Part B- B777 & A330- English

BOEING 777 & AIRBUS A330 LONR / P1

AIRCRAFT HANDLING MANUAL LIST OF NORMAL REVISIONS Rev 06

01 Jan 07

LIST OF NORMAL REVISIONS

Revísion No Issue Date Insert Date Signature

00 01 JAN 07

BOEING 777 & AIRBUS A330 LOEP / P1

AIRCRAFT HANDLING MANUAL LIST OF EFFECTIVE PAGES Rev 06

01 Jan 07

LIST OF EFFECTIVE PAGES

Section Page Rev # Issued Effective Remark

LONR 1 06 01 Jan 07 01 Jan 07 LOEP 1 06 01 Jan 07 01 Jan 07 LOD 1, 2 06 01 Jan 07 01 Jan 07 LOB 1 06 01 Jan 07 01 Jan 07 TOC 1 06 01 Jan 07 01 Jan 07 1.0 1 06 01 Jan 07 01 Jan 07 1.1 1 – 6 06 01 Jan 07 01 Jan 07 1.2 1 – 5 06 01 Jan 07 01 Jan 07 1.3 1 – 30 06 01 Jan 07 01 Jan 07 1.4 1 – 17 06 01 Jan 07 01 Jan 07 1.5 1 – 10 06 01 Jan 07 01 Jan 07 1.6 1 – 16 06 01 Jan 07 01 Jan 07 1.7 1 – 8 06 01 Jan 07 01 Jan 07 2.0 1 06 01 Jan 07 01 Jan 07 2.1 1 – 6 06 01 Jan 07 01 Jan 07 2.2 1 – 5 06 01 Jan 07 01 Jan 07 2.3 1 – 33 06 01 Jan 07 01 Jan 07 2.4 1 – 23 06 01 Jan 07 01 Jan 07 2.5 1 – 5 06 01 Jan 07 01 Jan 07 2.6 1 – 6 06 01 Jan 07 01 Jan 07 2.7 1 – 5 06 01 Jan 07 01 Jan 07

BOEING 777 & AIRBUS A330 LOD / P1

AIRCRAFT HANDLING MANUAL LIST OF DISTRIBUTIONS Rev 06

01 Jan 07

LIST OF DISTRIBUTIONS

No Users Quantity Remark 01 Civil Aviation Administration of Vietnam 03 02 Flight Operation Dept. 01 03 Flight Traning Centre 01 04 Technical Dept. 01 05 Cargo Marketing & Planning Dept. 01 06 Quanlity Assurance Dept. 01 07 Safety & Security Dept. 01 08 Training Dept. 01 09 Marketing Services Dept. 02 10 Northern Regional Office 01 11 Middle Regional Office 01 12 Southern Regional Office 01 13 Noibai Operation Control Centre 01 14 Tansonnhat Operation Control Centre 01 15 Noibai International Airport Ground Services 04 16 Danang International Airport Ground Services 03 17 Tansonnha International Airport Ground Services 04 18 Aircraft Maintenace Centre A75 01 19 Aircraft Maintenance Centre A76 01 20 Vietnam Airlines Branch Offices at ICN 01 21 Ground Handling Company at ICN 01 22 Vietnam Airlines Branch Offices at PUS 01 23 Ground Handling Company at PUS 01 24 Vietnam Airlines Branch Offices at TPE 01 25 Ground Handling Company at TPE 01 26 Vietnam Airlines Branch Offices at KIX 01 27 Ground Handling Company at KIX 01 28 Vietnam Airlines Branch Offices at NRT 01 29 Ground Handling Company at NRT 01 30 Vietnam Airlines Branch Offices at NGO 01 31 Ground Handling Company at NGO 01 32 Vietnam Airlines Branch Offices at PAR 01 33 Ground Handling Company at PAR 01 34 Vietnam Airlines Branch Offices at MOW 01 35 Ground Handling Company at DME 01

BOEING 777 & AIRBUS A330 LOD / P2

AIRCRAFT HANDLING MANUAL LIST OF DISTRIBUTIONS Rev 06

01 Jan 07

LIST OF DISTRIBUTIONS

No Users Quantity Remark

36 Vietnam Airlines Branch Offices at FRA 01 37 Ground Handling Company at FRA 01 38 Vietnam Airlines Branch Offices at MEL 01 39 Ground Handling Company at MEL 01 40 Vietnam Airlines Branch Offices at SYD 01 41 Ground Handling Company at SYD 01 42 Vietnam Airlines Branch Offices at KUL 01 43 Ground Handling Company at KUL 01 44 Vietnam Airlines Branch Offices at BKK 01 45 Ground Handling Company at BKK 01 46 Storage 13 Total 70

BOEING 777 & AIRBUS A330 LOB / P1

AIRCRAFT HANDLING MANUAL LIST OF BULLETINS Rev 06

01 Jan 07

LIST OF BULLETINS

Bulletin No. Date Insert Date Remvove Date Signature

BOEING 777 & AIRBUS A330 TOC / P2

AIRCRAFT HANDLING MANUAL TABLE OF CONTENT Rev 06

01 Jan 07

TABLE OF CONTENT CHAPTER 1 – AIRCRAFT A777 1.1 General 1.2 Aircraft limitation & features 1.3 Cargo hold limitations & versions 1.4 Maximum package & restrictions due to restraint deficiencies 1.5 Door operation 1.6 Cargo loading system 1.7 Form

CHAPTER 2 – AIRCRAFT A330 2.1 General 2.2 Aircraft limitation & features 2.3 Cargo hold limitations & versions 2.4 Maximum package & restrictions due to restraint deficiencies 2.5 Door operation 2.6 Cargo loading system 2.7 Form

CHƯƠNG 1 MÁY BAY BOEING 777

CHAPTER 1

AIRCRAFT BOEING 777

BOEING 777 1.0 / P1

AIRCRAFT HANDLING MANUAL CONTENT Rev 06

01 Jan 07

CONTENT 1.1 General 1.1.1 List of aircraft 1.1.2 Exterior dimension 1.1.3 Ground clearance 1.1.4 Weight and balance definitions 1.2 Aircraft limitation & features 1.2.1 Certificate limitations 1.2.2 Standardized weight and index 1.2.3 Aircraft configuration 1.2.4 Standard taxi fuel 1.2.5 Standardized weight per passenger/ crew 1.2.6 Last minute change 1.2.7 Stretcher 1.3 Cargo hold limitation & version 1.3.1 Structural load limitation 1.3.2 Maximum load for ULD 1.3.3 Lower deck version 1.3.4 Carriage of special load 1.4 Maximum package & restrictions due to restraint deficiencies 1.4.1 Cargo hold and compartment arrangement 1.4.2 Maximum allowable weight due missing or inoperative restraints 1.5 Door operation 1.5.1 Cabin door 1.5.2 Cargo door 1.5.3 Systems requirements for ground service equipment 1.6 Cargo loading system 1.6.1 Cargo handling control system 1.6.2 Restraint system 1.7 Form 1.7.1 Loadsheet 1.7.2 Balance chart for aircraft VNA141/142/149/150 1.7.3 Balance chart for aircraft VNA143/144/145/146 1.7.4 Balance chart for aircraft VNA147 1.7.5 Balance chart for aircraft VNA151 1.7.6 Loading instruction report VNA141/142/149/150/151 1.7.7 Loading instruction report VNA143/144/145/146 1.7.8 Loading instruction report VNA147

1.1 /P1 1.1 /P2 1.1 /P3 1.1 /P3 1.2 /P1 1.2 /P2 1.2 /P2 1.2 /P2 1.2 /P2 1.2 /P5 1.2 /P5 1.3 /P1 1.3 /P3 1.3 /P9 1.3 /P28 1.4 /P1 1.4 /P5 1.5 /P1 1.5 /P2 1.5 /P8 1.6 /P1 1.6 /P3 1.7 /P1 1.7 /P2 1.7 /P3 1.7 /P4 1.7 /P5 1.7 /P6 1.7 /P7 1.7 /P8

BOEING 777 1.1 / P1

AIRCRAFT HANDLING MANUAL GENERAL Rev 06

01 Jan 07

1.1 GENERAL 1.1.1 LIST OF AIRCRAFT This manual is effective for the following aircraft

Model Registration number Configuration

VNA141 C25Y282

VNA142 C25Y282

VNA143 C32Y306

VNA144 C32Y306

VNA145 C32Y306

VNA146 C32Y306

VNA147 C12Y283

VNA149 C25Y282

VNA150 C25Y282

B777-200ER

VNA151 35C 290Y

BOEING 777 1.1 / P2


01 Jan 07

1.1.2 EXTERIOR DIMENSION

BOEING 777 1.1 / P3


01 Jan 07

1.1.3 GROUND CLEARANCE

BOEING 777 1.1 / P4


01 Jan 07

1.1.4 WEIGHT AND BALANCE DEFINITIONS

1. BASIC WEIGHT : Aircraft weight including the furnishing,

fixed equipment

2. DRY OPERATING WEIGHT (DOW)

: Basic weight plus crew and pantry weight and the other. Operational items (such as ballast fuel, stretcher..., if applied).

3. DEADLOAD : Gross weight of the cargo, mail, baggage and empty ULDs.

4. OPERATING WEIGHT : Dry operating weight plus take off fuel.

5. PAYLOAD : Weight of the passengers, cargo, mail, baggage and ULDs.(these may be revenue and/or nonrevenue)

6. ZERO FUEL WEIGHT (ZFW)

: Dry operating weight plus payload.

7. TAKE OFF WEIGHT (TOW)

: Zero fuel weight plus take off fuel

8. DEADLOAD WEIGHT (DLW)

: Zero fuel weight minus the weight of passengers.

9. MAXIMUM TAKE OFF WEIGHT (MTOW)

: Maximum weight at brake release as limited by aircraft (MTOW) strength and airworthiness requirements.

10. MAXIMUM LANDING WEIGHT (MLDW)

: Maximum weight for landing as limited by aircraft (MLDW) strength and airworthiness requirements.

BOEING 777 1.1 / P5


01 Jan 07

11. MAXIMUM ZERO FUEL WEIGHT (MZFW)

: Maximum weight allowed before usable fuel must be (MZFW) loaded in the aircraft as limited by strength and airworthiness requirement.

12. MAXIMUM TAXI WEIGHT (MTW)

: Maximum weight for ground maneuver as limited by (MTW) aircraft strength and airworthiness requirements. (It includes weight of taxi fuel.)

13. C.G

: Center of gravity

14. BA

: Balance arms which are a true measure in inches from the reference datum.

15. %MAC (Percentage of Mean Aerodynamic Chord)

: The location of the aircraft C.G. relative to the leading edge of mean aerodynamic chord (MAC)

16. Index

: The parameter used to express the variation or location of C.G. which is the shortened moment of a certain I weight.

17. Basic index (BI)

: The C.G. Of aircraft basic weight expressed with index

18. Dry Operating Index (DOI)

: The C.G. Of aircraft dry operating weight expressed with index.

19. Laden Index Zero Fuel Weight (LIZFW)

: The C.G. Of aircraft zero fuel weight expressed with (LIZFW) index.

20. Laden Index take off weight (LITOW)

: The C.G. Of aircraft take off weight expressed with (LITOW) index.

21. Index of deadload weight (DLI)

: The C.G. Of aircraft dead load weight expressed with (DLI) index.

22. %MAC of Zero Fuel Weight (MACZFW)

: The C.G. Of aircraft zero fuel weight expressed with % MAC.

23. %MAC of take off weight (MACTOW)

: The C.G. Of aircraft take off weight expressed with % MAC.

24. %MAC of dead load weight (MACDLW)

: The C.G. Of aircraft dead load weight expressed with % MAC.

BOEING 777 1.1 / P6


01 Jan 07

25. Take off fuel

: The amount of fuel on board less the fuel consumed before the take off run.

