Part B- ATR & F70- English

ATR72 & FOKKER70 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

ATR72 & FOKKER70 LOFP / 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 00 01 Jan 07 01 Jan 07 LOEP 1 00 01 Jan 07 01 Jan 07 LOD 1, 2, 3 00 01 Jan 07 01 Jan 07 LOB 1 00 01 Jan 07 01 Jan 07 TOC 1 00 01 Jan 07 01 Jan 07 5.0 1 00 01 Jan 07 01 Jan 07 5.1 1 – 6 00 01 Jan 07 01 Jan 07 5.2 1 – 5 00 01 Jan 07 01 Jan 07 5.3 1,2,3 00 01 Jan 07 01 Jan 07 5.4 1,2,3 00 01 Jan 07 01 Jan 07 5.5 1 – 8 00 01 Jan 07 01 Jan 07 5.6 1,2 00 01 Jan 07 01 Jan 07 5.7 1,2,3 00 01 Jan 07 01 Jan 07 6.0 1 00 01 Jan 07 01 Jan 07 6.1 1 – 6 00 01 Jan 07 01 Jan 07 6.2 1 – 5 00 01 Jan 07 01 Jan 07 6.3 1 – 4 00 01 Jan 07 01 Jan 07 6.4 1,2 00 01 Jan 07 01 Jan 07 6.5 1 – 7 00 01 Jan 07 01 Jan 07 6.6 1,2,3 00 01 Jan 07 01 Jan 07 6.7 1 – 4 00 01 Jan 07 01 Jan 07

ATR72 & FOKKER70 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 17 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 SQH 01 22 Vietnam Airlines Representative at DIN 01 23 Vietnam Airlines Representative at VII 01 24 Vietnam Airlines Representative at HUI 01 25 Vietnam Airlines Representative at PXU 01 26 Vietnam Airlines Representative at BMV 01 27 Vietnam Airlines Representative at DLI 01 28 Vietnam Airlines Representative at TBB 01 29 Vietnam Airlines Representative at UIH 01 30 Vietnam Airlines Representative at NHA 01 31 Vietnam Airlines Representative at PQC 01 32 Vietnam Airlines Representative at VKG 01

ATR72 & FOKKER70 LOD / P2

GROUND OPERATION MANUAL LIST OF DISTRIBUTIONS Rev 06

01 Jan 07

LIST OF DISTRIBUTIONS

No Users Quantity Remark 33 Vietnam Airlines Branch Offices at VTE 01 34 Ground Handling Company at VTE 01 35 Ground Handling Company at LPQ 01 36 Vietnam Airlines Branch Offices at PNH 01 37 Ground Handling Company at PNH 01 38 Vietnam Airlines Branch Offices at REP 01 39 Ground Handling Company at REP 01 40 Storage 09 Total 60

ATR72 & FOKKER70 LOB / P1

GROUND OPERATION MANUAL LIST OF BULLETINS Rev 06

01 Jan 07

LIST OF BULLETINS

Bulletin No. Date Insert Date Remvove Date Signature

ATR72 & FOKKER70 TOC / P2

GROUND OPERATION MANUAL TABLE OF CONTENT Rev 06

01 Jan 07

TABLE OF CONTENT

CHAPTER 5 – FOKKER 70 5.0 Content 5.1 General 5.2 Aircraft limitation & features 5.3 Cargo hold limitations & versions 5.4 Maximum package & restrictions due to restraint deficiencies 5.5 Door operation 5.6 Cargo loading system 5.7 Form CHAPTER 6 – ATR72 6.0 Content 6.1 General 6.2 Aircraft limitation & features 6.3 Cargo hold limitations & versions 6.4 Maximum package & restrictions due to restraint deficiencies 6.5 Door operation 6.6 Cargo loading system 6.7 Form

