N951AL
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| Air Methods Corp. (QMLA) | Certificate holder | — | Matched 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, 2015-04-21 – 2018-10-16.
Part: CHIP DETECTOR — ACTIVATED (TRANSMISSION) · airframe 6,750 hrs · 29,207 cycles
XMSN OIL CHIP (YELLOW CAUTION LIGHT) ILLUMINATED IN FLIGHT. IN ACCORDANCE WITH THE RFM SUPPLEMENT PAGES, ATTEMPTED TO EXTINGUISH THE CAUTION LIGHT WITH MOMENTARY ACTIVATION OF THE "CHIP BURNER" SWITCH. CAUTION LIGHT REMAINED ILLUMINATED. IN ACCORDANCE WITH RFM EMERGENCY AND MALFUNCTION PROCEDURES PAGE 3-9, REDUCED POWER AND LANDED AS SOON AS POSSIBLE.
Part: VERTICAL GYRO — INOPERATIVE (COCKPIT) · airframe 6,650 hrs · 28,849 cycles
AIRCRAFT BEGAN TO MAKE LEFT AND RIGHT UN-COMMANDED ROLL INPUTS. THE INPUTS INCREASED IN AMPLITUDE AND RATE OVER THE COURSE OF THE NEXT TWO MINUTES. NO AIRCRAFT CAUTION INDICATIONS CAME ON, ISOLATED THE INPUTS USING SAS SWITCHES, ONCE SAS 2 WAS SWITCHED OFF, THE INPUTS STOPPED.
Part: LONGERON — CRACKED (FUSELAGE) · airframe 5,009 hrs · 22,175 cycles
WHILE PERFORMING AN AIRWORTHINESS CHECK, THE MECHANIC FOUND A 50 MILLIMETER HAIRLINE CRACK IN THE SKIN OF THE LT AFT FUSELAGE, STATION 5460, JUST ABOVE THE BAGGAGE COMPARTMENT DOOR. FURTHER INVESTIGATION REVEALED THAT THE UPPER LT LONGERON OF THE AFT FUSELAGE IS CRACKED AT STATION 5460, WL 1285 & LBL 450, ALL STATIONS REFLECTED IN MILLIMETERS.