26. Taxi fuel

: A standard quantity of fuel to cover engine starts and ground maneuvers until start of take off, APU consumption, the amount may be increased when required by local conditions.

27. Trip fuel

: Fuel required to fly from the airport of departure to the planned destination, based on "Planned Operating Conditions". This amount shall include fuel for take off, acceleration, climb, cruise, descent, approach and landing.

28. Ballast fuel

: The fuel in lieu of payload which is specifically loaded for longitudinal balance control.

29. Usable fuel

: Fuel available for aircraft propulsion.

30. Unusable fuel :

Fuel can not be used due to technical limitations and must be included in weight and balance concerns.

BOEING 777 1.2 / P1

AIRCRAFT HANDLING MANUAL AIRCRAFT LIMITATIONS & FEATURES Rev 06

01 Jan 07

1.2 AIRCRAFT LIMITATIONS & FEATURES 1.2.1 CERTIFICATE LIMITATIONS 1.2.1.1 AIRCRAFT GROSS WEIGHT LIMITATIONS

Item VNA141/2 VNA143/4/5/6 VNA147/151 VNA149/150

Max. Taxi weight

Max. Zero fuel weight

Max. Take off weight

Max. Landing weight

298010

195044

297556

208652

265805

195044

264897

208652

263990

195044

263083

208652

298010

195044

297556

208652

1.2.1.2 PERFORMANCE OPERATING WEIGHT To comply with the performance requirements of the aircraft manufacturer, the maximum allowable takeoff and landing weights may be less than structural limits. The maximum allowable weight for that flight that must not exceed the least of the following weights:

− Maximum allowable takeoff weight for the runway intended to be used (including corrections for altitude and gradient, and wind and temperature conditions existing at the takeoff time).

− Maximum takeoff weight considering anticipated fuel and oil consumption that

allows compliance with applicable enroute performance limitations. − Maximum take off weight considering anticipated fuel and oil consumption that

allows compliance with landing distance limitations or arrival at the destination and alternate airports.

BOEING 777 1.2 / P2


01 Jan 07

1.2.2 STANDARDIZED WEIGHT AND INDEX

Please refer to AHM050 validated by Flight Operation Department.

BOEING 777 1.2 / P3


01 Jan 07

1.2.3 AIRCRAFT CONFIGURATION

Aircraft REG Pax Configuration ROW Cabin zone

No of pax

VNA141

VNA142

VNA149

VNA150

25C282Y

1-4

10-16

30-42

45-58

0A

0B

0C

0D

25

54

111

117

VNA143

VNA144

VNA145

VNA146

32C306Y

1-5

10-31

32-46

0A

0B

0C

32

183

123

VNA147 12C283Y

1-2

4-17

20-32

35-49

0A

0B

0C

0D

12

43

117

123

VNA151 35C290Y

1-5

14-32

35-49

0A

0B

0C

35

167

123

BOEING 777 1.2 / P4


01 Jan 07

1.2.4 STANDARD TAXI FUEL

Standard taxi fuel for B777 is : 400 KG 1.2.5 STANDARDIZED WEIGHT PER PASSENGER/CREW

Specification Standard weight (KG)

Chartter flight Definition of age

Adult 75 76 Above 12 years

Child 35 35 Under 12 years but above 2 years Passenger

Infant 00 00 Under 2 years

Cockpit crew 90 Crew

Cabin crew 75

NOTES:

− All standard weights listed above are typical average weight including carry-on baggage. Check-in baggage must be weighed and included in the weight and balance calculation.

− One piece of hand baggage suitable for placing in the closed overhead rack or under

the passenger's seat may be carried on board the aircraft; provided that such maximum dimensions (the sum of the three outside dimensions) must not exceed 23cm x 36cm x 56cm and the weight of the bag must not exceed 7 KG. (Please refer to the decision 854/TCT-DVTT)

− For loading non-standard weight groups, such as athletic or military squads and their

baggage, the actual weights for both passengers and baggage must be utilized.

− The number of passengers whose weights are outside the typical range must be indicated in the Supplementary Information (SI) column of the loadsheet by the load controller responsible for the weight and balance control of this flight.

BOEING 777 1.2 / P5


01 Jan 07

1.2.6 LAST MINUTE CHANGE

The LMC tolerance is: +/- 1500 kg. If exceeded, a new loadsheet is required. The following must be checked : a. Traffic load only: - The LMC positive total weight is lower than the underload before LMC. - No loading limitation exceeded. - The balance at MACZFW and MACTOW remains within the allowed limits. - All the LMC data on the loadsheet is completed.

b. Useable fuel only : - Issue the new loadsheet when change in fuel figures

1.2.7 STRETCHER

Aircraft VNA141/142/149/150 Stretcher position : 55ABC + 56ABC + 57ABC

Total : 9 seats Aircraft VNA143/4/5/6 Stretcher position : 43ABC + 44ABC + 45ABC

Total : 9 seats Aircraft VNA147 Stretcher position : 45A + 46AC + 47AC + 48AC

Total : 7 seats Aircraft VNA151

Stretcher position : 46AC + 47AC + 48AC

Total : 6 seats

BOEING 777 1.3 / P1

AIRCRAFT HANDLING MANUAL CARGO HOLD LIMITATIONS & VERSION Rev 06

01 Jan 07

1.3 CARGO HOLD LIMITATIONS & VERSION 1.3.1 STRUCTURAL LOAD LIMITATION 1.3.1.1 MAXIMUM LOAD FOR CARGO HOLD

COMP. VNA141,142,143,144,

145,146,149,150,151

COMBINED LOAD VNA147

Floor loading limit

1 15.306 kgs 15308 kgs 90,7 kg/ft2

2 16.554 kgs 30.617 kgs

17780 kgs 90,7 kg/ft2

3 11.452 kgs 12677 kgs 90,7 kg/ft2

4 12.700 kgs 22.226 kgs

12700 kgs 90,7 kg/ft2

5 3.806 kgs 3.806 kgs 4082 kgs 68 kg/ft2

1.3.1.2 MAXIMUM GROSS WEIGHT FOR POSITIONS 1.3.1.2.1 FOR CONTAINERS

POSITION ALL POSITIONS

AKE 1587

MAX WEIGHT (KG) DQF (FWD hold only, Except for VNA147) 2449

BOEING 777 1.3 / P2


01 Jan 07

1.3.1.2.2 FOR PALLETS

POSITION 11P 12P 13P 21P 22P 23P 31P 32P 41P 42P

88” 4676 4676 4676 4676 4676 5102 5102 4676 4676 4676 Max weight (KG) 96” 5102 5102 5102 5102 5102 6350 6350 5102 5102 5102

NOTES :

− Crew rest is located on VNA141, VNA142, VNA149, VNA150 only − Aircraft VNA143, VNA144, VNA145, VNA146 can not load pallet at the Aft hold − Aircraft VNA147, VNA151 can load 4 pallet aft hold

BOEING 777 1.3 / P3


01 Jan 07

1.3.2 MAXIMUM LOAD FOR ULD

Type Base Dimension (In)

W X L X H

Volume

(Cu ft) Tare Weight (Kg)

Maximum Gross Weight

(Kg)

AVE/ AKE 60.4” X 61.5” X 64.0” 159 110 1587

DQF 60.4” X 96.0” X 64.0” 252 156 2450

PAG 88” X 125” 381 115 6000

PAJ 88” X 125” 381 110 6000

P1P 88” X 125” 381 105 6000

P6P/ PMC 96” X 125” 407 120 6696 NOTES:

− Comparing with the ULD load limitation and the aircraft structure load limitation where the ULD will be located, choose the lower one as the actual allowable load for the designated ULD position.

− The ULD contents must be loaded in such a manner that they are sufficiently

secured to prevent them from damaging airplane structure as a result of shifting.

− The maximum load includes the tare weight of the ULD and is based on all required restraints being engaged.

BOEING 777 1.3 / P4


01 Jan 07

1.3.2.1 LOADING SIZE CODE K

BOEING 777 1.3 / P5


01 Jan 07

1.3.2.2 LOADING SIZE CODE L

BOEING 777 1.3 / P6


01 Jan 07

1.3.2.3 LOADING SIZE CODE P

1.3.2.4 LOADING SIZE CODE Q

BOEING 777 1.3 / P7


01 Jan 07

1.3.2.5 LOADING SIZE CODE A

BOEING 777 1.3 / P8


01 Jan 07

1.3.2.6 LOADING SIZE CODE M

BOEING 777 1.3 / P9


01 Jan 07

1.3.3 LOWER DECK VERSION 1.3.3.1 FORWARD HOLD 1.3.3.1.1 VERSION TABLE

LDV No.

No of PLT

No of CTNR CPT 1 CPT 2

F000 0P 18A 11LR 12LR 13LR 14LR 21LR 22LR 23LR 24LR 25LR

F101 1P 16A 11P 12LR 13LR 14LR 21LR 22LR 23LR 24LR 25LR

F102 1P 14A 11LR 12P 14LR 21LR 22LR 23LR 24LR 25LR

F103* 1P 14A 11LR 12LR 13LR 14LR 21P 23LR 24LR 25LR

F104 1P 12A 11LR 12LR 13P 22LR 23LR 24LR 25LR

F201 2P 12A 11P 12P 14LR 21LR 22LR 23LR 24LR 25LR

F202* 2P 12A 11P 12LR 13LR 14LR 21P 23LR 24LR 25LR

F203 2P 10A 11P 12LR 13P 22LR 23LR 24LR 25LR

F204 2P 10A 11LR 12P 13P 22LR 23LR 24LR 25LR

F205* 2P 10A 11LR 12P 14LR 21P 23LR 24LR 25LR

F206 2P 10A 11LR 12LR 13P 21P 23LR 24LR 25LR

F207* 2P 10A 11LR 12LR 13LR 14LR 21P 22P 25LR

F301 3P 8A 11P 12P 13P 22LR 23LR 24LR 25LR

F302* 3P 8A 11P 12P 14LR 21P 23LR 24LR 25LR

F303 3P 8A 11P 12LR 13P 21P 23LR 24LR 25LR

F304* 3P 8A 11P 12LR 13LR 14LR 21P 22P 25LR

BOEING 777 1.3 / P10


01 Jan 07

F305 3P 8A 11LR 12P 13P 21P 23LR 24LR 25LR

F306* 3P 8A 11LR 12LR 13LR 14LR 21P 22P 23P

F307* 3P 6A 11LR 12P 14LR 21P 22P 25LR

F308 3P 6A 11LR 12LR 13P 21P 22P 25LR

F401 4P 6A 11P 12P 13P 21P 23LR 24LR 25LR

F402* 4P 6A 11P 12LR 13LR 14LR 21P 22P 23P

F403* 4P 4A 11P 12P 14LR 21P 22P 25LR

F404 4P 4A 11LR 12LR 13P 21P 22P 23P

F405 4P 4A 11LR 12P 13P 21P 22P 23P

F406* 4P 4A 11LR 12P 14LR 21P 22P 23P

F407 4P 4A 11P 12LR 13P 21P 22P 25LR

F501 5P 2A 11P 12P 13P 21P 22P 25LR

F502* 5P 2A 11P 12P 14LR 21P 22P 23P

F503 5P 2A 11P 12LR 13P 21P 22P 23P

F504 5P 2A 11LR 12P 13P 21P 22P 23P

F600 6P 0A 11P 12P 13P 21P 22P 23P

BOEING 777 1.3 / P11


01 Jan 07

NOTES

− Load full-size containers (DQF, ALF) into lower deck cargo compartments with their doors facing toward the compartment doorway. In case the full-size container is deadly stuck in the compartment, the cargo or baggage loaded inside the container may be removed without breaking the container.

− Do not apply * to VNA147, VNA151.