CHƯƠNG 5 MÁY BAY FOKKER 70

CHAPTER 5

AIRCRAFT FOKKER 70

FOKKER 70 5.0 / P1

AIRCRAFT HANDLING MANUAL CONTENT Rev 06

01 Jan 07

CONTENT 5.1. General 5.1.1. List of aircraft 5.1.2. Exterior dimension 5.1.3. Ground clearance 5.1.4. Weight and balance definitions 5.2. Aircraft limitation & features 5.2.1. Certificate limitations 5.2.2. Standardized weight and index 5.2.3. Aircraft configuration 5.2.4. Standard taxi fuel 5.2.5. Standardized weight per passenger/ crew 5.2.6. Last minute change 5.2.7. Stretcher 5.3. Cargo hold limitation & version 5.3.1. Structural load limitation 5.3.2. Maximum load for ULD 5.3.3. Lower deck version 5.3.4. Carriage of special load 5.4. Maximum package & restrictions due to restraint deficiencies 5.4.1. Cargo hold and compartment arrangement 5.4.2. Maximum allowable weight due missing or inoperative restraints 5.5. Door operation 5.5.1. Cabin door 5.5.2. Cargo door 5.5.3. Systems requirements for ground service equipment 5.6. Cargo loading system 5.6.1. Cargo handling control system 5.6.2. Restraint system 5.7. Form 5.7.1. Loadsheet 5.7.2. Balance chart 5.7.3. Loading instruction report

5.1 /P1 5.1 /P2 5.1 /P3 5.1 /P4 5.2 /P1 5.2 /P2 5.2 /P3 5.2 /P4 5.2 /P4 5.2 /P5 5.2 /P5 5.3 /P1 5.3 /P2 5.3 /P3 5.3 /P3 5.4 /P1 5.4 /P3 5.5 /P1 5.5 /P3 5.5 /P6 5.6 /P1 5.6 /P1 5.7 /P1 5.7 /P2 5.7 /P3

FOKKER 70 5.1 / P1

AIRCRAFT HANDLING MANUAL GENERAL Rev 06

01 Jan 07

5.1 GENERAL 5.1.1 LIST OF AIRCRAFT This manual is effective for the following aircraft

Model Registration number Configuration

VNA502 FOKKER 70

VNA504 79Y

FOKKER 70 5.1 / P2


01 Jan 07

5.1.2 EXTERIOR DIMENSION

FOKKER 70 5.1 / P3


01 Jan 07

5.1.3 GROUND CLEARANCE

NA

FOKKER 70 5.1 / P4


01 Jan 07

5.1.4 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.

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.

FOKKER 70 5.1 / P5


01 Jan 07

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.

25 Take off fuel

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

FOKKER 70 5.1 / P6


01 Jan 07

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.

FOKKER 70 5.2 / P1

AIRCRAFT HANDLING MANUAL AIRCRAFT LIMITATIONS & FEATURES Rev 06

01 Jan 07

5.2 AIRCRAFT LIMITATIONS & FEATURES 5.2.1 CERTIFICATE LIMITATIONS 5.2.1.1 AIRCRAFT GROSS WEIGHT LIMITATIONS

Item Maximum limitation

Max. Taxi weight

Max. Zero fuel weight

Max. Take off weight

Max. Landing weight

38329

32658

38100

35834

5.2.1.2 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.

FOKKER 70 5.2 / P2


01 Jan 07

5.2.2 STANDARDIZED WEIGHT AND INDEX

Please refer to AHM050 validated by Flight Operation Department.

FOKKER 70 5.2 / P3


01 Jan 07

5.2.3 AIRCRAFT CONFIGURATION

Aircraft REG Pax Configuration ROW Cabin zone

No of Pax

VNB502/504 79Y 1-11

12-17

0A

0B

55

24

FOKKER 70 5.2 / P4


01 Jan 07

5.2.4 STANDARD TAXI FUEL

Standard taxi fuel for Fokker70 is : 200 KG 5.2.5 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.

