Part B- A320 & A321- English

AIRBUS A320 & A321 LONR / P1

GROUND OPERATION MANUAL LIST OF NORMAL REVISIONS Rev 06

01 Jan 07

LIST OF NORMAL REVISIONS

Revísion No Issue Date Insert Date Signature

06 01 JAN 07

AIRBUS A320 & A321 LOEP / P1

GROUND OPERATION 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 3.0 1 06 01 Jan 07 01 Jan 07 3.1 1 – 6 06 01 Jan 07 01 Jan 07 3.2 1 – 5 06 01 Jan 07 01 Jan 07 3.3 1 – 8 06 01 Jan 07 01 Jan 07 3.4 1 – 10 06 01 Jan 07 01 Jan 07 3.5 1 – 6 06 01 Jan 07 01 Jan 07 3.6 1 – 9 06 01 Jan 07 01 Jan 07 3.7 1 – 5 06 01 Jan 07 01 Jan 07 4.0 1 06 01 Jan 07 01 Jan 07 4.1 1 – 6 06 01 Jan 07 01 Jan 07 4.2 1,2,3 06 01 Jan 07 01 Jan 07 4.3 1 – 8 06 01 Jan 07 01 Jan 07 4.4 1 – 11 06 01 Jan 07 01 Jan 07 4.5 1 – 9 06 01 Jan 07 01 Jan 07 4.6 1 – 9 06 01 Jan 07 01 Jan 07 4.7 1,2,3 06 01 Jan 07 01 Jan 07

AIRBUS A320 & A321 LOD / P1

GROUND OPERATION 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 16 Tansonnha International Airport Ground Services 04 18 Aircraft Maintenace Centre A75 01 19 Aircraft Maintenance Centre A76 01 20 Vietnam Airlines Representative at HPH 01 21 Vietnam Airlines Representative at VII 01 22 Vietnam Airlines Representative at HUI 01 23 Vietnam Airlines Representative at BMV 01 24 Vietnam Airlines Representative at NHA 01 25 Vietnam Airlines Branch Offices at ICN 01 26 Ground Handling Company at ICN 01 27 Vietnam Airlines Branch Offices at PUS 01 28 Ground Handling Company at PUS 01 29 Vietnam Airlines Branch Offices at KIX 01 30 Ground Handling Company at KIX 01 31 Vietnam Airlines Branch Offices at NRT 01 32 Ground Handling Company at NRT 01 33 Vietnam Airlines Branch Offices at FUK 01 34 Ground Handling Company at FUK 01 35 Vietnam Airlines Branch Offices at NGO 01 36 Ground Handling Company at NGO 01 37 Vietnam Airlines Branch Offices at HKG 01 38 Ground Handling Company at HKG 01

AIRBUS A320 & A321 LOD / P2

GROUND OPERATION MANUAL LIST OF DISTRIBUTIONS Rev 06

01 Jan 07

LIST OF DISTRIBUTIONS

No Users Quantity Remark 39 Vietnam Airlines Branch Offices at BJS 01 40 Ground Handling Company at BJS 01 41 Vietnam Airlines Branch Offices at KMG 01 42 Ground Handling Company at KMG 01 43 Vietnam Airlines Branch Offices at CAN 01 44 Ground Handling Company at CAN 01 45 Vietnam Airlines Branch Offices at KHH 01 46 Ground Handling Company at KHH 01 47 Vietnam Airlines Branch Offices at TPE 01 48 Ground Handling Company at TPE 01 49 Vietnam Airlines Branch Offices at BKK 01 50 Ground Handling Company at BKK 01 51 Vietnam Airlines Branch Offices at VTE 01 52 Ground Handling Company at VTE 01 53 Vietnam Airlines Branch Offices at PNH 01 54 Ground Handling Company at PNH 01 55 Vietnam Airlines Branch Offices at REP 01 56 Ground Handling Company at REP 01 57 Vietnam Airlines Branch Offices at SIN 01 58 Ground Handling Company at SIN 01 59 Vietnam Airlines Branch Offices at KUL 01 60 Ground Handling Company at KUL 01 61 Storage 09 Total 80

AIRBUS A320 & A321 LOB / P1

GROUND OPERATION MANUAL LIST OF BULLETINS Rev 06

01 Jan 07

LIST OF BULLETINS

Bulletin No. Date Insert Date Remvove Date Signature

AIRBUS A320 & A321 TOC / P2

GROUND OPERATION MANUAL TABLE OF CONTENT Rev 06

01 Jan 07

TABLE OF CONTENT

CHAPTER 3 – AIRCRAFT A320 3.1 General 3.2 Aircraft limitation & features 3.3 Cargo hold limitations & versions 3.4 Maximum package & restrictions due to restraint deficiencies 3.5 Door operation 3.6 Cargo loading system 3.7 Form

