0.

0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0

0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 1

9 8 6 5 4 3 2 1 0 0 1 2 3 4 5 6 7 8 9 0

5 2 8 8 8 7 7 7 6 3 3 4 4 4 5 5 5 6 6 6

Note: Rows 3, 4, 11 and 13 are absent.


A.Nutretsov

AHM 560 B737-500


2 8 8 5 2 8 5 2 8 5 8 2 5 8 2 5 8 2 5 8



9.

VP-BVZ VP-BYM

C Sheet 12.1

Configuration(s) VP-BVL VP-BYL

AHM 560

A/C Type B737-500

VP-BVN VP-BYK

Carrier UT

DETAILS FOR COMPARTMENT TRIM

Compartment Number

Description

Gross Weight /kg/

CPT 1 CPT 2 CPT 3 CPT 4

FWD FWD AFT AFT

703** 869 1756 1132

Maximum Capacity Length of arm Volume * from reference 3 /m / station /in/

- 262,50 - 184,00 + 143,00 + 280.00

Index per t x* 1 kg +

+ +

0.00875 0.00613 0.00477 0.00933

Security locker (DIP)

* Volume information required for bulk compartments only.

Remarks: ** Crew baggage is normally loaded in Forward part of FWD Cargo Compartment. It’s weight 180 kg included in DOW and DOI for Crew Code 2/4 must be subtracted from Gross Weight of CPT1.

9.1

Combined Load Limitations

Yes

N/A

Yes

N/A

Appropriate data shown or attached? 9.2

Cumulative Load Limitations Appropriate data shown or attached?


A.Nutretsov

AHM 560 B737-500




9.

VQ-BAD VP-BXV

VQ-BAE VP-BXU

C Sheet 12.2

Configuration(s) VQ-BAC VP-BXR

AHM 560

VP-BXO VP-BXY

VP-BXQ VP-BXZ

A/C Type B737-500

Carrier UT

DETAILS FOR COMPARTMENT TRIM

Compartment Number

Description

Gross Weight /kg/

CPT 1 CPT 2 CPT 3 CPT 4

FWD FWD AFT AFT

638** 869 1756 1132

Maximum Capacity Length of arm Volume * from reference 3 /m / station /in/

- 259,50 - 184,00 + 143,00 + 280.00

Index per t x* 1 kg +

+ +

0.00865 0.00613 0.00477 0.00933

Security locker (DIP)

* Volume information required for bulk compartments only.

Remarks: ** Crew baggage is normally loaded in Forward part of FWD Cargo Compartment. It’s weight 180 kg included in DOW and DOI for Crew Code 2/4 must be subtracted from Gross Weight of CPT1.

9.1

Combined Load Limitations

Yes

N/A

Yes

N/A

Appropriate data shown or attached? 9.2

Cumulative Load Limitations Appropriate data shown or attached?


A.Nutretsov

AHM 560 B737-500

Issue No.: C12.2/1.9 Date: 02-Oct-2009



C Sheet 13

Configuration(s)

A/C Type B737-500

All

10.

AHM 560

Carrier UT

DETAILS FOR BAY / SECTION TRIM Maximum Capacity

Bay / Section

Gross Weight

Volume *

Length of arm from reference station

+

Index per x* weight unit

N/A

Security Locker (DIP) * Volume information required for bulk compartments only. Note 1: Attach a plan for each compartment configuration. Note 2: Use additional sheets as required.

10.1

Lateral / asymmetrical Limitations Yes

N/A

Appropriate data shown or attached?


A.Nutretsov

AHM 560 B737-500



AHM 560

AIRCRAFT DATA



11.

C Carrier UT

BALLAST FIXED PROVISIONS FOR CARRYING BALLAST?

YES

NO

If YES, specify below:

LOCATION

WEIGHT

+ Index

N/A

Remarks:


A.Nutretsov

AHM 560 B737-500



AHM 560

AIRCRAFT DATA


Sheet 1 A/C Ty pe B737-500

1.

CG – LIMITS

1.1

Ideal Trim Line at ZFW for Fuel Savin g Purposes


D

Weight

Index

25 000 kg

43.3

46 720 kg

46.3

A.Nutretsov

AHM 560 B737-500

Carrier UT

Issue No.: D1/1.0 Date: 21-Feb-08


AHM 560

AIRCRAFT DATA



2.

D Carrier UT

UNIT LOAD DEVICES DETAILS Maximum Capacity Type Code

Tare Weight

Gross Weight

Volume*

Position or height restriction

Remarks

N/A

* Containers /Igloos only Note: For pallets, specify height. Indicated restriction means it cannot be loaded.


A.Nutretsov

AHM 560 B737-500



AHM 560

AIRCRAFT DATA



3.

D Carrier UT

SPECIAL LOAD At tach relevant co mpany regul ati ons f or sp ecial load (AVI, Dang erou s Goods, etc.).

TO BE OBTAINED LOCALLY FROM STATION MANAGER


A.Nutretsov

AHM 560 B737-500


Weigh jrkr t and Balance Info rmatio n

A/C Reg. VP-BVL

B 737-500 Doc. №

WBI - VP-BVL - 02

msn 28926

Issue Date

Effective From

Issued By

Contact to

30-Aug-2008

30-Aug-2008

A.Nutretsov

[email protected]

At tenti on: This information sheet supersedes all previously issued Weight and Balance Information for this aircraft. Preceding WB Information should be removed and replaced with new ones.

Maximum Taxi Weight kg

Maximum Take-off Weight kg

60 781

60 554

49 895

46 720

Basic Weight Data

Basic Empty Weight, kg

Basic Empty Index, units

Center of Gravity, %

31 698

43.24

19.30

Max Passenger Capacity

Available Version

114

8C + 106Y

Configuration Data

Pantry Data

Maximum Landing Weight Maximum Zero Fuel Weight kg kg

Pantry Code “ A”

Pantry Code “ R”

Pantry Code “ S”

Pantry Code “ O”

Normal Flight

Reduced Flight

Short Flight

Training or Ferry Flight

Weight, kg

Ind.

