# Service difficulty reports: BMW Rolls BR700-710A220

A list on [BMW Rolls BR700-710A220](https://openairdocs.org/engine/bmw-rolls-br700-710a220.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 4 · 189 reports

- [SDR U5QA202610020182](https://openairdocs.org/sdr/U5QA202610020182.md): Engine · flamed out · Oct 2, 2026 · N500VJ · Bombdr BD7001A11 · Engine (Turbine/Turboprop)
  > DURING 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 RENTAL
- [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 DXTA2026060408300](https://openairdocs.org/sdr/DXTA2026060408300.md): Fmu · failed · May 31, 2026 · N100QS · Bombdr BD7001A11 · Fuel Control/Turbine Engines
  > WHILE 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 TU
- [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 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 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 2024F00136](https://openairdocs.org/sdr/2024F00136.md): Module · false indication · May 17, 2024 · N412PB · Bombdr BD7001A11 · Air Data Computer
  > ON CLIMB OUT THE CREW REPORTED THAT ALL ADC'S FAILED (CAS MSG.) CREW REPORTED AN EMERGENCY AND DIVERTED TO KPDX.
- [SDR 7ORR2024031418598](https://openairdocs.org/sdr/7ORR2024031418598.md): Blade · broken · Mar 14, 2024 · Bombdr BD7001A10 · Turbine Section
  > DURING POST LEASE MAINTENANCE VISIT, A CUSTOMER REQUESTED BORESCOPE OF HPT STAGE 1 ROTOR BLADES WAS ACCOMPLISHED. DAMAGE WAS FOUND TO BE IN EXCESS OF SERVICEABLE LIMITS FOR HPT STAGE 1 ROTOR BLADES. UPON FURTHER EXAMINATION, SECONDARY DAMAGE WAS ALSO NOTED ON
- [SDR 85LY20230623223](https://openairdocs.org/sdr/85LY20230623223.md): Unknown · unknown · Jun 18, 2023 · N605RP · Bombdr BD7001A10 · Electrical Power System
  > AIRCRAFT N605RP DEPARTED FROM SWITZERLAND TO THE US, DURING THE FLIGHT THE BATTERY HEAT CB POPPED AND WAS NOT ABLE TO BE RESET. ONCE BACK AT BASE T/S WAS CARRIED OUT. FAULT WAS FOUND TO BE A WIRE TRAPPED/CRUSHED UNDER A BATTERY TIE BAR AND THE LINER SPACER KIT
- [SDR CWQA20220825001](https://openairdocs.org/sdr/CWQA20220825001.md): Oil System · leaking · Aug 22, 2022 · N898MJ · Bombdr BD7001A10 · Engine Oil Storage (Airframe Furnished)
  > DURING CRUISE, CREW RECEIVED "R OIL LOW QTY" AMBER MESSAGE, ALL OTHER ENGINE INDICATIONS NORMAL. DUE TO LOCATION AND PROXIMITY TO GANDER, CREW DECIDED TO PERFORM UNSCHEDULED LANDING, CHECKLIST FOLLOWED, EMERGENCY DECLARED, AND LANDED WITHOUT INCIDENT. MESSAGE
- [SDR 2022FA0000326](https://openairdocs.org/sdr/2022FA0000326.md): None · none · Jul 1, 2022 · N28ZD · Bombdr BD7001A10 · Miscellaneous Hardware
