Bombardier BD-100-1A10
Service difficulty reports · 1,845
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 = 'BD1001A10' 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 = 'BD1001A10' 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 DXTA2026101910244Light Sys · faultedEMERGENCY LIGHTS ABOVE SEATS 2L AND 3R DO NOT ILLUMINAT WHEN THE EMER LTS SWITCH IS IN ON POSITION. LIGHTS DO OPERATE WITH NORMAL CABLTS SWITCH. REMOVED FWD EMERGENCY BATTERY POWER SUPPLY P/N OFF BR9767-001 S/N OFF C0926 AND INSTALLED NEW / FWD EMERGENCY BATTSDR DXTA2026101610172Nut · looseEVERYTHING WAS NORMAL IN ALL PHASES OF FLT, EXCEPT TAKEOFF WHEN GEAR WAS RETRACTED, A GRINDING, OR THUMPING SOUND HAS HEARD, FOLLOWED BY A VIOLENT SHAKING VIBRATION THROUGH PLANE, CONTINUES AFTER TRACTION FOR A FEW SECS & THEN STOPPED. EVERYTHING NORMAL DURSDR DXTA2026101610153Light · inoperativeEMERGENCY LIGHT ABOVE SEAT L4 IS INOPERATIVE WITH EMER LIGHTS IN ON. REMOVED DEFECTIVE READING LIGHT AND INSTALLED AS RECEIVED NEW READING LIGHT. OPS CHECKS GOOD WITH NO / DEFECTS NOTED AT THIS TIME. ALL WORK WAS PERFORMED IAW SMM 33-20-05.SDR DXTA2026101410122Engine · flamed outDURING DESCENT AUDIBLE AND TACTILE VIBRATION OCCURRED FOLLOWED BY AMBER VIB INDICATION. RIGHT ENGINE INDICATIONS FLUCTUATED. RIGHT ENGINE FLAMED OUT. SECURED ENGINE AND LANDED. REPLACED ENGINE. OPS/LEAK CHECKED GOOD IAW LMM 72-00-00.SDR DXTA2026101310117Door · openDURING APPROACH TO LANDING AT APPROXIMATELY 500 FEET, CREW COULD FEEL CABIN PRESSURE CLIMBING RAPIDLY. FEELING WAS VISUALLY VERIFIED ON EICAS WITH CABIN CLIMBING AT OVER 1,500. DURING THIS EVENT AMBER CAS MESSAGE CARGO DOOR ILLUMINATED AND TRANSITIONED TO A WHSDR DXTA2026101210096Pitot Tube · faultedREPEAT WRITE UP. AMBER CAS EFIS MISCOMPARE AT 31000 FT. WE ALSO GOT THE ALT BOXED FLAG ON PFD 1 AND PFD 2. AT 31000 FEET THE ALTIMETER SPLITS BETWEEN ONE AND TWO WAS 160 FEET. REPEAT. PHASE OF FLIGHT CRUISE. R & R FAULTY RT PITOT PROBE IAW AMM 34-11-01. ACCSDR DXTA2026100810046Guide · damagedUPON OPENING AIRCRAFT DOOR THE UPPER ROLLER ON THE RIGHT HAND SIDE SHEARED OFF AND FELL TO THE GROUND. THE SIDE WITH THE NUT AND COTTER PIN WAS NOT RECOVERED BUT MAY BE IN THE DOOR; THERE SEEMED TO BE A GRINDING AND VIBRATION FROM THE DOOR RIGGING WHEN CLOSINGSDR DXTA2026100810061Strut · leakingMAIN CABIN DOOR IS HARD TO CLOSE. BOTH PISTONS ON EACH SIDE OF THE DOOR HAS DRIED FLUID ON