BOEING 777 1.3 / P12


01 Jan 07

1.3.3.1.2 SAMPLES F000: 0 PALLET 18 CONTAINERS 25L 24L 23L 22L 21L 14L 13L 12L 11L

25R 24R 23R 22R 21R 14R 13R 12R 11R

FWD F101: 1 PALLET 16 CONTAINERS 25L 24L 23L 22L 21L 14L 13L 12L

25R 24R 23R 22R 21R 14R 13R 12R

11P

FWD F102: 1 PALLET 14 CONTAINERS 25L 24L 23L 22L 21L 14L 11L

25R 24R 23R 22R 21R 14R

12P

11R

FWD F103*: 1 PALLET 14 CONTAINERS 25L 24L 23L 14L 13L 12L 11L

25R 24R 23R

21P

14R 13R 12R 11R

FWD

BOEING 777 1.3 / P13


01 Jan 07

F104: 1 PALLET 12 CONTAINERS 25L 24L 23L 22L 12L 11L

25R 24R 23R 22R

13P

12R 11R

FWD F201: 2 PALLETS 12 CONTAINERS 25L 24L 23L 22L 21L 14L

25R 24R 23R 22R 21R 14R

12P 11P

FWD F202*: 2 PALLETS 12 CONTAINERS 25L 24L 23L 14L 13L 12L

25R 24R 23R

21P

14R 13R 12R

11P

FWD F203: 2 PALLETS 10 CONTAINERS 25L 24L 23L 22L 13P 12L

25R 24R 23R 22R 12R

11P

FWD

BOEING 777 1.3 / P14


01 Jan 07

F204: 2 PALLETS 10 CONTAINERS 25L 24L 23L 22L 11L

25R 24R 23R 22R

13P 12P

11R

FWD F205*: 2 PALLETS 10 CONTAINERS 25L 24L 23L 14L 11L

25R 24R 23R

21P

14R

12P

11R

FWD F206: 2 PALLETS 10 CONTAINERS 25L 24L 23L 13P 12L 11L

25R 24R 23R

21P

12R 11R

FWD F207*: 2 PALLETS 10 CONTAINERS 25L 14L 13L 12L 11L

25R

22P 21P

14R 13R 12R 11R

FWD

BOEING 777 1.3 / P15


01 Jan 07

F301: 3 PALLETS 8 CONTAINERS 25L 24L 23L 22L 12P

25R 24R 23R 22R

13P

11P

FWD F302*: 3 PALLETS 8 CONTAINERS 25L 24L 23L 14L 12P

25R 24R 23R

21P

14R

11P

FWD F303: 3 PALLETS 8 CONTAINERS 25L 24L 23L 13P 12L

25R 24R 23R

21P

12R

11P

FWD F304*: 3 PALLETS 8 CONTAINERS 25L 14L 13L 12L

25R

22P 21P

14R 13R 12R

11P

FWD

BOEING 777 1.3 / P16


01 Jan 07

F305: 3 PALLETS 8 CONTAINERS 25L 24L 23L 13P 12P 11L

25R 24R 23R

21P

11R

FWD F306*: 3 PALLETS 8 CONTAINERS

14L 13L 12L 11L 23P 22P 21P

14R 13R 12R 11R

FWD F307*: 3 PALLETS 6 CONTAINERS 25L 14L 12P 11L

25R

22P 21P

14R 11R

FWD F308: 3 PALLETS 6 CONTAINERS 25L 13P 12L 11L

25R

22P 21P

12R 11R

FWD

BOEING 777 1.3 / P17


01 Jan 07

F401: 4 PALLETS 6 CONTAINERS 25L 24L 23L 12P

25R 24R 23R

21P 13P

11P


14L 13L 12L 23P 22P 21P

14R 13R 12R

11P

FWD F403*: 4 PALLETS 4 CONTAINERS 25L 14L 12P

25R

22P 21P

14R

11P

FWD F404: 4 PALLETS 4 CONTAINERS

13P 12L 11L 23P 22P 21P

12R 11R

FWD

BOEING 777 1.3 / P18


01 Jan 07

F405*: 4 PALLETS 4 CONTAINERS

14L 11L 23P 22P 21P

14R

12P

11R

FWD F406: 4 PALLETS 4 CONTAINERS 25L 13P 12L

25R

22P 21P

12R

11P

FWD F501: 5 PALLETS 2 CONTAINERS 25L

25R

22P 21P 13P 12P 11P


14L 23P 22P 21P

14R

12P 11P

FWD

BOEING 777 1.3 / P19


01 Jan 07

F503: 5 PALLETS 2 CONTAINERS

13P 12L 23P 22P 21P

12R

11P


11L 23P 22P 21P 13P 12P

11R

FWD F600: 6 PALLETS 0 CONTAINER 23P 22P 21P 13P 12P 11P

FWD

BOEING 777 1.3 / P20


01 Jan 07

1.3.3.2 AFT HOLD 1.3.3.2.1 LOAD VERSION OF VNA143, VNA144, VNA145, VNA146

LDV No.

No of PLT


A000 0P 14A 31LR 32LR 33LR 41LR 42LR 43LR 44LR

1.3.3.2.2 SAMPLE VERSION OF AIRCRAFT VNA143, VNA144, VNA145, VNA146 44L 43L 42L 41L 33L 32L 31L

44R 43R 42R 41R 33R 32R 31R

FWD 1.3.3.2.3 LOAD VERSION OF VNA141, VNA142, VNA149, VNA150

LDV No.

No of PLT


A000 0P 10A 33LR 41LR 42LR 43LR 44LR

A101 1P 6A 32P* 42LR 43LR 44LR

A102 1P 6A 33LR 41LR 41P 44LR

A103 1P 6A 33LR 41LR 42LR 42P

A201 2P 4A 32LR 41LR 41P 42P

A202 2P 2A 32P* 41P 44LR

A203 2P 2A 32P* 42P 42LR

A300 3P 0A 32P* 41P 42P

NOTES: − * : Must be 96” pallet

BOEING 777 1.3 / P21


01 Jan 07

1.3.3.2.4 SAMPLE VERSION OF AIRCRAFT VNA141, VNA142, VNA149, VNA150 A000: 0 PALLET 10 CONTAINERS 44L 43L 42L 41L 33L

44R 43R 42R 41R 33R

CRC

FWD A101: 1 PALLET 6 CONTAINERS 44L 43L 42L

44R 43R 42R

32P*

CRC

FWD A102: 1 PALLET 6 CONTAINERS 44L 41P 41L 33L

44R 41R 33R

CRC

FWD A103: 1 PALLET 6 CONTAINERS 42P 42L 41L 33L

42R 41R 33R

CRC

FWD

BOEING 777 1.3 / P22


01 Jan 07

A201: 2 PALLETS 4 CONTAINERS

41P 41L 33L 42P

41R 33R

CRC

FWD A202: 2 PALLETS 2 CONTAINERS

44L 41P

44R

32P*

CRC


42P 42L

42R

32P*

CRC


41P 42P

32P*

CRC

FWD

BOEING 777 1.3 / P23


01 Jan 07

1.3.3.2.5 LOADING VERSION OF VNA147, VNA151

LDV No.

No of PLT



A101 1P 10A 31P 33LR 41LR 42LR 43LR 44LR

A102 1P 10A 31LR 32LR 33LR 41LR 42LR 42P

A103 1P 10A 31LR 32LR 33LR 41LR 41P 44LR

A201 2P 8A 31LR 32LR 33LR 41LR 41P 42P

A202 2P 6A 31P 32P* 42LR 43LR 44LR

A203 2P 6A 31P 33LR 41LR 42LR 42P

A204 2P 6A 31P 33LR 41LR 41P 44LR

A205 2P 4A 31LR 32P* 41P 44LR

A206 2P 4A 31LR 32P* 42LR 42P

A300 3P 4A 31P 33LR 41LR 41P 42P

A301 3P 2A 31P 32P* 42LR 42P

A302 3P 2A 31P 32P* 41P 44LR

A303 3P 2A 31LR 32P* 41P 42P

A400 4P 0A 31P 32P* 41P 42P

NOTES: − * : Must be 96” pallet

BOEING 777 1.3 / P24


01 Jan 07

1.3.3.2.6 SAMPLE VERSION OF AIRCRAFT VNA147, VNA151 A000: 0 PALLET 14 CONTAINERS 44L 43L 42L 41L 33L 32L 31L

44R 43R 42R 41R 33R 32R 31R

FWD A101: 1 PALLET 10 CONTAINERS 44L 43L 42L 41L 33L

44R 43R 42R 41R 33R

31P

FWD A102: 1 PALLET 10 CONTAINERS

42P 42L 41L 33L 32L 31L

42R 41R 33R 32R 31R


44L 41P 41L 33L 32L 31L

44R 41R 33R 32R 31R

FWD

BOEING 777 1.3 / P25


01 Jan 07


41P 41L 33L 32L 31L 42P

41R 33R 32R 31R


44L 43L 42L

44R 43R 42R

32P* 31P


42P 42L 41L 33L

42R 41R 33R

31P


44L 41P 41L 33L

44R 41R 33R

31P

FWD

BOEING 777 1.3 / P26


01 Jan 07


44L 41P 31L

44R

32P

31R


42P 42L 31L

42R

32P

31R


41P 41L 33L 42P

41R 33R

31P


42P 42L

42R

32P* 31P

FWD

BOEING 777 1.3 / P27


01 Jan 07

A302: 3 PALLETS 2 CONTAINERS 44L 41P

44R

32P* 31P


42P 31L

41P 32P*

31R


41P 42P

32P* 31P

FWD

BOEING 777 1.3 / P28


01 Jan 07

1.3.4 CARRIAGE OF SPECIAL LOAD 1.3.4.1 Magnetized Materials (MAG) Loading

− In order to avoid the significant effect on the aircraft navigation system, Packages of magnetized materials must be loaded not to exceed 2000 kg of magnets per aircraft.

− Packages of magnetized materials must not to be loaded in compartment 1, 2, and 4

1.3.4.2 Other special load 1.3.4.2.1 Dry Ice

Maximum weight/ hold

(With live animal, AVI)


(Without live animal, AVI) Maximum weight/ aircraft

120 KG 200 KG 400 KG

1.3.4.2.2 Live animal

Ventilation system on aircraft

A/C Reg. Hold Ventilation Temperature control

FWD Yes 40C - 270C

AFT No 70C - 210C VNA141, VNA142, VNA149, VNA150

BULK Yes 70C - 210C

FWD Yes 40C - 270C

AFT No 70C - 210C VNA143, VNA144, VNA145, VNA146

BULK Yes 70C - 210C

FWD No No

AFT No 70C - 210C VNA147, VNA151

BULK Yes 70C - 210C

BOEING 777 1.3 / P29


01 Jan 07

Live animal is loaded in compartment 5 only with these limitation:

Live animal (AVI) Quantity/ weight Position

Baby chicken (one day old) 2700 Compartment 5

Bird (Including baby chicken) 1,7 cubic meter Compartment 5

Dog, Cat 2,5 cubic meter Compartment 5

Monkey 100/ 350 KG Compartment 5

Reptile 2,5 cubic meter Compartment 5

Miscellaneous (Small AVI) 1,5 cubic meter Compartment 5

1.3.4.2.3 Radioactive material Radioactive material type A package has category II yellow or category III yellow can be stored in the ULD and loaded at the FWD or AFT hold. The minimum separation distance from the top of the package to nearest inside surface of the floor of the aircraft cabin must be determined in accordance with the below table:

Minimum distance Total sum of TI Meters Ft.in

0.1 - 1.0

1.1 - 2.0

2.1 - 3.0

3.1 - 4.0

4.1 - 5.0

5.1 - 6.0

6.1 - 7.0

7.1 - 8.0

8.1 - 9.0

9.1 - 10.0

0.30

0.50

0.70

0.85

1.00

1.15

1.30

1.45

1.55

1.65

1’00”

1’08”

2’04”

2’10”

3’04”

3’10”

4’04”

4’09”

5’01”

5’05”

If the package of radioactive material can not use the distance separation from above table, It can be devided into 2 or more packages. Each package must be separated to the other at least 3 times of the higher transport index distance

