B737-400 AIRPORT HANDLING MANUAL (AHM 560) (IN KILOGRAM – KG)
B737-400 AIRPORT HANDLING MANUAL
INTRODUCTION
Chapter Page Rev.No. Date
TITLE PAGE
B737-400 AIRPORT HANDLING MANUAL (AHM 560) (IN KILOGRAM – KG) DOCUMENT NO: TWI-M-FO-07 Revision No: 16 16.08.2012 ISTANBUL
OM
INTRO 1 of 33 16 16.08.2012
B737-400 AIRPORT HANDLING MANUAL
INTRODUCTION
Chapter Page Rev.No. Date
TITLE PAGE
B737-400 AIRPORT HANDLING MANUAL (AHM 560) (IN KILOGRAM – KG) DOCUMENT NO: TWI-M-FO-07 Revision No: 16 16.08.2012 ISTANBUL
OM
INTRO 1 of 33 16 16.08.2012
B737-400 AIRPORT HANDLING MANUAL
INTRODUCTION
Chapter Page Rev.No. Date
INTRO 2 of 33 6 29.06.2010
TABLE OF CONTENTS TITLE PAGE .................................................................................................................... 1 TABLE OF CONTENTS ................................................................................................... 2 RECORDS OF REVISION ............................................................................................... 4 DISTRIBUTION LIST ....................................................................................................... 5 LIST OF EFFECTIVE PAGES ......................................................................................... 6 SYSTEM OF AMENDMENT AND REVISIONS ............................................................... 7 2.1. REFERENCES .................................................................................................... 8 A.
COMMUNICATION ADDRESSES .................................................................................. 9
1
SUPPLIERS (HANDLING AGENTS)’ CONTACT ADDRESS ............................. ............ 9
2
TAILWIND AIRLINES CONTACT ADDRESS ADDRESS ................................................................. ............................................. .................... 9
3
AUTOMATICALLY PRODUCED PRODUCED DOCUMENTS DOCUMENTS ........................... .............................. .. 10
4
MESSAGE REQUIREMENTS......................... .............................. ............................. ... 10
5
MESSAGE ADDRESSES........................... ............................. .............................. ........ 10
6
DEFINITION OF CLASS CODES ............................ ............................ .......................... 10
7
DEFINATION OF UNITS OF MEASURE .......................... .............................. .............. 10
8
MULTIPLE SHEETS NUMBERING ............................... ............................... ................. 10
B.
GENERAL INFORMATION ............................ ............................. .............................. .... 11
1
PASSENGER AND BAGGAGE WEIGHTS ............................. .............................. ........ 11
1.1 1.2 1.3
Passenger Weights ........................................................................................... 11 Cabin Baggage Weights .................................................................................... 11 Checked Baggage Weight ................................................................................. 11
2
CREW AND CREW BAGGAGE WEIGHTS WEIGHTS .................................................................. .............................................. .................... 12
2.1. 2.2.
Crew Weights .................................................................................................... 12 Crew Baggage Weights ..................................................................................... 12
3
DRY OPERATING WEIGHT AND DRY OPERATING INDEX SPECIFICATIONS ....... 13
C.
AIRCRAFT DATA ......................................................................................................... 14
1
BALANCE AND SPECIAL INFORMATION – OUTPUT ON LOADSHEET ................... 14
1.1 1.2 1.3 1.3.1 1.3.2.
Balance Output ................................................................................................. 14 Passenger Trim Output ..................................................................................... 14 Special Information ........................................................................................... 14 Captain Information ........................................................................................... 14 Load Message ................................................................................................... 14
2
BASIC INDEX AND MAC FORMULA.......................... ............................... ................... 15
2.1. 2.2.
