- Registered owner
- Copley Mark H
- Location
- Colorado Springs, CO
- Owner type
- Individual
- Serial number
- 028903
- Year built
- 2002
- Type
- Glider
- Engine
- None
- Airworthiness
- Standard, glider
- Airworthiness date
- July 31, 2002
- Certificate issued
- September 12, 2026
- Expires
- September 30, 2033
- Mode S code
- A50327
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 0
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
No ADs matched this aircraft’s modelsADs on appliances, propellers and installed equipment aren’t matched by model; check those separately.
Information bulletins that may apply
Advisory, not mandatory.
No bulletins matched this aircraft’s models
NTSB investigations
No NTSB investigations matched to N422BAMatched 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 L13 AC BLANIK aircraft
FAA incident reports
No FAA accident or incident reports matched to N422BAMatched 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 L13 AC BLANIK aircraft
Service difficulty reports · 4
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2010FA0001141Hinge · bentRT AILERON HINGE ASSY BENT, HINGE BEARING RACE ALSO BENT. SUSPECT DISCREPENCY OCCURED DURING AEROBATIC FLIGHT. DISCOVERED ON 2 ACFT.SDR DOSS12Longeron · crackedFIRST LONGERON (N434BA) WAS FOUND CRACKED AT THE ELEVATOR TRIM GUIDE ATTACH POINT, NEAR THE REAR COCKPIT (RCP) LT RUDDER PEDAL, DURING A SCHEDULED INSPECTION. SUBSEQUENT FINDINGS OCCURRED AS RESULT OF QUALITY DEPARTMENT ISSUING A ONE TIME INSPECTION OF ALL MDSSDR 2005FA0000854Control Cable · frayedLEFT AND RIGHT RUDDER CABLES FOUND FRAYED AT FRONT AND REAR PULLEY POSITIONS.SDR 2002FA0001309Frame · detachedDURING ACCEPTANCE INSPECTION UPON DELIVERY FROM THE CZECHOSLOVAKIA SOCIALIST 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 1
STCs that may be installed
No STCs matched this aircraft’s modelsSTCs are matched through the model’s type certificate data sheet, and this registry model isn’t matched to one.