N407GV

CESSNA 208B · 1997 · Valid Registration

Registered owner: AVION CAPITAL CORP, 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)Operator2021-03-12 – 2021-03-12Operator named in NTSB report

Accident & incident history

Acc · 2021-03-12 Operator named in NTSB report
CESSNA 208B None injury Part 135GRANT AVIATION INC
Source: NTSB case ANC21LA025
Accident · 2000-03-04 Matched by aircraft (N-number)
Cessna 208B None injuryGRANT AVIATION INC
Source: NTSB case ANC00LA033

Maintenance disclosures

H · 2025-11-01 Matched by certificate designator
ATA 2400

PILOT NOTE DISCREPANCY AS AN ELECTRICAL POWER LOSS/MULTIPLE BUS BREAKERS POP/PFD LOSS. MAINTENANCE INSPECTED ELECTRICAL SYSTEM AND COULD NOT DUPLICATE. AIRCRAFT IS SCHEDULED TO PERFORM AN OPERATIONAL CHECK FLIGHT FOR THE ELECTRICAL SYSTEM.

Source: SDR ENHA20251103001 · FAA SDRS
H · 2025-11-01 Matched by certificate designator
ATA 2497

AFTER SECURING LOOSE SCREW ON BUS 2 STANDBY POWER CIRCUIT BREAKER (LOG PAGE 263019)AND SUCCESSFUL CHECK FLIGHT THE AIRCRAFT WAS RETURNED TO SERVICE.

Source: SDR ENHA20251101002 · FAA SDRS
O · 2023-10-14 Matched by certificate designator
ATA 5744

LEFT WING MOVES DURING FLIGHT /FLAP OPERATION. MAINTENANCE INSPECTED LEFT WING AND DETERMINED AFT ATTACH FITTINGS WERE DAMAGED AND REQUIRE REPLACEMENT. THE FOLLOWING FITTINGS WERE REPLACED: 2622021-9,2622021-1,2611139-1,2611139-2.

Source: SDR ENHA202310160001 · FAA SDRS
O · 2007-09-05 Matched by certificate designator
ATA 5730

DURING ROUTINE INSPECTION, DISCOVERED 4" CRACK ON UPPER RT AFT WING SKIN 18" FROM WING ROOT AT WS 53.00. DAMAGE WAS REPAIRED IAW CESNNA MM 51-75-00. AIRCRAFT WAS RETURNED TO SERVICE.

Source: SDR EPUA092007A · FAA SDRS
O · 2004-01-30 Matched by certificate designator
ATA 5340

PILOT REPORTED WHEN RETRACTING FLAPS ON ROLL-OUT THE FLAP CIRCUIT BREAKER TRIPPED. MX INSPECTED AND FOUND THE FLAP TRANSMISSION SUPPORT ASSY. CRACKED AND BUCKLED. THERE WAS NO EVIDENCE OF THE STANDBY FLAP SYSTEM BEING ACTIVATED.

Source: SDR EPUA300104A · FAA SDRS