Weight, kg

Ind.

Weight, kg

Ind.

526

+3.07

463

+2.36

392

+1.73

Weight, kg

288

Ind.

+2.03

Dry Operating Data Crew Code 2/ 2/ 2/ 3/ 3/ 3/ 4/ 4/ 4/ 2/ 3/ 4/

5 4 3 5 4 3 5 4 3 0 0 0

Cockpit Cabin Crew Crew 2 2 2 3 3 3 4 4 4 2 3 4

5 4 3 5 4 3 5 4 3 0 0 0

Cabin crew Location

Pantry Code “A”

Pantry Code “R”

Pantry Code “S”

Pantry Code “O”

FWD Utility Zone

Aft Utility Zone

DOW

DOI

DOW

DOI

DOW

DOI

DOW

DOI

2 2 1 2 2 1 2 2 1 -

3 2 2 3 2 2 3 2 2 -

33 372 33 267 33 162 33 482 33 377 33 272 33 592 33 487 33 382 -

44,60 43,94 45,10 43,24 42,57 43,74 41,87 41,21 42,37 -

33 308 33 203 33 098 33 418 33 313 33 208 33 528 33 423 33 318 -

43,89 43,23 44,39 42,53 41,86 43,03 41,16 40,50 41,66 -

33 237 33 132 33 027 33 347 33 242 33 137 33 457 33 352 33 247 -

43,27 42,60 43,77 41,90 41,24 42,40 40,54 39,87 41,04 -

32 609 32 719 32 829

43,90 42,54 41,17

Note: Flight with Crew Configuration 2 / 4 and Pantry Code “ A” is accepted as Normal Flight NOTE:    

Pantry Code “ A”: Normal flight (maximum Operational capacity of pantry) Pantry Code “R”: Reduced flight (3/4 of Normal Flight Pantry) Pantry Code “S”: Short flight (half capacity of Normal Flight Pantry) Pantry Code “O”: Training or ferry flight only

Page 1 of 1

Weigh t and Balance Info rmatio n

A/C Reg. VP-BVN

B 737-500 Doc. №

WBI - VP-BVN- 02

Issue Date

Effective From

30-Aug-2008

30-Aug-2008

msn 27540

Issued By

Contact to

A.Nutretsov [email protected]




58 967

58 740

49 895

46 720

Basic Weight Data




31 552

43.26

19.33


Available Version

114

8C + 106Y

Configuration Data

Pantry Data






Normal Flight

Reduced Flight

Short Flight


Weight, kg

Ind.

Weight, kg

Ind.

Weight, kg

526

+3.07

463

+2.36

392

Ind.

Weight, kg

Ind.

288

+2.03

+1.73


5 4 3 5 4 3 5 4 3 0 0 0

Cockpit Crew

Cabin Crew

2 2 2 3 3 3 4 4 4 2 3 4

5 4 3 5 4 3 5 4 3 0 0 0

Cabin crew Location

Pantry Code “ A” Pantry Code “ R”



FWD Utility Zone

Aft Utility Zone

DOW

DOI

DOW

DOI

DOW

DOI

DOW

DOI

2 2 1 2 2 1 2 2 1 -

3 2 2 3 2 2 3 2 2 -

33 225 33 120 33 015 33 335 33 230 33 125 33 445 33 340 33 235 -

44,63 43,96 45,13 43,26 42,60 43,76 41,90 41,23 42,40 -

33 162 33 057 32 952 33 272 33 167 33 062 33 382 33 277 33 172 -

43,92 43,25 44,42 42,55 41,89 43,05 41,19 40,52 41,69 -

33 091 32 986 32 881 33 201 33 096 32 991 33 311 33 206 33 101 -

43,29 42,63 43,79 41,93 41,26 42,43 40,56 39,90 41,06 -

32 462 32 572 32 682

43,93 42,56 41,20



Page 1 of 1


A/C Reg. VP-BVZ

B 737-500 Doc. №

WBI - VP-BVZ - 01

msn 28925

Issue Date

Effective From

Issued By

Contact to

1-Sept-2008

1-Sept-2008

A.Nutretsov

[email protected]




60 781

60 554

49 895

46 720

Basic Weight Data




31 755

44.38

20.11


Available Version

114

8C + 106Y

Configuration Data

Pantry Data






Normal Flight

Reduced Flight

Short Flight


Weight, kg

526

Ind.

Weight, kg

Ind.

Weight, kg

463

+2.36

392

+3.07

Ind.

+1.73

Weight, kg

Ind.

288

+2.03


5 4 3 5 4 3 5 4 3 0 0 0


5 4 3 5 4 3 5 4 3 0 0 0

Cabin crew Location

Pantry Code “A”

Pantry Code “R” Pantry Code “S”

Pantry Code “O”

FWD Utility Zone

AFT Utility Zone

DOW

DOI

DOW

DOI

DOW

DOI

DOW

DOI

2 2 1 2 2 1 2 2 1 -

3 2 2 3 2 2 3 2 2 -

33 428 33 323 33 218 33 538 33 433 33 328 33 648 33 543 33 438 -

45,75 45,08 46,25 44,38 43,72 44,88 43,02 42,36 43,52 -

33 365 33 260 33 155 33 475 33 370 33 265 33 585 33 480 33 375 -

45,04 44,37 45,54 43,67 43,01 44,17 42,31 41,65 42,81 -

33 294 33 189 33 084 33 404 33 299 33 194 33 514 33 409 33 304 -

44,41 43,75 44,91 43,05 42,38 43,55 41,68 41,02 42,18 -

32 665 32 775 32 885

45,05 43,68 42,32



Page 1 of 1

Weigh t and Balance Info rmatio n

A/C Reg. VP-BYK

B 737-500 Doc. №

WBI - VP-BYK- 02

Issue Date

Effective From

30-Aug-2008

30-Aug-2008

msn 28918

Issued By

Contact to

A.Nutretsov [email protected]




60 781

60 554

49 895

46 720

Basic Weight Data




31 799

44.29

20.04


Available Version

114

8C + 106Y

Configuration Data

Pantry Data






Normal Flight

Reduced Flight

Short Flight


Weight, kg

Ind.

