N2245Y
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
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, 1995-01-09 – 2002-05-28.
Part: SKID — CORRODED (MLG)
SKID TUBE CORRODED BEYOND LIMITS. SCRAPPED.
Earlier reports · 1995–1999 · 32 reports
1999
Part: STARTER — FAILED (STARTER/GEN)
STARTER/GENERATOR BURNED UP. INSPECTED BY ACCESSORY SHOP AND FOUND COMMUTATOR AND BRUSHES BURNED AND PITTED.
Part: INDICATOR — LEAKS (ENGINE OIL)
LEAKS INTERMITTENTLY.
Part: INDICATOR — READS HIGH (TOT)
TOT INDICATOR READS 10 DEGREES HIGH.
1998
Part: ANGLE — MISMANUFACTURED (FUSELAGE)
ANGLE MISMANUFACTURED. NO EDGE DISTANCE TO INSTALL NUT PLATES ON ANGLE. THE ANGLE REMOVED IS .9375 INCH WIDE, NEW ANGLE IS .8125 INCH WIDE.
Part: TRANSCEIVER — BROKEN (COCKPIT)
FRONT PLATE BROKEN ON RADAR ALTIMETER.
Part: LONGERON — MISMANUFACTURED (FUSELAGE)
WHEN LONGERON IS INSTALLED, NO EDGE DISTANCE ON FASTENER HOLES--LONGERON IS TOO WIDE.
Part: SKIN — DENTED (HORIZ STAB)
EXCESSIVE DENTS ON OUTER STAB SKIN.
Part: SKID TUBE — CRACKED (MLG)
SKID TUBE ASSY HAS CRACKS AT SEVERAL INSERTS AS MARKED.
1997
Part: INDICATOR — FAILED (ENG OIL)
INDICATOR WAS REMOVED FROM BOWL AND CLEANED. INSTALLED INDICATOR BACK ON BOWL, TESTED AND INDICATOR STILL DID NOT WORK. SCRAPPED INDICATOR AND REPLACED WITH SERVICEABLE PART.
Part: PUMP — SHAFT WORN (FUEL PUMP)
FOUND DRIVE SHAFT AND GEAR SPLINE WEAR.
Part: INDICATOR — DEFECTIVE (ENG OIL)
WHEN PRESSURE IS APPLIED FLUID LEAKS INTO FACE OF GLASS.
Part: RESTRAINT — BEARING WORN (XMSN)
XMSN RESTRAINT BEARINGS WORN AND UNSTAKED.
Part: FIN ASSY — CORROSION (SKIN)
FIN ASSY CORROSION THROUGH EXISTING METAL. SKIN BEYOND LIMITS.
Part: GEARSHAFT — WORN (SPUR ADAPTER)
ENGINE REMOVED DUE TO FLUCTUATING OIL PRESSURE. COMPRESSOR DISASSEMBLED DUE TO LOW POWER ON TEST CELL. UPON INPSECTION OF COMPRESSOR PARTS NOTED: STEP WEAR BEYOND SERVICEABLE LIMITS ON SPUR GEARSHAFT SPLINES.
Part: ANTENNA — DEFECTIVE (RADAR ALT)
RADIO ALT. NEEDLE FLUCTUATION.
Part: COLLECTOR STRUT — CRACKED (TURB EXHAUST)
ENGINE REMOVED DUE TO FLUCTUATING OIL PRESSURE. TURBINE DISASSEMBLED DUE TO LOW POWER ON TEST CELL. DISASSEMBLY INSPECTION REVEALED: CRACKED BEYOND SERVICEABLE LIMITS ON EXHAUST COLLECTOR STRUT & EXCESSIVE RUNOUT ON CARBON SEAL BORE .006 (SPECS.0015) INSTALLED A DALLAS AIRMOTIVE OVERHAULED EXHAUST COLLECTOR.
1996
Part: REAR SUPPORT — MIS MFG (COMPRESSOR)
RECEIVING INSPECTION REVEALED: IMPROPERLY MACHINED REAR SUPPORT RETAINING RING GROOVE. REPLACED DISCREPANT PART.
