N44FV1969 Schempp-Hirth STANDARD CIRRUS
This N-number isn't registered right now. Below is its last known registration, canceled Dec 20, 2021.
Safety record in brief:No NTSB accidents or incidents since 1982No ADs since 1998 matched1 service difficulty report
- Registration
- Deregistered
Registration
FAA Aircraft Registry · Oct 17, 2026- Last registered owner
- Individual owner
- City, state
- Red Bluff, CA
- Certificate issued
- Feb 24, 2020
- Canceled
- Dec 20, 2021
- Airworthiness
- Experimental · Amateur Built
- Airworthiness date
- Sep 7, 1979
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
- Schempp-Hirth
- Model
- STANDARD CIRRUS
- Year
- 1969
- Serial number
- V1
- Aircraft type
- Glider
- Category
- Land
- Certification
- Type Certificated
- Seats
- 1
- Max takeoff weight
- Up to 12,499 lb
- Mode S code
- A548D5
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- 2020 – 2021Individual ownerRed Bluff, CA
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 17, 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 (1)
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.
- Stabilizers · spar · crackedNov 5, 2002
MAIN SPAR OF TAILPLANE (STABILATOR) WAS FOUND TO CONTAIN MULTIPLE CRACKS IN WOOD STRUCTURE AFT MOUNTING HOLES. PLYWOOD FACE PLATES WERE DELAMINATED AND HIDING CRACKS. ALL ATTACHMENT HARDWARE WERE RUSTED. TAILPLANE WAS LOOSE WITH EXCESSIVE PLAY AFTER HARD LANDING, PILOT INDICATED IT WAS ALWAYS LOOSE.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 17, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 17, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026