# BMW Rolls BR700-710A110

- Type: Engine model (FAA registry)
- Registry code: 09496
- Manufacturer (registry): BMW ROLLS
- Model: BR700-710A110
- Engine type: Turbo-fan
- Power: 14,750 lb thrust
- Data sheet: [TCDS E00057EN](https://openairdocs.org/tcds/E00057EN) (OpenAirDocs)
- Holder: Rolls-Royce Deutschland Ltd & Co KG
- Installed in: 8 registered aircraft
- Page: https://openairdocs.org/engine/bmw-rolls-br700-710a110

Model codes come from the FAA registry's reference file.

## ADs that may apply (OpenAirDocs)

Matched to this engine model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment.

- [AD 2025-06-03](https://openairdocs.org/ad/2025-06-03): Turbine Engine Compressor Section · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Apr 23, 2025
- [AD 2022-26-02](https://openairdocs.org/ad/2022-26-02): Accessory Gearboxes · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20, BR700-710C4-11 and 1 more. Effective Jan 27, 2023
- [AD 2021-12-07](https://openairdocs.org/ad/2021-12-07): Turbine Engine Compressor Section · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Aug 12, 2021
- [AD 2016-13-12](https://openairdocs.org/ad/2016-13-12): Pawl carrier pivot pins · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Aug 5, 2016
- [AD 2013-03-17](https://openairdocs.org/ad/2013-03-17): High-pressure turbine (HPT) stage 1 and stage 2 discs · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Mar 21, 2013
- [AD 2011-22-01](https://openairdocs.org/ad/2011-22-01): Touch-and-go and overshoot on life cycle counting · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Nov 23, 2011
- [AD 2010-25-05](https://openairdocs.org/ad/2010-25-05): Turbine Discs · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Jan 13, 2011
- [AD 2005-21-05](https://openairdocs.org/ad/2005-21-05): Fan discs and fan blades · Rolls-Royce Deutschland BR700-710A1-10 and BR700-710A2-20. Effective Nov 25, 2005
- [AD 2001-01-01](https://openairdocs.org/ad/2001-01-01): Oil Filter · Rolls-Royce Deutschland BR700-710A1-10 and BR700-710A2-20. Effective Jan 31, 2001
- [AD 98-24-03 R1](https://openairdocs.org/ad/98-24-03-R1): Combustion Core Fairings · Rolls-Royce Deutschland BR700-710A1-10 and BR700-710A2-20. Effective Dec 27, 1999

Historical (superseded or no longer in force):

- [AD 2022-24-06](https://openairdocs.org/ad/2022-24-06) (historical): Turbine Engine Compressor Section · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Jan 6, 2023
- [AD 2013-05-13](https://openairdocs.org/ad/2013-05-13) (historical): Fuel pump splined couplings · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Apr 24, 2013
- [AD 2003-07-11](https://openairdocs.org/ad/2003-07-11) (historical): Fan discs · Rolls-Royce Deutschland BR700-710A1-10 and BR700-710A2-20. Effective Apr 28, 2003
- [AD 2001-05-06](https://openairdocs.org/ad/2001-05-06) (historical): Fan Disk · BMW Rolls-Royce BR700-710A1-10 and BR700-710A2-20. Effective Mar 29, 2001

