# BMW Rolls BR700-710A220 - Type: Engine model (FAA registry) - Registry code: 09495 - Manufacturer (registry): BMW ROLLS - Model: BR700-710A220 - 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: 27 registered aircraft - Page: https://openairdocs.org/engine/bmw-rolls-br700-710a220 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 2021-21-12](https://openairdocs.org/ad/2021-21-12): Turbine Engine Compressor Section · Rolls-Royce Deutschland BR700-710A2-20. Effective Dec 13, 2021 - [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 2018-18-14](https://openairdocs.org/ad/2018-18-14): Engine Controls · Rolls-Royce Deutschland BR700-710A2-20 and BR700-710C4-11. Effective Oct 12, 2018 - [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 (27) - [N142QS](https://openairdocs.org/aircraft/N142QS): built 2012, S/N 9485 - [N152QS](https://openairdocs.org/aircraft/N152QS): built 2016, S/N 9773 - [N18WZ](https://openairdocs.org/aircraft/N18WZ): [Ewz Aviation Inc](https://openairdocs.org/faa-owner/EWZ%20AVIATION%20INC), [Santa Monica, CA](https://openairdocs.org/faa-place/CA/Santa%20Monica), built 2009, S/N 9338 - [N190JA](https://openairdocs.org/aircraft/N190JA): [Jacob Wing LLC](https://openairdocs.org/faa-owner/JACOB%20WING%20LLC), [New York, NY](https://openairdocs.org/faa-place/NY/New%20York), built 2008, S/N 9274 - [N2AC](https://openairdocs.org/aircraft/N2AC): [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 2011, S/N 9455 - [N404NA](https://openairdocs.org/aircraft/N404NA): [Tvpx Ars Inc Trustee](https://openairdocs.org/faa-owner/TVPX%20ARS%20INC%20TRUSTEE), [North Salt Lake, UT](https://openairdocs.org/faa-place/UT/North%20Salt%20Lake), built 2009, S/N 9356 - [N411XT](https://openairdocs.org/aircraft/N411XT): [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 2003, S/N 9133 - [N417CS](https://openairdocs.org/aircraft/N417CS): [Wpa Aviation II LLC](https://openairdocs.org/faa-owner/WPA%20AVIATION%20II%20LLC), [Greenwich, CT](https://openairdocs.org/faa-place/CT/Greenwich), built 2007, S/N 9255 - [N443PR](https://openairdocs.org/aircraft/N443PR): [Ruffin Development Acquisitions LLC](https://openairdocs.org/faa-owner/RUFFIN%20DEVELOPMENT%20ACQUISITIONS%20LLC), [Wichita, KS](https://openairdocs.org/faa-place/KS/Wichita), built 2012, S/N 9520 - [N44GX](https://openairdocs.org/aircraft/N44GX): [D3t2 LLC](https://openairdocs.org/faa-owner/D3T2%20LLC), [New York, NY](https://openairdocs.org/faa-place/NY/New%20York), built 2004, S/N 9142 - [N487JG](https://openairdocs.org/aircraft/N487JG): [Artemis Aviation LLC](https://openairdocs.org/faa-owner/ARTEMIS%20AVIATION%20LLC), [Houston, TX](https://openairdocs.org/faa-place/TX/Houston), built 2012, S/N 9487 - [N506VJ](https://openairdocs.org/aircraft/N506VJ): [Tvpx Trust Co LLC Trustee](https://openairdocs.org/faa-owner/TVPX%20TRUST%20CO%20LLC%20TRUSTEE), [North Salt Lake, UT](https://openairdocs.org/faa-place/UT/North%20Salt%20Lake), built 2006, S/N 9214 - [N562TH](https://openairdocs.org/aircraft/N562TH): [Global One Tjh LLC](https://openairdocs.org/faa-owner/GLOBAL%20ONE%20TJH%20LLC), [San Antonio, TX](https://openairdocs.org/faa-place/TX/San%20Antonio), built 2001, S/N 9085 - [N588CV](https://openairdocs.org/aircraft/N588CV): [9354 Leasing LLC](https://openairdocs.org/faa-owner/9354%20LEASING%20LLC), [West Palm Beach, FL](https://openairdocs.org/faa-place/FL/West%20Palm%20Beach), built 2009, S/N 9354 - [N609AK](https://openairdocs.org/aircraft/N609AK): [Peck Ventures LLC](https://openairdocs.org/faa-owner/PECK%20VENTURES%20LLC), [Henderson, NV](https://openairdocs.org/faa-place/NV/Henderson), built 2009, S/N 9346 - [N60BJ](https://openairdocs.org/aircraft/N60BJ): [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 2010, S/N 9402 - [N715TS](https://openairdocs.org/aircraft/N715TS): [Tvpx Trust Co LLC](https://openairdocs.org/faa-owner/TVPX%20TRUST%20CO%20LLC), [North Salt Lake, UT](https://openairdocs.org/faa-place/UT/North%20Salt%20Lake), built 2018, S/N 9836 - [N724MF](https://openairdocs.org/aircraft/N724MF): [Mbf Leasing Of Florida LLC](https://openairdocs.org/faa-owner/MBF%20LEASING%20OF%20FLORIDA%20LLC), [Coral Gables, FL](https://openairdocs.org/faa-place/FL/Coral%20Gables), built 2011, S/N 9457 - [N731SR](https://openairdocs.org/aircraft/N731SR): [83/80 LLC](https://openairdocs.org/faa-owner/83%2F80%20LLC), [New York, NY](https://openairdocs.org/faa-place/NY/New%20York), built 2013, S/N 9597 - [N797CT](https://openairdocs.org/aircraft/N797CT): [Caterpillar Inc](https://openairdocs.org/faa-owner/CATERPILLAR%20INC), [Fort Worth, TX](https://openairdocs.org/faa-place/TX/Fort%20Worth), built 2012, S/N 9435 - [N7CG](https://openairdocs.org/aircraft/N7CG): [Coulson Aviation (USA) Inc](https://openairdocs.org/faa-owner/COULSON%20AVIATION%20(USA)%20INC), [Portland, OR](https://openairdocs.org/faa-place/OR/Portland), built 2000, S/N 9075 - [N83WG](https://openairdocs.org/aircraft/N83WG): [Cooper Burger LLC](https://openairdocs.org/faa-owner/COOPER%20BURGER%20LLC), [Coral Gables, FL](https://openairdocs.org/faa-place/FL/Coral%20Gables), built 1999, S/N 9030 - [N84YU](https://openairdocs.org/aircraft/N84YU): [Txpx Aircraft Solutions Inc Trustee](https://openairdocs.org/faa-owner/TXPX%20AIRCRAFT%20SOLUTIONS%20INC%20TRUSTEE), [North Salt Lake, UT](https://openairdocs.org/faa-place/UT/North%20Salt%20Lake), built 2008, S/N 9300 - [N878SC](https://openairdocs.org/aircraft/N878SC): [Tvpx Ars Inc Trustee](https://openairdocs.org/faa-owner/TVPX%20ARS%20INC%20TRUSTEE), [North Salt Lake, UT](https://openairdocs.org/faa-place/UT/North%20Salt%20Lake), built 2014, S/N 9614 - [N90FX](https://openairdocs.org/aircraft/N90FX): [Citation X Parts LLC](https://openairdocs.org/faa-owner/CITATION%20X%20PARTS%20LLC), [Liberty, NC](https://openairdocs.org/faa-place/NC/Liberty), built 1999, S/N 9017 - [N915JG](https://openairdocs.org/aircraft/N915JG): [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE), [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City), built 2002, S/N 9115 - [N926PN](https://openairdocs.org/aircraft/N926PN): [Sn 9003 LLC](https://openairdocs.org/faa-owner/SN%209003%20LLC), [Van Nuys, CA](https://openairdocs.org/faa-place/CA/Van%20Nuys), built 1997, S/N 9003 ## NTSB investigations None matched to aircraft with this engine model. ## 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 20111120027421I](https://openairdocs.org/incident/20111120027421I), Nov 20, 2011: Bombardier Inc BD-700-1A10 (N981TS), Newark, NJ, Minor damage. During taxi operations ground person marshaled the aircraft too close to a parked aircraft and collision occured. ## Service difficulty reports (187, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR DXTA2026082409378](https://openairdocs.org/sdr/DXTA2026082409378), Aug 21, 2026: ENGINE. UNKNOWN. 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 - [SDR DXTA2026060408300](https://openairdocs.org/sdr/DXTA2026060408300), May 31, 2026: FMU. FAILED. 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 - [SDR DXTA2026010706444](https://openairdocs.org/sdr/DXTA2026010706444), Jan 5, 2026: ANTI-ICE VALVE. FAULTY. 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 - [SDR J7SA2025032700000](https://openairdocs.org/sdr/J7SA2025032700000), Mar 23, 2025: ENGINE. POWER LOSS. 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. APPROX - [SDR 2024F00136](https://openairdocs.org/sdr/2024F00136), May 17, 2024: MODULE. FALSE INDICATION. 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), Mar 14, 2024: BLADE. BROKEN. 