N9651M

CESSNA 207A · 1981 · Valid Registration

Registered owner: GRANT AVIATION INC, AK (owner ≠ operator)

Operators of this aircraft

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

OperatorRolePeriodBasis
GRANT AVIATION INC (ENHA)Certificate holderMatched by certificate designator
GRANT AVIATION INC (ENHA)Operator2024-06-02 – 2024-06-02Operator named in NTSB report

Accident & incident history

Acc · 2024-06-02 Operator named in NTSB report
CESSNA 207A None injury Part 135GRANT AVIATION INC
Source: NTSB case ANC24LA043
Accident · 1991-02-10 Unresolved
Cessna 207 Minor injuryoperator not yet resolved
Source: NTSB case ANC91LA027
Accident · 1988-12-28 Unresolved
Cessna 207 Minor injuryoperator not yet resolved
Source: NTSB case ANC89LA029
Accident · 1971-07-08 Unresolved
Mooney M20F Fatal injuryoperator not yet resolved
Source: NTSB case NYC72AN005

Maintenance disclosures

B · 2022-08-23 Matched by certificate designator
ATA 2312

PILOT REPORTS AUDIO CIRCUIT BREAKER POPPED, SMOKE. MAINTENANCE INSPECTED AUDIO PANEL ELECTRICAL SYSTEM. NO DEFECTS NOTED, REPLACED AUDIO PANEL, OPS CHECK GOOD.

Source: SDR ENHA LP229029 · FAA SDRS
H · 2022-08-19 Matched by certificate designator
ATA 2424

DURING FLIGHT RADIO AND ADSB STOPPED WORKING WHILE IN FLIGHT. MAINTENANCE INSPECTED AIRCRAFT AND REPLACED VOLTAGE REGULATOR AND MAIN BATTERY.

Source: SDR ENHA202290240002 · FAA SDRS
J B · 2020-07-16 Matched by certificate designator
ATA 2434

LOW VOLTAGE LIGHT ILLUMINATED. 30 SECONDS LATER A STRONG ELECTRICAL BURNING SMELL CAME FROM BEHIND THE PANEL FOLLOWED BY A VERY SMALL AMOUNT OF SMOKE. RAN ELECTRICAL FIRE IN FLIGHT CHECKLIST AND LANDED 10 MINUTES LATER IN CHEFORNAK AND CALLED MX CONTROL TO REPORT ISSUE

Source: SDR 2020FA0000338 · FAA SDRS
R J · 2011-07-12 Matched by certificate designator
ATA 8500

AFTER MAKING A NORMAL TAKEOFF FROM THE AIRPORT AND CLIMBING TO 2000 FT, APPROX 5 MINUTES INTO THE FLIGHT, THE PILOT NOTED AN ENGINE SURGE AFTER WHICH THE RPM DROPPED SLIGHTLY. THIS WAS FOLLOWED BY ENGINE ROUGHNESS. A CHECK OF THE ENGINE INSTRUMENTS CONFIRMED ALL ENGINE INDICATIONS WERE WITHIN THE NORMAL OPERATING PARAMATERS. THE PILOT SIMULTANEOUSLY EXECUTED A 180 DEGREE TURN TO RETURN TO AIRPORT. APROX 30 SECONDS LATER THERE WAS A LOUD BANG FOLLOWED BY A SUDDEN STOPAGE OF THE PROP. THE PILOT SUCCESSFULLY EXECUTED A POWER OFF LANDING ON A REMOTE BEACH THAT RESULTED IN NO DAMAGE TO THE ACFT. UPON EXAMINATION BY MX, A LARGE HOLE WAS DISCOVERED IN THE UPPER LT SIDE OF THE ENGINE CASE. A CONNECTING ROD IS PROTRUDING FROM THE CASE AND CRANKSHAFT COUNTERWEIGHT APPEARS TO BE DETACHED FROM THE CRANKSHAFT. THE EXACT CAUSE OF THE CATESTROPHIC INTERN ENGINE FAILURE IS AT THIS TIME, BEYOND THE SCOPE OF OUR ABILITIES TO DETERMINE.

Source: SDR ENHA2011F00000 · FAA SDRS
O · 2005-05-01 Matched by certificate designator
ATA 2420

ALTERNATOR LOW VOLTAGE.

Source: SDR ENHA0515 · FAA SDRS
O · 2004-09-10 Matched by certificate designator
ATA 2420

FIELD OPEN. UNIT FAILED.

Source: SDR ENHA0501 · FAA SDRS