## Registered aircraft (8)

- [N1556](https://openairdocs.org/aircraft/N1556): [Metro Builders Supply Inc](https://openairdocs.org/faa-owner/METRO%20BUILDERS%20SUPPLY%20INC), [Tulsa, OK](https://openairdocs.org/faa-place/OK/Tulsa), built 1998, S/N 556
- [N166AA](https://openairdocs.org/aircraft/N166AA): [E D Santos & Associates LLC Trustee](https://openairdocs.org/faa-owner/E%20D%20SANTOS%20%26%20ASSOCIATES%20LLC%20TRUSTEE), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), built 1998, S/N 548
- [N223A](https://openairdocs.org/aircraft/N223A): [Emmanuel Group](https://openairdocs.org/faa-owner/EMMANUEL%20GROUP), [North Wilkesboro, NC](https://openairdocs.org/faa-place/NC/North%20Wilkesboro), S/N 5583
- [N591BC](https://openairdocs.org/aircraft/N591BC): [International Bank Of Commerce](https://openairdocs.org/faa-owner/INTERNATIONAL%20BANK%20OF%20COMMERCE), [Laredo, TX](https://openairdocs.org/faa-place/TX/Laredo), built 1999, S/N 577
- [N626JE](https://openairdocs.org/aircraft/N626JE): [Mmap III LLC](https://openairdocs.org/faa-owner/MMAP%20III%20LLC), [Houston, TX](https://openairdocs.org/faa-place/TX/Houston), built 2001, S/N 642
- [N677F](https://openairdocs.org/aircraft/N677F): [National Science Foundation](https://openairdocs.org/faa-owner/NATIONAL%20SCIENCE%20FOUNDATION), [Alexandria, VA](https://openairdocs.org/faa-place/VA/Alexandria), built 2002, S/N 677
- [N73ZZ](https://openairdocs.org/aircraft/N73ZZ): [Global Aircraft II LLC](https://openairdocs.org/faa-owner/GLOBAL%20AIRCRAFT%20II%20LLC), [Eden Prairie, MN](https://openairdocs.org/faa-place/MN/Eden%20Prairie), built 1999, S/N 593
- [N90JE](https://openairdocs.org/aircraft/N90JE): [Tvpx Aircraft Solutions Inc Trustee](https://openairdocs.org/faa-owner/TVPX%20AIRCRAFT%20SOLUTIONS%20INC%20TRUSTEE), [North Salt Lake, UT](https://openairdocs.org/faa-place/UT/North%20Salt%20Lake), built 1998, S/N 552

## NTSB investigations (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB ERA18LA112](https://openairdocs.org/ntsb/ERA18LA112), Mar 21, 2018: Gulfstream Aerospace G V (N90JE), Miami, FL, no damage. Probable cause: The passengers' failure to comply with the fasten seatbelt sign, with resulted in their injury during an inflight turbulence encounter.

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20180321009789I](https://openairdocs.org/incident/20180321009789I), Mar 21, 2018: Gulfstream G-V (N90JE), Miami, FL, No damage. Gulfstream G-V, N90JE part 91 operator, departed brazil (sbgl) inbound to Miami International Airport (mia) with five passengers and a crew of three…

## Service difficulty reports (188, newest 50)

As reported by operators and repair stations, by the model named in the report.