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 SERVICEABL - [SDR 85LY20230623223](https://openairdocs.org/sdr/85LY20230623223), Jun 18, 2023: UNKNOWN. UNKNOWN. 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 CARRIE - [SDR CWQA20220825001](https://openairdocs.org/sdr/CWQA20220825001), Aug 22, 2022: OIL SYSTEM. LEAKING. 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 PERFOR - [SDR 2022FA0000326](https://openairdocs.org/sdr/2022FA0000326), Jul 1, 2022: NONE. NONE. 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 B - [SDR 2022F00238](https://openairdocs.org/sdr/2022F00238), May 24, 2022: FREQUENCY GEN. DAMAGED. 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 T - [SDR 1JCA202112221001](https://openairdocs.org/sdr/1JCA202112221001), Dec 22, 2021: WARNING MESSAGE. ILLUMINATED. 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 REQUIRE - [SDR KKVA20211019002](https://openairdocs.org/sdr/KKVA20211019002), Oct 19, 2021: ENGINE. ODOR. 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 - [SDR M2MR202104080001](https://openairdocs.org/sdr/M2MR202104080001), Apr 8, 2021: HOUSING. LEAKING. 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 F - [SDR AWKA2020100201](https://openairdocs.org/sdr/AWKA2020100201), Sep 19, 2020: SWITCH. FAILED. 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 PHO - [SDR CA190801008](https://openairdocs.org/sdr/CA190801008), Jul 29, 2019: CONTACTOR. DAMAGED. (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 FAIL - [SDR CA190802003](https://openairdocs.org/sdr/CA190802003), Jul 28, 2019: FREQUENCY GEN. MALFUNCTIONED. (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), Jul 25, 2019: TIRE. FAILED. (CAN) UNCOMMANDED BRAKE PRESSURE APPLIED TO 1 WHEEL LEAD TO A TIRE BURST DURING LANDING (TC# 20190726030) - [SDR CA190730014](https://openairdocs.org/sdr/CA190730014), Jul 20, 2019: TORQUE TUBE. DISCONNECTED. (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 - [SDR 2019FA0000207](https://openairdocs.org/sdr/2019FA0000207), Jul 1, 2019: HOSE. BROKEN. DURING AN AIRCRAFT 10 YEAR INSPECTION THE PASSENGER OXYGEN SYSTEM HAD ALREADY PASSED THE REQUIRED FUNCTIONAL TEST. AFTER THE AIRCRAFT SUBSEQUENT MAIN CABIN AND - [SDR CA190702018](https://openairdocs.org/sdr/CA190702018), Jun 29, 2019: DISPLAY. FAILED. (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 - [SDR CA190815010](https://openairdocs.org/sdr/CA190815010), Jun 14, 2019: WIRE. BURNED. (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 WER - [SDR CA190607010](https://openairdocs.org/sdr/CA190607010), Jun 5, 2019: HOSE. DAMAGED. (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), Jun 3, 2019: SUPPORT. CRACKED. (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 PA - [SDR CA190529005](https://openairdocs.org/sdr/CA190529005), May 28, 2019: DISPLAY. FAILED. (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 WIT - [SDR CA190521027](https://openairdocs.org/sdr/CA190521027), May 14, 2019: BATTERY. FAILED. (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 SHU - [SDR CA190514006](https://openairdocs.org/sdr/CA190514006), May 12, 2019: OVEN. SMOKE. (CAN) AT APPROX 1915Z CABIN FLIGHT ATTENDANT SPOTTED SOME SMOKE COMING OUT OF THE BACK OF THE MICROWAVE. THEY IMMEDIATELY ISOLATED THE MICROWAVE ELECTRICALLY AN - [SDR CA190509005](https://openairdocs.org/sdr/CA190509005), May 9, 2019: SOFTWARE. MALFUNCTIONED. (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), May 3, 2019: SUPPORT. CRACKED. (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 CABL - [SDR CA190502004](https://openairdocs.org/sdr/CA190502004), May 1, 2019: SELECTOR VALVE. MALFUNCTIONED. (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 - [SDR CA190501020](https://openairdocs.org/sdr/CA190501020), Apr 30, 2019: FREQUENCY