- Registered owner
- Lufthansa Aviation Training USA Inc
- Location
- Goodyear, AZ
- Owner type
- Non-citizen corporation
- Serial number
- 85003
- Year built
- 2001
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, utility, acrobatic
- Airworthiness date
- March 4, 2002
- Certificate issued
- July 22, 2026
- Expires
- July 31, 2033
- Mode S code
- ABDA02
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 11
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 2003 | 1 |
|---|---|
| 2004 | 1 |
| 2005 | 5 |
| 2009 | 1 |
| 2010 | 1 |
| 2014 | 1 |
| 2015 | 2 |
Airframe · Grob-Werke G 120A
AD 2015-09-06StartingAD 2014-09-11StabilizersAD 2010-20-01WingsAD 2009-12-15Electric PowerAD 2005-22-14Switch panels below the left-hand instrument panelAD 2005-12-09Nose landing gear (NLG) assemblyAD 2005-13-09Main landing gear (MLG)AD 2005-11-08Main landing gear front and rear spherical bearingsAD 2005-01-19Mode S transpondersAD 2004-22-21Vertical stabilizer main sparAD 2003-19-13Flight control system operating leversSuperseded and historical ADs · 1
Information bulletins that may apply · 2
Advisory, not mandatory.
Airframe · Grob-Werke G 120A
SAIB SW-18-31Navigation, Attitude, and Direction Data SystemSAIB CE-07-04Recurring cracks in the landing gearNTSB investigations · 1
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
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 · 24
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2011FA0000149Pump · failedAFTER INSTALLING ENGINE DRIVEN FUEL PUMP ON THE ENG, MECHANIC WENT OUT TO PERFORM AN ENGINE OPS CHECK AND FOUND ENGINE WOULDN’T KEEP RUNNING UNLESS BOOST PUMP WAS IN THE ON POSITION. UPON TROUBLESHOOTING MECHANIC FOUND THE SHAFT WAS SHEARED ON THE FUEL PUMP. SDR 2011FA0000148Pump · leakingMECHANIC PERFORMED A LEAK CHECK AFTER INSTALLING ENGINE DRIVEN FUEL PUMP ON THE ENGINE AND FOUND FUEL LEAKING FROM SHAFT DRIVE. NO PROBABLE CAUSE OR RECOMMENDATIONS AT THIS TIME.SDR 2005FA0000800Plate · debondedDURING FLEET - WIDE INSPECTION OF AIRCRAFT, TECH FOUND EXCESSIVE MOVEMENT BETWEEN RUDDER AND RUDDER LEVER ASSY. FURTHER INSPECTION SHOWED DISBONDING BETWEEN THE RUDDER SPAR AND THE RUDDER LEVER ASSY SPACER PLATE. PROBABLE CAUSE APPEARS TO BE EXCESSIVE FLEXIN
See all 24 reportsSTCs that may be installed · 45
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Grob-Werke G 120A
STC SA02571SEInstallation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display).STC SA12428CHInstallation of the Lycoming Engines Electronic Ignition System (EIS)STC SA04837NYInstallation of AeroLED's Holdings, LLC., position lights, navigation lights, strobe lights and beacon lights