N70076

No registry detail on file · not in current registry

Operators of this aircraft

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

OperatorRolePeriodBasis
MARKAIR EXPRESS, INC.Operatoron 1992-01-15Operator named in NTSB report
DICK NELSONOperatoron 1988-12-12Operator named in NTSB report
Wings of AlaskaOperatoron 1984-10-15Operator named in NTSB report

Accident & incident history

Cessna 207 No injuries Part 91operator not named in the NTSB record
Source: NTSB case ANC96LA017
Incident · 1992-01-15 Operator named in NTSB report
CESSNA 207 No injuries Part 135MARKAIR EXPRESS, INC.

Operated by MARKAIR EXPRESS (per NTSB report)

Source: NTSB case ANC92IA029
Accident · 1988-12-12 Operator named in NTSB report
CESSNA 207 No injuries Part 91DICK NELSON

Operated by DICK NELSON (per NTSB report)

Source: NTSB case ANC89LA023
Accident · 1984-10-15 Operator named in NTSB report
CESSNA C-207 No injuries Part 135Wings of Alaska

Operated by WINGS OF ALASKA (per NTSB report)

Source: NTSB case SEA85LA010

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, 1996-01-16 – 2011-02-16.

ENGINE STOPPAGE · 2011-02-16 Unresolved
ATA 8520

Part: CRANKSHAFT — BROKEN (CRANKCASE) · airframe 230,000 hrs

CRANKSHAFT BROKE IN FLIGHT BETWEEN NR 3 & 4 CYLINDERS FORCING AN UNSCHEDULED LANDING.

Source: SDR PNYA20110216001
OTHER · 2001-09-11 Unresolved
ATA 8530

Part: CYLINDER — CRACKED (ENGINE)

CYLINDER INSTALLED 8/13/99, CRACK FOUND AROUND SPARK PLUG HOLE.

Source: SDR CY42001F00000
WARNING INDICATION; PARTIAL RPM/PWR LOSS · 1996-01-16 Unresolved
ATA 8520

Part: CRANKSHAFT — BROKE (ENGINE)

PERFORMED EMERGENCY LANDING ON FROZEN LAKE. DURING THE LANDING ROLL, THE RIGHT WING TIP STRUCK A SPRUCE TREE. THE AIRCRAFT RECEIVED DAMAGE TO THE RIGHT WING AND AILERON. THE ENGINE WAS REPLACED WITH THE AIRCRAFT ON THE FROZEN LAKE. THE EMERGENCY LANDING WAS FORCED DUE TO LOSS OF OIL PRESSURE AND ENGINE RPM AT THE SAME TIME. THIS WAS THE RESULT OF THE CRANKSHAFT BEING BROKEN IN TWO. NOTE: VAR CRANKSHAFT INSTALLED IN THIS IO-520 ENGINE.

Source: SDR 96ZZZX587