part b- atr & f70- english
TRANSCRIPT
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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
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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
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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
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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
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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
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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
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CHƯƠNG 5 MÁY BAY FOKKER 70
CHAPTER 5
AIRCRAFT FOKKER 70
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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
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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
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FOKKER 70 5.1 / P2
AIRCRAFT HANDLING MANUAL GENERAL Rev 06
01 Jan 07
5.1.2 EXTERIOR DIMENSION
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FOKKER 70 5.1 / P3
AIRCRAFT HANDLING MANUAL GENERAL Rev 06
01 Jan 07
5.1.3 GROUND CLEARANCE
NA
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FOKKER 70 5.1 / P4
AIRCRAFT HANDLING MANUAL GENERAL Rev 06
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.
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FOKKER 70 5.1 / P5
AIRCRAFT HANDLING MANUAL GENERAL Rev 06
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.
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FOKKER 70 5.1 / P6
AIRCRAFT HANDLING MANUAL GENERAL Rev 06
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.
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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.
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FOKKER 70 5.2 / P2
AIRCRAFT HANDLING MANUAL AIRCRAFT LIMITATIONS & FEATURES Rev 06
01 Jan 07
5.2.2 STANDARDIZED WEIGHT AND INDEX
Please refer to AHM050 validated by Flight Operation Department.
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FOKKER 70 5.2 / P3
AIRCRAFT HANDLING MANUAL AIRCRAFT LIMITATIONS & FEATURES Rev 06
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
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FOKKER 70 5.2 / P4
AIRCRAFT HANDLING MANUAL AIRCRAFT LIMITATIONS & FEATURES Rev 06
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.
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FOKKER 70 5.2 / P5
AIRCRAFT HANDLING MANUAL AIRCRAFT LIMITATIONS & FEATURES Rev 06
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
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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
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FOKKER 70 5.3 / P2
AIRCRAFT HANDLING MANUAL CARGO HOLD LIMITATIONS & VERSIONS Rev 06
01 Jan 07
5.3.2 MAXIMUM LOAD FOR ULD
Not applicable
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FOKKER 70 5.3 / P3
AIRCRAFT HANDLING MANUAL CARGO HOLD LIMITATIONS & VERSIONS Rev 06
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.
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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
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FOKKER 70 5.4 / P2
AIRCRAFT HANDLING MANUAL
MAXIMUM PACKAGE & RESTRICTIONS Rev 06 01 Jan 07 DUE TO RESTRAINT DEFICIENCIES
5.4.1.2 AFT HOLD
5.4.1.2.1 Allowable package sizes through AFT cargo door
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FOKKER 70 5.4 / P3
AIRCRAFT HANDLING MANUAL
MAXIMUM PACKAGE & RESTRICTIONS Rev 06 01 Jan 07 DUE TO RESTRAINT DEFICIENCIES
5.4.2 MAXIMUM ALLOWABLE WEIGHT DUE MISSING OR INOPERATIVE RESTRAINTS
Not applicable
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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
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FOKKER 70 5.5 / P2
AIRCRAFT HANDLING MANUAL DOOR OPERATION Rev 06
01 Jan 07
Service door
Emergency Exit
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FOKKER 70 5.5 / P3
AIRCRAFT HANDLING MANUAL DOOR OPERATION Rev 06
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.
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FOKKER 70 5.5 / P4
AIRCRAFT HANDLING MANUAL DOOR OPERATION Rev 06
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
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FOKKER 70 5.5 / P5
AIRCRAFT HANDLING MANUAL DOOR OPERATION Rev 06
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
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FOKKER 70 5.5 / P6
AIRCRAFT HANDLING MANUAL DOOR OPERATION Rev 06
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
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FOKKER 70 5.5 / P7
AIRCRAFT HANDLING MANUAL DOOR OPERATION Rev 06
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
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FOKKER 70 5.5 / P8
AIRCRAFT HANDLING MANUAL DOOR OPERATION Rev 06
01 Jan 07
5.5.3.4 Aircraft Servicing arrangement. (not madatory)
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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
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FOKKER 70 5.6 / P2
AIRCRAFT HANDLING MANUAL CARGO LOADING SYSTEM Rev 06
01 Jan 07
AFT hold
oo o oo oo oo oo oo oo
oo o oo oo oo oo oo oo
Tied down point
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FOKKER 70 5.7 / P1
AIRCRAFT HANDLING MANUAL FORM Rev 06
01 Jan 07
5.7 FORM 5.7.1 LOADSHEET
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FOKKER 70 5.7 / P2
AIRCRAFT HANDLING MANUAL FORM Rev 06
01 Jan 07
5.7.2 BALANCE CHART
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FOKKER 70 5.7 / P3
AIRCRAFT HANDLING MANUAL FORM Rev 06
01 Jan 07
5.7.3 LOADING INSTRUCTION REPORT (LIR)
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CHƯƠNG 6 MÁY BAY ATR72
CHAPTER 6
AIRCRAFT ATR72
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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
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ATR 72 6.1 / P1
AIRCRAFT HANDLING MANUAL GENERAL Rev 06
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
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ATR 72 6.1 / P2
AIRCRAFT HANDLING MANUAL GENERAL Rev 06
01 Jan 07
6.1.2 EXTERIOR DIMENSION
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ATR 72 6.1 / P3
AIRCRAFT HANDLING MANUAL GENERAL Rev 06
01 Jan 07
6.1.3 GROUND CLEARANCE
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ATR 72 6.1 / P4
AIRCRAFT HANDLING MANUAL GENERAL Rev 06
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.
