- Registered owner
- Civil Air Patrol
- Location
- Maxwell Afb, AL
- Owner type
- Corporation
- Serial number
- 029012
- Year built
- 2002
- Type
- Glider
- Engine
- None
- Airworthiness
- Standard, normal
- Airworthiness date
- August 19, 2002
- Certificate issued
- January 2, 2013
- Expires
- January 31, 2029
- Mode S code
- A52338
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 5
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 2005 | 1 |
|---|---|
| 2009 | 1 |
| 2010 | 2 |
| 2011 | 1 |
| 2020 | 1 |
Superseded and historical ADs · 1
Information bulletins that may apply
Advisory, not mandatory.
No bulletins matched this aircraft’s models
NTSB investigations
No NTSB investigations matched to N430BAMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Let L-23 SUPER BLANIK aircraft
FAA incident reports
No FAA accident or incident reports matched to N430BAMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Let L-23 SUPER BLANIK aircraft
Service difficulty reports · 3
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2009FA0000429Control Cable · frayedFRAYS DISCOVERED IN RUDDER CABLES - CHRONIC PROBLEM. NO FRAYS ALLOWED IAW MAINTENANCE MANUAL. CABES ARE SUPPOSED TO LAST 1000 HOURS, THIS DISCOVERED AT 375 PART TISSDR DOSS06Longeron · crackedFIRST 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 ASSDR 2005FA0000877Control Cable · frayedLEFT RUDDER CABLE FOUND FRAYED AT AFT PULLEY. RIGHT RUDDER CABLE FOUND FRAYED AT FORWARD AND AFT PULLEYS.
STCs that may be installed · 2
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.