  > AIRCRAFT REGISTRATION N28ZD SN 9191 WAS IN MAINTENANCE AND A JACKING PAD WAS FITTED TO LH WING IN ORDER TO DEFUEL THE RH WING. THE JACKING PAD WAS NOT REMOVED BEFORE THE AIRCRAFT WAS RELEASED TO SERVICE. WHEN ENGINEER FITTED THE JACKING PAD THE ENGINEER HAD NO
- [SDR 2022F00238](https://openairdocs.org/sdr/2022F00238.md): Frequency Gen · damaged · May 24, 2022 · Bombdr BD7001A10 · Powerplant System
  > IN FLIGHT A GEN 1 FAIL WARNING MESSAGE APPEARED ON THE CAS, AFTER INSPECTION IT WAS DISCOVERED THAT THE CAUSE WAS A CATASTROPHIC FAILURE OF THE #1 VFG LEADING TO DAMAGE OF SURROUNDING PARTS/COMPONENTS, DEBRIS FROM THE FAILURE WAS FOUND WITHIN THE LH ENGINE COW
- [SDR 1JCA202112221001](https://openairdocs.org/sdr/1JCA202112221001.md): Warning Message · illuminated · Dec 22, 2021 · N871FR · Gulstm GIV · Elevator Control System
  > ENROUTE FROM LSGG-RJAA WITH 4 CREW ON BOARD AND 0 PAX. FL 430 OVER RUSSIA AT TIME 2000Z WE HAD 2 AMBER CAS MESSAGES, L ELEVATOR FAIL AND FCS MAINTENANCE REQUIRED. WE DECLARED A PAN AND AFTER RUNNING CHECKLIST CONCLUDED TO DIVERT FOR LANDING. OUR ALTERNATE UE
- [SDR KKVA20211019002](https://openairdocs.org/sdr/KKVA20211019002.md): Engine · odor · Oct 19, 2021 · N702DR · Bombdr BD7001A10 · Engine (Turbine/Turboprop)
  > EMERGENCY DECLARED AFTER SMOKE FROM BOTH ENGINES WAS REPORTED FROM TOWER AND FUMES WERE PRESENT IN THE COCKPIT. POST INCIDENT OPERATIONAL CHECKS AT 65%, 85% N1 AND FULL POWER PER AMM 71-00-00-866-806 REVEALED NO INTERIOR ODOR OR ENGINE SMOKE EMISSIONS AND NORM
- [SDR M2MR202104080001](https://openairdocs.org/sdr/M2MR202104080001.md): Housing · leaking · Apr 8, 2021 · Bombdr BD7001A10 · Engine Fuel Distribution
  > FUEL LEAK DISCOVERED AFTER OPERATION ON RIGHT ENGINE COWLING. FUEL FILTER HOUSING O-RING WAS FOUND LEAKING. ON REPLACEMENT OF SEAL AND FILTER ONE OF THE COVER FASTENER BOLTS WAS FOUND PULLED OUT OF THE MAIN FILTER HOUSING. REPLACEMENT OF THE ENTIRE FUEL/OIL FI
- [SDR AWKA2020100201](https://openairdocs.org/sdr/AWKA2020100201.md): Switch · failed · Sep 19, 2020 · N503VJ · Bombdr BD7001A11 · Engine Thrust Reverser
  > WHILE ENROUTE TO VNY, FLIGHT CREW RECEIVED A CYAN LEFT REVERSER UNLOCK FAULT CAS MESSAGE. CREW CONSULTED WITH MX CONTROL AND BOMBARDIER TECH SUPPORT VIA SAT PHONE, AND WAS ADVISED THAT IT’S LIKELY A MALFUNCTIONING MICROSWITCH, AND THAT THERE ARE NO OTHER INDI
- [SDR CA190801008](https://openairdocs.org/sdr/CA190801008.md): Contactor · damaged · Jul 29, 2019 · Bombdr BD7001A10 · AC Generation System
