N138AE

BELL HELICOPTER TEXTRON 206L-1 · 1983 · 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, 2010-06-02 – 2024-09-06.

OTHER · 2024-09-06 Matched by certificate designator
ATA 5300

Part: UNKNOWN — CRACKED (BS 145) · airframe 22,160 hrs · 40,103 cycles

CRACK IN 145 STATION

Source: SDR EVCA0202490600241
OTHER · 2023-09-26 Matched by certificate designator
ATA 5311

Part: FRAME — CRACKED (STATION 155) · airframe 21,680 hrs · 38,638 cycles

CRACK IN R/H ROLLOVER CLOSE OUT PANEL APPROX 1 INCH LONG EXTENDING TO EDGE OF PANEL. P/N 206-031-117-443. THIS PART WILL PROBABLY HAVE TO BE REMOVED TO REPAIR THE FRAME MIGHT CONSIDER REPLACEMENT OF PANEL IF PROCURABLE.

Source: SDR EVCA09262023
OTHER · 2023-01-11 Matched by certificate designator
ATA 6210

Part: BLADE — CRACKED (MAIN ROTOR) · airframe 21,250 hrs · 37,309 cycles

VAN HORN MAIN ROTOR BLADE INBOARD TAB ATTACHMENT TO BLADE SURFACE HAS CRACKS AT BOTH INBOARD AND OUTBOARD ATTACH POINTS ON BOTH UPPER AND LOWER BLADE SURFACES.

Source: SDR EVCA2023011100001
OTHER · 2020-01-02 Matched by certificate designator
ATA 5340

Part: STRUCTURE — CRACKED · airframe 19,748 hrs · 32,489 cycles

DURING 300 HOUR INSPECTION, AN AMT DISCOVERED CLIP P/N 206-033-306-008 CRACKED JUST FWD OF TB ATTACH ACCESS AREA IN THE UPPER R/H QUADRANT ADJACENT TO THE TR AND ELEVATOR BELL CRANK SUPPORT FITTING.

Source: SDR EVCA20200104001
INFLIGHT SEPARATION · 2010-09-21 Matched by certificate designator
ATA 5610

Part: CHIN BUBBLE — DETACHED (ZONE 100) · airframe 15,489 hrs · 20,317 cycles

APPROX 3 NM NW OF AIRPORT HEARD A NOISE. A FEW MOMENTS PASSED AND THEN THERE WAS A "POP", A QUICK PRESSURE CHANGE AND AIRFLOW INTO THE COCKPIT. DISCOVERED THE GAPING HOLE WHERE THE CHIN BUBBLE SHOULD BE INSTALLED. IMMEDIATELY TURNED TOWARD THE AIRPORT AND NOTIFIED CENCOM OF A PRECAUTIONARY LANDING. MEANWHILE WE REDUCED SPEED AND BEGAN A SHALLOW APPROACH INTO THE AIRPORT.

Source: SDR EVCA00007
OTHER · 2010-06-02 Matched by certificate designator
ATA 5312

Part: BULKHEAD — CRACKED (BS 142) · airframe 15,294 hrs · 19,833 cycles

DURING A ROUTINE INSP, MECHANIC FOUND CRACK ON BULKHEAD STA NR 142, WL 61, ON THE RT SIDE GENERATING FROM A NUTPLATE SCREW LOCATION.

Source: SDR EVCA00006