N1704U

CESSNA 207 · 1975 · Fixed-wing single-engine · 1 engine · 6 seats · Valid Registration

Registered owner: KUSPUK SCHOOL DISTRICT, AK (owner ≠ operator)

Operators of this aircraft

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

OperatorRolePeriodBasis
Flight AlaskaOperatoron 2013-03-06Operator named in NTSB report

Accident & incident history

Accident · 2013-03-06 Operator named in NTSB report
CESSNA 207 No injuries Part 135Flight Alaska

Operated by Flight Alaska Inc. (per NTSB report)

Source: NTSB case ANC13LA029
CESSNA 207 No injuries Part 135operator not named in the NTSB record
Source: NTSB case ANC86LA106

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.

4 reports on file, 1995-05-18 – 2015-05-14.

OTHER · 2015-05-14 Unresolved
ATA 8530

Part: CYLINDER HEAD — CRACKED (NR 5) · airframe 33,885 hrs

DURING 100HR INSPECTION BORESCOPING ENG, FOUND NR 5 CYLINDER CRACKED FROM LOWER SPARK PLUG BOSS PROCEEDING TO CYLINDER TO EXHAUST VLV. CRACK WAS 1/2 INCH LONG.

Source: SDR YAAA2015051419
OTHER · 2015-05-14 Unresolved
ATA 8530

Part: CYLINDER HEAD — CRACKED (NR 2) · airframe 33,885 hrs

DURING 100HR INSPECTION BORESCOPING ENG, FOUND NR 2 CYLINDER CRACKED FROM LOWER SPARK PLUG BOSS PROCEEDING TOWARDS EXHAUST VLV. CRACK WAS APPROX 1/2 INCH LONG.

Source: SDR YAAA2015051418
ENGINE STOPPAGE; ENGINE CASE PENETRATION; PARTIAL RPM/PWR LOSS · 2013-03-06 Unresolved
ATA 8520

Part: PISTON — FRACTURED (ENGINE) · airframe 31,641 hrs

NUMBER 1 PISTON WAS FRACTURED AT THE PISTON PIN BORE, RELEASING THE NR 1 ROD AND PISTON PIN ASSY AT THE SMALL END. THE UNSUPPORTED NR 1 ROD AND PISTON ASSY CAUSED EXTREME MECHANICAL DAMAGE TO THE REAR SECTION OF THE CRANKCASE AND CAMSHAFT.

Source: SDR YAAA201306200001
OTHER · 1995-05-18 Unresolved
ATA 8520

Part: CAMSHAFT — FAILED (CYL 3-4 LOBE)

FAILURE OF CAMSHAFT AT NR 3 AND NR 4 INTAKE LOBE. DESTROYED LIFTER BODIES, METAL IN ENGINE, ETC. TIME SINCE OVERHAUL 486.1 HOURS.

Source: SDR 95ZZZX4262