BOEING 777 1.3 / P30


01 Jan 07

Maximum Transport Index 9.0

Bulk load

8.0

ULD load

Minimum distance 155 cm 145 cm

1.3.4.2.4 Priority baggage Priority baggage (BC) and crew baggage (D) must be loaded at AFT hold door side (position 42)

BOEING 777 1.4 / P1

AIRCRAFT HANDLING MANUAL

MAXIMUM PACKAGE & RESTRICTIONS Rev 06 01 Jan 07 DUE TO RESTRAINT DEFICIENCIES

1.4 MAXIMUM PACKAGE & RESTRICTIONS DUE TO RESTRAINT

DEFICIENCIES 1.4.1 CARGO HOLD AND COMPARTMENT ARRANGEMENT 1.4.1.1 FORWARD HOLD 1.4.1.1.1 For Container

1.4.1.1.2 For Pallet

1.4.1.1.3 Allowable package sizes through FWD cargo door

BOEING 777 1.4 / P2



1.4.1.2 AFT HOLD 1.4.1.2.1 For container

1.4.1.2.2 For pallet

BOEING 777 1.4 / P3



1.4.1.2.3 Allowable package sizes through AFT cargo door (Applicable for

VNA141/142/147/149/150/151 only)

1.4.1.2.4 Allowable package sizes through AFT cargo door (Applicable for

VNA143/144/145/146 only)

BOEING 777 1.4 / P4



1.4.1.2.5 Bulk

1.4.1.2.6 Allowable package sizes through bulk cargo door

BOEING 777 1.4 / P5



1.4.2 MAXIMUM ALLOWABLE WEIGHT DUE MISSING OR INOPERATIVE

RESTRAINTS 1.4.2.1 FWD HOLD 1.4.2.1.1 ULDs with size code K, L, P & Q

BOEING 777 1.4 / P6



1.4.2.1.2 Maximum allowable loads with missing FWD, AFT Restraints:

BOEING 777 1.4 / P7



BOEING 777 1.4 / P8



1.4.2.1.3 Maximum allowable loads with missing side Restraints:

1.4.2.1.4 Maximum allowable loads with missing vertical Restraints:

BOEING 777 1.4 / P9



1.4.2.1.5 ULDs with size code A, M

BOEING 777 1.4 / P10



1.4.2.1.5.1 Maximum allowable loads with missing restraint for side code A

BOEING 777 1.4 / P11



1.4.2.1.5.2 Maximum allowable loads with missing restraint for side code M

BOEING 777 1.4 / P12



1.4.2.2 AFT HOLD : 1.4.2.2.1 ULDs with size code K,L and P

1.4.2.2.2 Maximum allowable loads with missing FWD, AFT Restraints:

BOEING 777 1.4 / P13



BOEING 777 1.4 / P14



1.4.2.2.3 Maximum allowable loads with missing Side Restraints:

1.4.2.2.4 Maximum allowable loads with missing Vertical Restraints:

BOEING 777 1.4 / P15



1.4.2.2.5 ULDs with size code A, M

BOEING 777 1.4 / P16



1.4.2.2.5.1 Maximum allowable loads with missing restraint for side code A

BOEING 777 1.4 / P17



1.4.2.2.5.2 Maximum allowable loads with missing restraint for side code M

BOEING 777 1.5 / P1

AIRCRAFT HANDLING MANUAL DOOR OPERATION Rev 06

01 Jan 07

1.5 DOOR OPERATION 1.5.1 CABIN DOOR Cabin door of B777 is installed as follow

Aircraft Doors

(Entry/ Service) Overwing Exits

B777-200ER 6 2

BOEING 777 1.5 / P2


01 Jan 07

1.5.2 CARGO DOOR B777-200ER has 02 holds for loading ULD and 01 for bulk loading. Forward cargo hold is devided into compartment 1 and compartment 2 which can load both container and pallet. AFT cargo hold is devided into compartment 3 and compartment 4. Both container and pallet can be loaded at the AFT hold for the aircraft VNA141/2/7/9/50/51 because of large door. Aircraft VNA143/4/5/6 can only load container at the AFT hold because of narrow door.

BOEING 777 1.5 / P3


01 Jan 07

1.5.2.1 CARGO DOOR OPERATION WARNING:

− Do not operate the door in winds more than 40 knots. − Do not let the door stay open in winds more than 65 knots. Injuries to persons or

damage to equipment can occur. − Do not open the door when the aircraft is pressurized. Injuries to persons or damage

to equipment can occur. CAUTION: Do not operate the door electrically more than 2 full open/close cycles within 5 minutes. Damage to the lift mechanism can occur. 1.5.2.1.1 Open the cargo door

− Open cargo door actuation panel WARNING: Stay away from the path of the lock handle. The lock handle is spring-

loaded to open when you pull the catch release lever and injuries to persons or damage to equipment can occur.

− Push the lock handle access cover in and pull the catch release lever out. − Make sure the lock handle is fully OPEN and UNLOCKED shows on each side of

the handle. − Make sure the vent door is OPEN. − Make sure the green DOOR LATCHED light on the control panel is ON. − Make sure all persons and equipment are clear of the door. − Unlatch and open the door as follows:

(1) Hold the external CARGO DOOR CONTROL switch in the OPEN position. (2) Release the switch when the door is fully open and the yellow DOOR UP light comes on.

− Close cargo door actuation panel. 1.5.2.1.2 Close the cargo door

− Open cargo door actuation panel. CAUTION: Make sure the access panels are closed on the sides of the door cutout before you close the cargo door. The cargo door can cause damage to open access panels when it closes.

− Make sure the access panels doors are closed on the sides of the door cutout. − Make sure all persons and equipment are clear of the door. − Hold the external CARGO DOOR CONTROL switch in the CLOSE position. − Make sure the yellow DOOR UP light goes off. − Release the switch when the door is fully closed and the green DOOR LATCHED

light comes on. − Make sure the vent door is open. − Push the lock handle up and inboard to close the lock handle. − Make sure the lock handle and catch release lever are flush with the door skin − Make sure the vent door is closed.

BOEING 777 1.5 / P4


01 Jan 07

Forward cargo door

BOEING 777 1.5 / P5


01 Jan 07

AFT cargo door (Large cargo door)

BOEING 777 1.5 / P6


01 Jan 07

AFT cargo door (Small cargo door)

BOEING 777 1.5 / P7


01 Jan 07

Bulk cargo door

BOEING 777 1.5 / P8


01 Jan 07

1.5.3 SYSTEMS REQUIREMENTS FOR GROUND SERVICE EQUIPMENT 1.5.3.1 Aircraft doors – sill heights and dimensions.

Sill Height Door

Distance from A/C Nose

Door Size Minimum Maximum

Number Metres Inches Metres Inches Metres Inches Metres Inches A 6.74 266 1.07x1.88 42x74 4.71 185 5.00 197 B 11.07 672 1.07x1.88 42x74 4.88 192 5.07 200 C 36.32 1,430 1.07x1.88 42x74 5.16 203 5.30 209 D 49.53 1,950 1.07x1.88 42x74 5.28 208 5.53 218 E 11.80 465 2.69x1.70 106x67 2.81 111 3.05 120

F(s) 41.25 1,624 1.78x1.70 70x67 3.23 127 3.40 134 F(I)* 41.77 1,645 1.70x2.69 67x106 3.23 127 3.41 134

G 46.32 1,824 0.91x1.14 36x45 3.39 133 3.61 142

* F(I) = Large Cargo Door optional

1.5.3.2 Requirement for GSE. System Requirements Notes

Electrical Type Power Requirement

115/200V AC 90 kVA

180 kVA Recommened

Air Conditioning

Maximum Flow Rate Maximum Output Pressure Cooling Capacity Heating Capacity

1,55 ppm 42 psi

100 ton/hr 992,000 Btu/hr

kg/min kg/cm2

kcal/sec

Pneumatic Minimum Capacity Maximum Pressure Minimum Pressure

300 ppm 50 psi 24 psi

kg/cm2

kg/cm2

Potable Water Total Capacity Maximum Pressure Recommended Flow Rate

218 U.S gal 55 psi

BOEING 777 1.5 / P9


01 Jan 07

Lavatory Total Waste Capacity Total Rinse Capacity Total Precharge Maximum Delivery Pressure Recommended Flow Rate

189 U.S gal 60 U.S gal 18 U.S gal

125 psi 10 gpm

L L L

kg/cm2

38 L/min

3 Tanks (6 gal each) 80 psig (flushing) Nominal

The arc of opening/closing cargo compartment doors is lower than the operating sill height. - Small door: 23.41 inch - Lager door: 25.9 inch

1.5.3.3 Ground servicing points location.

Distance Height from Ground Aft of Nose From A/C

System Metres Inches Metres Inches

Metres

Inches

Notes 1. Air conditioning 24.40 961 1.06LR 42LR 2.40 94 2. Electrical 7.07 278 1.14R 45R 2.74 108 3. Fule 28.33 1,115 12.16

L(R) 479 L(R)

5.22 206 RH Optional

4. Potable Water - AFT

44.90 1,768 1.04L 41L 3.03 119

*. Potable Water-FWD 8.75 344 1.25R 49R 2.67 105 * Optional 5. Lavatory 47.05 1,853 0.30L 12L 3.09 122 6. Pneumatic 24.35 959 1.72L 68L 2.37 94

BOEING 777 1.5 / P10


01 Jan 07

1.5.3.4 Aircraft servicing arrangement. (Not mandatory)

BOEING 777 1.6 / P1

AIRCRAFT HANDLING MANUAL CARGO LOADING SYSTEM Rev 06

01 Jan 07

1.6 CARGO LOADING SYSTEM 1.6.1 CARGO HANDLING CONTROL SYSTEM Cargo handling control system operate the loading system by power. It is located inside and outside the FWD/AFT cargo holds near the door.

BOEING 777 1.6 / P2


01 Jan 07

CARGO HANDLING CONTROL SYSTEM

− VNA141/142/147/149 has the large AFT cargo door − Aircraft which has the small AFT cargo door does not have PALLET/CONTAINER

SWITCH in the panel

BOEING 777 1.6 / P3


01 Jan 07

1.6.2 RESTRAINT SYSTEM

BOEING 777 1.6 / P4


01 Jan 07

1.6.2.1 MECHANICAL COMPONENT - MANUAL OPERATION 1.6.2.1.1 GENERAL (1)These are the mechanical components that are manually operated during loading and offloading of pallets and containers:

(a) Partial Load Stops (b) Pallet Locks (c) Center Stop Locks (d) Rollout Stops/Locks (e) Retractable Guide Roller/Lock (f) Stop/Locks (g) Center Guides (h) Lateral Guide vertical restraints

(2) The partial load stops give longitudinal restraint for containers when other containers are not adjacent to it. (3) The pallet locks and locks/stops give vertical and longitudinal restraint for pallets. (4) The center guides in and adjacent to the ball panel area lock down to load and unload pallets. (5) The vertical restraints on the lateral guides turn to lock down pallets

BOEING 777 1.6 / P5


01 Jan 07

1.6.2.1.2 PARTIAL LOAD STOP (a) Lift the stop head up until the pawl locks the stop head in the stop position. (b) Hold the stop head while you pull up on the pawl to put the partial load stop in the down position. NOTE: The stop head will go down automatically when you lift the fork.

BOEING 777 1.6 / P6


01 Jan 07

1.6.2.1.3 SINGLE PALLET LOCKS (a) Lift the vertical restraint until the link locks the single pallet lock in the LOCK position. Make sure that the link is at the end of the slot. (b) Push the lower part of the link to the vertical position to put the single pallet lock in the DOWN position. NOTE: The vertical restraint will go down automatically when you push the lower part of the link to it.

