N719PH
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.
96 reports on file, 1998-07-27 – 2019-04-01.
Part: SKIN — CORRODED (FUSELAGE) · airframe 14,509 hrs
FORWARD SHELL ASSEMBLY OUTER SKIN WAS FOUND TO BE CORRODED. THE FORWARD SHELL ASSEMBLY WILL THEN BE REPAIRED IN ACCORDANCE WITH THE FAA APPROVED REPAIR DATA.
Earlier reports · 1998–2012 · 95 reports
2012
Part: PANEL — CORRODED · airframe 10,017 hrs
UPPER SKIN ON OIL COOLER PANEL ASSY WAS FOUND TO BE CORRODED.
2003
Part: CELL — BURNED (BATTERY) · airframe 2,751 hrs
BATTERY CELL BURNED. REPLACED BATTERY.
Part: VALVE — LEAKING (FLOAT BOTTLE) · airframe 2,751 hrs
FLOAT BOTTLE VALVE LEAKING. REPLACED VALVE 206-373-901-103 DUE TO LEAKING AT PILOT VALVE VENT. REPAIRED.
Part: MOUNT — WORN (ENGINE) · airframe 2,668 hrs
ENGINE MOUNT HAS A WORN BEARING.
Part: UNIVERSAL — WORN (M/R DRIVE) · airframe 2,614 hrs
MAIN ROTOR DRIVE UNIVERSAL WORN.
Part: BATTERY — WEAK (MAIN)
MAIN BATTERY WEAK. REPAIRED.
Part: SHAFT — WORN (BLOWER ASSY) · airframe 2,390 hrs
BLOWER ASSY SHAFT SPLINES ARE WORN BEYOND LIMITS. REPAIRED.
Part: CONTACTOR — FAILED (ELECTRICAL) · airframe 2,285 hrs
DURING START ATTEMPTS STARTER FAILED TO CATCH.
Part: PLENUM — CRACKED (ENGINE) · airframe 2,390 hrs
PLENUM IS CRACKED.
Part: SUPPORT — WORN (HEADREST) · airframe 2,390 hrs
PIN HOLES WORN ON HEADREST CAUSING BINDING.
Part: WINDSHIELD — CRAZED (COCKPIT) · airframe 2,390 hrs
RT WINDSHIELD CRAZED.
Part: CONE — CORRODED (M/R GEARBOX) · airframe 2,390 hrs
MAIN ROTOR GEARBOX LOWER CONE PITTED ON FACE.
Part: WINDSHIELD — CRAZED (COCKPIT) · airframe 2,390 hrs
RT WINDSHIELD CRAZED.
Part: LINK — DAMAGED (TAIL ROTOR) · airframe 2,390 hrs
LINK ASSY HAS A ROUGH AND DAMAGED BEARING.
Part: PITCH LINK — CORRODED (MAIN ROTOR) · airframe 2,390 hrs
MAIN ROTOR PITCH LINK HAS CORROSION.
Part: SPLINE ADAPTER — WORN (ENGINE TO GB) · airframe 2,390 hrs
ENGINE TO GEARBOX SPLINE ADAPTER HAS WORN SPLINES.
Part: BOLT — DAMAGED (M/R BLADES) · airframe 2,390 hrs
MAIN ROTOR BLADE BOLTS HAVE MECHANICAL DAMAGE AT TOP OF SHANK AT GROOVE.
Part: PIN — GALLED (M/R DRIVE LINK) · airframe 2,390 hrs
GALLING AND PITTING ON THE INBOARD END OF THE MAIN ROTOR DRIVE LINK PIN.
Part: UNIVERSAL — WORN (MAIN ROTOR) · airframe 2,380 hrs
MAIN ROTOR UNIVERSAL HAS BEARING WEAR.
Part: BOLT — WORN (M/R BLADE) · airframe 2,390 hrs
MAIN ROTOR BLADE BOLT SHANK HAS TWO WORN SPOTS.
Part: HOUSING — CRACKED (BLOWER) · airframe 2,390 hrs
TAIL ROTOR BLOWER HOUSING CRACKED.
Part: INTAKE — CORRODED (BELLMOUTH) · airframe 2,390 hrs
BELLMOUTH INTAKE HAS CORROSION.
