Registered owner
Civil Air Patrol
Owner type
Corporation
Serial number
029005
Year built
2002
Type
Glider
Engine
None
Airworthiness
Standard, glider
Airworthiness date
April 15, 2002
Certificate issued
December 5, 2012
Expires
December 31, 2028
Mode S code
A4D43A

From the FAA registry file of October 24, 2026.

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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.

2005In forceSuperseded2026
ADs by the year they took effect: 6 ADs
20051
20091
20102
20111
20201
Superseded and historical ADs · 1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 N410BAMatched 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 N410BAMatched 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 · 7

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

SDR 2011FA0000021Control Cable · frayedRUDDER CABLES FOUND FRAYED AT 494.3 HOURS. LIFE SB 1000 HRS IAW MFG. CHRONIC PROBLEM.Jan 12, 2011 · N410BA · Let L23SUPERBLAN · Rudder Control SystemSDR 2010FA0000830Rib · crackedCRACK FOUND NR3 RIB UPPER FLANGE, RT AND LT WING. CHRONIC PROBLEM.Aug 13, 2010 · N410BA · Let L23SUPERBLAN · Fuselage Main, BulkheadSDR 2010FA0000227Hinge · 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.Feb 8, 2010 · N410BA · Let L23SUPERBLAN · Elevator StructureSDR 2009FA0000729Control Cable · frayedRUDDER CABLES FOUND FRAYED DURING 100 HR INSP. TT ON LT AND RT RUDDERS - 186.1 HOURS. SHOULD LAST 1000 HOURS IAW LET MM. THIS IS A CHRONIC PROBLEM.Aug 21, 2009 · N410BA · Let L23SUPERBLAN · Rudder Control SystemSDR DOSS13Longeron · 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 AS IMay 2, 2006 · N410BA · Let L23SUPERBLAN · Fuselage Main, Longeron/StringerSDR 2005FA0001441Control Cable · frayedRT RUDDER CABLE FOUND FRAYED AT FORWARD NR 1 PULLEY.Oct 21, 2005 · N410BA · Let L23SUPERBLAN · Rudder Control SystemSDR 2005FA0000881Control Cable · frayedLEFT RUDDER CABLE FOUND FRAYED AT FORWARD AND AFT PULLEYS.Jun 21, 2005 · N410BA · Let L23SUPERBLAN · Rudder Control System

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.