  > (CAN) ON AC 9193, CUSTOMER FOUND DURING LH ENGINE SHUT DOWN AC BUS 1 SHED. PER CAIMS READ OUT, THEY GET THE FOLLOWING MESSAGE: ACPC APULC-EPLC CONTACTOR-K1 FAILED. DURING FURTHER TS, THEY FOUND ON THE CAIMS AC SYNOPTIC DATA - ACPC B THE AC BUS 1 WAS STILL CON
- [SDR CA190802003](https://openairdocs.org/sdr/CA190802003.md): Frequency Gen · malfunctioned · Jul 28, 2019 · Bombdr BD7001A10 · AC Generation System
  > (CAN) #3 VFG S/N 6553 FAILURE IN FLIGHT. POST FLIGHT INSPECTION REVEALED THAT THE VFG HOUSING HAS FRACTURED AT THE VFG OIL PUMP FLANGE. (TC# 20190802003)
- [SDR CA190726030](https://openairdocs.org/sdr/CA190726030.md): Tire · failed · Jul 25, 2019 · Bombdr BD7001A11 · Tire
  > (CAN) UNCOMMANDED BRAKE PRESSURE APPLIED TO 1 WHEEL LEAD TO A TIRE BURST DURING LANDING (TC# 20190726030)
- [SDR CA190730014](https://openairdocs.org/sdr/CA190730014.md): Torque Tube · disconnected · Jul 20, 2019 · Bombdr BD7001A10 · Trailing Edge Flap Control System
  > (CAN) DURING POST FLIGHT WALK-AROUND, MAINTENANCE PERSONNEL FOUND THE #3 DRIVE TORQUE TUBE WAS DISCONNECTED FROM THE RH #1 FLAP ACTUATOR. THE ATTACHING/LOCKING BOLT WAS FOUND TO BE ENGAGED IN THE TORQUE TUBE ONLY AND NOT ENGAGED THROUGH THE FLAP ACTUATOR SPLIN
- [SDR 2019FA0000207](https://openairdocs.org/sdr/2019FA0000207.md): Hose · broken · Jul 1, 2019 · N700MH · Bombdr BD7001A11 · Passenger Oxygen System
  > DURING AN AIRCRAFT 10 YEAR INSPECTION THE PASSENGER OXYGEN SYSTEM HAD ALREADY PASSED THE REQUIRED FUNCTIONAL TEST. AFTER THE AIRCRAFT SUBSEQUENT MAIN CABIN AND LAV DISASSEMBLY FOR FURTHER INSPECTION, THE REFERENCED LINE WAS FOUND BROKEN IN TWO PLACES. THIS M
- [SDR CA190702018](https://openairdocs.org/sdr/CA190702018.md): Display · failed · Jun 29, 2019 · Bombdr BD7001A10 · Integrated Flight System
  > (CAN) ENROUTE IN CRUISE PHASE OF FLIGHT, THE PILOT`S PRIMARY FLIGHT DISPLAY (DISPLAY UNIT #1) AND MULTIFUNCTION DISPLAY (DISPLAY UNIT #2) BLANKED OUT AND COULD NOT BE RECOVERED. AT THE SAME TIME, THE AIR DATA INFORMATION ON THE BF GOODRICH ELECTRONIC STANDBY I
- [SDR CA190815010](https://openairdocs.org/sdr/CA190815010.md): Wire · burned · Jun 14, 2019 · Bombdr BD7001A10 · Electrical Power System Wiring
  > (CAN) CUSTOMER REPORTED BURNT WIRES INSIDE THE DCPC. IT APPEAR TO BE FEEDER CABLES TO THE CIRCUIT BREAKER PANEL ON THE DCCP. NO EMERGENCY WAS DECLARED. THEY WERE TROUBLESHOOTING AN ELECTRICAL PROBLEM. (TC# 20190815010)
- [SDR CA190607010](https://openairdocs.org/sdr/CA190607010.md): Hose · damaged · Jun 5, 2019 · Bombdr BD7001A11 · Oxygen System
  > (CAN) DURING SCHEDULED MAINTENANCE IT WAS REPORTED BY SERVICE CENTER THAT THE 4 HOSES FOR PASSENGER OXYGEN WERE FOUND DAMAGED.
