- Registered owner
- Civil Air Patrol
- Location
- Maxwell Afb, AL
- Owner type
- Corporation
- Serial number
- 029006
- Year built
- 2002
- Type
- Glider
- Engine
- None
- Airworthiness
- Standard, utility
- Airworthiness date
- May 17, 2002
- Certificate issued
- December 5, 2012
- Expires
- December 31, 2028
- Mode S code
- A4F5A9
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Superseded and historical ADs · 1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 N419BAMatched 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 N419BAMatched 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 2010FA0000770Control Cable · frayedFRAYED RUDDER CABLES, CHRONIC PROBLEM. SUPPOSED TO LAST 1000 HOURS, THIS SET FAILED AT 178.1 TIS.SDR 2010FA0000226Hinge · 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 2009FA0000950Bracket · crackedDURING A 100 HOUR INSPECTION, A SMALL CRACK WAS DISCOVERED IN A WELD ON THE STEEL BRACKET THAT PROVIDES THE AFT ATTACHMENT OF THE HORIZONTAL STABILIZER TO THE VERTICAL STABILIZER.SDR DOSS11Longeron · 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 2005FA0000880Control Cable · frayedLEFT AND RIGHT RUDDER CABLES FOUND FRAYED AT 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.