Examples and Definitions .................................................................................. 15 Index Formula ................................................................................................... 15
OM
B737-400 AIRPORT HANDLING MANUAL
INTRODUCTION
Chapter Page Rev.No. Date
INTRO 3 of 33 6 29.06.2010
2.3. MAC Information ............................................................................................... 15 2.4. Stabilizer Trim Setting ....................................................................................... 16 2.4.1. Stabilizer Trim Setting Flaps 5 .......................................................................... 16 2.4.2. Stabilizer Trim Setting Flaps 15 ........................................................................ 17 2.5. AIRCRAFT REGISTRATIONS, WEIGHT AND INDEX DETAILS ..................... 18 2.6. LIMITATIONS .................................................................................................... 19 2.6.1. Aircraft Weight Limitations................................................................................. 19 2.7. CG – Limits for Loadsheet Purposes................................................................. 20 2.7.1. TC-TLA, TC-TLB, TC-TLC, TC-TLD, TC-TLE ................................................... 20 2.7.2. Trim Sheet (Sample) ......................................................................................... 21 2.8. EFFECT OF FUEL ............................................................................................ 22 2.9. CREW ............................................................................................................... 23 2.9.1. Number of Cockpit Crew Seats and Average Location ..................................... 23 2.9.2. Number of Cabin Crew Seats and Average Location ........................................ 23 2.10. GALLEY AND PANTRY .................................................................................... 24 2.10.1. Galleys .............................................................................................................. 24 2.10.2. Pantry Weight/Pantry Code ............................................................................... 25 2.11. PASSENGER CABIN ........................................................................................ 26 2.11.1. Passenger Seats ............................................................................................... 26 2.11.2. Class/Cabin Sections ........................................................................................ 26 2.12. Seating Layout .................................................................................................. 27 2.12.1. Seating Layout Codes ....................................................................................... 27 2.12.2. Seat Plan Layout Facilities and Row Index Influence ........................................ 28 2.13. DETAILS FOR COMPARTMENT TRIM ............................................................ 29 2.14. DETAILS FOR BAY/SECTION TRIM ................................................................ 30 2.15. BALLAST .......................................................................................................... 31 D.
LOAD PLANNING DATA .............................................................................................. 32
1
UNIT LOAD DEVICES DETAILES .................................................... ............................ 32
2
SPECIAL LOADS .......................................................................................................... 33
OM
Chapter Page Rev.No. Date
B737-400 AIRPORT HANDLING MANUAL
INTRODUCTION
INTRO 4 of 33 16 16.08.2012
RECORDS OF REVISION Rev. No.
Edited / Amended Page(s)
Effective Date
Inserted by
Insert Date
0
Original
11.05.2009
Levent SON
11.05.2009
1
1,4,6,9,24
06.07.2009
Levent SON
06.07.2009
2
1, 4, 6, 13, 18, 25, 26, 28, 29, 33
25.08.2009
Ali ASLAN
25.08.2009
3
Skipped for agreement with LB version
4
1, 4, 5, 6, 9, 18, 25, 26, 28
15.02.2010
Alaz BA ŞKAYA
15.02.2010
5
1, 4, 6, 18, 19, 20, 25, 26, 28, 29
19.03.2010
Alaz BA ŞKAYA
22.03.2010
6
1, 3, 4, 6, 9, 18, 19, 20, 25, 26, 28, 29
29.03.2010
Alaz BA ŞKAYA
30.06.2010
7
1, 4, 6, 7, 18, 22
27.07.2010
Alaz BA ŞKAYA
28.07.2010
8
1, 4, 5, 6, 18, 26, 28, 29
09.11.2010
Alaz BA ŞKAYA
15.11.2010
9
1, 4, 6, 9, 18, 26, 28, 29
17.03.2011
Ali ASLAN
17.03.2011
10
1, 4, 5, 6, 18, 26, 28
29.04.2011
Özlem MORO ĞLU
03.05.2011
11
1, 4, 6, 18, 25
27.05.2011
Ali ASLAN
31.05.2011
12
1, 4, 6, 18, 25
08.07.2011
Ali ASLAN
12.07.2011
13
1, 4, 6, 18
15.09.2011
Ali ASLAN
17.09.2011
14
1, 4, 6, 18
24.05.2012
Özlem MORO ĞLU
24.05.2012
15
1, 4, 6, 22
26.06.2012
Ali ASLAN
26.06.2012
16
[ 1, 4, 6, 13, 18
16.08.2012
Özlem MOROĞLU ]
17 18 19 20 21 22
OM
Chapter Page Rev.No. Date
B737-400 AIRPORT HANDLING MANUAL
INTRODUCTION
INTRO 5 of 33 10 29.04.2011
DISTRIBUTION LIST COPY NO.
HOLDERS
COPY
REMARKS
1
Quality Director
1
Digital
2
Ground Operations Director
1
Digital
3
Sub-Contracted Handling Agents
1
Digital
4
Performance Engineer
1
A4
TOTAL NOTE: This document is available via library on Company Network. For more information, consult Quality or Flight Support Department.