FOKKER 70 5.2 / P5


01 Jan 07

5.2.6 LAST MINUTE CHANGE

The LMC tolerance is: +/- 300 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

5.2.7 STRETCHER

Stretcher position : 15AB + 16AB + 17AB

Total : 6 seats

FOKKER 70 5.3 / P1

AIRCRAFT HANDLING MANUAL CARGO HOLD LIMITATIONS & VERSIONS Rev 06

01 Jan 07

5.3 CARGO HOLD LIMITATIONS & VERSIONS 5.3.1 STRUCTURAL LOAD LIMITATION 5.3.1.1 MAXIMUM LOAD FOR CARGO HOLD

Forward hold Compartment 11 12 13

Max Allowed Load (kg) 650 1750 Max Floor Load/ Flat Floor (kg/m2) 1000 Max Floor Load/ Curved Floor (kg/m2) 366 Max Running Load/ Tied Cargo (kg/m) 600 Max Running Load/ Untied Cargo (kg/m) 372 Net usable volume (m3) 2.24 1.708 4.025 Max length (mm) 6383 Max width (mm) 2100 Max height 770

AFT hold Compartment 41 42

Max Allowed Load (kg) 741 Max Floor Load/ Flat Floor (kg/m2) 1000 Max Floor Load/ Curved Floor (kg/m2) 366 Max Running Load/ Tied Cargo (kg/m) 600 Max Running Load/ Untied Cargo (kg/m) 372 Net usable volume (m3) 2.50 2.13 Max length (mm) 4206 Max width (mm) 2100 Max height 770

5.3.1.2 MAXIMUM GROSS WEIGHT FOR POSITIONS 5.3.1.2.1 FOR CONTAINERS

Not applicable

5.3.1.2.2 FOR PALLETS

Not applicable

FOKKER 70 5.3 / P2


01 Jan 07

5.3.2 MAXIMUM LOAD FOR ULD

Not applicable

FOKKER 70 5.3 / P3


01 Jan 07

5.3.3 LOWER DECK VERSION

Not applicable

5.3.4 CARRIAGE OF SPECIAL LOAD 5.3.4.1 Magnetized Materials (MAG) Loading

− Not applicable. 5.3.4.2 Other special load 5.3.4.2.1 Dry Ice

− Maximum 20kg/ Flight. 5.3.4.2.2 Live animal

Ventilation system on aircraft

A/C Reg. Hold Ventilation Temperature control

FWD No No ALL

AFT No No

− Live animal : Not applicable. 5.3.4.2.3 Radioactive material

− Not applicable.

FOKKER 70 5.4 / P1

AIRCRAFT HANDLING MANUAL

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

5.4 MAXIMUM PACKAGE & RESTRICTIONS DUE TO RESTRAINT

DEFICIENCIES 5.4.1 CARGO HOLD AND COMPARTMENT ARRANGEMENT 5.4.1.1 FORWARD HOLD

5.4.1.1.1 Allowable package sizes through FWD cargo door

FOKKER 70 5.4 / P2



5.4.1.2 AFT HOLD

5.4.1.2.1 Allowable package sizes through AFT cargo door

FOKKER 70 5.4 / P3



5.4.2 MAXIMUM ALLOWABLE WEIGHT DUE MISSING OR INOPERATIVE RESTRAINTS

Not applicable

FOKKER 70 5.5 / P1

AIRCRAFT HANDLING MANUAL DOOR OPERATION Rev 06

01 Jan 07

5.5 DOOR OPERATION 5.5.1 CABIN DOOR Cabin door of Fokker 70 is installed as follow

Passenger door

FOKKER 70 5.5 / P2


01 Jan 07

Service door

Emergency Exit

FOKKER 70 5.5 / P3


01 Jan 07

5.5.2 CARGO DOOR Fokker 70 has 02 holds for bulk loading. Forward cargo hold is 1. It is devided into 11, 12 & 13 AFT cargo hold is 4 . It is devided into 41 & 42

5.5.2.1 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.

