- Registered owner
- Alliance Air Parts Acquisitions Corp
- Location
- Oklahoma City, OK
- Owner type
- Non-citizen corporation
- Serial number
- 206
- Year built
- 1979
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- August 7, 1984
- Certificate issued
- September 17, 2024
- Expires
- September 30, 2031
- Mode S code
- A45A47
- Registry status
- Non-citizen corporation, flight hours not reported
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Garrett TFE731 model are included below.
On this page
Airworthiness directives that may apply · 67
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1974 | 5 |
|---|---|
| 1975 | 1 |
| 1978 | 2 |
| 1980 | 5 |
| 1981 | 1 |
| 1982 | 2 |
| 1983 | 1 |
| 1984 | 1 |
| 1985 | 2 |
| 1986 | 3 |
| 1987 | 2 |
| 1988 | 1 |
| 1989 | 2 |
| 1990 | 2 |
| 1991 | 1 |
| 1992 | 2 |
| 1993 | 1 |
| 1994 | 2 |
| 1995 | 4 |
| 1996 | 5 |
| 1997 | 1 |
| 1998 | 2 |
| 1999 | 3 |
| 2000 | 2 |
| 2001 | 3 |
| 2004 | 1 |
| 2005 | 3 |
| 2007 | 2 |
| 2008 | 2 |
| 2010 | 1 |
| 2012 | 1 |
| 2014 | 1 |
| 2016 | 1 |
| 2018 | 1 |
| 2022 | 1 |
See all 72 ADs
Information bulletins that may apply · 5
Advisory, not mandatory.
Airframe · Gates Learjet 35A
SAIB 2026-07MAIN LANDING GEAR ATTACH SECTION, Trunnion PinsSAIB NM-16-24Fuselage: Main Plate/SkinSAIB NM-13-38Flight Controls Control Column SectionSAIB NM-11-48Ice and Rain Protection: Wing Transverse Duct AssemblyEngine · Garrett TFE731 series
SAIB NE-06-70NTSB investigations
No NTSB investigations matched to N38PSMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Gates Learjet 35A aircraft
FAA incident reports · 1
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Service difficulty reports · 4
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR ZP7A20160605001Oil System · reads highLEFT OIL TEMP SPIKED ON CLIMBOUT AT 150 DEGREES, BOUNCED BETWEEN 130-150 DEGREES.SDR ZP7A201605090001Engine · failedLEFT ENGINE FAILURE IN FLIGHT. FLUCTUATION IN ITT TEMP BEFORE FAILURE RISE AND FALL. ATTEMPTED TO RESTART. NO LIGHT OFF.SDR ZP7A20130214001Master Switch · faultyFAILURE OF PRIMARY PITCH TRIM. AFTER ROTATION, PF NOTICED INCREASED CONTROL PRESSURES REQUIRED TO MAINTAIN FLIGHT ATTITUDE, DESPITE ACTUATING NOSE DOWN TRIM. PF ASKED PNF TO ATTEMPT TO TRIM AC FROM THE RIGHT YOKE. NO EFFECT. MEMORY ITEMS WERE ACCOMPLISHED SDR ZP7A20110802001Brake Sys · contaminatedCREW REPORTED THAT THE BRAKES WORKED INTERMITTENTLY ON TAXI. A FEW MINUTES INTO THE TAXI, THE PEDALS WERE FIRM BUT BRAKING ACTION WAS MINIMAL OR NON-EXISTENT. CREW RETURNED TO THE FBO. MAINTENANCE CHECKED IT OUT - BLED THE BRAKE SYSTEM, SERVICED THE HYDRAUL
STCs that may be installed · 230
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Gates Learjet 35A
STC ST01305WI-DModification of a Collins ALT-50A or ALT-55B Radio Altimeter system installation to a Collins ALT-1000 or ALT-4000 Radio Altimeter system installation in accordance with Collins Drawing Index as listed on AML No. ST01305WI-D, Revision -, or later FAA approved revision.STC ST12461IBInstallation of Cockpit Voice Recorder with optional RIPS UpgradeSTC SA2622NMInstallation of Precise Flight Pulselite Control Unit in landing/taxi system. (767-200 B17) (DHC-8 101)