N100GX2007 IAI GULFSTREAM G150
Safety record in brief:No NTSB accidents or incidents since 198211 ADs may apply1 service difficulty report
Registration
FAA Aircraft Registry · Oct 18, 2026- Registered owner
- Brulecreek Aviation LLC
- Owner type
- LLC
- City, state
- Park City, UT
- Certificate issued
- Feb 5, 2019
- Expires
- Feb 28, 2029
- Airworthiness
- Standard · Transport
- Airworthiness date
- May 3, 2016
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Airframe & engine
FAA Registry + type dataAirframe
- Manufacturer
- IAI
- Model
- GULFSTREAM G150
- Year
- 2007
- Serial number
- 228
- Aircraft type
- Fixed wing multi engine
- Category
- Land
- Certification
- Type Certificated
- Seats
- 11
- Engines
- 2
- Max takeoff weight
- 20,000 and over lb
- Mode S code
- A00560
Engine
- Make and model
- Honeywell Tfe731-40ar
- Type
- Turbo-fan
- Power
- 4,420 lb thrust
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 2019 – nowBrulecreek Aviation LLCPark City, UT · current
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 18, 2026 · SDRs · Oct 16, 2026NTSB events (0)
No NTSB accidents or incidents found for this airframe since 1982.
Accident history for this modelADs published since 1998 that may apply (11)
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2026-18-06 | Time limits/ Maintenance checks | Oct 16, 2026 | Airframe (GULFSTREAM G150) |
| 2019-05-07 | Turbine Engine Compressor Section | Apr 25, 2019 | Engine (TFE731-40AR)Serial numbers per Table 9 of Honeywell Service Bulletin TFE731-72-5256, Revision 0. Only with: Fan disk P/N 3060287-2 with S/N listed in Table 9 of the SB, without "T43374" marked adjacent to the fan disk P/N or S/N. |
| 2019-03-13 | Electrical power | Apr 8, 2019 | Airframe (GULFSTREAM G150)Certain serial numbers: 201–326 |
| 2017-21-04 | Doors | Nov 27, 2017 | Airframe (GULFSTREAM G150)Certain serial numbers: 201–318 |
| 2014-15-19 | Operations information | Oct 14, 2014 | Airframe (GULFSTREAM G150) |
Show all 11 ADsShow fewer ADs
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2014-12-52 | Honeywell International Inc. (Type Certificate Previously Held by AlliedSignal Inc.… | Jul 28, 2014 | Engine (TFE731-40AR)Only with: Engines with LPT2 blades P/N 3075424-1, -2, or -3 installed. |
| 2012-17-05 | Honeywell International Inc. Turbofan Engines | Oct 2, 2012 | Engine (TFE731-40AR)Only with: Applies only with specific first stage low-pressure turbine (LPT1) rotor assembly P/Ns installed: TFE731-5 with P/N 3075184-2, -3, or -4; TFE731-5AR/-5BR with P/N 3075447-1, -2, -4, 3075713-1, -2, -3, or 3074748-5; TFE731-4, -4R, -5AR, -5BR, -5R with P/N 3074748-4, -5, 3075447-1, -2, -4, 3075713-1, -2, or -3. |
| 2012-16-14 | Honeywell International Inc. Turbofan Engines | Oct 1, 2012 | Engine (TFE731-40AR)Serial numbers per Table 4 of Honeywell Service Bulletin TFE731-72-5221, Revision 0. Only with: Engines listed in Table 4 of the SB, or with LPT2 rotor assembly P/N 3060608-2, -3, or -5 that had LPT2 rotor blades P/N 3075424-2 replaced between March 2009 and September 2010, or P/N 3075424-3 replaced between July 2010 and September 2010. |
| 2012-13-51 | Fuel | Aug 13, 2012 | Airframe (GULFSTREAM G150)Certain serial numbers: 201–290 |
| 2011-23-07 | Gulfstream Aerospace LP (Type Certificate Previously Held by Israel Aircraft Industries… | Dec 15, 2011 | Airframe (GULFSTREAM G150)Certain serial numbers: Gulfstream G150 201–286; Galaxy 004–231; Gulfstream 200 004–231 |
| 2008-19-12 | Honeywell International Inc. TFE731-4, -4R, -5, -5AR, -5BR, and -5R Series Turbofan… | Oct 27, 2008 | Engine (TFE731-40AR)Only with: Interstage turbine transition (ITT) duct P/N 3075292-1, 3075292-3, 3074766-1, 3077063-1, 3075655-1, 3075655-2, 3075699-1, or 3075699-3 installed. |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (1)
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
- Landing gear · connecting rod · brokenAug 26, 2020
WHILE PERFORMING WALK AROUND OF AIRCRAFT FOUND RT NLG DOOR ROD END SNAPPED. UPON FURTHER INVESTIGATION FOUND THAT THE RT NLG DOOR CARDAN ASSEMBLY HAD SEIZED CAUSING THE ROD END TO SNAP. DISASSEMBLED, CLEANED, AND LUBRICATIED CARDAN. REMOVED AND REPLACED BROKE ROD END AND PERFORMED LANDING GEAR…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 18, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 18, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026