Bombardier BD-700-1A11
Service difficulty reports · 187
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 = 'BD7001A11' 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 = 'BD7001A11' 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 DXTA2026102610323Door · bindingMAIN CABIN DOOR WONT GO UP FAR ENOUGH TO SHUT. ITS NOT CATCHING AT THE TOP TO GET THE HANDLE TO GO DOWN AND SHUT.SDR DXTA2026101510145Sealant · missingAILERON JAMMED IN CRUISE FLIGHT. BOTH SIDES AFFECTED. WAS ABLE TO SLOWLY TURN THE AIRCRAFT. POURING RAIN FOR HOURS BEFORE OUR DEPARTURE. PICTURES ARE OF WATER DRAINING FROM AILERON AT DESTINATION. COMPLETED OPS CHECK & GVI, NO DEFECTS, NOTED HORIZONTAL LEADISDR U5QA202610020182Engine · flamed outDURING TAXI, L ENG FLAMEOUT EICAS. ENG AUTO SHUTDOWN. MX C/A: MULTIPLE DAYS OF TROUBLESHOOTING, BORESCOPE INSPECTIONS, ETC. ALONGSIDE ROLLS ROYCE. COULD NOT IDENTIFY ISSUE(S). DECIDED TO LH R&R ENGINE. AWAITED RENTAL AVAILABILITY, R&R LH ENGINE WITH RENTALSDR DXTA2026093009933Rod · lack of lubeMAIN ENTRANCE DOOR WILL NOT CLOSE FAR ENOUGH USING THE MOTOR. AFTER IT STOPS AT THE TOP IT REQUIRES A SIGNIFICANT PUSH FROM THE OUTSIDE OR A PULL FROM INSIDE IN ORDER TO LATCH IT CLOSED. LUBRICATED PASSENGER DOOR TELESCOPIC RODS AND PERFORMED SATISFACTORY OSDR DXTA2026092209797Elec Connector · looseAMBER PASSENGER DOOR CAS DISPLAYED IN CRUISE. SCHEMATIC OF DOOR SHOWED OPEN AS WELL. NO CHANGE IN CABIN PRESSURE OR DIFFERENTIAL NOTED. SECURED LOOSE CANNON PLUG. OPS CHECK GOOD. IAW SPM 20W-20-00SDR DXTA2026092209778Door Seal · leakingDURING CRUISE AT FL450, MAIN CABIN DOOR WAS SQUEALING LOUDLY. LOWER ALTITUDE WAS SELECTED AND SQUEAL VOLUME LOWERED WITH ALTITUDE. LIGHT COULD BE SEEN COMING FROM MIDDLE RIGHT SIDE OF CABIN DOOR. REMOVED AND REPLACED THE PASSENGER DOOR SEAL IAW GL5500 AMM 5SDR DXTA2026092109773Wire Harness · damagedTHE AMBER PASSENGER DOOR EICAS MESSAGE POSTED DURING FLIGHT, THEN CANCELLED THEN POSTED AGAIN, MULTIPLE TIMES (15+) DURING CRUISE FLIGHT . THE PAX DOOR ON THE STATUS SYNOPTIC SHOWED AMBER OPEN. THE CABIN ALTITUDE REMAINED CONSTANT, AND THE CABIN RATE WAS ZERO.SDR DXTA2026090809581Unknown · noiseREACHING FL450 VERY LOUD ABNORMAL AIR RUSHING SOUND FROM MAIN CABIN DOOR AREA. MORE PRONOUNCED FROM FWD PORTION OF DOOR. NO ABNORMAL PRESSURIZATION OR DOOR INDICATIONS. CABIN ALT 4500'. CABIN DIFF 10.31. SOUND