Textron 560XL
Service difficulty reports · 3,810
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 aircraft_model_key = '560XL' 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.
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 aircraft_model_key = '560XL' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR DXTA2014112105929Apu · smokeCABIN FILLED WITH SMOKE WHEN APU BLEED AIR TURNED ON. R & R THE APU IAW MM 49-10-00. OPS & LEAK CHECKED GOOD.SDR O2GA2014112450301Proximity Switch · faultyAT 16,800` CABIN DOOR ANNUNCIATOR & RED CABIN ALTITUDE WARNING ILLUMINATED. CABIN ALTITUDE CLIMBED TO 12,600’. FOLLOWED EMER CHECKLIST, DECLARED AN EMER TO FACILITATE DESCENT TO 10,000’. ACFT DIVERTED & LANDING WAS UNEVENTFUL. MX TROUBLE SHOT THE DISCREPANCSDR CA141202018Unknown · odor(CAN) ON CLIMB, THE PILOT NOTICED AN OIL ODOR. NORMAL CHECKS CARRIED OUT. DECISION WAS TAKEN TO CONTINUE FLIGHT. MECHANICS ARE TESTING TO IDENTIFY WHICH ENGINE EMITTED THE OIL ODOR.SDR O2GA2014112450302Lock Pin · frozenMAIN CABIN DOOR WOULD NOT OPEN UPON ARRIVAL. THE DOOR LOCK PINS WERE FROZEN DUE TO MOISTURE & COLD TEMPERATURE WHILE ENROUTE. DUE TO PAXS MEETING & SCHEDULE THE EMER EXIT DOOR WAS USED. PAXS WERE ASSISTED BY CREW. REMOVED STANDING WATER IN DOOR FRAME. ALLSDR CA141202012Engine · unknown(CAN) AFTER LEVELING OFF AT FL410, POWER WAS BEING REDUCED TO SET NORMAL CRUISE THRUST, A LOUD NOISE WAS HEARD FROM THE RT SIDE OF THE PLANE. THE PLANE SHOOK AND YAWED BRIEFLY TO THE RT. OCCURRENCE HAPPENED ONLY ONCE. FUEL FLOW AND ITT REMAINED STABLE. THESDR EBVR20141107001Fitting · crackedWE ARE FINDING MORE OF THESE PIVOT FITTING ASSEMBLY HAVING CRACKS PN 6631102-15 & T CLIP PN 6631202-7 HAVING LOOSE HARDWARE.SDR CA141202005Engine · malfunctioned(CAN) LEFT ENGINE ITT KEPT SPIKING DURING THE CLIMB. AT FIRST INDICATION IT CLIMBED TO 730 FOR 10 SECONDS. COULD NOT MAINTAIN CLIMB POWER WITHOUT EXCEEDING LIMITATIONS. ALL OTHER ENGINE INDICATIONS WERE NORMAL.SDR 9JLA2015012906973Torque Motor · failedDURING THE TAKEOFF ROLL THE NR 1 ENG COMPUTER, LEEC, WENT INTO MANUAL MODE REQUIRING THE CREW TO ABORT THE TAKEOFF. THE DISCREPANCY WITH THE LEEC WAS DEFERRED. TROUBLESHOOTING AFTER THE ACFT RETURNED TO HOME BASE IDENTIFIED THE NR 1 ENG TORQUE MOTOR PN 30J34SDR DXTA2014103005919Metering Valve · failedDURING LT BRAKE APPLICATION AT LOW SPEEDS, THE ENTIRE AIRPLANE SHUDDERED & HAD THREE PULSES CAN BE HEARD THROUGH THE ENTIRE CABIN. PULSING CAN BE FELT AND HEARD AND IS STRONGEST AT SLOW SPEEDS AND WHEN USING LEFT BRAKE ONLY. TAXIED ACFT AND DUPLICATED THE PROBSDR CA141103012Engine · power loss(CAN) DURING CLIMB AT 18K FEET, THE RIGHT HAND ENGINE HAD A POWER ROLLBACK. THE PILOT BROUGHT THE POWER BACK TO IDLE AND RESET THE EEC BREAKER AND FLIGHT RESUMED WITH NO MORE INCIDENTS. TROUBLESHOOTING ONGOING.SDR CA141103008Oil System · low pressure(CAN) AT APPROX. 