- Registered owner
- Civil Air Patrol
- Location
- Maxwell Afb, AL
- Owner type
- Corporation
- Serial number
- 029014
- Year built
- 2002
- Type
- Glider
- Engine
- None
- Airworthiness
- Standard, glider
- Airworthiness date
- October 18, 2002
- Certificate issued
- December 5, 2012
- Expires
- December 31, 2028
- Mode S code
- A52E5D
From the FAA registry file of October 21, 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Superseded and historical ADs · 1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 N433BAMatched by N-number and event date. 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 N433BAMatched by N-number and event date. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Let L-23 SUPER BLANIK aircraft
Service difficulty reports · 5
SDR 2011FA0000439Control Cable · frayedRUDDER CABLES FRAYED AT 471.8 TIS. SHOULD LAST 1000 HRS IAW MFG.SDR 2010FA0000891Rib · crackedNR3 RIB AT UPPER FLANGE, LT WING FOUND CRACKED.SDR 2009FA0000632Support Fitting · crackedTHIS AIRCRAFT WAS DISCOVERED WITH A CRACKED MLG WELDED SUPPORT FITTING AFTER A HARD LANDING.SDR DOSS08Longeron · crackedFIRST LONGERON (N434BA) WAS FOUND CRACKED AT THE ELEVATOR TRIM GUIDE ATTACH POINT, NEAR THE RCP LH 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 ISDR 2005FA0000885Control Cable · frayedRIGHT RUDDER CABLE FOUND FRAYED AT FORWARD AND AFT PULLEYS.