CHAPTER 4 – AIRCRAFT A321 4.1 General 4.2 Aircraft limitation & features 4.3 Cargo hold limitations & versions 4.4 Maximum package & restrictions due to restraint deficiencies 4.5 Door operation 4.6 Cargo loading system 4.7 Form

CHƯƠNG 3 MÁY BAY AIRBUS A320

CHAPTER 3

AIRCRAFT AIRBUS A320

AIRBUS A320 3.0 / P1

AIRCRAFT HANDLING MANUAL CONTENT Rev 06

01 Jan 07

CONTENT 3.1. General 3.1.1. List of aircraft 3.1.2. Exterior dimension 3.1.3. Ground clearance 3.1.4. Weight and balance definitions 3.2. Aircraft limitation & features 3.2.1. Certificate limitations 3.2.2. Standardized weight and index 3.2.3. Aircraft configuration 3.2.4. Standard taxi fuel 3.2.5. Standardized weight per passenger/ crew 3.2.6. Last minute change 3.2.7. Stretcher 3.3. Cargo hold limitation & version 3.3.1. Structural load limitation 3.3.2. Maximum load for ULD 3.3.3. Lower deck version 3.3.4. Carriage of special load 3.4. Maximum package & restrictions due to restraint deficiencies 3.4.1. Cargo hold and compartment arrangement 3.4.2. Maximum allowable weight due missing or inoperative restraints 3.5. Door operation 3.5.1. Cabin door 3.5.2. Cargo door 3.5.3. Systems requirements for ground service equipment 3.6. Cargo loading system 3.6.1. Cargo handling control system 3.6.2. Restraint system 3.7. Form 3.7.1. Loadsheet 3.7.2. Balance chart 3.7.3. Loading instruction report

3.1 /P1 3.1 /P2 3.1 /P3 3.1 /P4 3.2 /P1 3.2 /P2 3.2 /P3 3.2 /P4 3.2 /P4 3.2 /P5 3.2 /P5 3.3 /P1 3.3 /P3 3.3 /P4 3.3 /P6 3.4 /P1 3.4 /P6 3.5 /P1 3.5 /P2 3.5 /P6 3.6 /P1 3.6 /P2 3.7 /P1 3.7 /P2 3.7 /P3

AIRBUS 320 3.1 / P1

AIRCRAFT HANDLING MANUAL GENERAL Rev 06

01 Jan 07

3.1 GENERAL 3.1.1 LIST OF AIRCRAFT This manual is effective for the following aircraft

Model Registration number Configuration

VNA301

VNA302

VNA303

VNA304

VNA305

VNA306

VNA307

VNA308

VNA309

A320

VNA311

12C/138Y

AIRBUS 320 3.1 / P2


01 Jan 07

3.1.2 EXTERIOR DIMENSION

AIRBUS 320 3.1 / P3


01 Jan 07

3.1.3 GROUND CLEARANCE

AIRBUS 320 3.1 / P4


01 Jan 07

3.1.4 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 320 3.1 / 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 320 3.1 / 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 320 3.2 / P1

AIRCRAFT HANDLING MANUAL AIRCRAFT LIMITATIONS & FEATURES Rev 06

01 Jan 07

3.2 AIRCRAFT LIMITATIONS & FEATURES 3.2.1 CERTIFICATE LIMITATIONS 3.2.1.1 AIRCRAFT GROSS WEIGHT LIMITATIONS

Maximum limitation Item

VNA301/2/3/4/5/6/7/8 VNA309/VNA311

Max. Taxi weight

Max. Zero fuel weight

Max. Take off weight

Max. Landing weight

73900

61000

73500

64500

77900

61000

77000

64500

3.2.1.2 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 320 3.2 / P2


01 Jan 07

3.2.2 STANDARDIZED WEIGHT AND INDEX

Please refer to AHM050 validated by Flight Operation Department.

