# Service difficulty reports: Bombardier BD-700-1A10

A list on [Bombardier BD-700-1A10](https://openairdocs.org/model/bombardier-bd-700-1a10.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 8 · 370 reports

- [SDR DXTA2026102310269](https://openairdocs.org/sdr/DXTA2026102310269.md): Controller · faulty · Oct 19, 2026 · N162QS · Bombdr BD7001A10 · Passenger/Crew Doors
  > CABIN DOOR POWER ASSIST MOTOR STARTED CYCLING ON AND OFF AS WE TAXIIED OUT. WHEN YOU GO TO OPEN DOOR, THE MOTOR WOULD CYCLE ON - UNCOMMANDED- AND THE DOOR WOULD TRY AND CLOSE ITSELF. THIS CYCLE WOULD HAPPEN REPEATEDLY. AVIONICS BATTERY WAS DISCONNECTED TO KEEP
- [SDR DXTA2026100510001](https://openairdocs.org/sdr/DXTA2026100510001.md): Sign · inoperative · Oct 2, 2026 · N158QS · Bombdr BD7001A10 · Emergency Lighting
  > INTERIOR LIGHTED EMER EXIT SIGN LOCATED BELOW OVER WING EXIT, NEXT TO THE FLOOR IS INOP. REMOVED AND REPLACED LOWER EMER EXIT BELOW OVER WING EXIT DUE TO BEING INOP WITH CUSTOMER SUPPLIED NEW ONE AND CHARGED EMER POWER SUPPLY BATTERY OPS CHECKS GOOD IAW AMM 3
- [SDR 4T1R00002](https://openairdocs.org/sdr/4T1R00002.md): Spigot · corroded · Oct 2, 2026 · N925G · Bombdr BD7001A10 · Flight Control System
  > DURING THE BORESCOPE INSPECTION OF THE INBOARD FLAP INTERNAL STRUCTURE PER AMM 57-51-00-290-801, STEP F.(3), CORROSION WAS IDENTIFIED INSIDE THE AFT SPIGOT TUBE INNER BORE ON THE RIGHT-HAND INBD. FLAP. REFERENCE BOMBARDIER REPAIR ENGINEERING ORDER 700-57-51-53
- [SDR 4T1R20261005001](https://openairdocs.org/sdr/4T1R20261005001.md): Spigot · corroded · Oct 2, 2026 · N925G · Bombdr BD7001A10 · Trailing Edge Flaps
  > DURING THE BORESCOPE INSPECTION OF THE INBOARD FLAP INTERNAL STRUCTURE PER AMM 57-51-00-290-801, STEP F.(3), CORROSION WAS IDENTIFIED INSIDE THE AFT SPIGOT TUBE INNER BORE ON THE LEFT-HAND INBD FLAP.REFERENCE BOMBARDIER REPAIR ENGINEERING ORDER 700-57-51-535
- [SDR DXTA2026092809858](https://openairdocs.org/sdr/DXTA2026092809858.md): Window · defective · Sep 23, 2026 · N155QS · Bombdr BD7001A10 · Windshield/Door Rain/Ice Removal
  > L WINDOW HEAT FAIL AMBER CAS ILLUMINATED IN CRUISE FLIGHT AT FL450. COMPLETED QRH CHECKLIST ISOLATING THE L WINDOW HEAT CHANNEL BY PULLING CB F11. SMALL CRACK BETWEEN PANES APPEARS FROM FAULT POINT NEAR WINDOW FRAME REMOVED DEFECTIVE COCKPIT LH SIDE WINDOW AND
- [SDR DXTA2026082409378](https://openairdocs.org/sdr/DXTA2026082409378.md): Engine · unknown · Aug 21, 2026 · N148QS · Bombdr BD7001A10 · Engine (Turbine/Turboprop)
  > AT ABOUT 200-300 FT AGL ON TAKEOFF, TOWER INFORMED SAW SMOKE COMING FROM ONE ENG. DEPARTED RUNWAY 12 AT KTUS WHICH PUT RT ENG ON TOWER SIDE, BUT TOWER COULD NOT TELL WHICH ENG SMOKE COMING FROM. THEY ALSO DID NOT DESCRIBE THE SMOKE IN ANY MANNER. RETURNED T
- [SDR DXTA2026082009338](https://openairdocs.org/sdr/DXTA2026082009338.md): Warning Light · false activation · Aug 18, 2026 · N158QS · Bombdr BD7001A10 · Aircraft Fuel Distribution System
  > ON TAKEOFF APPROXIMATELY 70KTS CENTER FUEL TRANSFER FAIL AMBER CAS MESSAGE ILLUMINATED. TAKEOFF ABORTED. PERFORMED OPERATIONAL TEST OF THE CENTER TRANSFER PUMPS IAW AMM 28-22-00. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED.