WENT AWAY AS WE DESCENDED BELOW FL410. INSPESDR U5QA202608310179Hydraulic Line · crackedNR 1 HYD LEAK IN AIR. UNEVENTFUL LANDING. HYD FLUID NOTICED ON BOTTOM OF AFT FUSELAGE. COMPLIED WITH CAMP CARD 20260831-23. INSPECTED AREAS WITH HYD FLUID & FOLLOWED TO AFT EQUIP BAY. LARGEST CONCENTRATION OF FLUID AROUND LT HYD FILTER MANIFOLD. TORQUED HSDR DXTA2026081809290Proximity Sensor · faultedCARGO DOOR OPEN CAS ILLUMINATED ON CLIMB AT APPROXIMATELY 10000 FT. CABIN DEPRESSURIZED. CABIN PRESSURE WAS CONTROLLABLE IN MANUAL MODE. FOUND THE DOOR LOCK PROX SENSOR DAMAGED. REMOVED DAMAGED DOOR LOCK PROX SENSOR PN:8-642-03 SN:64499 AND INSTALLED NEW PRSDR DXTA2026060408300Fmu · failedWHILE DESCENDING, AT APROX FL340 THE CREW OBSERVED 2 LARGE BANGS SOUNDED LIKE COMPRESSOR STALLS. FLT ATTENDANT NOTED BANGS LOUDER IN BACK THAN WHAT PERCEIVED IN FRONT. AFTER LOUD BANGS, RT FADEC FAIL MESSAGE WAS ILLUMINATED. FOLLOWED THAT CHECKLIST WHILE TUSDR DXTA2026052608191Indication Sys · malfunctionedLEFT WING FUEL QUANTITY WILL RAPIDLY INCREASE IN INDICATED AMOUNT. THIS LARGE INCREASE CREATES A FUEL IMBALANCE AMBER CAS MESSAGE, AND THE AUTO TRANSFER SYSTEM WILL ATTEMPT TO TRANSFER FUEL FROM THE PERCEIVED HEAVY LEFT WING TO THE RIGHT WING, CREATING AN ACTUSDR DXTA2026050607904Pressure Switch · failedDURING TAKEOFF ROLL, AFTER APPLYING TAKEOFF POWER, BLUE CAS MESSAGE: L OIL FILTER MESSAGE ILLUMINATED. INITIATED ABORT. WHEN THROTTLES RETARDED, MESSAGE DISAPPEARED. REMOVED LT ENGINE DIFFERENTIAL PRESSURE SWITCH, AND INSTALLED INSPECTED TESTED PART. PERFORMSDR DXTA2026042707774Steering Unit · failedNOSE STEERING FAIL CAS IN CLIMB WOULD NOT RESET. REPLACED STEERING CONTROL UNIT WITH K-BALLED UNIT FROM IAW AMM 32-51-01-400-801.SDR DXTA2026042707750Shutoff Valve · defectiveAFTER EXTENDING THE LANDING GEAR WE RECEIVED THE BRAKE 50% DEGRADED AND AUTOBRAKE FAIL CAUTION MESSAGES. REMOVED AND REPLACED R/H OUTBD BRAKE SHUTOFF VALVE PN OFF GW415-6175-3 SN OFF 2071T, PER BOMBARDIER GLOBAL 5500 AMM TASK 32-43-25-400-801. OPERATIONAL CHSDR DXTA2026031207191Pressure Switch · failedFIRST FLIGHT OF DAY ON LANDING ROLL OUT NOSE STEER FAIL MESSAGE DISPLAYED. STOPPED AIRCRAFT RESET NOSE STEER AND CONTINUED TO FBO. DEPARTED TO FLY MULTIPLE LEGS WITH NO ISSUE. AFTER FORTH LANDING OF DAY NOSE STEER FAILED AGAIN ON ROLL OUT. STOPPED AIRCRAFT ANSDR DXTA2026022006937Microwave