THEM. REMOVED BOTH FORWARD AND AFT FAULTY TELESCOPIC STRUTS AND REPLACED WITH NEW TELESCOPIC STRUTS. PERFORMED SEVERAL OPERATIONAL CHECKS WITH NO DISCREPANCIES TO NOTEDSDR J7SA2026100200527Acm · seizedAFTER ADVANCING POWER DURING A GO AROUND, A BURNING SMELL EMANATED FROM THE VENTS. ADDITIONALLY, A LOUD WHISTLING SOUND WAS HEARD. THE ECS WOULD NOT BLOW COLD. FOUND AIR CYCLE MACHINE TURBINE SEIZED. REPLACED ACM IAW BOMBARDIER CH 350 AMM 21-52-13. AIR CONDITISDR U5QA202609280181Seal · damagedON INITIAL CLIMB CREW REPORTED A RED RT PYLON LEAK MESSAGE POSTED. REMOVED AND REPLACED FWD AND AFT E-SEALS CONDITION: NEW. REMOVED AND REPLACED FWD AND AFT COUPLINGS. STARTED ENGINES. TAXIED TO RUN PAD. PERFORMED LEAK CHECKS. LEAK CHECK GOOD. OPERATIONAL CHSDR L5VR202606011524Support Beam · corrodedBS 641.750 TO 669.759 FOUND WITH CORROSION AT BEAM BAGGAGE DOOR AROUND NUT-PLATE HOLES (1 AREA HEAVY OUT OF LIMITS). DISCOVERED WHILE IN 96 MONTH INSPECTION.SDR J7SA2026100500529Coffeemaker · odorBURNING ODOR MOMENTARILY DETECTED FROM GALLEY AC POWER OUTLET AFTER COFFEE MACHINE FAILED. COFFEE MACHINE DISCONNECTED AND AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED KEURIG COFFEE MAKER, OPS CHECK GOOD.SDR J7SA2026100500528Hmu · unserviceableDIVERSION DUE TO THE LEFT ENGINE SURGING IN CRUISE WITH NO ASSOCIATED CAS MESSAGE. AIRCRAFT LANDED WITHOUT INCIDENT AT PHNL. REPLACED THE SUSPECTED FAULTY HYDROMECHANICAL UNIT IAW CH350 AMM 73-20-01. OPERATIONAL AND LEAK CHECKS GOOD.SDR J7SA2026092900520Ecu · unserviceableDIVERTED DUE TO R FADEC FAIL CAS PRESENTED AND R ENGINE SHUTDOWN ON DESCENT INTO KPNE AT 9000 FT AND 230-250 KTS. CREW COMPLETED CHECKLIST, NOTIFIED ATC, AND DECLARED AN EMERGENCY. ATTEMPTED RELIGHT OF THE #2 ENGINE WAS UNSUCCESSFUL (N1, N2, AND OIL PRESSURE ISDR DXTA2026092309827Flap System · failedAFTER DEPARTING KCRQ, RECEIVED AN AMBER FLAPS FAIL MESSAGE ON THE EICAS DURING FLAP RETRACTION. DIVERTED TO KLAX. FLAPS FAILED AT 3 DEGREES B3 CODE: B3-276369 PERFORMED AW300-27-0427. DOWNLOADED MDC DATA. SUBMITTED FILES TO BOMBARDIER CRC. REQUEST THE VESDR U5QA202609010180Rvdt · inoperativeDECLARED EMERGENCY. SPOILERS FAULT CAUTION, STAB TRIM FAIL ADVISORY. CYAN STAB TRIM FAULT ON LANDING: REMOVED AND REPLACED RT OTBD MULTI-FUNCTION SPOILIER ROTARY VARIABLE-DIFFERENTIAL TRANSFORMER (MFS RVDT) AND INSTALLED A NEW RT OUTBOARD RVDT IAW AMM 27-61SDR U5QA202608200177Pump · leakingLEFT