N208

CESSNA 208 · 2002 · Fixed-wing single-engine · 1 engine · 10 seats · Valid Registration

Registered owner: JMP AIRCRAFT SERVICES LLC TRUSTEE, AK (owner ≠ operator)

Operators of this aircraft

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

No operator established for this aircraft.

Accident & incident history

No NTSB accidents or incidents on file for this aircraft.

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.

3 reports on file, 2001-12-20 – 2011-12-05.

OTHER · 2011-12-05 Unresolved
ATA 5712

Part: RIB — CRACKED (WING) · airframe 7,764 hrs · 7,476 cycles

LT LEADING EDGE CLOSURE RIBS CRACKED. REPAIRED IAW TD340-57-11-17. CONTROL= 4208-33.

Source: SDR NSVA2011324
OTHER · 2002-08-10 Matched by certificate designator
ATA 5315

Part: FLOORBEAM — CHAFED (FUSELAGE)

BS 740 FLOORBEAM IS CHAFED RBL 43 TO LBL 56 WL 208 UPPER AFT FLANGE. REMOVED AND REPLACED FLOORBEAM PER EA 7-5310-65351.

Source: SDR 02FDEA00611
OTHER · 2001-12-20 Matched by certificate designator
ATA 3040

Part: CONTROLLER — FAILED (WINDOW HEAT)

WINDSHIELD PANEL L1 OUTER PANE SUFFERED A TOTAL FAILURE IN FLT AT FL310. WINDSHIELD WAS EXCESSIVELY HOT TO TOUCH. (WINDSHIELD OVERHEAT PROTECTION DID NOT ACTIVATE) DECLARED EMERGENCY AND DIVERTED TO PHX. (UNABLE TO COMPLETE FLT UTILIZING CREW 02). REMOVED AND REPLACED L1 WINDSHIELD PER MM 56-11-011-4 & AS PER 30-41-042-5 THE PIN NUMBERS OF THE TRANSFORMER TAPS WERE CONNECTED TO 12. PLACED PINS ON 11 PER 30-41-042-5 FIG 501. REMOVED AND REPLACED L1 WIND HEAT CONTROLLER PER MM 20-10-017-2.

Source: SDR 01FDEA01093