N1276P

No registry detail on file · not in current registry

Operators of this aircraft

Who operated this tail, and how firmly we know it.

No operator established for this aircraft.

Accident & incident history

Accident · 2004-02-10 Unresolved
Cessna 208B No injuries Part 135 — operator not named in the NTSB record
Source: NTSB case ANC04LA032
Accident · 2003-01-30 Unresolved
Cessna 208B No injuries Part 135 — operator not named in the NTSB record
Source: NTSB case ANC03LA030
Accident · 1971-04-26 Unresolved
PIPER PA-23 No injuries Part 91 — operator not named in the NTSB record
Source: NTSB case DEN71FQD18
Accident · 1968-01-05 Unresolved
PIPER PA-23 No injuries Part 91 — operator not named in the NTSB record
Source: NTSB case LAX68F0252

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.

5 reports on file, 2003-01-20 – 2003-09-04.

INADEQUATE Q C · 2003-09-04 Matched by certificate designator
ATA 2750

Part: BELLCRANK — MISMANUFACTURED (ZONE 600) · airframe 3,453 hrs

FLAP 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.

Source: SDR ENHA200320807
OTHER · 2003-09-04 Matched by certificate designator
ATA 2750

Part: BELLCRANK — DAMAGED (TE FLAP) · airframe 3,453 hrs

FLAP 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/N 2622311-7 OF NEW DESIGN.

Source: SDR ENHA200320805
FLT CONT AFFECTED · 2003-01-21 Matched by certificate designator
ATA 2752

Part: SUPPORT — CRACKED (FLAP ACTUATOR) · airframe 2,858 hrs · 5,423 cycles

FLAP 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 OF FLAP SYSTEM BY MAINTENANCE PERSONNEL FOUND THE FLAP ACTUATOR SUPPORT BRACKETS CRACKED AND BROKEN.

Source: SDR ENHA200300001
OTHER · 2003-01-20 Matched by certificate designator
ATA 5720

Part: BRACKET — CRACKED (FLAP ACTUATOR) · airframe 2,858 hrs · 5,243 cycles

STRUCTURAL 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 INTACT. FURTHER VISUAL INSPECTION OF THE FLAP SYSTEM BY MAINTENANCE PERSONNEL FOUND THE FLAP ACTUATOR SUPPORT BRACKETS CRACKED AND BROKEN.

Source: SDR 2003F00100
OTHER · 2003-01-20 Unresolved
ATA 2752

Part: STRUCTURE — CRACKED (FLAP ACTUATOR) · airframe 2,858 hrs · 5,243 cycles

SUPPORT 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. FURTHER VISUAL INSPECTION OF THE FLAP SYSTEM PERFORMED BY MAINTENANCE PERSONNEL FOUND THE FLAP ACTUATOR SUPPORT BRACKETS CRACKED AND BROKEN.

Source: SDR 208000103