# Service difficulty reports: BMW Rolls BR700-710A110

A list on [BMW Rolls BR700-710A110](https://openairdocs.org/engine/bmw-rolls-br700-710a110.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 4 · 188 reports

- [SDR DXTA2026021606878](https://openairdocs.org/sdr/DXTA2026021606878.md): Engine · failed · Feb 12, 2026 · N128QS · Bombdr BD7001A11 · Engine (Turbine/Turboprop)
  > CLIMBING 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. ACCOMPLISH
- [SDR DALA2025061504507](https://openairdocs.org/sdr/DALA2025061504507.md): Compressor · stalled · Jun 13, 2025 · N957AT · Boeing 717200 · Turbine Engine Compressor Section
  > SHIP 9516 - DIV - DIVERSION TO ORD DUE TO LEFT ENGINE COMPRESSOR STALL ON CLIMB. CORRECTIVE ACTION: PERFORMED BORESCOPE INSPECTION AND FOUND SEVERAL HPC BLADES DAMAGED. REPLACED NBR 1 ENGINE. (LP 7264142)
- [SDR PAZR202408010001](https://openairdocs.org/sdr/PAZR202408010001.md): Pump · sheared · Jul 13, 2024 · N194MF · Gulstm GV · Turbine Engine Oil System
  > AFTER APPROXIMATELY 45 MIN OF FLIGHT, RED CAS MESSAGE “R ENG LOW OIL PRES” WAS DISPLAYED IN COCKPIT. OBSERVED A STEADY BUT SLOW INCREASE ON THE RIGHT ENGINE OIL TEMPERATURE. RETURNED TO MAINTENANCE FACILITY. INVESTIGATION REVEALED OIL PUMP SPLINED DRIVE COUPLI
- [SDR 2024FA0000001](https://openairdocs.org/sdr/2024FA0000001.md): Bleed Air Sys · failed · Jan 1, 2024 · N227CV · Gulstm GVSPG550 · Engine Bleed Air System
  > THE CREW PASSING THROUGH FL019 NOTICED AN AMBER EICAS MESSAGE L BAS FAIL- LEFT BLEED AIR SYSTEM FAIL. I WORKED THE CHECKLIST WITH THE CREW AND ADVISED THEY NEED TO TURN BACK TO THEIR DEPARTURE DESTINATION. THE ACFT ARRIVED BACK TO PHKO WITH NO INCIDENT. I HA
- [SDR 7ORR202309150036](https://openairdocs.org/sdr/7ORR202309150036.md): Blade · fractured · Sep 13, 2023 · N270LE · Gulstm GVI · Turbine Section
  > HPT 1 BLADE RELEASE #2 ENGINE, AND SUBSEQUENT COLLATERAL DAMAGE TO TRAILING TURBINE STAGES; WHICH COULD RESULT IN ENGINE FAILURE AND SUBSEQUENT SINGLE ENGINE OPERATION. BORESCOPE INSPECTION WAS INITIATED AT THE BEHEST OF ROLLS-ROYCE DEUTSCHLAND LTD & CO KG ESC
- [SDR 2022F00336](https://openairdocs.org/sdr/2022F00336.md): Pma · swollen · Sep 9, 2022 · N709AA · Gulstm GULFSTREAMGV · Fuel Control/Turbine Engines
  > ENGINE FAILURE ON CLIMB PASSING FL270 THE RIGHT ENGINE FAILED. R CONT IGN WAS SELECTED IN ORDER TO ATTEMPT AN AUTOMATIC RELIGHT. NO RELIGHT. ENGINE WIND MILLING. NO OBVIOUS INDICATION ON WHY THE ENGINE FAILED. RETURNED TO BANGKOK, EXECUTED ENGINE SHUTDOWN IN F
