This N-number isn't registered right now. Below is its last known registration, canceled Mar 29, 2001.
Safety record in brief:1 NTSB accident (destroyed damage, Mar 1999)4 ADs may apply92 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 loss of control as a result of the spring-steel extension becoming entangled with the hatch door handle during takeoff. A contributing factor was the flat design of the spring-steel extension.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for FTW99FA094)
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.
HOSE WORN.
From FAA Service Difficulty Reports; matched by N-number and serial number.PAD CORRODED BEYOND LIMITS. REPLACED WITH SERVICEABLE PART.
From FAA Service Difficulty Reports; matched by N-number and serial number.RIGHT PAD ASSEMBLY HAD CORROSION BEYOND LIMITS. REPLACED WITH SERVICEABLE PART.
From FAA Service Difficulty Reports; matched by N-number and serial number.PITCH ROD HAS WORN BEARING.
From FAA Service Difficulty Reports; matched by N-number and serial number.FREQUENTY ADAPTER HAS RUBBER SEPARATED. SERIAL NUMBERS REMOVED ARE 9401, 9421, AND 9395.
From FAA Service Difficulty Reports; matched by N-number and serial number.BRAKE ASSEMBLY HAS RUBBER SEPARATED.
From FAA Service Difficulty Reports; matched by N-number and serial number.BEARINGS WORN. PART SCRAPPED ON SITE.
From FAA Service Difficulty Reports; matched by N-number and serial number.ROD, PITCH CONTROL BEARINGS WORN.
From FAA Service Difficulty Reports; matched by N-number and serial number.TAIL ROTOR BEARINGS ROUGH AND SEALS HARD.
From FAA Service Difficulty Reports; matched by N-number and serial number.WORN ROD END BEARINGS. SERIAL NUMBERS REMOVED ARE PMA33051 AND PMA1403.
From FAA Service Difficulty Reports; matched by N-number and serial number.Showing the 10 most recent of 92 reports.