OM
Chapter Page Rev.No. Date
B737-400 AIRPORT HANDLING MANUAL
INTRODUCTION
INTRO 6 of 33 16 16.08.2012
LIST OF EFFECTIVE PAGES Page No. Rev. No.
OM
Revision Date
Page No.
Rev. No.
Revision Date
1
16
16.08.2012
18
16
16.08.2012
2
6
29.06.2010
19
6
29.06.2010
3
6
29.06.2010
20
6
29.06.2010
4
16
16.08.2012
21
0
11.05.2009
5
10
29.04.2011
22
15
26.06.2012
6
16
16.08.2012
23
0
11.05.2009
7
7
27.07.2010
24
1
06.07.2009
8
0
11.05.2009
25
12
08.07.2011
9
9
17.03.2011
26
10
29.04.2011
10
0
11.05.2009
27
0
11.05.2009
11
0
11.05.2009
28
10
29.04.2011
12
0
11.05.2009
29
6
29.06.2010
13
16
16.08.2012
30
0
11.05.2009
14
0
11.05.2009
31
0
11.05.2009
15
0
11.05.2009
32
2
25.08.2009
16
0
11.05.2009
33
2
25.08.2009
17
0
11.05.2009
B737-400 AIRPORT HANDLING MANUAL
INTRODUCTION SYSTEM OF AMENDMENT AND REVISIONS [ Refer to TWI-P-QD-001 ]
OM
Chapter Page Rev.No. Date
INTRO 7 of 33 7 27.07.2010
B737-400 AIRPORT HANDLING MANUAL
INTRODUCTION 2.1.
REFERENCES
•
SHT J, Turkish Directorate General of Civil Aviation (DGCA)
•
EU-OPS 1.620, EASA
•
AHM560, IATA
•
Performance Engineering Manual, Boeing
•
Aircraft Weight and Balance Manual, Boeing
•
Airplane Flight Manual, Boeing
•
Aircraft LOPA
•
Aircraft Weighting Report
•
Tailwind Airlines catering weight
OM
Chapter Page Rev.No. Date
INTRO 8 of 33 0 11.05.2009
B737-400 AIRPORT HANDLING MANUAL
COMMUNICATIONADDRESSES EDP-SYSTEM SEMI-PERMANENT DATA FOR CHECK-IN AND LOAD CONTROL
Chapter Page Rev.No. Date
COMMUNICATION ADDRESSES
A 9 of 33 9 17.03.2011
A Sheet 1
TWI A.
COMMUNICATION ADDRESSES
1
SUPPLIERS (HANDLING AGENTS)’ CONTACT ADDRESS
Contact Name
Zafer KARAGÖZOĞLU
Phone
+90-212-465 38 77
Fax
+90-212-465 38 79
SITA Address
ISTTLXH
E- mail
[email protected]
Addresses
Atatürk Havalimanı İç Hatlar C Blok DCM-133 Yeşilköy / İstanbul / Turkey
2
TAILWIND AIRLINES CONTACT ADDRESS
Trade Name
Tailwind Havayollar ı A.Ş.
Doing Business As
Tailwind Airlines
Airline 3-letter Code
TWI
Contact Name
Özlem MOROĞLU
Tel
+90-212-465 37 37
Fax
+90-212-465 37 31
SITA address
N/A
E-Mail
[email protected]
Address
Dünya Ticaret Merkezi A-2 Blok K:13 No:395 Istanbul / Turkey
OM
B737-400 AIRPORT HANDLING MANUAL
COMMUNICATIONADDRESSES
Chapter Page Rev.No. Date
COMMUNICATION ADDRESSES
EDP-SYSTEM SEMI-PERMANENT DATA FOR CHECK-IN AND LOAD CONTROL
A 10 of 33 0 11.05.2009
A Sheet 2
TWI 3
AUTOMATICALLY PRODUCED DOCUMENTS X NOTOC X SEAT PLAN X LOAD PLAN PASSENGER INFO LIST X LOAD SHEET X LOADING INSTRUCTION REPORT
4
MESSAGE REQUIREMENTS X LDM - Load Message AHM 583 ALI - Abbreviated Load İnformation Message AHM 584 CPM - Container / Pallet Message AHM 587 UCM - ULD Control Message AHM 424 (Dispatch Only) X MVT - Movement Message AHM 730 and 780 X DIV - Diversion Message AHM 781 X SOM - Seat Occupied Message Recommended Practice 1712 PTM - Passenger Transfer Message Recommended Practice 1718 X 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 1719 X PNL/ADL - Pasenger Name List and Additions and Deletions List 1708 (Acceptance Only) SAL - Seats Avaible List Recommended Practice 1713 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
6
DEFINITION OF CLASS CODES F: FIRST C: BUSINESS Y: ECONOMY M: ECONOMY DISCOUNTED
7
8
DEFINATION OF UNITS OF MEASURE Weight
Kg
Volume
Cu.mtr
Lengh
Inches
Liquid Volume
Liter
MULTIPLE SHEETS NUMBERING
For example: C1.a, C2.b, C3.a, C3.b, etc.
