Allison 501-D13H

Service difficulty reports · 23

Newest first. General aviation reporting is voluntary.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE engine_model_key = '501D13H'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR CA150825009Fuel Control · failed(CAN) NR 1 ENGINE SPOOLED DOWN WHILE LOADING RETARDANT. ENGINE WOULD NOT RESTART. FCU HAD FAILED.Aug 21, 2015 · Cvac 340CVAC · Fuel Control/Turbine EnginesSDR CA150727025Skin · cracked(CAN) RT WING SKIN CRACK DETECTED DURING MMSR179-057-011-012, EXTERNAL HFEC.Jul 24, 2015 · Cvac 340CVAC · Wing, Plate/SkinSDR CA140812005Compressor · malfunctioned(CAN) PILOT HEARD LOUD BANGS, TWO OF THEM. LOSS OF HORSEPOWER WITH RISE IN TIT, PILOT E-HANDLED ENGINE WITH NO FURTHER ISSUES. PILOT REPORTED TIT OVER 1000C WITH RED WARNING LIGHT ON. SUSPECT COMPRESSOR BEARING FALURE - METAL FOUND EJECTING FROM FORWARD TURBINAug 5, 2014 · Cvac 340CVAC · Turbine Engine Compressor SectionSDR CA140620013Warning Light · false activation(CAN) ALTERNATOR WAS DISPLAYING VOLTAGE AND PROVIDING POWER TO BUSS, WITH INOPERATIVE LIGHT ILLUMINATED.Jun 18, 2014 · Cvac 340CVAC · AC Generator-AlternatorSDR CA130823012Computer · failed(CAN) AOA SYSTEM FAIL LIGHT ILLUMINATED IN FLIGHT. AOA COMPUTER FOUND TO BE FAILED.Aug 21, 2013 · Cvac 340CVAC · Stall Warning SystemSDR CA120822009Hinge · broken(CAN) ENGINE NR 1 REPORTED TO HAVE LOW HP. DAMAGE TO THE COMPRESSOR WAS FOUND TO BE THE CAUSE. A HINGE ACCESS PANEL ABOVE THE INTAKE DUCT BROKE OFF AND THE HINGE PIN APPEARS TO HAVE GONE THROUGH THE COMPRESSOR.Aug 16, 2012 · Cvac 340CVAC · DoorsSDR CA120720008Switch · binding(CAN) PILOT DISCOVERED LT FEATHER BUTTON SUCKED IN WHEN BATTERY MASTER TURNED ON. FOUND ON DI BEFORE DISPATCH. WE FOUND THE LT E-HANDLE SWITCH BLOCK PLUNGER JAMMED IN THE DRPRESSED POSITION. THE SPRING THAT NORMALLY PUSHES IT BACK HAD FALLEN OUT DUE TO THE RJul 17, 2012 · Cvac 340CVAC · Propeller Feathering/ReversingSDR CA120626008Relief Valve · leaking(CAN) HYDRAULIC FLUID LEAKING FROM NLG RELIEF VALVE.Jun 24, 2012 · Cvac 340CVAC · Hydraulic System, MainSDR CA090316003Volt Regulator · unserviceable(CAN) SMELL OF SMOKE WAS PRESENT IN THE COCKPIT. ALL POWER WAS SHUTOFF IN ACFT. ACFT LANDED WITHOUT 0 INCIDENT. THE AC GENERATOR VOLTAGE REGULATOR WAS FOUND DEFECTIVE. REGULATOR REPLACED AND GROUND CHECKED SERVICEABLE.Mar 11, 2009 · Cvac 340CVAC · AC RegulatorSDR CA080702013Valve · failed(CAN) NR 2 PROPELLER WOULD NOT GO INTO BETA OR REVERSE ON LANDING. PROPELLER GOVERNOR AND PITCH LOCK VALVE REPLACED AND PROP FUNCTION CHECKED SERVICEABLE ON GROUND RUN.Jun 30, 2008 · Cvac · Propeller GovernorSDR CA070709001Shaft · cracked(CAN) THE ROLL FORCE MODIFICATION WAS BEING INSTALLED IN THE AIRCRAFT IAW STC SA05-49. UPON TORQUING THE PILOT`S YOKE ASSEMBLY SHAFT IAW THE INSTRUCTIONS CONTAINED IN DOCUMENT K130-102-001-012, THE FLANGE ON THE SHAFT P/N 240-3140402-1 CRACKED. THE REMAININJul 6, 2007 · Cvac 30 · Flight Control SystemSDR CA050824020Wire · shorted(CAN) DURING CLIMBOUT, NR 2 ENGINE ZONE 1 FIRE LIGHT ILLUMINATED AND BELL SOUNDED. THE ENGINE WAS E-HANDLED, NO OTHER INDICATION OF FIRE WAS EVIDENT. THE AIRCRAFT LANDED SAFELY. DURING INVESTIGATION BY MAINTENANCE