- [SDR CA190603001](https://openairdocs.org/sdr/CA190603001.md): Support · cracked · Jun 3, 2019 · Bombdr BD7001A10 · Passenger/Crew Doors
  > (CAN) AFT PASSENGER DOOR SURROUNDING STRUCTURE GS217-0155 (NHA GS219-0005) WAS FOUND CRACKED. THIS CRACK WAS FOUND WHILE INSPECTING THE DOOR SURROUND AFTER A PAX DOOR FREE FALL OCCURED. REF TO CASE 000333233 (TC# 20190603001)
- [SDR CA190529005](https://openairdocs.org/sdr/CA190529005.md): Display · failed · May 28, 2019 · Bombdr BD7001A11 · Flight Environment Data
  > (CAN) MULTIPLE DISPLAY UNIT (DU) FAILURES WERE EXPERIENCED IN FLIGHT ON DU #1, DU #2, DU #4, AND DU #6. THE TEMPERATURE AT THE ORIGIN AIRPORT WAS 32 CELSIUS WITH 75-80 PERCENT HUMIDITY. PRIOR TO DEPARTURE AT APPROXIMATELY 0745 ZULU, #4 DU BLANKED OUT. THE DI
- [SDR CA190521027](https://openairdocs.org/sdr/CA190521027.md): Battery · failed · May 14, 2019 · Bombdr BD7001A11 · Airborne Auxiliary Power Unit (APU) System
  > (CAN) A FEW WEEKS AGO, THE FLIGHT CREW NOTICED APU BATT TEMP WAS HIGHER THAN AVIONICS BATTERY AND CLIMBING. CREW SAID THEY SAW TEMP AROUND 50 CELSIUS BEFORE SHUTTING DOWN AIRCRAFT. THEY CYCLED APU BATTERY CONNECTOR AND POWERED BACK ON WITH ALL INDICATIONS NORM
- [SDR CA190514006](https://openairdocs.org/sdr/CA190514006.md): Oven · smoke · May 12, 2019 · Bombdr BD7001A11 · Buffet/Galleys
  > (CAN) AT APPROX 1915Z CABIN FLIGHT ATTENDANT SPOTTED SOME SMOKE COMING OUT OF THE BACK OF THE MICROWAVE. THEY IMMEDIATELY ISOLATED THE MICROWAVE ELECTRICALLY AND THE PROBLEM STOPPED. NO EMERGENCY WAS DECLARED. MICROWAVE HAS BEEN INSPECTED AND TESTED WITH NO
- [SDR CA190509005](https://openairdocs.org/sdr/CA190509005.md): Software · malfunctioned · May 9, 2019 · Bombdr BD7001A10 · Auto Throttle System
  > (CAN) AUTO THROTTLE HUNTING/OSCILLATION CAN OCCUR WHEN AT OPERATED WHEN IAS IS USED AS A SPEED TARGET INSTEAD OF MN. (TC# 20190509005)
- [SDR CA190503026](https://openairdocs.org/sdr/CA190503026.md): Support · cracked · May 3, 2019 · Bombdr BD7001A10 · Passenger/Crew Doors
  > (CAN) FWD PASSENGER DOOR SURROUNDING STRUCTURE GS217-0155 (NHA GS219-0005) WAS FOUND CRACKED. THIS CRACKED WAS FOUND WHILE INVESTIGATING A LOOSE IN THE FWD CABLE PAX DOOR CABLE AND A ROTATION OF THE FWD HANDRAIL SUPPORT PIN. FURTHER DISCUSSION REVEALED THE A/C
- [SDR CA190502004](https://openairdocs.org/sdr/CA190502004.md): Selector Valve · malfunctioned · May 1, 2019 · Bombdr BD7001A11 · Landing Gear Retraction/Extension System