- [SDR DXTA2026081409263](https://openairdocs.org/sdr/DXTA2026081409263.md): Wire Harness · multiple fail · Aug 12, 2026 · N151QS · Bombdr BD7001A10 · Door System Wiring
  > AFTER TAKEOFF CARGO DOOR CAS MESSAGE ILLUMINATED AND CAB ALT ROSE. LEVELED AT 4000FT AT WHICH POINT THE CARGO DOOR LIGHT WENT OUT. CABIN CONTINUED TO RISE TO 4000FT. RETURNED TO PDK UNEVENTFULLY. WILL LEAVE DOOR AS IS. REMOVED BROKEN BAGGAGE DOOR LOCKED PR
- [SDR DXTA2026071308774](https://openairdocs.org/sdr/DXTA2026071308774.md): Light · detached · Jul 10, 2026 · N143QS · Bombdr BD7001A10 · Flight Compartment Lighting
  > CAPT'S MAP READING LIGHT IS DETACHED AND DANGLING FROM ITS WIRES. IT SPARKS AND SMOKES WHEN TURNED ON OR MOVED. REMOVED AND REPLACED CAPT'S MAP READING LIGHT DUE TO BEING BROKEN WITH CUSTOMER SUPPLIED NEW ONE OPS CHECKS GOOD.
- [SDR DXTA2026060108251](https://openairdocs.org/sdr/DXTA2026060108251.md): Autobrake Sys · defective · May 28, 2026 · N167QS · Bombdr BD7001A10 · Landing Gear Brake System
  > AFTER TAKEOFF R MAIN GEAR DID NOT FULLY RETRACT AND NOSE GEAR DOOR DID NOT CLOSE CAUSING VIBRATIONS. DURING GEAR UP WE HAD NORMAL INDICATION ON NOSE AND LEFT MAIN AND RIGHT MAIN HAD YELLOW HATCHED INDICATION. RECEIVED 4 YELLOW CAS MESSAGES "GEAR DISAGREE" "NOS
- [SDR 2026FA0000466](https://openairdocs.org/sdr/2026FA0000466.md): Display · failed · May 28, 2026 · N807DC · Bombdr BD7001A10 · Central Display
  > IN RESPONSE TO YOUR REQUEST, PLEASE FIND BELOW A DETAILED PILOT-IN-COMMAND (PIC) REPORT REGARDING THE EVENT THAT OCCURRED ON MAY 10, 2026, INVOLVING LEARJET 60, N269GJ. FOLLOWING THE OCCURRENCE, I ALSO REVIEWED THE EVENT WITH BOTH FLIGHT CREWMEMBERS IN MY CAPA
- [SDR DXTA2026052708212](https://openairdocs.org/sdr/DXTA2026052708212.md): Engine · failed · May 24, 2026 · N168QS · Bombdr BD7001A10 · Engine (Turbine/Turboprop)
  > DURING CRUISE AT FL430, HEARD A LOUD NOISE, SOUNDED LIKE GRINDING/SIEZING, SHORTLY BY COCKPIT FILLED WITH SMOKE. COMPLIED WITH MEMORY ITEMS & CHECKLISTS. RT FADEC FAILED ALONG WITH RT ENG & AN INTENSE VIBRATION THAT CAUSED OVERHEAD PANELS TO FALL. CONTINUE
