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Aircraft record

N2011A1995 Schweizer 269C-1

DeregisteredUnclaimedSource: FAA, updated Oct 17, 2026

This N-number isn't registered right now. Below is its last known registration, canceled Oct 29, 2013.

Safety record in brief:1 NTSB accident (destroyed damage, Jul 2008)3 ADs may apply1 service difficulty report

Registration
Deregistered
Last based in
Atherton, CA
owner city / state
Engine
HO-360 · 180 hp
Lycoming
Owners
1
since 2008
NTSB events
1
destroyed, 2008
ADs may apply
3
confirm with A&P
Service reports
1
since 1995

Registration

FAA Aircraft Registry · Oct 17, 2026
Last registered owner
Quadrus INC
Owner type
Corporation
City, state
Atherton, CA
Certificate issued
May 7, 2008
Canceled
Oct 29, 2013
Airworthiness
Standard · Normal
Airworthiness date
Nov 21, 1995

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
Schweizer
Model
269C-1
Year
1995
Serial number
0016
Aircraft type
Rotorcraft
Category
Land
Certification
Type Certificated
Seats
3
Engines
1
Max takeoff weight
Up to 12,499 lb
Type certificate data sheet
4H12
Mode S code
A19836

Engine

Make and model
Lycoming Ho-360
Type
Reciprocating
Power
180 hp

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

Ownership history

Ownership history from FAA records
  1. 2008 – 2013Quadrus INCAtherton, CA

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 17, 2026 · SDRs · Oct 16, 2026

NTSB events (1)

Accident · destroyed

Jul 4, 2008 · Sunol, CA

The pilots' failure to maintain adequate clearance from transmission wires during cruise flight. Contributing to the accident were the dark night and low fog.

Damage
Destroyed
Injuries
Fatal
Report
LAX08LA213

From NTSB records; matched by serial number.Read NTSB report (search CAROL for LAX08LA213)

Accident history for this model

ADs published since 1998 that may apply (3)

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.

ADSubjectEffectiveApplies to
2017-14-06Sikorsky Aircraft Corporation Helicopters (Type Certificate Previously Held by Schweizer…Aug 25, 2017Airframe (269C-1)Only with: Lower coupling driveshaft P/N 269-5412, 269A5504, 269A5504-003, 269A5504-005, 269A5559, or 269A5559-003 installed.
2015-23-01Sikorsky Aircraft Corporation (Type Certificate Previously Held by Schweizer Aircraft…Dec 15, 2015Airframe (269C-1)
99-17-10Schweizer Aircraft Corporation Model 269A, 269A-1, 269B, 269C, 269C-1, and 269D…Sep 2, 1999Airframe (269C-1)Only with: Tail rotor swashplate shaft P/N 269A6049-3 installed.

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

Service Difficulty Reports (1)

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.

  • Fuselage · strut · crackedNov 9, 1998

    ONE INCH CRACK LOCATED AT UPPER PART OF DRIVE PULLEY FRAME STRUT ASSEMBLY. CRACK ORIGINATED AT WELD.

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

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 17, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 17, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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