  > (CAN) ON GEAR EXTENSION, GEAR DID NOT EXTEND. AIRCRAFT PERFORMED A GO AROUND AND USED THE EMERGENCY EXTENSION AND LANDED. SUSPECT FAULTY GEAR SELECTOR VALVE NO3 (TC# 20190502004)
- [SDR CA190501020](https://openairdocs.org/sdr/CA190501020.md): Frequency Gen · malfunctioned · Apr 30, 2019 · Bombdr BD7001A10 · AC Generator-Alternator
  > (CAN) DURING FLIGHT #4 VFG CYAN GEN #4 FAIL CAS MESSAGE. 9358`S #4 GENERATOR HAD AN UNCONTAINED FAILURE IN FLIGHT. FRAGMENTS OF THE OIL SUMP PASSED THROUGH THE COWLING AND DEPARTED THE AIRCRAFT. (TC# 20190501020)
- [SDR CA190430009](https://openairdocs.org/sdr/CA190430009.md): Drain Line · separated · Apr 29, 2019 · Bombdr BD7001A11 · Hydraulic System, Main
  > (CAN) CREW DECLARED EMERGENCY: HYDRAULIC SYSTEM #2 FLUID LEVEL DOWN TO 0%. HYDRAULIC FLUID LEAK PRESENT INSIDE AFT EQUIPMENT BAY ASSOCIATED CAS MESSAGE/FAULT CODE: HYD 2 LO QTY, PICTURES FROM MTC SHOWING SYSTEM #2 CASE DRAIN LINE BROKE. INFO: BOMBARDIER HAS S
- [SDR CA190509004](https://openairdocs.org/sdr/CA190509004.md): Switch · dirty · Apr 24, 2019 · Bombdr BD7001A10 · Engine Thrust Reverser
  > (CAN) L REV UNLOCK CYAN ON TAKE OFF. OCCURRED DURING TAKE OFF ROLL AT 40 KNOTS, TAKE OFF WAS ABORTED AND A/C TAXIED BACK TO HANGAR FAULT CLEARED ON ITS OWN BUT PASSENGER ELECTED NOT TO CONTINUE WITH THE FLIGHT. TROUBLESHOOTING FOUND LH ENGINE UPPER OUTBOARD TR
- [SDR CA190425012](https://openairdocs.org/sdr/CA190425012.md): Actuator · malfunctioned · Apr 23, 2019 · Bombdr BD7001A11 · Stabilizer Actuator
  > (CAN) DURING PREFLIGHT STAB TRIM CHECK CREW REGISTERED UNUSUAL VIBRATION AND THUD SOUND WHICH COULD FELT IN THE FIRST MOMENT OF STAB TRIM ACTIVATION. ONCE STAB WAS IN MOTION NOTHING UNUSUAL WAS OBSERVED. THE MOMENT TRIM SWITCHES WAS RELEASED (STAB TRIM MOVEMEN
- [SDR CA190506006](https://openairdocs.org/sdr/CA190506006.md): Connector · damaged · Apr 22, 2019 · Bombdr BD7001A10 · Light System Wiring
  > (CAN) TAIL NAV INOP. AFTER REPLACEMENT OF LIGHT CONNECTOR AT BULLET FAIRING PROBLEM STILL PERSISTENT. CONNECTOR P707 IN TAIL AREA WAS FOUND WITH WATER INSIDE AND PART OF THE WIRING WERE FOUND BURNT. WIRING IS BURNT AND CONNECTOR REQUIRES REPLACEMENT. (TC# 2019
- [SDR CA190417010](https://openairdocs.org/sdr/CA190417010.md): Flt Controls · malfunctioned · Apr 16, 2019 · Bombdr BD7001A10 · Flight Control System
  > (CAN) CREW REPORTS HAVING ISSUES IN CONTROLLING THE AIRCRAFT ON CLIMB OUT PASSING FL100, DECLARED EMERGENCY AND RETURN TO DEPARTING FIELD. AIRCRAFT LH AND RH WING TOUCHING THE RUNWAY PRIOR TO HARD LANDING.