OM
Chapter Page Rev.No. Date
B737-400 AIRPORT HANDLING MANUAL
GENERAL INFORMATION
GENERAL INFORMATION
EDP-SYSTEM SEMI-PERMANENT DATA FOR CHECK-IN AND LOAD CONTROL
B 11 of 33 0 11.05.2009
B Sheet 1
TWI B. 1
GENERAL INFORMATION PASSENGER AND BAGGAGE WEIGHTS
1.1 Passenger Weights Passenger Seats 20 and more
Passenger mass
30 and more
Male
Female
All Adult
All Flight except Holiday charter
88 kg
70 kg
84 kg
Holiday Charter
83 kg
69 kg
76 kg
Children
35 kg
35 kg
35 kg
(Ref: EU-OPS 1.620)
1.2 Cabin Baggage Weights Carry-on Baggage weight is included in the above mentioned Passenger Weights.
1.3 Checked Baggage Weight Checked Baggage weights must be calculate for each baggage during the Checkin.
OM
B737-400 AIRPORT HANDLING MANUAL
GENERAL INFORMATION EDP-SYSTEM SEMI-PERMANENT DATA FOR CHECK-IN AND LOAD CONTROL
Chapter Page Rev.No. Date
GENERAL INFORMATION
B 12 of 33 0 11.05.2009
B Sheet 2
TWI 2 2.1.
2.2.
CREW AND CREW BAGGAGE WEIGHTS Crew Weights Cockpit crew
85 kg
Cabin crew
75 kg
Crew Baggage Weights Crew weights include hand baggage. Hold baggage is to be treated as follows:
Long Haul: Not Applicable Short Haul: Not Applicable
OM
B737-400 AIRPORT HANDLING MANUAL
GENERAL INFORMATION
Chapter Page Rev.No. Date
GENERAL INFORMATION
EDP-SYSTEM SEMI-PERMANENT DATA FOR CHECK-IN AND LOAD CONTROL
B 13 of 33 16 16.08.2012
B Sheet 3
TWI 3
DRY OPERATING WEIGHT AND DRY OPERATING INDEX SPECIFICATIONS
DOW Item
DOI
Include Exclude Include Exclude
Basic Weight
X
X
Cockpit Crew
X
X
Cabin Crew
X
X
Crew Baggage
X
X
Pantry
X
X
Containers
X
X
Pallets
X
X
Potable Water
[ EIC
X
X X
EIC: Equipment in cargo compartment
OM
Remarks
X
]
Chapter Page Rev.No. Date
B737-400 AIRPORT HANDLING MANUAL
AIRCRAFT DATA EDP-SYSTEM SEMI-PERMANENT DATA FOR CHECK-IN AND LOAD CONTROL
AIRCRAFT DATA
1
C Sheet 1
TWI
B737-400 C.
C 14 of 33 0 11.05.2009
AIRCRAFT DATA BALANCE AND SPECIAL INFORMATION – OUTPUT ON LOADSHEET
1.1 Balance Output Remarks Basic Index Dry Operating Index Deadload Index Deadload MAC Loaded Index at Zero Fuel Weight Loaded Index at Take-off Weight Loaded Index at Landing Weight MAC - at Zero Fuel Weight MAC - at Take-off Weight MAC - at Landing Weight Stabilizer Trim Setting at Take-off
