N192AE
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.
5 reports on file, 2010-04-29 – 2024-04-11.
Part: B-NUT — LOOSE (FUEL SYSTEM) · airframe 24,846 hrs · 55,584 cycles
CREW REPORTS STRONG FUEL SMELL IN AFT CABIN. FINDINGS: REMOVED CENTER AFT FACING SEAT PANEL AND ACCESS COVER TO GAIN ACCESS TO FUEL SYSTEM. FOUND FUEL SEEPING AT AFT B-NUT OF EJECTOR PUMP. TIGHTENED B-NUT AND PERFORMED LEAK CHECK WITH BOOST PUMPS ON WITH NO LEAKS NOTED. REINSTALLED ACCESS COVER AND SEAT PANEL. WORK DONE IN REFERENCE TO BHT-206L1-MM-CH28. PARTICIPATING MECHANICS: JOHN WILKINSON AND DUANE RICHEY
Part: PANEL — CRACKED (BS 209) · airframe 24,846 hrs · 55,584 cycles
DURING SCHEDULED MAINTENANCE EVENT AMT FOUND 2.0" LONG CRACK IN AIRFRAME AT OIL COOLER BLOWER SHAFT HANGER ASSEMBLY, AFT RH, ATTACHMENT POINT. APPROXIMATE STA 209.0, WL 73.586.
Part: TACH GENERATOR — FAILED (HYDRAULIC SYS) · airframe 21,367 hrs · 48,215 cycles
DURING FLIGHT PILOT LOST HYDRAULIC POWER TO FLIGHT CONTROLS AND PERFORMED AN UNPLANNED LANDING AT AN AIRPORT. DURING MAINTENANCE INVESTIGATION IT WAS FOUND THAT THE SPLINES IN THE TACHOMETER GENERATOR DRIVE THAT DRIVE THE SHAFT FOR THE HYDRAULIC PUMP HAD FAILED.
Part: ATTACH FITTING — CRACKED (TAILBOOM) · airframe 20,527 hrs · 46,438 cycles
UPPER LT TAILBOOM ATTACHMENT FITTING, PN: 206-032-409-001P, CRACKED.
Part: FRAME — CRACKED (AFT BULKHEAD) · airframe 17,270 hrs · 38,672 cycles
DURING THE INSTALLATION OF A BELL KIT (BHT-SI-2050) TAILBOOM REQUIRED REMOVAL FOR REPLACEMENT. AFTER REMOVAL OF TAILBOOM, CRACKED NOTICED ON AIRFRAME AFT BULKHEAD RING. AIRFRAME AFT BULKHEAD RING R & R.