GEN. MALFUNCTIONED. (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 - [SDR CA190430009](https://openairdocs.org/sdr/CA190430009), Apr 29, 2019: DRAIN LINE. SEPARATED. (CAN) CREW DECLARED EMERGENCY: HYDRAULIC SYSTEM #2 FLUID LEVEL DOWN TO 0%. HYDRAULIC FLUID LEAK PRESENT INSIDE AFT EQUIPMENT BAY ASSOCIATED CAS MESSAGE/FAULT CO - [SDR CA190509004](https://openairdocs.org/sdr/CA190509004), Apr 24, 2019: SWITCH. DIRTY. (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 - [SDR CA190425012](https://openairdocs.org/sdr/CA190425012), Apr 23, 2019: ACTUATOR. MALFUNCTIONED. (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 - [SDR CA190506006](https://openairdocs.org/sdr/CA190506006), Apr 22, 2019: CONNECTOR. DAMAGED. (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 AN - [SDR CA190417010](https://openairdocs.org/sdr/CA190417010), Apr 16, 2019: FLT CONTROLS. MALFUNCTIONED. (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 WI - [SDR CA190416006](https://openairdocs.org/sdr/CA190416006), Apr 15, 2019: APU. FIRE. (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 AIRCR - [SDR CA190405009](https://openairdocs.org/sdr/CA190405009), Apr 4, 2019: FMU. MALFUNCTIONED. (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 SUBS - [SDR CA190409010](https://openairdocs.org/sdr/CA190409010), Apr 3, 2019: SERVO. DAMAGED. (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 (I - [SDR CA190328001](https://openairdocs.org/sdr/CA190328001), Mar 26, 2019: PUMP. LEAKING. (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 - [SDR CA190327013](https://openairdocs.org/sdr/CA190327013), Mar 25, 2019: ARM. DAMAGED. (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 TA - [SDR CA190325002](https://openairdocs.org/sdr/CA190325002), Mar 24, 2019: ENGINE. POWER LOSS. (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 N - [SDR CA190318015](https://openairdocs.org/sdr/CA190318015), Mar 13, 2019: VALVE. FAILED. (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 LIMITATIO - [SDR CA190318022](https://openairdocs.org/sdr/CA190318022), Mar 7, 2019: WIRE. BURNED. (CAN) AIRCRAFT 9726 HAD AN ISSUES WITH THE UPPER TAIL NAV LIGHT. AFTER INSVESTIGATION, WHEN DISMANTELING THE BACKSHELL OF CONNECTOR P707 FOR WIRING INSPECTION, - [SDR KKVA20190305002](https://openairdocs.org/sdr/KKVA20190305002), Feb 28, 2019: WARNING SYSTEM. FALSE ACTIVATION. 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 YEL - [SDR CA190304008](https://openairdocs.org/sdr/CA190304008), Feb 24, 2019: BATTERY BOX. CONTAMINATED. (CAN) CUSTOMER REPORTED DEICING FLUID FOUND IN THE BATTERY BOXES. AT EVERY BATTERY INSPECTION WE ARE FINDING TRACES OF DEICING FLUID. THE ONLY LOGICAL EXPLANATI - [SDR CA190322007](https://openairdocs.org/sdr/CA190322007), Dec 20, 2018: BUSHING. MISSING. (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 H - [SDR CA180925008](https://openairdocs.org/sdr/CA180925008), Sep 21, 2018: COMPRESSOR. MALFUNCTIONED. (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 ROT - [SDR CA180925010](https://openairdocs.org/sdr/CA180925010), Sep 21, 2018: CONTROL CABLE. MISALIGNED. (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 - [SDR DXTA201808231283](https://openairdocs.org/sdr/DXTA201808231283), Aug 8, 2018: CONTROLLER. MALFUNCTIONED. DURING ENGINE START AT DESTINATION, HAD BOTH CYAN LEFT AND RIGHT BLEED FAULT CAS MESSAGES AFTER ENGINE START. VERIFIED ON GO, NO GO, OK. AFTER TAKEOFF AND AFTER - [SDR CA180718008](https://openairdocs.org/sdr/CA180718008), Jul 16, 2018: CONTROLLER. BURNED. (CAN) THE CUSTOMER IS REPORTING AN ELECTRICAL BURNING SMELL IN THE BAGGAGE BAY AREA COMING FROM THE ACPC. NO FAULT ON THE AIRCRAFT, A VISUAL INSPECTION OF THE A All 187: https://openairdocs.org/engine/bmw-rolls-br700-710a220/reports.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.