N135AE
Registered owner: DODSON INTERNATIONAL PARTS INC, KS (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.
28 reports on file, 1996-01-31 – 2011-08-26.
Part: PISTON — MISMANUFACTURED
IMPROPER PISTON SKIRT MACHINING CAUSED PISTON CONTACT WITH CONNECTING ROD AND CRANK SHAFT. PISTON, PN 654857C. NEED IMPROVED QA IN MACHINING.
Earlier reports · 1996–2003 · 27 reports
2003
Part: BATTERY — OVERHEATED (MASTER) · airframe 8,032 hrs
BATTERY STARTS SLOW AND GETS HOT. SHOP REPAIR.
Part: GPS — INOPERATIVE (COCKPIT) · airframe 7,789 hrs
PILOT REPORTS GPS IS INOPERATIVE. TO BE SENT TO VENDOR FOR REPAIR.
Part: BATTERY — INOPERATIVE (MAIN)
AIRCRAFT WILL NOT START. REPLACED MAIN BATTERY.
2002
Part: ROTOR HEAD — DAMAGED (TAIL ROTOR)
UNABLE TO BALANCE TAIL ROTOR HEAD. REPAIRED. REPLACED TWO EACH BLADES DUE TO PAINT ERODED.
Part: GPS — MALFUNCTIONED (COCKPIT) · airframe 7,679 hrs
PILOT REPORTS THAT GPS TAKES 5-10 MINUTES TO CHANGE FUNCTIONS. PERFORMED PRELIMINARY INSPECTION. VERIFIED UNIT TAKES TOO LONG TO LOCK ON AND CRSR AND ENT BUTTONS INTERMITTENT AND NAV LED NOT WORKING. SENT TO GARMIN INTERNATIONAL FOR INSPECTION AND REPAIR.
1999
Part: TRANSDUCER — INOPERATIVE (FUEL SYSTEM)
TRANSDUCER INOPERATIVE.
Part: PUMP — LEAKING (FUEL BOOST)
MOTOR FLANGE SEEP/STATIC LEAK.
Part: AUDIO CONTROL — MALFUNCTIONED (COCKPIT)
AUDIO CONTROL CAUSED LOUD SQUEAL IN HEADSETS.
Part: CASE — CORRODED (T/R GEARBOX)
TAIL ROTOR GEARBOX CORRODED ON CASE ASSEMBLY.
Part: FILTER ASSEMBLY — MALFUNCTIONED (ENGINE OIL)
FILTER ASSEMBLY WILL NOT BYPASS.
Part: TRANSCEIVER — MALFUNCTIONED (E/E BAY)
TRANSCEIVER HAS LOW POWER OUT ON HIGH END OF FREQUENCY BAND.
1998
Part: TRANSDUCER — MALFUNCTIONED (FUEL SYSTEM)
TRANSDUCER - FLUCTUATING READINGS.
Part: INDICATOR — STICKING (MAST MOMENT)
MAST MOMENT INDICATION INTERMITTENT, NEEDLE STICKS.
Part: WARNING BOX — MALFUNCTIONED (ROTOR RPM)
RPM WARNING, INTERMITTENT DURING CRUISE FLIGHT.
Part: TRANSMITTER — MALFUNCTIONED (MAST MOMENT)
TORQUE TRANSMISSION INTERMITTENT, NEEDLE STICKS.
Part: VALVE — FAULTY (ENGINE COMPART)
DOES NOT CLOSE COMPLETELY WHEN ECU STARTER OFF.
Part: BEARING — UNBONDED (MIXING LEVER)
TEFLON UNBONDING FROM BEARING. REPLACED WITH NEW BEARING.
Part: GPS — FAILED (COCKPIT)
GPS INTERNAL BATTERY IS DEAD.
Part: COMPASS — FAILED (COCKPIT)
MAG COMPASS DOES NOT COMPENSATE.
1997
Part: NOZZLE — CRACKED (TURBINE NR 1)
ENGINE REMOVED DUE TO N1 DRAG. UPON INSPECTION OF TURBINE PARTS NOTED: BURNT AND CRACKED BEYOND SERVICEABLE LIMITS ON NR1 NOZZLE VANES. INSTALLED A DALLAS AIRMOTIVE OVERHAULED NR1 NOZZLE.
Part: GPS 150 — FAILED (COCKPIT)
GPS INTERNAL BATTERY DEAD.
Part: SEAL — LEAKING (OIL PUMP)
1 YEAR DUE 8-23-97. SHAFT SEAL LEAKING OUT SEAL DRAIN.
Part: BATTERY — FAILED (DC SYS)
BATTERY DEAD; NOT CHARGED. WOULD NOT HOLD CHARGE.
1996
Part: RPM WARN BOX — FAILED (M/R)
WARNING HORN AND LIGHT WOULD COME ON IN LEVEL FLIGHT.
Part: TRANSPONDER — MALFUNCTION (COCKPIT ATC)
TRANSPONDER WORKS INTERMITTENTLY. FOUND MAXIMUM POWER OUT TO BE APPROXIMATELY 20 WATTS. REPLACED CAVITY TUBE V101. REPAIRED. ADJUSTED FREQUENCY. COOKED UNIT UNDER HEAT LAMP, VIBRATED AND PUT IN FREEZER. BENCH CHECK GOOD.
Part: TRANSCEIVER — INOPERATIVE (COCKPIT)
RADIO INOPERATIVE.
Part: DISPLAY — FAILED (COCKPIT VHF)
NO DISPLAY. FOUND BROKEN DISPLAY. REPLACED DISPLAY DS901. APPLIED DC4 COMPOUND. REPAIRED.