- [SDR 2026FA0000426](https://openairdocs.org/sdr/2026FA0000426.md): Stall Warning · false indication · May 11, 2026 · N228SS · Bombdr BD7001A10 · Stall Warning System
  > AT 190 KNOTS ASKED FOR CLEAN WING AUTO PILOT ON. SHORTLY AFTER THAT SELECTION AND CLOSE TO 200 KNOTS INDICATED AIRSPEED THE STICK SHAKER WENT OFF ALONG WITH THE AURAL WARNING "STALL, STALL, STALL" WE LEVELED OFF AT AROUND 3700 FEET MSL AND CONFIRMED THE AUTOPI
- [SDR DXTA2026043007825](https://openairdocs.org/sdr/DXTA2026043007825.md): Wire Harness · failed · Apr 28, 2026 · N152QS · Bombdr BD7001A10 · Door System Wiring
  > WE HAD A CARGO DOOR WARNING ON WE CLOSED THE DOOR 3 TIMES AND CHECKED THE VENT DOOR ON THE OUTSIDE AND EVERYTHING LOOKED CLOSED. HOWEVER AFTER AIRBORNE WE LOST PRESSURIZATION AND RETURNED BACK TO THE FIELD. AFTER TOTAL RESET THE CARGO DOOR WARNING REMAINED
- [SDR DXTA2026031107170](https://openairdocs.org/sdr/DXTA2026031107170.md): Receptacle · broken · Mar 8, 2026 · N146QS · Bombdr BD7001A10 · Landing Gear Position and Warning
  > AFTER TAKEOFF GEAR WOULD NOT RETRACT. CYCLED ONCE STILL WOULD NOT RETRACT. WHEN GEAR HANDLE WAS UP WE GOT AN AMBER CAS GEAR DISAGREE. PUT GEAR HANDLE DOWN AND CONTINUED SHORT FLIGHT. REVIEWED PREVIOUS STEPS AND PROCEEDED WITH THE FOLLOWING; GAINED ACCESS TO
- [SDR DXTA2026021606891](https://openairdocs.org/sdr/DXTA2026021606891.md): Relay · faulted · Feb 13, 2026 · N164QS · Bombdr BD7001A10 · Passenger/Crew Doors
  > MAIN CABIN DOOR AUTOMATIC CLOSING MODE INOP. BOTH EXTERIOR & INTERIOR AUTO SWITCHES WILL NOT CLOSE DOOR. DOOR CLOSES NORMALLY USING THE MANUAL EXTERIOR SWITCH. REMOVED AND REPLACED RDE NR 1 IAW SMM 44-10-52. OPS CHECKED NO DEFECTS NOTED. MAIN CABIN DOOR AUT
- [SDR E0YA20260430001](https://openairdocs.org/sdr/E0YA20260430001.md): Controller · odor · Feb 8, 2026 · N54DP · Bombdr BD7001A10 · Windshield/Door Rain/Ice Removal
  > L WINDSHIELD HEAT FAIL CAS MESSAGE FOLLOWED BY BURNING SMELL.