Oven · faultedIN FLIGHT OUR FA ATTEMPTED TO USE THE MICROWAVE TO WARM PASSENGER FOOD. WITHIN 5 SECONDS OF USE, THE MICROWAVE BEGAN TO ARC INSIDE ON THE TOP, MADE A HIGH PITCH SQUEELING SOUND, AND GAVE OFF AN ACRID SMELL. WE STOPPED THE PROCESS AND ISOLATED THE CIRCUIT VIA TSDR DXTA2026021606885Battery Pack · faultedAFT OVER WING EMERGENCY LIGHT IS INOP CORRECTIVE ACTION: AND REMOVED POWER SUPPLY DUE TO LIGHT BEING INOP. INSTALLED CUSTOMER SUPPLIED REPAIRED POWER SUPPLY IAW AMM 33-51-09, OPS CHECKED GOOD.SDR DXTA2026021606878Engine · failedCLIMBING OUT OF 10,000 FEET, THE RIGHT ENGINE HAD A VIOLENT FAILURE. THERE WAS A LOUD BANG, AND SHOCK THROUGH THE AIRPLANE, AND THE PLANE LURCHED HARD TO THE RIGHT. SUSPECT POSSIBLE COMPRESSOR STALL, OR INTERNAL FAILURE. THE ENGINE QUICKLY SHUTDOWN. ACCOMPLISHSDR DXTA2026021206861Target · looseAFTER TAKEOFF, CARGO DOOR EICAS ILLIMINATED WITH THE CARGO DOOR SHOWING OPEN. ON LANDING, VISUALLY INSPECTED DOOR, IT WAS LOCKED & SECURE. POWERED ON & VERIFIED CARGO DOOR AMBER CAS MESSAGE PRESENT, WHILE BAGGAGE DOOR IS CLOSED & LOCKED. CYCLED THE DOOR MSDR DXTA2026020206739Battery Pack · defectiveWHEN PLANE IS POWERED IN EMERGENCY LIGHTS ARE ON THE ARM OR OFF POSITION. ALL EMERGED LIGHTS ARE OFF AS EXPECTED. WHEN THE AP IS SHUTDOWN THE FWD EMERGENCY LIGHTS ARE RECEIVING POWER & ON. THIS INCLUDES THE EXTERIOR EMERGENCY LIGHTS TO RT OF CABIN DOOR AS WELLSDR DXTA2026012306636Battery Pack · faultyWHEN PLANE IS POWERED IN EMERGENCY LIGHTS ARE ON THE ARM OR OFF POSITION. ALL EMERGENCY LIGHTS ARE OFF AS EXPECTED. WHEN THE APU IS SHUT DOWN THE FORWARD EMERGENCY LIGHTS ARE OUR RECEIVING POWER AND ON. THIS INCLUDES THE EXTERIOR EMERGENCY LIGHT TO THE RIGHT OSDR DXTA2025122906287Seat · faultedDURING CRUISE, AN ELECTRICAL/PLASTIC INSULATION BURNING ODOR IN CABIN, AND A VERY LIGHT HAZE OF SMOKE NOTICEABLE AGAINST INCOMING SUNLIGHT, CREW WAS ABLE TO LOCATE THE SOURCE AREA, LOWER SIDEWALL ADJACENT TO SEAT NR 4, LOCATION THAT ALSO PRESENTS AN AREA OF DSDR DXTA2025121506086Actuator · defectiveMED WILL NOT CLOSE. NEITHER THE INTERIOR OR EXTERIOR SWITCH HAVE ANY EFFECT. CORRECTIVE ACTION: REMOVED DEFECTIVE PAX DOOR ACTUATOR AND REPLACED IT WITH CUSTOMER SUPPLIED REPAIRED ACTUATOR. PERFORMED A SATISFACTORY FUNCTIONAL TEST OF THE PASSENGER DOOR WITH SDR DXTA2025120305948Door · icedMAIN CABIN DOOR