N895CR

PILATUS AIRCRAFT LTD PC-12/47 · 2007 · Fixed-wing single-engine · 1 engine · 12 seats · Valid Registration

Registered owner: AIR METHODS LLC, CO (owner ≠ operator)

Operators of this aircraft

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

OperatorRolePeriodBasis
Air Methods Corp. (QMLA)Certificate holderMatched by certificate designator

Accident & incident history

No NTSB accidents or incidents on file for this aircraft.

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, 2023-07-27 – 2025-02-27.

PARTIAL RPM/PWR LOSS · 2025-02-27 Matched by certificate designator
ATA 7532

Part: BLEED VALVE — MALFUNCTIONED (ENGINE) · airframe 8,709 hrs · 7,413 cycles

UPON DEPARTURE, SET MY POWER TO ROUGHLY 34.5 TORQUE & AFTER ROTATION, ATTEMPTED TO ADD MORE POWER. WHEN ADDED MORE POWER NOTHING HAPPENED & TORQUE STAYED AROUND 34.5 AND THE ITT STAYED AROUND 680. PLACED PCL FULL FORWARD AND POWER NEVER INCREASED. AT THAT TIME IINCREASED RATE OF CLIMB & LET ATC KNOW WAS GOING TO RETURN TO AIRPORT. HAD SUFFICIENT ALTITUDE AND PREPARED FOR AN EMERGENCY IF NECESSARY. LANDED WITH OUT ANY ISSUES & MX WAS IMMEDIATELY CONTACTED ABOUT THE REDUCED POWER. REMOVED AND INSTALLED NEW P3 AIR FILTER, REMOVED AND INSTALLED NEW COMPRESSOR BLEED VALVE,

Source: SDR QMLA2025022720029
WARNING INDICATION · 2024-06-10 Matched by certificate designator
ATA 3297

Part: CIRCUIT BREAKER — TRIPPED (MLG) · airframe 7,970 hrs · 8,384 cycles

DURING TAKE OFF THE GEAR DID NOT RETRACT SO THE FLIGHT WAS ABORTED AFTER FINDING THE CIRCUIT BREAKER WAS OUT. MAINTENANCE FOUND THAT THE HYD. CTR (NON ESSENTIAL BUS) POPPED. RESET CIRCUIT BREAKER, NO DEFECTS NOTED.

Source: SDR QMLA2024061020061
WARNING INDICATION · 2023-07-27 Matched by certificate designator
ATA 2900

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 6,928 hrs · 4,501 cycles

EN ROUTE TO HOME STATION, THE HYDRAULIC CAWS LIGHT ILLUMINATED. QRH PROCEDURES WERE FOLLOWED AND THE LANDING GEAR WAS PUMPED DOWN MANUALLY. AIRCRAFT LANDED WITHOUT FURTHER EVENT. MAINTENANCE FOUND THE HYDRAULIC SYSTEM NITROGEN PRECHARGE TO BE LOW, CAUSING THE HYDRAULIC PUMP TO CYCLE ON AND OFF EXCESSIVELY, WHICH LED TO THE HYDRAULIC CAWS CAUTION LIGHT ILLUMINATING.

Source: SDR QMLA2023073120057