HYD AMBER HIGH TEMP CAS FOLLOWED BY LT SOV CLOSED. LOSS OF ALL LT HYD (B3-303036 CODE), MANUAL GEAR EXTENSION DUE TO LOSS OF LT SIDE HYD. INSTALLED A REPAIRED LT ED HYD PUMP. FLUSHED THE LT HYD SYS. INSTALLED A NEW LT OTBD CASE DRAIN FILTER. A NEW LSDR J7SA2026090100513Acm · faultedAIR TURN BACK DUE TO A PACK COOL AIR FAIL MESSAGE DURING CLIMB OUT OF KDEN AT 30,000 FT FOLLOWED BY A PACK FAIL CAS AT 40,000 FT. CREW RAN THE PACK FAIL CHECKLIST AND SWITCHED TO TRIM AIR ONLY, AFTER WHICH THE COCKPIT FILLED WITH SMOKE AND THE CREW DONNED OXYGSDR DXTA2026082109351Proximity Sensor · faultedON APPROACH TO LANDING WITH GEAR SELECTED DOWN, CAS MESSAGE PROX SYS FAULT APPEARED B3-224420. REPEAT WRITE UP. ON LANDING ROLLOUT, AFTER SIGNIFICANT SHUDDERING (LIKE A FLAT SPOT ON ALL TIRES) CAS MESSAGE BREAK FAULT APPEARED B3-007414. REMOVED INTERMITTENTSDR U5QA202608180176Acm · seizedCREW REPORTS, THAT THEY WERE ON THE RAMP WITH THE APU RUNNING, AND AFTER THEY SELECTED THE CABIN AIR ON, THEY GOT AN ACRID SMELL AND SMOKE IN THE CABIN. MX C/A: REMOVED AND REPLACED ACM WITH REPAIRED UNIT. PERFORMED SATISFACTORY OPERATIONAL CHECK. REFERENCED SDR J7SA2026090300518Microwave Oven · inoperativeMICROWAVE DOES NOT HEAT WHEN TURNED ON AND EMITS AN ELECTRICAL BURNING SMELL UNTIL MICROWAVE IS TURNED OFF. REPLACED MICROWAVE IAW BD-100 SMM 25-30-03. OPS CHECK GOOD.SDR U5QA202608120175Pump · failedPILOT REPORTS USE OF EMERGENCY EXTENSION ON APPROACH TO KBGR. LEFT ENG HYD PUMP FAILED IN FLT, DUMPING NR 1 HYD SYS OVRBRD RESULTING IN LOSS OF GEAR DOWN COMMAND & NOSE WHEEL STEERING AFTER LANDING. R & R LTENG HYD PUMP IAW AMM 29-12-01. OPS & LEAK CHKD GOODSDR DXTA2026081209211Acm · faultedON CLIMB OUT, NOTICED A WHISTLING NOISE, FOLLOWED BY A UNDESCRIBABLE ODOR. FOLLOWED BY HOT AIR COMING OUT OF THE AIR-CONDITIONING. ON THE ECS PAGE THE ONLY ABNORMALITY WAS THE SUPPLY LINES WERE 61 AND 65 DEGREES. REMOVED FAULTY ACM P/N OFF 3471A020000 S/N OFFSDR DXTA2026081009219Trim Panel · out of adjustHEARD CLICKING NOISE DURING CLOSING OF MAIN CABIN DOOR IN THE VICINITY OF THE DOOR RETRACT MECHANISM. ON POST FLIGHT CHECKED THE EMERGENCY RETRACT HANDLE. PULLED IT SEVERAL TIMES AND DOOR DID NOT RETRACT. FOUND DECORATIVE TRIM PIECE HITTING THE AFT DOOR STRSDR 3EJA393JS080626Pump · failedDURING DECENT INTO DJI EXPERIENCED A VIBRATION FOLLOWED BY A CYAN RT HYD PUMP FAIL CAS MESSAGE. AS WE WERE JOINING THE