- [SDR DALA2022082905782](https://openairdocs.org/sdr/DALA2022082905782.md): None · none · Aug 26, 2022 · N893AT · Boeing 717200 · Fuel Control/Turbine Engines
  > SHIP 9553 -MISC/DE- THE FLIGHT CREW DECLARED AN EMERGENCY WITH ATC WHILE DUE TO THE #1 ENGINE BEING DIFFICULT TO CONTROL DURING CLIMB. THE ENGINE WAS NOT SHUT DOWN. THE LANDING AT THE SCHEDULED ARRIVAL AIRPORT WAS UNEVENTFUL. MAINTENANCE COULD NOT FIND ANY SOU
- [SDR DALA2022040802422](https://openairdocs.org/sdr/DALA2022040802422.md): Tailpipe · plugged · Apr 6, 2022 · N988AT · Boeing 717200 · Turbine Engine Compressor Section
  > SHIP 9521 - THE FLIGHT CREW RETURNED THE AIRCRAFT BACK TO ATL AND LANDED WITHOUT FURTHER INCIDENT AFTER THE #2 ENGINE EXPERIENCED A COMPRESSOR STALL DURING CLIMB OUT. AT FL230, A LOUD REPORT WAS HEARD, FOLLOWED BY STRONG VIBRATIONS (9.9 UNITS) FROM THE ENGINE,
- [SDR 2021FA0000411](https://openairdocs.org/sdr/2021FA0000411.md): None · binds · Nov 20, 2021 · N588AT · Gulstm GV · Elevator Tab Control System
  > DISCRPANCY:PILOT NOTIFIED MAINTENANCE AND OPERATIONS IN FLIGHT THE #1 & # 2 FLIGHT GUIDANCE COMPUTER IS INTERMITTENT, AND THE PITCH TRIM DISENGAGED. CORRECTIVE ACTION:GULFSTREAM MAINTENANCE FOUND A PITCH TRIM SERVO DRUM AT FAULT. THE PITCH TRIM SERVO DRUM AND
- [SDR W6JA20210907047](https://openairdocs.org/sdr/W6JA20210907047.md): Engine · power loss · Sep 5, 2021 · N188ES · Gulstm GVSP · Engine (Turbine/Turboprop)
  > CREW REPORTED THEY DEPARTED FROM KBZN TO KLAS 9/5/2021. TAKEOFF / CLIMB TO FL450 WITH NO ABNORMAL INDICATIONS. APPROXIMATELY 35 MINUTES INTO THE FLIGHT HEARD A MODERATE BOOM SOUND ACCOMPANIED BY THE AUTO-THROTTLES DISENGAGING, A RED A/T FLASHING ON THE PFD, A
- [SDR HALA2020120800216](https://openairdocs.org/sdr/HALA2020120800216.md): Engine · failed · Dec 7, 2020 · N492HA · Boeing 717200 · Engine (Turbine/Turboprop)
  > ATB-RT ENGINE COMP STALL RT ENGINE OIL PRESS 0. REMOVED & REPLACED #2 ENG PER W/O 181624 REF TASK CARD E1128-717-72-003-INSTALL OPS/LEAK CHECK OK.
- [SDR DALA2020110903639](https://openairdocs.org/sdr/DALA2020110903639.md): Panel · missing · Nov 8, 2020 · N717JL · Boeing 717200 · Engine Thrust Reverser
  > THE INBOARD SIDE NR 1 ENGINE THRUST REVERSER PANEL MISSING. MAINTENANCE INSTALLED A NEW PANEL USING NEW HARDWARE. PERFORMED AN OPERATIONAL AND LEAK CHECK OF THE THRUST REVERSER, PER B717 AMM 78-30. AIRCRAFT OK FOR SERVICE.
