N430BA2002 Let L-23 SUPER BLANIK
Safety record in brief:No NTSB accidents or incidents since 1982No ADs since 1998 matched3 service difficulty reports
Registration
FAA Aircraft Registry · Oct 17, 2026- Registered owner
- Civil Air Patrol
- Owner type
- Corporation
- City, state
- Maxwell Afb, AL
- Certificate issued
- Jan 2, 2013
- Expires
- Jan 31, 2029
- Airworthiness
- Standard · Normal
- Airworthiness date
- Aug 19, 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
- Let
- Model
- L-23 SUPER BLANIK
- Year
- 2002
- Serial number
- 029012
- Aircraft type
- Glider
- Category
- Land
- Certification
- Type Certificated
- Seats
- 2
- Max takeoff weight
- Up to 12,499 lb
- Mode S code
- A52338
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- 2013 – nowCivil Air PatrolMaxwell Afb, AL · current
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 (3)
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 · control cable · frayedMay 22, 2009
FRAYS DISCOVERED IN RUDDER CABLES - CHRONIC PROBLEM. NO FRAYS ALLOWED IAW MAINTENANCE MANUAL. CABES ARE SUPPOSED TO LAST 1000 HOURS, THIS DISCOVERED AT 375 PART TIS
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · longeron · crackedMay 2, 2006
FIRST LONGERON (N434BA) WAS FOUND CRACKED AT THE ELEVATOR TRIM GUIDE ATTACH POINT, NEAR THE RCP LT RUDDER PEDAL, DURING A SCHEDULED INSPECTION. SUBSEQUENT FINDINGS OCCURRED AS RESULT OF QUALITY DEPARTMENT ISSUING A ONE TIME INSPECTION OF ALL MDS. IT LOOKS AS IF THE OPERATOR, IN THE REAR COCKPIT…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Flight controls · control cable · frayedJun 21, 2005
LEFT RUDDER CABLE FOUND FRAYED AT AFT PULLEY. RIGHT RUDDER CABLE FOUND FRAYED AT FORWARD AND AFT PULLEYS.
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