N2753F
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.
33 reports on file, 1996-02-28 – 2003-06-13.
Part: BOLT — DAMAGED (TURBINE ASSY) · airframe 2,276 hrs
TURBINE WAS REMOVED FOR 1750 HOUR INSPECTION. UPON INSPECTION OF PARTS NOTED FRETTING MUTE ON TIE BOLT. PART SCRAPPED.
Part: BATTERY — MALFUNCTIONED (MAIN)
BATTERY HAS HIGH TEMP ON STARTS. REPLACED BATTERY.
Part: FUEL CELL — DAMAGED (FUSELAGE) · airframe 21,965 hrs
BLISTERS FILLED WITH FLUID IN AND OUTSIDE OF CELL.
Part: SKID — CORRODED (MLG) · airframe 21,965 hrs
EXCESSIVE CORROSION ON ENTIRE LENGTH OF SKID TUBE. SCRAPPED.
Part: TRANSPONDER — INOPERATIVE (ATC SYSTEM) · airframe 22,530 hrs
ATC TRANSPONDER NOT TRANSMITTING. FOUND PHOTOCELL V301 BAD, PHOTOCELL LENS MISSING AND CODE SWITCHES NOISY. REPLACED PHOTOCELL V301, LENS AND CLEANED CODE SWITCHES. REPAIRED. BENCH CHECK GOOD.
Part: PITCH LINK — CORRODED (M/R HEAD) · airframe 21,965 hrs
MAIN ROTOR PITCH CONTROL LINK HAS EXCESSIVE CORROSION ON AREA OF FORK MOUNT POINTS. SCRAPPED.
Part: SERVO — LEAKING (FLIGHT CONTROL) · airframe 21,965 hrs
FLIGHT CONTROL SERVO LEAKING. REPAIRED.
Earlier reports · 1996–2002 · 26 reports
2002
Part: OIL COOLER — MALFUNCTIONED (ENGINE) · airframe 11,965 hrs
OIL TEMPERATURE AT 100 DEGREES NEAR RED LINE IN FLIGHT.
Part: SERVO — LEAKING (ROTOR SERVO SYS) · airframe 21,965 hrs
ROTOR SERVO LEAKING. REPLACED WITH SERVICEABLE PART.
Part: SERVO — LEAKING (ROTOR SERVO SYS) · airframe 21,965 hrs
ROTOR SERVO LEAKING. REPLACED WITH SERVICEABLE PART.
Part: BEARING — CORRODED (ANTI TORQUE SYS)
TAIL ROTOR ANTI TORQUE LINKAGE BEARING CORRODED AND RUSTY. REPLACED WITH SERVICEABLE PART.
Part: TUBE — CORRODED (CYCLIC CONTROL) · airframe 21,965 hrs
CORROSION ON OUTSIDE OF TUBE CHAMFER EDGE. REPLACED WITH SERVICEABLE PART.
Part: TUBE — CORRODED (CYCLIC CONTROL)
CYCLIC CONTROL LINKAGE TUBE IS CORRODED. REPLACED WITH SERVICEABLE PART.
Part: CROSSTUBE — CORRODED (MLG) · airframe 21,960 hrs
CROSSTUBE CORRODED BEYOND LIMITS. SCRAPPED.
Part: TUBE — CORRODED (MAIN ROTOR) · airframe 21,965 hrs
CONTROL TUBE HAS CORROSION ON INSIDE OF TUBE CHAMFER EDGE. REPLACED WITH SERVICEABLE PART.
Part: CROSSTUBE — CORRODED (MLG) · airframe 21,960 hrs
CROSSTUBE CORRODED BEYOND LIMITS. REPLACED WITH SERVICEABLE CROSSTUBE.
Part: SUPPORT — CORRODED (MAIN ROTOR) · airframe 21,965 hrs
CYCLIC CONTROL LINKAGE SUPPORT CORRODED. REPLACED WITH SERVICEABLE PART.
Part: SERVO — LEAKING (ROTOR SERVO SYS) · airframe 21,965 hrs
ROTOR SERVO SYS LEAKING. REPLACED WITH SERVICEABLE PART.
2001
Part: FUEL CONTROL — MALFUNCTIONED (ENGINE) · airframe 21,293 hrs
GOING HOT AND WOULD NOT RESPOND TO ADJUSTMENTS. REPLACED WITH SERVICEABLE FUEL CONTROL.
Part: GPS — MALFUNCTIONED (COCKPIT) · airframe 21,109 hrs
BUTTONS HARD TO PRESS. SENT TO TRIMBLE NAVIGATION FOR INSPECTION AND REPAIR.
1999
Part: GEARSHAFT — SPALLED (GEARBOX)
ENGINE REMOVED DUE TO MAKING METAL. UPON INSPECTION OF GEARBOX NOTED THE FOLLOWING: SPALLING BEYOND SERVICEABLE LIMITS ON F/C O/P GEAR TEETH. INSTALLED NEW PART.
Part: TRANSCEIVER — BROKEN (COCKPIT)
TRANSCEIVER'S CIRCUIT RUN ON R 477 BROKEN AND RIGHT HAND SIDE RAIL BROKEN.
Part: INDICATOR — READS LOW (ENGINE OIL)
ENGINE OIL TEMPERATURE READS 15 DEGREES LOW AT STATIC, WILL NOT GO ABOVE 30 DEGREES WITH ENGINE RUNNING.
Part: STARTER — NOISY (START/GENERATOR)
GRINDING NOISE AND THROWING SPARKS.
Part: ACTUATOR — FAILED (ENGINE DEICE)
ACTUATOR WILL NOT ACTUATE.
Part: ACTUATOR — INOPERATIVE (MAIN ROTOR)
ACTUATOR WILL NOT EXTEND OR RETRACT.
1998
Part: RECEIVER — INTERMITTENT (COCKPIT GPS)
GPS RECEIVER INTERMITTENTLY LOCKING ON TO SATELLITES.
Part: INDICATOR — MALFUNCTION (COCKPIT)
ATTITUDE INDICATOR SLOW TO REACT TO MOVEMENT.
1997
Part: FIN — CORRODED (VERT FIN)
VERT FIN CORROSION AND SEPARATED BEYOND REPAIR.
Part: SENSOR — FLUCTUATES (TANK UNIT)
TANK UNIT FLUCTUATES.
Part: FUEL VALVE — LEAKING (SHAFT)
FUEL VALVE LEAKING FROM SHAFT.
1996
Part: INDICATOR — DEFECTIVE (COCKPIT)
INDICATOR FACE IS ROTATED 45 DEGREES FROM VERTICAL.
Part: STRAP — CRACKED (RT BOX BEAM)
R/H BOX BEAM STRAP CRACKED AT UPPER AFT RADIUS JUST BELOW HIGH SHEER RIVETS. REPLACED STRAP AND RETURNED TO SERVICE.