- [SDR DXTA2026012106601](https://openairdocs.org/sdr/DXTA2026012106601.md): Transducer · faulted · Jan 19, 2026 · N164QS · Bombdr BD7001A10 · Landing Gear Brake System
  > REPEAT WRITE UP. AFTER LOWERING MLG, AMBER AUTOBRAKE FAIL CASS MESSAGE ILLUMINATED ACCOMPANIED BY CYAN BRAKE FAULT CASS MESSAGE. MAINT FAULT CODE 3246015HA DISPLAYED IN FMS OF MAINT PAGE. COULD NOT DUPLICATE. NO FAULT MESSAGES ON POWER UP. RAN ENGS & HYD POWE
- [SDR DXTA2026010906458](https://openairdocs.org/sdr/DXTA2026010906458.md): Distribution Box · faulty · Jan 6, 2026 · N163QS · Bombdr BD7001A10 · Ice/Rain Protection System Wiring
  > IN FLIGHT WE GOT A CYAN R PROBE MON FAIL MESSAGE, WHICH THEN TRIGGERED THREE AMBER CAS MESSAGES: R AOA HEAT FAIL, PITOT 2 HT FAIL AND STBY PITOT HT FAIL. THIS ALL BEGAN WHEN THE HBMU 2 CIRCUIT BREAKER TRIPPED ON THE EMS-CDU. T/S SYSTEM, REMOVED SUSPECTED HB
- [SDR DXTA2026010706444](https://openairdocs.org/sdr/DXTA2026010706444.md): Anti-Ice Valve · faulty · Jan 5, 2026 · N164QS · Bombdr BD7001A10 · Engine Anti-Icing System
  > AFTER TAKEOFF AND DURING CLIMB OUT THE ANTI-ICE SYSTEMS WERE SELECTED ON (IN ICING CONDITIONS). THE CYAN "L COWL A/ICE FAULT" CAS CAME ON. CHECKLIST PROCEDURES WERE NOTED. THE ANTI-ICE BLEED SYNOPTIC SHOWED THE LEFT ENGINE ANTI-ICE BLEED VALVE IN AMBER WHIL
- [SDR DXTA2025120805965](https://openairdocs.org/sdr/DXTA2025120805965.md): Drain · venting · Dec 4, 2025 · N164QS · Bombdr BD7001A10 · Fuel Storage
  > ENROUTE IT WAS NOTED THAT THE ACFT KEPT BALANCING FUEL & FMS POSTED A FUEL QTY DISAGREE. STARTED WITH AN OVERAGE OF 1500 LBS, DEGRADED TO 3500LB DEFICIT. LT TANK HIGHER LOSS THAN RT TANK. RATE OF LOSS INCREASING. POST FLT, FUEL DRIPPING ALL ALONG AFT FUSE.
- [SDR 3J7R2025120500001](https://openairdocs.org/sdr/3J7R2025120500001.md): Power Supply · inoperative · Dec 4, 2025 · N163QS · Bombdr BD7001A10 · Emergency Lighting
  > EXIT SIGN ON FWD BULKHEAD IN THE CABIN ABOVE SEAT 1 INOPERATIVE.
- [SDR JGVR20251104001](https://openairdocs.org/sdr/JGVR20251104001.md): Skin · corroded · Nov 4, 2025 · N142QS · Bombdr BD7001A10 · Wing, Plate/Skin
  > REPAIRED CORRODED AREA OF LH LOWER WING SKIN NEAR CWS 537.40 BY BLENDING AREA, PERFORMING NDT, REPORTING FOR REPAIR DISPOSITION, FABRICATING AND INSTALLING REPAIR DOUBLER IN ACCORDANCE WITH ENGINEERING REPAIR ORDER.
- [SDR DXTA2025102005329](https://openairdocs.org/sdr/DXTA2025102005329.md): Actuator · failed · Oct 15, 2025 · N163QS · Bombdr BD7001A10 · Passenger/Crew Doors
  > WHILE CLOSING MED DOOR, SOMETHING CAME LOOSE & ENTIRE DOOR CAME SLAMMING DOWN. MX CORRECTED THE PAX DOOR DISCREPANCY BY REMOVING UNSERVICEABLE DOOR ACTUATOR & REPLACING IT WITH A REPAIRED SERVICEABLE UNIT IAW AMM 52-11-25-400-801, FOLLOWED BY FULL RIGGING OF
