N5007Q
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.
42 reports on file, 1995-04-21 – 2003-01-06.
Part: RELAY — STUCK (DC SYSTEM) · airframe 21,672 hrs
BATTERY RELAY STICKING.
Earlier reports · 1995–2002 · 41 reports
2002
Part: COMPASS — LEAKING (COCKPIT) · airframe 21,543 hrs
COMPASS LEAKING. REPLACED WITH SERVICEABLE PART.
Part: BEARING — WORN (IDLER LINKAGE) · airframe 21,740 hrs
IDLER LINKAGE HAS A WORN BEARING. REPLACED WITH SERVICEABLE PART.
2001
Part: GPS — FAILED (COCKPIT) · airframe 21,731 hrs
TAKES AN EXTENDED PERIOD OF TIME TO ACQUIRE SATTELITES. REPLACED WITH SERVICEABLE PART.
Part: INDICATOR — PRECESSES (COCKPIT) · airframe 21,690 hrs
WILL NOT CAGE AND PRECESSES. REPLACED WITH SERVICEABLE PART.
Part: CROSSTUBE — CORRODED (MLG SKID) · airframe 21,431 hrs
CORROSION PITS. SCRAPPED AND REPLACED WITH SERVICEABLE PART.
Part: INDICATOR — MALFUNCTIONED (COCKPIT) · airframe 21,141 hrs
INSTRUMENT INDICATES 3-4 PERCENT WHEN SYSTEMS ARE SHUT DOWN AND TAKES 5-6 SECONDS TO START INDICATING DURING STARTS.
Part: BUSHING — WORN (TAIL ROTOR) · airframe 21,305 hrs
WORN. REPLACED WITH SERVICEABLE ASSY.
Part: FILTER — LEAKING (ENGINE OIL) · airframe 20,909 hrs
COULD NOT GET FACET FILTER TO STOP LEAKING.
Part: GYRO — PRECESSES (COCKPIT) · airframe 20,896 hrs
PRECESSES 2 DEGREES EVERY 5 MINUTES. REPLACED WITH SERVICEABLE PART.
Part: GPS — FAILED (COCKPIT) · airframe 20,847 hrs
LOOSES SATELLITES DURING FLIGHT.
Part: INDICATOR — SPLIT (DUAL TACH) · airframe 20,894 hrs
2 PERCENT SPLIT IN NEEDLE INDICATION.
Part: COVER — LOOSE (FLOAT) · airframe 21,348 hrs
LEFT AFT FLOAT COVER FLAP VELCRO HAS COME LOOSE FROM COVER. STITCHING CAME OUT. REPLACED WITH SERVICEABLE PART.
Part: BATTERY — DISCHARGED (DC SYSTEM) · airframe 21,418 hrs
UNABLE TO START AIRCRAFT ON FIRST START ATTEMPT AND WAS WEAK ON THE SECOND START ATTEMPT. REPLACED WITH SERVICEABLE BATTERY.
1999
Part: ACTUATOR — DAMAGED (DROOP COMP)
ACTUATOR HAD EXCESSIVE PLAY ON ROD END.
Part: INDICATOR — STICKS (TORQUE METER)
TORQUE METER INDICATOR'S NEEDLE STICKS INTERMITTENTLY.
Part: GYRO — PRECESSES (COCKPIT)
DIRECTIONAL GYRO PRECESSES EXCESSIVELY.
1998
Part: PUMP — STUCK (HYD)
HYDRAULIC PUMP DRIVE SHAFT STUCK IN TACH GEN AND SPLINES WORN.
Part: INDICATOR — STICKS (COCKPIT TOT)
INDICATOR INTERMITTENTLY STICKS AT ZERO.
Part: CARTRIDGE — FAULTY (FUEL SYSTEM)
FUEL SYSTEM HAS LOW PRESSURE OUTPUT.
Part: INDICATOR — STICKS (GAS PRODUCER)
GAS PRODUCER NEEDLE STICKS AT START.
Part: ACTUATOR — FAILED (M/R)
ACTUATOR SHAFT LOOSE IN MOTOR HOUSING.