AIRBUS 320 3.2 / P3


01 Jan 07

3.2.3 AIRCRAFT CONFIGURATION

Aircraft REG Pax Configuration ROW Cabin zone

No of pax

A320 12C138Y

1-3

4-15

16-27

0A

0B

0C

12

66

72

AIRBUS 320 3.2 / P4


01 Jan 07

3.2.4 STANDARD TAXI FUEL

Standard taxi fuel for A320 is : 200 KG 3.2.5 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 320 3.2 / P5


01 Jan 07

3.2.6 LAST MINUTE CHANGE

The LMC tolerance is: +/- 500 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

3.2.7 STRETCHER

Stretcher position : 25ABC + 26ABC + 27ABC

Total : 9 seats

AIRBUS 320 3.3 / P1

AIRCRAFT HANDLING MANUAL CARGO HOLD LIMITATIONS & VERSIONS Rev 06

01 Jan 07

3.3 CARGO HOLD LIMITATIONS & VERSIONS 3.3.1 STRUCTURAL LOAD LIMITATION 3.3.1.1 MAXIMUM LOAD FOR CARGO HOLD

COMP. A320 Fleet COMBINED LOAD Floor loading limit

1 3402 3402 732 kg/sqm

3 2268 732 kg/sqm

4 2268 732 kg/sqm

5 1497

6033

732 kg/sqm

3.3.1.2 MAXIMUM GROSS WEIGHT FOR POSITIONS 3.3.1.2.1 FOR CONTAINERS

POSITION ALL POSITIONS

MAX WEIGHT (KG) AKH 1134

AIRBUS 320 3.3 / P2


01 Jan 07

3.3.1.2.2 FOR PALLETS


MAX WEIGHT (KG) PKC 1134

AIRBUS 320 3.3 / P3


01 Jan 07

3.3.2 MAXIMUM LOAD FOR ULD

Type Base Dimension (In)

W X L X H

Volume

(Cu ft) Tare Weight (Kg)

Maximum Gross Weight

(Kg)

AKH 60.4” X 61.5” X 46.0” 127 105 1134

PKC 60.4” X 61.5” 127 60 1134 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 320 3.3 / P4


01 Jan 07

3.3.3 LOWER DECK VERSION 3.3.3.1 FORWARD HOLD Maximum load in forward hold: 03 container LD3-46W/ LD3-46/ LD3-46R or 03 pallet LD3-46P or Both containers and pallets combined.

AIRBUS 320 3.3 / P5


01 Jan 07

3.3.3.2 AFT HOLD Maximum load in AFT hold 04 containers LD3-46W/ LD3-46/ LD3-46R or 04 pallets LD3-46P or Both containers and pallets combined.

AIRBUS 320 3.3 / P6


01 Jan 07

NOTES

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

3.3.4 CARRIAGE OF SPECIAL LOAD 3.3.4.1 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

3.3.4.2 Other special load 3.3.4.2.1 Dry Ice

Maximum weight/ hold

(With live animal, AVI)


(Without live animal, AVI) Maximum weight/ aircraft

100 KG 180 KG 360 KG

3.3.4.2.2 Live animal

Ventilation system on aircraft

A/C Reg. Hold Ventilation Temperature control

FWD No No

AFT Yes No ALL

BULK Yes No

AIRBUS 320 3.3 / P7


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

1000

Compartment 4

Compartment 5

Bird (Including baby chicken) 1,5 cubic meter Compartment 4+5

Dog, Cat 2,2 cubic meter Compartment 4+5

Monkey 100/ 350 KG Compartment 4+5

Reptile 4,0 cubic meter Compartment 4+5

Miscellaneous (Small AVI) 1,5 cubic meter Compartment 4+5

3.3.4.2.3 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”

AIRBUS 320 3.3 / P8


01 Jan 07

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

Maximum Transport Index 6.0

Bulk load

5.0

ULD load

Minimum distance 115 cm 100 cm

3.3.4.2.4 Priority baggage Priority baggage (BC) and crew baggage (D) must be loaded at AFT hold door side (position 41)

AIRBUS 320 3.4 / P1

AIRCRAFT HANDLING MANUAL

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

3.4 MAXIMUM PACKAGE & RESTRICTIONS DUE TO RESTRAINT

DEFICIENCIES 3.4.1 CARGO HOLD AND COMPARTMENT ARRANGEMENT 3.4.1.1 FORWARD HOLD 3.4.1.1.1 For Container

3.4.1.1.2 For Pallet

AIRBUS 320 3.4 / P2


MAXIMUM PACKAGE & RESTRICTIONS DUE TO RESTRAINT DEFICIENCIES

Rev 06 01 Jan 07

3.4.1.1.3 Allowable package sizes through FWD cargo door

For upright loading

WIDTH HEIGHT LENGTH

(m) (in) (m) (in) (m) (in)

1.499 59.0 1.194 47.0 1.643 64.7

For Tilted loading WIDTH HEIGHT LENGTH

(m) (in) (m) (in) (m) (in)

