N426AE
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.
9 reports on file, 2001-03-15 – 2016-09-17.
Part: STIFFENER — CRACKED (ZONE 200) · airframe 3,278 hrs · 7,420 cycles
DURING INSPECTION, FOUND RT SIDE WEB OF THE VERTICAL CONTROLS TUNNEL TO HAVE A CRACK AT THE TOP AFT EDGE OF THE STRUCTURE. UPON DETAILED INSPECTION FOUND THE AFT RT VERTICAL TUNNEL STIFFENER TO BE CRACKED THROUGH.
Part: FITTING — CRACKED (TAILBOOM) · airframe 1,397 hrs · 3,509 cycles
DURING ROUTINE INSPECTION FOUND THE TAIL BOOM FITTING, PN 206-032-409-001, CRACKED.
Part: MODULE — SHORTED (AUTO PILOT)
UNIT INOPERATIVE. POPS NUMBER 2 APM CIRCUIT BREAKER. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (102HN) (K)
Part: BUSS TIE — OPEN (ELECTRICAL BOX)
UNIT INOPERTIVE. NUMBER 1 BUSS TIE STAYS OPEN. Z 200 CORD INSIDE HAS BURN SPOT. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (102HN) (K)
Part: COOLING FAN — INOPERATIVE (INST PANEL)
PROPIMAX FAN INOPERATIVE. FAN WILL NOT ROTATE WHEN POWER APPLIED. REPLACED WITH NEW UNIT CORRECTED PROBLEM. (M)
Part: SEAL — TORN (ENGINE)
BELLOWS IS TORN AROUND CLAMP AND FOLD AREAS. REPLACED WITH NEW UNIT CORRECTED PROBLEM. (M)
Part: LIGHT — INOPERATIVE (ANTI-COLLISION)
ANTI-COLLISION LIGHT INOPERATIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (M)
Part: ENGINE — FOD (LEFT)
FOREIGN OBJECT DAMAGE. DAMAGE OCCURRED PRIOR TO TAKING DELIVERY OF AIRCRAFT. SUSPECT THAT RIVET FRAGMENTS ENTERED ENGINE DURING FINAL PHASE OF AIRFRAME ASSEMBLY.
Part: ENGINE — FOD (RIGHT)
FOREIGN OBJECT DAMAGE. DAMAGE OCCURRED PRIOR TO TAKING DELIVERY OF AIRCRAFT. SUSPECT THAT RIVET FRAGMENTS ENTERED ENGINE DURING FINAL PHASE OF AIRFRAME ASSEMBLY.