- [SDR DXTA2025101305237](https://openairdocs.org/sdr/DXTA2025101305237.md): Probe · defective · Oct 8, 2025 · N148QS · Bombdr BD7001A10 · Fuel Indicating System
  > DURING FLT, AMBER FUEL IMBALANCE CAS MESSAGE CAME ON IMMEDIATELY, RT SIDE INCREASE BY 2900 LBS. TOTAL FUEL ALSO INCREASED BY 2900 LBS. FOLLOWED QRH FUEL IMBALANCE. FUEL IMBALANCE BEGAN TO CORRECT. IMBALANCE CONINTUED TO CORRECT & STOPPED. TOTAL FUEL BEGAN
- [SDR DXTA2025081504613](https://openairdocs.org/sdr/DXTA2025081504613.md): Fuel Sys · out of balance · Aug 15, 2025 · N148QS · Bombdr BD7001A10 · Aircraft Fuel Distribution System
  > THE FUEL QUANTITY INDICATED ON RIGHT GAUGE WAS SHOWING A COUPLE THOUSAND POUNDS MORE THAN IT ACTUALLY HAD. THE RESULT WAS INACCURATE FUEL TRANSFERRING LEADING TO FUEL IMBALANCE. THIS HAPPENED FOR 2 HOURS AND THEN RETURNED BACK TO NORMAL INDICATIONS. TROUBLE
- [SDR DXTA2025080404427](https://openairdocs.org/sdr/DXTA2025080404427.md): Door · leaking · Jul 31, 2025 · N157QS · Bombdr BD7001A10 · Passenger/Crew Doors
  > LOUD SQUEAL FROM DOOR DURING CLIMB. STARTED AT 15000 FT, DELTA P 6.15, CABIN ALT 500FT. ENDED AT 20000 FT, DELTA P 7.45, CABIN ALT 900FT. NOT DURING DECENT.. PRESSURIZATION INDICATIONS NORMAL. REPEAT WRITE-UP. PERFORMED GVI OF PAX DOOR SEAL & NO DAMAGE NOTED
- [SDR JGVR2025072800528](https://openairdocs.org/sdr/JGVR2025072800528.md): Manual · inaccurate · Jul 28, 2025 · N44GX · Bombdr BD7001A10 · Standard Practices/Structures
  > THE AMM PROCEDURE FOR THE GROUND SLATS DOES NOT SPECIFY IN THE PROCEDURE THE DIRECTION OF THE BOLT HEAD AND SPACER. THE ILLUSTRATION ASSOCIATED WITH THE TASK COVERS ONLY ONE SIDE OF THE AIRCRAFT AND IS NOT THE EASIEST TO READ PERTAINING TO THE BOLT ORIENTATION
- [SDR 2025FA0000456](https://openairdocs.org/sdr/2025FA0000456.md): Skin · cracked · Jul 8, 2025 · N9506G · Bombdr BD7001A10 · Nacelle/Pylon, Plate/Skin
  > FIXED COWL SKIN HAS TWO SECTIONS OF TORN AND CURLED SKIN AROUND FRONT MOUNT BEAM.
- [SDR DXTA2025070104077](https://openairdocs.org/sdr/DXTA2025070104077.md): Battery Pack · inoperative · Jun 28, 2025 · N164QS · Bombdr BD7001A10 · Emergency Lighting
  > GALLEY FORWARD EMERGENCY EXIT SIGN AND FORWARD EMERGENCY LIGHT FLASH INTERMITTENTLY, AND AFT GALLEY EMERGENCY LIGHT INOP WHEN COCKPIT EMERGENCY LIGHT SWITCH IS IN ON POSITION. CORRECTIVE ACTION; REPLACED #1 & #2 ELPS INTERNAL BATTERY PACKS IAW GL6000 MM 33-51-
- [SDR DXTA2025062704032](https://openairdocs.org/sdr/DXTA2025062704032.md): Seal · leaking · Jun 24, 2025 · N150QS · Bombdr BD7001A10 · Passenger/Crew Doors