0.250 10.0 0.250 10.0 5.000 197.0

0.500 20.0 0.500 20.0 4.930 194.0

0.750 30.0 0.750 30.0 4.890 192.5

AIRBUS 320 3.4 / P3



3.4.1.2 AFT HOLD 3.4.1.2.1 For container

3.4.1.2.2 For pallet

AIRBUS 320 3.4 / P4



3.4.1.2.3 Allowable package sizes through AFT cargo door

For Upright loading

WIDTH HEIGHT LENGTH

(m) (in) (m) (in) (m) (in)

1.499 59.0 1.194 47.0 1.715 67.5

For Tilted loading WIDTH HEIGHT LENGTH

(m) (in) (m) (in) (m) (in)

0.250 10.0 0.250 10.0 5.309 209.0

0.500 20.0 0.500 20.0 5.144 202.5

0.750 30.0 0.750 30.0 4.915 193.5

3.4.1.2.4 Bulk

AIRBUS 320 3.4 / P5



3.4.1.2.5 Allowable package sizes through bulk cargo door

AIRBUS 320 3.4 / P6



3.4.2 MAXIMUM ALLOWABLE WEIGHT DUE MISSING OR INOPERATIVE

RESTRAINTS 3.4.2.1 FWD HOLD Key of latch types with restriction requirement

AIRBUS 320 3.4 / P7



3.4.2.1.1 Container and pallet latching

AIRBUS 320 3.4 / P8



Maximum allowable loads for missing or inoperative restrains :

AIRBUS 320 3.4 / P9



3.4.2.2 AFT HOLD : Key of latch types with restriction requirement

AIRBUS 320 3.4 / P10




AIRBUS 320 3.4 / P11



Maximum allowable loads for missing or inoperative restrains

AIRBUS 320 3.5 / P1

AIRCRAFT HANDLING MANUAL DOOR OPERATION Rev 06

01 Jan 07

3.5 DOOR OPERATION 3.5.1 CABIN DOOR Cabin door of A320 is installed as follow

AIRBUS 320 3.5 / P2


01 Jan 07

3.5.2 CARGO DOOR A320 has 02 holds for loading ULD and 01 for bulk loading. Forward cargo hold is compartment 1 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 .

Con

tain

ers

/ Pal

let

AIRBUS 320 3.5 / P3


01 Jan 07

3.5.2.1 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. 3.5.2.1.1 Open the FWD/ AFT cargo door

AIRBUS 320 3.5 / P4


01 Jan 07

3.5.2.1.2 Close the FWD/ AFT cargo door

3.5.2.1.3 Open the bulk cargo door

3.5.2.1.4 Close the bulk cargo door

AIRBUS 320 3.5 / P5


01 Jan 07

AIRBUS 320 3.5 / P6


01 Jan 07

3.5.3 SYSTEMS REQUIREMENTS FOR GROUND SERVICE EQUIPMENT 3.5.3.1 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 5.02 198 0.81x1.85 32x73 3.42 135 3.47 137 B 29.64 1,167 0.81x1.85 32x73 3.55 140 3.73 147 C 8.16 321 1.82x1.23 71.5x48.3 2.03 80 2.09 82 D 22.69 893 1.82x1.23 71.5x48.3 2.11 83 2.25 88.5 E 22.69 1,035 0.86x0.94 34x37 2.35 92.5 2.51 99

3.5.3.2 Requirement for GSE.

System Requirements Notes

Electrical Type Power Requirement

DC amp

115/200V AC 90 kVA

3 phase 400 Hz Receptical

Air Conditioning

Maximum Flow Rate Maximum Output Pressure Cooling Capacity Heating Capacity

130 ppm 0.735 psig

1 451 BTU/min 2 561 BTU/min

0.98 kg/min 50 mbar

25 500 W 45 000 W

Inlet temperature 20C

Pneumatic Minimum Capacity Maximum Pressure Minimum Pressure

ppm psi psi

kg/cm2

kg/cm2

Potable Water Total Capacity Maximum Pressure Recommended Flow Rate

53 US gal 50 psi

18 US gpm

200 L 3.45 bar 67 l/min

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

53 US gal US gal

2.5 Us gal 35 psi

18 US gpm

200 L L

9.5 L

per tank

2.4 bar 67 l/min

The arc of opening/closing cargo compartment doors is lower than the operating sill height. - Fwd compartment door: 21.93 inch (55.7 cm) - Aft department door: 21.93 inch (55.7 cm)

AIRBUS 320 3.5 / P7


01 Jan 07

3.5.3.3 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 12.45 490

1.11L 44L 1.73 68 2. Electrical 2.55 100 0.00 0.00 2.00 79 3a. Fuel 17.50 689 10 R 694R 3.50 138 3b. Fuel panel 12.45 490 1.11 R 42R 1.75 69 4. Potable Water-FWD 27.80 1,049 0.42 R 16.5L 2.60 102 5. Lavatory 3.40