WILL NOT CLOSE. UNABLE TO CLOSE FROM EITHER OUTSIDE, OR INSIDE. FOUND BUILDUP OF ICE INSIDE DOOR. REMOVED ICE FROM INSIDE DOOR AND PERFORMED MULTIPLE SATISFACTORY OPERATIONAL CHECKS IAW GL-5500 AMM 52-11-00. NO OTHER DEFECTS NOTED AT THIS TIMSDR DXTA2025120205903Control Valve · defectiveRECEIVED A BRAKE 50% DEGRADED AMBER CAS MESSAGE. R & R LT OTBD BRAKE CONTROL VALVE IAW AMM 32-43-09. BLED & LEAK CHKD NR 2 HYDRAULIC SYSTEM IAW AMM 29-10-00. OPS CHKD GOOD.SDR DXTA2025120105882Shutoff Valve · faultedTHE BRAKE 50% DEGRADED & AUTO BRAKE FAIL AMBER CAS MESSAGE CAME ON SHORTLY AFTER GEAR EXTENSION. INTERROGATED OMD DATA FOR FAULTS AND SENT BRAKE SYS OMS DOWNLOADS TO MCC FOR REVIEW. INTERROGATED OMD DATA FOR FAULTS & SENT FAULT MESSAGE OMS DOWNLOADS TO MCC FOSDR DXTA2025112005751Actuator · weakWHEN CLOSING MAIN CABIN DOOR ON OUTSIDE OF AIRPLANE USING EXTREMAL SWITCH IN AUTO MODE, MED WENT UP ABOUT 1/3 OF THE WAY AND THEN STOPPED AND CAME BACK DOWN. WAS UNABLE TO USE OUTSIDE SWITCH IN EITHER AUTO OR MANUAL TO RAISE DOOR. TRIED USING SWITCH ON INSIDSDR DXTA2025111705694Battery Pack · intermittentCABIN EMERGENCY LIGHTS ARE TURNING OFF AND ON UNCOMMANDED WHEN EMERGENCY LIGHT SWITCH IS IN ON POSITION. CABIN EMERGENCY LIGHTS ARE TURNING OFF AND ON UNCOMMANDED WHEN EMER LIGHT SWITCH IS IN ON POSITION: REMOVED #4 EMERGENCY LIGHT POWER SUPPLY P/N 8ES40980SDR DXTA2025111705701Actuator · noisyWHEN CLOSING MAIN ENTRY DOOR FROM INSIDE THERE IS A LOUD POP WHEN THE DOOR STARTS UP. WHEN DOOR IS CLOSED AND THE HANDLE IS PUSHED DOWN. THERE IS A GRINDING NOISE THAT GOES ON FOR A FEW SECONDS BEFORE DOOR SEAL IS PRESSURIZED CORRECTIVE ACTION: REMOVED MAIN SDR DXTA2025092905092Contactor · faultedDURING POWER UP CHECKS ON PREFLIGHT, RED SMOKE AVIONICS BAY CAS MESSAGE AND AUDIO CAME ON. AFTER PERFORMING THE SMART OPS PROCEDURE FOR AN ASSOCIATED ELEC SYS FAULT MESSAGE THE CAS MESSAGE CLEARED. AFTER ENGINE START THE SAME RED SMOKE AVIONICS BAY CAS MESSAGESDR DXTA2025092605088Door · bindingMAIN DOOR CLOSES NORMALLY FROM INSIDE, MAIN DOOR REQUIRES SIGNIFICANT FORCE TO CLOSE FROM THE OUTSIDE. MAIN DOOR OPENS NORMALLY. PERFORMED GVI OF MAIN DOOR IAW AMM 52-11-00 WITH NO DISCREPANCIES NOTED. LUBED COMPONENTS AND PERFORMED FUNCTIONAL TEST OF THE DOSDR DXTA2025091904996Striker · out of adjustON THE DECENT AT ABOUT 17000 THE R EMER EXIT DOOR CAS MESSAG