BI DOI DLI MACDLW LIZFW LITOW LILAW MACZFW MACTOW MACLAW STABTO*
X
X X X X X X X
*Specify ANU (Aircraft Nose Up) or AND (Aircraft Nose Down) as appropriate
1.2 Passenger Trim Output Remarks
Class Trim
Not Allowed
Cabin Area Trim
X
Seat Row Trim
X
1st Priority
1.3 Special Information Specify the information to be entered in the lower parts of EDP Loadsheet.
1.3.1 Captain Information Captain’s information/notes, Center of Gravity Limits, ramp weight, etc.
1.3.2. Load Message Load message before LMC, if required to be shown. OM
B737-400 AIRPORT HANDLING MANUAL
INTRODUCTION EDP-SYSTEM SEMI-PERMANENT DATA FOR CHECK-IN AND LOAD CONTROL
AIRCRAFT DATA B737-400
2 2.1.
Chapter Page Rev.No. Date
C 15 of 33 0 11.05.2009
C Sheet 2a
TWI
BASIC INDEX AND MAC FORMULA Examples and Definitions
Index = I =
W ( Sta - Ref. Sta ) -----------------------------C
% MAC =
C(I - K) [-------------- + Ref. Sta. ] - LEMAC W -------------------------------------------------MAC -----------------100
+K
W Sta.
Weight actual Station, horizontal distance in inches or metres from station zero to the location. Ref. Sta. Reference station/axis. Selected station around which all index values are calculated Constant used as a plus value to avoid negative index figures. K Constant used as a denominator to convert moment values into index C values. I (Index) value corresponding to respective weight. Length of Mean Aerodynamic Chord in inches or meters. MAC LEMAC Horizontal distance in inches or metres from the station zero to location of the Leading Edge of the MAC.
2.2.
2.3.
OM
Index Formula Ref. Sta. = 648.5
Inches from zero
K
= 40
Constant
C
= 31.752
Kg.inch - Constant
MAC Information Length of MAC = 134.5
inches
LEMAC at
Inches from zero
= 625.6
B737-400 AIRPORT HANDLING MANUAL
AIRCRAFT DATA EDP-SYSTEM SEMI-PERMANENT DATA FOR CHECK-IN AND LOAD CONTROL
AIRCRAFT DATA B737-400
2.4. 2.4.1.
OM
Stabilizer Trim Setting Stabilizer Trim Setting Flaps 5
Chapter Page Rev.No. Date
C 16 of 33 0 11.05.2009
C Sheet 2b
TWI
B737-400 AIRPORT HANDLING MANUAL
AIRCRAFT DATA EDP-SYSTEM SEMI-PERMANENT DATA FOR CHECK-IN AND LOAD CONTROL
AIRCRAFT DATA B737-400
2.4.2.
OM
Stabilizer Trim Setting Flaps 15
Chapter Page Rev.No. Date
C 17 of 33 0 11.05.2009
C Sheet 3
TWI
Chapter Page Rev.No. Date
B737-400 AIRPORT HANDLING MANUAL
AIRCRAFT DATA EDP-SYSTEM SEMI-PERMANENT DATA FOR CHECK-IN AND LOAD CONTROL
AIRCRAFT DATA
C Sheet 3
TWI
B737-400 2.5.
C 18 of 33 16 16.08.2012
AIRCRAFT REGISTRATIONS, WEIGHT AND INDEX DETAILS
DRY OPERATING WEIGHT [ ]
BASIC EMPTY WEIGHT [ X ]
NOTE: The standard fleet weight and index shown below should only be used for load planning purposes and must never be used for the final loadsheet. The loadsheet must always show the actual Basic Weight/Index. If the actual is not shown below it can be obtained from the incoming load message but must always be checked against the weight schedule on board.
[ Fleet Weight
Fleet Index
34.208
33,06
Standard Registration
Weight Adjustment Difference BEW From Std.
Index Adjustment BI
Difference From Std.
TC-TLA
34.258
51
33,45
0,39
TC-TLB
34.144
-64
32,49
-0,57
TC-TLC
34.348
140
32,55
-0,51
TC-TLD
34.168
-40
33,78
0,72
TC-TLE
34.120
-88
33,03
-0,03 ]
BEW includes potable water (79 Kg) and Toilet Chemical (23 Kg) [ ] .
Note: Notification for data changes at short notice may also be made by means of a data exchange message (AHM 562). Note that all weights in this manual are in kilogram (Kg).