1500 FT, THE PILOT GOT A LOW OIL PRESSURE ANNUNCIATOR AND VERIFIED INDICATED OIL PRESSURE DROPPED TO ZERO. THE CAPTAIN REDUCED POWER TO IDLE, ENGINE INDICATIONS WERE ALL NORMAL EXCEPT OIL PRESSURE. HE ADVANCED THE POWER ONE MORE TIME AND ALL ISDR DXTR2014102101Fitting · crackedHORIZONTAL STABILIZER FITTING ASSY CRACKED ABOVE CLIP ATTACH POINT.SDR CA141103006Oil System · low pressure(CAN) THE AIRCRAFT DEPARTED WITH ALL INDICATIONS NORMAL. THE FLIGHT CREW TOOK OFF, LEVELED AT 3000 FEET, THEN WAS CLEARED TO 13,000 FT. 4 MINUTES INTO THE FLIGHT PASSING 5000 FEET, CREW GOT AN RED OIL PRESSURE LIGHT, CHECKED THE OIL GAUGE WHICH WAS AT ZERO PSISDR DXTR2014102002Link Pin · galledWHILE ATTEMPTING TO DISASSEMBLE THE RT MLG TO REPLACE THE TRUNNION ASSY. THE PIVOT LINK PIN WAS BADLY GULLED FROM NO LUBRICATION. THE PIN HAD TO BE FORCIBLY DRIVEN OUT.SDR DXTR2014102001Lock Pin · galledWHILE ATTEMPTING TO R & R THE RT MLG ACTUATOR BECAUSE OF LEAKING FLUID, IT WAS DISCOVERED THAT THE SIDEBRACE ATTACH PIN AND THE LOCKING BOLT WERE SO BADLY GALLED AND FROZEN IN PLACE FROM LACK OF GREASE THEY HAD TO BE DRILLED & DRIVEN OFF TO FREE ACTUATOR END.SDR DXTA2014102005914Unknown · odorWITH APU RUNNING ON THE GROUND & WITH THE ENGINES OFF, HAD SMOKE IN THE AFT CABIN. COMPLETED PRELIMINARY INSPECTION OF APU & RELATED PLUMBING. RAN APU , CONTACT BLEED AIR SUPPLIED FOR 1.0 WITH NO INDICATION OF SMOKE IN THE AFT CABIN OR SMOKE ODOR IN ACFT. SDR DXTA2014101705912Unknown · smokeSMOKE WAS OBSERVED IN THE COCKPIT & CABIN. ODOR WAS ALSO OBSERVED.SDR CWQR20141015008Hinge · corrodedDURING A SCHEDULED INSPECTION WE FOUND THE LOWER AFT MAIN CABIN DOOR HINGE HALF CORRODED. THE HINGE HALF MATERIAL HAD SWELLED FROM INTERGRANULAR CORROSION FROM THE EDGE OF THE HINGE & TRAVELED INTO TWO FASTENER HOLES. REMOVED HINGE & FOUND NO DAMAGE OR CORROSDR CA141025004Oil System · low pressure(CAN) DURING CLIMB OUT THE LOW OIL PRESSURE ANNUNCIATED. THE PILOT NOTICED THE OIL PRESSURE INDICATION WAS HEADING TO "0". THE ENGINE WAS SHUT DOWN AND SECURED ENGINE. AIRCRAFT CONTINUED TO HOME BASE WHERE AN UNEVENTFUL SINGLE ENGINE LANDING TOOK PLACE. GROUNDSDR DXTA2014101305910Wheel · failedDURING ROTATION, ACFT PITCHED UP VIOLENTLY REQUIRING SIGNIFICANT FWD PRESSURE ON THE YOKE TO AVOID OVER ROTATION. REMOVED ELEVATOR TRIM WHEEL & FOUND TRIM INDICATOR TRACK CRACKED & 3/4 INCH PIECE MISSING, TRIM IS