BOEING 777 1.6 / P7


01 Jan 07

1.6.2.1.4 DOUBLE PALLET LOCKS NOTE: The pallet locks are combinations of the single pallet lock and the double pallet lock. For operation of a single pallet lock, see the steps above. (a) Lift the vertical restraints until the pawl locks the double pallet lock in the LOCK position. (b) Hold the vertical restraints up while you pull the top part of the pawl down to put the double pallet lock in the DOWN position. NOTE: The vertical restraints will go down automatically when you pull the top part of the pawl away from them.

BOEING 777 1.6 / P8


01 Jan 07

1.6.2.1.5 CENTER STOP/ LOCKS (a) Hold the vertical restraint while pulling on the top end of the pawl until the vertical restraint retracts. (b) Lift the vertical restraint until it locks in the vertical position.

BOEING 777 1.6 / P9


01 Jan 07

1.6.2.1.6 ROLLOUT STOP/ LOCKS NOTE: The stop/locks are combinations of the partial load stop and pallet lock. (a) Lift the vertical restraint or stop head until the pawl or the link locks them in the UP position. (b) Do the same steps for the partial load stop and pallet lock to to put the stop/lock in the DOWN position.

BOEING 777 1.6 / P10


01 Jan 07

1.6.2.1.7 RETRACTABLE GUIDE ROLLER/ LOCK (a) Push the manual release pedal down to lower the vertical restraint. (b) Pull the vertical restraint up until it locks in the vertical position.

BOEING 777 1.6 / P11


01 Jan 07

1.6.2.1.8 CENTER GUIDES (a) Push and hold the vertical restraint of the center guide all the way down in the forward or aft direction. (b) Push the pedal down to release the center guide to the vertical position.

BOEING 777 1.6 / P12


01 Jan 07

1.6.2.1.9 LARGE LATERAL GUIDES

BOEING 777 1.6 / P13


01 Jan 07

1.6.2.1.10 AUXILIARY GUIDES

BOEING 777 1.6 / P14


01 Jan 07

1.6.2.1.11 AUXILIARY STOP/ LOCKS

BOEING 777 1.6 / P15


01 Jan 07

1.6.2.2 ELECTRICAL COMPONENT MANUAL OPERATION

BOEING 777 1.6 / P16


01 Jan 07

BOEING 777 1.7 / P1

AIRCRAFT HANDLING MANUAL FORM Rev 06

01 Jan 07

1.7 FORM 1.7.1 LOADSHEET

BOEING 777 1.7 / P2


01 Jan 07

1.7.2 BALANCE CHART FOR AIRCRAFT VNA141/142/149/150

BOEING 777 1.7 / P3


01 Jan 07

1.7.3 BALANCE CHART FOR AIRCRAFT VNA143/144/145/146

BOEING 777 1.7 / P4


01 Jan 07

1.7.4 BALANCE CHART FOR AIRCRAFT VNA147

BOEING 777 1.7 / P5


01 Jan 07

1.7.5 BALANCE CHART FOR AIRCRAFT VNA151

BOEING 777 1.7 / P6


01 Jan 07

1.7.6 LOADING INSTRUCTION REPORT VNA141/142/149/150/151

BOEING 777 1.7 / P7


01 Jan 07

1.7.7 LOADING INSTRUCTION REPORT VNA143/144/145/146

BOEING 777 1.7 / P8


01 Jan 07

1.7.8 LOADING INSTRUCTION REPORT VNA147

CHƯƠNG 2 MÁY BAY AIRBUS A330

CHAPTER 2

AIRCRAFT AIRBUS A330

AIRBUS A330 2.0 / P1

AIRCRAFT HANDLING MANUAL CONTENT Rev 06

01 Jan 07

CONTENT 2.1. General 2.1.1. List of aircraft 2.1.2. Exterior dimension 2.1.3. Ground clearance 2.1.4. Weight and balance definitions 2.2. Aircraft limitation & features 2.2.1. Certificate limitations 2.2.2. Standardized weight and index 2.2.3. Aircraft configuration 2.2.4. Standard taxi fuel 2.2.5. Standardized weight per passenger/ crew 2.2.6. Last minute change 2.3. Cargo hold limitation & version 2.3.1. Structural load limitation 2.3.2. Maximum load for ULD 2.3.3. Lower deck version 2.3.4. Carriage of special load 2.4. Maximum package & restrictions due to restraint deficiencies 2.4.1. Cargo hold and compartment arrangement 2.4.2. Maximum allowable weight due missing or inoperative restraints 2.5. Door operation 2.5.1. Cabin door 2.5.2. Cargo door 2.5.3. Systems requirements for ground service equipment 2.6. Cargo loading system 2.6.1. Cargo handling control system 2.6.2. Restraint system 2.7. Form 2.7.1. Loadsheet 2.7.2. Balance chart 2.7.3. Loading instruction report

2.1 /P1 2.1 /P2 2.1 /P3 2.1 /P4 2.2 /P1 2.2 /P2 2.2 /P3 2.2 /P4 2.2 /P4 2.2 /P5 2.3 /P1 2.3 /P3 2.3 /P4 2.3 /P31 2.4 /P1 2.4 /P5 2.5 /P1 2.5 /P2 2.5 /P6 2.6 /P1 2.6 /P2 2.7 /P1 2.7 /P2 2.7 /P5

AIRBUS 330 2.1 / P1


01 Jan 07

2.1 GENERAL 2.1.1 LIST OF AIRCRAFT This manual is effective for the following aircraft

Model Registration number Configuration

A330-300 VNA368 C36Y284

AIRBUS 330 2.1 / P2


01 Jan 07

2.1.2 EXTERIOR DIMENSION

AIRBUS 330 2.1 / P3


01 Jan 07

2.1.3 GROUND CLEARANCE

AIRBUS 330 2.1 / P4


01 Jan 07

2.1.4 WEIGHT AND BALANCE DEFINITIONS

1 BASIC WEIGHT : Aircraft weight including the furnishing,

fixed equipment 2 DRY OPERATING WEIGHT

(DOW) : Basic weight plus crew and pantry weight

and the other. Operational items (such as ballast fuel, stretcher..., if applied).

3 DEADLOAD : Gross weight of the cargo, mail, baggage and

empty ULDs. 4 OPERATING WEIGHT : Dry operating weight plus take off fuel. 5 PAYLOAD : Weight of the passengers, cargo, mail,

baggage and ULDs.(these may be revenue and/or nonrevenue)

6 ZERO FUEL WEIGHT (ZFW)

: Dry operating weight plus payload.

7 TAKE OFF WEIGHT

(TOW)

: Zero fuel weight plus take off fuel

8 DEADLOAD WEIGHT (DLW)

: Zero fuel weight minus the weight of passengers.

9 MAXIMUM TAKE OFF

WEIGHT (MTOW) : Maximum weight at brake release as limited

by aircraft (MTOW) strength and airworthiness requirements.

10 MAXIMUM LANDING

WEIGHT (MLDW)

: Maximum weight for landing as limited by aircraft (MLDW) strength and airworthiness requirements.

AIRBUS 330 2.1 / P5


01 Jan 07

11 MAXIMUM ZERO FUEL

WEIGHT (MZFW)

: Maximum weight allowed before usable fuel must be (MZFW) loaded in the aircraft as limited by strength and airworthiness requirement.

12 MAXIMUM TAXI WEIGHT

(MTW)

: Maximum weight for ground maneuver as limited by (MTW) aircraft strength and airworthiness requirements. (It includes weight of taxi fuel.)

13 C.G

: Center of gravity

14 BA

: Balance arms which are a true measure in inches from the reference datum.

15 %MAC (Percentage of Mean Aerodynamic Chord)

: The location of the aircraft C.G. relative to the leading edge of mean aerodynamic chord (MAC)

16 Index

: The parameter used to express the variation or location of C.G. which is the shortened moment of a certain I weight.

17 Basic index (BI)

: The C.G. Of aircraft basic weight expressed with index

18 Dry Operating Index (DOI)

: The C.G. Of aircraft dry operating weight expressed with index.

19 Laden Index Zero Fuel Weight (LIZFW)

: The C.G. Of aircraft zero fuel weight expressed with (LIZFW) index.

20 Laden Index take off weight (LITOW)

: The C.G. Of aircraft take off weight expressed with (LITOW) index.

21 Index of deadload weight (DLI)

: The C.G. Of aircraft dead load weight expressed with (DLI) index.

22 %MAC of Zero Fuel Weight (MACZFW)

: The C.G. Of aircraft zero fuel weight expressed with % MAC.

23 %MAC of take off weight (MACTOW)

: The C.G. Of aircraft take off weight expressed with % MAC.

24 %MAC of dead load weight (MACDLW)

: The C.G. Of aircraft dead load weight expressed with % MAC.

AIRBUS 330 2.1 / P6


01 Jan 07

25 Take off fuel

: The amount of fuel on board less the fuel consumed before the take off run.

26 Taxi fuel

: A standard quantity of fuel to cover engine starts and ground maneuvers until start of take off, APU consumption, the amount may be increased when required by local conditions.

27 Trip fuel

: Fuel required to fly from the airport of departure to the planned destination, based on "Planned Operating Conditions". This amount shall include fuel for take off, acceleration, climb, cruise, descent, approach and landing.

28 Ballast fuel

: The fuel in lieu of payload which is specifically loaded for longitudinal balance control.

29 Usable fuel

: Fuel available for aircraft propulsion.

30 Unusable fuel :

Fuel can not be used due to technical limitations and must be included in weight and balance concerns.

AIRBUS 330 2.2 / P1


01 Jan 07

2.2 AIRCRAFT LIMITATIONS & FEATURES 2.2.1 CERTIFICATE LIMITATIONS 2.2.1.1 AIRCRAFT GROSS WEIGHT LIMITATIONS

Item Maximum limitation

Max. Taxi weight

Max. Zero fuel weight

Max. Take off weight

Max. Landing weight

215900

167000

215000

177000

2.2.1.2 PERFORMANCE OPERATING WEIGHT To comply with the performance requirements of the aircraft manufacturer, the maximum allowable takeoff and landing weights may be less than structural limits. The maximum allowable weight for that flight that must not exceed the least of the following weights:

− Maximum allowable takeoff weight for the runway intended to be used (including corrections for altitude and gradient, and wind and temperature conditions existing at the takeoff time).

− Maximum takeoff weight considering anticipated fuel and oil consumption that

allows compliance with applicable enroute performance limitations. − Maximum take off weight considering anticipated fuel and oil consumption that

allows compliance with landing distance limitations or arrival at the destination and alternate airports.

AIRBUS 330 2.2 / P2


01 Jan 07

2.2.2 STANDARDIZED WEIGHT AND INDEX

Please refer to AHM050 validated by Flight Operation Department.

AIRBUS 330 2.2 / P3


01 Jan 07

2.2.3 AIRCRAFT CONFIGURATION

Aircraft REG Pax Configuration ROW Cabin zone

No of pax

VNA368 36C284Y

1-6

14-33

34-51

0A

0B

0C

36

152

132

AIRBUS 330 2.2 / P4


01 Jan 07

2.2.4 STANDARD TAXI FUEL

Standard taxi fuel for A330 is : 300 KG 2.2.5 STANDARDIZED WEIGHT PER PASSENGER/CREW

Specification Standard weight (KG)

Chartter flight Definition of age

Adult 75 76 Above 12 years

Child 35 35 Under 12 years but above 2 years Passenger

Infant 00 00 Under 2 years

Cockpit crew 90 Crew

Cabin crew 75

NOTES:

− All standard weights listed above are typical average weight including carry-on baggage. Check-in baggage must be weighed and included in the weight and balance calculation.

− One piece of hand baggage suitable for placing in the closed overhead rack or under

the passenger's seat may be carried on board the aircraft; provided that such maximum dimensions (the sum of the three outside dimensions) must not exceed 23cm x 36cm x 56cm and the weight of the bag must not exceed 7 KG. (Please refer to the decision 854/TCT-DVTT)

− For loading non-standard weight groups, such as athletic or military squads and their

baggage, the actual weights for both passengers and baggage must be utilized.

