Textron 560XL
Service difficulty reports · 3,809
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 DXTA2022052762830Door · lack of lubeMAIN DOOR: UNABLE TO FULLY ENGAGE THE LATCH TO LOCK THE MAIN CABIN DOOR FROM EITHER THE INSIDE OR THE OUTSIDE. REMOVED MED STEPS AND CLEANED AND LUBED ALL MOVING COMPENANTS AFTER WORKING LUBE IN THE LOCK LOSSENED UP AND IS MUCH EASIER TO LOCK. RE -INSTALLEDSDR EBVR20220526None · noneEMERGENCY EXIT SURROUND DOUBLER HAS 1 EACH CHAFE LOCATION AT FS335.625.
SDR DXTA2022052062280Flag · missingMAIN DOOR: DURING PREFLIGHT, FLAG ON MAIN CABIN DOOR STEP MISSING/OUT OF VIEW. REMOVED CABIN STEPS AND CENTERED ALL GREEN "LOCKED" FLAGS IN OBSERVATION WINDOWS AS NEEDED IN REFERENCE TO CE-560XL MM 52-10-02. RESECURED STEPS TO ORIGINAL CONFIGURATION. WORK PSDR DXTA2022051962090Diode · defectiveEMERG EXIT SIGN/LIGHT: FORWARD EMERGENCY EXIT LIGHTS INOP. FORWARD EMERGENCY LIGHTING BATTERY PACK DEPLETED. REMOVED DAMAGED AMBER EMERGENCY LIGHT "NOT ARMED" LIGHT & REPLACED WITH A NEW LIGHT & LAMP IAW SPM 20-30-30. REMOVED FAILED DIODE DI051 & REPLACED WISDR EBVR20220518None · noneCLAFING WAS FOUND AT F.S. 337.625 ON EXISTING INTERIOR REPAIR DOUBLER AT RH SURROUND DOUBLER, EMERGENCY EXIT LOCATION.
SDR 9JLA2022051919088Brake · failedTHE FLIGHT CREW REPORTED THAT AFTER LANDING THE PILOT SIDE LEFT BRAKE WAS INOP. THE MAINTENANCE VENDOR FOUND THE PILOTS LEFT BRAKE CABLE FAILED JUST PASSED THE FIRST PULLEY STARTING FROM THE RUDDER PEDAL. THE TECH INDICATED NO SIGNS OF RUBBING IN OR AROUND THESDR DXTA2022051661860Seal · tornMAIN DOOR PRIMARY SEAL: DURING CLIMB THRU 32000 DOOR SEAL LIGHT ILLUMINATED 5 MINUTES LATER HEARD LOAD RUSH OF AIR FOR 1 MINUTE WITH CABIN CLIMB THEN CABIN STABILIZED. LIGHT REMAINED ILLUMINATE FOR30 MINUTES UNTIL BELOW 24000. REPEAT WRITEUP // SIGNOFF// REMOSDR CVGA20220519001Oil System · low pressureDURING CLIMB OUT BETWEEN 8000 - 9000' THE LO OIL PRESS R ANNUNCIATOR LIGHT AND RED MASTER WARING LITE ILLUMINATED AND THE OIL PRESSURE R GAUGE DROPPED BELOW 20PSI TWICE FOR ABOUT 1-2 SECONDS. ALL OTHER INDICATIONS NORMAL.SDR DXTA2022051661750Connector · intermittentFLOOR EMERG EXIT LIGHT: LEFT SIDE AISLE EMERGENCY LIGHTS FROM MID CAIN TO DOOR ARE VERY DIM //SIGNOFF// UPON INSPECTING RIGHT HAND AISLE LIGHTS, FOUND LIGHTS TO BE OPERATING INTERMITTENTL Y. CLEANED THE CONNECTION LEADS IN REFERENCE TO CE560XL AMM 20-30·05. AISDR DXTA2022051161590None · noneMAIN DOOR HANDLE: MAIN CABIN DOOR HANDLE IS EXTREMELY STIFF AND DIFFICULT TO OPEN AND CLOSE BOTH INSIDE AND AND OUTSIDE OF THE AIRCRAFT///CORRECTIVE ACTION///LUBRICATED MAIN DOOR HANDLE LINKAGE IAW CE560XL AMM 12-20-52 AS REQUIRED OPS CHECK GOOD.SDR DXTA2022051061530Door Seal · malfunctionedMAIN DOOR: WITH APU RUNNING AND BLEED AIR ON THE MAIN CABIN DOOR WOULD NOT CLOSE. THE DOOR SEAL WAS INFLATED. SHUT OFF THE BLEED AIR WITH NO CHANGE. WHEN WE SHUT OFF THE APU THE SEAL DEFLATED AND THE DOOR CLOSES NORMALLY. /// CORRECTIVE ACTION /// OPS CHECKSDR DXTA2022050661340Battery Pack · dischargedEMERGENCY LIGHTING: FORWARD INTERIOR CABIN EMERGENCY LIGHTING BATTERY APPEARS TO BE DEAD. EXIT LIGHT, SEAT 3 AND 10 LIGHTS, FWD FLOOR LIGHTING AND RIGHT SIDE DOOR EXIT LIGHT ALL INOP WITH BATTERY CONNECTED AND SWITCH ON.