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Ground Handling Manual
Aircraft Presentations
Page: 1 Chapter: 1 Re-issue 2,Rev. 5 Date: 25/01/2011
1.0 Contents
1.0 Contents ................................................................................................................................................................... 1
1.1 Aircraft Presentation – General ............................................................................................................................. 3
1.1.1 Aircraft Presentation........................................................................................................................................... 3
1.1.1.1 B757-200 ......................................................................................................................................................... 3
1.1.1.2 B737-300 ......................................................................................................................................................... 3
1.1.1.3 G550 ................................................................................................................................................................ 4
1.1.1.4 G450 ................................................................................................................................................................ 4
1.1.1.5 G200 ................................................................................................................................................................ 4
1.1.1.6 Global Express XRS ( BD-700) ....................................................................................................................... 5
1.1.2 Exterior Dimensions ........................................................................................................................................... 6
1.1.2.1 B757- 200 ........................................................................................................................................................ 6
1.1.2.2 B737-300 ......................................................................................................................................................... 7
1.1.2.3 G550 ................................................................................................................................................................ 8
1.1.2.4 G450 ................................................................................................................................................................ 9
1.1.2.5 G200 .............................................................................................................................................................. 10
1.1.2.6 Global Express XRS (BD-700) ...................................................................................................................... 11
1.1.3 Cabin Layout .................................................................................................................................................... 12
1.1.3.1 B757-200 ....................................................................................................................................................... 12
1.1.3.2 B737-300 ....................................................................................................................................................... 13
1.1.3.3 G550 .............................................................................................................................................................. 14
1.1.3.4 G450 .............................................................................................................................................................. 15
1.1.3.5 G200 .............................................................................................................................................................. 16
1.1.3.6 Global Express XRS ...................................................................................................................................... 17
1.1.4 Ground Service Equipment .............................................................................................................................. 18
1.1.5 Cargo Compartments ........................................................................................................................................ 19
1.1.5.1 B757 -200 ...................................................................................................................................................... 19
1.1.5.2 B737-300 ....................................................................................................................................................... 20
1.1.5.3 G550 .............................................................................................................................................................. 21
1.1.5.4 G450 .............................................................................................................................................................. 22
1.1.5.5 G200 .............................................................................................................................................................. 23
1.1.5.6 EMB500 ......................................................................................................................................................... 24
1.1.5.7 Load and Loading Restrictions ...................................................................................................................... 25
1.1.5.8 Ground Stability ............................................................................................................................................. 26
� B757- 200 & B737-300 ................................................................................................................................. 26
1.1.6 Thrust Management .......................................................................................................................................... 27
1.1.6.1 B757- 200 ...................................................................................................................................................... 27
1.1.6.2 B737-300 ....................................................................................................................................................... 29
1.1.6.3 G550 .............................................................................................................................................................. 31