OUT OF ADJUSTMENT. FURTHER INSPECTION REVEALSDR DXTA2014101005909Pump · failedWHEN ACFT WAS ROLLING TO A STOP, THE BRAKES FAILED. THE EMERGENCY BRAKE WAS USED TO BRING THE ACFT TO A STOP. REMOVED AND REPLACED THE PUMP ASSEMBLY. OPS CHECKED GOOD. WORK ACCOMPLISHED IAW MM 32-42-06.SDR DXTA2014100905907Control Unit · failedAFTER TAKEOFF, SELECTED GEAR UP & IT DID NOT RETRACT. R & R THE LANDING GEAR HANDLE CONTROL UNIT IAW MM 32-30-01. OPS CHECKED GOOD.SDR CA141024015Engine · power loss(CAN) TAKEOFF ABORTED DURING INITIAL ROLL, DUE TO INABILITY TO ACHIEVE TAKEOFF POWER AND N1 FLUCTUATION.SDR DXTA2014100605905Engine · malfunctionedRIGHT ENGINE OIL PRESSURE WENT TO 17 PSI INFLIGHT. SHUTDOWN ENGINE. R & R THE ENGINE & OPS & LEAK CHECKED GOOD. PERFORMED A 5 POINT PERFORMANCE CHECK.SDR DXTA2014100605904Display · failedNR 1 DISPLAY UNIT INOPERATIVE, NOTICED SMOKE AS WELL. REMOVED AND REPLACED THE NR 1 DISPLAY UNIT, OPS CHECKED GOOD. NO DEFECTS NOTED, WORK COMPLETED IAW MM 31-50-01.SDR CA141024003Engine · flamed out(CAN) DURING TAXI, THE PILOT PULLED THE POWER BACK ONCE OUT OF THE BLOCKS AND THE ENGINE SPOOLED DOWN AND FLAMED OUT. CREW CALLED MAINTENANCE AND THEY RESTARTED THE ENGINE NORMALLY. PILOT ADDED POWER TO ENGINE AND PULLED POWER BACK AND THE ENGINE FLAMED OUT SDR CA141010011Oil System · leaking(CAN) CREW EXPERIENCED AN OIL PRESSURE LOSS ON THE LT ENGINE DURING CLIMB OUT. THE CREW FOLLOWED THE EMERGENCY PROCEDURES AND SHUTDOWN ENGINE, TURNED AROUND AND LANDED BACK AT POINT OF DEPARTURE. DURING INSPECTION, AN OIL LEAK WAS FOUND FROM THE BOTTOM OF THSDR DXTA2014092905899Coalescer Bag · odorENVIRONMENTAL SYS ODOR, NO VISIBLE SMOKE, WHILE DESCENDING A STRONG SYNTHETIC ODOR LIKE HOT GLUE OR EPOXY WAS PRESENT IN THE COCKPIT. OZONE CONVERTERS & WATER SEPARATOR REMOVED. CLEANED & REINSTALLED IAW AMM 21-71-00 & 12-19-02. ENVIRONMENTAL CONTROL SYS OSDR 2014FA0000556Tube · delaminatedINSPECTING HUMIDITY REGULATOR FOUND PARTICLES OF FLAKED OFF MATERIAL TRAPPED IN THE SOCK. INSPECTED UPSTREAM AND FOUND THAT THE COATING IN THE TUBE WAS FLAKING OFF.SDR DXTA2014092505893Brake Sys · contaminatedDURING TAXI THE ACFT PULLS HARD TO THE LT WHEN EVEN BRAKE PRESS APPLIED FROM THE RT SEAT. OPERATIONS CHECKED BRAKES & LT BRAKE FEELS SPONGY. HOOKED BRAKE BLEEDING HOSE & COMPLIED WITH BRAKE BLEEDING PROCEDURE IAW MM CH 32-44-00. REMOVED A LOT OF AIR OUT OFSDR CWQR20140924006Acm · failedAIRCRAFT WAS POSITIONED ON THE RAMP WITH GROUND POWER CART ON, ACFT POWER ON AND THE FREON AIR-CONDITIONING SYSTEM IN OPERATION. THE CREW NOTICED SMOKE COMING FROM THE TAIL AREA OF THE ACFT AND ALERTED LINE PERSONNEL. THE