28.60 134

1,126 1.20 R 0.80 R

47R 32R

2.35 2.79

93 110

Gravity unit Vacuum unit

6. Pneumatic 13.00 512 0.84 L 33L 1.76 69

AIRBUS 320 3.5 / P8


01 Jan 07

3.5.3.4 Aircraft Servicing arrangement. (not mandatory) Note: AS: Air Starter Unit BL: Conveyor belt F: Fuel Truck GL:Hight loader GPU: Ground Power Unit GS: Galley Service Truck ST: Passenger Stair LS: Lavatory Service Truck W: Water Service Truck GC: Air Conditioning Unit P: Passenger Bridge D: Dolly * Air stater unit and ground air conditioning unit must be parked at the same place Use Passenger Stair

AIRBUS 320 3.5 / P9


01 Jan 07

Use passenger Bridge

AIRBUS 320 3.6 / P1

AIRCRAFT HANDLING MANUAL CARGO LOADING SYSTEM Rev 06

01 Jan 07

3.6 CARGO LOADING SYSTEM 3.6.1 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 320 3.6 / P2


01 Jan 07

3.6.2 RESTRAINT SYSTEM 3.6.2.1 Restraint system in forward hold and AFT hold

Forward hold

AIRBUS 320 3.6 / P3


01 Jan 07

AIRBUS 320 3.6 / P4


01 Jan 07

AFT hold

AIRBUS 320 3.6 / P5


01 Jan 07

AIRBUS 320 3.6 / P6


01 Jan 07

3.6.2.1.1 XZ latches (Fixed)

3.6.2.1.2 XZ Latch Two Side Loaded (Retractable)

AIRBUS 320 3.6 / P7


01 Jan 07

3.6.2.1.3 YZ Latch ( Fixed )

3.6.2.1.4 Retractable XZ-latches

AIRBUS 320 3.6 / P8


01 Jan 07

3.6.2.1.5 Overridable Component

3.6.2.1.6 Fixed Guide

AIRBUS 320 3.6 / P9


01 Jan 07

3.6.2.1.7 Roller Tray

3.6.2.1.8 Ball Transfer Panel

AIRBUS 320 3.7 / P1

AIRCRAFT HANDLING MANUAL FORM Rev 06

01 Jan 07

3.7 FORM 3.7.1 LOADSHEET

AIRBUS 320 3.7 / P2


01 Jan 07

3.7.2 BALANCE CHART

AIRBUS 320 3.7 / P3


01 Jan 07

3.7.3 LOADING INSTRUCTION REPORT (LIR)

CHƯƠNG 4 MÁY BAY AIRBUS A321

CHAPTER 4

AIRCRAFT AIRBUS A321

AIRBUS A321 4.0 / P1

AIRCRAFT HANDLING MANUAL CONTENT Rev 06

01 Jan 07

CONTENT 4.1. General 4.1.1. List of aircraft 4.1.2. Exterior dimension 4.1.3. Ground clearance 4.1.4. Weight and balance definitions 4.2. Aircraft limitation & features 4.2.1. Certificate limitations 4.2.2. Standardized weight and index 4.2.3. Aircraft configuration 4.2.4. Standard taxi fuel 4.2.5. Standardized weight per passenger/ crew 4.2.6. Last minute change 4.2.7. Stretcher 4.3. Cargo hold limitation & version 4.3.1. Structural load limitation 4.3.2. Maximum load for ULD 4.3.3. Lower deck version 4.3.4. Carriage of special load 4.4. Maximum package & restrictions due to restraint deficiencies 4.4.1. Cargo hold and compartment arrangement 4.4.2. Maximum allowable weight due missing or inoperative restraints 4.5. Door operation 4.5.1. Cabin door 4.5.2. Cargo door 4.5.3. Systems requirements for ground service equipment 4.6. Cargo loading system 4.6.1. Cargo handling control system 4.6.2. Restraint system 4.7. Form 4.7.1. Loadsheet 4.7.2. Balance chart VNA343 4.7.3. Balance chart VNA344/5/7/8/9 4.7.4. Loading instruction report VNA343 4.7.5. Loading instruction report VNA344/5/7/8/9

4.1 /P1 4.1 /P2 4.1 /P3 4.1 /P4 4.2 /P1 4.2 /P2 4.2 /P3 4.2 /P4 4.2 /P4 4.2 /P5 4.2 /P5 4.3 /P1 4.3 /P3 4.3 /P4 4.3 /P6 4.4 /P1 4.4 /P5 4.5 /P1 4.5 /P2 4.5 /P7 4.6 /P1 4.6 /P2 4.7 /P1 4.7 /P2 4.7 /P3 4.7 /P4 4.7 /P5