1.1.6.4 G450 .............................................................................................................................................................. 33
1.1.6.5 G200 .............................................................................................................................................................. 34
1.1.6.6 Global Express XRS (BD-700) ...................................................................................................................... 35
1.1.7 Package size dimension charts ......................................................................................................................... 36
1.1.7.1 B757 - 200 ..................................................................................................................................................... 36
1.1.7.2 B737 - 200 ..................................................................................................................................................... 37
1.1.7.3 G550 & G450 & G200 ................................................................................................................................... 37
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Ground Handling Manual
Aircraft Presentations
Page: 3 Chapter: 1 Re-issue 2,Rev. 6 Date: 30/11/2011
1.1 Aircraft Presentation – General
Gain Jet operates presently the following aircraft:
Aircraft Type Version Registration
Boeing B757-200 VIP 78 SX - RFA
Boeing B737-300 VIP 48 SX - MTF
Gulfstream G550 VIP 18 SX- GJJ
Gulfstream G450 VIP 14 SX-GAB
Gulfstream G200 VIP 10 SX-IDA ,SX–IFB,.SX-TAJ
Global Experss XRS VIP 15 SX-GJN
1.1.1 Aircraft Presentation 1.1.1.1 B757-200
Manufacturer Boeing Company
P.O.Box 3707,Seattle
Washington 98124, UAS
Passenger Capacity VIP 78
Crew Capacity 4 Flight Deck Crew
7 Cabin Crew
Engines Rolls-Royce RB211 – 535E4
Speed M 0,80 TAS 440 kts
Range 4000NM
Maximum Take Off Weight 220.000 Lbs / 99.790 Kgs
1.1.1.2 B737-300
Manufacturer Boeing Company
P.O.Box 3707,Seattle
Washington 98124, UAS
Passenger Capacity VIP 48
Crew Capacity 4 Flight Deck Crew
4 cabin crew
Engines CFM56-3B2
Speed M 0,75 TAS 420 kts
Range 2.300 NM
Maximum Take Off Weight 63.276 kgr
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Ground Handling Manual
Aircraft Presentations
1.1.1.3 G550
Manufacturer
500 Gulfstream Road
Savannah,GA 31408
USA
Passenger Capacity VIP 18
Crew Capacity 2 Flight Deck Crew,
1 cabin crew
Engines BR700-710C4-11
Speed M 0,80 TAS 460 kts
Range 6750 NM
Maximum Take Off Weight 91.000 Lbs
1.1.1.4 G450
Manufacturer
500 Gulfstream Road
Savannah,GA 31408
USA
Passenger Capacity VIP 14
Crew Capacity 2 Flight Deck Crew,
1 cabin crew
Engines ROLLS ROYCE TAY 611-8C
Speed M 0,80 TAS 460 kts
Range 3 NM
Maximum Take Off Weight 74.600 LBS
1.1.1.5 G200
Manufacturer Gulfstream Aerospace,
7440 Aviation Place,
Dallas, Texas 75235
Passenger Capacity VIP 10
Crew Capacity 2 Flight Deck Crew
1 cabin crew
Engines Pratt & Whitney PW 306A
Speed M 0,75 TAS 410 kts
Range 3500 NM
Maximum Take Off Weight 35.450 LBS
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Ground Handling Manual
Aircraft Presentations
Page: 5 Chapter: 1 Re-issue 2,Rev. 5 Date: 25/01/2011
1.1.1.6 Global Express XRS ( BD-700)
Manufacturer Bombardier INC PO Box 6087 Station Centre –Villle Montreal Quelen , Canada H3C 3G9l
Passenger Capacity VIP15
Crew Capacity 02 Flight Deck Crew
Engines BR700-710A2-20
Speed M 0,89 TAS 500 kts
Range 5000 NM
Maximum Take Off Weight 42.415 kgr
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Ground Handling Manual
Aircraft Presentations
1.1.2 Exterior Dimensions
1.1.2.1 B757- 200
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Aircraft Presentations
Page: 7 Chapter: 1 Re-issue 2,Rev. 3 Date: 06/09/2010
1.1.2.2 B737-300
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Ground Handling Manual
Aircraft Presentations
1.1.2.3 G550
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Aircraft Presentations
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1.1.2.4 G450
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Ground Handling Manual
Aircraft Presentations
1.1.2.5 G200
Overall exterior height—21 feet 5 inches Tail spar—22 feet 6 inches Cabin height—6 feet 3 inches Cabin length (cockpit divider to aft pressure bulkhead)—24 feet 5 inches Cabin width—7 feet 2 inches Cockpit length—6 feet 1 inch Cockpit width—7 feet 2 inches Cabin door height—6 feet 0 inches Cabin entrance door width—2 feet 9 inches Passenger cabin volume—868 cubic feet External baggage compartment volume—125 cubic feet and 1,980 pounds
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Aircraft Presentations
Page: 11 Chapter: 1 Re-issue 2,Rev.5 Date: 25/01/2011
1.1.2.6 Global Express XRS (BD-700)
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Ground Handling Manual
Aircraft Presentations
1.1.3 Cabin Layout 1.1.3.1 B757-200
Gain Jet
Ground Handling Manual
Aircraft Presentations
Gain Jet B757-200 (78 VIP seats)
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Aircraft Presentations
Page: 13 Chapter: 1 Re-issue 2,Rev.3 Date: 06/09/2010
1.1.3.2 B737-300
BOEING 737-300 ( VIP 48 Seats )
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Ground Handling Manual
Aircraft Presentations
1.1.3.3 G550
Gulfstream G
Ground Handling Manual
Aircraft Presentations
ulfstream G 550 (18 VIP seats)
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Aircraft Presentations
Page: 15 Chapter: 1 Re-issue 2,Rev.2 Date: 16/04/2010
1.1.3.4 G450
Gulfstream G 450 (14 VIP seats)
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Ground Handling Manual
Aircraft Presentations
1.1.3.5 G200
Gulfstream G 200 (10 VIP seats)
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Aircraft Presentations
Page: 17 Chapter: 1 Re-issue 2,Rev.5 Date: 25/01/2011
1.1.3.6 Global Express XRS
BD – 700 (15 VIP Seats)
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Ground Handling Manual
Aircraft Presentations
1.1.4 Ground Service Equipment
SI:VEHICLES APROVED BY THE HANDLING AGENT FOR ASSISTANCE DURING GROUND HANDLING
BUS CREW/PAX
Ground Handling Manual
Aircraft Presentations
APROVED BY THE HANDLING AGENT FOR ASSISTANCE DURING GROUND HANDLING
H/LOADER FOR WCHR’s
BUS CREW/PAX
APROVED BY THE HANDLING AGENT FOR ASSISTANCE DURING GROUND HANDLING
H/LOADER FOR WCHR’s
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1.1.5 Cargo Compartments
1.1.5.1 B757 -200
There are two cargo holds in the aircraft and each hold is divided into two
FWD Hold = CPT 1 and 2, and AFT hold = Cpt 3 and 4.