Weight, kg

Ind.

Weight, kg

526

+3.07

463

+2.36

392

Ind.

Weight, kg

+1.73

288

Ind.

+2.03

Dry Operating Data Crew Code

Cockpit Crew

Cabin Crew

2/5 2/4 2/3 3/5 3/4 3/3 4/5 4/4 4/3 2/0 3/0 4/0

2 2 2 3 3 3 4 4 4 2 3 4

5 4 3 5 4 3 5 4 3 0 0 0

Cabin crew Location

Pantry Code “A”

Pantry Code “R”

FWD Utility Zone

Aft Utility Zone

DOW

DOI

DOW

DOI

2 2 1 2 2 1 2 2 1 -

3 2 2 3 2 2 3 2 2 -

33 472 33 367 33 262 33 582 33 477 33 372 33 692 33 587 33 482 -

45,66 44,99 46,16 44,29 43,63 44,79 42,93 42,27 43,43 -

33 408 33 303 33 198 33 518 33 413 33 308 33 628 33 523 33 418 -

44,95 44,28 45,45 43,58 42,92 44,08 42,22 41,56 42,72 -

Pantry Code “S” DOW 33 337 33 232 33 127 33 447 33 342 33 237 33 557 33 452 33 347 -

DOI 44,32 43,66 44,82 42,96 42,30 43,46 41,60 40,93 42,10 -

Pantry Code “O” DOW 32 709 32 819 32 929

DOI 44,96 43,60 42,23



Page 1 of 1


A/C Reg. VP-BYL

B 737-500 Doc. №

WBI - VP-BYL- 01

msn 28920

Issue Date

Effective From

Issued By

Contact to

30-Aug-2008

30-Aug-2008

A.Nutretsov

[email protected]




60 781

60 554

49 895

46 720

Basic Weight Data




31 666

42.97

19.11


Available Version

114

8C + 106Y

Configuration Data

Pantry Data






Normal Flight

Reduced Flight

Short Flight


Weight, kg

Ind.

Weight, kg

Ind.

Weight, kg

526

+3.07

463

+2.36

392

Ind.

+1.73

Weight, kg

Ind.

288

+2.03


5 4 3 5 4 3 5 4 3 0 0 0

Cockpit Crew

Cabin Crew

2 2 2 3 3 3 4 4 4 2 3 4

5 4 3 5 4 3 5 4 3 0 0 0

Cabin crew Location

Pantry Code “A” Pantry Code “R”

Pantry Code “S” Pantry Code “O”

FWD Utility Zone

Aft Utility Zone

DOW

DOI

DOW

DOI

DOW

DOI

DOW

DOI

2 2 1 2 2 1 2 2 1 -

3 2 2 3 2 2 3 2 2 -

33 339 33 234 33 129 33 449 33 344 33 239 33 559 33 454 33 349 -

44,33 43,67 44,83 42,97 42,30 43,47 41,60 40,94 42,10 -

33 276 33 171 33 066 33 386 33 281 33 176 33 496 33 391 33 286 -

43,62 42,96 44,12 42,26 41,59 42,76 40,89 40,23 41,39 -

33 205 33 100 32 995 33 315 33 210 33 105 33 425 33 320 33 215 -

43,00 42,33 43,50 41,63 40,97 42,13 40,27 39,60 40,77 -

32 576 32 686 32 796

43,63 42,27 40,90



Page 1 of 1


A/C Reg. VP-BYM

B 737-500 Doc. №

WBI - VP-BYM - 01

msn 28917

Issue Date

Effective From

Issued By

Contact to

30-Aug-2008

30-Aug-2008

A.Nutretsov

[email protected]




60 781

60 554

49 895

46 720

Basic Weight Data




31 479

43.55

19.54


Available Version

114

8C + 106Y

Configuration Data

Pantry Data






Normal Flight

Reduced Flight

Short Flight

Training or Ferry Flight Weight, Ind. kg

Weight, kg

Ind.

Weight, kg

Ind.

Weight, kg

526

+3.07

463

+2.36

392

Ind.

+1.73

288

+2.03

Dry Operating Data Crew Code

Cockpit Crew

Cabin Crew

2/5 2/4 2/3 3/5 3/4 3/3 4/5 4/4 4/3 2/0 3/0 4/0

2 2 2 3 3 3 4 4 4 2 3 4

5 4 3 5 4 3 5 4 3 0 0 0

Cabin crew Location

Pantry Code “A”

Pantry Code “R” Pantry Code “S”

Pantry Code “O”

FWD Utility Zone

Aft Utility Zone

DOW

DOI

DOW

DOI

DOW

DOI

DOW

DOI

2 2 1 2 2 1 2 2 1 -

3 2 2 3 2 2 3 2 2 -

33 152 33 047 32 942 33 262 33 157 33 052 33 372 33 267 33 162 -

44,91 44,25 45,41 43,55 42,88 44,05 42,18 41,52 42,68 -

33 089 32 984 32 879 33 199 33 094 32 989 33 309 33 204 33 099 -

44,20 43,54 44,70 42,84 42,17 43,34 41,47 40,81 41,97 -

33 017 32 912 32 807 33 127 33 022 32 917 33 237 33 132 33 027 -

43,58 42,91 44,08 42,21 41,55 42,71 40,85 40,19 41,35 -

32 389 32 499 32 609

44,21 42,85 41,49



Page 1 of 1


A/C Reg. VQ-BAC

B 737-500 Doc. №

WBI - VQ-BAC - 01

msn 27321

Issue Date

Effective From

Issued By

Contact to

02-Feb-2009

02-Feb-2009

A.Nutretsov

[email protected]




58 967

58 740

49 895

46 720

Basic Weight Data




32 161

46.65

21.64


Available Version

114

8C + 106Y

Configuration Data

Pantry Data






Normal Flight

Reduced Flight

Short Flight


Weight, kg

Ind.

Weight, kg

Ind.

