N63AE

BELL HELICOPTER TEXTRON 206L-1 · Rotorcraft · 1 engine · 7 seats · Valid Registration

Registered owner: AIR EVAC EMS INC, MO (owner ≠ operator)

Operators of this aircraft

Who operated this tail, and how firmly we know it.

OperatorRolePeriodBasis
Air Evac EMS, Inc. (EVCA)Certificate holderMatched 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.

6 reports on file, 2012-01-23 – 2024-03-17.

FLUID LOSS; SMOKE/FUMES/ODORS/SPARKS · 2024-03-17 Matched by certificate designator
ATA 2820

Part: SWITCH — LEAKING (FUEL FLOW) · airframe 33,213 hrs · 15,151 cycles

STRONG SMELL OF FUEL IN AIRCRAFT.

Source: SDR EVCA2024031800024
OTHER · 2020-06-24 Matched by certificate designator
ATA 5320

Part: COVER PLATE — CORRODED (ZONE 100) · airframe 31,352 hrs · 21,182 cycles

CORROSION ON LEFT HAND FORWARD LOWER SHELL ASSEMBLY UNDER CO-PILOT STEP COVER PLATE.

Source: SDR EVCA20200624001
OTHER · 2020-06-24 Matched by certificate designator
ATA 5320

Part: STRUCTURE — CORRODED (BS 113.05) · airframe 31,352 hrs · 21,182 cycles

DURING PERIODIC INSPECTION, FOUND CORROSION ON AFT LOWER SHELL ASSEMBLY AT APPROXIMATELY FS 113.05 AND RBL 2.85.

Source: SDR EVCA20200624002
OTHER · 2018-06-13 Matched by certificate designator
ATA 5312

Part: CHANNEL — CORRODED (AFT FIRE WALL) · airframe 30,482 hrs · 57,391 cycles

ON REMOVAL OF TOP AND LEFT CHANNELS ON THE AFT ENGINE FIREWALL, CORROSION FOUND ON RIGHT CHANNEL. REMOVED AND REPLACED THE CHANNEL IAW SRM.

Source: SDR EVCA20180618003
OTHER · 2018-02-21 Matched by certificate designator
ATA 5302

Part: ATTACH FITTING — CRACKED (TAILBOOM) · airframe 30,351 hrs · 57,010 cycles

DURING INSPECTION AND COMPLIANCE WITH RECURRING AD 2013-25-10 FOUND THE UPPER LT TAIL BOOM ATTACHMENT FITTING TO BE CRACKED

Source: SDR EVCA201802211
OTHER · 2012-01-23 Matched by certificate designator
ATA 5534

Part: CAP — MALFUNCTIONED (VERTICAL STAB) · airframe 27,563 hrs · 49,198 cycles

VERTICAL FIN STROBE ASSY, DETACHED IN FLIGHT DUE TO VERTICAL FIN FORWARD CAP ASSY MALFUNCTION.

Source: SDR EVCA2012012300026