CPT 1
Capacity: 2469 kg
Volume: Fwd: 19,8 m
Combined load limitations: Cpt 1 and 2 = 4672 kg
FWD HOLD , Cpt 1 and 2
Cpt 3 and 4 = 7393 kg
AFT
Ground Handling Manual
Aircraft Presentations
two cargo holds in the aircraft and each hold is divided into two compartments.
FWD Hold = CPT 1 and 2, and AFT hold = Cpt 3 and 4.
CPT 2 CPT 3
4672 kg 3773 kg
d: 19,8 m3
Aft: 31 m3
Cpt 1 and 2 = 4672 kg
Cpt 3 and 4 = 7393 kg
HOLD, Cpt 3 and 4
Cpt 2
Cpt 1
Cpt 4
Cpt 3
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compartments.
CPT 4
5606kg
HOLD, Cpt 3 and 4
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Ground Handling Manual
Aircraft Presentations
1.1.5.2 B737-300
There are two cargo holds/compartments in the aircraft.
FWD Hold = CPT 1, and AFT hold = Cpt 4.
CPT 1 CPT 4
Capacity: 2269 kg 3469 kg
Volume: Fwd: 12,03 m3 Aft: 18,3 m3
FWD HOLD , Cpt 1
AFT HOLD, Cpt 4
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Aircraft Presentations
Page: 21 Chapter: 1 Re-issue 2,Rev. 1 Date: 15/05/2009
1.1.5.3 G550 There is one cargo compartment aft in the aircraft. The compartment is available both through the external door and from inside of the aircraft (up to 40000ft).
CPT 6
Capacity: 1900 Lb
Door opening: 91,4 x 96,5 cm (36 x 38 inch)
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Ground Handling Manual
Aircraft Presentations
1.1.5.4 G450
There is one cargo compartment aft in the aircraft. The compartment is available both through the external door and from inside of the aircraft (up to 40000ft).
CPT 6 Capacity: 950 Lb Volume: 4,78 m
3
Door opening: 101,6 x 89,5 cm (40 x 35,25 inch) .
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Page: 23 Chapter: 1 Re-issue 2,Rev.1 Date: 15/05/2009
1.1.5.5 G200
A pressurized, heated, lockable, lighted baggage compartment (next figure) is located in the center fuselage, aft of the fuselage tank. The compartment is lined with fibreglass overlaid with electric heating panels to maintain a uniform temperature.The compartment design allows complete baggage loading by one crewmember. Internal shelving allows baggage loading at the top of the compartment, leaving space for additional bag-gage on the floor.A cargo net prevents cargo from shifting.Cargo is loaded from the left exterior of the air-plane through a door (approximately 35 inches high by 35 inches wide) or (0,89m x 0,89m). The cargo door hinges downward with interior airstairs for easy access. The door handle must be stowed for the aircraft to pressurize.
Cargo Net must be arranged to provide restraint in all directions.
Specifications of the only one baggage compartment in G200 are:
Description Max cap, LBS Max cap, Kg Max floor load
lbs/ft2
Max floor load kg/m
2
Baggage Compartment 1,980 898 126 615
Note: If the baggage compartment interior is not installed (Mod 7074), the baggage compartment is not eligible for use. With Mod 7266 installed, the baggage compartment is eligible for use
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Ground Handling Manual
Aircraft Presentations
1.1.5.6 Global Expess XRS ( BD – 700 )
Description of Baggage Compartment
There is one cargo compartment aft in the aircraft. The compartment is available both through the external door and from inside of the aircraft (up to 40000ft).