FOKKER 70 5.5 / P4


01 Jan 07

5.5.2.1.1 Open, close the FWD cargo door

Open − Push flap to grasp handle 1 − Lift locking handle 1 up − Pull latching hadle 2 down − Pull out door with latching handle . − Release push/pull rod (From AFT side of door) − Push door fully open into uplocks

Close

− UNLOCK BOTH uplocks (At sides of door opening) − Pull door down and stow push/pull rod − Push door closed − Push latching handle 2 flush − Push locking handle 1 flush − CHECK: vent flap closed

FOKKER 70 5.5 / P5


01 Jan 07

5.5.2.1.2 Open/ Close the AFT cargo door

Open

− Push flap to grasp handle 1 − Lift locking handle 1 up − Pull latching handle 2 down − Pull out door with latching handle − Release push/pull rod (From forward side of door) − Push door fully open into uplock

Close

− UNLOCK uplock (At side of door opening) − Pull door down and stow push/pull rod − Push door closed − Push latching handle 2 flush − Push locking handle 1 flush − CHECK: vent flap closed

FOKKER 70 5.5 / P6


01 Jan 07

5.5.3 SYSTEMS REQUIREMENTS FOR GROUND SERVICE EQUIPMENT 5.5.3.1 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 4.24 167 0.61x1.29 24x50.6 2.04 80 2.44 96 B 4.36 172 0.86x2.21 33.9x87 1.56* 61* 196* 77* C 8.08 318 1.40x1.45 55x57 1.19 47 1.51 59 D 19.48 767 0.97x1.24 38.2x48 1.51 59 1.80 71 E 4.36 172 0.86x2.21 33.9x87 2.04 80 2.44 96

5.5.3.2 Requirement for GSE

System Requirements Notes

Electrical Type Power Requirement

28V DC 30 amp

115/200V AC 40 kVA

AC: 3 phase 400 Hz 60 kVA for 1 miniute* DC: 180 Amps for 1 min* 800 Amps for 0.5 sec* * for engine starting

Air Conditioning

Maximum Flow Rate Maximum Output Pressure Cooling Capacity Heating Capacity

75 ppm 0.7 psi ton/hr

34.0 kg/min 0.05 kg/cm2

kcal/sec Btu

Max. air temperature 700C

Pneumatic Minimum Capacity Maximum Pressure Minimum Pressure

65 ppm

50 psi

20 psi

29.5 kg/min

3.52 kg/cm2

1.41 kg/cm2

at 150C ambient temperature Max. temperature 2500C at 150C ambient tempersture

Potable Water Total Capacity Maximum Pressure Recommended Flow Rate

21 US gal 35 psi

20 l/min

80 L 2.46 kg/cm2

psi

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

39 US gal US gal

9 US gal 50 psi

gpm

147.6L L

36 L 3.52 kg/cm2

l/s

Base on 3 toilets F70: 1 standard + 2 optional

FOKKER 70 5.5 / P7


01 Jan 07

5.5.3.3 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 5.08 200 1.25R 49R 1.54 61 2. Electrical 3.24 128 1.10R 43R 1.45 57 3. Fule 13.94 549 2.89R 114R 1.64 65 4. Potable Water 11.60 457 0.68L 27L 1.29 51