OM
Chapter Page Rev.No. Date
B737-400 AIRPORT HANDLING MANUAL
AIRCRAFT DATA EDP-SYSTEM SEMI-PERMANENT DATA FOR CHECK-IN AND LOAD CONTROL
AIRCRAFT DATA B737-400
2.6.
LIMITATIONS
2.6.1.
Aircraft Weight Limitations
Operator defined maximum weights for: A/C REG.
MTW MTOW MZFW MLW BEW BI
OM
MTW (kg)
MTOW (kg)
MLW (kg)
MZFW (kg)
TC-TLA
65.317
65.090
54.885
51.256
TC-TLB
65.317
65.090
54.885
51.256
TC-TLC
65.317
65.090
54.885
51.256
TC-TLD
65.317
65.090
54.885
51.256
TC-TLE
65.317
65.090
54.885
51.256
: Maximum Designed Taxi Weight : Maximum Designed Takeoff Weight : Maximum Zero Fuel Weight : Maximum Landing Weight : Basic Empty Weight : Basic Index
C 19 of 33 6 29.06.2010
C Sheet 4
TWI
Chapter Page Rev.No. Date
B737-400 AIRPORT HANDLING MANUAL
AIRCRAFT DATA EDP-SYSTEM SEMI-PERMANENT DATA FOR CHECK-IN AND LOAD CONTROL
C 20 of 33 6 29.06.2010
C
AIRCRAFT DATA
Sheet 5a
TWI
B737-400 2.7.
CG – Limits for Loadsheet Purposes
Enter the forward and aft balance limits in the boxes, commencing at the lowest weight and terminating at the highest weight to be checked.
IMPORTANT: If limits are affected and/or determined by passenger/fuel/version or other conditions, specify each set of limits on a separate sheet, entering the special condition(s) in the box. 2.7.1. TC-TLA, TC-TLB, TC-TLC, TC-TLD, TC-TLE FORWARD
AFT
Zero Fuel Weight limit
Zero Fuel Weight limit
Weight (Kg) MZFW
Index Value
Weight (Kg)
31.752
30.0
31.752
47.0
44.452
25.0
44.000
60.5
47.627
26.0
51.256
62.0
51.256
18.5
MZFW
Landing Weight (Kg) MLW
Landing Index Value
Weight (Kg)
26.5
31.752
47.0
54.885
16.7
44.000
60.5
54.885
62.5
Take-off Weight (Kg)
OM
Index Value
31.752
MLW
MTOW
Index Value
Take-off Index Value
Weight (Kg)
Index Value
31.752
26.5
31.752
47.0
60.555
14.5
44.000
60.5
63.503
16.5
64.864
64.5
65.090
45.5
65.090
56.5
MTOW
B737-400 AIRPORT HANDLING MANUAL
AIRCRAFT DATA EDP-SYSTEM SEMI-PERMANENT DATA FOR CHECK-IN AND LOAD CONTROL
AIRCRAFT DATA B737-400
2.7.2. Trim Sheet (Sample)
OM
Chapter Page Rev.No. Date
C 21 of 33 0 11.05.2009
C Sheet 5b
TWI
B737-400 AIRPORT HANDLING MANUAL
AIRCRAFT DATA EDP-SYSTEM SEMI-PERMANENT DATA FOR CHECK-IN AND LOAD CONTROL
AIRCRAFT DATA B737-400
2.8.
Chapter Page Rev.No. Date
C 22 of 33 15 26.06.2012
C Sheet 6
TWI
EFFECT OF FUEL Remarks Standard Procedure
X
Non-Standard Procedure FUEL DENSITY: 0.8507 KG/LT [
Fuel Weight (kg)
Fuel Index
907
-1,05
1.814
-1,80
2.722
-2,50
3.629
-2,90
4.536
-3,30
5.443
-3,60
6.350
-3,70
7.257
-3,40
8.165
-2,65
9.072
-0,60
9.655
0,67
9.979
0,16
10.886
-1,33
11.793
-2,70
12.701
-3,80
13.608
-5,25
14.515
-6,68
15.422
-7,90
16.329
-9,30
17.104
-10,50
] OM
Chapter Page Rev.No. Date
B737-400 AIRPORT HANDLING MANUAL
AIRCRAFT DATA EDP-SYSTEM SEMI-PERMANENT DATA FOR CHECK-IN AND LOAD CONTROL
AIRCRAFT DATA B737-400
2.9. 2.9.1.
