- Registered owner
- Maxus Capital Group LLC
- Location
- Cleveland, OH
- Owner type
- LLC
- Serial number
- 96029
- Type
- Fixed wing multi engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- October 23, 2004
- Certificate issued
- March 6, 2023
- Expires
- March 31, 2030
- Mode S code
- AAB6F9
Gulfstream AM Corp Comm Div 695ATCDS 2A4Airframe · Gulfstream AM Corp Comm Div 695AEngine modelAiResearch TPE331 series
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every AiResearch TPE331 model are included below.
On this page
Airworthiness directives that may apply · 55
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1972 | 1 |
|---|---|
| 1974 | 2 |
| 1975 | 2 |
| 1976 | 1 |
| 1979 | 3 |
| 1980 | 2 |
| 1984 | 3 |
| 1987 | 1 |
| 1988 | 2 |
| 1989 | 1 |
| 1993 | 4 |
| 1994 | 2 |
| 1995 | 4 |
| 1996 | 1 |
| 1997 | 1 |
| 1998 | 7 |
| 1999 | 1 |
| 2000 | 1 |
| 2001 | 1 |
| 2002 | 2 |
| 2003 | 2 |
| 2004 | 1 |
| 2005 | 1 |
| 2006 | 2 |
| 2008 | 1 |
| 2009 | 1 |
| 2011 | 1 |
| 2012 | 1 |
| 2015 | 2 |
| 2016 | 2 |
| 2018 | 4 |
Airframe · Gulfstream AM Corp Comm Div 695A
AD 2006-16-18 R1Installing a warning placard on the TAWS/RMIAD 2005-01-19Mode S transpondersAD 2003-07-03Wing and fuselage structureInformation bulletins that may apply · 5
Advisory, not mandatory.
Airframe · Gulfstream AM Corp Comm Div 695A
SAIB 2023-14Landing Gear Retract/Extend SystemNTSB investigations · 1
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
FAA incident reports · 2
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Accident 20180426000309ALanding: Rollout · Bishop, CAN79PH a turbo commander experienced a collasped left main gear during landing on runway 12 at Bishop California airport (bih). Aircraft skidded to a stop on the left hand side of runway 12 with substantial damage. Bih weather was clear with a slight…Incident 20011129034869IClimb · South Bend, IN(-23) Aircraft was climbing out of FL180 to FL210 when windshield on pilots side cracked. The pilot declared an emergency with ATC and landed at sbn airport w/o further incident. Investigation revealed that outside windshield panel shattered on pilot side.
Service difficulty reports · 7
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR FTU2003F00003Regulator · failedHYDRAULIC REGULATOR WAS INSTALLED IN THIS AIRCRAFT AS A OVERHAULED, EXCHANGED. THIS UNIT FAILED DURING TAKEOFF, WHICH PREVENTED HYDRAULIC PRESSURE TO BUILD UP TO SYSTEM PRESSURE. UNIT WAS REMOVED AND REPLACED BY THE OWNERS ORIGINAL REGULATOR AFTER IT WAS OVESDR 98ZZZX4215Windshield · shatteredLEFT WINDSHIELD OUTER LAYER SHATTERED AT ALTITUDE. WINDSHIELD HEAT OPERATED NORMALLY PRIOR TO INCIDENT. 500 HOURS ON WINDSHIELD.SDR 97ZZZX3339Skin · corrodedACFT RETURNED FOR FUSELAGE INSP AND FINAL REPAIRS OF THE RT WING. DURING INSP, CORROSION FND IN THE LT WING IN SAME AREA, WS 39, BOTTOM SIDE, FWD OF THE MAIN SPAR. EFFECTED PARTS, THE L/E SKIN, STR NR 6 INBD, AND 2 ANGLES FWD. EXTENT OF CORROSION REQUIRED TSDR 97ZZZX3338Skin · corrodedACFT RETURNED FOR FUSELAGE INSP AND FINAL REPAIRS OF THE RT WING. DURING INSP, CORROSION FND IN THE LT WING IN SAME AREA, WS 39, BOTTOM SIDE, FWD OF THE MAIN SPAR. EFFECTED PARTS, THE L/E SKIN, STR NR 6 INBD, AND 2 ANGLES FWD. EXTENT OF CORROSION REQUIRED TSDR 96ZZZX2236Angle · crackedDURING A 100-HOUR INSPECTION, THE RT MLG INBOARD TRUSS ATTACH ANGLE WAS FOUND TO HAVE A 0.9 INCH RADIUS CRACK 1.0 INCH FROM AFT END. THIS CRACK WAS STOP DRILLED AND A DOUBLER AND RADIUS BLOCK WAS INSTALLED PER DER'S REPAIR SCHEME. CRACKS APPEAR TO BE ASSOCIASDR 96ZZZX2235Firewall · crackedTHE LT AND RT ENGINE FIREWALLS FOUND TO HAVE CRACKS IN THE ALUMINUM PORTION OF FIREWALL AT THE AFT ENGINE MOUNT UPPER ATTACH FASTENERS DURING OTHER MAINTENANCE REQUIRING THE LOWER AFT NACELLES TO BE REMOVED. WITH THE NACELLES REMOVED, THE CRACKS ARE VISIBLE. SDR 96ZZZX2229Truss Support · damagedAFTER RIGHT AFT LOWER NACELLE REMOVED TO FACILITATE MAINTENANCE, DISCOVERED THAT DURING A PREVIOUS LANDING GEAR REMOVAL, THE LEFT AND RIGHT OUTBOARD MLG TRUSS SUPPORTS WERE ACCIDENTLY DRILLED WHEN THE OUTBOARD TRUNNION PIN COVER WAS DRILLED OFF. THE LEFT TRUS
STCs that may be installed · 137
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Gulfstream AM Corp Comm Div 695A
STC SA02571SEInstallation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display).STC SA01800SEFabrication and installation of new or replacement of existing instrument panel lights dimmer control.STC SA01861SEFabrication and installation of Landing Light Controller