Weight, kg

Ind.

Weight, kg

526

+3.07

463

+2.36

392

+1.73

288

Ind.

+2.03


5 4 3 5 4 3 5 4 3 0 0 0

Cockpit Crew

Cabin Crew

2 2 2 3 3 3 4 4 4 2 3 4

5 4 3 5 4 3 5 4 3 0 0 0

Cabin crew Location

Pantry Code “A” Pantry Code “R”

Pantry Code “S”

Pantry Code “O”

FWD Utility Zone

Aft Utility Zone

DOW

DOI

DOW

DOI

DOW

DOI

DOW

DOI

2 2 1 2 2 1 2 2 1 -

3 2 2 3 2 2 3 2 2 -

33 573 33 468 33 363 33 683 33 578 33 473 33 793 33 688 33 583 -

46,87 46,20 47,36 45,51 44,84 46,00 44,15 43,48 44,64 -

33 510 33 405 33 300 33 620 33 515 33 410 33 730 33 625 33 520 -

46,16 45,49 46,65 44,80 44,13 45,29 43,44 42,77 43,93 -

33 439 33 334 33 229 33 549 33 444 33 339 33 659 33 554 33 449 -

45,53 44,87 46,03 44,17 43,51 44,67 42,81 42,15 43,31 -

32 810 32 920 33 030

46,15 44,79 43,43



Page 1 of 1


A/C Reg. VQ-BAD

B 737-500 Doc. №

Issue Date

WBI - VQ-BAD - 01

Effective From

02-Feb-2009 02-Feb-2009

msn 27331

Issued By

Contact to

A.Nutretsov

[email protected]




58 967

58 740

49 895

46 720

Basic Weight Data




31 881

46.54

21.60


Available Version

114

8C + 106Y

Configuration Data

Pantry Data






Normal Flight

Reduced Flight

Short Flight


Weight, kg

Ind.

Weight, kg

Ind.

Weight, kg

526

+3.07

463

+2.36

392

Ind.

Weight, kg

+1.73

288

Ind.

+2.03

Dry Operating Data Crew Code 2/5 2/4 2/3 3/5 3/4 3/3 4/5 4/4 4/3 2/0 3/0 4/0


5 4 3 5 4 3 5 4 3 0 0 0

Cabin crew Location



Pantry Code “ S” Pantry Code “ O”

FWD Utility Zone

Aft Utility Zone

DOW

DOI

DOW

DOI

DOW

DOI

DOW

DOI

2 2 1 2 2 1 2 2 1 -

3 2 2 3 2 2 3 2 2 -

33 473 33 368 33 263 33 583 33 478 33 373 33 693 33 588 33 483 -

48,16 47,49 48,65 46,80 46,13 47,29 45,43 44,77 45,93 -

33 410 33 305 33 200 33 520 33 415 33 310 33 630 33 525 33 420 -

47,45 46,78 47,94 46,09 45,42 46,58 44,72 44,06 45,22 -

33 339 33 234 33 129 33 449 33 344 33 239 33 559 33 454 33 349 -

46,82 46,15 47,31 45,46 44,79 45,95 44,10 43,43 44,59 -

32 710 32 820 32 930

47,44 46,08 44,72



Page 1 of 1


A/C Reg. VQ-BAE

B 737-500 Doc. №

Issue Date

WBI - VQ-BAE - 01

Effective From

24-Feb-2009 24-Feb-2009

msn 27320

Issued By

Contact to

A.Nutretsov

[email protected]




58 967

58 740

49 895

46 720

Basic Weight Data




31 920

45.20

20.66


Available Version

114

8C + 106Y

Configuration Data

Pantry Data






Normal Flight

Reduced Flight

Short Flight


Weight, kg

Ind.

Weight, kg

Ind.

Weight, kg

526

+3.07

463

+2.36

392

Ind.

Weight, kg

+1.73

288

Ind.

+2.03



5 4 3 5 4 3 5 4 3 0 0 0

Cabin crew Location




FWD Utility Zone

Aft Utility Zone

DOW

DOI

DOW

DOI

DOW

DOI

DOW

DOI

2 2 1 2 2 1 2 2 1 -

3 2 2 3 2 2 3 2 2 -

33 474 33 369 33 264 33 584 33 479 33 374 33 694 33 589 33 484 -

46,91 46,24 47,40 45,55 44,88 46,04 44,19 43,52 44,68 -

33 411 33 306 33 201 33 521 33 416 33 311 33 631 33 526 33 421 -

46,20 45,53 46,69 44,84 44,17 45,33 43,48 42,81 43,97 -

33 340 33 235 33 130 33 450 33 345 33 240 33 560 33 455 33 350 -

45,57 44,91 46,07 44,21 43,55 44,71 42,85 42,19 43,35 -

32 711 32 821 32 931

46,20 44,83 43,47



Page 1 of 1


A/C Reg. VP-BXO

B 737-500 Doc. №

Issue Date

WBI - VP-BXO - 01

Effective From

11-Aug-2009 11-Aug-2009

msn 27314

Issued By

Contact to

A.Nutretsov

[email protected]




58 967

58 740

49 895

46 720

Basic Weight Data




31 935

45.17

20.64


Available Version

114

8C + 106Y

Configuration Data

Pantry Data






Normal Flight

Reduced Flight

Short Flight


Weight, kg

Ind.

Weight, kg

Ind.

Weight, kg

526

+3.07

463

+2.36

392

Ind.

Weight, kg

+1.73

288

Ind.