AIRBUS 321 4.1 / P1


01 Jan 07

4.1 GENERAL 4.1.1 LIST OF AIRCRAFT This manual is effective for the following aircraft

Model Registration number Configuration

VNA343 16C/169Y

VNA344 16C/168Y

VNA345 16C/168Y

VNA347 16C/168Y

VNA348 16C/168Y

A321

VNA349 16C/168Y

AIRBUS 321 4.1 / P2


01 Jan 07

4.1.2 EXTERIOR DIMENSION

AIRBUS 321 4.1 / P3


01 Jan 07

4.1.3 GROUND CLEARANCE

AIRBUS 321 4.1 / P4


01 Jan 07

4.1.4 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 321 4.1 / 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 321 4.1 / 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 321 4.2 / P1


01 Jan 07

4.2 AIRCRAFT LIMITATIONS & FEATURES 4.2.1 CERTIFICATE LIMITATIONS 4.2.1.1 AIRCRAFT GROSS WEIGHT LIMITATIONS

Item Maximum limitation

Max. Taxi weight

Max. Zero fuel weight

Max. Take off weight

Max. Landing weight

89400

71500

89000

75500

4.2.1.2 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 321 4.2 / P2


01 Jan 07

4.2.2 STANDARDIZED WEIGHT AND INDEX

Please refer to AHM050 validated by Flight Operation Department.

AIRBUS 321 4.2 / P3


01 Jan 07

4.2.3 AIRCRAFT CONFIGURATION

Aircraft REG Pax Configuration ROW Cabin zone

No of pax

VNA343 16C169Y

1-7

8-20

21-33

0A

0B

0C

33

75

77

VNA344

VNA345

VNA347

VNA348

VNA349

16C168Y

1-14

15-27

28-39

0A

0B

0C

40

77

67

AIRBUS 321 4.2 / P4


01 Jan 07

4.2.4 STANDARD TAXI FUEL

Standard taxi fuel for A321 is : 200 KG 4.2.5 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 321 4.2 / P5


01 Jan 07

4.2.6 LAST MINUTE CHANGE

The LMC tolerance is: +/- 500 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

4.2.7 STRETCHER

Aircraft VNA343 Stretcher position : 31ABC + 32ABC + 33ABC

Total : 9 seats Aircraft VNA344/5/7/9 Stretcher position : 37DEG + 38DEG + 39EG

Total : 8 seats Aircraft VNA348

Stretcher position : 37DEG + 38DEG + 39G

Total : 7 seats

AIRBUS 321 4.3 / P1


01 Jan 07

4.3 CARGO HOLD LIMITATIONS & VERSIONS 4.3.1 STRUCTURAL LOAD LIMITATION 4.3.1.1 MAXIMUM LOAD FOR CARGO HOLD

COMP. VNA343 COMBINED LOAD Floor loading limit

1 2268 732 kg/sqm

2 3402 5670

732 kg/sqm

3 2268 732 kg/sqm

4 2268 732 kg/sqm

5 1497

6033

732 kg/sqm

COMP. VNA344/5/7/8/9 COMBINED LOAD Floor loading limit

1 2268 732 kg/sqm

2 3402 5670

732 kg/sqm

3 3402 732 kg/sqm

4 2268 732 kg/sqm

5 1497

7167

732 kg/sqm

AIRBUS 321 4.3 / P2


01 Jan 07

4.3.1.2 MAXIMUM GROSS WEIGHT FOR POSITIONS 4.3.1.2.1 FOR CONTAINERS


MAX WEIGHT (KG) AKH 1134

4.3.1.2.2 FOR PALLETS


MAX WEIGHT (KG) PKC 1134

Notes: The position 31 on A/C VNA343 is ACT (Auxiliary Centre Tank)

AIRBUS 321 4.3 / P3


01 Jan 07

4.3.2 MAXIMUM LOAD FOR ULD

Type Base Dimension (In)

W X L X H

Volume

(Cu ft) Tare Weight (Kg)

Maximum Gross Weight

(Kg)

AKH 60.4” X 61.5” X 46.0” 127 105 1134

PKC 60.4” X 61.5” 127 60 1134 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 321 4.3 / P4


01 Jan 07

4.3.3 LOWER DECK VERSION 4.3.3.1 FORWARD HOLD Maximum load in forward hold: 05 container LD3-46W/ LD3-46/ LD3-46R or 05 pallet LD3-46P or Both containers and pallets combined.

