N914EF

No registry detail on file · not in current registry

Operators of this aircraft

Who operated this tail, and how firmly we know it.

OperatorRolePeriodBasis
CJ Systems Aviation GroupOperatoron 2006-04-21Operator named in NTSB report

Accident & incident history

Accident · 2006-04-21 Operator named in NTSB report
Eurocopter Deutschland EC135T2 Minor injury Part 91CJ Systems Aviation Group

Operated by CJ Systems Aviation Group (per NTSB report)

Source: NTSB case MIA06CA096

Maintenance disclosures

Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.

3 reports on file, 2011-03-07 – 2012-12-20.

WARNING INDICATION · 2012-12-20 Matched by certificate designator
ATA 6320

Part: PINION GEAR — DAMAGED (GEARBOX) · airframe 2,038 hrs · 9,985 cycles

PRIOR TO TAKEOFF, MGB CHIP LIGHT ILLUMINATED. INSPECTED CHIP DETECTOR AND FILTER ELEMENT, FINDINGS CLASSIFIED AS STAGE "B" DEPOSITS IAW SECTION 3, PART 3, FIG 5. REPLACED OIL FILTER AND CLEANED CHIP PLUG. PERFORMED 15 MIN GROUND RUN WITH NO DEFECTS NOTED. CHIP EVENT REQUIRED A TOOTHING INSPECTION IAW ASB EC135-63A-012 WITHIN 10 HOURS. INSPECTED MGB INPUT GEARSETS IAW ASB EC135-63A-012. FOUND PITTING DAMAGE ON SEVERAL TEETH ON NR 2 SIDE INPUT PINION PN: 4649 302 041. FOUND PITTING DAMAGE ON NR 1 & NR 2 SIDE BEVEL GEAR PN: 4649 303 034. IAW THE ASB THE DAMAGE NOTED IS CAUSE FOR REJECTION OF THE MAIN GEARBOX ASSY.

Source: SDR QMLA2012122012198
WARNING INDICATION · 2011-04-02 Matched by certificate designator
ATA 3150

Part: SWITCH PANEL — DEFECTIVE (FADEC) · airframe 1,419 hrs · 6,781 cycles

THE CAD DISPLAYED "IDLE" WHEN FADEC SWITCH WAS TURNED ON. THE ENG WAS NOT RUNNING AT THIS POINT. THE 20VE SWITCH PANEL WAS FOUND TO BE THE CAUSE. THE PANEL WAS REPLACED AND THE ACFT WAS RETURNED TO SERVICE.

Source: SDR QMLA2011040211043
OTHER · 2011-03-07 Matched by certificate designator
ATA 7810

Part: PANEL — DELAMINATED (LT EXHAUST) · airframe 1,399 hrs · 6,662 cycles

THE MECHANIC INSPECTED AND FOUND SOME DELAMINATION ON THE LT REAR ENGINE COWLING PANEL AFT OF THE EXHAUST OUTLET IN EXCESS OF THE LIMITS SPECIFIED IN THE AEC SRM 51-10-11, 2-1, PARA 3. THE MECHANIC HAS SENT THE COWLING TO OUR REPAIR STATION FOR THEIR EVALUATION. THAT EVALUATION HAS DETERMINED THAT THE DAMAGE IS BEYOND THE LIMITS AS THE MECHANIC PREVIOUSLY STATED. AEC WILL BE PROVIDING AN APPROVED REPAIR.

Source: SDR QMLA2011030711032