+2.03



5 4 3 5 4 3 5 4 3 0 0 0

Cabin crew Location




FWD Utility Zone

Aft Utility Zone

DOW

DOI

DOW

DOI

DOW

DOI

DOW

DOI

2 2 1 2 2 1 2 2 1 -

3 2 2 3 2 2 3 2 2 -

33 490 33 385 33 280 33 600 33 495 33 390 33 710 33 605 33 500 -

46,88 46,21 47,37 45,52 44,85 46,01 44,16 43,49 44,65 -

33 426 33 321 33 216 33 536 33 431 33 326 33 646 33 541 33 436 -

46,17 45,50 46,66 44,81 44,14 45,30 43,45 42,78 43,94 -

33 355 33 250 33 145 33 465 33 360 33 255 33 575 33 470 33 365 -

45,54 44,88 46,04 44,18 43,51 44,68 42,82 42,15 43,31 -

32 727 32 837 32 947

46,16 44,80 43,44



Page 1 of 1


A/C Reg. VP-BXQ

B 737-500 Doc. №

Issue Date

WBI - VP-BXQ - 01

Effective From

11-Aug-2009 11-Aug-2009

msn 27315

Issued By

Contact to

A.Nutretsov

[email protected]




58 967

58 740

49 895

46 720

Basic Weight Data




31 908

44.59

20.23


Available Version

114

8C + 106Y

Configuration Data

Pantry Data






Normal Flight

Reduced Flight

Short Flight


Weight, kg

Ind.

Weight, kg

Ind.

Weight, kg

526

+3.07

463

+2.36

392

Ind.

Weight, kg

+1.73

288

Ind.

+2.03



5 4 3 5 4 3 5 4 3 0 0 0

Cabin crew Location




FWD Utility Zone

Aft Utility Zone

DOW

DOI

DOW

DOI

DOW

DOI

DOW

DOI

2 2 1 2 2 1 2 2 1 -

3 2 2 3 2 2 3 2 2 -

33 462 33 357 33 252 33 572 33 467 33 362 33 682 33 577 33 472 -

46,29 45,63 46,79 44,93 44,27 45,43 43,57 42,90 44,07 -

33 399 33 294 33 189 33 509 33 404 33 299 33 619 33 514 33 409 -

45,58 44,92 46,08 44,22 43,56 44,72 42,86 42,19 43,36 -

33 328 33 223 33 118 33 438 33 333 33 228 33 548 33 443 33 338 -

44,96 44,29 45,45 43,60 42,93 44,09 42,24 41,57 42,73 -

32 699 32 809 32 919

45,58 44,22 42,86



Page 1 of 1


A/C Reg. VP-BXR

B 737-500 Doc. №

Issue Date

WBI - VP-BXR - 01

Effective From

11-Aug-2009 11-Aug-2009

msn 27316

Issued By

Contact to

A.Nutretsov

[email protected]




58 967

58 740

49 895

46 720

Basic Weight Data




32 077

45.60

20.92


Available Version

114

8C + 106Y

Configuration Data

Pantry Data






Normal Flight

Reduced Flight

Short Flight


Weight, kg

Ind.

Weight, kg

Ind.

Weight, kg

526

+3.07

463

+2.36

392

Ind.

Weight, kg

+1.73

288

Ind.

+2.03



5 4 3 5 4 3 5 4 3 0 0 0

Cabin crew Location




FWD Utility Zone

Aft Utility Zone

DOW

DOI

DOW

DOI

DOW

DOI

DOW

DOI

2 2 1 2 2 1 2 2 1 -

3 2 2 3 2 2 3 2 2 -

33 632 33 527 33 422 33 742 33 637 33 532 33 852 33 747 33 642 -

47,30 46,64 47,80 45,94 45,28 46,44 44,58 43,92 45,08 -

33 568 33 463 33 358 33 678 33 573 33 468 33 788 33 683 33 578 -

46,59 45,93 47,09 45,23 44,57 45,73 43,87 43,21 44,37 -

33 497 33 392 33 287 33 607 33 502 33 397 33 717 33 612 33 507 -

45,97 45,30 46,46 44,61 43,94 45,10 43,25 42,58 43,74 -

32 869 32 979 33 089

46,59 45,23 43,87



Page 1 of 1


A/C Reg. VP-BXV

B 737-500 Doc. №

Issue Date

WBI - VP-BXV - 01

Effective From

11-Aug-2009 11-Aug-2009

msn 27322

Issued By

Contact to

A.Nutretsov

[email protected]




58 967

58 740

49 895

46 720

Basic Weight Data




32 085

45.34

20.74


Available Version

114

8C + 106Y

Configuration Data

Pantry Data






Normal Flight

Reduced Flight

Short Flight


Weight, kg

Ind.

Weight, kg

Ind.

Weight, kg

526

+3.07

463

+2.36

392

Ind.

Weight, kg

+1.73

288

Ind.

+2.03



5 4 3 5 4 3 5 4 3 0 0 0

Cabin crew Location




FWD Utility Zone

Aft Utility Zone

DOW

DOI

DOW

DOI

DOW

DOI

DOW

DOI

2 2 1 2 2 1 2 2 1 -

3 2 2 3 2 2 3 2 2 -

33 640 33 535 33 430 33 750 33 645 33 540 33 860 33 755 33 650 -

47,04 46,38 47,54 45,68 45,02 46,18 44,32 43,65 44,82 -

33 576 33 471 33 366 33 686 33 581 33 476 33 796 33 691 33 586 -

46,33 45,67 46,83 44,97 44,31 45,47 43,61 42,94 44,11 -

33 505 33 400 33 295 33 615 33 510 33 405 33 725 33 620 33 515 -

45,71 45,04 46,20 44,35 43,68 44,84 42,99 42,32 43,48 -

32 877 32 987 33 097

46,33 44,97 43,61



Page 1 of 1


A/C Reg. VP-BXU

B 737-500 Doc. №

Issue Date

WBI - VP-BXU - 01

Effective From

17-Sept-2009 17-Sept-2009

msn 27318

Issued By

Contact to

A.Nutretsov

[email protected]




58 967

58 740

49 895

46 720

Basic Weight Data




31 830

44.86

20.43


Available Version

114

8C + 106Y

Configuration Data

Pantry Data






Normal Flight

Reduced Flight

Short Flight


Weight, kg

Ind.

Weight, kg

Ind.

Weight, kg

526

+3.07

463

+2.36

392

Ind.

Weight, kg

+1.73

288

Ind.

