Models / Hughes / 269A / N90270 Aircraft record N90270 1966 Hughes 269A Registration valid Unclaimed Source: FAA, updated Oct 17, 2026Safety record in brief: 3 NTSB accidents (substantial damage at worst, latest Jun 2023) · 5 ADs may apply
Registration Valid expires Apr 30, 2028 NTSB events 3 substantial, 2023 ADs may apply 5 confirm with A&P Service reports 0 since 1995
Registration FAA Aircraft Registry · Oct 17, 2026
Registered owner Co-owners
City, state Anderson, SC
Certificate issued Apr 21, 2015
Expires Apr 30, 2028
Airworthiness Standard · Normal
Airworthiness date Apr 5, 1979 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 Hughes
Model 269A
Year 1966
Serial number 66-18283
Aircraft type Rotorcraft
Category Land
Certification Type Certificated
Seats 2
Engines 1
Max takeoff weight Up to 12,499 lb
Type certificate data sheet 4H12
Mode S code AC7A00 Engine
Make and model Lycoming Hio-360 Ser
Type Reciprocating
Power 205 hp Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history Ownership history from FAA records 2015 – now Co-owners Anderson, SC · current 1966 Intermountain Aviation INC different airframe: Beechcraft Snb-5 S/N 39777 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 (3)
Accident · substantial damage Jun 27, 2023 · Anderson, SC The mechanics’ improper torquing of the main rotor blade dampers, which resulted in a ground resonance event during landing.
Damage Substantial
Injuries None
Report ERA23LA289 From NTSB records; matched by serial number. Read NTSB report (search CAROL for ERA23LA289)
Accident · substantial damage Dec 26, 1990 · Sellersburg, IN A PILOT INDUCED LOSS OF ENGINE POWER BY INADVERTENT DEACTIVATION OF THE FUEL MIXTURE CONTROL.
Damage Substantial
Injuries None
Report CHI91LA048 From NTSB records; matched by serial number. Read NTSB report (search CAROL for CHI91LA048)
Accident · substantial damage Feb 20, 1987 · Jacksonville, FL THE INSTRUCTOR PLT WAS DEMONSTRATING A HOVERING AUTOROTATION LANDING WITH FORWARD MOVEMENT, WHEN, AFTER THE THROTTLE WAS CLOSED, THE HELICOPTER HUNG IN THE AIR. FORWARD CYCLIC WAS THEN APPLIED WHEN HE REALIZED THAT THE ROTOR RPM BEGAN TO DETERIORATE. THE HELICOPTER THEN CONTACTED THE GROUND IN A SLIGHT NOSE LOW ATTITUDE, AFTER WHICH, REAR CYCLIC WAS APPLIED. THE MAIN ROTOR BLADES THEN SEVERED…
Damage Substantial
Injuries None
Report MIA87LA089 From NTSB records; matched by serial number. Read NTSB report (search CAROL for MIA87LA089)
Accident history for this model ADs published since 1998 that may apply (5) 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.
AD Subject Effective Applies to 2017-14-06 Sikorsky Aircraft Corporation Helicopters (Type Certificate Previously Held by Schweizer… Aug 25, 2017 Airframe (269A)Only with: Lower coupling driveshaft P/N 269-5412, 269A5504, 269A5504-003, 269A5504-005, 269A5559, or 269A5559-003 installed. 2015-23-01 Sikorsky Aircraft Corporation (Type Certificate Previously Held by Schweizer Aircraft… Dec 15, 2015 Airframe (269A) 2001-25-52 Schweizer Aircraft Corporation Model 269A, 269A-1, 269B, 269C, and TH-55A Helicopters May 8, 2002 Airframe (269A)Only with: With tailboom support strut assemblies P/N 269A2015 or 269A2015-5, tailboom center attach fitting P/N 269A2324, or center frame aft cluster fitting P/N 269A2234 or 269A2235 installed. 99-17-10 Schweizer Aircraft Corporation Model 269A, 269A-1, 269B, 269C, 269C-1, and 269D… Sep 2, 1999 Airframe (269A)Only with: Tail rotor swashplate shaft P/N 269A6049-3 installed. 95-21-02 Schweizer Aircraft Corporation and Hughes Helicopters, Inc. Model 269A, 269A-1, 269B… Nov 17, 1995 Airframe (269A)Only with: Main rotor drive shaft P/N 269A5305-3 or 269A5305-11 installed, except drive shafts with serial number prefix "SZ" or "ZS".
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (0) No Service Difficulty Reports found for this airframe since 1995.
Sources FAA Aircraft Registry Registration, owner city and state, airframe, engine updated Oct 17, 2026 NTSB accident and incident database Accidents and incidents since 1982 updated Oct 15, 2026 FAA Airworthiness Directives (Federal Register) ADs published since 1998 updated Oct 17, 2026 FAA Service Difficulty Reports Reports since 1995 updated Oct 16, 2026 Request owner name removal Report an error in this record