1997
Part: WINDSHIELD — MIS MFG (COCKPIT LT)
INBOARD SIDE OF WINDSHIELD TOO SHORT 3/4".
Part: PANEL — CORRODED (FUSELAGE)
PANEL CORRODED AND SEPARATED.
Part: LONGERON — MIS MFG (FUSELAGE)
PART IS NOT THE SAME CONTOUR AS ORIGINAL ANGLE 1/16" SMALLER THAN ORIGINAL CAUSING EDGE DISTANCE PROBLEMS AND TOTAL LENGTH OF PART IS 3/8" TOO SHORT.
Part: FUEL CELL — LEAKING (FUEL SYS)
FUEL CELL LEAKING.
Part: INDICATOR — READS HIGH (ENG TORQUE)
TORQUE METER INDICATES HIGH AT 80% TO 100%.
Part: FUEL CELL — SEEPAGE (FUEL SYS)
FUEL CELL SEEPAGE THROUGH FABRIC.
Part: FUEL CELL — SEEPAGE (FUEL SYS)
FUEL CELL SEEPAGE THROUGH FABRIC.
Part: FLEXURE — DETERIORATED (XMSN)
FLEXURE RUBBER DETERIORATED.
Part: FLEXURE — DETERIORATION (M/R)
FLEXURE RUBBER DETERIORATION.
Part: GYRO — DEFECTIVE (COCKPIT DG)
DIR GYRO PRECESSES AND GLASS IS CRACKED.
Part: TACH GEN — DEFECTIVE (ROTOR)
TACH GEN BAD STATOR.
1996
Part: TUBE ASSY — CRACKED (M/R CONTROL)
FOUR EACH CRACKS AT CLEVIS END OF TUBE APPROXIMATELY 1/2" TO 3/4" LONG. REPLACED WITH SERVICEABLE TUBE.
Part: TRANSCEIVER — DEFECTIVE (COCKPIT)
STANDBY LED DIGITS NOT ALL LIGHTING UP.
Part: BEARING — FAILED (XMSN)
BEARING BALLS AND RACER SPALLED CAUSING TRANSMISSION METAL IN OIL. REPLACED WITH SERVICEABLE BEARING.
Part: FRAME — CRACKED (TAILBOOM)
CRACKED IN UPPER L/H CORNER. REPLACED WITH SERVICEABLE FRAME.
1995
Part: TRANSCEIVER — DEFECTIVE (COCKPIT)
LED DISPLAY INOPERATIVE. REPLACED DS901. STILL HAD INTERMITTENT DISPLAY WHEN BOTTOM OF UNIT PRESSED ON. FOUND THAT MOVEMENT OF Q507 TRANSISTOR CAUSED DISPLAY TO FLICKER. RESOLDERED Q507 TRANSISTOR AND REPAIRED PROBLEM. UNIT BENCH CHECK GOOD.
Part: TRANSCEIVER — FAILED (COCKPIT)
INOPERATIVE. FOUND THAT UNIT WOULD NOT RECEIVE OR TRANSMIT. REPLACED CAVITY TUBE V101. REPAIRED PROBLEM. ADJUSTED FREQUENCY AND ALIGNED RECEIVER TO SPECS. CLEANED CONTACTS ON ALL WAFERS. BENCH CHECK GOOD.
Part: REGULATOR — MALFUNCTION (DC SYS)
REGULATOR CAUSING GEN. TO NOT COME ON LINE.
Part: BEARING — CRACKED (T/R)
BEARINGS CRACKED. ALSO REPLACED 2 EACH SLEEVES P/N 206-010-733-003. BEARINGS SCRAPPED LOCALLY. SEE MMIR'S # 4831 THROUGH # 4844 FOR ADDITIONAL BEARINGS.
Part: BEARING — CRACKED (T/R)
BEARINGS CRACKED. ALSO REPLACED 2 EACH SLEEVES P/N 206-010-733-003. BEARINGS SCRAPPED LOCALLY. SEE MMIR'S # 4831 THROUGH # 4844 FOR ADDITIONAL BEARINGS.