N440AE
Registered owner: AIR EVAC EMS INC, MO (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| Air Evac EMS, Inc. (EVCA) | 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.
7 reports on file, 2000-12-04 – 2024-08-20.
Part: BULKHEAD — CRACKED (ZONE 100) · airframe 7,766 hrs
LH FS 145 & STIFFENER CLIP CRACKED
Part: BULKHEAD — CRACKED (ZONE 100) · airframe 7,766 hrs
RH FS 145 & STIFFENER CLIP CRACKED
Part: MOTOR — UNKNOWN (EVAPORATOR BLWR) · airframe 6,943 hrs · 18,545 cycles
SLIGHT ELECTRICAL BURNING SMELL COMING FROM THE AC DUCTING. HAPPENS WITH AC ON OR BLOWER ONLY.
Part: ATTACH FITTING — CRACKED (TAILBOOM) · airframe 4,125 hrs · 21,191 cycles
DURING INSPECTION, THE TAILBOOM UPPER LH ATTACHMENT FITTING WAS VISUALLY IDENTIFIED AS CRACKED.
Part: STIFFENER — CRACKED (FUSELAGE) · airframe 3,857 hrs · 10,732 cycles
VERTICAL TUNNEL AFT RT CORNER STIFFENER CRACKED.
Part: SHAFT — JAMMED (MAIN ROTOR) · airframe 1,380 hrs · 3,644 cycles
WHILE REPLACING A LEAKING HYD PUMP & LEAKING TRANSMISSION OIL PUMP, IT WAS DISCOVERED THAT THE ROTOR TACH GEN TO HYD PUMP DRIVE SPLINES, SHAFT PN 20546AA, WERE SEIZED IN THE ROTOR TACH GEN. APPARENT CAUSE WAS OIL & HYD FLUID WASHING OUT LUBRICATING GREASE.
Part: COMPUTER — FAILED (NR 1 MFC)
MCO - FLT 5276 - AIRCRAFT LOST ALL BRAKING POWER ON TAXI-OUT. FOUND MFC 1 FAILING CROSSTALK CHECK REMOVED AND REPLACED NR 1 MFC SYSTEM. OPS CHECKED GOOD IAW ATR 72 AMM 31-48-21 RAI 11000-001. (M)