///CORRECTIVE ACTION/// INSTALLED P/N-SDR EBVR202200503None · noneREPAIRED CRACKS ON MAIN ENTRY DOOR AFT FRAME IN ACCORDANCE WITH AEROSPACE QUALITY RESEARCH AND DEVELOPMENT MRO ERO-971781 REV IR DATED APRIL 26, 2022 APPROVED BY FAA FORM 8110-3 (DERT-806568252) DATED APRIL 26, 2022.SDR DXTA2022050261110None · noneMAIN DOOR CABLE: WHEN OPENING MAIN CABIN DOOR FROM INSIDE, DOOR FALLS FAST WITH NO TENSION // SIGNOFF// PERFORMED OPERATIONAL CHECK OF MAIN DOOR COULD NOT VERIFY SQUAWK. REMOVED AIRSTAIRS STEP ASSEMBLY AND VERIFIED RIGGING OF THE MED
SYSTEM WITH NO DEFECTS NSDR DXTA2022042961080Pcb · defectiveANNUNCIATOR WARNING SYSTEM: CABIN DOOR WARNING LIGHT ILLUMINATED AS AIRCRAFT WAS IN A CLIMB AND PASSING THROUGH 33,000'. REPEAT GRIPE. REMOVED CABIN DOOR PCB NZ007 P/N:6618707-26 S/N:0282 INSTALLED CUSTOMER SUPPLIED NEW CABIN DOOR PCB NZ007 P/N:6618707-26 S/NSDR DXTA2022042961070Valve · faultedMAIN DOOR PRIMARY SEAL: AFTER LANDING, WITH APU STARTED AIRBORNE IN THE TERMINAL AREA, & STILL RUNNING IN THE CHOCKS, MAIN DOOR PRIMARY SEAL TOOK 12-15 SECS TO DEFLATE AFTER DOOR HANDLE WAS ROTATED TO OPEN POSITION, PREVENTING DOOR FROM OPENING. AFTER OWNER SDR R3WA 22.02Data Box · dirtyCREW WAS DESCENDING TO KMDW WHEN ADC #2 ALTITUDE TAPE FAILED ON FO SCREEN. CREW DECLARED AN EMERGENCY AS THEY WERE APPROACHING CLASS B AIRSPACE. CREW RAN CHECKLIST AND PERFORMED A REVERSION TO THE #1 ADC. LANDED WITHOUT INCIDENT. MAINTENANCE WENT TO AIRCRAFT PSDR DXTA2022042861020None · noneMAIN CABIN DOOR INTERMITTENTLY DOES NOT OPEN FROM THE OUTSIDE AND INSIDE EVEN IF YOU PULL THE PRE-CATCH, THE DOOR DOES NOT OPEN. YOU NEED TO RE-LOCK THE DOOR AND THEN OPEN AGAIN. "CORRECTIVE ACTION" CLEANED AND LUBRICATED CABIN DOOR PINS PER CE560XLS AMM 52-10SDR 3EJA840CC04/24/2None · nonePRIOR TO DEPARTURE, WHILE TAXING THE ANTI-SKID INOP AND LOW BRAKE PRESSURE LIGHTS ILLUMINATED, THEN A COMPLETE LOSS OF BRAKING WAS EXPERIENCED. EMERGENCY BRAKES WERE USED.SDR DXTA2022042560800Actuator · damagedNLG LANDING GEAR UNLOCK LIGHT: DURING GEAR RETRACTION, "UNLOCK" LIGHT REMAINED ILLUMINATED. HYD PRESS LIGHT FOLLOWED SHORTLY AFTER. QRH PROCEDURES FOLLOWED AND GEAR WAS LOWERED. THREE GREEN ILLUMINATED AND HYD PRESS LIGHT EXTINGUISHED. NORMAL LANDING. REMSDR DXTA2022042560850None · noneCABIN EXTERNAL HANDLE IS VERY LOOSE. IF ANY WEIGHT IS PLACED ON IT, IT DROPS DOWN ALMOST TO THE DOOR SUPPORTS. ANYONE USING IT AS A HAND RAIL WHILE DEPARTING THE PLANE WILL MOST DEFINITELY FALL. "CORRECTIVE ACTION" INSTALLED CUSTOMER SUPPLIED NEW PIN PN MS3567SDR DXTA2022042560900Landing Gear · malfunctionedGEAR POSITION & WARNING: ON CLIMBOUT, AFTER THE GEAR GEAR AND FLAPS WERE SELECTED UP, THE 3 GREEN GEAR INDICATORS EXTINGUISHED AND THE GEAR UNLOCK LIGHT REMAINED ON WITH THE STAB