Safety record in brief:1 NTSB accident (substantial damage, Jun 2001)5 ADs may apply1 service difficulty report
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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 rotor rpm during a practice autorotational landing, which resulted in a hard landing.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for LAX01LA219)
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.
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.
TENSION SPRING FOR MAIN ROTOR DRIVE CLUTCH ACTUATOR FAILED. RECEIVED AND INSTALLED NEW SPRING ON 27 JAN 95. AIRCRAFT FLEW ON 19 FEB 95 AND BROKEN SPRING WAS DISCOVERED ON DAILY INSPECTION ON THE MORNING OF 20 FEB 95.
From FAA Service Difficulty Reports; matched by N-number and serial number.