- [SDR HALA2020011400013](https://openairdocs.org/sdr/HALA2020011400013.md): Probe · faulty · Jan 10, 2020 · N485HA · Boeing 717200 · Fuel Control/Turbine Engines
  > ATB - SELECT FADEC ALTERNATE (L) ILLUMINATED DURING CLIMBOUT - ABOUT 1,300 FEET C/W QRH PROCEDURES, LIGHT DID NOT GO OUT - RETURNED TO HNL. PER FIM 73-21 TASK 814 STEPS A TO D (4) MECH: CONTINUED FROM STEP D.(3)(B). REMOVED AND REPLACED P2/T2 PROBE PER AMM 73
- [SDR 2019FA0000380](https://openairdocs.org/sdr/2019FA0000380.md): Valve · constricted · Nov 16, 2019 · N828SN · Gulstm GVI · Engine (Turbine/Turboprop)
  > "LEFT ENGINE FAIL" CAS MESSAGE FOLLOWED BY AUTO RELIGHT. CREW FOLLOWED QRH PROCEDURES AND AIRCRAFT LANDED SAFELY. TROUBLESHOOTING REVEALED HP#5 VALVE TO BE CONSTRICTED DUE TO COMPRESSION RING OUT OF PLACE. COMPRESSION RING WAS CORRECTLY INSTALLED PER AMM 36
- [SDR 2019FA0000351](https://openairdocs.org/sdr/2019FA0000351.md): Generator · failed · Oct 25, 2019 · N901GX · Bombdr BD7001A10 · AC Generator-Alternator
  > AIRCRAFT 9001 RETURNED FROM FLT 3763 WITH A #1 GEN FAIL. THE NO.1 ENGINE WAS SHUT DOWN AS A PRECAUTION DUE TO PREVIOUS VFG DISINTEGRATION HISTORY, AND RETURNED TO BASE. THE UPON INSPECTION FOUND OIL STREAKS ON THE #1 ENGINE (ESN 12832) COWLS AND FOUND THE #1 V
- [SDR AOQA201908061001](https://openairdocs.org/sdr/AOQA201908061001.md): Line · broken · Jul 31, 2019 · N820HB · Gulstm GV · Navigation System
  > DISCOVERED DURING GROUND OPERATION. NO AIR WAS FELT AT THE BACK OF THE TAT PROBES. INSPECTION OF THE BLEED AIR FEED LINE STARTING AT THE TAT SOLENOID IN THE AFT EQUIPMENT BAY AREA FOUND A LINE HAD SEPARATED JUST AFTER AN ADEL SUPPORT CLAMP. NO ADDITIONAL SURRO
- [SDR 2020FA0000101](https://openairdocs.org/sdr/2020FA0000101.md): Compressor Blade · galled · Jun 7, 2019 · N278PH · Gulstm GV · Turbine Engine Compressor Section
  > DURING ROUTINE 1000 HOUR REAPPLICATION OF THE DRY FILM LUBRICANT ON THE FAN BLADE ROOT AREA IT WAS NOTICED THAT GAULLING ON THE BLADE ROOT WAS BEYOND THE.004 MANUFACTURE LIMIT. A FLY ON DISPOSITION WAS NOT GRANTED BY ROLLS ROYCE AND ALL 24 BLADES ON THE BOTH
- [SDR 2019FA0000136](https://openairdocs.org/sdr/2019FA0000136.md): Generator · disintegrated · May 1, 2019 · N760AG · Bombdr BD7001A10 · AC Generator-Alternator
  > APPROXIMATELY THREE HOURS INTO FLIGHT THE CREW REPORTED RECEIVING A "GEN 4 FAIL" MESSAGE. CREW RESPONDED BY RESETTING THE NR 4 VARIABLE FREQUENCY GENERATOR (VFG). FOLLOWING THE RESET THE CREW SAID THEY HEARD A "THUNK" SOUND AND A SHUDDER WITHIN THE AIRCRAFT. T
- [SDR CA180907016](https://openairdocs.org/sdr/CA180907016.md): Filler · out of date · Sep 4, 2018 · Turbine Engine Combustion Section
  > (CAN) AS PER TLM TASK 05-00-03-800-001 (SUBTASK 05-00-03-870-004), MAXIMUM APPROVED LIVES FOR ANNULUS FILLERS P/N BRR19433 IS 4500 CYCLES. AS PER RECORDS AVAILABLE, THE ACTUAL LIFE OF ANNULUS FILLERS P/N BRR19433 IS 4887 CYCLES. THIS ANNULUS FILLER HAS EXCEE
- [SDR CA180907017](https://openairdocs.org/sdr/CA180907017.md): Filler · out of date · Sep 4, 2018 · Turbine Engine Combustion Section
  > (CAN) AS PER TLM TASK 05-00-03-800-001 (SUBTASK 05-00-03-870-004) MAXIMUM APPROVED LIVES FOR FILLERS P/N BRR19433 IS 4500 CYCLES. AS PER RECORDS AVAILABLE, THE ACTUAL LIFE OF QTY 3 ANNULUS FILLERS P/N BRR19433 IS 4867 CYCLES. THESE ANNULUS FILLERS HAVE EXCEE
- [SDR 2CPA2019F00036](https://openairdocs.org/sdr/2CPA2019F00036.md): Cowling · delaminated · Aug 3, 2018 · N780W · Gulstm GV · Engine Cowling System
  > DELAMINATION (BLISTER) OF INNER BARREL OF ENGINE INLET COWL AT THE 9 O'CLOCK POSITION.
