N787BN2007 IAI GULFSTREAM G150
This N-number isn't registered right now. Below is its last known registration, canceled Aug 7, 2025.
Safety record in brief:No NTSB accidents or incidents since 198211 ADs may apply5 service difficulty reports
- Registration
- Deregistered
Registration
FAA Aircraft Registry · Oct 18, 2026- Last registered owner
- Bank Of Utah Trustee
- Owner type
- Corporation
- City, state
- Salt Lake City, UT
- Certificate issued
- Jul 29, 2025
- Canceled
- Aug 7, 2025
- Airworthiness
- Standard · Transport
- Airworthiness date
- Jul 19, 2007
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
- 231
- 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
- AAAAAD
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- 2025Bank Of Utah TrusteeSalt Lake City, UT
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 (5)
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 · landing light · burned outJun 3, 2024
CAPTAIN INFORMED MX THAT THE UPON APPROACH TO LONG BEACH AIRPORT AND DURING GEAR EXTENSION, THE RIGHT HAND MAIN LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE. THE CREW CHECKED AND CONFIRMED THAT THE GEAR WAS DOWN AND LOCKED, THE CREW HAD DECLARED EMERGENCY AND LANDED THE AIRCRAFT SAFELY.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Flight controls · stabilizer · failedNov 20, 2021
WHILE CRUISING AT 38,000 FT. WE HAD A MACH TRIM FAIL INDICATION. AUTO PILOT KICKED OFF AND AIRCRAFT STARTED TO PITCH UP. WE NO TRIM CONTROL AND TOOK BOTH PILOTS TO PUSH THE YOKE FORWARD TO KEEP AIRPLANE LEVEL.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Flight controls · drive unit · inoperativeNov 2, 2011
FLAPS WOULD NOT RETRACT AFTER TAKEOFF. AIRCRAFT DIVERTED FOR MAINTENANCE. FOUND DRIVE UNIT INOPERATIVE.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 5 reportsShow fewer reports
- Engine · fitting · failedApr 16, 2010
APPROX 11:30 PST, FLIGHT LEVEL 390, CAPTAIN REPORTED FLUCTUATING OIL PRESSURE, SECURED RT ENGINE AND DIVERTED. DISPATCHED MX CREW TO ACFT, INSP REVEALED OIL PRESSURE FITTING ON THE FWD 4 OCLOCK POSITION VIEWED FWD, HAD PULLED THE THREADS OUT OF THE HSG. THE PUMP HAD BEEN REPLACED 271 HOURS…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Hydraulic power · line · unserviceableJan 18, 2010
PILOT REPORTED AT 40K FT, ABOUT 4 HOURS INTO THE FLIGHT BACK, WHEN THEY HAD A VIBRATION. PILOT NOTICED A SPLIT IN THE GENERATORS AND AN INCREASE IN VIBES ON THE RT ENGINE. AFTER A FEW MINUTES THE GENERATORS WENT BACK TO ABOUT A 5 VOLT SPLIT. AFTER ABOUT ANOTHER 15 MINUTES THEY LOST THE RT…
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