LINE PERSONNEL OPENED THE AFT BAGGAGSDR CWQA20140923001Outflow Valve · malfunctionedDURING CRUISE CREW EXPERIENCED CABIN PRESSURIZATION FLUCTUATIONS & THEN LOSS OF CABIN PRESS CONTROL. CHECK LIST FOLLOWED, EMER DECLARED, OXYGEN MASKS DEPLOYED, EMER DECENT & UNSCHEDULED LANDING PERFORMED WITHOUT INCIDENT. PRIMARY OUTFLOW VLV REPLACED PN 9912SDR 2014FA0000545Control Cable · brokenDURING PRE-FLIGHT INSPECTION AFTER MAINTENANCE FOUND RUDDER FLIGHT CONTROL CABLE LOOSE. OPEN AFT BAGGAGE OVERHEAD ACCESS PANELS AND FOUND UPPER RUDDER CABLE BROKEN AT FORWARD PULLEY. DURING INVESTIGATION FOUND NO DAMAGE TO SURROUNDING AREA.SDR EBVR20140923002Fitting · crackedFOUND 2 HORIZONTAL STAB PIVOT FITTING ASSEMBLY CRACKED PN 6631102-15 DURING OUR INSPECTION. MECHANICS NEED TO PAY CLOSE ATTENTION TO THIS AREA WHILE DOING INSPECTIONS ON THE HORIZONTAL & VERTICAL TAIL AREA.SDR EBVR20140923001Fitting · crackedFOUND 2 HORIZONTAL STAB PIVOT BOLT FITTING ASSEMBLY PN 6631102-15 CRACKED DURING OUR INSPECTIONS. MECHANICS NEED TO PAY CLOSE ATTENTION TO THIS AREA DURING INSPECTIONS INVOLVING THE HORIZONTAL & VERTICAL TAIL STRUCTURES.SDR CA141008010Eec · malfunctioned(CAN) CUSTOMER REPORTED AN ENGINE ROLLED BACK IN FLIGHT. IT WAS RECOMMENDED TO REPLACE THE LATEST ELECTRONIC ENGINE CONTROL IAW SB30478 AND LATEST FMU IAW SB30370. THE CUSTOMER HAS ORDERED PARTS AND THEY HAVE ARRIVED. WAITING FURTHER INFORMATION FROM CUSTOMESDR CA141008007Engine · malfunctioned(CAN) DURING REPOSITIONING FLIGHT TO ACCOMPLISH HIGH ITT FAULT ISOLATION CREW REPORTED OIL ODOR IN CABIN AT 40000 FT. CREW ISOLATED SOURCE TO RT ENGINE USING BLEED CONTROLS. SUCCESSFUL LANDING WITH 2 CREW ONLY ON BOARD. MAINTENANCE HAVE PERFORMED CHECKS AND SDR DXTA2014091905887Starter Gen · malfunctionedWHILE LOADING PAX AND BAGS WE NOTICED AN UNUSUAL NOISE COMING FROM THE APU AREA. IT SOUNDED LIKE A VERY LOUD VACUUM CLEANER CYCLING OFF AND ON EVERY 5 TO 15 SECONDS. AFTER WE HEARD THE NOISE - THE APU GENERATOR FELL OFF LINE. WE TRIED TO RESET THE GENERATORSDR DXTA2014091505882Metering Valve · unserviceableDURING TAXI AT SLOW SPEED RT BRAKE GRABS & PULLS ACFT TO THE RT. ALSO MAKES AN AUDIBLE NOISE. REPLACED BRAKE METERING VALVE WITH A UNIT OVH'D. OPERATIONAL CHECK AND LEAK CHECK SATISFACTORY. ALL WORK IAW CE-560XL MM CH 32-44-20.SDR DXTA2014091205880Brake Sys · contaminatedLEFT MAIN BRAKE IS GRABBING WITH MODERATE BRAKE APPLICATIONS. MOST PRONOUNCED AT HIGHER SPEEDS INCLUDING LANDING ROLLOUT. A BINDING NOISE CAN BE HEARD WHEN APPLYING HARDER LEFT BRAKE APPLICATIONS. BLED LEFT AND RIGHT BRAKES AND PERFORMED OPERATIONAL CHECK OSDR CA141006009Engine · overtemp(CAN) DURING TAKEOFF ROLL, THE PILOT ELECTED TO ABORT TAKEOFF DUE TO HIGH ITT. RETURNED TO RAMP UNEVENTFULLY. TROUBLESHOOTING IS ONGOING.SDR DXTA2014090505874Motor · unserviceableON TAKEOFF AFTER RELEASE OF BRAKES WE RECEIVED LO BRAKE PRESS. ALSO ANTI-SKID INOPERATIVE LIGHTS, FOLLOWED BY MASTER CAUTION LIGHT. ABORTED TAKEOFF AT APPROX 20K. LOST MAIN HYD BRAKES, USED AIR BRAKES & THRUST REVERSE TO STOP. NOTICED POWER BRAKES CB POPPSDR CWQR20140905005Housing · brokenINSTALLED REPAIRED SERVICEABLE ENG ON THE NR 2 POSITION ON ACFT. DURING THE ENG LEAK & RUN UP CHECKS WE DISCOVERED THAT THE T1 PROBE HOUSING THAT IS IN THE INLET AIR STREAM HAS BROKEN OFF & DAMAGED THE FAN, FAN LINER & BYPASS DUCT. REMOVED ENG & RETURNED FORSDR DXTA2014090305871Apu · defectiveGRAY SMOKE FILLED COCKPIT AND CABIN ON GROUND. APU WAS RUNNING WITH ACM. IMMEDIATELY SHUT DOWN APU AND ALL ELECTRICAL POWER. ENGINES WERE NOT RUNNING. SMOKE ODOR UNIDENTIFIED. COMPLIED WITH INSPECTION OF THE APU CONTAINMENT BOX AND CLEANED BLEED VALVE DUCSDR CA140903010Damper · misoverhauled(CAN) THE DAMPER WAS REPAIRED AT A VENDOR IN 2011, AND WAS REASSEMBLED INCORRECTLY. IT WAS THEN INSTALLED BACKWARDS TO MAKE UP FOR THE IMPROPER ASSEMBLY. IN 2013 VENDOR DID A PHASE 2 AND PHASE B ON THE AIRCRAFT AND DID NOT NOTE ANY DEFECTS. WE WERE CONDUCTING SDR CA140908005Warning Message · illuminated(CAN) THE PILOT REPORTED A LOW OIL PRESSURE WARNING FOLLOWED BY A COMMANDED SHUTDOWN AND UNEVENTFUL SINGLE ENGINE LANDING. TROUBLESHOOTING ON-GOING.SDR Z5FA2014082357101Unknown · malfunctionedON A POSITION FLIGHT CLIMBING OUT OF 18000, APU WAS SHUTDOWN. HOWEVER, AS THE RPM REACHED 20 % ON THE SHUTDOWN PROCESS, APU STARTED AN UNCOMMANDED RESTART INFLIGHT. AFTER THE COMPLETION OF THE START SEQUENCE, APU WAS SHUTDOWN FOR THE SECOND TIME. AGAIN THE SDR DXTA2014082705868Spar Cap · corrodedLEFT & RIGHT WING UPPER SPAR CAP TOP SURFACE HAS CORROSION. ACCOMPLISHED REPAIR TO THE LT AND RT WING UPPER SPAR CAP TOP SURFACE CORROSION AREAS IAW S-560XL-5548/02PRD.SDR DXTA2014082205864Unknown · smokeAFTER STARTING APU & TURNING ON BLEED AIR, WHITE SMOKE STARTED TO FILL THE COCKPIT & CABIN. APU DID NOT SHUT ITSELF DOWN, NOR DID ANY VISUAL OR AURAL FIRE WARNINGS ILLUMINATE OR SOUND. SHUTDOWN APU & CALLED AIRPORT FIRE DEPARTMENT. THEY DID NOT FIND ANY INDSDR DXTA2014082105862Strut · faultyDURING FLIGHT GEAR UNSAFE RED LIGHT ILLUMINATED, NO GREEN LIGHTS ILLUMINATED. COMPLIED WITH APPLICABLE CHECKLIST. TROUBLE SHOT NLG RETRACTION & EXTENSION COMPONENTS. FOUND NLG STRUT EXTENSION OUT OF LIMITS IAW CMM 32-20-01. DISASSEMBLED NLG LOWER STRUT AS
Back to Textron 560XL