C 23 of 33 0 11.05.2009
C Sheet 7
TWI
CREW Number of Cockpit Crew Seats and Average Location Cockpit
Captain First Officer First Observer Second Observer
Maximum number of cockpit seats 1 1 1 1
Length of Arm Weight from Reference (Kg) Station 85 85 85 85
-570,5 -570,5 -535,5 -542,5
Arm
Index Influence per 1 Kg
78 78 113 106
-0.01797 -0.01797 -0.01687 -0.01709
Remarks: Pilots NAV BAGs are considered in length of arm from reference station. The CREW MEMBERs, their BAGGAGE and NAV BAGs are considered in the DOWs/DOIs. 2.9.2.
Number of Cabin Crew Seats and Average Location
Cabin Fwd entry door Aft entry door
OM
Maximum number of cockpit seats 2 3
Weight (Kg)
Length of arm from Reference Station
Arm
Index Influence per 1 Kg
75 75
-486,5 458,5
162 1107
-0.01532 0.01444
Chapter Page Rev.No. Date
B737-400 AIRPORT HANDLING MANUAL
AIRCRAFT DATA EDP-SYSTEM SEMI-PERMANENT DATA FOR CHECK-IN AND LOAD CONTROL
C 24 of 33 1 06.07.2009
AIRCRAFT DATA
C Sheet 8a
TWI
B737-400 2.10. GALLEY AND PANTRY 2.10.1.
Galleys
FWD G1
Max. Weight (kg) 567
FWD G2
680
-449,5
199,0
-0.01416
AFT G4B
1030
511,5
1.160,0
0.01611
Galleys
OM
Length of arm from reference station -518,5
H-Arm
Index Influence per 1 kg
130,0
-0.01633
Chapter Page Rev.No. Date
B737-400 AIRPORT HANDLING MANUAL
AIRCRAFT DATA EDP-SYSTEM SEMI-PERMANENT DATA FOR CHECK-IN AND LOAD CONTROL
AIRCRAFT DATA
C Sheet 8b
TWI
B737-400 2.10.2.
C 25 of 33 12 08.07.2011
Pantry Weight/Pantry Code
TC-TLA / TC-TLB / TC-TLC / TC-TLD / TC-TLE International 2 Way 1 Way
Domestic 2 Way 1 Way
Ferry Flight
18,6
10,8
18,6
10,8
13,7
-449,5
199 -0,01416 212,0
127,3
127,0
108,0
84,0
511,5
1160 0,01611 393,3
266,2
136,8
115,4
84,0
Total
404,4
282,4
234,2
181,7
Galley
Max Weight
Length of arm
G1
567
-518,5
130 -0,01633
G2
680
G4B
1.030
OM
Arm (inc)
Ind Eff. Per 1 kg
623,9
Chapter Page Rev.No. Date
B737-400 AIRPORT HANDLING MANUAL
AIRCRAFT DATA EDP-SYSTEM SEMI-PERMANENT DATA FOR CHECK-IN AND LOAD CONTROL
AIRCRAFT DATA B737-400
C 26 of 33 10 29.04.2011
C Sheet 9
TWI
2.11. PASSENGER CABIN 2.11.1.
Passenger Seats
TC-TLA , TC-TLB, [TC-TLC], TC-TLD, TC-TLE CABIN SECTION CABIN-A
Rows Number 01-09
CABIN-B
10-19
CABIN-C
20-28
Class/Cabin Sections
NOT AVAILABLE
OM
Length of ARM from Ref. Station
ARM (Inc)
Index Influence Per 1 Kg
-288.70
359.80
-0.00909
60Y
-0.20
648.30
0.00000
54Y
281.50
930.00
0.00886
168Y
TOTAL
2.11.2.
Total Seats 54Y
B737-400 AIRPORT HANDLING MANUAL
INTRODUCTION EDP-SYSTEM SEMI-PERMANENT DATA FOR CHECK-IN AND LOAD CONTROL
Chapter Page Rev.No. Date
C 27 of 33 0 11.05.2009
AIRCRAFT DATA B737-400
C Sheet 10
TWI
2.12. Seating Layout 2.12.1.
Seating Layout Codes
Show the passenger seating layout for the configurations 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.
