Page: 1 Ground Handling Manual Chapter: 1 Re-issue 2,Rev. 5 Aircraft Presentations 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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Page: 3 Ground Handling Manual Chapter: 1 Re-issue 2,Rev. 6 Aircraft Presentations 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 Page: 4 Chapter: 1 Ground Handling Manual Re-issue 2,Rev.2 Date: 16/04/2010 Aircraft Presentations
1.1.1.3 G550 500 Gulfstream Road Savannah,GA 31408 Manufacturer USA
Passenger Capacity VIP 18 2 Flight Deck Crew, Crew Capacity 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 500 Gulfstream Road Savannah,GA 31408 Manufacturer 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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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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1.1.2 Exterior Dimensions
1.1.2.1 B757- 200
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1.1.2.2 B737-300
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1.1.2.3 G550
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1.1.2.4 G450
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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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1.1.2.6 Global Express XRS (BD-700)
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1.1.3 Cabin Layout 1.1.3.1 B757-200
Gain Jet B757-200 (78 VIP seats)
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1.1.3.2 B737-300
BOEING 737-300 ( VIP 48 Seats )
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1.1.3.3 G550
Gulfstream G 550 (18 VIP seats)
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1.1.3.4 G450
Gulfstream G 450 (14 VIP seats)
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1.1.3.5 G200
Gulfstream G 200 (10 VIP seats)
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1.1.3.6 Global Express XRS
BD – 700 (15 VIP Seats)
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1.1.4 Ground Service Equipment
BUS CREW/PAX
H/LOADER FOR WCHR’s
SI:VEHICLES APROVED BY THE HANDLING AGENT FOR ASSISTANCE DURING GROUND HANDLING
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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 compartments. FWD Hold = CPT 1 and 2, and AFT hold = Cpt 3 and 4. CPT 1 CPT 2 CPT 3 CPT 4 Capacity: 2469 kg 4672 kg 3773 kg 5606kg Volume: Fw d: 19,8 m 3 Aft: 31 m 3 Combined load limitations: Cpt 1 and 2 = 4672 kg FWD HOLD , Cpt 1 and 2 Cpt 3 and 4 = 7393 kg
Cpt 1
Cpt 2
AFT HOLD, Cpt 3 and 4
Cpt 3
Cpt 4
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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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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) .
Page: 22 Chapter: 1 Ground Handling Manual Re-issue 2,Rev. 2 Date: 16/04/2010 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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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: Max floor load Max floor load Description Max cap, LBS Max cap, Kg 2 2 lbs/ft kg/m 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
Page: 24 Chapter: 1 Ground Handling Manual Re-issue 2,Rev. 5 Date: 25/01/2011 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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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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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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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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Page: 29 Ground Handling Manual Chapter: 1 Re-issue 2,Rev. 3 Aircraft Presentations Date: 06/09/2010
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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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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1.1.6.6 Global Express XRS (BD-700)
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1.1.7 Package size dimension charts 1.1.7.1 B757 - 200
Page: 37 Ground Handling Manual Chapter: 1 Re-issue 2,Rev. 5 Aircraft Presentations 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 Quantity of Dimensions in cm Baggages in pieces 20x20x20 380 30x30x30 100 40x40x40 40 50x50x50 20 60x60x60 10 70x70x70 6 80x80x80 4
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