+2.03



5 4 3 5 4 3 5 4 3 0 0 0

Cabin crew Location




FWD Utility Zone

Aft Utility Zone

DOW

DOI

DOW

DOI

DOW

DOI

DOW

DOI

2 2 1 2 2 1 2 2 1 -

3 2 2 3 2 2 3 2 2 -

33 384 33 279 33 174 33 494 33 389 33 284 33 604 33 499 33 394 -

46.57 45.90 47.06 45.21 44.54 45.70 43.85 43.18 44.34 -

33 321 33 216 33 111 33 431 33 326 33 221 33 541 33 436 33 331 -

45.86 45.19 46.35 44.50 43.83 44.99 43.14 42.47 43.63 -

33 250 33 145 33 040 33 360 33 255 33 150 33 470 33 365 33 260 -

45.24 44.57 45.73 43.87 43.21 44.37 42.51 41.85 43.01 -

32 621 32 731 32 841

45.86 44.50 43.13



Page 1 of 1


A/C Reg. VP-BXY

B 737-500 Doc. №

Issue Date

WBI - VP-BXY - 01

Effective From

25-Sept-2009 25-Sept-2009

msn 27328

Issued By

Contact to

A.Nutretsov

[email protected]




58 967

58 740

49 895

46 720

Basic Weight Data




31 990

43.84

19.70


Available Version

114

8C + 106Y

Configuration Data

Pantry Data






Normal Flight

Reduced Flight

Short Flight


Weight, kg

Ind.

Weight, kg

Ind.

Weight, kg

526

+3.07

463

+2.36

392

Ind.

Weight, kg

+1.73

288

Ind.

+2.03



5 4 3 5 4 3 5 4 3 0 0 0

Cabin crew Location




FWD Utility Zone

Aft Utility Zone

DOW

DOI

DOW

DOI

DOW

DOI

DOW

DOI

2 2 1 2 2 1 2 2 1 -

3 2 2 3 2 2 3 2 2 -

33 663 33 558 33 453 33 773 33 668 33 563 33 883 33 778 33 673 -

45,22 44,56 45,72 43,86 43,19 44,36 42,50 41,83 42,99 -

33 600 33 495 33 390 33 710 33 605 33 500 33 820 33 715 33 610 -

44,51 43,85 45,01 43,15 42,48 43,65 41,79 41,12 42,28 -

33 529 33 424 33 319 33 639 33 534 33 429 33 749 33 644 33 539 -

43,89 43,22 44,38 42,53 41,86 43,02 41,17 40,50 41,66 -

32 900 33 010 33 120

44,51 43,15 41,79



Page 1 of 1


A/C Reg. VP-BXZ

B 737-500 Doc. №

WBI - VP-BXZ - 01

Issue Date

Effective From

Issued By

02-Oct-2009

02-Oct-2009

A.Nutretsov

msn 27329 Contact to

[email protected]




58 967

58 740

49 895

46 720

Basic Weight Data




31 730

43.86

19.74


Available Version

114

8C + 106Y

Configuration Data

Pantry Data






Normal Flight

Reduced Flight

Short Flight


Weight, kg

Ind.

Weight, kg

Ind.

Weight, kg

526

+3.07

463

+2.36

392

Ind.

Weight, kg

+1.73

288

Ind.

+2.03



5 4 3 5 4 3 5 4 3 0 0 0

Cabin crew Location




FWD Utility Zone

Aft Utility Zone

DOW

DOI

DOW

DOI

DOW

DOI

DOW

DOI

2 2 1 2 2 1 2 2 1 -

3 2 2 3 2 2 3 2 2 -

33 332 33 227 33 122 33 442 33 337 33 232 33 552 33 447 33 342 -

45.38 44.72 45.88 44.02 43.36 44.52 42.66 41.99 43.16 -

33 269 33 164 33 059 33 379 33 274 33 169 33 489 33 384 33 279 -

44.67 44.01 45.17 43.31 42.65 43.81 41.95 41.28 42.45 -

33 198 33 093 32 988 33 308 33 203 33 098 33 418 33 313 33 208 -

44.05 43.38 44.54 42.69 42.02 43.18 41.33 40.66 41.82 -

32 569 32 679 32 789

44.67 43.31 41.95



Page 1 of 1

WEIGHT AND BALANCE SHEET

Aircraft

Boeing 737-500

VP-BVL VP-BYK VP-BYL VP-BVZ

8C + 106Y 60 781 kg 60 554 kg 49 895 kg 46 720 kg 16 100 kg

MTW MTOW MLW MZFW MFC (0.8 kg/l)

CPT 1

CPT 2

Cargo Weight Index kg

57 171 286 400 514 629 703

Cargo Weight kg

0

82

-1

245

-2

408

-3

571

-4

734

-5

869

-6

CPT 3 Cargo Weight kg

Index

G2

0

Cargo Weight kg

0

-1

105 315

+1

-2

525

+2

-3

735

+3

-4

945

+4

-5

1 155

+5 +6

1 365

D

1 756

Row 5

Row 6

Row 7

Row 8

Row 9

Row 10

Row 12

OB

+ 100 kg + 100 kg + 100 kg

Cargo CPTs FWD CPT 1 FWD CPT 2 AFT CPT 3 AFT CPT 4

+ + + +

100 kg 100 kg 100 kg 100 kg

OA

OB

Pax Index

0

365 1 300 2 600 4 800

Fuel Weight kg

9 800

-1

10 500

-2

11 100

-3

11 800

-4

12 400

-3

13 000

7 000 7 800 -2

13 700

-1

14 400

0

15 000

-2

Index

Pax

1

0

1

3

-2

2-4

-1

2-5

+1

1 2-3

4

-3

5-7

-2

6-9

+2

4

+1

5-6

-4

8 - 10

-3

10 - 13

+3

5-6

+2

7

-5

11 - 12

-4

14 - 17

+4

8

-6

13 - 15

-5

18 - 22

+5

7 8

16 - 18

-6

23 - 26

+6

9 - 10

19 - 21

-7

27 - 30

+7

11

+5 +6

22 - 24

-8

31 - 34

+8

25 - 27

-9

35 - 38

+9

+7

28 - 30

-10

39 - 42 + 10

31 - 33

-11

43 - 46 + 11

+3 +4

804

+8

911

Index

Pax

34 - 36

Pax

0

+1

-12

Specification

PaxZone or Cargo CPT

INDEX -

Index

+2 +3

OA

Index

OB

PAX CABIN

+4 +5 + + + +

-4

6 7 8 9

FWD CPT AFT CPT

OC OD CPT 1 CPT 2 CPT 3 CPT 4

EXTRA CREW EXTRA GALLEY

TOTALS INDEX

16 000 16 100

WEIGHT kg

Loaded Index ZFW (LIZFW)

Weight

+/- TO Fuel IND Corr.

