N1026V

CESSNA 208B · 1992 · 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

Accident & incident history

No NTSB accidents or incidents on file for this aircraft.

Maintenance disclosures

B · 2019-11-08 Matched by certificate designator
ATA 3097

PILOT LOG PAGE DISCREPANCY: "USE OF WINDSHIELD HEAT CAUSED ELECTRICAL SPARKS TO COME FROM L/H CIRCUIT BREAKER PANEL"

Source: SDR ENHA20191111618 · FAA SDRS
O · 2019-09-26 Matched by certificate designator
ATA 5512

FROM FAA FORM 337: LEFT OUTBOARD HORIZONTAL STABILIZER LEADING EDGE DENTED. REPLACED OUTBOARD LEADING EDGE SKIN P/N 2632000-3, LEADING EDGE RIB P/N 2632021-7 AND P/N 2632021-8 WITH NEW PARTS USING ORIGINAL RIVET SIZE AND SPACING IAW SRM 55-30-00.

Source: SDR ENHA2019092600002 · FAA SDRS
O · 2019-09-26 Matched by certificate designator
ATA 5330

FROM FAA FORM 337: FOUND RT UPPER FUSELAGE SKIN (P/N 2611001-2) CRACKED AT FS 186.45, RBL 25.40, AND WL 141.00. REPLACED SKIN P/N 2611001-2 WITH NEW PART IAW FIELD REPAIR #FR-208B0319-7011.

Source: SDR EHNA2019092600003 · FAA SDRS
O · 2019-09-26 Matched by certificate designator
ATA 5730

FROM FAA FORM 337: REPAIRED SMALL HOLE APPROXIMATELY 1/8" DIAMETER ON RIGHT WING UPPER SKIN JUST FORWARD OF TRAILING EDGE AT RIGHT WING STATION 46. INSTALLED SMALL CIRCULAR PATCH IAW MODEL STRUCTURAL REPAIR MANUAL 51-78-00-8.

Source: SDR ENHA2019092600004 · FAA SDRS
O · 2019-09-26 Matched by certificate designator
ATA 5312

FROM FAA FOR 337: REPAIRED SMALL CRACK IN FUSELAGE BULKHEAD @ FS 400. STOP DRILLED CRACK AND INSTALLED DOUBLER IAW MODEL SERIES STRUCTURAL REPAIR MANUAL 53-20-00.

Source: SDR ENHA2019092600001 · FAA SDRS
O · 2019-09-26 Matched by certificate designator
ATA 5730

FROM FAA FORM 337: REPAIRED SMALL CRACK APPROXIMATELY 1" LENGTH ON RIGHT WING UPPER SKIN JUST FORWARD OF TRAILING EDGE AT RIGHT WING STATION 53. STOP DRILLED CRACK AND INSTALLED SMALL REPAIR PATCH IAW MODEL STRUCTURAL REPAIR MANUAL 51-78-00-8.

Source: SDR ENHA2019092600005 · FAA SDRS
B · 2013-11-08 Matched by certificate designator
ATA 3400

UPON TAKEOFF THE PILOT NOTICED A BURNED ODOR IN THE COCK-PIT. ALL CIRCUIT BREAKERS WERE IN, NOTHING TRIPPED. PILOT NOTICED THAT THE TRANSPONDER WAS DISPLAYING A "FAILURE" ON THE SCREEN. TURNED POWER OFF TO TRANSPONDER, AND CAME BACK AROUND FOR A SAFE LANDING. MX DETERMINED THAT THE BURNED ODOR WAS IN FACT COMING FROM THE TRANSPONDER.

Source: SDR AJAA2014F00027 · FAA SDRS
J · 2006-09-21 Matched by certificate designator
ATA 5270

ON TAKEOFF OUT OF BOS PILOT HAD A DOOR AJAR LIGHT COME ON. ABORTED TAKEOFF SECURED CARGO DOOR AND CONTINUED WITH FLIGHT.

Source: SDR BSYA200600026 · FAA SDRS
B · 2003-10-24 Matched by certificate designator
ATA 2120

GOT A STRONG ODOR (ELECTRICAL) IN COCKPIT. HAD MAINTENANCE LOOK AT AIRCRAFT COULD NOT DUPLICATE PROBLEM.

Source: SDR BSY2004F00000 · FAA SDRS
B · 2002-08-09 Matched by certificate designator
ATA 6197

ON TAKE OFF OUT OF BOSTON, SPARKS WERE FLYING OUT FROM UNDERNEATH PILOTS PANEL, RETURNED TO BASE. FOUND EXPOSED WIRE OUT OF CONNECTOR P160 ON WIRE NR HA20 ON PROPELLER DEICE CIRCUIT, SHORTED ON SIDE PANEL REPAIRED CONNECTOR, OPS GOOD.

Source: SDR BSY2002F00020 · FAA SDRS