N7138Q

CESSNA U206F · 1975 · Fixed-wing single-engine · 1 engine · 6 seats · Valid Registration

Registered owner: ARCTIC AVIATION LEASING LLC, AK (owner ≠ operator)

Operators of this aircraft

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

OperatorRolePeriodBasis
Smokey Bay Air, Inc (X53A)Certificate holderMatched by certificate designator
James ChristensenOperatoron 2009-10-07Operator named in NTSB report

Accident & incident history

Accident · 2009-10-07 Operator named in NTSB report
CESSNA U206F No injuries Part 91James Christensen

Operated by James Christensen (per NTSB report)

Source: NTSB case ANC10CA003
Accident · 2005-06-15 Matched by aircraft (N-number)
Cessna U206F No injuries Part 91Smokey Bay Air, Inc
Source: NTSB case ANC05LA087
CESSNA 172 Serious injury Part 91operator not named in the NTSB record
Source: NTSB case NYC77FNC17

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, 2000-08-17 – 2012-07-23.

VIBRATION/BUFFET · 2012-07-23 Matched by certificate designator
ATA 8530

Part: CYLINDER — CRACKED (NR 5) · airframe 14,842 hrs

ON FIRST RUN UP OF THE DAY PILOT NOTED ACFT RAN ROUGH AND SOUNDED DIFFERENT. MX PERSONAL PERFORMED A VISUAL INSPECTION OF CYLINDERS AND FOUND NR 5 CYLINDER MISSING SEVERAL COOLING FINS AND A HOLE THE SIZE OF A PENCIL IN THE AREA OF THE EXHAUST PORT ON THE TOP OF THE CYLINDER HEAD. AFTER REMOVING CYLINDER A CRACK WAS NOTED FROM EXHAUST PORT ACROSS TOP SPARK PLUG BOSS TO INJECTOR PORT AND THOUGHT INTAKE PORT. ON THE INSIDE OF CYLINDER A CRACK PROPAGATED FROM TOP SPARK PLUG BOSS TO BOTH INTAKE AND EXHAUST SEATS. PN AEC63197, SN 20356-B, PART TT 1127.8, AD 2004-08-10 ADDRESSES SAME PN CYLINDER BUT LOWER SN THAN EFFECTED PART.

Source: SDR 2012F00147
OTHER · 2007-08-24 Matched by certificate designator
ATA 8530

Part: CYLINDER — CRACKED (ENGINE)

BOTH CYLINDER HAVE VISIBLE CRACKS ORIGINATING AT THE EXHAUST VALVE SEAT. (K)

Source: SDR ENE2007F00000
OTHER · 2000-08-17 Matched by certificate designator
ATA 8520

Part: CAMSHAFT — MAKING METAL

FERROUS MATERIAL FOUND IN OIL FILTER. ENGINE DIS-ASSEMBLED, PROBLEM FOUND TO BE FAILED CAMSHAFT AND LIFTER BODIES. (X)

Source: SDR 20000817SH016