This N-number isn't registered right now. Below is its last known registration, canceled Mar 16, 2001.
Safety record in brief:1 NTSB accident (substantial damage, Aug 1995)5 ADs may apply2 service difficulty reports
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Individual owners are shown by city and state only.
The pilot's failure to maintain adequate terrain clearance which resulted in an inflight collision with the ground.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for NYC95TA190)
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 (269C)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 (269C) |
| 2001-25-52 | Schweizer Aircraft Corporation Model 269A, 269A-1, 269B, 269C, and TH-55A Helicopters | May 8, 2002 | Airframe (269C)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 (269C)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 (269C)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.
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.
THE NEW STYLE CANOPY SLAT (ALUMINUM) REPLACES THE FIBERGLASS SLATS. THE ALUMINUM SLAT APPEARS TO BE MANUFACTURED TOO WIDE TO FIT PROPERLY ON THE CANOPY. THIS RESULTS IN THE SLAT BEING BOWED AT THE CENTER WHEN INSTALLED. THE CENTER SLAT SUPPORT PULLED AWAY FROM THE SLAT, WHILE IN-FLIGHT, AT THE…
From FAA Service Difficulty Reports; matched by N-number and serial number.THIS CANOPY SLAT IS A NEW DESIGN FROM SCHWEIZER. IT IS OF ALL ALUMINUM CONSTRUCTION AND REPLACES THE OLDER FIBERGLASS SLAT. THIS NEW TYPE SLAT APPEARS TO BE SLIGHTLY WIDER THAN THE PREVIOUS TYPE. WHEN IT'S BOLTED TO THE CABIN, IT BOWS SLIGHTLY AT THE CENTER SECTION. THE MFG WAS NOTIFIED BY US…
From FAA Service Difficulty Reports; matched by N-number and serial number.