CPT 6
Capacity: 900 Lb
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Page: 25 Chapter: 1 Re-issue 2,Rev.5 Date: 25/01/2011
1.1.5.7 Load and Loading Restrictions
���� B757
A careful planning of all activities must be made.
1. All goods must be inspected for leakage or otherwise damaged shipments.
2. All goods must be labelled clearly indicating point of unloading.
3. Mail should not be mixed with cargo.
4. The goods must be properly secured to prevent shifting while the aircraft is in flight.
The cargo must be inspected and properly distributed to avoid concentrated weight loads that may damage the aircraft floor structure. It is also important that the aircraft is not damaged by ground equipment while the loading is taking place.
���� B737
A careful planning of all activities must be made.
- All goods must be inspected for leakage or otherwise damaged shipments.
- All goods must be labelled clearly indicating point of unloading.
- Mail should not be mixed with cargo.
���� G550 & G450
The cargo compartment,also referred to as baggage compartment, is located aft of the aircraft passenger compartment.Access is from the passenger compartment through a sliding door or the aircraft exterior via a slide up cargo door. The cargo compartment houses equipment racks and a water storage tank.It is also equipped with cargo nets and lifting devices
���� G200
1. Whenever the maximum area load is exceeded, the weight must be distributed over a larger area to avoid damage to the aircraft structure underneath the floor (beams, cross beams etc.).
2. Load passengers, baggage and cargo ,ensuring forward or aft cg limits are not exceeded
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Aircraft Presentations
1.1.5.8 Ground Stability
���� B757- 200 & B737-300
All individual items, which by nature, shape or density may constitute a hazard, shall be lashed. Pieces weighing 330Lbs or 150kgs or more, when loaded as bulk in lower compartments should be tied down except when the compartment is volumetrically full. Compartments, which are filled up to three-quarters, are considered to be volumetrically full.
Particular attention must be given to lashing of Dangerous Goods. In general, all packages containing Dangerous Goods must be stowed in an upright position if so indicated, have the Hazard label visible, and they must be lashed to prevent themselves from shifting or any crushing, tipping or damage by other load.
���� G550 & G450
An equipment rack is installed on forward right side of baggage compartment. Enclosed in cabinetry,the rack contains multiple shelves equipped with mounting trays for installation of electronic components .A fan is installed to provide cooling air. A shelf assembly for mounting of the conformal water tank is located on the aft right side of the compartment.
���� G200
When loading baggage in excee of 440 lb,without passengers , crew and fuel ,ensure that ground handling aft cg limit of 445.787in(50% MAC)is not exceeded.
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Page: 27 Chapter: 1 Re-issue 2,Rev. 1 Date: 15/05/2009
1.1.6 Thrust Management
1.1.6.1 B757- 200
Reverse thrust shall normally not be used during ground operation, as there is a potential hazard for FOD at low speeds (below 60 kt IAS) even at idle reverse Handling of throttles during ground operation demands sound judgement and technique. The jet blast can cause damage and injuries even at low thrust settings. Aircraft response to throttle movement is slow, particularly at high gross weight
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1.1.6.2 B737-300
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1.1.6.3 G550
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1.1.6.4 G450
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Aircraft Presentations
1.1.6.5 G200
Reverse thrust shall normally not be used during ground operation, as there is a potential hazard for FOD at low speeds (below 60 kt IAS) even at idle reverse Handling of throttles during ground operation demands sound judgement and technique. The jet blast can cause damage and injuries even at low thrust settings. Aircraft response to throttle movement is slow, particularly at high gross weight.
• Jet blast effect area
To initiate taxiing, advance throttles slowly to not more than approximately 65% N2.
After aircraft is in motion, idle thrust will normally cause aircraft to accelerate, therefore periodic braking may be required.
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Page: 35 Chapter: 1 Re-issue 2,Rev. 5 Date: 25/01/2011
1.1.6.6 Global Express XRS (BD-700)
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Ground Handling Manual
Aircraft Presentations
1.1.7 Package size dimension charts 1.1.7.1 B757 - 200
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Aircraft Presentations
Page: 37 Chapter: 1 Re-issue 2,Rev. 5 Date: 25/01/2011
1.1.7.2 B737 - 200
1.1.7.3 G550 & G450 & G200 & BD-700
Approximate quantity of baggages according their size:
Baggage Dimensions in cm
Quantity of Baggages in pieces
20x20x20 380
30x30x30 100
40x40x40 40
50x50x50 20
60x60x60 10
70x70x70 6
80x80x80 4
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