# N422BA: 2002 Let L13 AC BLANIK

- Status: Valid registration
- Airframe: [Let L13 AC BLANIK](https://openairdocs.org/model/let-l13-ac-blanik) (registry code 1360312, 2 seats)
- Engine: [NONE](https://openairdocs.org/engine/none) (registry code 00000)
- Serial number: 028903
- Year built: 2002
- Type: Glider
- Engine type: None
- Airworthiness: Standard, glider
- Airworthiness date: July 31, 2002
- Certificate issued: September 12, 2026
- Expires: September 30, 2033
- Mode S code: A50327
- Registered owner: [Copley Mark H](https://openairdocs.org/faa-owner/COPLEY%20MARK%20H)
- Location: [Colorado Springs, CO](https://openairdocs.org/faa-place/CO/Colorado%20Springs)
- Owner type: Individual
- Owner's area on the map: 38.7526° N, 104.8782° W: Placed by OpenAirDocs at the center of ZIP code 80906, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=422BA
- Page: https://openairdocs.org/aircraft/N422BA

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination.

## ADs that may apply (OpenAirDocs): 0 in force

### Matched by airframe (Let L13 AC BLANIK)

None in force.

### Matched by engine (NONE)

None in force.

## Information bulletins (advisory)

None matched.

## NTSB investigations

None matched to N422BA.

## FAA accident and incident reports

None matched to N422BA.

## Service difficulty reports (4)

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

- [SDR 2010FA0001141](https://openairdocs.org/sdr/2010FA0001141), Oct 27, 2010: HINGE. BENT. RT AILERON HINGE ASSY BENT, HINGE BEARING RACE ALSO BENT. SUSPECT DISCREPENCY OCCURED DURING AEROBATIC FLIGHT. DISCOVERED ON 2 ACFT.
- [SDR DOSS12](https://openairdocs.org/sdr/DOSS12), May 2, 2006: LONGERON. CRACKED. FIRST LONGERON (N434BA) WAS FOUND CRACKED AT THE ELEVATOR TRIM GUIDE ATTACH POINT, NEAR THE REAR COCKPIT (RCP) LT RUDDER PEDAL, DURING A SCHEDULED INSPECTION. S
- [SDR 2005FA0000854](https://openairdocs.org/sdr/2005FA0000854), Jun 21, 2005: CONTROL CABLE. FRAYED. LEFT AND RIGHT RUDDER CABLES FOUND FRAYED AT FRONT AND REAR PULLEY POSITIONS.
- [SDR 2002FA0001309](https://openairdocs.org/sdr/2002FA0001309), Nov 19, 2002: FRAME. DETACHED. DURING ACCEPTANCE INSPECTION UPON DELIVERY FROM THE CZECHOSLOVAKIA SOCIALIST REPUBLIC, EXTERNAL DAMAGE WAS NOTED WHERE THE AFT FUSELAGE RESTS IN THE TRAILER TAI

## STCs that may be installed (OpenAirDocs)

None matched to this aircraft's models.

## Related

- Other Let L13 AC BLANIK aircraft: https://openairdocs.org/model/let-l13-ac-blanik/aircraft.md
- The NONE engine: https://openairdocs.org/engine/none.md

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.