- [SDR HALA2017071200183](https://openairdocs.org/sdr/HALA2017071200183.md): Engine · damaged · Jul 12, 2017 · N480HA · Boeing 717200 · Engine (Turbine/Turboprop)
  > LEFT ENGINE HAD SEVERE DAMAGE.
- [SDR HALA2016111700516](https://openairdocs.org/sdr/HALA2016111700516.md): Valve · malfunctioned · Nov 17, 2016 · N487HA · Boeing 717200 · Turbine Engine Compressor Section
  > RT ENGINE COMPRESSOR STALL AFTER START. REMOVED AND REPLACED THE BYPASS AND VENT VALVE IAW TASK 73-13-04-000-801, 73-13-04-400-801.ENGINE RUN AND LEAK CHECKED GOOD. OK FOR SERVICE.
- [SDR 2016FA0000331](https://openairdocs.org/sdr/2016FA0000331.md): Engine · shutdown · Jul 15, 2016 · N17ND · Gulstm GV · Engine (Turbine/Turboprop)
  > DURING CRUISE FLIGHT, THE NR 2 ENGINE SHUTDOWN. DID NOT ATTEMPT RESTART. FOLLOWED POH AND LANDED.
- [SDR MGTY20160708075](https://openairdocs.org/sdr/MGTY20160708075.md): Battery Cable · mismanufactured · Jul 8, 2016 · N900KS · Gulstm GVI · Electrical Power System Wiring
  > LEFT MAIN BATTERY LOW VOLTS CAS MESSAGE AS REPORTED BY THE CREW. ON INVESTIGATION IT WAS DISCOVERED THAT THE LT MAIN BATTERY NEGATIVE CABLE TO AIRFRAME TERMINAL HAD BEEN ARCING WHICH HAD CAUSED EXTENSIVE DAMAGE TO THE TERMINAL ITSELF AND ATTACHING AIRFRAME BR
- [SDR DALA2016060704397](https://openairdocs.org/sdr/DALA2016060704397.md): Engine · fire · Apr 6, 2016 · N974AT · Boeing 717200 · Engine (Turbine/Turboprop)
  > THE CREW SAFELY ABORTED THE TAKEOFF AT LESS THAN 80 KTS DUE TO A FIRE INDICATION ON THE NR 1 ENGINE. THE FIRE WAS CONFIRMED, BUT THE CAUSE HAS NOT BEEN IDENTIFIED. MAINTENANCE HAS REPLACED THE NR 1 ENGINE.
- [SDR 1SWA2016032800103](https://openairdocs.org/sdr/1SWA2016032800103.md): Cowling · cracked · Mar 25, 2016 · N620JF · Gulstm GVSPG550 · Engine Cowling System
  > WHILE COMPLYING WITH CMP 711016, FOUND RT ENG UPPER COWL LE TO BE CRACKED & TO HAVE LOOSE CARBON FIBER MATERIAL SHOWING. INSPECTED & TAP TEST RT ENG UPPER COWL FOR SUSPECTED UNBONDING, MARKED OUT LINE OF UNBOND AREA. UNBONDING STARTS ABOUT 4 INCHES AFT OF RT
- [SDR CA151214004](https://openairdocs.org/sdr/CA151214004.md): Case · corroded · Dec 11, 2015 · Gulstm GV · Turbine Engine Air Inlet Section
  > (CAN) DURING PRELIMINARY INSPECTION OF THE FAN CASE (LEVEL 3 OVERHAUL) MINOR BULGING OF THE FAN TRACK LINING WAS NOTICED AT BOTTOM DEAD CENTER POSITION. IN ORDER TO DETERMINE THE ROOT CAUSE OF THIS BULGING, THE INSPECTOR HAS REQUESTED FOR REMOVAL OF THE AFFECT
- [SDR CA150930008](https://openairdocs.org/sdr/CA150930008.md): Bolt · broken · Sep 28, 2015 · Bombdr BD7001A10 · Turbine Section
  > (CAN) BOLTS QTY 9, PART CONDITION: BROKEN LOCATION OF DEFECT: HPT1 TO HPT2 DISC INTERFACE PART TSN/CSN: SAME AS THE ENGINE, FIRST SHOP VISIT. DURING STRIP OF 12320/41121221 FOUND 9 BROKEN BOLTS ATA 72-41-44 01-205, TOTAL IPC QUANTITY IS 19. DAMAGES WERE F
- [SDR HALA2015082500168](https://openairdocs.org/sdr/HALA2015082500168.md): Engine · flamed out · Aug 25, 2015 · N491HA · Boeing 717200 · Engine (Turbine/Turboprop)
  > NR 1 ENGINE FLAMED OUT AT 40 KNOTS, DURING TAKEOFF ROLL. ENGINE CHANGE IN PROCESS.