Forward 3.30 130 1.10L 43L 1.46 57 5. Lavatory Aft 19.68 775 0.99L 39L 1.74 69

6. Pneumatic 21.06 829 0.63R 25R 1.76 69

FOKKER 70 5.5 / P8


01 Jan 07

5.5.3.4 Aircraft Servicing arrangement. (not madatory)

FOKKER 70 5.6 / P1

AIRCRAFT HANDLING MANUAL CARGO LOADING SYSTEM Rev 06

01 Jan 07

5.6 CARGO LOADING SYSTEM 5.6.1 CARGO HANDLING CONTROL SYSTEM

Not applicable 5.6.2 RESTRAINT SYSTEM

Forward hold

oo oo

oo oo oo oo oo

Tied down point

oo o oo oo oo oo oo oo oo oo oo

oo o oo oo oo oo oo oo oo

FOKKER 70 5.6 / P2


01 Jan 07

AFT hold

oo o oo oo oo oo oo oo

oo o oo oo oo oo oo oo

Tied down point

FOKKER 70 5.7 / P1

AIRCRAFT HANDLING MANUAL FORM Rev 06

01 Jan 07

5.7 FORM 5.7.1 LOADSHEET

FOKKER 70 5.7 / P2


01 Jan 07

5.7.2 BALANCE CHART

FOKKER 70 5.7 / P3


01 Jan 07

5.7.3 LOADING INSTRUCTION REPORT (LIR)

CHƯƠNG 6 MÁY BAY ATR72

CHAPTER 6

AIRCRAFT ATR72

ATR 72 6.0 / P1

AIRCRAFT HANDLING MANUAL CONTENT Rev 06

01 Jan 07

CONTENT 6.1. General 6.1.1. List of aircraft 6.1.2. Exterior dimension 6.1.3. Ground clearance 6.1.4. Weight and balance definitions 6.2. Aircraft limitation & features 6.2.1. Certificate limitations 6.2.2. Standardized weight and index 6.2.3. Aircraft configuration 6.2.4. Standard taxi fuel 6.2.5. Standardized weight per passenger/ crew 6.2.6. Last minute change 6.2.7. Stretcher 6.3. Cargo hold limitation & version 6.3.1. Structural load limitation 6.3.2. Maximum load for ULD 6.3.3. Lower deck version 6.3.4. Carriage of special load 6.4. Maximum package & restrictions due to restraint deficiencies 6.4.1. Cargo hold and compartment arrangement 6.4.2. Maximum allowable weight due missing or inoperative restraints 6.5. Door operation 6.5.1. Cabin door 6.5.2. Cargo door 6.5.3. Systems requirements for ground service equipment 6.6. Cargo loading system 6.6.1. Cargo handling control system 6.6.2. Restraint system 6.7. Form 6.7.1. Loadsheet & Balance chart form for aircraft VNB202/4/6/8/42/46 6.7.2. Loadsheet & Balance chart form for aircraft VNB210/2/4 6.7.3. Loadsheet & Balance chart form for aircraft VNBB216 6.7.4. Loading instruction report

6.1 /P1 6.1 /P2 6.1 /P3 6.1 /P4 6.2 /P1 6.2 /P2 6.2 /P3 6.2 /P4 6.2 /P4 6.2 /P5 6.2 /P5 6.3 /P1 6.3 /P2 6.3 /P2 6.3 /P4 6.4 /P1 6.4 /P2 6.5 /P1 6.5 /P4 6.5 /P5 6.6 /P1 6.6 /P1 6.7 /P1 6.7 /P2 6.7 /P3 6.7 /P4

ATR 72 6.1 / P1


01 Jan 07

6.1 GENERAL 6.1.1 LIST OF AIRCRAFT This manual is effective for the following aircraft

Model Registration number Configuration

VNB202

VNB204

VNB206

VNB208

VNB246

VNB248

VNB210

VNB212

VNB214

66Y ATR72

VNB216 70Y

ATR 72 6.1 / P2


01 Jan 07

6.1.2 EXTERIOR DIMENSION

ATR 72 6.1 / P3


01 Jan 07

6.1.3 GROUND CLEARANCE

ATR 72 6.1 / P4


01 Jan 07

6.1.4 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.

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.

ATR 72 6.1 / P5


01 Jan 07

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.

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

ATR 72 6.1 / P6


01 Jan 07

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.

ATR 72 6.2 / P1


01 Jan 07

6.2 AIRCRAFT LIMITATIONS & FEATURES 6.2.1 CERTIFICATE LIMITATIONS 6.2.1.1 AIRCRAFT GROSS WEIGHT LIMITATIONS

Maximum limitation

Item VNB202/4/6/8

VNB246/248/216

VNB210/212/214

Max. Taxi weight

Max. Zero fuel weight

Max. Take off weight

Max. Landing weight

21530

19700

21500

21350

22670

20300

22500

22350

6.2.1.2 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.