ILLUMATED AND THE EMER DOOR SHOWED UNSARE ON THE AIRCRAFT SYNOPTIC THE PROX SWITCH STRIKER BRACKET WAS OUT OF ADJUSTMENT, AIR GAP MEASURED .080". ADJUSTED STRIKER BRACKET AS NEEDED TO ACHIEVE THE REQSDR DXTA2025080104418Overheat Sensor · false indicationAFTER LANDING, LEFT BRAKE TEMP ROSE TO 14, RIGHT BRAKES WERE A MORE TYPICAL 4. UNLOADING BAGGAGE LEFT MAINS WERE SMOKING. PF OBSERVED SLIGHT PULLING TO THE LEFT. JACKED AIRCRAFT AND FOUND #1 AND #2 BRAKES NOT DRAGGING OR ANY OTHER DISCREPANCIES. #1 BRAKE PINSSDR DXTA2025072104286Control Unit · faultedFIRE DETECT CH B - BATT - TRIP CAME ON IN FLIGHT ON EMS. ATTEMPTED RESET ON BATTERY POWER ON THE GROUND. BUT DID NOT RESET. REMOVED FIDEX AND INSTALLED INSPECTED/TESTED FIDEX CU IAW AMM 26-10-01. COMPLIED WITH OPERATIONAL TEST OF THE FIRE DETECTION AND EXSDR DXTA2025072104273Proximity Sensor · out of adjustLEVEL FLIGHT AT FL 450 THE PASSENGER DOOR CAS MESSAGE CAME ON. ALSO YELLOW PAX DOOR SHOWED OPEN ON STATUS PAGE. ON DESCENT ALL MESSAGES WENT OUT AT FL320. NO FAULT CODE MESSAGES TO PULL UP. ADJUSTED AFT PASSENGER DOOR PROXIMITY SENSOR. OPS CHECK GOOD. IAW BOSDR DXTA2025062504015Pin · stuckUNABLE TO REMOVE EMERGENCY EXIT PIN. REMOVED EMERGENCY EXIT DOOR AND INSPECTED PIN AND HOLES. PIN WAS DIFFICULT TO REMOVE, ONCE REMOVED INSPECTED PIN HOLES AND FOUND PAINT AND DEBRIS IN HOLES. CLEANED HOLES AS NECESSARY TO REMOVED DEBRIS AND PAINT. PIN IS NOW SDR 3J7R2025062400001Battery Pack · faultedFORWARD EMERGENCY LIGHTS ASSOCIATED WITH #1 BATTERY PACK STAY ILLUMINATED AFTER SWITCH IS PLACED IN OFF POSITION.SDR U5QA202506180153Windshield · smokeON CLIMB OUT PASSING 17000FT, SMOKE OBSERVED COMING OUT FROM BETWEEN FRAME OF LEFT WINDSHIELD AND LEFT SIDE WINDOW. MX C/A: RE-TORQUED THE LH WINDSHIELD TERMINALS T1 / T2 AND S2 TO PROPER TORQUE SPECS AS REQUIRED REF GVFD5000 AMM 56-10-01-400-801 STEP F(33). PSDR DXTA2025061203836A/C Pack · faultedWHILE ON THE GROUND DURING COCKPIT PREP THERE WAS SMOKE IN CABIN AND COCKPIT. TURNED OFF PACKS AND GPU BLEED. WHILE RUNNING THRU CHECKLIST THE AMBER LEFT PACK FAIL ILLUMINATED. TEMP ON ECS SYNOPTIC FOR LEFT PACK SHOWED 115 DEGREES. SYSTEM WORKS FINE WITH R PSDR DXTA2025061203824Relay · defectiveMAIN CABIN DOOR SWITCH NOT CLOSING DOOR. REPLACED RELAY DRIVE EQUIPMENT. OPS CHECK GOOD. IAW GL-5000 AMM 44-10-40SDR DXTA2025061003800Tire · explodedMLG: LEFT OUTBOARD MAIN TIRE #1 EXPLODED DURING TAXI INTO RAMP. REPLACED BOTH LH IB AND LH OB MLG WHEEL/TIRE ASSEMBLIES IAW BOMBARDIER GL-5000 GVFD AMM 32-41-01.SDR DXTA2025051903526Control Panel · defectiveMAIN DOOR MOTOR SWITCH: INTERIOR AIRSTAIR DOOR SWITCH INOP. WHEN PRESSED, DOOR WILL NOT CLOSE. CORRECTIVE ACTION; REPLACED INTERIOR MED SWITCH PANEL IAW GLOBAL 5000 MM 52-11-09. OPS CHECK GOOD.SDR DXTA2025050803408Door · malfunctionedMAIN DOOR: UNABLE TO CLOSE THE MAIN DOOR, EITHER FROM INSIDE OR OUTSIDE USING NORMAL PROCEDURES. DOOR IS ABLE TO CLOSE WHEN THE CABIN SYSTEMS ELECTRICAL POWER IS CUT OFF. CORRECTIVE ACTION: CYCLED POWER, PERFORMED OPERATIONAL OF MED WITH INTERRIOR AND EXTERIORSDR DXTA2025042403177Latch · bindingWHILE IN FLIGHT COULD NOT OPEN LAV DOOR DOOR KNOB WILL TURN BUT DOES NOT MOVE LATCH INSIDE IF THE JAM MADE SEVERAL ATTEMPTS TO OPEN COULD NOT CORRECTIVE ACTION: COMPLETED FULL ADJUSTMENT OF THE AFT LAVATORY DOOR AS REQUIRED FOR PROPER DOOR OPERATION. WORK DONESDR DXTA2025041403050None · pax errorPASSENGER COMPARTMENT EQUIPMENT: FA REPORTED ELECTRICAL BURNING SMELL NEAR THE CREDENSA, JUST AFT OF FORWARD CLUB. NO SMOKE OR FIRE. CORRECTIVE ACTION: COULD NOT DUPLICATE. VAPING DEVICE FOUND IN LAV GARBAGE CAN. IAW GL5000 SMM 25-24-52.SDR DXTA2025030602575Control Unit · defectiveAUTOBRAKE FAIL AMBER CAS: EICAS ILLUMINATED AFTER TAKE OFF AND AUTOBRAKE SWITCH KICKED OUT OF "LOW" POSITION TO "OFF" AND WOULD NOT STAY IN "LOW." "BRAKE 50% DEGRADED" EICAS ILLUMINATED SHORTLY AFTER CORRECTIVE ACTION; REPLACED BRAKE CONTROL UNIT. ALL POST MSDR DXTA2025022802502Actuator · faultyMAIN DOOR MOTOR: MAIN CABIN DOOR MOTOR INTERMITTENTLY CUTS OUT WHEN CLOSING THE DOOR USING THE INTERIOR CONTROLS. ALSO, DURING DOOR CLOSING, WHEN THE DOOR REACHES THE TOP THE MOTOR SOMETIMTES CUTS OUT AND DOOR FALLS IMMEDIATELY TO THE OPEN POSITION OR THE DOSDR U5QA202502270147Windshield · crackedLH WINDSHIELD CRACKED IN FLIGHT AT FL450. MX C/A: R&R LH WINDSHIELD ASSY, OPS AND LEAK CKS GOOD.SDR DXTA2025021702356Microwave Oven · failedIN FLIGHT, MICROWAVE MADE A LOUD BANG WHILE IN USE. IMMEDIATELY FOLLOWED BY AN ELEC SMOKE ODOR IN CABIN. FA REPORTED MICROWAVE CB LOCKED. MICROWAVE SHUTDOWN AFTER BANG, ONLY FUMES. R & R MICROWAVE IAW SMM 25-30-66. PERFORMED OPS CHECK, COULD NOT GET CPB'S TO
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