FINAL APPROACH COURSE AN AMBER R HYD PUMP FAIL MESSAGE APPEARED. RAN CHECKLIST FOR THE CAS MESSAGE. DECLARED AN EMERGENCY ONCE RECEIVED THE SDR 6TXA2026080600626Pump · low pressureRT HYDRAULIC PRESSURE FLUCTUATES AND DASHES WHEN SYSTEM IS PRESSURIZED WITH DCMP. R EDP DOESN’T PRODUCE PRESSURE AT LOW POWER SETTING LOST HYDRAULIC PRESSURE ON THE RIGHT SIDE SYSTEM IN FLIGHT. INCREASING POWER ON THE RIGHT ENGINE BUILT PRESSURE BUT AS SOON ASDR DXTA2026081009150Wire Harness · damagedON INITIAL TAKEOFF LANDING GEAR HANDLE WAS RAISED AND RECEIVED GEAR DISAGREE CAS MESSAGE ALONG WITH PROX SYS FAULT MESSAGE. B3 CODE 007504. TOWER CONFIRMED ALL GEAR WERE IN THE UP POSITION WITH THE GEAR HANDLE UP. GEAR INDICATIONS SHOWED RIGHT MAIN AND NOSE UPSDR J7SA2026081300511Acm · overtempDIVERSION DUE TO PACK TEMP HIGH CAS WITH A HIGH PITCH WHISTLE FROM THE VENTS, A LIGHT BURNING ODOR AND RISING CABIN TEMPERATURE, NOTED WHILE EXECUTING A MISSED APPROACH AT KOXC. CREW CONTINUED TO KHPN. REPLACED AIR CYCLE MACHINE IAW BD 100 AMM 21-52-13. OPS CHSDR DXTA2026080609135Control Valve · defectiveON TAKEOFF WE RECEIVED A LT OTBD BRAKE FAIL MESSAGE. THIS WAS FOLLOWED SHORTLY BY A R OTBD BRAKE FAIL MESSAGE. ABORTED. THE MESSAGES CAME ON AND OFF INTERMITTANTLY AFTER THAT. B3 CODES ARE AS FOLLOWS: B3-007830 AND B3-007107. REPLACED BRAKE CONTROL VALVE. OPSSDR DXTA2026072708985Unknown · odorAFTER FMS 1 FAILED, STARTED TO SMELL A BURNING PLASTIC TYPE OF ODOR. WHEN ADDING THROTTLE, COULD SMELL THE SCENT MORE, ESPECIALLY WHEN TAXING. POWEREDACFT & TURNED ON ALL SYS & PERFORMED MULTIPLE ENG RUNS IAW MCCS REQUEST & DIDN'T SMELL OR SEE ANY SIGNS OF BSDR DXTA2026072708973Bypass Valve · faultedIN CRUISE AT 26000' WE GOT AN AMBER R HYD TEMP HIGH MSG. SHORTLY FOLLOWED BY A CYAN CAS MISCOMPARE MSG. THE LEFT MFD HYD PG SHOWED RIGHT HYDRAULIC SYSTEM GREEN 100C. THE LEFT MFD HYD PG SHOWED AMBER 100C. RAN THE QRH AND DECLARED THE EMERGENCY. WHEN DESCENDINGSDR DXTA2026072708974Bypass Valve · faultedON CLIMB OUT FROM KLAS PASSING 10,000FT WE GOT AN AMBER EMERGENCY EXIT CAS MSG. LEVELED OFF AT 12,000FT & RAN THE QRH CHECKLIST. IT WAS NOTED THAT AT SPEEDS ABOVE 300KTS A DISTINCT VIBRATION WAS FELT IN THE CONTROL COLUMN AS WELL AS THE FUSELAGE. SLOWED TO 290SDR U5QA202607220173Engine · vibrationDURING DESCENT REDUCED POWER AND IMMEDIATELY FELT ENGINE VIBRATION. ITT STARTED TO RISE AND R ENGINE VIBRATION CAS APPEARED. ITT