Gulfstream G200 (Private Plane)

2001 - Gulfstream G200

   

https://www.avbuyer.com/aircraft/private-jets/gulfstream/g200/364368

Aircraft Description:

AIRFRAME / ENGINES / APU / WEIGHT / TOTAL LANDING
AIRFRAME
C of A Date: February 23, 2001
Total Hours: 7,224.6
Total Landings: 3823
Location: Lima, Peru
Previously EASA (PH-YMA)
Previously N (N108SC)
ENGINES
Pratt & Whitney PW306A

Engine #1
Serial Numbers: PCE-CC0068
Total Hours: 6,927.7
Total Cycles: 3682

Engine #2
Serial Numbers: PCE-CC0067
Total Hours: 6,993
Total Cycles: 3704

Engines enrolled on Pratt & Whitney ESP Gold Program
APU
HONEYWELL GTCP36-150
SERIAL NUMBER: P-134
TOTAL HOURS: 4,089
TOTAL CYCLES: 5,389
APU ENROLLED ON HONEYWELL MSP PROGRAM
WEIGHTS
Basic Empty Weight (B.E.W): 20,490 lbs
Max Take-off Weight (M.T.O.W): 35,450 lbs
Max Zero Fuel Weight (M.Z.F.W): 24,000 lbs

    AVIONICS & CONNECTIVITY
    Collins Proline 4 Avionics Suite
    Dual Universal UNS-1C+ FMS (Including GPS)
    Dual Garmin GTX-3000 Transponders (STC ST04021AT-D)
    Dual Collins VHF-422D VHF
    Dual Bendix King HF
    Single Collins ADF-462
    Dual Collins DME-442 DME
    Honeywell MARK V EGPWS
    Collins ALT-4000 Radio Altimeter
    Collins TRA-858 WX Radar
    Honeywell TTR-4000 TCAS II 7.0
    Dual Collins VIR-432 VOR
    Universal CVR-120 CVR
    Honeywell AR-256 FDR
    Artex C406-2 ELT
    Interior & Entertainment
    Refurbished 2008. 10 passenger configuration having forward galley, forward 4-place club seating, aft 4-place conference group opposite a 3-place divan. Divan is certified for two occupants during take-off and landing.
    Airshow 4000, 2 DVD, 12 CD Changer/Player, 14.5″ Monitor At Fwd Bulkhead, 14.5″ Monitor At Aft Bulkhead, TIA Coffee Maker, TIA Flight Oven, Single AirCell ST3100 Satellite Telephone System.
    EXTERIOR
    Matterhorn White with Blue Markings

Falcon 900LX ( Private Jet )

 

Falcon 900XL (Bought by Bram- private plane, new):

Falcon 900XL

https://www.dassaultfalcon.com/en/Aircraft/Models/900LX/Pages/overview.aspx


The reimagined Falcon 900LX features a highly refined cabin that brilliantly answers the needs of any business traveler. No detail has been overlooked, from the shape of the credenza to the style of the seats, to create an enhanced difference in comfort, convenience and connectivity. Advanced acoustic technology makes this the quietest cabin in the 900 series. And with room enough for three separate lounge areas, passengers can work, relax over a fine meal, then retire to sleep as they travel to their next destination.

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Cabin: THE SUPERIOR COMFORTS OF QUALITY.
Cabin Length*:   33 ft 2 in   10.11 m
Cabin Height:   6 ft 2 in   1.88 m
Cabin Width:   7 ft 8 in   2.34 m
Cabin Volume*:   1,264 ft3   35.8 m3

*excluding flight deck and baggage

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The Falcon 900LX is powered by three Honeywell TFE731-60 engines. Reliable and time-tested, these engines deliver more power with lower fuel consumption, and require less maintenance.

POWERFUL AND PROVEN

Each of the engines that power the 900LX produces 5,000 pounds (22.25 kN) of thrust at sea level up to ISA +17°C and provides unbeatable efficiency in this power range, along with a reputation for low fuel consumption and quiet operation. With more than 11,000 engines entered into service and 100 million hours of operation logged, the reliability and fuel-efficient performance of the TFE731 series are well proven.

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The 900LX has a maximum range of 4,750 nm (8,800 km) and a maximum speed of Mach .84. It can take you from Geneva to Chicago, Mumbai to London City or Hong Kong to Sydney, nonstop, while consuming far less fuel than its competitors. In addition to airfield agility, the hallmark of trijet design, the 900LX allows more direct, over-water routing, an advantage that saves both time and fuel, while also enhancing safety.

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 Imperial Metric
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Performance
Range at Mach 0.80 (6 passengers; 2 crew)
   
4,750 nm
Maximum operating speed (VMO)
   
370/350 kias
Maximum operating mach number (MMO)
   
Mach .87 / .84
Takeoff distance (sea level - isa, max take off weight)
   
5,360 ft
Approach speed (typical landing weight)
   
110 kias
Maximum certificated altitude
   
51,000 ft
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External dimensions
Length
   
66.4 ft
Height
   
25.2 ft
Wing span
   
70.2 ft
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Internal dimensions
Cabin length (excluding cockpit and baggage)
   
33.2 ft
Maximum headroom
   
74.00 in
Maximum width
   
92.00 in
Cabin volume (excluding cockpit and baggage)
   
1,264 cu ft
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Weights
Maximum takeoff weight
   
49,000 lb
Maximum zero fuel weight
   
30,864 lb
Maximum fuel
   
20,905 lb
Maximum landing weight
   
44,500 lb