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N258BA

Open the Markdown

Let L-23 SUPER BLANIK · NONE

Open in FAA registry

© OpenStreetMap
Registered owner
Omaha Soaring Club Inc
Location
Omaha, NE
Owner type
Corporation
Serial number
938018
Type
Glider
Engine
None
Airworthiness
Standard, glider
Airworthiness date
September 8, 1993
Certificate issued
February 14, 2012
Expires
February 29, 2028
Mode S code
A27550
Let L-23 SUPER BLANIKAirframe model · 2 seats · 83 registeredTCDS G60EUAirframe · Let L-23 SUPER BLANIKEngine modelNONE

From the FAA registry file of October 24, 2026.

On this page

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
Superseded and historical ADs · 1
AD 2010-08-01StabilizersHistoricalEffective Apr 26, 2010 · Replaced by AD 2010-15-05

Information bulletins that may apply

Advisory, not mandatory.

No bulletins matched this aircraft’s models

NTSB investigations

No NTSB investigations matched to N258BAMatched 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 · 1

FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.

Incident 20050807021569ITo Init Climb(1st Pwr Reduct) · White Bear Tnsh, MN(-23) On August 07, this blanik L-23 was being towed to flight at 6MN9. After take-off roll the tow aircraft experienced an inability to generate sufficient power to maintain a successful tow operation. The tow aircraft then radioed pilot of blanik L-23. The…Aug 7, 2005 · Minor damage

Service difficulty reports · 1

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

SDR 2014FA0000716Skin · crackedAFTER LANDING, IT WAS NOTICED THAT THE LANDING GEAR RETRACTION EXTENSION LINKAGES SEEMED LOOSE. FURTHER INVESTIGATION REVEALED A SKIN CRACK HAD DEVELOPED IN FLOOR AREA NR 3 DIRECTLY BENEATH PIVOT ASSY, PN 8X56 333.1 AND THAT THE PIVOT ASSY COULD BE ROCKED FOREDec 19, 2014 · N258BA · Let L23SUPERBLAN · Fuselage Main, Plate/Skin

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.