Index

Loaded Index TOW (LITOW) LMC

- 0.9 + 0.93

Total

Trip Fuel (kg)

If Last Minute Change is more than 500 kg new Weight and Balance Sheet must be prepared

Note:

- 1.31 - 1.12 +1.11

% MAC and Stab Setting % MAC

INDEX

Stab

+/- Landing Fuel IND Corr.

Zero Fuel

Loaded Index LAW (LILAW)

Landing

0

65 000

10 4

5

6

20

30

10

8

WEIGHT kg


Takeoff

- 0.88 - 0.61 +0.48 +0.93

12

14

INDEX 40

16 % MAC 18

50 20

60 22

24

70

26

28

80

65 000

30

60 000

60 000 55 000

55 000

2

50 000

MLW 49 895 Kg

3

-5

50 000

MZFW 46 720 Kg

1

45 000

45 000

-6

-10 0

WEIGHT (kg)

+

DOI / DOW

+1

19 + 14 20 - 21 + 15 22 + 16 23 + 17 24 + 18

+10

40 000

40 000 3

35 000

Do not operate in shaded area!

30 000

1 Zero Fuel Check

30 000

2 Take-Off Check

-10.6

3 Landing Check

25 000 For more accuracy see the next page

35 000

2

15 600

9 200

Row 24

BALANCE CALCULATION TABLE

12 13 - 14 + 10 15 + 11 16 - 17 + 12 18 + 13

+9

-3

-9

9 000

Row 23

OD

-8

8 700

Row 22

MTOW 60 554 Kg -1

-7

8 300

9 800

Index

Row 21

OD

-1

0

696

OC

1-2

Fuel Adjustment Index Index

Row 20

OC

+1person / 80 kg - 1.1

Galleys G1 G2 G4B

Row 19

Passenger Compartment Index Corrections

Index

589

-1person / 75 kg -1person / 75 kg

Row 18

A

OA

Miscellanious Index Corrections

Fuel Weight kg

Row 17

A

Last Minute Change

Cabin Crew FWD Attend. AFT Attend.

Row 16

B A

482

Number/Weight

Row 15

A

1 132 +11

Place Cockpit

Row 14

B

A

375

1 125

Row 2

C

LAVA

268

1 018

A G4B

Row 1

A

161

+8

CPT 4

E

54

+7

1 575

CPT 3

E

CPT 4

Index

CPT 2

F

F

G1

Cargo Compartment Index Corrections CPT 1

PREPARED BY

PAX VERSION 8C + 106 Y Seats

VP-BYM

Configuration

FLIGHT № DATE

0

10

20

30

Rev. 0 21-Feb-2008

40

50

60

70

25 000

80

WEIGHT AND BALANCE SHEET

Aircraft

FLIGHT № DATE

Boeing 737-500

VP-BVN

PREPARED BY

PAX VERSION 8C + 106 Y Seats CPT 1

Configuration

8C + 106Y 58 967 kg 58 740 kg 49 895 kg 46 720 kg 16 100 kg

MTW MTOW MLW MZFW MFC (0.8 kg/l)

G2

CPT 2


57 171 286 400 514 629 703

Cargo Weight kg

0

82

-1

245

-2

408

-3

571

-4

734

-5

869

-6


Index

0

Cargo Weight kg

0

-1

105 315

+1

-2

525

+2

-3

735

+3

-4

945

+4

-5

1 155

+5 +6

1 365

D

1 756

Row 6

Row 7

Row 8

Row 9

Row 10

Row 12

OB

OA

+ 100 kg + 100 kg + 100 kg


+ + + +

100 kg 100 kg 100 kg 100 kg

OB

Pax Index

365 1 300 2 600 4 800

Fuel Weight kg

0

9 800

-1

10 500

-2

11 100

-3

11 800

-4

12 400

-3

13 000

7 000 7 800 -2

13 700

-1

14 400

0

15 000

-1 -2

Pax

0

1

3

-2

2-4

-1

2-5

+1

1 2-3

4

-3

5-7

-2

6-9

+2

4

+1

5-6

-4

8 - 10

-3

10 - 13

+3

5-6

+2

7

-5

11 - 12

-4

14 - 17

+4

8

-6

13 - 15

-5

18 - 22

+5

7 8

16 - 18

-6

23 - 26

+6

9 - 10

19 - 21

-7

27 - 30

+7

11

+5 +6

22 - 24

-8

31 - 34

+8

25 - 27

-9

35 - 38

+9

+7

28 - 30

-10

39 - 42 + 10

31 - 33

-11

43 - 46 + 11

+3 +4

804

+8

911

Index

Index

1

34 - 36

-12

-4


+1

Index

DOI / DOW

+1 +2 +3

OA

Index

OB

PAX CABIN

+4 +5 + + + +

6 7 8 9

FWD CPT

12 13 - 14 + 10 15 + 11 16 - 17 + 12 18 + 13

AFT CPT



TOTALS INDEX

16 000 16 100

WEIGHT kg


Weight

Loaded Index TOW (LITOW) LMC

- 0.9 + 0.93

Total

Trip Fuel (kg)


Note:

- 1.31 - 1.12 +1.11


INDEX

Stab


Zero Fuel


Landing

0

65 000

10 4

5

6

20

30

10

8

WEIGHT kg


Takeoff

- 0.88 - 0.61 +0.48 +0.93

12

14

60 000

INDEX 40

16 % MAC 18

50 20

60 22

24

70

26

28

80

65 000

30

60 000

MTOW 58 740 Kg

55 000

55 000

2

50 000

MLW 49 895 Kg

3

50 000

MZFW 46 720 Kg

1

45 000

45 000

-6

-10 0

WEIGHT (kg)

+

+/- TO Fuel IND Corr.

