N229AE

BELL HELICOPTER TEXTRON 206L-1 · 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

O · 2019-10-10 Matched by certificate designator
ATA 5310

FIRST RIVET HOLE OUTBOARD OF LT AFT NODAL BEAM MOUNT AT STA 145 CRACKED APPROXIMATELY .5"

Source: SDR EVCA2019101000001 · FAA SDRS
E · 2019-09-04 Matched by certificate designator
ATA 6410

DURING FLIGHT, THE PILOT NOTED A SUDDEN VIBRATION IN THE ANTI-TORQUE CONTROLS AND PRECAUTIONARILY LANDED THE HELICOPTER. UPON INSPECTION, ONE TIP WEIGHT WAS FOUND MISSING FROM TAIL ROTOR BLADE PN: 2062200-301.

Source: SDR EVCA2019090400000 · FAA SDRS
E · 2019-09-03 Matched by certificate designator
ATA 6410

DURING FLIGHT, THE PILOT NOTED A SUDDEN VIBRATION IN THE ANTI-TORQUE CONTROLS AND PRECAUTIONARILY LANDED THE HELICOPTER. UPON INSPECTION, ONE TIP WEIGHT WAS FOUND MISSING FROM TAIL ROTOR BLADE PN: 2062200-301.

Source: SDR EVCA201909040001 · FAA SDRS
O · 2019-03-19 Matched by certificate designator
ATA 5522

RT ELEVATOR HAS CORROSION ON INBOARD LEADING EDGE. REMOVED AND REPLACED AFFECTED RT ELEVATOR WITH NEW PART, P/N: 206-023- 119-179, IAW BHT-206L1-MM-1, CH. 27.

Source: SDR EVCA2019031900000 · FAA SDRS
O · 2017-05-20 Matched by certificate designator
ATA 6710

WHILE PERFORMING PREFLIGHT OF THE AIRCRAFT FOUND ONE CYCLIC TUBE TO HAVE THE FIXED AND NONADJUSTABLE CLEVIS ON THE SERVO END OF THE CONTROL TUBE TO BE ROTATING WITHIN THE TUBE.

Source: SDR EVCA201705201 · FAA SDRS
B · 2016-07-08 Matched by certificate designator
ATA 2842

WHILE IN FLIGHT, PILOT AND CREW REPORTED A STRONG FUEL ODOR. THEY DECIDED TO TERMINATE THE FLIGHT AND RETURN TO BASE. UPON INVESTIGATION THE AFT FUEL PROBE WAS REPOSITIONED IN ITS OPENING. FURTHER OPS CHECKS DETERMINED FUEL ODOR TO BE GONE.

Source: SDR EVCA201607081 · FAA SDRS
O · 2010-03-02 Matched by certificate designator
ATA 5320

CRACK IN NECK OF PART AT RELIEF HOLE. CRACK IS 0.9" LONG. PART CONNECTS PILOT'S YOKE TO ACFT FLOOR.

Source: SDR 2010F00062 · FAA SDRS