N763FE

CESSNA 208B · 1991 · 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

Accident & incident history

No NTSB accidents or incidents on file for this aircraft.

Maintenance disclosures

O · 2011-12-13 Matched by certificate designator
ATA 3240

THE PILOT REPORTED AS HE WAS TAXIING N763FE BACK TO THE PARKING SPACE AND MAKING A LEFT TURN THE LEFT BRAKE PEDAL WENT ALL THE WAY DOWN TO THE FLOOR. HE STATED HE WAS ABLE TO CONTROL THE AIRCRAFT WITH LEFT BRAKE AND A LITTLE REVERSE. AIRCRAFT WAS INVOLVED IN A RIGHT BRAKE FAILURE THE WEEK PRIOR AND IS SUSPECTED AIR MAY HAVE ENTERED THE LEFT BRAKE SYSTEM DURING PREVIOUS MAINTENANCE.

Source: SDR AWHA121311 · FAA SDRS
O · 2011-11-30 Matched by certificate designator
ATA 3243

PILOT FOR FLIGHT 7706 REPORTED AS HE WAS TAXIING FROM THE RAMP FOR DEPARTURE THE AIRCRAFT WAS OPERATING NORMAL, WINDS AT THE TIME WERE FROM 02 AT 14G22KTS (TAXIING WITH A TAILWIND). UPON REACHING FOR TAKEOFF AND MAKING A RT TURN FOR DEPARTURE THE RT BRAKE PEDAL WENT ALL THE WAY DOWN TO THE FLOOR. HE WAS ABLE TO CONTROL THE AC WITH LT BRAKE AND A LITTLE REVERSE. HE EXITED THE RUNWAY AND TAXIED BACK TO THE RAMP. ON THE WAY BACK HE TRIED TO PUMP UP THE RT BRAKE. IT CAME UP A LITTLE, BUT WAS STILL VERY SOFT. AFTER PARKING AT THE RAMP, TRIED THE RIGHT BRAKE ONCE MORE. IT FELT LIKE IT WAS A LITTLE BETTER BUT WAS STILL SOFT. THE RT MASTER CYLINDER IS ORIGINAL TO THE AIRCRAFT INSTALLED IN 1991 WITH 9392.9 TSN.

Source: SDR AWHA113011 · FAA SDRS
O · 2008-02-21 Matched by certificate designator
ATA 2710

PILOT REPORTED BINDING AND NOISE IN THE OVERHEAD IN AILERON CONTROL SYSTEM. FLIGHT CONTINUED NORMAL AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE ATTACH BLOCK OF THE AILERON CONTROL CABLE LOOP SYSTEM ROTATED AND WAS STRIKING THE LOWER BELL CRANK QUAD ASSEMBLY. THE BLOCK WAS REPOSITIONED TO ACHIEVE CLEARANCE AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Source: SDR 022708 · FAA SDRS
O · 2006-02-22 Matched by certificate designator
ATA 7314

PRECAUTIONARY INSPECTION OF THE FUEL PUMP DRIVE SPLINE IAW MM. FUEL PUMP COUPLING IN SITU INSPECTION. MAINTENANCE FOUND THE FUEL PUMP FUEL PUMP DRIVE SPLINE CORRODED. THE FUEL PUMP ASSY WAS REPLACED WITH AN OVERHAULED UNIT AND THE AIRCRAFT RETURNED TO SERVICE. (K)

Source: SDR AWH2006F00007 · FAA SDRS
O · 2002-11-22 Matched by certificate designator
ATA 3197

THE SUBJECT AIRCRAFT DOES NOT HAVE THE HOUR METER OPTION INSTALLED. HOWEVER THE AIRCRAFT IS WIRED FOR THIS OPTION, CLOCK OR HOUR METER. MAINTENANCE HAS FOUND AT THE CIRCUIT BREAKER CB75 BOTH OPTIONS POWERED AND THE WIRE DF2 TERMINAL IMPROPERLY STOWED. THE TERMINAL END OF WIRE DF2 IS NOT PROTECTED FROM SHORTING AND IMPROPER TIE WRAPPING ALLOWS THE TERMINAL END TO FLOP AROUND. TERMINAL END DF7 IS A GROUNDED CIRCUIT AND IS STOWED WITH DF2 TERMINAL. FOUND THIS AIRCRAFT WIRING TIES BEHIND CO-PILOTS INSTRUMENTS PANEL. DF2,DF7 TERMINAL ENDS LOOSE. C/A: MAINTENANCE IS DISCONNECTING TERMINAL DF1 AT CB75, HEAT SHRINKING TERMINAL END FOR PROTECTION AND PROPERLY STOWING WIRE.

Source: SDR AWHA1125 · FAA SDRS