This N-number isn't registered right now. Below is its last known registration, canceled Sep 14, 2015.
Safety record in brief:1 NTSB accident (substantial damage, May 2008)6 ADs may apply1 service difficulty report
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 compensate for the excessive rate of descent on final approach. A contributing factor was the reported down draft.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for DFW08TA137)
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 |
|---|---|---|---|
| 2015-23-01 | Sikorsky Aircraft Corporation (Type Certificate Previously Held by Schweizer Aircraft… | Dec 15, 2015 | Airframe (269D) |
| 2015-11-09 | Sikorsky Aircraft Corporation (Type Certificate Previously Held by Schweizer Aircraft… | Jul 14, 2015 | Airframe (269D)Only with: Ring gear carrier assembly P/N 269A5194 installed. |
| 2010-16-08 | Schweizer Aircraft Corporation (Schweizer) Model 269D Helicopters | Aug 20, 2010 | Airframe (269D) |
| 2003-09-05 | Schweizer Aircraft Corporation Model 269D Helicopters | May 16, 2003 | Airframe (269D)Certain serial numbers: 269D 0001–0022. Only with: Aluminum horizontal stabilizer endplate P/N 269D3413-11 installed. |
| 99-17-10 | Schweizer Aircraft Corporation Model 269A, 269A-1, 269B, 269C, 269C-1, and 269D… | Sep 2, 1999 | Airframe (269D)Only with: Tail rotor swashplate shaft P/N 269A6049-3 installed. |
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 98-26-06 | Schweizer Aircraft Corporation Model 269D Helicopters | Feb 3, 1999 | Airframe (269D)Only with: Large diameter main rotor hub P/N 269A1002-11 and main rotor drive shaft P/N 269A5305-139, -143, -145, or -147 installed. |
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.
OIL COOLER IMPELLER WAS INSPECTED FOR CRACKS IN THE BLADE/SHOUD REGION IAW MFG RECOMMENDATIONS EVERY 100 HRS OF OPERATION. 2 CRACKS WERE CONFIRMED AND SEVERAL OTHERS SUSPECTED. THE CURRENTLY MFG IMPELLER, 269D4530-001, IS APPARENTLY THE LATEST GENERATION THAT EVOLVED FROM PREVIOUS INCIDENTS AND…
From FAA Service Difficulty Reports; matched by N-number and serial number.