This N-number isn't registered right now. Below is its last known registration, canceled Jul 18, 2017.
Safety record in brief:1 NTSB accident (substantial damage, Jun 2002)4 ADs may apply3 service difficulty reports
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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.
A loss of tail rotor effectiveness and the pilot's failure to maintain control of the helicopter. Factors associated with the accident were the binding of the tail rotor pitch changed rod, the gusty wind conditions, and the pilot’s lack of total experience in this make and model of helicopter.
From NTSB records; matched by N-number.Read NTSB report (search CAROL for CHI02FA174)
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)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)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)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)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.
VHF/FM TRANSCEIVER, UNIT INOPERATIVE. TRANSMITS FIRST TIME THEN FAILS TO TRANSMIT EVEN WHILE TRANSMIT LIGHT IS ILLUMINATED. ANTENNA CHECKS, OK. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
From FAA Service Difficulty Reports; matched by N-number and serial number.ENGINE OIL PRESSURE TRANSMITTER INOPERATIVE. FAULTY INDICATION. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (M)
From FAA Service Difficulty Reports; matched by N-number and serial number.ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT FROM 1 EACH KIT P/N 355A09-1036-01 CORRECTED PROBLEM. FOUR HALF SHELLS EQUALS 1 KIT. (M)
From FAA Service Difficulty Reports; matched by N-number and serial number.