N784P
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.
4 reports on file, 2007-07-28 – 2015-03-25.
Part: O-RING — CUT (NR 2 ENGINE OIL) · airframe 8,229 hrs
DURING CRUISE FLIGHT NOTICED MASTER CAUTION BEGIN TO FLICKER. OBSERVED NR 2 ENGINE OIL PRESSURE BEGIN TO FLUCTUATE AND DROP. EVENTUALLY PRESSURE DROPPED BELOW RED LINE AND ENGINE OIL PRESSURE WARNING LIGHT ILLUMINATED. ON INSPECTION FOUND CUT O-RING ON OIL UNIO OF TURBINE OIL PRESSURE AND SUMP STRUT.
Part: PRESSURE SWITCH — WARNING LIGHT (HYDRAULIC SYSTEM) · airframe 2,277 hrs
NR1 HYDRAULIC SERVO LIGHT ILLUMINATED AND FLICKERED INTERMITTENTLY. FOUND WATER IN THE NR 1 HYDR PRESSURE SWITCH CONNECTOR PLUG. REMOVED WATER AND SWAPPED NR 1 AND NR 2 HYD PRESSURE SWITCHES.
Part: ACTUATOR — MALFUNCTIONED · airframe 551 hrs
DURING CLIMB, AIRCRAFT YAWED NOTICEABLY AND WAS ACCOMPANIED BY AN IE27 YAW FAILURE CAUTION LIGHT. RESET BOTH AP1 AND AP2 SWITCHES AND CAUTION LIGHT EXTINGUISHED. COLLECTIVE YAW CIRCUIT BREAKER WAS THEN FOUND TO BE TRIPPED. RESET CIRCUIT BREAKER. DURING DESCENT, A VERTICAL SPEED WAS ESTABLISED AT 400 FPM. AIRCRAFT THEN NOSED OVER AND REACHED A RATE OF 1100 FPM BEFORE PILOT DECOUPLED AP AND HAND FLEW AIRCRAFT TO LANDING. NOSE OVER WAS ACCOMPANIED BY AN IE40 ERROR. REPLACED NR 1 PITCH LINEAR ACTUATOR.
Part: PROXIMITY SWITCH — OUT OF ADJUST (NLG) · airframe 473 hrs
AFTER TAKEOFF, NOSE WHEEL CENTERING LIGHT STAYED ON. UNABLE TO RETRACT GEAR. RETURNED TO DEPARTURE. MAINTENANCE ADJUSTED GAP ON NOSE WHEEL POSITIONING ADVISORY SYSTEM.