Skip to content
KnownTail
Aircraft record

N865AF2002 Grob-Werke G 120A

Registration validUnclaimedSource: FAA, updated Oct 20, 2026

Safety record in brief:1 NTSB accident (substantial damage, Aug 2010)10 ADs may apply33 service difficulty reports

Registration
Valid
expires Jun 30, 2033
Based in
Goodyear, AZ
owner city / state
Owners
1
since 2026
NTSB events
1
substantial, 2010
ADs may apply
10
confirm with A&P
Service reports
33
since 1995

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 3, 2026
Expires
Jun 30, 2033
Airworthiness
Standard · Utility, Acrobatic
Airworthiness date
Mar 28, 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 data

Airframe

Manufacturer
Grob-Werke
Model
G 120A
Year
2002
Serial number
85005
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
ABE170

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
  1. 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, 2026

NTSB events (1)

Accident · substantial damage

Aug 24, 2010 · Buckeye, AZ

The student pilot's improper flare, which resulted in a hard landing.

Damage
Substantial
Injuries
None
Report
WPR10LA426

From NTSB records; matched by serial number.Read NTSB report (search CAROL for WPR10LA426)

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.

ADSubjectEffectiveApplies to
2015-09-06StartingJun 16, 2015Airframe (G 120A)Certain serial numbers: G115EG …–82323/E; G120A …–85063
2014-09-11StabilizersJun 13, 2014Airframe (G 120A)Certain serial numbers: G120A 85001–85007; G120A 85026–85056; G120A 85058
2010-20-01G ROB-WERKE Model G120A AirplanesOct 12, 2010Airframe (G 120A)
2009-12-15GROB-Werke Model G120A AirplanesJul 1, 2009Airframe (G 120A)Certain serial numbers: G120A 85001–85007; G120A 85026–85034
2005-22-14GROB-WERKE Model G120A AirplanesDec 19, 2005Airframe (G 120A)
Show all 10 ADs
ADSubjectEffectiveApplies to
2005-19-11Lycoming Engines (Formerly Textron Lycoming) AEIO-360, IO-360, O-360, LIO-360, LO-360…Oct 21, 2005Engine (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.
2005-12-09GROB-WERKE Model G120A AirplanesJul 28, 2005Airframe (G 120A)
2005-11-08GROB-WERKE Model G120A AirplanesJul 18, 2005Airframe (G 120A)
2004-22-21GROB-WERKE Model G120A AirplanesDec 27, 2004Airframe (G 120A)
2004-05-24Lycoming Engines (Formerly Textron Lycoming) AEIO-540, IO-540, LTIO-540, O-540, and…Mar 30, 2004Engine (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 (33)

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.

  • pump · wornOct 30, 2006

    DURING FLIGHT SUCTION PRESSURE READING DROPPED TO ZERO, DURING FURTHER TROUBLESHOOTING, TECH FOUND THE ENGINE DRIVEN AIR PUMP WAS NOT PRODUCTING ENOUGH SUCTION. PROBABLE CAUSE COULD BE FROM PISTION WEARING INSIDE OF PUMP. RECOMMENDATION AT THIS TIME IS FOR THE MFG TO INVESTIGATE WHY PUMP PISTON IS…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • shaft · brokenSep 26, 2006

    DURING ENGINE START, SUCTION PRESSURE WAS READING ZERO, DURING FURTHER TROUBLESHOOTING, TECH FOUND THE ENGINE DRIVEN DRIVEN DRY AIR PUMP HAD A BROKEN SHAFT. PROBABLE CAUSE COULD BE FROM VIBRATION OR HARD START. NO RECOMMENDATION AT THIS TIME. (K)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Air conditioning and pressurization · blower motor · wornFeb 27, 2006

    PILOT REPORTED EXCESSIVE VIBRATION WITH AIR CONDITION ON. WHILE TECH WAS TROUBLESHOOTING SYSTEM FOUND THAT BLOWER MOTOR HAD TOO MUCH END PLAY ON BLOWER FAN SHAFT MAKING IT VIBRATE. NO RECOMMENDATIONS AT THIS TIME. (K)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Engine fuel and control · servo · malfunctionedJun 14, 2005

    PILOT REPORTED ENGINE QUIT AFTER LANDING WITH BOOST PUMP ON. ON GROUND RUN PERFORMING MIXTURE IDLE CHECK, WE FOUND WITH BOOST PUMP OFF, WE HAD .5 INCH MANIFOLD PRESSURE DROP AND WITH BOOST PUMP ON. WE HAD 1.5 INCH MANIFOLD PRESURE DROP. ON FURTHER INVESTIGATION, WE FOUND ICO LEVER STICKY AND ROUGH…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Ignition · ignition switch · inoperativeJan 18, 2005

    PILOT REPORTED STARTER WOULD NOT ENGAGE, AFTER FURTHER INVESTIGATION FOUND IGNITION SWITCH WAS BAD. NO PROBABLE CAUSE OR RECOMMENDATIONS AT THIS TIME. (K)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Flight controls · lever · bindingSep 29, 2003

    DURING PRE-FLIGHT INSPECTION, FLIGHT CREW FELT BINDING ON THE AILERON SYSTEM UPON FURTHER INSPECTION FOUND BEARINGS IN AILERON LEVER 2 ASSY. 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…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Flight controls · bearing · bulgedAug 11, 2003

    DURING SPECIAL INSPECTION OF THE AIRCRAFT REVEALED THAT THE BEARING ON THE LT AILERON LEVER ASSY IS SHOWING SIGNS OF BULGING . PROBABLE CAUSE IS DESIGN OF LEVER ASSY. THE AMOUNT OF USE OF THIS SYSTEM. REDESIGN OR REPLACE BEARING OF A HIGHER QUALITY.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Hydraulic power · relay · shortedJun 8, 2003

    WHILE PERFORMING GEAR CHECK, THE HYDRAULIC PRESSURE WOULD NOT BUILD UP. FOUND RELAY SHORTED OUT. RECOMMEND INSTALLING AN INLINE FUSE IN THE SYSTEM. WHEN THIS RELAY FAILS, THE RELAY AND DIODES BOARD ALSO FAILS.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Pneumatic · shaft · shearedJun 4, 2003

    DURING FLIGHT, THE INSTRUMENT VACUUM SYSTEM FAILED. THE AIRCRAFT RETURNED TO MAINTENANCE AND AN INSPECTION OF THE SYSTEM REVEALED THAT THE ROTOR SHAFT HAD SHEARED. PROBABLE CAUSE MAY BE THE ENGINE MOUNTS USED ARE TOO SOFT AND ALLOW THE ENGINE TO VIBRATE TOO MUCH AND THIS CAUSES THE PUMP SHAFT TO…

    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 33 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

Request owner name removalReport an error in this record