- [SDR 9PVA2015030500001](https://openairdocs.org/sdr/9PVA2015030500001.md): Pump · failed · Feb 28, 2015 · N50JE · Gulstm GV · Fuel Boost Pump
  > CREW REPORTED LT MAIN FUEL BOOST PUMP FAILED IN FLIGHT.
- [SDR HALA2014121300209](https://openairdocs.org/sdr/HALA2014121300209.md): Compressor · stalled · Dec 13, 2014 · N487HA · Boeing 717200 · Turbine Engine Compressor Section
  > COMPRESSOR STALL ON LT ENGINE 1000 FT, MAX POWER. ACCOMPLISHED AMM 72-00-00-200-801 FROM PAR D THRU E(3) 15856. REMOVED NR 1 ENGINE IAW M144-717. ENGINE RUN, LEAK-CHECK OF INHIBIT PORT ON TUBE BETWEEN FMU AND BVV AT BOTTOM OF ENGINE GOOD IAW AMM 71-00-11
- [SDR HALA2014110400179](https://openairdocs.org/sdr/HALA2014110400179.md): Engine · vibration · Nov 4, 2014 · N486HA · Boeing 717200 · Engine (Turbine/Turboprop)
  > ENGINE VIBRATION HIGH ALERT FOLLOWED BY SUDDEN GROWLING NOISE, CLIMBING THROUGH 5000 FEET LT N2 VIB. REACHED 6.2 AND DROPPED LOWER WITH REDUCED POWER. ALL OTHER ENGINE INDICATIONS NORMAL. AIR TURN BACK.
- [SDR DXTA2013120905597](https://openairdocs.org/sdr/DXTA2013120905597.md): Unknown · malfunctioned · Dec 10, 2013 · N531QS · Gulstm 520 · Engine (Turbine/Turboprop)
  > AMBER CAS RT ENG EXCEEDANCE PRIOR TO TAKEOFF. ATMOSPHERIC CONDITIONS ON THE GND WERE PRODUCING FREEZING FOG. TEMP DEW POINT -3C -3C. ENG INDICATIONS DURING START & TAXI WERE NORMAL, ENG ANTI-ICE ON. AS PILOT ADVANCED THROTTLES FOR TAKEOFF, EXPERIENCED NOTI
- [SDR CA130905004](https://openairdocs.org/sdr/CA130905004.md): Bulb · shorted · Sep 2, 2013 · Gulstm GV · Central Warning
  > (CAN) HAD A FAILURE OF COPILOTS MASTER WARNING ANNUNCIATOR. TROUBLESHOOTING REVEALED THAT 1 OF 4 LED LIGHT BULBS HAD FAILED SHORTED. THIS RESULTED IN ALL 4 BULBS FAILING TO ILLUMINATE. WITH THE FAILURE OF ONLY 1 BULB IN THE ANNUNCIATOR, NONE OF THE OTHER BU
- [SDR HALA2013030200027](https://openairdocs.org/sdr/HALA2013030200027.md): Proximity Sensor · inoperative · Mar 2, 2013 · N485HA · Boeing 717200 · Landing Gear Position and Warning
  > LEFT GEAR RED AFTER TAKEOFF, ALL THREE GREEN (NO RED) ON ARRIVAL. KEPT AIRSPEED BELOW 230 KTS. R & R D1-1057 LT MAIN GEAR UP & LATCHED PROXIMITY SENSOR IAW AMM 32-61-02. OPS CHECK OK.
