N5748Q
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.
21 reports on file, 1995-03-01 – 1998-10-07.
Part: SUPPORT — MISMANUFACTURED (ENGINE)
ENGINE REMOVED DUE TO CRACKED SCROLL. FRONT SUPPORT WAS TRANSFERRED TO COMPRESSOR S/N CAC70646. ENGINE FAILED CELL TEST DUE TO HIGH COMPRESSOR VIBS. REPLACED FRONT SUPPORT. CURED PROBLEM. TRANSFERRED FRONT SUPPORT TO COMPRESSOR S/N CAC70016. ENGINE FAILED DUE TO HIGH COMPRESSOR VIBS. REPLACED FRONT SUPPORT.
Earlier reports · 1995–1997 · 20 reports
1997
Part: CARTRIDGE — DEFECTIVE (FUEL SYS)
FUEL PRESSURE READS LOW WHEN GENERATOR IS OFF LINE.
Part: ACTUATOR — INOPERATIVE (M/R CONTROL)
ACTUATOR INOPERATIVE.
Part: GYRO — PRECESSES (COCKPIT DG)
IN SLAVE MODE, DG PRECESSES AND SLAVE METER WILL NOT SWING PLUS OR MINUS 5 VOLTS.
Part: GYRO — PRECESSES (COCKPIT DG)
DIR GYRO PRECESSES EXCESSIVELY.
Part: AIRSPEED IND — FAILED (COCKPIT)
AIRSPEED NEEDLE STUCK AT 140 MPH.
1996
Part: BATTERY — DEFECTIVE (DC SYS)
BATTERY INSPECTED BY ACCESSORY SHOP AND FOUND BATTERY WOULD NOT PASS CAPACITY TEST. BATTERY PUT INTO SERVICE 2-27-95.
Part: HANGER ASSY — OUT OF LIMITS (T/R DRIVE)
REMOVED PER ASB 206L-95-101 REV. A. (SPRING I.D. OUT OF LIMITS)
Part: SPLINE ADAPTER — WORN (GEARSHAFT)
ENGINE REMOVED DUE TO TURBINE OVERHAUL AND COMPRESSOR N1 SHAFTING INSPECTION. UPON INSPECTION OF COMPRESSOR PARTS NOTED THE FOLLOWING: STEP WEAR BEYOND SERVICEABLE LIMITS ON SPUR ADAPTER GEARSHAFT AFT SPLINES AND STEP WEAR BEYOND SERVICEABLE LIMITSON SPLINE ADAPTER INTERNAL SPLINES. REPLACED DISCREPANT PART.
Part: LINK ASSY — DEFECTIVE (XMSN MOUNT)
BEARING IS BAD AND RUBBER IS MISSING.
Part: LINK ASSY — DETERIORATED (M/R XMSN)
LINK ASSY DETERIORATED RUBBER.
1995
Part: STIFFENER — CRACKED (FUSELAGE)
CRACKED COMPLETELY IN TWO 4 3/8" FROM TOP OF STIFFENER. REPLACED WITH SERVICEABLE PART.
Part: ALTIMETER — READS HIGH (COCKPIT)
NEEDLE INDICATES 40 FEET HIGH AT ZERO.
Part: BEARING — CRACKED (T/R)
OUTBOARD BEARINGS CRACKED. REMOVED FROM T/R HUB S/N A4984, T.T. 3723:15. ALSO REMOVED 2 EACH SLEEVES P/N 206-010-733-003. PARTS SCRAPPED LOCALLY.
Part: BEARING — CRACKED (T/R)
INBOARD BEARING CRACKED. REMOVED FROM T/R HUB S/N A4984, T.T. 3723:15. ALSO REMOVED 1 EACH SLEEVES P/N 206-010-733-003. PARTS SCRAPPED LOCALLY.
Part: BEARING — CRACKED (T/R)
INBOARD BEARING CRACKED. REMOVED FROM T/R HUB S/N A4984, T.T. 3723:15. ALSO REMOVED 1 EACH SLEEVES P/N 206-010-733-003. PARTS SCRAPPED LOCALLY.
Part: VALVE — LEAKING (FUEL SYS)
FUEL VALVE LEAKING FUEL AT ROTATING SHAFT OF OPEN AND CLOSE SECTION OF VALVE. REPLACED WITH SERVICEABLE VALVE.
Part: TUBE ASSY — LEAK (XMSN OIL)
TUBE ASSEMBLY DEVELOPED A PIN HOLE LEAK AROUND "B" NUT COLLAR. PIN HOLE APEARS TO BE CAUSED BY CORROSION. "B" NUT FERRULE ON TUBE ASSEMBLY WAS STAINLESS STEEL AS THIS IS AN ALUMINUM LINE.
Part: TRANSCEIVER — DEFECTIVE (COCKPIT ATC)
KNOB WILL NOT TURN TO TEST. VERIFIED. REPLACED FACEPLATE ASSEMBLY DUE TO KNOB BROKEN. INSTALLED HEATSINK DUE TO SERVICE BULLETIN KT76A-6. REPLACED CAVITY OSCILLATOR V101 DUE TO WEAK POWER. REPLACED V301 PHOTOCELL DUE TO BEING WEAK. REPLACED DETERIORATED R477 RESISTOR.REPAIRED.
Part: PUMP — LEAKING (M/R XMSN)
OIL LEAKING OUT OF SPLINE SHAFT. REPLACED SHAFT SEAL .
Part: INDICATOR — LIGHTS INOP (COCKPIT TOT)
INTERNAL LIGHTS INOPERATIVE.