- [SDR CA190416006](https://openairdocs.org/sdr/CA190416006.md): Apu · fire · Apr 15, 2019 · Bombdr BD7001A10 · APU Core Engine
  > (CAN) OPERATOR REPORTED THAT THE CREW EXPERIENCED ENGINE NO-START ISSUES DUE TO A FAULTY BLEED AIR SOURCE APU MAINTENANCE PERSONNEL WERE DISPATCHED TO THE AIRCRAFT TO TROUBLESHOOT THE ENGINE START ISSUE AND TO ATTEMPT AN ENGINE START ON THE RH ENGINE. THE STAR
- [SDR CA190405009](https://openairdocs.org/sdr/CA190405009.md): Fmu · malfunctioned · Apr 4, 2019 · Bombdr BD7001A10 · Fuel Controlling System
  > (CAN) CUSTOMER REPORTED A LOSS OF THRUST CONTROL: ON ROUTE, APPROXIMATELY 15 MINUTES AFTER DEPARTURE, THE FLIGHT CREW NOTICED RH FADEC FAIL EICAS MSG AND A SUBSEQUENT ROLL BACK TO IDLE OF THE RH ENGINE. THE CREW DISCONNECTED THE AUTO THROTTLE AND MANUALLY ADVA
- [SDR CA190409010](https://openairdocs.org/sdr/CA190409010.md): Servo · damaged · Apr 3, 2019 · Bombdr BD7001A10 · Aileron Control System
  > (CAN) THE CREW WERE CARRYING OUT PRE-FLIGHT CHECKS AND DURING THE AILERON CONTROL SWEEP FOUND THAT THEY COULD ONLY ACHIEVE ABOUT HALF DEFLECTION TO THE RIGHT (IT WAS BLOCKED), BUT FULL DEFLECTION TO THE LEFT. THEY TRIED TO MOVE THE AILERONS USING HEADING MODE
- [SDR CA190328001](https://openairdocs.org/sdr/CA190328001.md): Pump · leaking · Mar 26, 2019 · Bombdr BD7001A10 · Engine Fuel Pump
  > (CAN) CUSTOMER REPORTED A FUEL LEAK DURING ENGINE START FROM THE AREA AROUND THE FUEL PUMP PRESSURE RELIEF VALVE. INITIAL INVESTIGATION FOUND THAT IN ACCORDANCE WITH EMM TASK 71-71-00-200-801 THE FUEL LEAK IS EXCEEDING THE LIMIT. BASED ON TROUBLESHOOTING RESUL
- [SDR CA190327013](https://openairdocs.org/sdr/CA190327013.md): Arm · damaged · Mar 25, 2019 · Bombdr BD7001A10 · Main Landing Gear Strut/Axle/Truck
  > (CAN) DURING TAXI WITH NO BRAKES APPLIED, CREW FELT THE AIRCRAFT MOMENTARILY PULL TO THE RIGHT FOLLOWED BY A R OUTBD BRAKE FAIL MESSAGE POSTED ON EICAS. POST TAXI INSPECTION REVEALED SEVERE DISCOLORATION OF THE #4 WHEEL HUB CAP AS WELL AS A PIECE OF MATERIAL P
- [SDR CA190325002](https://openairdocs.org/sdr/CA190325002.md): Engine · power loss · Mar 24, 2019 · Bombdr BD7001A11 · Engine (Turbine/Turboprop)
  > (CAN) GLOBAL 5000 VISION REPORTED A R ENGINE ROLL BACK IN DESCENT WITH A SUBSEQUENT CYAN ENG SYNC LIMITED EICAS MESSAGE. THE CREW SWITCHED FROM AT1 TO AT2 AND NORMAL ENGINE OPERATION WAS RESTORED AND NO FURTHER DISCREPANCIES WERE NOTED. TROUBLESHOOTING ONGOING
- [SDR CA190318015](https://openairdocs.org/sdr/CA190318015.md): Valve · failed · Mar 13, 2019 · Bombdr BD7001A10 · Engine Bleed Air System
  > (CAN) EXPERIENCED A RH BLEED FAIL DURING TAKE-OFF AND A ABORTED TAKE-OFF. IF THIS FAULT WOULD HAVE HAPPEN DURING FLIGHT OUR AFM GIVE THE PROCUDURE AND LIMITATIONS TO CONTINUE THE FLIGHT. BOMBARDIER ANALYZED THE NVM AND CONFIRM THE HIGH PRESSURE VALVE (HPV)