CONTINUED TO RISE AND EVENTUALLY LED TO ENGINE SHUTDOWN IN FLIGHT. MX R & R RT ENGINE.SDR DXTA2026072308934Warning Message · false activationEMERGENCY EXIT POSTED ON CAS CLIMBING THROUGH 8000'. LEVELED OFF AT 10,000' AND RAN THE ASSOCIATED QRH. AFTER ABOUT 4 MINUTES THE CAS EXTINGUISHED. RETURNED TO THE AIRPORT AND LANDED WITHOUT INCIDENT. OBSERVED THAT THE EMERGENCY WAS SECURE AND THE EXTERNSDR DXTA2026072108896Adc · defectiveDURING SHORT FLIGHT, JUST AFTER LEVELING OFF AT 12,000', AMBER EFIS MISCOMPARE AND ALT FLAG (ON PFD2) DISPLAYED. THE RIGHT, PFD2 DISPLAYED A 140' LOW DIFFERENCE COMPARED TO THE LEFT PFD1. BOTH MESSAGES DISAPPEARED ONCE WE STARTED OUR DESCENT. QRH PROCEDURESDR DXTA2026071708843Potentiometer · out of adjustSECOND WRITE UP. DURING LANDING ROLLOUT, THE NOSE WHEEL STEERING FAIL CASS MESSAGE APPEARED. UNABLE TO CONTROL NOSE WHEEL, STEERING WITH PEDALS OR TILLER. TECHS ARRVIED TO ACFT AND WERE UNABLE TO DUPLICATE THE FAULT, TECHS ATTEMPTED TO PERFORM THE NWS NVM DOWNSDR DXTA2026071708804Engine · vibrationAT CRUISE AT FL400 FELT A VIBRATION IN PLANE. ABOUT A MIN LATER L ENG VIBRATION CASS MESS CAME ON. WHILE PULLING OUT QRH, RECEIVED A LT ITT EXCEEDANCE WARNING. BEGAN SMELLING SMOKE IN CABIN. PUT ON O2 MASK. RECEIVED A LT ENG FLAMEOUT CASS MESSAGE NEXT. RAN QRSDR J7SA2026080400510Acm · faultedDURING CRUISE, CREW RECEIVED PACK TEMP HIGH CAS, HEARD A SQUEAL NOISE, AND NOTICED A BURNT SMELL. AIRCRAFT LANDED WITHOUT INCIDENT AT KDPA. FOUND AIR CYCLE MACHINE SEIZED. REPLACED ACM. OPS AND LEAK CHECKS SATISFACTORY. WORK COMPLETED IAW CL350 AMM 21-52-13.SDR DXTA2026070708681Light Sys · malfunctionedSEAT 4R RED AND WHITE EMERGENCY LIGHTS REMAIN ILLUMINATED SHINING ONTO THE FLOOR WITH THE EMER LIGHTS SWITCH IN THE OFF POSITION. TROUBLESHOT 4R EMERGENCY LIGHT. DISCOVERED THAT WHEN EMERGENCY LIGHTS ARE COMMANDED, SEAT ACCENT LIGHT ILLUMINATES,& EMERGENCY LISDR DXTA2026070608657Switch · failedINTERIOR EMERGENCY LIGHTS ABOVE SEAT 2L AND 3R DO NOT ILLUMINATE WHEN EMER LIGHT SWITCH IS PLACED TO ON. LIGHTS ILLUMINATE NORMALLY WITH CABIN LIGHT SWITCH TO ON.SDR 2026FA0000554Flap System · failedFLAP FAIL CAS MESSAGE AFTER TAKEOFF WHEN RETRACTING FLAPS. FLAPS WERE SELECTED 0 BUT REMAINED AT 10DEGREES. SAME ISSUE HAD OCCOURED ON N545DL MUTIPLE TIMES. FLAP RESET WORKED AND TESTED GOOD.SDR 3EJA20260814001Wheel · failedLOST RIGHT MAIN INBOARD TIRE ASSEMBLY AFTER ROTATION FROM TJSJ.