− The number of passengers whose weights are outside the typical range must be indicated in the Supplementary Information (SI) column of the loadsheet by the load controller responsible for the weight and balance control of this flight.

AIRBUS 330 2.2 / P5


01 Jan 07

2.2.6 LAST MINUTE CHANGE

The LMC tolerance is: +/- 1000 kg. If exceeded, a new loadsheet is required. The following must be checked : a. Traffic load only: - The LMC positive total weight is lower than the underload before LMC. - No loading limitation exceeded. - The balance at MACZFW and MACTOW remains within the allowed limits. - All the LMC data on the loadsheet is completed.

b. Useable fuel only : - Issue the new loadsheet when change in fuel figures

AIRBUS 330 2.3 / P1

AIRCRAFT HANDLING MANUAL CARGO HOLD LIMITATIONS & VERSIONS Rev 06

01 Jan 07

2.3 CARGO HOLD LIMITATIONS & VERSIONS 2.3.1 STRUCTURAL LOAD LIMITATION 2.3.1.1 MAXIMUM LOAD FOR CARGO HOLD

COMP. VNA368 COMBINED LOAD Floor loading limit

1 9522 kgs 488 kg/sqm

2 19044 kgs

22861 488 kg/sqm

3 13878 kgs 488 kg/sqm

4 9522 kgs

18507 488 kg/sqm

5 3468 kgs 3468 732 kg/sqm

2.3.1.2 MAXIMUM GROSS WEIGHT FOR POSITIONS 2.3.1.2.1 FOR CONTAINERS

POSITION ALL POSITIONS

AKE 1587 MAX WEIGHT (KG)

DQF (AFT hold only) 2449

AIRBUS 330 2.3 / P2


01 Jan 07

2.3.1.2.2 FOR PALLETS

AIRBUS 330 2.3 / P3


01 Jan 07

2.3.2 MAXIMUM LOAD FOR ULD

Type Base Dimension (In)

W X L X H

Volume

(Cu ft) Tare Weight (Kg)

Maximum Gross Weight

(Kg)

AVE/ AKE 60.4” X 61.5” X 64.0” 159 110 1587

DQF 60.4” X 96.0” X 64.0” 252 156 2450

PAG 88” X 125” 381 115 6000

PAJ 88” X 125” 381 110 6000

P1P 88” X 125” 381 105 6000

P6P/ PMC 96” X 125” 407 120 6696 NOTES:

− Comparing with the ULD load limitation and the aircraft structure load limitation where the ULD will be located, choose the lower one as the actual allowable load for the designated ULD position.

− The ULD contents must be loaded in such a manner that they are sufficiently

secured to prevent them from damaging airplane structure as a result of shifting.

− The maximum load includes the tare weight of the ULD and is based on all required restraints being engaged.

AIRBUS 330 2.3 / P4


01 Jan 07

2.3.3 LOWER DECK VERSION 2.3.3.1 FORWARD HOLD 2.3.3.1.1 VERSION TABLE

LDV No.

No of PLT


F000 0P 18A 11LR 12LR 13LR 21LR 22LR 23LR 24LR 25LR 26LR

F101 1P 14A 11P 13LR 21LR 22LR 23LR 24LR 25LR 26LR

F102 1P 14A 11LR 12P 21LR 22LR 23LR 24LR 25LR 26LR

F103 1P 14A 11LR 12LR 13LR 21P 23LR 24LR 25LR 26LR

F104 1P 14A 11LR 12LR 13LR 21LR 22P 24LR 25LR 26LR

F105 1P 14A 11LR 12LR 13LR 21LR 22LR 23LR 23P 26LR

F106 1P 14A 11LR 12LR 13LR 21LR 22LR 23LR 24LR 24P

F201 2P 12A 11P 12P 21LR 22LR 23LR 24LR 25LR 26LR

F202 2P 12A 11LR 12LR 13LR 21P 22P 24LR 25LR 26LR

F203 2P 12A 11LR 12LR 13LR 21LR 22LR 23LR 23P 24P

F204 2P 10A 11P 13LR 21P 23LR 24LR 25LR 26LR

F205 2P 10A 11P 13LR 21LR 22P 24LR 25LR 26LR

F206 2P 10A 11P 13LR 21LR 22LR 23LR 23P 26LR

F207 2P 10A 11P 13LR 21LR 22LR 23LR 24LR 24P

F208 2P 10A 11LR 12P 21P 23LR 24LR 25LR 26LR

F209 2P 10A 11LR 12P 21LR 22P 24LR 25LR 26LR

F210 2P 10A 11LR 12P 21LR 22LR 23LR 23P 26LR

F211 2P 10A 11LR 12P 21LR 22LR 23LR 24LR 24P

AIRBUS 330 2.3 / P5


01 Jan 07

F212 2P 10A 11LR 12LR 13LR 21P 23LR 23P 26LR

F213 2P 10A 11LR 12LR 13LR 21P 23LR 24LR 24P

F214 2P 10A 11LR 12LR 13LR 21LR 22P 23P 26LR

F215 2P 10A 11LR 12LR 13LR 21LR 22P 24LR 24P

F301 3P 8A 11P 12P 21P 23LR 24LR 25LR 26LR

F302 3P 8A 11P 12P 21LR 22P 24LR 25LR 26LR

F303 3P 8A 11P 12P 21LR 22LR 23LR 23P 26LR

F304 3P 8A 11P 12P 21LR 22LR 23LR 24LR 24P

F305 3P 8A 11P 13LR 21P 22P 24LR 25LR 26LR

F306 3P 8A 11LR 12P 21P 22P 24LR 25LR 26LR

F307 3P 8A 11P 13LR 21LR 22LR 23LR 23P 24P

F308 3P 8A 11LR 12P 21LR 22LR 23LR 23P 24P

F309 3P 6A 11LR 12P 21P 23LR 23P 26LR

F310 3P 6A 11P 13LR 21P 23LR 23P 26LR

F311 3P 6A 11LR 12P 21LR 22P 24LR 24P

F312 3P 6A 11P 13LR 21LR 22P 24LR 24P

F401 4P 6A 11P 12P 21P 22P 24LR 25LR 26LR

F402 4P 6A 11P 12P 21LR 22LR 23LR 23P 24P

F403 4P 6A 11LR 12LR 13LR 21P 22P 23P 24P

F404 4P 4A 11P 12P 21P 23LR 23P 26LR

F405 4P 4A 11P 12P 21LR 22P 24LR 24P

F406 4P 4A 11P 13LR 21P 23LR 23P 24P

F407 4P 4A 11LR 12P 21P 23LR 23P 24P

F408 4P 4A 11P 13LR 21P 22P 24LR 24P

AIRBUS 330 2.3 / P6


01 Jan 07

F409 4P 4A 11LR 12P 21P 22P 24LR 24P

F410 4P 4A 11P 13LR 21P 22P 23P 26LR

F411 4P 4A 11LR 12P 21P 22P 23P 26LR

F501 5P 2A 11P 12P 21P 22P 23P 26LR

F502 5P 2A 11P 12P 21P 22P 24LR 24P

F503 5P 2A 11P 12P 21P 23LR 23P 24P

F504 5P 2A 11P 12P 21LR 22P 23P 24P

F505 5P 2A 11P 13LR 21P 22P 23P 24P

F506 5P 2A 11LR 12P 21P 22P 23P 24P

F600 6P 0A 11P 12P 21P 22P 23P 24P

NOTES

− Load full-size containers (DQF, ALF) into lower deck cargo compartments with their doors facing toward the compartment doorway. In case the full-size container is deadly stuck in the compartment, the cargo or baggage loaded inside the container may be removed without breaking the container.