  > INFLIGHT AT FL430, LOUD CONTINUOS NOISE FROM MAIN ENTRY DOOR. OCCAISIONAL LOUD RASPING NOISE. CABIN ALTITUDE WAS STEADY AT 4100', CABIN PSI DIFFERENTIAL WAS HOLDING AT 7.5. NOISE DID NOT START TILL WE REACHED FL430. CALLED MCC FOR HISTORY. MCC STATED NO RECEN
- [SDR DXTA2025060903796](https://openairdocs.org/sdr/DXTA2025060903796.md): Door · unknown · Jun 6, 2025 · N154QS · Bombdr BD7001A10 · Passenger/Crew Doors
  > MAIN CABIN DOOR WOULD NOT CLOSE ON 2 ATTEMPTS. MOTOR WORKED FINE. IT CLOSED FROM INSIDE ON 3RD ATTEMPT. DOOR IS CURRENTLY CLOSED. EXIT AIRCRAFT BY CARGO DOOR. INSPECTED MAIN CABIN DOOR ACTUATOR, CHAIN, TENSATOR SPRINGS AND ALL WORKING PARTS WITH NO DEFECT
- [SDR DXTA2025052703607](https://openairdocs.org/sdr/DXTA2025052703607.md): Rde · contaminated · May 22, 2025 · N162QS · Bombdr BD7001A10 · Passenger/Crew Doors
  > ENTRANCE DOOR CYCLES PART WAY UP & DOWN WITH POWER ON THE ACFT POWERED DOWN. DOOR IS LATCHED CLOSED, MOTOR STILL CYCLES ON & OFF. LIGHTS & SHADES FLICKERING. CYCLED DOOR SEVERAL TIMES NO DEFECTS. POWERED ACFT & CYCLED DOOR, NO DEFECTS. PERFORMED GVI & FOUND
- [SDR DXTA2025052303581](https://openairdocs.org/sdr/DXTA2025052303581.md): None · none · May 21, 2025 · N162QS · Bombdr BD7001A10 · Standard Practices/Structures
  > AFTER TAKEOFF AND GEAR UP WE EXPERIENCED MODERATE TURBULENCE IN A TURN WHILE THE SLATS AND FLAPS WERE RETRACTING. AIRSPEED SPIKED TO 211/212 MAX WHILE THEY WERE RETRACTING. PERFORMED UNSCHEDULE OVERSPEED CONDITION INSPECTION AND NO DEFECTS FOUND AT THIS TIME
- [SDR DXTA2025050703384](https://openairdocs.org/sdr/DXTA2025050703384.md): Motor · failed · May 7, 2025 · N168QS · Bombdr BD7001A10 · Passenger/Crew Doors
  > MAIN DOOR MOTOR: WHEN RAISING THE MAIN CABIN DOOR USING THE AIR STAIR DOOR SWITCH FROM INSIDE THE CABIN. THE DOOR RAISES NORMALLY. BUT AFTER LOWERING THE LOCKING HANDLE TO THE LOCKED POSITION. THE MOTOR (THAT I ASSUME OPERATES, THE LOCKING PINS) RUNS WHAT I CO
- [SDR DXTA2025050203304](https://openairdocs.org/sdr/DXTA2025050203304.md): Wire Harness · faulted · Apr 30, 2025 · N163QS · Bombdr BD7001A10 · Navigation System Wiring
  > AIR DATA COMPUTER: AFTER TAKEOFF WINDSHEAR ON THE PFD DISPLAYED FOLLOWED BY AUTO THROTTLES OFF AND THE AUTO PILOT WOULD NOT RE-ENGAGE. BOTH PFDS HAD MULTI FAILURES AND THEN BEGAN FLASHING AND SWITCHING BETWEEN SVS ON AND OFF. AFTER TURNING OFF SVS SOME OF T
- [SDR DXTA2025050203306](https://openairdocs.org/sdr/DXTA2025050203306.md): Heater · faulted · Apr 30, 2025 · N152QS · Bombdr BD7001A10 · Windshield/Door Rain/Ice Removal
  > L WINDOW HEAT FAIL AMBER CAS: L WINDOW HEAT FAIL CAS MESSAGE APPEARED IN CRUISE FLIGHT 41000 FT. CREW FOLLOWED QRH PROCEDURES, UNABLE TO RESET, AND LEFT THE CIRCUIT BREAKER PULLED (CCBP F-11) AS DIRECTED BY THE PROCEDURE CORRECTIVE ACTION: VERIFIED DISCREPANC