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ATR 72 6.1 / P5
AIRCRAFT HANDLING MANUAL GENERAL Rev 06
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
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ATR 72 6.1 / P6
AIRCRAFT HANDLING MANUAL GENERAL Rev 06
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.
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ATR 72 6.2 / P1
AIRCRAFT HANDLING MANUAL AIRCRAFT LIMITATIONS & FEATURES Rev 06
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.
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ATR 72 6.2 / P2
AIRCRAFT HANDLING MANUAL AIRCRAFT LIMITATIONS & FEATURES Rev 06
01 Jan 07
6.2.2 STANDARDIZED WEIGHT AND INDEX
Please refer to AHM050 validated by Flight Operation Department.
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ATR 72 6.2 / P3
AIRCRAFT HANDLING MANUAL AIRCRAFT LIMITATIONS & FEATURES Rev 06
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
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ATR 72 6.2 / P4
AIRCRAFT HANDLING MANUAL AIRCRAFT LIMITATIONS & FEATURES Rev 06
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.
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ATR 72 6.2 / P5
AIRCRAFT HANDLING MANUAL AIRCRAFT LIMITATIONS & FEATURES Rev 06
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
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ATR 72 6.3 / P1
AIRCRAFT HANDLING MANUAL CARGO HOLD LIMITATIONS & VERSIONS Rev 06
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
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ATR 72 6.3 / P2
AIRCRAFT HANDLING MANUAL CARGO HOLD LIMITATIONS & VERSIONS Rev 06
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
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ATR 72 6.3 / P3
AIRCRAFT HANDLING MANUAL CARGO HOLD LIMITATIONS & VERSIONS Rev 06
01 Jan 07
Forward hold
AFT Hold
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ATR 72 6.3 / P4
AIRCRAFT HANDLING MANUAL CARGO HOLD LIMITATIONS & VERSIONS Rev 06
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.
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ATR 72 6.4 / P1
AIRCRAFT HANDLING MANUAL
MAXIMUM PACKAGE & RESTRICTIONS Rev 06 01 Jan 07 DUE TO RESTRAINT DEFICIENCIES
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*
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ATR 72 6.4 / P2
AIRCRAFT HANDLING MANUAL
MAXIMUM PACKAGE & RESTRICTIONS Rev 06 01 Jan 07 DUE TO RESTRAINT DEFICIENCIES
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
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ATR 72 6.5 / P1
AIRCRAFT HANDLING MANUAL DOOR OPERATION Rev 06
01 Jan 07
6.5 DOOR OPERATION 6.5.1 CABIN DOOR Cabin door of ATR72 is installed as follow
Passenger door
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ATR 72 6.5 / P2
AIRCRAFT HANDLING MANUAL DOOR OPERATION Rev 06
01 Jan 07
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ATR 72 6.5 / P3
AIRCRAFT HANDLING MANUAL DOOR OPERATION Rev 06
01 Jan 07
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ATR 72 6.5 / P4
AIRCRAFT HANDLING MANUAL DOOR OPERATION Rev 06
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.
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ATR 72 6.5 / P5
AIRCRAFT HANDLING MANUAL DOOR OPERATION Rev 06
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
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ATR 72 6.5 / P6
AIRCRAFT HANDLING MANUAL DOOR OPERATION Rev 00
01 Jan 07
ATR 72 6.5 / P6
AIRCRAFT HANDLING MANUAL DOOR OPERATION Rev 00
01 Jan 07
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ATR 72 6.5 / P7
AIRCRAFT HANDLING MANUAL DOOR OPERATION Rev 00
01 Jan 07
Aircraft Servicing arrangement. (Not mandatory)
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ATR 72 6.6 / P1
AIRCRAFT HANDLING MANUAL CARGO LOADING SYSTEM Rev 06
01 Jan 07
6.6 CARGO LOADING SYSTEM 6.6.1 CARGO HANDLING CONTROL SYSTEM
Not applicable 6.6.2 RESTRAINT SYSTEM
Forward hold
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ATR 72 6.6 / P2
AIRCRAFT HANDLING MANUAL CARGO LOADING SYSTEM Rev 06
01 Jan 07
ooooooooooooooooooooooooooooooo
ooooooooooooooooooooooooooooooo
ooooooooooooooooooooooooooooooo
ooooooooooooooooooooooooooooooo
AFT hold
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ATR 72 6.6 / P3
AIRCRAFT HANDLING MANUAL CARGO LOADING SYSTEM Rev 06
01 Jan 07
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ATR 72 6.6 / P4
AIRCRAFT HANDLING MANUAL CARGO LOADING SYSTEM Rev 06
01 Jan 07
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ATR 72 6.7 / P1
AIRCRAFT HANDLING MANUAL FORM Rev 06
01 Jan 07
6.7 FORM 6.7.1 LOADSHEET & BALANCE FORM FOR AIRCRAFT VNB202/4/6/8/42/46
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ATR 72 6.7 / P2
AIRCRAFT HANDLING MANUAL FORM Rev 06
01 Jan 07
6.7.2 LOADSHEET & BALANCE FORM FOR AIRCRAFT VNB210/2/4
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ATR 72 6.7 / P3
AIRCRAFT HANDLING MANUAL FORM Rev 06
01 Jan 07
6.7.3 LOADSHEET & BALANCE FORM FOR AIRCRAFT VNB216
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ATR 72 6.7 / P4
AIRCRAFT HANDLING MANUAL FORM Rev 06
01 Jan 07
6.7.4 LOADING INSTRUCTION REPORT