- [SDR DXTA2026021606878](https://openairdocs.org/sdr/DXTA2026021606878), Feb 12, 2026: ENGINE. FAILED. 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 RI
- [SDR DALA2025061504507](https://openairdocs.org/sdr/DALA2025061504507), Jun 13, 2025: COMPRESSOR. STALLED. SHIP 9516 - DIV - DIVERSION TO ORD DUE TO LEFT ENGINE COMPRESSOR STALL ON CLIMB. CORRECTIVE ACTION: PERFORMED BORESCOPE INSPECTION AND FOUND SEVERAL HPC BLADES 
- [SDR PAZR202408010001](https://openairdocs.org/sdr/PAZR202408010001), Jul 13, 2024: PUMP. SHEARED. 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
- [SDR 2024FA0000001](https://openairdocs.org/sdr/2024FA0000001), Jan 1, 2024: BLEED AIR SYS. FAILED. 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
- [SDR 7ORR202309150036](https://openairdocs.org/sdr/7ORR202309150036), Sep 13, 2023: BLADE. FRACTURED. HPT 1 BLADE RELEASE #2 ENGINE, AND SUBSEQUENT COLLATERAL DAMAGE TO TRAILING TURBINE STAGES; WHICH COULD RESULT IN ENGINE FAILURE AND SUBSEQUENT SINGLE ENGINE OP
- [SDR 2022F00336](https://openairdocs.org/sdr/2022F00336), Sep 9, 2022: PMA. SWOLLEN. 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
- [SDR DALA2022082905782](https://openairdocs.org/sdr/DALA2022082905782), Aug 26, 2022: NONE. NONE. 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 D
- [SDR DALA2022040802422](https://openairdocs.org/sdr/DALA2022040802422), Apr 6, 2022: TAILPIPE. PLUGGED. 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 CLIM
- [SDR 2021FA0000411](https://openairdocs.org/sdr/2021FA0000411), Nov 20, 2021: NONE. BINDS. DISCRPANCY:PILOT NOTIFIED MAINTENANCE AND OPERATIONS IN FLIGHT THE #1 & # 2 FLIGHT GUIDANCE COMPUTER IS INTERMITTENT, AND THE PITCH TRIM DISENGAGED. CORRECTIVE 
- [SDR W6JA20210907047](https://openairdocs.org/sdr/W6JA20210907047), Sep 5, 2021: ENGINE. POWER LOSS. 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 
- [SDR HALA2020120800216](https://openairdocs.org/sdr/HALA2020120800216), Dec 7, 2020: ENGINE. FAILED. 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), Nov 8, 2020: PANEL. MISSING. 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
- [SDR HALA2020011400013](https://openairdocs.org/sdr/HALA2020011400013), Jan 10, 2020: PROBE. FAULTY. 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 8
- [SDR 2019FA0000380](https://openairdocs.org/sdr/2019FA0000380), Nov 16, 2019: VALVE. CONSTRICTED. "LEFT ENGINE FAIL" CAS MESSAGE FOLLOWED BY AUTO RELIGHT. CREW FOLLOWED QRH PROCEDURES AND AIRCRAFT LANDED SAFELY. TROUBLESHOOTING REVEALED HP#5 VALVE TO BE CONS
- [SDR 2019FA0000351](https://openairdocs.org/sdr/2019FA0000351), Oct 25, 2019: GENERATOR. FAILED. 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 
- [SDR AOQA201908061001](https://openairdocs.org/sdr/AOQA201908061001), Jul 31, 2019: LINE. BROKEN. 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
- [SDR 2020FA0000101](https://openairdocs.org/sdr/2020FA0000101), Jun 7, 2019: COMPRESSOR BLADE. GALLED. 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 M
- [SDR 2019FA0000136](https://openairdocs.org/sdr/2019FA0000136), May 1, 2019: GENERATOR. DISINTEGRATED. 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
- [SDR CA180907016](https://openairdocs.org/sdr/CA180907016), Sep 4, 2018: FILLER. OUT OF DATE. (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 AVAILA
- [SDR CA180907017](https://openairdocs.org/sdr/CA180907017), Sep 4, 2018: FILLER. OUT OF DATE. (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 
- [SDR 2CPA2019F00036](https://openairdocs.org/sdr/2CPA2019F00036), Aug 3, 2018: COWLING. DELAMINATED. DELAMINATION (BLISTER) OF INNER BARREL OF ENGINE INLET COWL AT THE 9 O'CLOCK POSITION.
- [SDR HALA2017071200183](https://openairdocs.org/sdr/HALA2017071200183), Jul 12, 2017: ENGINE. DAMAGED. LEFT ENGINE HAD SEVERE DAMAGE.
- [SDR HALA2016111700516](https://openairdocs.org/sdr/HALA2016111700516), Nov 17, 2016: VALVE. MALFUNCTIONED. 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 G
- [SDR 2016FA0000331](https://openairdocs.org/sdr/2016FA0000331), Jul 15, 2016: ENGINE. SHUTDOWN. DURING CRUISE FLIGHT, THE NR 2 ENGINE SHUTDOWN. DID NOT ATTEMPT RESTART. FOLLOWED POH AND LANDED.
