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Gulfstream G100

Specifications

Airframe

Total time
3,868 hr

Performance (across variants)

Range
2,720 nm
Cruise
396 kt
Service ceiling
45,000 ft
MTOW
10,600 kg

Description

This Gulfstream G100 aircraft has flown a total of 3868 hours and has completed 2577 landings. It features Honeywell TFE 731-40R-200G engines. The left engine, with serial number P-113242, has 3848 hours total, while the right engine, with serial number P-113243, has 3821 hours total. The auxiliary power unit is a Honeywell GTCP 36-150(W) with serial number P-669, totaling 2036 hours. The avionics suite includes a Collins Pro Line 4 system with a 4-tube EFIS, dual Collins RTU-4220 radio tuning units, dual Collins VHF-422D comms, dual Collins VIR-432 navs, dual Collins DME-442 DMEs, dual Collins HF-9000 HF comms, dual Collins ADF-462 ADFs, dual Universal UNS-1EW FMS (WAAS/LPV), dual Collins TDR-94D transponders, a Collins TWR-850 weather radar, a Collins ALT-55B radio altimeter, dual Collins ADC-850C air data systems, dual Collins AHC-85E AHRS computers, a Honeywell Laseref V inertial reference unit, a Collins TTR-920 TCAS II with Change 7.0, a Honeywell MK V EGPWS, a Collins APS-85 autopilot, an Aero M satellite phone, Aviator 300 SwiftBroadband Wi-Fi, a Universal UL-601 UniLink AFIS, an AvtechTyee CSD-10 SELCAL, a Collins DBU-4000 database unit, a Collins DAU-4002 data acquisition unit, a Universal CVR-120 cockpit voice recorder, a digital flight data recorder, and an Artex C406-2 emergency locator transmitter. Additional features include Canadian mods, JSSI engine program ($347.01/hour/engine), JSSI APU program ($19,361.09 annual fee), a 15.1" LCD flip-out monitor, Airshow 4000 system, DVD/CD player, microwave oven, dual Davtron M850A digital clocks, crew Eros oxygen masks, Precise Flight Pulselite system, tail logo lights, and long-range fuel tanks. There is no known damage history, and the aircraft is on a G-CMP maintenance program. The 1C inspection is due 01/31/24. Weights include a maximum ramp weight of 24,800 lbs, maximum take-off weight of 24,650 lbs, maximum landing weight of 20,700 lbs, maximum zero fuel weight of 17,000 lbs, basic operating weight of 14,440 lbs, and usable fuel of 8,692 lbs (9,365 lbs with extension tanks).

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Type certification

The FAA paperwork

TCDS A16NM · 6 · issued 2002-08-09

The FAA-issued Type Certificate for this model is on file (TCDS A16NM), but we haven't yet extracted the structured spec values.

Read the TCDS (PDF) →
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