AIRBUS 330 2.3 / P7


01 Jan 07

2.3.3.1.2 SAMPLES F000: 0 PALLET 18 CONTAINERS 26L 25L 24L 23L 22L 21L 13L 12L 11L

26R 25R 24R 23R 22R 21R 13R 12R 11R


26R 25R 24R 23R 22R 21R 13R

11P

PMC/ PAG


26R 25R 24R 23R 22R 21R

12P

PMC/ PAG 11R

FWD

F103: 1 PALLET 14 CONTAINERS 26L 25L 24L 23L 13L 12L 11L

26R 25R 24R 23R

21P

PMC/ PAG 13R 12R 11R

FWD

AIRBUS 330 2.3 / P8


01 Jan 07


26R 25R 24R

22P

PMC/ PAG 21R 13R 12R 11R

FWD


26R

23P

PMC/ PAG 23R 22R 21R 13R 12R 11R

FWD

F106: 1 PALLET 14 CONTAINERS

24L 23L 22L 21L 13L 12L 11L 24P

PMC/ PAG 24R 23R 22R 21R 13R 12R 11R

FWD F201: 2 PALLETS 12 CONTAINERS 26L 25L 24L 23L 22L 21L

26R 25R 24R 23R 22R 21R

12P

PMC/ PAG

11P

PMC/ PAG

FWD

AIRBUS 330 2.3 / P9


01 Jan 07

F202: 2 PALLETS 12 CONTAINERS 26L 25L 24L 13L 12L 11L

26R 25R 24R

22P

PMC/ PAG

21P



23L 22L 21L 13L 12L 11L 24P

PMC/ PAG

23P

PMC/ PAG 23R 22R 21R 13R 12R 11R

FWD


26R 25R 24R 23R

21P

PMC/ PAG 13R

11P

PMC/ PAG

FWD


26R 25R 24R

22P

PMC/ PAG 21R 13R

11P

PMC/ PAG

FWD

AIRBUS 330 2.3 / P10


01 Jan 07


26R

23P


11P

PMC/ PAG

FWD


24L 23L 22L 21L 13L 24P

PMC/ PAG 24R 23R 22R 21R 13R

11P

PMC/ PAG

FWD


26R 25R 24R 23R

21P

PMC/ PAG

12P

PMC/ PAG 11R

FWD F209: 2 PALLETS 10 CONTAINERS 26L 25L 24L 21L 11L

26R 25R 24R

22P

PMC/ PAG 21R

12P

PMC/ PAG 11R

FWD

AIRBUS 330 2.3 / P11


01 Jan 07


26R

23P


12P

PMC/ PAG 11R


24L 23L 22L 21L 11L 24P


12P

PMC/ PAG 11R

FWD F212: 2 PALLETS 10 CONTAINERS 26L 23L 13L 12L 11L

26R

23P

PMC/ PAG 23R

21P



24L 23L 13L 12L 11L 24P

PMC/ PAG 24R 23R

21P


FWD

AIRBUS 330 2.3 / P12


01 Jan 07


26R

23P

PMC/ PAG

22P



24L 21L 13L 12L 11L 24P

PMC/ PAG 24R

22P


FWD F301: 3 PALLETS 8 CONTAINERS 26L 25L 24L 23L

26R 25R 24R 23R

21P

PMC/ PAG

12P

PMC/ PAG

11P

PMC/ PAG


26R 25R 24R

22P

PMC/ PAG 21R

12P

PMC/ PAG

11P

PMC/ PAG

FWD

AIRBUS 330 2.3 / P13


01 Jan 07

F303: 3 PALLETS 8 CONTAINERS 26L 23L 22L 21L

26R

23P


12P

PMC/ PAG

11P

PMC/ PAG


24L 23L 22L 21L 24P


12P

PMC/ PAG

11P

PMC/ PAG


26R 25R 24R

22P

PMC/ PAG

21P

PMC/ PAG 13R

11P

PMC/ PAG


26R 25R 24R

22P

PMC/ PAG

21P

PMC/ PAG

12P

PMC/ PAG 11R

FWD

AIRBUS 330 2.3 / P14


01 Jan 07


23L 22L 21L 13L 24P

PMC/ PAG

23P


11P

PMC/ PAG


23L 22L 21L 11L 24P

PMC/ PAG

23P


12P

PMC/ PAG 11R

FWD F309: 3 PALLETS 6 CONTAINERS 26L 23L 11L

26R

23P

PMC/ PAG 23R

21P

PMC or PAG

12P

PMC/ PAG 11R


26R

23P

PMC/ PAG 23R

21P

PMC/ PAG 13R

11P

PMC/ PAG

FWD

AIRBUS 330 2.3 / P15


01 Jan 07


24L 21L 11L 24P

PMC/ PAG 24L

22P

PMC/ PAG 21R

12P

PMC/ PAG 11R

FWD


24L 21L 13L 24P

PMC/ PAG 24R

22P

PMC/ PAG 21R 13R

11P

PMC/ PAG


26R 25R 24R

22P

PMC/ PAG

21P

PMC/ PAG

12P

PMC/ PAG

11P

PMC/ PAG


23L 22L 21L 24P

PMC/ PAG

23P


12P

PMC/ PAG

11P

PMC/ PAG

FWD

AIRBUS 330 2.3 / P16


01 Jan 07


13L 12L 11L 24P

PMC/ PAG

23P

PMC/ PAG

22P

PMC/ PAG

21P


FWD F404: 4 PALLETS 4 CONTAINERS 26L 23L

26R

23P

PMC/ PAG 23R

21P

PMC/ PAG

12P

PMC/ PAG

11P

PMC/ PAG


24L 21L 24P

PMC/ PAG 24R

22P

PMC/ PAG 21R

12P

PMC/ PAG

11P

PMC/ PAG


23L 13L 24P

PMC/ PAG

23P

PMC/ PAG 23R

21P

PMC/ PAG 13R

11P

PMC/ PAG

FWD

AIRBUS 330 2.3 / P17


01 Jan 07


23L 11L 24P

PMC/ PAG

23P

PMC/ PAG 23R

21P

PMC/ PAG

12P

PMC/ PAG 11R


24L 13L 24P

PMC/ PAG 24R

22P

PMC/ PAG

21P

PMC/ PAG 13R

11P

PMC/ PAG


24L 11L 24P

PMC/ PAG 24R

22P

PMC/ PAG

21P

PMC/ PAG

12P

PMC/ PAG 11R

FWD F410: 4 PALLETS 4 CONTAINERS 26L 13L

26R

23P

PMC/ PAG

22P

PMC/ PAG

21P

PMC/ PAG 13R

11P

PMC/ PAG

FWD

AIRBUS 330 2.3 / P18


01 Jan 07

F411: 4 PALLETS 4 CONTAINERS 26L 11L

26R

23P

PMC/ PAG

22P

PMC/ PAG

21P

PMC/ PAG

12P

PMC/ PAG 11R

FWD F501: 5 PALLETS 2 CONTAINERS 26L

26R

23P

PMC/ PAG

22P

PMC/ PAG

21P

PMC/ PAG

12P

PMC/ PAG

11P

PMC/ PAG

FWD


24L 24P

PMC/ PAG 24R

22P

PMC/ PAG

21P

PMC/ PAG

12P

PMC/ PAG

11P

PMC/ PAG


23L 24P

PMC/ PAG

23P

PMC/ PAG 23R

21P

PMC/ PAG

12P

PMC/ PAG

11P

PMC/ PAG

FWD

AIRBUS 330 2.3 / P19


01 Jan 07


21L 24P

PMC/ PAG

23P

PMC/ PAG

22P

PMC/ PAG 21R

12P

PMC/ PAG

11P

PMC/ PAG


13L 24P

PMC/ PAG

23P

PMC/ PAG

22P

PMC/ PAG

21P

PMC/ PAG 13R

11P

PMC/ PAG


11L 24P

PMC/ PAG

23P

PMC/ PAG

22P

PMC/ PAG

21P

PMC/ PAG

12P

PMC/ PAG 11R

FWD F600: 6 PALLETS 0 CONTAINER 24P PMC/ PAG

23P PMC/ PAG

22P PMC/ PAG

21P PMC/ PAG

12P PMC/ PAG

11P PMC/ PAG

FWD

AIRBUS 330 2.3 / P20


01 Jan 07

2.3.3.2 AFT HOLD

AFT can load : 14 LD3

or 05 LD4/LD8 or 10 LD2 or 05 Size code A or 05 Size code A or 4 Size code M or 04 Size code M

2.3.3.2.1 LOAD VERSION OF VNA368

LDV No.

No of PLT



A101 1P 12A 31P 32LR 33LR 34LR 41LR 42LR 43LR

A102 1P 10A 31LR 32P 34LR 41LR 42LR 43LR

A103 1P 10A 31LR 32LR 33P 41LR 42LR 43LR

A104 1P 10A 31LR 32LR 33LR 34LR 41P 43LR

A105 1P 10A 31LR 32LR 33LR 34LR 41LR 42P

A201 2P 8A 31P 32P 34LR 41LR 42LR 43LR

A202 2P 8A 31P 32LR 33P 41LR 42LR 43LR

A203 2P 8A 31LR 32P 33P 41LR 42LR 43LR

A204 2P 8A 31P 32LR 33LR 34LR 41P 43LR

A205 2P 8A 31P 32LR 33LR 34LR 41LR 42P

A206 2P 8A 31LR 32LR 33LR 34LR 41P 42P

A207 2P 6A 31LR 32P 34LR 41P 43LR

A208 2P 6A 31LR 32P 34LR 41LR 42P

A209 2P 6A 31LR 32LR 33P 41P 43LR

A210 2P 6A 31LR 32LR 33P 41LR 42P

A301 3P 6A 31P 32P 33P 41LR 42LR 43LR

AIRBUS 330 2.3 / P21


01 Jan 07

A302 3P 6A 31P 32LR 33LR 34LR 41P 42P

A303 3P 4A 31P 32P 34LR 41P 43LR

A304 3P 4A 31P 32P 34LR 41LR 42P

A305 3P 4A 31LR 32P 33P 41P 43LR

A306 3P 4A 31LR 32P 33P 41LR 42P

A307 3P 4A 31P 32LR 33P 41P 43LR

A308 3P 4A 31P 32LR 33P 41LR 42P

A309 3P 4A 31LR 32P 34LR 41P 42P

A310 3P 4A 31LR 32LR 33P 41P 42P

A401 4P 2A 31P 32P 33P 41P 43LR

A402 4P 2A 31P 32P 33P 41LR 42P

A403 4P 2A 31P 32P 34LR 41P 42P

A404 4P 2A 31P 32LR 33P 41P 42P

A405 4P 2A 31LR 32P 33P 41P 42P

A406 4P 0A 31P 32P 41P 42P

A501 5P 0A 31P 32P 33P 41P 42P

AIRBUS 330 2.3 / P22


01 Jan 07

2.3.3.2.2 SAMPLE VERSION OF AIRCRAFT VNA368 A000: 0 PALLET 14 CONTAINERS 43L 42L 41L 34L 33L 32L 31L

43R 42R 41R 34R 33R 32R 31R

FWD A101: 1 PALLET 12 CONTAINERS 43L 42L 41L 34L 33L 32L

43R 42R 41R 34R 33R 32R

31P

PMC/PAG


43R 42R 41R 34R

32P

PMC/PAG 31R


43R 42R 41R

33P

PMC/PAG 32R 31R

FWD

AIRBUS 330 2.3 / P23


01 Jan 07

A104: 1 PALLET 10 CONTAINERS 43L 34L 33L 32L 31L

43R

41P

PAG 34R 33R 32R 31R


41L 34L 33L 32L 31L 42P

PMC/PAG 41R 34R 33R 32R 31R

FWD A201: 2 PALLETS 8 CONTAINERS 43L 42L 41L 34L

43R 42R 41R 34R

32P

PMC/PAG

31P

PMC/PAG


43R 42R 41R

33P

PMC/PAG 32R

31P

PMC/PAG

FWD

AIRBUS 330 2.3 / P24


01 Jan 07

A203: 2 PALLETS 8 CONTAINERS 43L 42L 41L 31L

43R 42R 41R

33P

32P

31R 32P and 33P: must be 2PAG or 1PAG + 1PMC


43R

41P

PAG 34R 33R 32R

31P

PMC/PAG


41L 34L 33L 32L 42P

PMC/PAG 41R 34R 33R 32R

31P

PMC/PAG

FWD


34L 33L 32L 31L 42P

PMC/PAG

41P

PAG 34R 33R 32R 31R

FWD

AIRBUS 330 2.3 / P25


01 Jan 07

A207: 2 PALLETS 6 CONTAINERS 43L 34L 31L

43R

41P

PAG 34R

32P

PMC/PAG 31R


41L 34L 31L 42P

PMC/PAG 41R 34R

32P

PMC/PAG 31R

FWD A209: 2 PALLETS 6 CONTAINERS 43L 32L 31L

43R

41P

33P

32R 31R 41P and 33P: must be 2PAG or 1PAG + 1PMC


41L 32L 31L 42P

PMC/PAG 41R

33P

PMC/PAG 32R 31R

FWD

AIRBUS 330 2.3 / P26


01 Jan 07

A301: 3 PALLETS 6 CONTAINERS 43L 42L 41L

43R 42R 41R

33P

32P 31P

31P, 32P and 33P: must be 1PAG + 2PMC or 2PAG + 1PMC or 3PAG


34L 33L 32L 42P

PMC/PAG

41P

PAG 34R 33R

31P

PMC/PAG 32R

FWD A303: 3 PALLETS 4 CONTAINERS 43L 34L

43R

41P

PAG 34R

32P

PAG/PMC

31P

PMC/PAG


41L 34L 42P

PAG/PMC 41R 34R

32P

PAG/PMC

31P

PAG/PMC

FWD

AIRBUS 330 2.3 / P27


01 Jan 07

A305: 3 PALLETS 4 CONTAINERS 43L 31L

43R

41P

33P 32P

31R 32P, 33P and 41P: must be 1PAG + 2PMC (PAG must be loaded at 33P or 41P) or 2PAG + 1PMC or 3PAG


41L 31L 42P

PMC/PAG 41R

33P

PMC/PAG

32P

PMC/PAG 31R

FWD A307: 3 PALLETS 4 CONTAINERS 43L 32L

43R

41P 33P 31P

PMC/PAG 32R 41P and 33P: must be 2PAG or 1PAG + 1PMC


41L 32L 42P

PMC/PAG 41R

33P

PMC/PAG

31P

PMC/PAG 32R

FWD

AIRBUS 330 2.3 / P28


01 Jan 07


34L 31L 42P

PMC/PAG

41P

PAG

32P

PMC/PAG 34R 31R


32L 31L 42P

41P 33P

32R 31R 33P, 41P and 42P: must be 1PAG + 2PMC (PAG must be loaded

at 33P or 41P) or 2PAG + 1PMC or 3PAG

FWD A401: 4 PALLETS 2 CONTAINERS 43L

43R

41P 33P 32P 31P

31P, 32P, 33P and 41P: must be 2PAG + 2PMC (2PAG must NOT be loaded at 31P and 32P at the same time) or 3PAG + 1PMC or 4PAG


41L 42P

PMC/PAG

33P

32P 31P

41R 31P, 32P and 33P: must be 1PAG + 2PMC or 2PAG + 1PMC or 3PAG

FWD

AIRBUS 330 2.3 / P29


01 Jan 07


34L 42P

PMC/PAG

41P

PAG

32P

PMC/PAG

31P

PMC/PAG 34R


32L 42P 41P 33P 31P

PMC/PAG 32R 33P, 41P and 42P: must be 1PAG + 2PMC (PAG must be loaded at 33P or 41P) or 2PAG + 1PMC or 3PAG


31L 42P 41P 33P 32P

31R 32P, 33P, 41P and 42P: must be 1PAG + 3PMC (PAG must NOT be loaded at 32P or 42P) or 2PAG + 2PMC or 3PAG + 1PMC or 4PAG

FWD A406: 4 PALLETS 0 CONTAINERS 42P

PMC/PAG

41P 32P

PMC/PAG

31P

PMC/PAG PMC/PAG

FWD

AIRBUS 330 2.3 / P30


01 Jan 07

A501: 5 PALLETS 0 CONTAINERS 42P

41P

33P 32P 31P

31P, 32P, 33P, 41P and 42P: must be 2PAG + 3PMC (2PAG must be loaded at 32P, 33P, 41P

or 31P, 41P OR 31P, 33P) or 3PAG + 2PMC or 4PAG + 1PMC or 5PAG

FWD

AIRBUS 330 2.3 / P31


01 Jan 07

2.3.4 CARRIAGE OF SPECIAL LOAD 2.3.4.1 Magnetized Materials (MAG) Loading

− In order to avoid the significant effect on the aircraft navigation system, Packages of magnetized materials must be loaded not to exceed 2000 kg of magnets per aircraft.

