N987FE

CESSNA 208B · 1989 · 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
WEST AIR, INC. (AWHA)Certificate holderMatched by certificate designator
WEST AIR, INC. (AWHA)Operatoron 1995-12-12Operator named in NTSB report

Accident & incident history

Accident · 1995-12-12 Operator named in NTSB report
Cessna 208B No injuries Part 135WEST AIR, INC.

Operated by WEST AIR INDUSTRIES (per NTSB report)

Source: NTSB case LAX96LA070

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.

2 reports on file, 2011-05-16 – 2018-12-17.

OTHER · 2018-12-17 Matched by certificate designator
ATA 5341

Part: ATTACH FITTING — CORRODED (FUSELAGE) · airframe 12,442 hrs · 14,488 cycles

DURING ROUTINE INSPECTION, CORROSION WAS FOUND IN THE NR 3, 5, AND 6 BOLT HOLE LOCATIONS IN THE RT UPPER AFT WING FITTINGS ATTACHMENT TO THE FUSELAGE AS REFERENCED IN THE NONDESTRUCTIVE TESTING MANUAL 53-20-06. REMOVAL OF THE CORROSION REQUIRED THE REAMING OF THREE BOLTS HOLE TO SPECIFIED HOLE DIAMETERS TO REMOVE THE CORROSION THAT WAS FOUND DURING INSPECTION. SPECIFICALLY, THE REPAIR INCREASES THE SIZE OF THREE SPECIFIC HOLES IN THE FITTING FROM A CLOSE TOLERANCE 1/4" BOLT TO CLOSE TOLERANCE 0.391” & 0.344". BOLT HOLE 3 WAS REAMED TO 0.391” BOLT HOLE 5 & 6 WERE REAMED TO 0.344” AFTER REAMING A VISUAL INSPECTION WAS PERFORMED UTILIZING A NR 10 POWER GLASS. SUBSEQUENT EDDY CURRENT INSPECTION WAS CONDUCTED AND FOUND AREAS TO BE FREE OF CORROSION OR CRACKS. NAS6605-38Y BOLT WAS INSTALLED IN THE NR 3 LOCATION. NAS6606-38X BOLTS WERE INSTALLED IN THE 5 & 6 LOCATIONS. FASTENERS WERE ASSEMBLED WET WITH ANTI-SEIZE COMPOUND AND TORQUED TO STANDARD TORQUE SPECIFICATIONS.

Source: SDR AWHA201812180001
OTHER · 2011-05-16 Matched by certificate designator
ATA 3243

Part: MASTER CYLINDER — FAILED (BRAKE SYS)

PILOT REPORTED DURING STRAIGHT TAXI TO LOADING POSITION, THE LT BRAKE PEDAL WENT TO THE FLOOR 3 TIMES. THE ACFT WAS SHUTDOWN AND SECURED AND THE PILOT CALLED MX. 30 MINUTES LATER, THE PILOT CALLED AND REPORTED THE LT BRAKE OPERATED NORMALLY. MX REPLACED THE LT MASTER CYLINDER WAS REPLACED AS A PRECAUTION.

Source: SDR AWH2011F00000