This N-number isn't registered right now. Below is its last known registration, canceled Jul 8, 2013.
Safety record in brief:2 NTSB accidents (destroyed damage at worst, latest Nov 2009)4 ADs may apply3 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 pilot became spatially disoriented while maneuvering on a dark night, which resulted in a loss of helicopter control.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for WPR10FA055)
FAILURE OF THE FAA FLIGHT EXAMINER (F/E) TO FOLLOW PROPER PROCEDURES CONCERNING THE AUTOROTATION, AND IMPROPER REMEDIAL ACTION BY THE PILOT-IN-COMMAND (PIC). FACTORS RELATED TO THE ACCIDENT WERE: LACK OF INFORMATION IN THE FLIGHT MANUAL CONCERNING AUTOROTATIONS, THE FLIGHT EXAMINER'S LACK OF EXPERIENCE IN THE AIRCRAFT, AND THE SOFT TERRAIN AND MOUND OF DIRT (DIRT BANK) IN THE EMERGENCY LANDING…
From NTSB records; matched by serial number.Read NTSB report (search CAROL for NYC89FA089)
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 |
|---|---|---|---|
| 2011-23-13 | Honeywell International Inc. Turboshaft Engines | Nov 29, 2011 | Engine (LTS101-600A3A)Only with: Power turbine governor (PTG) model AL-AB1, P/N 4-301-289-03, 4-301-289-05, 4-301-289-09, 4-301-101-16, or 4-301-101-18 installed, marked with compliance symbol N or P, or with no compliance symbol, on the PTG identification plate. |
| 2011-08-06 | Honeywell International Inc. LTS101 Series Turboshaft Engines and LTP101 Series… | May 17, 2011 | Engine (LTS101-600A3A)Only with: Power turbine rotor P/N 4-141-290-01, -02, -03, -05, -06, -11, -12, -13, -14, or -16 installed. |
| 2009-24-12 | Honeywell International Inc. LTS101 Series Turboshaft and LTP101 Series Turboprop Engines | Jan 4, 2010 | Engine (LTS101-600A3A)Only with: Engines with certain gas generator turbine discs, P/N 4-111-015-14, installed. |
| 2001-22-07 | Honeywell International, Inc. LTP 101 Series Turboprop and LTS101 Series Turboshaft… | Nov 30, 2001 | Engine (LTS101-600A3A)Only with: Rigid tube fuel manifolds P/N 4-301-042-02, -04, -05, -06, 4-301-236-01, -02, -03, -04, 4-301-286-01, -02, or 4-301-376-01 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.
EXHAUST STACK ASSY FOUND TO BE CRACKED AT RELIEF POINTS AROUND BASE IN 2 PLACES. 1ST STACK LASTED 411.1 HOURS, THEN INSTALLED REPAIRED STACK, THIS LASTED APPROX 200 HOURS WITH CRACKS IN SAME PLACE AS WELL AS AT TIP OF CONE. THE 3RD STACK CRACKED UPON INSTALLATION AT BASE RELIEF POINTS ALONG THE…
From FAA Service Difficulty Reports; matched by N-number and serial number.A REDUCED FUEL FLOW CONDITION DEVELOPED AS THE ELECTRIC FUEL BOOST PUMP BEGAN TO DISINTEGRATE AS IT NEARED IT TBO (APPROX 70 HRS TO REPLACEMENT). INTRODUCING METAL AND CONTAMINATING THE AIRFRAME FUEL FILTER, THIS IS A BYPASS CONDITION AND PROVIDED UNFILTERED FUEL TO THE FUEL CONTROL UNIT. THE…
From FAA Service Difficulty Reports; matched by N-number and serial number.AT APPROXIMATELY 0200, 22 DEC, 2006, WHILE RETURNING FROM A MEDICAL TRANSFER, AIRCRAFT EXPERIENCED AN ENGINE FAILURE WHILE IN CRUISE FLIGHT. PILOT INITIATED AN AUTOROTATION AND SUCCESSFULLY LANDED THE AIRCRAFT APPROXIMATELY 5SM WEST OF 4SD WITHOUT DAMAGE OR INJURY TO HIMSELF OR THE OTHER 2 CREW…
From FAA Service Difficulty Reports; matched by N-number and serial number.