N931FE

CESSNA 208B · 1987 · Fixed-wing single-engine · 1 engine · 12 seats · Valid Registration

Registered owner: FEDERAL EXPRESS CORPORATION, TN (owner ≠ operator)

Operators of this aircraft

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

OperatorRolePeriodBasis
Wiggins Airways, Inc. (AXSA)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.

5 reports on file, 1997-10-22 – 2016-09-29.

SMOKE/FUMES/ODORS/SPARKS · 2016-09-29 Matched by certificate designator
ATA 3452

Part: TRANSPONDER — FAILED (COCKPIT)

NR ONE TRANSPONDER FAILED WITH A PUFF OF SMOKE, PILOT TURNED UNIT OFF AND PULLED BREAKER.

Source: SDR AXSA201609290001
OTHER · 2016-08-23 Matched by certificate designator
ATA 7250

Part: RIVET — MISSING (CT BLADE) · airframe 13,388 hrs · 16,378 cycles

NOTICED THAT TWO RIVET TAILS THAT HOLD THE CT BLADES IN WERE MISSING.

Source: SDR AXSA08/23/16
OTHER · 1997-10-22 Matched by certificate designator
ATA 6111

Part: BLADE — CRACKED (BLADE FACE)

INSPECTION FOUND ALL 3 BLADES HAVE CHORDWISE CRACKS BEYOND THE 3.5 INCH LIMIT. ALL CRACKS LEAD UP TO AND POSSIBLY UNDER THE EROSION SHIELD. THE CRACKS WERE FOUND DURING INSPECTION PER HARTZELL JB 169A. PROPELLER REMOVED FROM SERVICE AT THIS TIME.

Source: SDR 97ZZZX4803
OTHER · 1997-10-22 Matched by certificate designator
ATA 6111

Part: BLADE — CRACKED (BLADE FACE)

INSPECTION FOUND ALL 3 BLADES HAVE CHORDWISE CRACKS BEYOND THE 3.5 INCH LIMIT. ALL CRACKS LEAD UP TO AND POSSIBLY UNDER THE EROSION SHIELD. THE CRACKS WERE FOUND DURING INSPECTION PER HARTZELL JB 169A. PROPELLER REMOVED FROM SERVICE AT THIS TIME.

Source: SDR 97ZZZX4805
OTHER · 1997-10-22 Matched by certificate designator
ATA 6111

Part: BLADE — CRACKED (BLADE FACE)

INSPECTION FOUND ALL 3 BLADES HAVE CHORDWISE CRACKS BEYOND THE 3.5 INCH LIMIT. ALL CRACKS LEAD UP TO AND POSSIBLY UNDER THE EROSION SHIELD. THE CRACKS WERE FOUND DURING INSPECTION PER HARTZELL JB 169A. PROPELLER REMOVED FROM SERVICE AT THIS TIME.

Source: SDR 97ZZZX4804