N867AF2002 Grob-Werke G 120A
Safety record in brief:No NTSB accidents or incidents since 198210 ADs may apply21 service difficulty reports
Registration
FAA Aircraft Registry · Oct 20, 2026- Registered owner
- Lufthansa Aviation Training USA INC
- Owner type
- Non Citizen Corporation
- City, state
- Goodyear, AZ
- Certificate issued
- Jun 18, 2026
- Expires
- Jun 30, 2033
- Airworthiness
- Standard · Normal, Utility
- Airworthiness date
- Jul 30, 2002
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
- Grob-Werke
- Model
- G 120A
- Year
- 2002
- Serial number
- 85007
- Aircraft type
- Fixed wing single engine
- Category
- Land
- Certification
- Type Certificated
- Seats
- 1
- Engines
- 1
- Max takeoff weight
- Up to 12,499 lb
- Mode S code
- ABE8DE
Engine
- Make and model
- Lycoming Aeio-540 Ser
- Type
- Reciprocating
- Power
- 260 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 2026 – nowLufthansa Aviation Training USA INCGoodyear, AZ · current
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026NTSB events (0)
No NTSB accidents or incidents found for this airframe since 1982.
ADs published since 1998 that may apply (10)
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 |
|---|---|---|---|
| 2015-09-06 | Starting | Jun 16, 2015 | Airframe (G 120A)Certain serial numbers: G115EG …–82323/E; G120A …–85063 |
| 2014-09-11 | Stabilizers | Jun 13, 2014 | Airframe (G 120A)Certain serial numbers: G120A 85001–85007; G120A 85026–85056; G120A 85058 |
| 2010-20-01 | G ROB-WERKE Model G120A Airplanes | Oct 12, 2010 | Airframe (G 120A) |
| 2009-12-15 | GROB-Werke Model G120A Airplanes | Jul 1, 2009 | Airframe (G 120A)Certain serial numbers: G120A 85001–85007; G120A 85026–85034 |
| 2005-22-14 | GROB-WERKE Model G120A Airplanes | Dec 19, 2005 | Airframe (G 120A) |
Show all 10 ADsShow fewer ADs
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2005-19-11 | Lycoming Engines (Formerly Textron Lycoming) AEIO-360, IO-360, O-360, LIO-360, LO-360… | Oct 21, 2005 | Engine (AEIO-540 SER)Only with: Engines rated at 300 HP or lower, manufactured new, rebuilt, or overhauled after March 1, 1999, or that had a crankshaft installed after March 1, 1999. |
| 2005-12-09 | GROB-WERKE Model G120A Airplanes | Jul 28, 2005 | Airframe (G 120A) |
| 2005-11-08 | GROB-WERKE Model G120A Airplanes | Jul 18, 2005 | Airframe (G 120A) |
| 2004-22-21 | GROB-WERKE Model G120A Airplanes | Dec 27, 2004 | Airframe (G 120A) |
| 2004-05-24 | Lycoming Engines (Formerly Textron Lycoming) AEIO-540, IO-540, LTIO-540, O-540, and… | Mar 30, 2004 | Engine (AEIO-540 SER)Only with: Engines with crankshaft gear retaining bolts P/N STD-2209 installed; excludes O-540-F series engines subject to AD 99-03-05 with bolt not since replaced, engines with bolt installed at original assembly or replaced by Lycoming per SB 554 after November 10, 1998, engines with bolt from replacement kits 05K19987, 05K23325, 05K23326, 05K23327, 05K23335 or 05K23336, and engines with single-drive dual magnetos. |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (21)
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.