A
Aisle
O
Over wing seat
B
Bassinet position
P
Stretcher location
C
Crew seat
Q
Quiet zone
E
Emergency exit
S
Smoking
G
Groups
T
Near toilet
H
Incapacitated passenger
U
Unaccompanied minor
I
Infant preference rows/seats
V
Seat left vacant / offered last
J
Rear facing seats
W
No movie
K
Near galley
X
No facility seat, e.g. no distinction between smoking and non-smoking
L
Leg space seat
Y
Not fitted
M
Wheel Chair
Z
Buffer zone
N
No smoking
Alpha / Characters – D, F, R, Blank, not used
OM
Chapter Page Rev.No. Date
B737-400 AIRPORT HANDLING MANUAL
AIRCRAFT DATA EDP-SYSTEM SEMI-PERMANENT DATA FOR CHECK-IN AND LOAD CONTROL
AIRCRAFT DATA B737-400
2.12.2.
C 28 of 33 10 29.04.2011
C Sheet 11
TWI
Seat Plan Layout Facilities and Row Index Influence
TC-TLA , TC-TLB, [TC-TLC], TC-TLD, TC-TLE 168Y ROW
A n i b a C
B n i b a C
C n i b a C
OM
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
A
LEFT B
C
D
RIGHT E
F
IUMH IUMH
IUMH IUMH
IUMH
IUMH
IUMH I I
IUMH I I
I I
I I
I I E
I I E
E I I
E
E
E
E
E
E
E
E
E I I
I I
I I
I I I
I I I
I I
I I
I I I
P
P
I I IP
IUMH IUMH
P P
P P
IPUMH IPUMH
Average Arm 242 271 301 330 360 389 419 448 478 507 535 564 602 640 669 698 727 756 785 814 843 872 901 930 959 988 1,017 1,046
Ind. Inf. per 1 Kg -0.01280 -0.01189 -0.01094 -0.01003 -0.00909 -0.00817 -0.00723 -0.00632 -0.00537 -0.00446 -0.00358 -0.00266 -0.00147 -0.00027 0.00065 0.00156 0.00247 0.00339 0.00430 0.00521 0.00613 0.00704 0.00795 0.00887 0.00978 0.01069 0.01161 0.01252
Chapter Page Rev.No. Date
B737-400 AIRPORT HANDLING MANUAL
AIRCRAFT DATA EDP-SYSTEM SEMI-PERMANENT DATA FOR CHECK-IN AND LOAD CONTROL
AIRCRAFT DATA B737-400
C 29 of 33 6 29.06.2010
C Sheet 12
TWI
2.13. DETAILS FOR COMPARTMENT TRIM For TC-TLA, TC-TLB, TC-TLC, TC-TLD, TC-TLE Compartment Number
Max.Weight Volume (kg) (cu meter)
Volume (cu ft)
Length of Arm from. Ref. Sta.
Arm (Inc)
Index Influence Per 1 kg
FWD HOLD-1
3.306
17,18
607
-279.6
368.9
-0.00880
AFT HOLD-4
4.188
21,69
766
238.0
886.5
0.00750
TOTAL
7.494
38,87
1373
OM
B737-400 AIRPORT HANDLING MANUAL
AIRCRAFT DATA EDP-SYSTEM SEMI-PERMANENT DATA FOR CHECK-IN AND LOAD CONTROL
AIRCRAFT DATA B737-400
2.14. DETAILS FOR BAY/SECTION TRIM Not applicable to TAILWIND AIRLINES
OM
Chapter Page Rev.No. Date
C 30 of 33 0 11.05.2009
C Sheet 13
TWI
B737-400 AIRPORT HANDLING MANUAL
AIRCRAFT DATA EDP-SYSTEM SEMI-PERMANENT DATA FOR CHECK-IN AND LOAD CONTROL
AIRCRAFT DATA B737-400
2.15. BALLAST Not applicable to TAILWIND AIRLINES
OM
Chapter Page Rev.No. Date
C 31 of 33 0 11.05.2009
C Sheet 14
TWI
B737-400 AIRPORT HANDLING MANUAL
LOADING PLANNING DATA EDP-SYSTEM SEMI-PERMANENT DATA FOR CHECK-IN AND LOAD CONTROL
Chapter Page Rev.No. Date
LOAD PLANNING DATA
D 32 of 33 2 25.08.2009
D Sheet 2
TWI D.
LOAD PLANNING DATA
1
UNIT LOAD DEVICES DETAILES
N/A
OM