Part: SERVO — LEAKING (ROTOR SERVO) · airframe 2,390 hrs
ROTOR SERVO HAS A STATIC LEAK.
Part: SKID — CORRODED (MLG) · airframe 2,390 hrs
SKID TUBE CORRODED BEYOND LIMITS.
Part: SERVO — WORN (CYCLIC) · airframe 2,390 hrs
CYCLIC SERVO BEARING ON AFT END OF SERVO IS WORN.
Part: DRIVE SHAFT — CORRODED (M/R GEARBOX) · airframe 2,390 hrs
MAIN ROTOR GEARBOX DRIVE SHAFT IS PITTED ON FLEX FRAMES AND INSIDE OF SHAFT.
Part: HANDLE — WORN (CREW DOOR) · airframe 2,390 hrs
CREW DOOR HANDLE WORN. TO BE SENT TO BELL FOR CREDIT.
Part: HOSE — CUT (FUEL DIST) · airframe 2,390 hrs
FUEL HOSE ASSY CUT IN COVERING, INTO THE BRAID.
Part: GPS — MALFUNCTIONED (COCKPIT) · airframe 2,390 hrs
GPS RECEIVER LOSES POWER WHEN CHECKING NAV FLAG.
Part: HANDLE — WORN (CREW DOOR) · airframe 2,390 hrs
CREW DOOR HANDLE WORN. TO BE SENT TO BELL FOR CREDIT.
2002
Part: SOLENOID VALVE — MALFUNCTIONED (ANTI ICE SYSTEM) · airframe 2,192 hrs
SOLENOID VALVE STICKING OPEN AND INTERMITTENT OPERATION.
Part: COVER — TORN (EMERGENCY FLOAT) · airframe 2,183 hrs
EMERGENCY FLOAT COVER FRONT FLAP FRAYED AND TORN.
Part: INDICATOR — INOPERATIVE (ENG OIL TEMP) · airframe 2,157 hrs
ENGINE OIL TEMPERATURE INDICATOR INOPERATIVE.
Part: INDICATOR — MALFUNCTIONED (ENG OIL TEMP) · airframe 2,145 hrs
ENGINE OIL TEMP INDICATOR LED LIGHTING WILL NOT BRIGHTEN.
Part: FILTER — BYPASSING (ENGINE OIL) · airframe 2,169 hrs
BYPASS BUTTON POPPED. REPLACED WITH SERVICEABLE FILTER.
Part: ECU — DAMAGED (ENGINE) · airframe 1,676 hrs
ECU HAS A BROKEN CONNECTOR PIN.
Part: CONNECTOR — CORRODED (ECU) · airframe 1,675 hrs
FADEC FAULT AND FADEC DEGRADE LIGHT ILLUMINATED. ECU HAS CORROSION ON CONNECTOR AND HAD QUIET MODE SWITCH FAULT INDICATED. REPLACED WITH SERVICEABLE ECU.
Part: MOUNT — WORN (ENGINE) · airframe 2,095 hrs
ENGINE MOUNT BEARING WORN.
Part: BEARING — ROUGH (PITCH CONTROL) · airframe 2,095 hrs
MAIN ROTOR PITCH CONTROL LINK BEARING ROUGH.
Part: UNIVERSAL — WORN (MAIN ROTOR) · airframe 1,968 hrs
MAIN ROTOR UNIVERSAL WORN.
Part: ECU — MALFUNCTIONED (ENGINE) · airframe 2,074 hrs
FADEC FAULT AND FADEC DEGRADE LIGHTS ILLUMINATED. CLEARED FAULT. REPLACED WITH SERVICEABLE ECU.
Part: BULB — BURNED OUT (EXTERNAL) · airframe 2,011 hrs
LIGHT BURNED OUT. SCRAPPED AND REPLACED WITH SERVICEABLE PART.
Part: WINDOW — CRACKED (PAX CABIN) · airframe 1,975 hrs
RT PASSENGER WINDOW IS CRACKED NEAR UPPER MOUNTING SCREW HOLE. SCRAPPED AND REPLACED WITH SERVICEABLE PART.
Part: TRANSMITTER — INTERMITTENT (TORQUE) · airframe 1,953 hrs
TORQUE INDICATION INTERMITTENT.
