N28GG2002 Schleicher ASW-28
Safety record in brief:No NTSB accidents or incidents since 1982No ADs since 1998 matched2 service difficulty reports
Registration
FAA Aircraft Registry · Oct 20, 2026- Registered owner
- Individual owner
- City, state
- Beavercreek, OH
- Certificate issued
- Mar 6, 2025
- Expires
- Mar 31, 2032
- Airworthiness
- Standard · Utility
- Airworthiness date
- Apr 22, 2010
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
- Schleicher
- Model
- ASW-28
- Year
- 2002
- Serial number
- 28056
- Aircraft type
- Glider
- Category
- Land
- Certification
- Type Certificated
- Seats
- 1
- Max takeoff weight
- Up to 12,499 lb
- Mode S code
- A2CC3F
Engine
- Make and model
- None None
- Type
- None
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 2025 – nowIndividual ownerBeavercreek, OH · 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.
Accident history for this modelADs published since 1998 that may apply (0)
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.
No ADs published since 1998 matched this airframe or engine model.
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (2)
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.
- Flight controls · clevis · failedOct 24, 2012
AIR BRAKE FAILURE DUE TO A DEFECTIVE WELD IN A CLEVIS WHICH IS COMPRISED OF A BOLT WELDED INTO A U-SHAPED PIECE OF METAL. THE WELD FAILED CAUSING THE BOLT TO PUSH THROUGH THE U SHAPED METAL. THIS CAUSED THE OTBD END OF THE AIR-BRAKE TO RAISE UP ABOVE THE WING SURFACE EVEN THOUGH THE OVER CENTER…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Wings · clevis · failedOct 24, 2012
AIR BRAKE FAILURE DUE TO A DEFECTIVE WELD IN A CLEVIS WHICH IS COMPRISED OF A BOLT WELDED INTO A U SHAPED PIECE OF METAL. THE WELD FAILED CAUSING THE BOLT TO PUSH THROUGH THE U SHAPED METAL. THIS CAUSED THE OUTBOARD END OF THE AIR-BRAKE TO RAISE UP ABOVE THE WING SURFACE EVEN THOUGH THE OVER…
From FAA Service Difficulty Reports; matched by N-number and serial number.
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