- Registered owner
- Civil Air Patrol
- Location
- Maxwell Afb, AL
- Owner type
- Corporation
- Serial number
- 029015
- 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
- A53D39
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Superseded and historical ADs · 1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 N437BAMatched 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 N437BAMatched 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 · 5
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR PF5R12032010001Hinge Bracket · crackedDISCOVERED CRACK IN THE RT ELEVATOR HINGE BRACKET DURING INSP.SDR 2010FA0000225Hinge · crackedDURING A 100 HR INSP, IT WAS DISCOVERED THAT THE INBD ELEVATOR HINGE BRACKET EXHIBITED SEVERAL CRACKS. ADDITIONAL CRACKS WERE FOUND ON THE ACFT AFTER A FLEET WIDE, ONE TIME INSP WAS COMPLETED.SDR 2005FA0001469Damper · crackedUPPER HINGE ARM OF GEAR STRUT CRACKED AT WELDS.SDR 2005FA0000879Control Cable · frayedLEFT AND RIGHT RUDDER CABLES FOUND FRAYED AT AFT PULLEYS.SDR 2003FA0000712Seat · mismanufacturedTHE WEIGHTED SEATS HAVE A HANDLE WELDED ON THE LEFT REAR CORNER. WITH THE SEAT BELT FASTENED IT IS POSSIBLE TO LIMIT FULL LEFT RUDDER TRAVEL DUE TO THE RUDDER PEDAL JAMMING THE SEAT BELT ATTACH TAB BETWEEN THE PEDAL AND THE HANDLE. IT ONLY HAPPENS WITH THE OPT
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.