N350LF
Registered owner: AIR METHODS LLC, CO (owner ≠ operator)
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.
5 reports on file, 2010-11-11 – 2025-10-23.
Part: DECK PLATE — DENTED (ZONE 200) · airframe 7,197 hrs · 15,729 cycles
A DENT WAS DISCOVERED ON THE TRANSMISSION DECK. THE DAMAGE MEASURES APPROX. 0.6" LONG, 0.6" WIDE WITH A MAXIMUM DEPTH OF 0.0120".
Part: ACCESS DOOR — CHAFED (BATTERY BAY) · airframe 4,701 hrs · 12,755 cycles
BATTERY ACCESS DOOR IN LT SIDE OF TAIL BOOM. DESCRIPTION NR 1: INTERNAL DOUBLER FOR BATTERY DOOR CUT OUT IS CRACKED AT UPPER FORWARD AND UPPER AFT CORNERS NEAR DOOR HINGE, NR 2: LOWER ANGLE DOUBLER HAS 100 % THICKNESS CHAFE DAMAGE FROM BATTERY DOOR LOWER CAMLOCK FASTENERS, NR 3; LOWER CAMLOCK RECEPTCALS HAVE BEEN MODFIED TO TRY TO MAKE THEM FIT INTO LOWER.
Part: DECK PLATE — CHAFED (ENGINE BAY) · airframe 4,701 hrs · 12,755 cycles
DAMAGE TO THE ENGINE DECK (PN: 350A21-1239.21) IN THE FORM OF A CHAFE. THE DAMAGE AREA WAS DISCOVERED TO BE JUST AFT OF THE SCUPPER DRAIN HOLE AND IS APPROXIMATELY 0.50 LONG, 0.375 WIDE, AND 0.015 DEEP AT THE DEEPEST POINT. THE REMAINDER OF THE CHAFE EXTENDS INBOARD AND OUTBOARD, BUT IS MEASURED TO BE APPROXIMATELY 0.003 DEEP.
Part: STRUCTURE — CORRODED (FLOOR) · airframe 4,701 hrs · 12,755 cycles
CORROSION WAS DISCOVERED ON THE RIGHT AND LEFT SIDE CABIN FLOOR EDGE SECTION.
Part: BEARING RACE — DEBONDED (MAIN ROTOR MAST) · airframe 848 hrs · 2,557 cycles
MAST BEARING INNER RACE HAS BECOME DEBONDED FROM THE MAIN ROTOR SHAFT.