N438BA

LET L-23 SUPER BLANIK · 2002 · Glider · 0 engines · 2 seats · Valid Registration

Registered owner: CIVIL AIR PATROL, AL (owner ≠ operator)

Operators of this aircraft

Who operated this tail, and how firmly we know it.

OperatorRolePeriodBasis
CIVIL AIR PATROLOperatoron 2023-06-03Operator named in NTSB report

Accident & incident history

Accident · 2023-06-03 Operator named in NTSB report
LET L-23 SUPER BLANIK No injuries Part 91CIVIL AIR PATROL

Operated by CIVIL AIR PATROL (per NTSB report)

Source: NTSB case WPR23LA362

Maintenance disclosures

Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.

5 reports on file, 2003-02-21 – 2010-07-22.

OTHER · 2010-07-22 Unresolved
ATA 5712

Part: RIB — CRACKED (ZONE 500) · airframe 1,842 hrs

DURING ROUTINE INSPECTION, (2) SMALL CRACKS WERE DISCOVERED ON RIB 3 UPPER FLANGE, LT WING. THIS IS THE SECOND RECENT OCCURRENCE.

Source: SDR 2010FA0000757
OTHER · 2006-05-02 Unresolved
ATA 5313

Part: LONGERON — CRACKED (REAR COCKPIT) · airframe 524 hrs

FIRST 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 IF THE OPERATOR, IN THE REAR COCKPIT (RCP), MAY BE STRIKING THE ELEVATOR TRIM GUIDE WITH HIS/HER FOOT WHILE ACTUATING THE RUDDER PEDAL - CAUSING THE SUPPORT STRUCTURE (LONGERON) TO WEAKEN AND FORM CRACKS AT THE ATTACH SCREWS.

Source: SDR DOSS10
OTHER · 2005-06-21 Unresolved
ATA 2720

Part: CONTROL CABLE — FRAYED (RUDDER) · airframe 415 hrs

RIGHT RUDDER CABLE FOUND FRAYED AT FORWARD AND AFT PULLEYS.

Source: SDR 2005FA0000884
OTHER · 2003-09-22 Unresolved
ATA 5743

Part: FAIRING — CRACKED (WING-TIP) · airframe 100 hrs

RADIAL CRACKS ARE BEING FOUND FLEETWIDE ON WING-TIP FAIRINGS.THERE HAVE BEEN NO COMPLETE FAILURES AT THIS TIME. FACTORY ADVISES WING TIPS ARE DESIGNED TO FAIL ON SIDE LOADS TO PREVENT MAJOR DAMAGE TO WING SPAR.

Source: SDR 2003FA0000957
F.O.D. · 2003-02-21 Unresolved
ATA 2720

Part: RING — MISSING (RUDDER PEDAL) · airframe 95 hrs

RUDDER PEDAL LOST VERTICAL STABILTY AND THE INSTRUCTOR PILOT REPORTED THE PROBLEM TO MAINTENANCE. MAINTENANCE INSPECTED THE AREA AND FOUND THE SAFETY RING,WHICH HOLDS THE RUDDER PEDAL ATTACH SHAFT TO THE FUSELAGE FITTING, MISSING. AN INSPECTION WAS MADE TO FIND THE RING, AND DETERMINED IT WAS NOT IN THE AIRCRAFT. MAINTENANCE QUESTIONED IF IT WAS INSTALLED AT THE FACTORY, WHICH INITIATED A FLEET WIDE ONE TIME INSPECTION. TWO MORE AIRCRAFT WERE FOUND TO BE MISSING THE SAFETY RINGS.THESE ARE NEW AIRCRAFT WITH LESS THAN A HUNDRED HOURS TIME IN SERVICE.

Source: SDR 2003FA0000228