- [SDR J7SA2025032700000](https://openairdocs.org/sdr/J7SA2025032700000.md): Engine · power loss · Mar 23, 2025 · N93FX · Bombdr BD7001A10 · Engine (Turbine/Turboprop)
  > DURING CLIMB THE #2 ENGINE ROLLED BACK APPROXIMATELY 0.2-0.3 EPR. POWER RESTORED WITHIN 2-3 SECONDS WITHOUT ANY CAS MESSAGES OR UNUSUAL PARAMETERS NOTED. APPROXIMATELY 2 MINUTES LATER, #2 ENGINE ROLLED BACK AGAIN BY 0.2-0.3 EPR AND RESTORED WITHIN 2-3 SECONDS,
- [SDR DXTA2025031902731](https://openairdocs.org/sdr/DXTA2025031902731.md): Controller · defective · Mar 16, 2025 · N156QS · Bombdr BD7001A10 · Windshield/Door Rain/Ice Removal
  > DURING TAXI OUT, R WSHLD HEAT FAIL CAS ILLUMINATED FOLLOWED BY A STRONG BURNING SMELL. SMELL WAS NOTICEABLE IN GALLEY AND CABIN. FAULT CODE: 3041012IN CORRECTIVE ACTION; REMOVED BULKHEAD COVERS BEHIND PILOT AND COPILOT SEAT!; AND INSPECTED. FOUND STRONG ODOR
- [SDR DXTA2025021402340](https://openairdocs.org/sdr/DXTA2025021402340.md): Actuator · defective · Feb 12, 2025 · N160QS · Bombdr BD7001A10 · Passenger/Crew Doors
  > MAIN DOOR: MAIN ENTRY DOOR IS OPEN WITH THE BOTTOM STEP EXTENDED AND WILL NOT CLOSE. AUTO FUNCTION WILL NOT WORK. CANNOT BE ACTUATED BY EITHER INTERIOR SWITCH OR EXTERIOR SWITCH (MANUAL OR AUTO). WHILE ATTEMPTING TO MANUALLY CLOSE THE DOOR WITHOUT THE MOTOR AS
- [SDR DXTA2025012702075](https://openairdocs.org/sdr/DXTA2025012702075.md): Door · damaged · Jan 22, 2025 · N163QS · Bombdr BD7001A10 · Landing Gear Doors
  > AFTER GEAR RETRACTION, FOUND NLG AFT DOOR DAMAGED. CORRECTIVE ACTION: REPLACED DOOR. OPS CHECK GOOD. IAW BOMBARDIER GL6000 AMM 32-22-05-000-801.
- [SDR DXTA2025012202055](https://openairdocs.org/sdr/DXTA2025012202055.md): Strut · discharged · Jan 20, 2025 · N164QS · Bombdr BD7001A10 · Nose/Tail Landing Gear Strut/Axle
  > NLG STRUT: NOSE GEAR STRUT IS FLAT AND STARTED TO BOTTOM OUT ON TAXI. CORRECTIVE ACTION: NOSE STRUT SERVICED. OPS CHECK GOOD. IAW GLOBAL 6000 AMM 12-15-00
- [SDR DXTA2024121601503](https://openairdocs.org/sdr/DXTA2024121601503.md): Hand Rail · detached · Dec 12, 2024 · N141QS · Bombdr BD7001A10 · Passenger/Crew Doors
  > MAIN ENTRANCE HAND RAIL DETACHES AND INTERFERES WITH MAIN ENTRY DOOR OPERATION WHEN DOOR IS RAISED FOR CLOSING. CORRECTIVE ACTION; INSPECT THE AREA AND FOUND THE MISSING SCREW ON THE RANDRAIL EXTENSION LOWER ATTACHING PIVOT FITTING REINSTALLED THE SCREW OPERAT
- [SDR DXTA2024121101446](https://openairdocs.org/sdr/DXTA2024121101446.md): Hand Rail · failed · Dec 8, 2024 · N146QS · Bombdr BD7001A10 · Passenger/Crew Doors
  > ENTRANCE STAIR HAND RAIL: HAND RAIL HAS COME APART AT TOP OF THE STAIR. LEFT HAND SIDE ENTERING AIRCRAFT. THERE IS A SCREW MISSING EXTRACTED BROKEN SCREW FROM CABIN DOOR HANDLE EXTENSION. INSTALLED SCREW AS REQUIRED. P/N: MS24693-C23. OPS CHECKED GOOD. REF G