AIRBUS 321 4.3 / P5


01 Jan 07

4.3.3.2 AFT HOLD Maximum load in AFT hold 05 containers LD3-46W/ LD3-46/ LD3-46R (VNA343 only 04 container) or 05 pallets LD3-46P (VNA343 only 04 mâm) or Both containers and pallets combined.

NOTES

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

AIRBUS 321 4.3 / P6


01 Jan 07

4.3.4 CARRIAGE OF SPECIAL LOAD 4.3.4.1 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

4.3.4.2 Other special load 4.3.4.2.1 Dry Ice


(With live animal, AVI)


(Without live animal, AVI) Maximum weight/ aircraft

100 KG 180 KG 360 KG

4.3.4.2.2 Live animal

Ventilation system on aircraft

A/C Reg. Hold Ventilation Temperature control

FWD No No

AFT Yes 50C - 260C ALL

BULK Yes 50C - 260C

AIRBUS 321 4.3 / P7


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

1000

Compartment 4

Compartment 5

Bird (Including baby chicken) 1,5 cubic meter Compartment 4+5

Dog, Cat 2,2 cubic meter Compartment 4+5

Monkey 100/ 350 KG Compartment 4+5

Reptile 4,0 cubic meter Compartment 4+5

Miscellaneous (Small AVI) 1,5 cubic meter Compartment 4+5

4.3.4.2.3 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”

AIRBUS 321 4.3 / P8


01 Jan 07

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

Maximum Transport Index 6.0

Bulk load

5.0

ULD load

Minimum distance 115 cm 100 cm

4.3.4.2.4 Hành lý ưu tiên Priority baggage (BC) and crew baggage (D) must be loaded at AFT hold door side (position 41)

AIRBUS 321 4.4 / P1



4.4 MAXIMUM PACKAGE & RESTRICTIONS DUE TO RESTRAINT

DEFICIENCIES 4.4.1 CARGO HOLD AND COMPARTMENT ARRANGEMENT 4.4.1.1 FORWARD HOLD 4.4.1.1.1 For Container

4.4.1.1.2 For Pallet

AIRBUS 321 4.4 / P2


MAXIMUM PACKAGE & RESTRICTIONS DUE TO RESTRAINT DEFICIENCIES

Rev 06 01 Jan 07

4.4.1.1.3 Allowable package sizes through FWD cargo door

For upright loading

WIDTH (m) HEIGHT (m) LENGTH (m)

1.499 1.194 1.524

For Tilted loading


0.254 0.254 5.300

0.508 0.508 5.150

0.762 0.762 5.000

AIRBUS 321 4.4 / P3



4.4.1.2 AFT HOLD 4.4.1.2.1 For container

4.4.1.2.2 For pallet

AIRBUS 321 4.4 / P4



4.4.1.2.3 Allowable package sizes through AFT cargo door

For Upright loading


1.499 1.194 1.524

For Tilted loading WIDTH (m) HEIGHT (m) LENGTH (m)

0.254 0.254 5.300

0.508 0.508 5.150

0.762 0.762 5.000

4.4.1.2.4 Bulk

4.4.1.2.5 Allowable package sizes through bulk cargo door

For Upright loading WIDTH (m) HEIGHT (m) LENGTH (m)

1.499 1.194 1.524

For Tilted loading


0.250 0.250 3.240

0.500 0.500 3.240

0.750 0.750 3.240

AIRBUS 321 4.4 / P5



4.4.2 MAXIMUM ALLOWABLE WEIGHT DUE MISSING OR INOPERATIVE

RESTRAINTS 4.4.2.1 FWD HOLD Key of latch types with restriction requirement

AIRBUS 321 4.4 / P6




AIRBUS 321 4.4 / P7



Maximum allowable loads for missing or inoperative restrains :

AIRBUS 321 4.4 / P8



4.4.2.2 AFT HOLD : Key of latch types with restriction requirement

AIRBUS 321 4.4 / P9




AIRBUS 321 4.4 / P10



Maximum allowable loads for missing or inoperative restrains

AIRBUS 321 4.5 / P1


01 Jan 07

4.5 DOOR OPERATION 4.5.1 CABIN DOOR Cabin door of A321 is installed as follow

AIRBUS 321 4.5 / P2


01 Jan 07

4.5.2 CARGO DOOR A321 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 .

Con

tain

ers

/ Pal

let

Con

tain

ers

/ Pal

let

AC

T

AIRBUS 321 4.5 / P3


01 Jan 07

4.5.2.1 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. 4.5.2.1.1 Open the FWD/ AFT cargo door