- [SDR CA121029001](https://openairdocs.org/sdr/CA121029001.md): Drum · cracked · Oct 29, 2012 · Bombdr BD7001A10 · Turbine Engine Compressor Section
  > (CAN) HPC FRONT DRUM ASSY WAS FOUND CRACKED IN CENTER LINE IN SLOPE OUT INSIDE EBW WELD STAGE 5/6 DURING OVERHAUL PROCESS.
- [SDR 2012FA0000713](https://openairdocs.org/sdr/2012FA0000713.md): Bonding Strap · shorted · Oct 19, 2012 · N132SD · Gulstm GV · Fire Detection
  > DURING CRUISE, CREW REPORTED AN INTERMITTENT FIRE WARNING INDICATION ON NR 1 ENGINE, WHICH SUBSEQUENTLY TURNED INTO A STEADY INDICATION. FOLLOWED PROCEDURES IN THE AFM IN ORDER TO CONFIRM OR EXCLUDE VALIDITY OF INDICATION. DETERMINED INDICATION WAS FALSE.
- [SDR LD2R20120403001](https://openairdocs.org/sdr/LD2R20120403001.md): Adapter · backed out · Apr 3, 2012 · Gulstm GV · Engine Fuel Pump
  > WHILE PERFORMING A SERVICE BULLITIN TO REPLACE THE FUEL PUMP SPLINE ADAPTER, WE FOUND THE ENGINE DRIVEN FUEL PUMP DRIVE SHAFT TO BE MIGRATING OUT OF THE FUEL PUMP AND INTO THE ACCESSORY GEAR CASE. UPON INSPECTION OF THE GEAR CASE WE FOUND A RETAINING PLUG IN
- [SDR ZI3R025M012720121](https://openairdocs.org/sdr/ZI3R025M012720121.md): Swirler · missing · Jan 24, 2012 · Gulstm GVSPG550 · Fuel Injector Nozzle
  > ZI3R RECEIVED 3 EA, BR710 FUEL NOZZLES FROM MFG. ONE (1) OF THE THREE (3) NOZZLES HAD A MISSING COMPONENT; THE INNER AIR SWIRLER. THE MISSING COMPONENT WAS DISCOVERED DURING AN CUSTOMER REQUIRED X-RAY INSPECTION PERFORMED BY OEM, AND THE MISSING PART WAS VER
- [SDR 2011FA0000636](https://openairdocs.org/sdr/2011FA0000636.md): Panel · damaged · Sep 28, 2011 · N661GA · Gulstm GV · Turbine Engine Bypass Section
  > APPROX 4" DIAMETER HOLE IN INNER BYPASS DUCT PANEL OVER NR1 IGNITOR OF RT ENGINE.