////// REPLACED RH MLG AND BOTH MAIN WHEEL ASSY.SDR DXTA2026062908584Bleed Air Sys · contaminatedNOTICED AN OILY BURNING SMELL IN THE AFT CABIN AFTER AIRCRAFT SHUTDOWN. PERFORMED CLEANING PROCEDURE FOR OIL IN THE BLEED AIR SYSTEM AND THE AIR CONDITIONING PACK IAW LIEBHERR-AEROSPACE SIL LS_CL300_01 REV. NO: 1 DATED AUG 07/19. NO DEFECTS NOTED, NO "BAD ODSDR 3EJAN631RP062126Seal · wornL BLEED LEAK RED CAS MESSAGE. RAN CHECKLIST AND LIGHT EVENTUALLY EXTINGUISHED. REMOVED AND REPLACED SEALS FOR BOTH PACK FLOW CONTROL VALVE. FOUND BLEED LEAK REPORT POINTS TO AREA AROUND
LEFT-INTERMEDIATE VALVE. FOUND VALVE LEAKING REINSTALLED INBD CLAMP. PESDR DXTA2026062408526Warning Message · illuminatedAFTER TAKEOFF AND SELECTING GEAR UP THE AMBER GEAR DISAGREE AND CYAN PROX SYS FAULT DISPLAYED ALONG WITH LT GEAR SHOWING EXTENDED WITH THE GEAR HANDLE IN THE UP POSITION. COMPLIED WITH CHECKLIST AND DIVERTED TO KIAD WITH NO FURTHER ISSUES. INTERROGATED THESDR 2026F00149Skin · damagedCOMPLIED WITH THE REPAIR LOCATED ON THE RIGHT SIDE OF THE FUSELAGE BETWEEN FS 384 & FS 422 I.A.W. ENGINEERING DWG SA-CL300-20160-M01 REV. IR,SDR DXTA2026061708450Elec Connector · inoperativeTOP EXIT SIGN LIGHT INOP BOTTOM IS ON. BEGAN TROUBLESHOOTING. POWERED UP AIRCRAFT AND PERFORMED OPS CHECKS OF INTERIOR EMERGENCY LIGHTS. FOUND THE TOP EXIT SIGN LIGHT AT THE EMERGENCY EXIT INOP. GAINED ACCESS TO CONNECTION AND FOUND CONNECTOR AT THE LIGHT ASSSDR DXTA2026052608193Engine · failedON CLIMBOUT SHORTLY AFTER TAKEOFF, RECEIVED A STRONG VIBRATION FOLLOWED BY A L ENG EXCEEDANCE CAS & A OVERTEMP ON ITT. REDUCED THUST LEVER TO BRING ITT DOWN. RECEIVED A LT ENG VIBRATION CAS FOLLOWED BY A LT ENG FLAMEOUT CASS. VIBRATION DECREASED BUT NEVER WENSDR DXTA2026052608187Latch · contaminatedAFTER COMPLETING THE FINAL WALK AROUND AND WALKING UP THE MAIN ENTRY DOOR STAIRS, LOCKING HANDLE POPPED OUT OF THE OPEN POSITION CAUSING THE DOOR TO MOVE DOWNWARD FORCING THE BOTTOM OF THE DOOR INTO FUSELAGE SKIN CAUSING 3 SCUFF MARKS. RETURNED HANDLE TO OPENSDR DXTA2026051808102Power Supply · inoperativeON-SITE TECHS REPORTS THE EMERGENCY LIGHTS ARE ON. CORRECTIVE ACTION: REMOVED #1 EMERGENCY POWER SUPPLY UNIT PN: RPS1-B SN: 28422 DUE TO FAULTY, AND INSTALLED NEW #1 EMERGENCY POWER SUPPLY UNIT PN: RPS1-B SN: 34030. REMOVED #2 EMERGENCY POWER SUPPLY UNIT PN: R
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