Part: LINK ASSY — WORN EXCESS (XMSN MOUNT)
BUSHING IS WORN. SENT TO LORD MANUFACTURING FOR EXCHANGE.
Part: BEARING — CRACKED (T/R BLADE)
RETIRED BLADE. REMOVED BEARINGS TO CHECK FOR SERVICEABILITY. FOUND BEARING CRACKED. SCRAPPED LOCALLY.
Part: TRANSCEIVER — DEFECTIVE (COCKPIT ATC)
UNIT NOT REPORTING ALTITUDE. VERIFIED UNIT TO HAVE VERY WEAK POWER OUT. TRIED ADJUSTING POWER TO SPECS. NO HELP. REPLACED CAVITY OSCILLATOR V101. REPAIRED. ADJUSTED FREQUENCY. BENCH CHECK GOOD.
1995
Part: EXHAUST ASSY — CRACKED (ENG)
EXHAUST ASSY IS CRACKED.
Part: TRANSCEIVER — DEFECTIVE (COCKPIT ATC)
BENCH CHECK REQUIRED. INSPECTED AND TESTED. REPLACED CAVITY TUBE V101 DUE TO LOW POWER OUT. REPAIRED. REPLACED PHOTOCELL V301 DUE TO WEAK REPLY LIGHT. REPAIRED. ALIGNED RECEIVER TO SPECS. ADJUSTED FREQUENCY. BENCH CHECK GOOD.
Part: BEARING — DEFECTIVE (T/R)
INBOARD BEARING ON BLADE S/N CS6823 WORN THROUGH ANODIZED SURFACE. INBOARD BEARING ON BLADE S/N CS6821 CRACKED. REPLACED BEARINGS AND SLEEVES. ROLLED STAKED AS REQUIRED.
Part: INDICATOR — PLUG LOOSE (COCKPIT ATTITUDE)
CANNON PLUG CONNECTOR LOOSE IN CASE. REPLACED WITH SERVICEABLE ATTITUDE INDICATOR.
Part: SEAL — FAILED (ENG GR BOX)
TRANSFERRING OIL FROM ENGINE TO TRANSMISSION. REPLACED FWD AND AFT DOUBLE LIP SEALS IN ENGINE GEARBOX.
Part: LONGERON — CRACKED (TAILBOOM)
LOOSE FITTING CAUSED TAILBOOM RING P/N 206-032-308-103S AND LONGERON P/N 206-031-314-037S TO CRACK. SEE MMIR # 5232 FOR FRAME INFORMATION.
Part: FRAME — CRACKED (TAILBOOM)
LOOSE FITTING CAUSED TAILBOOM RING P/N 206-032-308-103S AND LONGERON P/N 206-031-314-037S TO CRACK. SEE MMIR # 5233 FOR LONGERON INFORMATION.
Part: SUPPORT — REQ REPLACEMENT (M/R)
COMPLY WITH ASB 206L-93-89 REV. B (REPLACEMENT OF -109 SUPPORT WITH -113 SUPPORT)
Part: SHAFT — PITTED (FREEWHEEL)
PITTING ON CLUTCH RIDE.
Part: PUMP — LEAKING (TRANSMISSION)
FRONT SEAL ON PUMP LEAKING OIL. REPLACED WITH SERVICEABLE PUMP ASSEMBLY.
Part: EXHAUST ASSY — CRACKED (ENGINE)
ON DAILY INSPECTION, FOUND EXHAUST STACK CRACKED IN THE MIDDLE OF THE BACK SIDE. REPLACED WITH SERVICEABLE EXHAUST STACK.
Part: BEARING — CRACKED (T/R)
PAINT PEELING OFF BLADES. BLADE S/N CS6278 & CS6296, T.T. 906:40. INBOARD BEARINGS CRACKED. COMPLY WITH 206L-94-TBD. SCRAPPED LOCALLY.