Registered owner
Wright Air Service Inc
Owner type
Corporation
Serial number
208B0253
Year built
1991
Type
Fixed wing single engine
Engine
Turbo-prop
Airworthiness
Standard, normal
Airworthiness date
December 16, 1991
Certificate issued
May 27, 1992
Expires
April 30, 2030
Mode S code
A53C82

From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Pratt & Whitney PT6A model are included below.

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Airworthiness directives that may apply · 47

Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.

1968In forceSuperseded2026
ADs by the year they took effect: 53 ADs
19681
19691
19701
19751
19771
19782
19802
19861
19881
19903
19921
19941
19951
19961
19972
19982
20012
20022
20031
20042
20053
20063
20071
20083
20093
20112
20121
20142
20151
20161
20211
20221
20231
20241
See all 54 ADs

Information bulletins that may apply · 8

Advisory, not mandatory.

NTSB investigations

No NTSB investigations matched to N4365UMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Cessna 208B aircraft

FAA incident reports

No FAA accident or incident reports matched to N4365UMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Cessna 208B aircraft

Service difficulty reports · 7

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

SDR 2011FA0000809G Switch · inoperativeELT FAILED G-SWITCH TEST.Dec 27, 2011 · N4365U · Cessna 208B · Emergency Locator BeaconSDR 2007FA0000573Pin · unserviceableON A ROUTINE INSPECTION, A MECHANIC FOUND THAT THE PILOTS RT RUDDER PEDAL PIN WAS ABOUT TO FALL OUT OF THE RUDDER PEDAL. FURTHER INSPECTION FOUND THAT THE ROLL PIN PN: NAS561C318 HAD FALLEN OUR OF ITS HOLE CAUSING THE RUDDER PEDAL PIN TO MIGRATE FROM ITS POSIJun 6, 2007 · N4365U · Cessna 208B · Rudder Control SystemSDR 2007FA0000355Exhaust Duct · crackedCRACKING OCCURRED IN A SHORT TIME SPAN, DURING NORMAL OPERATION. CRACKS WERE OVER AN AREA APPROX 7 INCHES X 7 INCHES. ONE PIECE APPROX 3 INCHES X 3 INCHES SEPARATED FROM THE PART. AFTER CRACKING, DEFORMATION OF LOWER TRAILING EDGE OCCURRED BECAUSE IT WAS NOApr 17, 2007 · N4365U · Cessna 208B · Engine Collector/Tailpipe/NozzleSDR HYTA2004006Longeron · crackedLT LONGERON 261310531 AND RT LONGERON 261310528 WERE FOUND CRACKED AT THE LOWER AFTER CORNERS OF THE CUT-OUTS FOR THE CONTROL COLUMN TORQUE TUBE. THESE CUT-OUTS ARE LOCATED JUST FORWARD OF THE NOSE GEAR SPRING SUPPORT FITTINGS 26430633. RT LONGERON HAS ONE CApr 23, 2004 · N4365U · Cessna 208B · Fuselage Main, Longeron/StringerSDR HYTA2004005Spring · wornFLEXING OF MLG CENTER SPRING PN 2641014-3 CAUSES CENTER SPRING TO CONTACT MLG COVER PN 2611103-10 WHICH IS LOCATED BENEATH THE CENTER SPRING. CHAFING HAD WORN THROUGH THE PAINT ON THE LOWER SURFACE OF CENTER SPRING. TWO RIVETS HAD WORN INTO THE LOWER SURFACEMar 17, 2004 · N4365U · Cessna 208B · Main Landing GearSDR HYTA2004004Wire · misroutedFLASHING BEACON WIRE IN TAILCONE WAS ROUTED OVER THE BALLAST RESISTOR WHERE THERE IS LESS THAN .5 INCH CLEARANCE TO STRUCTURE. WIRE WAS NOT TOUCHING BALLAST RESISTOR OR AIRPLANE STRUCTURE, BUT INSULATION WAS BURNED CLEAR THROUGH TO BARE WIRE. WIRE SHOULD HAVMar 17, 2004 · N4365U · Cessna 208B · Light System WiringSDR HYTA2004003Bolt · corrodedWHILE CONDUCTING INITIAL INSPECTION, BOTH AFT WING TO FUSELAGE ATTACH BOLTS WERE FOUND SLIGHTLY RUSTED. DAMAGE WAS NEGLIGIBLE. THESE BOLTS AS WELL AS FORWARD ATTACH BOLTS AND UPPER AND LOWER STRUT ATTACH BOLTS WERE APPARENTLY INSTALLED DRY. THIS HARDWARE SHMar 17, 2004 · N4365U · Cessna 208B · Fasteners

STCs that may be installed · 357

Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.

See all 357 STCs

Earlier aircraft with this N-number · 2

These aircraft carried N4365U before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.