N9310F
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
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.
7 reports on file, 2005-02-21 – 2025-01-09.
Part: BOLT — BROKEN (ZONE 700) · airframe 26,042 hrs · 45,202 cycles
LEFT BRAKE CALIPER INOPERATIVE. MECHANICS FOUND THE BRAKE CALIPER GUIDE PIN BROKEN AND THE PIN/CALIPER HAD DAMAGED THE TORQUE PLATE AS WELL AS THE TIRE/WHEEL ASSEMBLY. MECHANICS REPLACED THE CALIPER, TORQUE PLATE AND WHEEL/TIRE ASSEMBLY WITH NEW OR SERVICEABLE PARTS. THESE PARTS ARE ON CONDITION AND THEIR TOTAL TIME IS NOT TRACKED. THE TOTAL TIMES AND CYCLES IN SERVICE BELOW ARE THE AIRCRAFT TOTAL TIMES AND CYCLES.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 24,576 hrs · 42,743 cycles
DURING SCHEDULED INSPECTIONS PER CESSNA TASK 53-10-00-257 ,A CRACK WAS NOTED AT THE HORIZONYAT RH AFT FITTING.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 24,576 hrs · 42,743 cycles
DURING SCHEDULED INSPECTION PER CESSNA TASK 53-10-00-250 ,A CRACK WAS NOTED AT UPPER CENTER ENGINE MOUNT FITTING.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 24,576 hrs · 42,753 cycles
DURING SCHEDULED INSPECTION PER CESSNA TASK # 57-10-01-250, CRACKS WERE NOTED ON LH&RH ,FWD AND AFT LOWER STRUT FITTINGS.
Part: BRAKE — UNKNOWN (RIGHT) · airframe 22,555 hrs · 38,771 cycles
PILOT REPORTED NO RIGHT BRAKE WHILE TURNING ONTO RUNWAY TO LINEUP AND TAKEOFF ON 19R AT PABE. MAINTENANCE INSPECTED BRAKE ASSEMBLY AND FOUND SERVICEABLE, REPLACED BRAKE LININGS FOR BEST PRACTICES.
Part: TURBINE BLADES — FAILED (ENGINE) · airframe 8,274 hrs · 10,169 cycles
IN CRUISE AT 9000 FT, PILOT HEARD A LOUD GRINDING NOISE & ENGINE LOST ALL POWER. DECLARED AN EMERGENCY, ATTEMPTED ENGINE RESTART, NO SUCCESS. STARTER WAS ENGAGED NG SHOWED NO ROTATION & INSTRUMENT LIGHTS DIMMED. PROP FEATHERED, NORMAL LANDING. PRELIMARY REPORT FROM MX, METAL FOUND IN OIL FILTER. ENGINE HAD A STATIC PROP STRIKE 3/27/2006 498 HRS PREVIOUSLY THAT REQUIRED PROP TO BE CHANGED. ENGINE INSPECTED PER MM 72-00-00 PG 641 & RETURNED TO SERVICE. ENGINE HAD 1321.8 HOURS REMAINING TO 6000 HR OVERHAUL & IS OPERATED WITH ON CONDITION HOT SECTION. OIL FILTER WAS LAST INSPECTED 8/13/2006 14 HRS PREVIOUSLY, NO DEFECTS FOUND. SEPTEMBER 19, 2006 THE ENGINE WAS SPLIT AT THE "C" FLANGE TO ACCESS THE CT DISK.
Part: PISTON — DISLODGED (BRAKE ASSY) · airframe 6,586 hrs · 6,899 cycles
ON LANDING AT KCG BRAKING WAS LOSS ON LT SIDE. AIRCRAFT ROLLED OUT NORMAL. MAINTENANCE FOUND TWO BRAKE PISTON SEALS ON LT BRAKE CALIPER HAD FAILED CAUSING A LOSS OF FLUID. CALIPER WAS REPLACED AND BRAKES BLED.