N407GV

CESSNA 208B · 1997 · Fixed-wing single-engine · 1 engine · 12 seats · 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)Operatoron 2021-03-12Operator named in NTSB report

Accident & incident history

Accident · 2021-03-12 Operator named in NTSB report
CESSNA 208B No injuries Part 135GRANT AVIATION INC

Operated by Grant Aviation (per NTSB report)

Source: NTSB case ANC21LA025
Accident · 2000-03-04 Matched by aircraft (N-number)
Cessna 208B No injuries Part 135GRANT AVIATION INC
Source: NTSB case ANC00LA033

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.

5 reports on file, 2004-01-30 – 2025-11-01.

ELECT. POWER LOSS-50 PC · 2025-11-01 Matched by certificate designator
ATA 2400

Part: ELECTRICAL SYS — MALFUNCTIONED · airframe 32,108 hrs

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
ELECT. POWER LOSS-50 PC · 2025-11-01 Matched by certificate designator
ATA 2497

Part: SCREW — LOOSE (BUSS) · airframe 32,108 hrs

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
OTHER · 2023-10-14 Matched by certificate designator
ATA 5744

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 29,869 hrs · 65,491 cycles

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
OTHER · 2007-09-05 Matched by certificate designator
ATA 5730

Part: SKIN — CRACKED (RT WING) · airframe 12,994 hrs · 31,226 cycles

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
OTHER · 2004-01-30 Matched by certificate designator
ATA 5340

Part: SUPPORT — CRACKED (ZONE 200)

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