This N-number isn't registered right now. Below is its last known registration, canceled Mar 25, 2024.
Safety record in brief:1 NTSB accident (substantial damage, Dec 2014)4 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 prevent the helicopter from settling with power while maneuvering at a low altitude, which resulted in a loss of control and subsequent hard landing.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for WPR15CA063)
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 |
|---|---|---|---|
| 2013-23-09 | Eurocopter France Helicopters | Dec 27, 2013 | Airframe (AS 350 B2 ECUREUIL)Only with: Helicopters with sliding doors installed, except those with modification AL.4262. |
| 2013-21-01 | Eurocopter France (Eurocopter) Helicopters | Oct 25, 2013 | Airframe (AS 350 B2 ECUREUIL)Only with: Tail rotor hub pitch horn assembly P/N 350A121368.01, .02, .03, or .04, with pitch horn P/N 350A121368.XX, installed. |
| 2013-08-19 | Eurocopter France Helicopters | Jun 5, 2013 | Airframe (AS 350 B2 ECUREUIL)Only with: Sliding door pre-modification (MOD) 073298 or pre-MOD 073308 installed. |
| 2010-11-51 | Eurocopter France (Eurocopter) Model AS350B, BA, B1, B2, C, D, and D1 Helicopters and… | Sep 2, 2010 | Airframe (AS 350 B2 ECUREUIL)Only with: Tail gearbox control lever P/N 350A33-1058-00, -01, -02, or -03 not marked with an "X" near the P/N 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.
DURING COMPLIANCE WITH AD, INSPECTED BOTH CONTROL RODS. FOUND BOTH BUSHINGS IN ELASTOMERIC BEARING CRACKED THROUGH TO BOTH ENDS. BOTH CONTROL RODS REJECTED FROM FURTHER SERVICE. INSTALLED NEW CONTROL RODS. NO RECORD OF REPLACEMENT IN AC LOGBOOK. THIS PUTS THE CONTROLS RODS AT PLUS 1528 HOURS TIME…
From FAA Service Difficulty Reports; matched by N-number and serial number.