MISCOMPARE AND HYD PRESS ANNUCIATORS ON. THE CHECKLIST WAS COMPLETED AND THE GEASDR 9JLA2022042530799Control Valve · defectiveTHE FLIGHT CREW REPORTED AT 45,000 FT THE INITIAL POWER REDUCTION FROM CLIMB POWER TO 90% YIELDED AN AUDIBLE "THUD" AND HOT AIR SMELL. THE MAINTENANCE VENDOR TROUBLESHOT AND DETERMINED THE LEFT AND RIGHT FLOW CONTROL VALVES TO BE DEFECTIVE. THE VALVES WERE REPSDR EBVR20220419None · noneREPAIRED CRACKS ON MAIN ENTRY DOOR AFT FRAME IN ACCORDANCE WITH AEROSPACE QUALITY RESEARCH AND DEVELOPMENT MRO ERO-971710 REV IR DATED APRIL 18, 2022 APPROVED BY FAA FORM 8110-3 (DERT-833246-CE) DATED APRIL 18, 2022.SDR DXTA2022041960640Tube · shearedMAIN DOOR HARDWARE: THE MAIN CABIN DOOR OVER CENTER BAR THAT CONNECTS THE HANDLE TO THE DOOR HAS SHEARED OFF WHEN WE ATTEMPTED TO PULL THE DOOR CLOSED. // SIGN OFF // REMOVED AND REPLACED DOOR LOWER ACTUATING LEVER TUBE ASSY, ROD END, DRIVE ARM, AND HARDWARE SDR DXTA2022041860360None · noneWHILE IN CRUISE AT 40,000 FEET, WE GOT THE "CABIN DOOR" ANNUNCIATOR. WE FOLLOWED THE QRH AND DIVERTED. UPON ARRIVAL T E DOOR PINS WERE INTACT AND LOCKED. // SIGNOFF// ATTEMPTED TO REPRODUCE PILOT WRITE UP. PERFORMED DOOR WARNING SYSTEM - OPERATIONAL CHECK ISDR 3EJA85104/14/22None · crackedLH COCKPIT SIDE WINDOW GLASS FRACTURED ENTIRE WINDOW ON CLIMB OUT.SDR DXTA2022041460260Lamp · burned outRIGHT MLG INDICATOR LIGHT: ON FINAL APPROACH WE SELECTED THE GEAR DOWN AND HAD NO RIGHT MAIN GEAR INDICATOR LIGHT TO ILLUMINATE. WE PERFORMED A GO AROUND, PERFORMED THE QRH, AND BLEW THE GEAR DOWN MANUALLY. WE DECLARED AN EMERGENCY AND LANDED UNEVENTFULLY. ///SDR DXTR202204131Light · burned outRIGHT MLG INDICATOR LIGHT: ON FINAL APPROACH WE SELECTED THE GEAR DOWN AND HAD NO RIGHT MAIN GEAR INDICATOR LIGHT TO ILLUMINATE. WE PERFORMED A GO AROUND, PERFORMED THE QRH, AND BLEW THE GEAR DOWN MANUALLY. WE DECLARED AN EMERGENCY AND LANDED UNEVENTFULLY. RESDR DXTA2022041360250Door · out of adjustMAIN DOOR: MAIN CABIN DOOR NEEDS ADJUSTMENT. DOOR HANDLE AND VENT DOOR ON THE 6 PACK STAY ILLUMINATED. AFTER SERVERAL TRIES REOPENING AND CLOSING THE DOOR THE LIGHTS WOULD EXTINGUISH // SIGNOFF// AFTER INVESTIGATING, FOUND INNER DOOR HANDLE LINKAGE RODS WERE SDR DXTA2022033159360Seal · unknownMAIN DOOR PRIMARY SEAL: WHEN EXITING AIRCRAFT AND MOVING MAIN DOOR LEVER TO THE OPEN POSITION DOOR TAKES AROUND 20 SECONDS TO BE ABLE TO OPEN BECAUSE THE DOOR SEALS DO NOT RETRACT AS THEY ARE REQUIRED TO DO.//CORRECTIVE ACTION//REMOVED PRIMARY AND ACOUSTIC DOSDR DXTA2022032959220Not Reported · not reportedNLG LANDING GEAR RETRACTION: INFLIGHT, AFTER GEAR RETRACTION RED UNLOCK LIGHT REMAINS ILLUMINATED. ALL 3 GREEN DOWN LIGHTS WERE EXTINGUISHED.//CORRECTIVE ACTION//JACKED UP AIRCRAFT. CHECKED NOSE STRUT EXTENSION AND FOUND TO BE AT
THE CORRECT DIMENSION OF 9.1SDR DXTA2022032859030Light · inoperativeEMERG EXIT SIGN/LIGHT: DURING TEST, THE EMERGENCY EXIT SIGN LIGHT ON THE FRONT LOWER BOTTOM OF LAV IS NOT ILLUMINATED WHEN ALL OTHER EMERGENCY LIGHTS ARE ON.
