N1275N

Cancelled 2022

Deregistered aircraft · 1999 Cessna 208B · Pratt & Whitney PT6A series

Cancelled
March 7, 2022
Exported to
Canada
Status when cancelled
Valid registration
Serial number
208B0756
Year built
1999
Type
Fixed wing single engine
Engine
Turbo-prop
Airworthiness
Standard, normal
Airworthiness date
June 24, 1999
Certificate issued
December 14, 2021
Last registry action
December 14, 2021
Mode S code
A070C7
Owner when cancelled
Win Win Aviation Inc
Owner type
Corporation

From the FAA registry file of November 3, 2026, cancelled registrations. Owners’ street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

NTSB investigations · 1

Matched to this aircraft by N1275N and the event date: after June 17, 1970, when the previous aircraft’s registration ended, through this one’s cancellation.

FAA incident reports · 1

FAA accident and incident reports matched to this aircraft by N1275N and the event date: after June 17, 1970, when the previous aircraft’s registration ended, through this one’s cancellation.

Service difficulty reports · 7

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

SDR EPUA20180227001Hinge · corrodedDURING SCHEDULE INSPECTION IT WAS NOTED THAT ELEVATOR HINGE PART NUMBER 2632055-1 HAD EXFOLIATED CORROSION TO THE EXTENT THAT THE PART HAD TO BE REPLACED.Feb 27, 2018 · N1275N · Cessna 208B · Elevator StructureSDR EPUA20131107001Structure · crackedLEFT AILERON L/E SKIN CRACKED AT OTBD BALANCE WEIGHT ATTACH POINT. REPLACED AILERON ASSEMBLE WITH SERVICEABLE UNIT.Oct 19, 2013 · N1275N · Cessna 208B · AileronsSDR 20001012SH023Angle · crackedFORWARD ANGLE ON LEFT NOSE CAP FOR INDUCTION AIR PLENUM ATTACHMENT CRACKED. (X)Aug 1, 2000 · N1275N · Cessna 208B · Engine Cowling SystemSDR 20000720SH021Actuator · shearedSTANDBY FLAP MOTOR INOPERATIVE. ACTUATOR SHAFT ROLL PIN SHEARED. JACKSCREW CONTAMINATED WITH METAL PARTICLES, MOTOR INOPERATIVE. UPON REPLACEMENT OF TRANSMISSION ASSY, ALSO DISCOVERED ELECTRICAL PIN IN PRIMARY FLAP MOTOR POWER CONNECTOR PARTIALLY DISENGAGED Jun 13, 2000 · N1275N · Cessna 208B · Trailing Edge Flap ActuatorSDR 20000720SH022Bleed Valve · failedMANUFACTURER RECALLED THIS SPECIFIC COMPRESSOR BLEED VALVE FOR TESTING OF INTERNAL PACKING FOR DEFECTS. BLEED VALVE SERIAL NUMBER FELL OUTSIDE OF ANY AD OR SB. (X)May 16, 2000 · N1275N · Cessna 208B · Compressor Bleed ValveSDR 20000720SH020Transmitter · shortedLEFT FUEL QUANTITY INDICATOR INACCURATE AND ERRATIC. REPLACED DEFECTIVE CENTER OUTBOARD FUEL SENDING UNIT. (X)May 16, 2000 · N1275N · Cessna 208B · Fuel Quantity SensorSDR 20000510SH005O-Ring · cutDURING A POST-FLIGHT INSPECTION, THE PILOT NOTED EXCESSIVE OIL ON THE LOWER COWL AND DOWN THE LEFT SIDE OF THE AIRCRAFT. UPON FURTHER INSPECTION, DETERMINED A NR 2 BEARING OIL SCAVENGETUBE COUPLING O-RING LOCATED AT C-FLANGE WAS LEAKING. UPON REMOVAL OF THE Apr 5, 2000 · N1275N · Cessna 208B · Turbine Engine Oil System

Other aircraft with N1275N · 1

The FAA can assign a mark to another aircraft once a registration is cancelled. No aircraft carries N1275N now.