N835CA
Registered owner: HILL DAVID C, NH (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
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.
8 reports on file, 1996-03-01 – 2002-03-22.
Part: LINK — DISCHARGED (SHOCK LINK ASSY)
DURING ROUTINE INSPECTION, FOUND LEFT ENGINE ANTI-ICE VANE DOOR SHOCK LINKS MISSING PARTS AND DOOR DISCONNECTED. NOTE: DOWEL PINS FELL OUTOF SPRING RETAINER.
Part: ENGINE — OVERSERVICED (LEFT) · airframe 4,711 hrs · 4,875 cycles
LEFT ENGINE OIL TEMP IN RED ZONE. ENGINE WAS OVERSERVICED WITH OIL. DRAINED EXCESS OIL AND REPAIRED OIL REPLENISHMENT SYSTEM.
Part: SEAL — LEAKING (ENGINE OIL)
POST-FLIGHT INSPECTION FOUND OIL LEAKING FROM RT ENGINE LOWER FORWARD COWL. INSPECTION REVEALED THE SOURCE OF LEAK TO BE THE POWER SECTION OIL TRANSFER TUBE ELBOW. REPLACED 3 EACH PACKINGS. LEAK CHECK SATISFACTORY ON GROUND RUN.
Part: TURBINE — FAILED (RT ENGINE)
RIGHT ENGINE POWER LOSS ON TAKEOFF ROLL PRIOR TO FULL POWER. TAKEOFF ABORTED WITHOUT INCIDENT. LOUD 'BANG' HEARD BY CREW PRIOR TO POWER LOSS. ENGINE WAS REMOVED AND REPLACED AND AIRCRAFT RETURNED TO SERVICE. (M)
Part: STABALON — DAMAGED (AFT LT FUSELAGE)
LEFT STABALON DAMAGED BY BAGGAGE TUG COLLISION. TUG COLLIDED WITH PARKED AIRCRAFT. REMOVED AND REPLACED LT STABALON IAW CHAPTER 55 BEECH MM.
Part: TORQUE GAUGE — FAILED (COCKPIT)
LEFT ENGINE TORQUE GAUGE INOPERATIVE.
Part: EFIS CONTROL — BURNED (COCKPIT)
CAPTAINS EHSI DISPLAY BLANK.
Part: RIVETS — LOOSE (VERT STAB)
DURING SCHEDULED INSPECTIONS, LOOSE FASTENERS ON BOTH SIDES OF VERTICAL STABLILIZER FORWARD SPAR WERE NOTED. ALTHOUGH A SIMILAR PROBLEM WAS ADDRESSED IN SB 2044 ON EARLIER MODEL 1900S, ADDITIONAL EVALUATION AND STUDIES ARE RECOMMENDED AS OTHER PREVIOUS IDENTIFIED AREAS OF CONCERN IN THE EMPENNAGE SECTION MAY BE RELATED. REPAIR WAS ACCOMPLISHED PER BEECHCRAFT RECOMMENDED PROCEDURE.