- [SDR MGTY20160708075](https://openairdocs.org/sdr/MGTY20160708075), Jul 8, 2016: BATTERY CABLE. MISMANUFACTURED. 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
- [SDR DALA2016060704397](https://openairdocs.org/sdr/DALA2016060704397), Apr 6, 2016: ENGINE. FIRE. 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 IDENTIFI
- [SDR 1SWA2016032800103](https://openairdocs.org/sdr/1SWA2016032800103), Mar 25, 2016: COWLING. CRACKED. 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 
- [SDR CA151214004](https://openairdocs.org/sdr/CA151214004), Dec 11, 2015: CASE. CORRODED. (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 ORDE
- [SDR CA150930008](https://openairdocs.org/sdr/CA150930008), Sep 28, 2015: BOLT. BROKEN. (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 12
- [SDR HALA2015082500168](https://openairdocs.org/sdr/HALA2015082500168), Aug 25, 2015: ENGINE. FLAMED OUT. NR 1 ENGINE FLAMED OUT AT 40 KNOTS, DURING TAKEOFF ROLL. ENGINE CHANGE IN PROCESS.
- [SDR 9PVA2015030500001](https://openairdocs.org/sdr/9PVA2015030500001), Feb 28, 2015: PUMP. FAILED. CREW REPORTED LT MAIN FUEL BOOST PUMP FAILED IN FLIGHT.
- [SDR HALA2014121300209](https://openairdocs.org/sdr/HALA2014121300209), Dec 13, 2014: COMPRESSOR. STALLED. 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, LE
- [SDR HALA2014110400179](https://openairdocs.org/sdr/HALA2014110400179), Nov 4, 2014: ENGINE. VIBRATION. 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
- [SDR DXTA2013120905597](https://openairdocs.org/sdr/DXTA2013120905597), Dec 10, 2013: UNKNOWN. MALFUNCTIONED. 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 STAR
- [SDR CA130905004](https://openairdocs.org/sdr/CA130905004), Sep 2, 2013: BULB. SHORTED. (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 BULB
- [SDR HALA2013030200027](https://openairdocs.org/sdr/HALA2013030200027), Mar 2, 2013: PROXIMITY SENSOR. INOPERATIVE. 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 
- [SDR CA121029001](https://openairdocs.org/sdr/CA121029001), Oct 29, 2012: DRUM. CRACKED. (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), Oct 19, 2012: BONDING STRAP. SHORTED. DURING CRUISE, CREW REPORTED AN INTERMITTENT FIRE WARNING INDICATION ON NR 1 ENGINE, WHICH SUBSEQUENTLY TURNED INTO A STEADY INDICATION. FOLLOWED PROCEDURES IN 
- [SDR LD2R20120403001](https://openairdocs.org/sdr/LD2R20120403001), Apr 3, 2012: ADAPTER. BACKED OUT. 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 PU
- [SDR ZI3R025M012720121](https://openairdocs.org/sdr/ZI3R025M012720121), Jan 24, 2012: SWIRLER. MISSING. 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 DISC
- [SDR 2011FA0000636](https://openairdocs.org/sdr/2011FA0000636), Sep 28, 2011: PANEL. DAMAGED. APPROX 4" DIAMETER HOLE IN INNER BYPASS DUCT PANEL OVER NR1 IGNITOR OF RT ENGINE.
- [SDR 2011FA0000443](https://openairdocs.org/sdr/2011FA0000443), Jun 25, 2011: HOSE. LEAKING. 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 FLU
- [SDR 2011F00114](https://openairdocs.org/sdr/2011F00114), May 15, 2011: WARNING SYSTEM. SHORTED. 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 
- [SDR EW7A2011F00112](https://openairdocs.org/sdr/EW7A2011F00112), May 12, 2011: FIRE WARNING. FALSE ACTIVATION. 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 V
- [SDR 2011FA0000300](https://openairdocs.org/sdr/2011FA0000300), Apr 29, 2011: LINE. CHAFED. 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 F
- [SDR CA110530010](https://openairdocs.org/sdr/CA110530010), Apr 27, 2011: WIRE. MISINSTALLED. 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 SEARCH
- [SDR DXTA2011030704494](https://openairdocs.org/sdr/DXTA2011030704494), Mar 5, 2011: PRESSURE SWITCH. FAILED. 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), Feb 15, 2011: BATTERY PACK. DISCHARGED. FIRST CLASS EMERGENCY LIGHTING NON FUNCTIONAL. FOUND BATTERY PACK DISCHARGED.
- [SDR 2009FA0000039](https://openairdocs.org/sdr/2009FA0000039), Jan 2, 2009: BRAKE. FAILED. 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. TH
- [SDR 2009FA0000040](https://openairdocs.org/sdr/2009FA0000040), Jan 2, 2009: BRAKE. FAILED. 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. TH

All 188: https://openairdocs.org/engine/bmw-rolls-br700-710a110/reports.md

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