Safety record in brief:2 NTSB accidents (substantial damage at worst, latest Jul 2023)3 ADs may apply42 service difficulty reports
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Fatigue failure of the overrunning clutch outer race and a subsequent inflight loss of power due to abnormal bending loads as a result of improper reassembly of the clutch subassembly following maintenance and the presence of microcracks on the clutch’s outer race.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for ERA23LA293)
The malfunction of the emergency fuel vent and the exhaustion of the fuel supply which resulted in the loss of engine power.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for BFO94LA155)
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 |
|---|---|---|---|
| 2006-16-04 | Rolls-Royce Corporation (Formerly Allison Engine Company, Allison Gas Turbine Division… | Sep 7, 2006 | Engine (250-C20B) |
| 2006-13-06 | Rolls-Royce Corporation (Formerly Allison Engine Company, Allison Gas Turbine Division… | Jul 26, 2006 | Engine (250-C20B)Only with: Engines with gas producer rotor assembly tie bolt P/Ns A23008020, E23008020 (EXTEX), 23008020, 6843388, 6876991 (RRC), A23008020 (SAP), or 23008020P (Pacific Sky Supply) installed. |
| 2005-10-13 | Rolls-Royce Corporation (Formerly Allison Engine Company) 250-B17B, -B17C, -B17D, -B17E… | Jun 22, 2005 | Engine (250-C20B)Only with: Engines that do not have turbine energy absorbing ring RRC P/N 23035175, or an equivalent FAA-approved serviceable ring, 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.
FUEL PUMP INOPERATIVE.
From FAA Service Difficulty Reports; matched by N-number and serial number.DUAL TACH INDICATOR NOISY.
From FAA Service Difficulty Reports; matched by N-number and serial number.MAKES ENGINE RUMBLE AT IDLE; ENGINE N1 DECREASES 1/2 TO 1 PERCENT WITH START PUMP ON AND RETURNS TO NORMAL WHEN OFF.
From FAA Service Difficulty Reports; matched by N-number and serial number.LOW ROTOR RPM ACTUATES WHEN EPO IS ACTIVATED.
From FAA Service Difficulty Reports; matched by N-number and serial number.TAIL ROTOR BELLCRANK EARS WORN AND SPRUNG.
From FAA Service Difficulty Reports; matched by N-number and serial number.TAIL ROTOR PITCH CONTROL IS WORN EXCESSIVELY.
From FAA Service Difficulty Reports; matched by N-number and serial number.FUEL VENT LINE IS BENT.
From FAA Service Difficulty Reports; matched by N-number and serial number.PART WARNING SIGNAL ACTIVATES.
From FAA Service Difficulty Reports; matched by N-number and serial number.PART IS WORN EXCESSIVELY.
From FAA Service Difficulty Reports; matched by N-number and serial number.PART IS WORN EXCESSIVELY.
From FAA Service Difficulty Reports; matched by N-number and serial number.Showing the 10 most recent of 42 reports.