(PRE-FLIGHT)
CORRECTIVE ACTION// REMOVED AND REPLACED AFT EMERGENCY BATTERY LIGHT OPS CHECK GOODSDR DXTA2022032558980Shade · defectiveCABIN WINDOW SHADE: CABIN WINDOW SHADE ON THE EMERGENCY EXIT DOOR AND OVER THE LAV IS INOP//CORRECTIVE ACTION//REMOVED WINDOW SHADE ASSY PN.6619325-27 SN.N/A AND INSTALLED NEW
CUSTOMER SUPPLIED WINDOW PN.6619325-27 SN.N/A. REF CE-560XL AMM
25-60-00SDR EBVR20220322None · noneA CRACK WAS FOUND ON THE MAIN ENTRY DOOR STRUCTURE UNDER THE AFT SUPPORT ROD MOUNT. REPAIRED CRACK ON MAIN ENTRY DOOR AFT FRAME IN ACCORDANCE WITH AEROSPACE QUALSDR 2022FA0000164None · noneA CRACK IN THE MAIN ENTRY DOOR FRAME UNDER THE AFT SUPPORT ROD MOUNT WAS FOUND DURING 600 HOUR INSPECTION. REPAIRED CRACK ON MAIN ENTRY DOOR AFT FRAME IN ACCORDANCE WITH AEROSPSDR DXTA2022032158730Tire · defectiveLEFT MLG TIRE: LEFT MAIN TIRE BLEW ON ROLL OUT AFTER LANDING RUNWAY 22 LEXINGTON. (AIRPORT HAS A/C OUT OF THE WAY NOW.)//CORRECTIVE ACTION// REMOVE AND REPLACE WHEEL ASSY NO DEFECTS NOTED.SDR 2022F00137Attach Fitting · gougedRMLG ACTUATOR GOUGED ACTUATOR FITTING. MINOR REPAIR ACCOMPLISHED IAW TEXTRON AVIATION ENGINEERING MEMO DQ34007 DATED MARCH 18, 2022; 560-5636, N657QS, REPAIR RECOMMENDATIONSDR 2022F00136Flap · delaminatedL/H IB FLAP HAS MULTIPLE AREAS OF DELAMINATION ON BOTTOM SIDE OF FLAPS. PN: 6525130-37 SN: 733. R/H IB FLAP HAS MULTIPLE AREAS OF DELAMINATION ON BOTTOM SIDE OF FLAPS. PN: 6525130-38 SN: 772. MAJOR REPAIR ACCOMPLISHED BY AEROSPACE QUALITY RESEARCH AND DEVELOPMSDR DXTA2022031858650Switch · dirtyMAIN DOOR: UPON CLOSING MAIN CABIN DOOR THE MIDDLE TOP AND BOTTOM RED SIXPACK LIGHTS REMAINED ON. WAS ABLE TO EXTINGUISH BOTTOM MIDDLE W VENT DOOR KNOB, BUT TOP REMAINED ILLUMINATED. TRIED THE DOOR MULTIPLE TIMES WITH AND WITHOUT APU AIR ON, AND UNABLE TO SECUSDR DXTA2022031458440Engine · damagedRIGHT ENGINE FUEL FLOW: IN FLIGHT AFTER ACTUATING THE CROSSFEED FROM LEFT TANK TO RIGHT ENGINE THE RIGHT FUEL BOOST PUMP AMBER ANNUNCIATOR ILLUMINATED STEADY AND REMAINED ILLUMINATED. CROSSFEED WAS TURNED OFF AND R FUEL BOOST AMBER REMAINED ILLUMINATED. APPRSDR DXTA2022031458460Seal · damagedMAIN DOOR ACOUSTIC SEAL: UPON POWER UP FOR TAKEOFF, WE EXPERIENCED A PERCUSSION EXPLOSION FROM THE CABIN. EXECUTED A LOW SPEED ABORT AND EXITED THE RUNWAY. UPON INSPECTION WE DISCOVERED THE MAIN CABIN DOOR DECORATIVE TRIM OUT OF POSITION, THE ACOUSTIC SEAL FRASDR DXTA2022031458480None · noneMAIN DOOR PRECATCH: WHEN OPENING THE LOCKED MAIN CABIN DOOR FROM THE INSIDE OR THE OUTSIDE THE PRE-CATCH WILL NOT RELEASE UNLESS PHYSICALLY PRESSED. ATTACHED VIDEOS ALSO INTERMITTENTLY WHEN THE DOOR IS CLOSED JUST ON THE PRE-CATCH WE ARE NOT ABLE TO MOVE THE SDR DXTA2022031458400None · noneMAIN DOOR PRECATCH: WHEN DOOR IS CLOSED AND LOCKED WITH THE PRE-CATCH ENGAGED. UPON OPENING THE DOOR FROM INSIDE OR OUTSIDE THE PRE-CATCH WILL NOT RELEASE // SIGNOFF// CONFIRMED DISCREPANCY. GAINED ACCESS TO PRE-CATCH MECHANISM AND ADJUSTED PRE-CATCH CABLE UNSDR 2022FA0000148Warning Horn · false indicationLANDING GEAR WARNING HORN: REPEAT. ON PRE FLIGHT WARNING HON WORKED WITH SEVERAL CHECKS USING ROTORY TEST. IN FLIGHT WARNING HORN INOP AT ALL ALTITUDES ON POST FLIGHT LANDING GEAR WARNING HORN INOP USING ROTORY TEST. LIGHTS (3 GREEN 1 RED) GEAR INDICATORS WORKSDR 9JLA2022031430792Transducer · defectiveTHE FLIGHT CREW REPORTED THAT THE RIGHT MAIN WHEEL BRAKE GRABBING AND JERKING ON APPLICATION. THE MAINTENANCE VENDOR TROUBLESHOT AND DETERMINED THAT THE RIGHT WHEEL TRANSDUCER WAS DEFECTIVE AND WAS REPLACED WITH AN OVERHAULED UNIT. OPERATIONAL CHECKS WERE SATISDR DXTA2022030357760Not Reported · not reportedOXYGEN HARDWARE: OXYGEN BOTTLE IN THE RIGHT FRONT NOSE COMPARTMENT IS SAFETY WIRED INCORRECTLY. THE ON/OFF LEVER IS NOT SAFETY WIRED TO THE ON POSITION. (ON PREFLIGHT)//CORRECTIVE ACTION// SAFETIED LEVER CORRECTLY IAW CE-560XL AMM CHAPTER 35-01-01SDR DXTR2022022801Autopilot Sys · brokenYAW DAMPER: YAW DAMPER DOESN'T SEEM TO WORK IN TURBULENT AIR. PLANE FISH TAILS AND DUTCH ROLLS IN UNSTABLE AIR, BUT IS FINE IN SMOOTH AIR. THE YAW DAMP ENGAGE SWITCH ILLUMINATES GREEN, INDICATING NORMAL OPERATION .UPON FURTHER INVESTIGATION FOUND THE RUDDER SDR DXTA2022022857520None · noneAFTER STARTING THE APU, WE WAITED APPROXIMATELY 3 MIN BEFORE THE BLEED AIR WAS TURNED ON. WITHIN 15 SECONDS OF TURNING THE APU BLEED AIR ON, THE CABIN STARTED TO FILL WITH A DUSTY HAZE. WE SHUT THE BLEED AIR OFF AND THE HAZE SLOWLY SUBSIDED. APPROX 1 MIN AFTERSDR 2022F00057Rudder · crackedRUDDER SKIN IS CRACKED NEAR THE LOWER END OF THE HINGE HALF. TEXTRON AVIATION ENGINEERING DEEMED THE DAMAGE AS MINOR IN SCOPE. ACCOMPLISHED TEXTRON AVIATION ENGINEERING MEMO DQ33703M1 DATED 24FEB2022, 560-5636 (N657QS) RUDDER AND RUDDER TRIM TAB SKIN DAMAGE (C
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