− Packages of magnetized materials must not to be loaded in compartment 1, 2, and 4

2.3.4.2 Other special load 2.3.4.2.1 Dry Ice


(With live animal, AVI)


(Without live animal, AVI) Maximum weight/ aircraft

120 KG 200 KG 400 KG

2.3.4.2.2 Live animal

Ventilation system on aircraft

A/C Reg. Hold Ventilation Temperature control

FWD No No

AFT No No VNA368

BULK Yes 50C - 250C

AIRBUS 330 2.3 / P32


01 Jan 07

Live animal is loaded in compartment 5 only with these limitation:

Live animal (AVI) Quantity/ weight Position

Baby chicken (one day old) 2000 Compartment 5

Bird (Including baby chicken) 1,5 cubic meter Compartment 5

Dog, Cat 2,5 cubic meter Compartment 5

Monkey 100/ 350 KG Compartment 5

Reptile 2,5 cubic meter Compartment 5

Miscellaneous (Small AVI) 1,5 cubic meter Compartment 5

2.3.4.2.3 Radioactive material Radioactive material type A package has category II yellow or category III yellow can be stored in the ULD and loaded at the FWD or AFT hold. The minimum separation distance from the top of the package to nearest inside surface of the floor of the aircraft cabin must be determined in accordance with the below table:

Minimum distance Total sum of TI Meters Ft.in

0.1 - 1.0

1.1 - 2.0

2.1 - 3.0

3.1 - 4.0

4.1 - 5.0

5.1 - 6.0

6.1 - 7.0

7.1 - 8.0

8.1 - 9.0

9.1 - 10.0

0.30

0.50

0.70

0.85

1.00

1.15

1.30

1.45

1.55

1.65

1’00”

1’08”

2’04”

2’10”

3’04”

3’10”

4’04”

4’09”

5’01”

5’05”

If the package of radioactive material can not use the distance separation from above table, It can be devided into 2 or more packages. Each package must be separated to the other at least 3 times of the higher transport index distance

AIRBUS 330 2.3 / P33


01 Jan 07

Maximum Transport Index 7.0

Bulk load

6.0

ULD load

Minimum distance 130 cm 115 cm

2.3.4.2.4 Priority baggage Priority baggage (BC) and crew baggage (D) must be loaded at AFT hold door side (position 43)

AIRBUS 330 2.4 / P1



2.4 MAXIMUM PACKAGE & RESTRICTIONS DUE TO RESTRAINT

DEFICIENCIES 2.4.1 CARGO HOLD AND COMPARTMENT ARRANGEMENT 2.4.1.1 FORWARD HOLD 2.4.1.1.1 For Container

2.4.1.1.2 For Pallet

2.4.1.1.3 Allowable package sizes through FWD cargo door

For upright loading

AIRBUS 330 2.4 / P2



For Tilted loading

2.4.1.2 AFT HOLD 2.4.1.2.1 For container

2.4.1.2.2 For pallet

AIRBUS 330 2.4 / P3



2.4.1.2.3 Allowable package sizes through AFT cargo door (Applicable for VNA368

only)

For Upright loading

For Tilted loading

AIRBUS 330 2.4 / P4



2.4.1.2.4 Bulk

2.4.1.2.5 Allowable package sizes through bulk cargo door

For Upright loading

For Tilted loading

AIRBUS 330 2.4 / P5



2.4.2 MAXIMUM ALLOWABLE WEIGHT DUE MISSING OR INOPERATIVE

RESTRAINTS 2.4.2.1 FWD HOLD Key of latch types with restriction requirement

AIRBUS 330 2.4 / P6



2.4.2.1.1 60.4”x 61.5” (LD3) half size container and pallet latching in forward cargo hold

AIRBUS 330 2.4 / P7



Maximum allowable loads for missing or inoperative restrains :

AIRBUS 330 2.4 / P8



2.4.2.1.2 88/96”x 125” full size ULD latching in forward cargo hold

AIRBUS 330 2.4 / P9



Maximum allowable loads for missing or inoperative restrains

AIRBUS 330 2.4 / P10



2.4.2.1.3 60.4”x 125” full size ULD latching in forward cargo hold

AIRBUS 330 2.4 / P11




AIRBUS 330 2.4 / P12



2.4.2.2 AFT HOLD : Key of latch types with restriction requirement

AIRBUS 330 2.4 / P13



2.4.2.2.1 60.4”x 61.5” (LD3) half size container and pallet latching in AFT cargo hold

AIRBUS 330 2.4 / P14




AIRBUS 330 2.4 / P15



AIRBUS 330 2.4 / P16



2.4.2.2.2 88/96”x 125” full size ULD latching in AFT cargo hold

AIRBUS 330 2.4 / P17




AIRBUS 330 2.4 / P18



2.4.2.2.3 60.4”x 125” full size ULD latching in AFT cargo hold

AIRBUS 330 2.4 / P19




AIRBUS 330 2.4 / P20



2.4.2.2.4 60.4”x 47” (LD2) half size ULD latching in AFT cargo hold

AIRBUS 330 2.4 / P21




AIRBUS 330 2.4 / P22



2.4.2.2.5 60.4”x 96” (LD4/LD8) ful size ULD latching in AFT cargo hold

AIRBUS 330 2.4 / P23




AIRBUS 330 2.5 / P1


01 Jan 07

2.5 DOOR OPERATION 2.5.1 CABIN DOOR Cabin door of A330 is installed as follow

AIRBUS 330 2.5 / P2


01 Jan 07

2.5.2 CARGO DOOR A330-300 has 02 holds for loading ULD and 01 for bulk loading. Forward cargo hold is devided into compartment 1 and compartment 2 which can load both container and pallet. AFT cargo hold is devided into compartment 3 and compartment 4. Both container and pallet can be loaded at the AFT hold .

AIRBUS 330 2.5 / P3


01 Jan 07

2.5.2.1 CARGO DOOR OPERATION WARNING:

− Do not operate the door in winds more than 40 knots. − Do not let the door stay open in winds more than 65 knots. Injuries to persons or

damage to equipment can occur. − Do not open the door when the aircraft is pressurized. Injuries to persons or damage

to equipment can occur. 2.5.2.1.1 Open the cargo door − A platform is necessary to gain access to the bulk cargo door. The operating procedure

is written on the fuselage − Push the button of the outer handle to release it from its recess. − Move the outer or inner handle to the open position. − Push the bulk cargo door partly inwards, then put the door handle in the locked position.

Move the door inward until the hook engages with the hook arrester. 2.5.2.1.2 Close the cargo door − To close the door use the outer handle. − Move the outer handle to the open position to unlock the door from the hook arrester. − Hold the door to prevent it from falling down. − Move the bulk cargo door down into the opening and put the door handle in the locked

position. − Put the handle back into its recess. − Remove the access platform.

AIRBUS 330 2.5 / P4


01 Jan 07

AIRBUS 330 2.5 / P5


01 Jan 07

AIRBUS 330 2.5 / P6


01 Jan 07

2.5.3 SYSTEMS REQUIREMENTS FOR GROUND SERVICE EQUIPMENT 2.5.3.1 Aircraft doors – sill heights and dimensions.

Sill Height Door

Distance from A/C Nose

Door Size Minimum Maximum

TT Metres Inches Metres Inches Metres Inches Metres Inches A 5.85 230 1.07x1.93 42x76 4.40 175 4.58 180 B 17.74 698 1.07x1.93 42x76 4.69 184 4.86 191 C 46.68 1838 1.07x1.93 42x76 5.47 215 5.70 224 D 9.53 375 1.07x2.70 70x106 2.58 101 2.73 107 E 40.09 1579 2.73x1.68 107.5x66 3.22 127 3.45 136 F 43.07 1696 0.95x0.95 37.4x37.4 3.36 132 3.58 141

2.5.3.2 Requirement for GSE.

System Requirements Notes Electrical Type

Power Requirement

115/200V AC

2 x 90 kVA

3 phase 400 Hz

Air Conditioning

Maximum Flow Rate Maximum Output Pressure Cooling Capacity Heating Capacity

ppm psi

ton/hr N/A

3.2 kg/min 70 mbar

280000kcal/h

Pneumatic Minimum Capacity Maximum Pressure Minimum Pressure

ppm psi psi

kg/cm2

kg/cm2

Potable Water

Total Capacity Maximum Pressure Recommended Flow Rate

U.S gal psi

gpm

700L/1050 L 8.62 bar

60 L/min

Lavatory Total Waste Capacity Total Rinse Capacity Total Precharge Maximum Delivery Pressure Recommended Flow Rate

U.S gal U.S gal U.S gal

psi gpm

700L/1050L 100 L

36/54 L 2.4 bar

38 L/min

AIRBUS 330 2.5 / P7


01 Jan 07

2.5.3.3 Ground servicing points location.

Distance Height from Ground Aft of Nose From A/C

System

Metres Inches Metres Inches

Metres

Inches

Notes 1. Air conditioning 29.00 1142 0.54L 21L 1.88 71 2. Electrical 7.00 276 Trªn trục 1.65 65 3a. Fuel 30.00 1181 12.60R 496R 4..20 165 3b. Fuel panel 39.42 1552 3.24R 128R 1.85 73 4. Potable Water-FWD 48.15 1896 0.51R 20R 3.15 124 5. Lavatory 50.56 1994 0.09L 3L 3.65 144 6. Pneumatic 30.75 1211 0.84L 33L 1.79 71

AIRBUS 330 2.6 / P1


01 Jan 07

2.6 CARGO LOADING SYSTEM 2.6.1 CARGO HANDLING CONTROL SYSTEM Cargo handling control system operate the loading system by : − Power Drive System − Conveying System − Restraint System

CARGO HANDLING CONTROL SYSTEM

AIRBUS 330 2.6 / P2


01 Jan 07

2.6.2 RESTRAINT SYSTEM 2.6.2.1 MECHANICAL COMPONENT - MANUAL OPERATION 2.6.2.1.1 Door sill latches

AIRBUS 330 2.6 / P3


01 Jan 07

2.6.2.1.2 Fixed YZ-latches and Side Guides

2.6.2.1.3 Overrideable Y-guides, splitters

AIRBUS 330 2.6 / P4


01 Jan 07

2.6.2.1.4 Retractable XZ-latches

AIRBUS 330 2.6 / P5


01 Jan 07

2.6.2.1.5 Roller trays

2.6.2.1.6 Retractable Y-guides

AIRBUS 330 2.6 / P6


01 Jan 07

2.6.2.1.7 Overrideable YZ-latches

AIRBUS 330 2.7 / P1


01 Jan 07

2.7 FORM 2.7.1 LOADSHEET

AIRBUS 330 2.7 / P2


01 Jan 07

2.7.2 BALANCE CHART

AIRBUS 330 2.7 / P3


01 Jan 07

AIRBUS 330 2.7 / P4


01 Jan 07

AIRBUS 330 2.7 / P5


01 Jan 07

2.7.3 LOADING INSTRUCTION REPORT (LIR)

Part B- B777 & A330- English

Documents

Transcript of Part B- B777 & A330- English