Part: INDICATOR — INTERMITTENT (ENG TORQUE) · airframe 1,962 hrs
TORQUE INDICATOR WORKS INTERMITTENTLY.
Part: PAD — FLAKING (BRAKE) · airframe 1,868 hrs
BRAKE PAD IS FLAKING, CAUSED BY VIBRATION.
Part: HOUSING — CORRODED (MAIN ROTOR) · airframe 1,868 hrs
MAIN ROTOR HOUSING REMOVED FOR AN EVALUATION DUE TO EXCESSIVE CORROSION UNDER PAINT.
Part: PUMP — LEAKING (FUEL BOOST) · airframe 1,868 hrs
FUEL BOOST PUMP LEAKING OUT OF SEAL DRAIN.
2001
Part: CARTRIDGE — INOPERATIVE (FUEL PUMP) · airframe 1,821 hrs
FUEL PUMP CARTRIDGE INOPERATIVE.
Part: FITTING — BROKEN (HYD HOSE) · airframe 1,729 hrs
FITTING BROKE OFF IN HOSE END, CANNOT REMOVE.
Part: HOUSING — CRACKED (T/R BLOWER) · airframe 1,623 hrs
BLOWER HOUSING HAS CRACKS. TO BE RETURNED TO VENDOR.
Part: COVER — WORN (FLOAT)
COVER WORN AND END CAP LOOSE. TO BE RETURNED TO VENDOR.
Part: DUCT — CRACKED (OIL COOLER) · airframe 1,623 hrs
OIL COOLER TRANSITION DUCT IS CRACKED. TO BE RETURNED TO VENDOR.
Part: BEARING — WORN (TAIL ROTOR)
WORN. TO BE RETURNED TO VENDOR. (J0168105-WA)
Part: TRANSMITTER — READS LOW (OIL PRESSURE) · airframe 1,622 hrs
ENGINE OIL PRESSURE READING LOW. TO BE RETURNED TO VENDOR.
Part: INLET — CRACKED (T/R OIL COOLER) · airframe 1,623 hrs
OIL COOLER INLET COVER CRACKED. TO BE RETURNED TO VENDOR.
Part: GAUGE — CONTAMINATED (MLG) · airframe 1,836 hrs
MOISTURE IN GAUGE.
Part: GAUGE — READS LOW (MLG) · airframe 1,536 hrs
READS LOW.
Part: RECEPTACLE — FAILED (TAIL) · airframe 1,392 hrs
TAIL LIGHT WON'T LIGHT. SCRAPPED LOCALLY.
Part: COVER — TORN (FLOAT) · airframe 1,459 hrs
FLOAT COVER HAS TORN END CAPS.
Part: CONTROL UNIT — FAILED (COCKPIT) · airframe 1,453 hrs
WHEN BATTERY SWITCH IS TURNED ON, FWD LANDING WOULD NOT TURN OFF. ALSO FWD LIGHT WOULD NOT PULSATE.
Part: BEARING — DAMAGED (ENGINE MOUNT) · airframe 1,440 hrs
REAR ENGINE MOUNT BEARING UNSTAKED. SENT TO DALLAS AIRMOTIVE FOR OVERHAUL.
2000
Part: DUCT — CRACKED (OIL COOLER)
DUCT IS CRACKED IN CORNER AT BLOWER END.
Part: BEARING — WORN (LEG ASSY)
EXCESSIVE WEAR ON BEARING.
Part: CHANNEL — CRACKED (FUSELAGE)
CHANNEL CRACKED IN RADIUS.
Part: ANGLE — CRACKED (FUSELAGE)
ANGLE CRACKED AT RIVET HOLE.
Part: OIL TUBE — CRACKED (SLEEVE)
OIL TUBE HAS CRACKED SLEEVE.
Part: LINK — WORN (TAIL ROTOR)
LINK HAD WORN BEARINGS. SERIAL NUMBERS REMOVED ARE NHFS-3303 AND NHFS-3299. REPLACED WITH SERIAL NUMBERS NHFS-4662 (DMR NR 65600801) AND NHFS-4672 (DMR NR 65600900).
Part: INDICATOR — FAILED (MGT)
MGT INDICATOR QUIT ON ENGINE WASH.
Part: SWITCH — STICKING (M/R GEARBOX)
PRESSURE SWITCH STICKS IN OPEN POSITION.
