N1026V
Registered owner: AVION CAPITAL CORP, AK (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| GRANT AVIATION INC (ENHA) | Certificate holder | — | Matched by certificate designator |
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
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.
10 reports on file, 2002-08-09 – 2019-11-08.
Part: WIRE — DAMAGED (HEAT SHIELD) · airframe 26,195 hrs
PILOT LOG PAGE DISCREPANCY: "USE OF WINDSHIELD HEAT CAUSED ELECTRICAL SPARKS TO COME FROM L/H CIRCUIT BREAKER PANEL"
Part: SKIN — CRACKED (FUSELAGE) · airframe 26,175 hrs · 28,161 cycles
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.
Part: SKIN — DAMAGED (RT WING) · airframe 26,175 hrs · 28,161 cycles
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.
Part: SKIN — CRACKED (RT WING) · airframe 26,175 hrs · 28,161 cycles
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.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 26,175 hrs · 28,161 cycles
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.
Part: SKIN — DENTED (LT HORIZ STAB) · airframe 26,175 hrs · 28,161 cycles
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.
Part: TRANSPONDER — FAILED (ZONE 100) · airframe 16,929 hrs · 18,871 cycles
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.
Part: DOOR — UNSECURE (CARGO) · airframe 9,989 hrs · 9,889 cycles
ON TAKEOFF OUT OF BOS PILOT HAD A DOOR AJAR LIGHT COME ON. ABORTED TAKEOFF SECURED CARGO DOOR AND CONTINUED WITH FLIGHT.
Part: ODOR — DETECTED (COCKPIT)
GOT A STRONG ODOR (ELECTRICAL) IN COCKPIT. HAD MAINTENANCE LOOK AT AIRCRAFT COULD NOT DUPLICATE PROBLEM.
Part: WIRE — LOOSE (PROP DEICE SYS)
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.