N767P
Registered owner: AVIATION INVESTMENTS INC, VA (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.
6 reports on file, 2006-02-12 – 2007-08-21.
Part: AUTOPILOT SYS — UNKNOWN · airframe 2,035 hrs
DURING HOVER FOR TAKEOFF, AFCS KICKED HARD. LANDED AIRCRAFT GROUND TAXIED TO PARKING. MAINTENANCE INSPECTED THE AIRCRAFT, CONNECTED A HYDRAULIC MULE AND WORKED ALL CONTROLS. THEY WERE UNABLE TO DUPLICATE THE DISCREPANCY.
Part: WIRE — CHAFED · airframe 1,824 hrs
TRIM FAIL AND MASTER CAUTION LIGHT BLINK IN HOVER. SYSTEM OPERATES NORMALLY. MAINTENANCE REPAIRED CHAFED WIRING IN CENTER CONSOLE TO CONTROL PANEL.
Part: WIRE HARNESS — DAMAGED (MLG) · airframe 1,812 hrs
RAISED GEAR. ALL (3) GREEN LIGHTS AND RED LIGHTS WENT OUT. RT MAIN GREEN LIGHT THEN CAME ON. LOWERED GEAR. RETURNED TO BASE. MAINTENANCE REPLACED RT MAIN PROXIMITY SWITCH HARNESS.
Part: PITOT TUBE — OBSTRUCTED · airframe 973 hrs
DURING AFTER TAKEOFF CHECK, RAISED GEAR AND LANDING GEAR LIGHT STAYED ILLUMINATED WITH AUDIO. MAINTENANCE FOUND MUD DOBBER WASP NEST IN THE PITOT TUBE INLET.
Part: STARTER GEN — FAILED (NR 2)
NR 2 GENERATOR FAIL LIGHT CAME ON 20 MINUTES INTO CRUISE FLIGHT. EXECUTED EMERGENCY PROCEDURE, DID NOT RESET. RETURNED TO DEPARTURE. MAINTENANCE REPLACED STARTER GENERATOR.
Part: TUBE — LOOSE (HYD SYS) · airframe 180 hrs
NR 1 SERVO LIGHT CAME ON. SLOWED AIRCRAFT BELOW 125 KTS. EXPERIENCED NO BINDING OF LOSS OF HYDRAULIC PRESSURE. RECYCLED SERVO JAM CIRCUIT BREAKER, LIGHT STAYED ON. LIGHT WENT OUT UPON LANDING. MAINTENANCE FOUND THE B-NUT ON THE FORWARD END OF TUBE HAD BACKED OFF AT FITTING PN AN924-4J IN THE FORWARD END OF THE TAIL BOOM ALLOWING A LOSS OF HYDRAULIC FLUID. TIGHTENED THE B-NUT AND SERVICED THE HYDRAULIC SYSTEM. RAN AIRCRAFT AND SYSTEM LEAK CHECKED GOOD.