1999
Part: UNIVERSAL — WORN (M/R DRIVE)
UNIVERSAL BEARING WORN.
Part: DUCT — CRACKED (EXHAUST)
DUCT CRACKED NEAR MOUNTING BRACKET.
Part: GASKET — MISSING (COMPASS)
COMPASS HAD GASKET MISSING UNDER FACEPLATE.
Part: PUMP — WORN (TRANSMISSION OIL)
TRANSMISSION OIL PUMP SPLINES WORN.
Part: HOUSING — CRACKED (M/R GEARBOX)
HOUSING ASSY CRACKED.
Part: ADAPTER — WORN (T/R SPLINE)
SPLINES WORN CONSIDERABLY ON THE TRANSMISSION OIL PUMP SIDE.
Part: COVER ASSY — FRAYED (FLOAT)
END COVER FRAYED ON FLOAT COVER. REFERENCE: DMR NR 686358.
Part: TRANSMITTER — FLUCTUATES (OIL PRESSURE)
ENGINE OIL PRESSURE FLUCTUATES ON WASH. REFERENCE: DMR NR 686434.
Part: TRANSMITTER — INTERMITTENT (ENGINE TORQUE)
TORQUE INTERMITTENTLY INOPERATIVE. REFERENCE: DMR NR 686461.
Part: INDICATOR — FLUCTUATES (ENGINE TORQUE)
TORQUE FLUCTUATES.
Part: UNIVERSAL — WORN (COLLECTIVE)
UNIVERSAL HAD WORN BEARINGS. REFERENCE: DMR NR 686205.
Part: LINK ASSY — WORN (PITCH CONTROL)
LINK ASSY HAD WORN BEARINGS.
Part: UNIVERSAL — WORN (M/R DRIVE)
UNIVERSAL HAD WORN BEARINGS.
Part: SWITCH — MALFUNCTIONED (TRANSMISSION OIL)
TRANS. OIL PRESSURE SEGMENT WOULD NOT COME ON. (LIGHT DOES NOT TURN ON).
Part: SWITCH — MALFUNCTIONED (COCKPIT)
FUEL LOW LIGHT STAYS ON.
Part: SIGNAL COND — CONTAMINATED (ENGINE)
SUSPECT OIL CONTAMINATION AT SIGNAL COND. LOW LEVEL FUEL INTERMITTENT.
Part: STARTER — FAILED (STARTER/GEN)
STARTER/GENERATOR FAILED 300-HOUR INSPECTION. INSPECTED BY ACCESSORY OVERHAUL SHOP AND FOUND BRUSHES EXCESSIVELY WORN AND SCARRING ON COMMUTATOR.
Part: BEARING — WORN (TAIL ROTOR)
WORN BEARINGS.
1998
Part: SWITCH — FAILED (FUEL SYSTEM)
FUEL LOW LEVEL LIGHT WAS ON WHEN BATTERY TURNED ON FOR PRE-FLIGHT. AIRCRAFT HAD 245 POUNDS OF FUEL.
Part: STARTER — FAILED (START/GEN)
GENERATOR FAILED IN-FLIGHT AND STARTER WOULD NOT TURN OVER. INSPECTED BY ACCESSORY OVERHAUL SHOP AND FOUND BRUSHES EXCESSIVELY WORN AND BURNED.
Part: INDICATOR — STICKING (MGB TACH)
MGT INDICATOR STICKS ON START-UP (WILL NOT REGISTER TEMP INDICATION UNTIL WELL INTO START).
Part: ARMATURE — FAILED (STARTER/GEN)
ARMATURE CAUSING EXCESSIVE ARCHING--BURNT SPOTS ON COMMUTATOR.
Part: GYRO — FAILED (COCKPIT)
ROTOR WILL NOT SPIN ON DIRECTIONAL GYRO. TIME SINCE REPAIR 71:00 HOURS.
Part: BEARING — ROUGH (TAIL ROTOR)
TAIL ROTOR HAS ROUGH BEARING. SERIAL NUMBERS REMOVED ARE A98-0440 AND A98-0512.
Part: GYRO — BROKEN (COCKPIT)
DIAL SCREW BACKED OUT OF CENTER DIAL SHAFT AND IS WEDGED BETWEEN DIAL AND FLAG IN DIRECTIONAL GYRO.