N1276P

Cancelled 2007

Deregistered aircraft · 2000 Cessna 208B · Pratt & Whitney PT6A series

Cancelled
July 5, 2007
Exported to
Indonesia
Status when cancelled
Sale reported
Serial number
208B0852
Year built
2000
Type
Fixed wing single engine
Engine
Turbo-prop
Airworthiness
Standard, normal
Airworthiness date
September 21, 2000
Last registry action
June 27, 2007
Mode S code
A070EB
Owner when cancelled
Sale Reported
Location
Xxx, OK
Owner type
Individual

From the FAA registry file of October 29, 2026, cancelled registrations. Owners’ street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

NTSB investigations · 2

Matched to this aircraft by N1276P and the event date: after November 9, 1979, when the previous aircraft’s registration ended, through this one’s cancellation.

FAA incident reports · 2

FAA accident and incident reports matched to this aircraft by N1276P and the event date: after November 9, 1979, when the previous aircraft’s registration ended, through this one’s cancellation.

Service difficulty reports · 5

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

SDR ENHA200320805Bellcrank · damagedFLAP BELLCRANK P/N 2622281-12, S/N 898 TCSN 997. INSPECTION FOUND MISSING WELDS AT MATING PORTIONS OF THE ASSEMBLY. BELLCRANK COULD BE SUBJECT TO CATASTROPHIC FAILURE. INSPECTION PROMPTED BY AL FSDO LETTER DATED 8/15/03. SUBJECT BELLCRANK REPLACED WITH P/NSep 4, 2003 · N1276P · Cessna 208B · Trailing Edge Flap Control SystemSDR ENHA200320807Bellcrank · mismanufacturedFLAP BELLCRANK INSPECTION FOUND MISSING WELDS AT MATING PORTIONS OF THE ASSEMBLY. BELLCRANK COULD BE SUBJECT TO CATASTROPHIC FAILURE. INSPECTION PROMPTED BY AL FSDO LETTER DATED 8/15/03. SUBJECT BELLCRANK REPLACED WITH P/N 2622311-7 OF NEW DESIGN.Sep 4, 2003 · N1276P · Cessna 208B · Trailing Edge Flap Control SystemSDR ENHA200300001Support · crackedFLAP ACTUATOR STRUCTURE SUPPORT ASSY FAILURE. PILOT REPORTED FLAPS SELECTED TO 10 DEGREE, FLAPS DEPLOYED TO 10 DEGREE. AT THE NEXT FLAP SELECTION, FLAP C/B TRIPPED, C/B WOULD NOT RESET. STANDBY FLAP SWITCH WAS NOT USED AND BREAKAWAY WIRE INTACT. INSPECTION Jan 21, 2003 · N1276P · Cessna 208B · Trailing Edge Flap ActuatorSDR 2003F00100Bracket · crackedSTRUCTURAL FAILURE (SUPPORT ASSY- FLAP ACTUATOR) PILOT REPORTED FLAPS SELECTED TO 10 DEG, FLAPS OPERATED TO 10 DEG, AT THE NEXT FLAP SELECTION THE FLAP CIRCUIT BREAKER TRIPPED, CIRCUIT BREAKER WOULD NOT RESET. STANDBY FLAP SW WAS NOT USED AND BREAK-AWAY WIRE Jan 20, 2003 · N1276P · Cessna 208B · Wing Miscellaneous StructureSDR 208000103Structure · crackedSUPPORT ASSEMBLY-FLAP ACTUATOR FAILURE. PILOT REPORTED FLAPS SELECTED 10 DEG FLAPS WENT TO 10 DEGREE STOPPED AT THE NEXT FLAP SELECTION CIRCUIT BREAKER TRIPPED, CIRCUIT BREAKER WOULD NOT RESET. STANDBY FLAP SW WAS NOT USED AND BREAK-AWAY WIRE INTACT. FURTHEJan 20, 2003 · N1276P · Cessna 208B · Trailing Edge Flap Actuator

Other aircraft with N1276P · 1

The FAA can assign a mark to another aircraft once a registration is cancelled. No aircraft carries N1276P now.