N130AE

BELL HELICOPTER TEXTRON 206L-1 · 1980 · 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.

8 reports on file, 2011-02-10 – 2025-06-02.

SMOKE/FUMES/ODORS/SPARKS · 2025-06-02 Matched by certificate designator
ATA 2121

Part: BLOWER MOTOR — ODOR (ZONE 100) · airframe 25,344 hrs · 19,261 cycles

AC SMELLS LIKE BURNT ELECTRIC WHEN TURN ON

Source: SDR EVCA20250603001
OTHER · 2023-10-02 Matched by certificate designator
ATA 5320

Part: STIFFENER — CRACKED (FRM 82) · airframe 24,406 hrs · 43,849 cycles

THE VERTICAL STIFFENER AT FS 82, WL 67 BL -3.3 IT IS CRACKED ON THE UPPER ANGLE.

Source: SDR EVCA202310090001
OTHER · 2023-01-22 Matched by certificate designator
ATA 6210

Part: TAB — CRACKED (M/R BLADE) · airframe 23,992 hrs · 16,447 cycles

MR BLADE TRIM TAB CRACKED

Source: SDR EVCA202301240001
OTHER · 2021-04-24 Matched by certificate designator
ATA 6210

Part: BLADE — CRACKED (MAIN ROTOR) · airframe 22,974 hrs · 40,469 cycles

BOTH VAN HORN M/R BLADES ARE CRACKED.

Source: SDR EVCA04242021
OTHER · 2021-04-24 Matched by certificate designator
ATA 6210

Part: BLADE — CRACKED (MAIN ROTOR) · airframe 22,974 hrs · 40,469 cycles

BOTH VAN HORN M/R BLADES ARE CRACKED.

Source: SDR EVCA04242021(1)
OTHER · 2019-01-27 Matched by certificate designator
ATA 7714

Part: TACH GENERATOR — BROKEN (ZONE 200) · airframe 22,279 hrs · 37,831 cycles

AMT ARRIVED ON SITE. INSPECTED AND TROUBLE SHOT HYDRAULIC SYSTEM. DISCOVERED RETAINER, SPRING AND SHAFT BROKEN ON TACH GENERATOR SIDE OF TRIPLE STACK ASSEMBLY. REMOVED AND REPLACED TACH GENERATOR WITH P/N 206-375-202-101 S/N 777,RETAINER P/N 25399, SPRING P/N 67588 AND SHAFT P/N 20546. PERFORMED GROUND RUN AND LEAK CHECK. NO FURTHER DEFECTS NOTED.

Source: SDR EVCA201901281
OTHER · 2017-10-18 Matched by certificate designator
ATA 5312

Part: STIFFENER — CRACKED (BS 145 BULKHEAD) · airframe 21,537 hrs · 36,069 cycles

WHILE PERFORMING 300 HOUR INSPECTION, FOUND A CRACKED STIFFENER ON THE BULKHEAD.

Source: SDR EVCA201710200001
OTHER · 2011-02-10 Matched by certificate designator
ATA 5340

Part: ATTACH FITTING — CRACKED (AFT BULKHEAD) · airframe 18,142 hrs · 26,591 cycles

DURING A ROUTINE INSP, MECHANIC FOUND UPPER LT ATTACHMENT FITTING ON FUSELAGE AFT BULKHEAD CRACKED. ATTACHMENT FITTING R & R.

Source: SDR EVCA00011