AIRBUS 321 4.5 / P4


01 Jan 07

4.5.2.1.2 Close the FWD/ AFT cargo door

4.5.2.1.3 Open the bulk cargo door

4.5.2.1.4 Close the bulk cargo door

AIRBUS 321 4.5 / P5


01 Jan 07

AIRBUS 321 4.5 / P6


01 Jan 07

AIRBUS 321 4.5 / P7


01 Jan 07

4.5.3 SYSTEMS REQUIREMENTS FOR GROUND SERVICE EQUIPMENT 4.5.3.1 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 5.02 189 0.81x1.85 32x73 3.43 135 3.45 137 B 8.82 1167 0.81x1.85 32x73 3.46 136 3.54 139 C 36.57 1440 0.81x1.85 32x73 3.54 139 3.73 147 D 8.16 321 1.82x1.23 71.5x48 2.03 80 2.09 82 E 29.72 1170 1.82x1.23 71.5x48 2.11 83 2.26 89 F 33.22 1370 0.86x0.94 34x37 2.34 92 2.51 99

4.5.3.2 Requirement for GSE.

System Requirements Notes Electrical Type

Power Requirement

DC

amp

115/200V AC

1 X 90 kVA

3 pha 400 Hz Receptical

Air Conditioning

Maximum Flow Rate Maximum Output Pressure Cooling Capacity Heating Capacity

ppm psig

BTU/min BTU/min

1.5 kg/sec 35 mbar

105000 kcal/h 200000 BTU.h

Inlet temperature 20C

Pneumatic Minimum Capacity Maximum Pressure Minimum Pressure

ppm psi psi

kg/cm2

kg/cm2

Potable Water

Total Capacity Maximum Pressure Recommended Flow Rate

US gal psi

US gpm

200 L 3.45 bar 60 l/min

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

53 US gal US gal

2.5 Us gal 35 psi

18 US gpm

170 L 57 L

9.5 L 2.4 bar

38 l/min

AIRBUS 321 4.5 / P8


01 Jan 07

4.5.3.3 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 16.72 490 1.11L 44L 1.73 68 2. Electrical 2.55 100 0.00 0.00 2.00 79 3a. Fuel 21.77 689 10 R 694R 3.50 138 3b. Fuel panel 16.72 490 1.11 R 42R 1.75 69 4. Potable Water-FWD 38.24 1,049 0.42 R 16.5L 2.60 102 5. Lavatory 35.50 980 0.80R 32R 2.79 110 6. Pneumatic 17.27 448 0.84 L 33L 1.76 69

AIRBUS 321 4.6 / P1


01 Jan 07

4.6 CARGO LOADING SYSTEM 4.6.1 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 321 4.6 / P2


01 Jan 07

4.6.2 RESTRAINT SYSTEM 4.6.2.1 Restraint system in forward hold and AFT hold

Forward hold

AIRBUS 321 4.6 / P3


01 Jan 07

AIRBUS 321 4.6 / P4


01 Jan 07

AFT hold

AIRBUS 321 4.6 / P5


01 Jan 07

AIRBUS 321 4.6 / P6


01 Jan 07

4.6.2.1.1 XZ latches (Fixed)

4.6.2.1.2 XZ Latch Two Side Loaded (Retractable)

AIRBUS 321 4.6 / P7


01 Jan 07

4.6.2.1.3 YZ Latch ( Fixed )

4.6.2.1.4 Retractable XZ-latches

AIRBUS 321 4.6 / P8


01 Jan 07

4.6.2.1.5 Overridable Component

4.6.2.1.6 Fixed Guide

AIRBUS 321 4.6 / P9


01 Jan 07

4.6.2.1.7 Roller Tray

4.6.2.1.8 Ball Transfer Panel

AIRBUS 321 4.7 / P1


01 Jan 07

4.7 FORM 4.7.1 LOADSHEET

AIRBUS 321 4.7 / P2


01 Jan 07

4.7.2 BALANCE CHART FOR AIRCRAFT VNA343

AIRBUS 321 4.7 / P3


01 Jan 07

4.7.3 BALANCE CHART FOR AIRCRAFT VNA344/5/7/8

AIRBUS 321 4.7 / P4


01 Jan 07

4.7.4 LOADING INSTRUCTION REPORT FOR AIRCRAFT VNA343

AIRBUS 321 4.7 / P5


01 Jan 07

4.7.5 LOADING INSTRUCTION REPORT FOR AIRCRAFT VNA344/5/7/8

Part B- A320 & A321- English

Documents

Transcript of Part B- A320 & A321- English