ATR 72 6.2 / P2


01 Jan 07

6.2.2 STANDARDIZED WEIGHT AND INDEX

Please refer to AHM050 validated by Flight Operation Department.

ATR 72 6.2 / P3


01 Jan 07

6.2.3 AIRCRAFT CONFIGURATION

Aircraft REG Pax Configuration ROW Cabin zone

No of Pax

VNB202/4/6/8

VNB246/8

VNB210/2/4

66Y

1-5

6-12

13-17

0A

0B

0C

20

28

18

VNB216 70Y

1-6

7-14

15-19

0A

0B

0C

24

28

18

ATR 72 6.2 / P4


01 Jan 07

6.2.4 STANDARD TAXI FUEL

Standard taxi fuel for ATR72 is : 50 KG 6.2.5 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.

ATR 72 6.2 / P5


01 Jan 07

6.2.6 LAST MINUTE CHANGE

The LMC tolerance is: +/- 300 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

6.2.7 STRETCHER

Stretcher position : 14CD + 15CD + 16CD

Total : 6 seats

ATR 72 6.3 / P1


01 Jan 07

6.3 CARGO HOLD LIMITATIONS & VERSIONS 6.3.1 STRUCTURAL LOAD LIMITATION 6.3.1.1 MAXIMUM LOAD FOR CARGO HOLD VNB202/204/206/208/210/212/214/216

Compartment Hold Hold Limit

Volume Running Load

Limitation

Floor Loading

Limit

Cumulative Hold

Maximum

Forward(RH) 1 480 3.0 510 400

Forward(LH) 1 448 2.8 510 400 928

After(FWD) 4 302 510 400

After(AFT) 4 442 4.65

510 400 744

VNB246/248

Compartment Hold

Hold Limit

Volume Running Load

Limitation

Floor Loading

Limit

Cumulative Hold

Maximum

Forward(RH) 1 480 3.0 510 400

Forward(LH) 1 448 2.8 510 400 928

After(FWD) 4 302 510 400

After(AFT) 4 442 4.8

510 400 744

ATR 72 6.3 / P2


01 Jan 07

6.3.1.2 MAXIMUM GROSS WEIGHT FOR POSITIONS 6.3.1.2.1 FOR CONTAINERS

Not applicable

6.3.1.2.2 FOR PALLETS

Not applicable

6.3.2 MAXIMUM LOAD FOR ULD

Not applicable 6.3.3 LOWER DECK VERSION

Not applicable

ATR 72 6.3 / P3


01 Jan 07

Forward hold

AFT Hold

ATR 72 6.3 / P4


01 Jan 07

6.3.4 CARRIAGE OF SPECIAL LOAD 6.3.4.1 Magnetized Materials (MAG) Loading

− Not applicable. 6.3.4.2 Other special load 6.3.4.2.1 Dry Ice

− Maximum 20kg/ Flight. 6.3.4.2.2 Live animal

Ventilation system on aircraft

A/C Reg. Hold Ventilation Temperature control

FWD No No ALL

AFT No No

− Live animal : Not applicable. 6.3.4.2.3 Radioactive material

− Not applicable.

ATR 72 6.4 / P1



6.4 MAXIMUM PACKAGE & RESTRICTIONS DUE TO RESTRAINT

DEFICIENCIES 6.4.1 CARGO HOLD AND COMPARTMENT ARRANGEMENT 6.4.1.1 FORWARD HOLD

6.4.1.1.1 Allowable package sizes through FWD cargo door

Package loaded in RH

Package loaded in LH

Height (cm ) 5/143

Width (cm ) Length (cm)

