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Aircraft record

N421BA2002 Let L13 AC BLANIK

DeregisteredUnclaimedSource: FAA, updated Oct 20, 2026

This N-number isn't registered right now. Below is its last known registration, canceled Sep 18, 2017.

Safety record in brief:No NTSB accidents or incidents since 1982No ADs since 1998 matched3 service difficulty reports

Registration
Deregistered
Last based in
Usaf Academy, CO
owner city / state
Engine
NONE
None
Owners
1
since 2002
NTSB events
None
since 1982
ADs may apply
0
confirm with A&P
Service reports
3
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Last registered owner
United States Air Force Academy 94 Fts Cc
Owner type
Government
City, state
Usaf Academy, CO
Certificate issued
Apr 9, 2002
Canceled
Sep 18, 2017
Airworthiness
Standard · Glider
Airworthiness date
Apr 15, 2002

We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.

Airframe & engine

FAA Registry + type data

Airframe

Manufacturer
Let
Model
L13 AC BLANIK
Year
2002
Serial number
028902
Aircraft type
Glider
Category
Land
Certification
Type Certificated
Seats
2
Max takeoff weight
Up to 12,499 lb
Mode S code
A4FF70

Engine

Make and model
None None
Type
None

Total time and engine hours aren't public. They appear here once the owner adds logbooks.

Ownership history

Ownership history from FAA records
  1. 2002 – 2017United States Air Force Academy 94 Fts CcUsaf Academy, CO

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026

NTSB events (0)

No NTSB accidents or incidents found for this airframe since 1982.

Accident history for this model

ADs published since 1998 that may apply (0)

These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.

No ADs published since 1998 matched this airframe or engine model.

AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.

Service Difficulty Reports (3)

Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.

  • Flight controls · control cable · frayedJun 21, 2005

    LEFT AND RIGHT RUDDER CABLES FOUND FRAYED AT FRONT AND REAR PULLLEY POSITIONS.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Flight controls · ring · missingFeb 21, 2003

    ONE TIME FLEET INSPECTION REVEALED SAFETY CLIP MISSING. THIS CLIP HOLDS THE SHAFT THAT ATTACHES THE RUDDER PEDAL TO THE FUSELAGE FITTING.ONE TIME INSPECTION INITIATED DUE TO ANOTHER AIRCRAFT IN FLEET HAVING PEDAL VERTICAL STABILTY DETERIORATE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · frame · detachedNov 19, 2002

    DURING ACCEPTANCE INSPECTION UPON DELIVERY FROM THE CZECH REPUBLIC, EXTERNAL DAMAGE WAS NOTED WHERE THE AFT FUSELAGE RESTS IN THE TRAILER TAIL DOLLY. INTERNAL INSPECTION OF THE FUSELAGE REVEALED DEFORMED AND TORN FUSELAGE FRAME MEMBERS NR 11, 12, AND 13. SUBSEQUENT INSPECTION OF THREE OTHER…

    From FAA Service Difficulty Reports; matched by N-number and serial number.

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 20, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 20, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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