N354CF
Registered owner: TRISTATE CAREFLIGHT 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, 2020-02-07 – 2025-01-30.
Part: BEAM — DAMAGED (ZONE 100) · airframe 5,763 hrs · 13,382 cycles
FASTENER HOLE DAMAGE (ELONGATION) WAS DISCOVERED ON THE LH MAINTENANCE FOOTSTEP BEAM (P/N 350A21124520) IN THE FUSELAGE REAR STRUCTURE.
Part: BULKHEAD — CHAFED (ZONE 100) · airframe 4,292 hrs · 10,625 cycles
DURING INSPECTION FOUND A CHAFE IN THE RIGHT HAND LATERAL BULKHEAD (X-FRAME) ON THE EXTERIOR SIDE AND IS .022" DEEP
Part: BULKHEAD — CHAFED (BS 4174) · airframe 4,292 hrs · 10,625 cycles
FOUND CHAFE DAMAGE AT THE BACK BAGGAGE COMPARTMENT ON THE FORWARD WALL IN THE TAILBOOM. STA.4174, BL. R355, WL. 2672.2. ATTACHED ARE THE PICTURES OF THE DAMAGE. THERE ARE 3 SEPARATE AREAS THAT MEASURE 10 IN. IN TOTAL LENGTH. THE DEEPEST GOUGE RUNS .028 IN.
Part: CABLE — UNKNOWN · airframe 4,292 hrs · 10,625 cycles
THE METAL FUEL CABLE FROM THE NEW CRFT. L/H INBOARD LOWER AFT LEG ON XFRAME, MAX DEPTH OF .009 APPROX LOCATION OF Z-2867 , X-3705, Y(-398)
Part: LONGERON — DAMAGED (XMSN DECK) · airframe 4,292 hrs · 10,625 cycles
CHAFING WAS DISCOVERED ON THE LOWER FLANGE OF THE TRANSMISSION DECK LONGERON AT APPROXIMATE STA AND RBL . THE DAMAGE MEASURES APPROXIMATELY 0.006â DEEP, 0.80â LONG, AND 0.12â WIDE. Y398, X3300, Z-1863. THE TAIL ROTOR YAW CABLE HAS .007 DEEP CHAFFING ON THE CORNER OF A CHANNEL.