5/35 180

40/50 170

40/50 180*

ATR 72 6.4 / P2



6.4.1.2 AFT HOLD

6.4.1.2.1 Allowable package sizes through AFT cargo door

6.4.2 MAXIMUM ALLOWABLE WEIGHT DUE MISSING OR INOPERATIVE

RESTRAINTS

Not applicable

ATR 72 6.5 / P1


01 Jan 07

6.5 DOOR OPERATION 6.5.1 CABIN DOOR Cabin door of ATR72 is installed as follow

Passenger door

ATR 72 6.5 / P2


01 Jan 07

ATR 72 6.5 / P3


01 Jan 07

ATR 72 6.5 / P4


01 Jan 07

6.5.2 CARGO DOOR ATR72 has 02 holds for bulk loading. Forward cargo hold is 1. AFT cargo hold is 4 .

6.5.2.1 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.

ATR 72 6.5 / P5


01 Jan 07

6.5.3 AIRCRAFT DOORS AND SYSTEMS REQUIREMENTS FOR GROUND

SERVICE EQUIPMENT 6.5.3.1 Requirement for GSE

System Requirements Notes

Electrical Type Nominal Total Power Requirement

28.5V DC

400 amp/12 kW

115V/400Hz AC

21 kVA

850 amp (for 25 sec) 1275 amp (for 5 sec)

170 lb/min 27” H2O (pressure at ground connection)

Air Conditioning

Maximum Flow Rate Maximum Output Pressure Cooling Capacity Heating Capacity

psi ton/hr

kg/cm2

kcal/sec

Pneumatic Minimum Capacity Maximum Pressure Minimum Pressure

ppm psi psi

kg/cm2

kg/cm2

Not applicable in normal operation

Potable Water Total Capacity Maximum Pressure Recommended Flow Rate

4 US gal 14 psi

gpm

15 L 1 kg/cm2

psi

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

18.5 US gal US gal US gal 14 psi

gpl 38 l/min

70 L L

9.5 L 1 kg/cm2

35 psi 2.5 kg/cm2

Max flow rate according to the neccessity

6.5.3.2 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 10.60 1.0 R 0.75 DC 2.40 0.90 R 0.85 2.

Electrical AC 2.65 0.95 R 0.85 3. Fule

Filling 21.35 0.90 L 1.65 4. Potable Water Overflow 21.45 0.90 L 1.65

Drain 21.0 0.2 L 1.30 5. Lavatory Flushing 21.10 0.15 L 1.30 6. Pneumatic Note: A: Tolet servicing connection B: Accumulator air charging C: Hydraulic power ground connection D: Hydraulic tank filling connection E: Engine oil filling connection F: Electrical ground connection

G: Pressure fueling connection H: Gravity fueling connection J: Pre-conditioning connection

ATR 72 6.5 / P6


01 Jan 07

ATR 72 6.5 / P6


01 Jan 07

ATR 72 6.5 / P7


01 Jan 07

Aircraft Servicing arrangement. (Not mandatory)

ATR 72 6.6 / P1


01 Jan 07

6.6 CARGO LOADING SYSTEM 6.6.1 CARGO HANDLING CONTROL SYSTEM

Not applicable 6.6.2 RESTRAINT SYSTEM

Forward hold

ATR 72 6.6 / P2


01 Jan 07

ooooooooooooooooooooooooooooooo




AFT hold

ATR 72 6.6 / P3


01 Jan 07

ATR 72 6.6 / P4


01 Jan 07

ATR 72 6.7 / P1


01 Jan 07

6.7 FORM 6.7.1 LOADSHEET & BALANCE FORM FOR AIRCRAFT VNB202/4/6/8/42/46

ATR 72 6.7 / P2


01 Jan 07

6.7.2 LOADSHEET & BALANCE FORM FOR AIRCRAFT VNB210/2/4

ATR 72 6.7 / P3


01 Jan 07

6.7.3 LOADSHEET & BALANCE FORM FOR AIRCRAFT VNB216

ATR 72 6.7 / P4


01 Jan 07

6.7.4 LOADING INSTRUCTION REPORT

Documents

Part B- ATR & F70- English