40 000

40 000 3

35 000


30 000

1 Zero Fuel Check

30 000

2 Take-Off Check

-10.6

3 Landing Check


35 000

2

15 600

9 200

Row 24

INDEX

Index

-5

-9

9 000

Row 23

-

-8

8 700

Row 22


19 + 14 20 - 21 + 15 22 + 16 23 + 17 24 + 18

+10

Specification

Pax

0

+9

-3

-7

8 300

9 800

Index

Row 21

OD

Pax

0

696

OC

-1


Row 20

OD

+1person / 80 kg - 1.1

Galleys G1 G2 G4B

Row 19

OC

1-2

Index

589


Row 18



Fuel Weight kg

Row 17

A

Last Minute Change


Row 16

A

OA

482

Number/Weight

Row 15

A

1 132 +11

Place Cockpit

Row 14

B A

375

1 125

Row 5

B

A

268

1 018

Row 2

C

LAVA

161

+8

A G4B

Row 1

A

54

+7

1 575

E

CPT 4

Index

CPT 4

E


CPT 3

F

F

G1

CPT 2

0

10

20

30

Rev. 0 10-Aug-2008

40

50

60

70

25 000

80

Aircraft

VQ-BAC VQ-BAD VQ-BAE VP-BXO VP-BXQ VP-BXR VP-BXV

WEIGHT AND BALANCE SHEET Boeing 737-500

VP-BXU VP-BXY

CPT 1

8C + 106Y 58 967 kg 58 740 kg 49 895 kg 46 720 kg 16 100 kg

MTW MTOW MLW MZFW MFC (0.8 kg/l) CPT 2


58 173 289 405 520 638

Cargo Weight kg

0

82

-1

245

-2

408

-3

571

-4

734

-5

869


Index

G2

0

Cargo Weight kg

0

-1

105 315

+1

-2

525

+2

-3

735

+3

-4

945

+4

-5

1 155

+5 +6

1 365

D

1 756

Row 5

Row 6

Row 7

Row 8

Row 9

Row 10

Row 12

OB

+ 100 kg + 100 kg + 100 kg


+ + + +

100 kg 100 kg 100 kg 100 kg

OA

OB

Pax Index

365 1 300 2 600 4 800

Fuel Weight kg

0

9 800

-1

10 500

-2

11 100

-3

11 800

-4

12 400

-3

13 000

7 000 7 800 -2

13 700

-1

14 400

0

15 000

-1 -2

Index

Pax

1

0

1

3

-2

2-4

-1

2-5

+1

1 2-3

4

-3

5-7

-2

6-9

+2

4

+1

5-6

-4

8 - 10

-3

10 - 13

+3

5-6

+2

7

-5

11 - 12

-4

14 - 17

+4

8

-6

13 - 15

-5

18 - 22

+5

7 8

16 - 18

-6

23 - 26

+6

9 - 10

19 - 21

-7

27 - 30

+7

11

+5 +6

22 - 24

-8

31 - 34

+8

25 - 27

-9

35 - 38

+9

+7

28 - 30

-10

39 - 42 + 10

31 - 33

-11

43 - 46 + 11

+3 +4

804

+8

911

Index

Pax

34 - 36

Pax

0

-4

-12

+1

Specification


INDEX

Index

+2 +3

OA

Index

OB

PAX CABIN

+4 +5 + + + +

6 7 8 9

FWD CPT AFT CPT



TOTALS INDEX

16 000 16 100

WEIGHT kg


Weight

+/- TO Fuel IND Corr. Loaded Index TOW (LITOW) LMC

- 0.9 + 0.93

Total

Trip Fuel (kg)


Note:

- 1.31 - 1.12 +1.11


INDEX

Stab


Zero Fuel


Landing

0

65 000

10 4

5

6

20

30

10

8

WEIGHT kg


Takeoff

- 0.87 - 0.61 +0.48 +0.93

12

14

60 000

INDEX 40

16 % MAC 18

50 20

60 22

24

70

26

28

80

65 000

30

60 000

MTOW 58 740 Kg

55 000

55 000

2

50 000

MLW 49 895 Kg

3

50 000

MZFW 46 720 Kg

1

45 000

45 000

-6

-10 0

WEIGHT (kg)

+

DOI / DOW

+1

Index

40 000

40 000 3

35 000


30 000

1 Zero Fuel Check

30 000

2 Take-Off Check

-10.6

3 Landing Check


35 000

2

15 600

9 200

Row 24

-

19 + 14 20 - 21 + 15 22 + 16 23 + 17 24 + 18

+10

-5

-9

9 000

Row 23


-8

8 700

Row 22

OD

12 13 - 14 + 10 15 + 11 16 - 17 + 12 18 + 13

+9

-3

-7

8 300

9 800

Index

Row 21

OD

-1

0

696

OC

1-2


Row 20

OC

+1person / 80 kg - 1.1

Galleys G1 G2 G4B

Row 19


Index

589


Row 18

A

OA


Fuel Weight kg

Row 17

A

Last Minute Change


Row 16

B A

482

Number/Weight

Row 15

A

1 132 +11

Place Cockpit

Row 14

B

A

375

1 125

Row 2

C

LAVA

268

1 018

A G4B

Row 1

A

161

+8

CPT 4

E

54

+7

1 575

CPT 3

E

CPT 4

Index

CPT 2

F

F

G1


PREPARED BY

PAX VERSION 8C + 106 Y Seats

VP-BXZ

Configuration

FLIGHT № DATE

0

10

20

30

Rev. 3 02-Oct-2009

40

50

60

70

25 000

80

AHM560 737-500 Rev9 Trim UTair

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