- [SDR DXTA2024120501358](https://openairdocs.org/sdr/DXTA2024120501358.md): Unknown · odor · Dec 1, 2024 · N141QS · Bombdr BD7001A10 · Air Distribution System
  > CABIN POWER (60 HZ): ON TAXI IN AND AFTER ENGINE SHUTDOWN A BURNING ELECTRICAL SMELL CAME FROM THE CABIN. THE SMELL WAS STRONGEST IN THE AFT LAV AREA WITH VISABLE SMOKE. THE SMELL AND SMOKE DISSIPATED ONCE CABIN POWER WAS TURNED OFF AND EVEN MORE AFTER THE AP
- [SDR DXTA2024120201299](https://openairdocs.org/sdr/DXTA2024120201299.md): Battery · defective · Nov 26, 2024 · N156QS · Bombdr BD7001A10 · Emergency Lighting
  > CABIN EMERG LIGHTS IN AFT CABIN WILL NOT EXTINGUISH WITH EMER SWITCH IN OFF POSITION. REMOVED FAULTY ELPS #5 AND REPLACED WITH NEW ELPS. PERFORMED SEVERAL OPERATIONAL / CHECKS WITH SATISFACTORY RESULTS. IAW AMM 33-51-09 AND 33-51-50
- [SDR 2024FA0000934](https://openairdocs.org/sdr/2024FA0000934.md): Pressure Blkhd · cracked · Nov 26, 2024 · N77NZ · Bombdr BD7001A10 · Fuselage Main, Bulkhead
  > REAR PRESSURE BULKHEAD AND SUPPORTING STRUCTURE FOUND CRACKED DURING SCHEDULED INSPECTION.
- [SDR Z7VAN378LT352](https://openairdocs.org/sdr/Z7VAN378LT352.md): Bleed Air Sys · leaking · Nov 24, 2024 · N378L · Bombdr BD7001A10 · Fire Protection System
  > DURING PRE-FLIGHT CHECKS ON THE GROUND WITH THE APU RUNNING, A "FIRE BOTTLE 2 LO PRESS" INDICATION FOLLOWED BY A "FIRE BOTTLE 1 LO PRESS" INDICATION APPEARED IN THE FLIGHT DECK. NO FIRE OCCURRED ON THE AIRCRAFT. IT WAS FOUND THAT THE AFT CLAMP ON THE LH FLOW C
- [SDR DXTA2024112701264](https://openairdocs.org/sdr/DXTA2024112701264.md): Gate · out of alignment · Nov 24, 2024 · N162QS · Bombdr BD7001A10 · Passenger/Crew Doors
  > MAIN DOOR VENT FLAP NOT ALIGNED, NOT SEALED AFTER TAKE OFF. CLEANED AND LUBRICATED SEAL PERFORMED SEVERAL OPS CHECK OF THE MAIN DOOR WITH NO DEFECTS NOTED. PERFORMED IAW BOMBARDIER GLOBAL 6000 MM CH 52·11·69.
- [SDR DXTA2024112601261](https://openairdocs.org/sdr/DXTA2024112601261.md): Light · malfunctioned · Nov 24, 2024 · N156QS · Bombdr BD7001A10 · Emergency Lighting
  > CABIN EMERGENCY LIGHTS IN AFT PASSENGER COMPARTMENT WILL NOT EXTINGUISH WITH EMER LIGHT SWITCH IN OFF POSITION. AFTER GAINING ACCESS TO AND ENTERING CABIN THERE WERE NO EMERGENCY LIGHTS ON. POWERED AIRCRAFT, STILL NO EMERGENCY LIGHTS ON. GAINED ACCESS TO AFT

Next page: https://openairdocs.org/model/bombardier-bd-700-1a10/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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 = 'BD7001A10'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/bombardier-bd-700-1a10/reports

---
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