- [SDR 2011FA0000443](https://openairdocs.org/sdr/2011FA0000443.md): Hose · leaking · Jun 25, 2011 · N673P · Gulstm GV · Hydraulic System, Main
  > LEFT HYD SYS OIL LEAKAGE WAS DETECTED ON THE SYNOPTIC DISPLAY. AT FL410 AND 1.5 HOURS OUT THE PIC ELECTED TO TURN BACK TO DEPARTURE. WITH 0.5 GALLONS OF HYD FLUID REMAINING, THE ACFT LANDED WITHOUT INCIDENT. MX DETECTED FLUID LEAKAGE FROM THE LT PYLON. UPO
- [SDR 2011F00114](https://openairdocs.org/sdr/2011F00114.md): Warning System · shorted · May 15, 2011 · N132SD · Gulstm GV · Fire Detection
  > DURING CRUISE, FLIGHT CREW REPORTED INTERMITTENT FIRE WARNING ON NR 2 ENGINE. FLIGHT CREW FOLLOWED PROCEDURES IN AFM IN ORDER TO CONFIRM OR EXCLUDE VALIDITY OF INDICATION. FLIGHT CREW DETERMINED INDICATION WAS FALSE. MX TROUBLESHOT SYS AND DETERMINED THAT WI
- [SDR EW7A2011F00112](https://openairdocs.org/sdr/EW7A2011F00112.md): Fire Warning · false activation · May 12, 2011 · N132SD · Gulstm GV · Fire Detection
  > DURING CRUISE, FLIGHT CREW REPORTED INTERMITTENT FIRE WARNING INDICATION ON NR 2 ENGINE. FLIGHT CREW FOLLOWED PROCEDURES IN AFM IN ORDER TO CONFIRM OR EXCLUDE VALIDITY OF INDICATION. FLIGHT CREW DETERMINED INDICATION WAS FALSE. MX VERIFIED THAT THE INDICATIO
- [SDR 2011FA0000300](https://openairdocs.org/sdr/2011FA0000300.md): Line · chafed · Apr 29, 2011 · N673P · Gulstm GV · Hydraulic System, Main
  > THE LT SYS HYD FLUID LEAKAGE WAS DETECTED AT MIDPOINT OF A 2 HR FLIGHT AT FL 410. DURING DESCENT, THE INDICATION WENT CLOSE TO ZERO. THE PIC ELECTED TO DIVERT FOR THE LARGER 12,000 FT RUNWAY IN CASE THE BRAKES AND NOSE WHEEL STEERING WERE DEGRADED. THE LAND
- [SDR CA110530010](https://openairdocs.org/sdr/CA110530010.md): Wire · misinstalled · Apr 27, 2011 · Bombdr BD7001A10 · Electrical Power System Wiring
  > THE DC POWER EMERGENCY OVERRIDE TEST HAS REVEALED THAT THE RMU NR 1 WAS NOT SHOWING ANY DASHES WHEN TRANSFERRED IN DC POWER EMERGENCY OVERIDE MODE. AFTER SEARCHING FOR THE FAILURE, DISCOVERED THAT THE SPDA DC ESS LOADS AND SPDA DC 2 LOAD WIRES WERE INVERT WHI
- [SDR DXTA2011030704494](https://openairdocs.org/sdr/DXTA2011030704494.md): Pressure Switch · failed · Mar 5, 2011 · N511QS · Gulstm GV · Engine Fuel Pump
  > LEFT MAIN FUEL PUMP FAILED IN FLIGHT. R & R LT MAIN FUEL PUMP PRESSURE SWITCH WORK ACCOMPLISHED IAW GV CMP 284305.
- [SDR 2011FA0000105](https://openairdocs.org/sdr/2011FA0000105.md): Battery Pack · discharged · Feb 15, 2011 · N169CA · Boeing 757236 · Emergency Lighting
  > FIRST CLASS EMERGENCY LIGHTING NON FUNCTIONAL. FOUND BATTERY PACK DISCHARGED.
- [SDR 2009FA0000039](https://openairdocs.org/sdr/2009FA0000039.md): Brake · failed · Jan 2, 2009 · N500E · Bombdr BD7001A10 · Flight Control System
  > ALL (4) ASSYMETRY BRAKES WERE REMOVED FROM THE ACFT IN OCT 2008, MODIFIED AND REINSTALLED. SINCE THAT TIME THE LT FLAP BRAKE FAILED AFTER 6 WEEKS IN SERVICE. THE 2ND BRAKE FAILED WITH 3 MONTHS IN SERVICE. (K)
- [SDR 2009FA0000040](https://openairdocs.org/sdr/2009FA0000040.md): Brake · failed · Jan 2, 2009 · N500E · Bombdr BD7001A10 · Leading Edge Devices
  > ALL (4) ASYMMETRY BRAKES WERE REMOVED FROM THE ACFT IN OCT 2008, MODIFIED AND REINSTALLED. SINCE THAT TIME THE LT FLAP BRAKE FAILED AFTER 6 WEEKS IN SERVICE. THE SECOND BRAKE FAILED WITH 3 MONTHS IN SERVICE. (K)

Next page: https://openairdocs.org/engine/bmw-rolls-br700-710a110/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 = 'BR700710A110'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/bmw-rolls-br700-710a110/reports

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