- [SDR CA190318022](https://openairdocs.org/sdr/CA190318022.md): Wire · burned · Mar 7, 2019 · Bombdr BD7001A10 · Light System Wiring
  > (CAN) AIRCRAFT 9726 HAD AN ISSUES WITH THE UPPER TAIL NAV LIGHT. AFTER INSVESTIGATION, WHEN DISMANTELING THE BACKSHELL OF CONNECTOR P707 FOR WIRING INSPECTION, THEY REALIZED THAT THERE WAS WATER INTRUSION IN THE HARNESS PART NUMBER GD598-0029-301-03, UPON INSP
- [SDR KKVA20190305002](https://openairdocs.org/sdr/KKVA20190305002.md): Warning System · false activation · Feb 28, 2019 · N504VJ · Bombdr BD7001A11 · Door Warning System
  > AFTER DEPARTING, UPON INITIAL CLIMB OUT, AT 1,000, WE HEARD SOME NOISE FROM THE DOOR AREA, AS IF SOMETHING HAD BECOME UNLATCHED, AND WE SIMULTANEOUSLY SAW A YELLOW DOOR INDICATION ON THE STATUS SYNOPTIC PAGE. WE DECLARED AN EMERGENCY, CONTINUED OUR CLIMB TO 2,
- [SDR CA190304008](https://openairdocs.org/sdr/CA190304008.md): Battery Box · contaminated · Feb 24, 2019 · Bombdr BD7001A10 · Battery Box Structure
  > (CAN) CUSTOMER REPORTED DEICING FLUID FOUND IN THE BATTERY BOXES. AT EVERY BATTERY INSPECTION WE ARE FINDING TRACES OF DEICING FLUID. THE ONLY LOGICAL EXPLANATION IS THAT IT IS ENTERING THROUGH THE VENT SYSTEM. WE HAVE NOT BEEN SUCCESSFUL IN PREVENTING THIS FO
- [SDR CA190322007](https://openairdocs.org/sdr/CA190322007.md): Bushing · missing · Dec 20, 2018 · Bombdr BD7001A10 · Engine Mount Section
  > (CAN) DURING MAINTENANCE IT WAS DISCOVERED A MISSING BUSHING AND DAMAGE TO THE FORWARD ENGINE MOUNT SYSTEM OF BR710 A2-20 ENGINE 13134 ON AIRCRAFT 9016 (RIGHT HAND SIDE). THE MISSING BUSHING WAS INFORMED TO BE PART NUMBER BRR15808. ROOT CAUSE: IT IS CONFIRME
- [SDR CA180925008](https://openairdocs.org/sdr/CA180925008.md): Compressor · malfunctioned · Sep 21, 2018 · Bombdr BD7001A10 · Cabin Compressor System
  > (CAN) DURING A CHECK-FLIGHT, POST 15 YEARS CHECK AT MAINTENANCE FACILITY (2 MONTHS DOWNTIME), CREW NOTICED DURING TAKE-OFF ROLL (ON GROUND AND SHORTLY AFTER ROTATION) A HEAVY OIL SMELL IN THE AFT CABIN/AFT LAV. THE OIL SMELL DISAPPEARED DURING FLIGHT. NO EME
- [SDR CA180925010](https://openairdocs.org/sdr/CA180925010.md): Control Cable · misaligned · Sep 21, 2018 · Bombdr BD7001A10 · Fuel Controlling System
  > (CAN) DURING SCHEDULED INSPECTION OF THE FUEL SHUT OFF CABLE, AS PER THE EMM, THE SHUT-OFF CABLE WAS REPORTED TO BE MISALIGNED WITH THE ELBOW GUIDE SLOT AND IN CONTACT WITH INNER SURFACE OF OGV. INVESTIGATION LAUNCHED TO DETERMINE ROOT CAUSE. (TC# 2018092501

Next page: https://openairdocs.org/engine/bmw-rolls-br700-710a220/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 engine_model_key = 'BR700710A220'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/bmw-rolls-br700-710a220/reports

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