- Engine controls · control cable · failedAug 19, 2011
PILOT REPORTED DURING FLIGHT HE EXPERIENCED A TOTAL LOSS OF MIXTURE CONTROL. INVESTIGATION REVEALED THE MIXTURE CONTROL CABLE HAD BROKEN AT THE CONTROL IN THE CABIN. NO RECOMMENDATIONS AT THIS TIME.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Engine fuel and control · pump · leakingMar 2, 2011
MECHANIC WAS PERFORMING A POST MAINTENANCE CHECK ON AIRCRAFT AND NOTICED FUEL STAINS ON THE DOG HOUSE, MECHANIC THEN PERFORMED A LEAK CHECK AND FOUND FUEL LEAKING FROM VENT ON ADJUSTMENT COVER ON ENGINE DRIVEN FUEL PUMP. NO PROBABLE CAUSE OR RECOMMENDATIONS AT THIS TIME.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Stabilizers · plate · debondedMay 13, 2005
DURING 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 FLEXING OF THE SPAR OR IMPROPER BONDING. (SPAR…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reportsShow fewer reports
- Flight controls · hinge · crackedMar 28, 2005
ON ROUTINE INSPECTION, MECHANIC FOUND HINGE ON LT AILERON TRIM TAB CRACKED AT ATTACH POINT FOR PUSH PULL ROD. CAUSE AT THIS TIME UNKNOWN, NO RECOMMENDATIONS AT THIS TIME. (K)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Landing gear · bolt · crackedNov 24, 2004
INSPECTION OF NOSE GEAR UPPER TRUNNION BOLTS FOUND CRACKS AROUND WELDS AND ON THE EARS FOR THE SWIVEL TUBE. PROBABLE CAUSE EXCESSIVE STRESSES IN THIS AREA. AT THIS TIME NO RECOMMENDATION UNTIL MFG MAKES DETERMINATION OF CAUSES. (K)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Flight controls · lever · bindingSep 29, 2003
DURING FLEET WIDE INSPECTION, FOUND BEARINGS IN AILERON LEVER 2 ASSY. PN 120A4242 TO BE DAMAGED AND BINDING. DAMAGE APPEARS TO BE CAUSED BY THE BUSHING PN 120A4435.02 IN THE FORK ENDS PN 120A4435.01. IT APPEARS THAT DESIGN LIMITATIONS OF THE BEARINGS ALLOWING BUSHING TO APPLY EXCESSIVE FORCE ON…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Landing gear · light · intermittentJun 18, 2003
PILOT REPORTED RT GEAR LIGHT INOPERATIVE IN FLIGHT, AFTER TOUCH DOWN GEAR INDICATOR LIGHT CAME ON. ON FURTHER INVESTIGATION WE BELIEVE WE HAD AN INTERMITTENT LIGHT INSIDE THE GEAR HANDLE, AFTER FOUR GEAR CYCLES THE LIGHT QUIT WORKING.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Landing gear · manifold · inoperativeJun 6, 2003
DURING FLIGHT THE FLIGHT CREW REPORTED THAT THE LEFT GEAR WAS SLOW TO EXTEND. MAINTENANCE PERSONNEL TROUBLESHOT SYSTEM AND FOUND LEFT EXTENSION VALVE BAD. PROBABLE CAUSE IS BELIEVED PARTICIALS INSIDE OF VALVE WHICH PREVENTED FLUID TO FLOW UNRESTRICTED.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Flight controls · actuator · failedMay 13, 2003
DURING FLIGHT, TRIM WOULD NOT STOP AND CONTINUED TO MOVE TO THE LEFT. PROBABLE CAUSE IS INTERNAL COMPONENT FAILURE IN THE AILERON TRIM ACTUATOR UNIT.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Flight controls · bearing · failedMay 12, 2003
DURING INSPECTION OF AIRCRAFT, FOUND BEARING TO BE FAILING. RETAINING CLIP AND SEAL WERE BEING FORCED OUT OF BEARING. PROBABLE CAUSE IS A DESIGN FLAW IN THE CONTROL SYSTEM WHICH ALLOWS THE CONTROL ROD DEFLECTION TO EXCEED THE DESIGN LIMIT OF THE BEARING. RECOMMEND A DESIGN CHANGE OR REPLACE…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Showing the 10 most recent of 21 reports.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 20, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 20, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026