STAFF THE FIRE ELEMENT P/N 35608-0-765 WAS INDAug 21, 2005 · Cvac 340CVAC · Fire Protection System WiringSDR CA040209009Wire Harness · chafed(CAN) DURING WINTER MAINTENANCE INSPECTION, WIRES WERE FOUND RUBBING AGAINST EACH OTHER AT A FUEL QUANTITY TRANSMITTER PROBE IN THE LT WING AT APPRX WS 253.0. ONE WIRE HAD CHAFED ENOUGH TO EXPOSED THE BARE WIRE. ALL OTHER AREAS IN BOTH WINGS WERE INSPECTED Feb 9, 2004 · Cvac 340CVAC · Engine Fuel System WiringSDR ERA2001F00000Fuel Control · malfunctionedLEFT ENGINE SHUTDOWN IN CRUISE DUE TO POWER DROPPING OFF, POWER LEVER ADVANCE HAD NO EFFECT. MADE UNEVENTFUL LANDING ANC. REPLACED NR 1 ENGINE FUEL CONTROL UNIT. GROUND OPERATIONAL CHECK GOOD. (M)May 21, 2001 · N569JA · Cvac 34031 · Fuel Control/Turbine EnginesSDR 99ZZZX2385Bearing · crackedBEARING DEFECTS ON TORQUE SHAFT DETECTED DURING MAGNETIC INSPECTION ON P. O. NR 26366 FROM PACIFIC SKY SUPPLY.Apr 9, 1999 · Turbine Engine Reduction GearSDR 98ZZZX2976Fcu · failedIN CRUISE AT 18,000 FEET, LEFT ENGINE GRADUALLY LOST POWER. HP DROPPED FROM 2,000 TO ZERO, TIT FROM 847 TO 450, FF FROM 1,110 TO 600. TRIED TD NULL OFF, POWER LOSS GOT WORSE. TRIED ENGINE HEAT, NO EFFECT. SHUT ENGINE DOWN. DISCONNETED EDC PER CHECKLIST. Jul 20, 1998 · N565EA · Cvac 440 · Fuel Control/Turbine EnginesSDR ERA96001Cone Assy · missingREAR TURBINE SCAVENGE INSULATOR CONE MISSING FROM NR 2 ENGINE. INSPECTED TURBINE AND TAILPIPE FOR DAMAGE AND REPLACED THE INSULATOR CONE.Jul 1, 1996 · N566EA · Cvac 440 · Turbine SectionSDR ERA00017Td Syst · malfunctionedON TAKEOFF, NR 1 ENGINE WOULD NOT MAKE POWER. CREW ABORTED TAKEOFF AND RETURNED TO GATE. TD SYSTEM HAD BEEN PREVIOUSLY DEFERRED, HOWEVER SYSTEM WAS TURNED ON. DEACTIVATED TD SYSTEM, GROUND CHECKED GOOD.Oct 24, 1995 · N566EA · Cvac 440 · Fuel Controlling SystemSDR 95ZZZX4503Fuel Cntrl Unit · failedDEN/BIL - FLT 8072 - THE LT ENGINE WAS SHUT DOWN DUE TO RPM FLUCTUATION FROM 13,000 RPM TO 15,000 RPM. AIRCRAFT RETURNED TO DEN. THE LT FUEL CONTROL UNIT WAS REPLACED. SUBSEQUENT GROUND RUNS AND TEST FLIGHT WERE SATISFACTORY.Jul 22, 1995 · N73301 · Cvac 34030 · Fuel Control/Turbine EnginesSDR ERA00006Switch Bracket · looseLEFT GEAR DOWN LIGHT WOULD NOT ILLUMINATE. RETURNED TO ANC AND MADE UNEVENTFUL LANDING. TIGHTENED AND RERIGGED LOOSE LT MLG DOWNLOCK SWITCH BRACKET IAW CV580 M/M 32-61-31 PG 501 AND 502. RETRACT TEST SUCCESSFUL.May 24, 1995 · N569JA · Cvac 34031 · Landing Gear Position and WarningSDR ERA00002Uplock Lever · crackedNOSE LANDING GEAR WOULD NOT RETRACT. FOUND LEVER P/N 240-8557101-6 CRACKED. THIS CRACKED LEVER WOULD NOT ALLOW THE NLG UPLOCK TO ACTUATE.Feb 16, 1995 · N569JA · Cvac 34031 · Landing Gear Retraction/Extension SystemSDR ERA00003Uplock Lever · crackedGEAR UNLOCK LIGHT WOULD NOT GO OUT AFTER DEPARTURE. FOUND LEVER P/N 240-8557101-6 CRACKED. THIS CRACKED LEVER WOULD NOT ALLOW THE NLG UPLOCK TO ACTUATE. RE-RIGGED NOSE LANDING GEAR AND PERFORMED RETRACT TEST.Feb 16, 1995 · N569JA · Cvac 34031 · Landing Gear Retraction/Extension SystemSDR ERA00001Battery Pack · dischargedINTERIOR EMERGENCY EXIT LIGHT ON RT SIDE ROW 3 INOP. REPLACED BATTERY PACK.Jan 25, 1995 · N569JA · Cvac 34031 · Emergency Lighting
Back to Allison 501-D13H