# BMW Rolls BR700-715C130

- Type: Engine model (FAA registry)
- Registry code: 09497
- Manufacturer (registry): BMW ROLLS
- Model: BR700-715C130
- Engine type: Turbo-fan
- Power: 21,430 lb thrust
- Data sheet: [TCDS E00061EN](https://openairdocs.org/tcds/E00061EN) (OpenAirDocs)
- Holder: Rolls-Royce Deutschland Ltd & Co KG
- Installed in: 1 registered aircraft
- Page: https://openairdocs.org/engine/bmw-rolls-br700-715c130

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 2026-21-04](https://openairdocs.org/ad/2026-21-04): Engine (Turbine/Turboprop) · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Nov 23, 2026
- [AD 2023-17-11](https://openairdocs.org/ad/2023-17-11): Turbine Engine Compressor Section · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Sep 20, 2023
- [AD 2021-14-03](https://openairdocs.org/ad/2021-14-03): Turbine Section · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Aug 19, 2021
- [AD 2014-08-05](https://openairdocs.org/ad/2014-08-05): Low-pressure compressor (LPC) case ice impact panels · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective May 23, 2014
- [AD 2014-07-02](https://openairdocs.org/ad/2014-07-02): High-pressure (HP) compressor stages 1 to 6 rotor disc assemblies · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective May 8, 2014
- [AD 2012-14-01](https://openairdocs.org/ad/2012-14-01): LP compressor booster rotor · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Oct 19, 2012
- [AD 2009-07-01 R1](https://openairdocs.org/ad/2009-07-01-R1): High-pressure (HP) turbine stage 1 discs, and HP turbine stage 2 discs · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Aug 6, 2012
- [AD 2009-21-04](https://openairdocs.org/ad/2009-21-04): Engine Failure · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Dec 3, 2009
- [AD 2009-04-13](https://openairdocs.org/ad/2009-04-13): Low pressure (LP) compressor (fan) · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Mar 26, 2009
- [AD 2005-16-12](https://openairdocs.org/ad/2005-16-12): Independent Overspeed Protection (IOP) unit. · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Aug 26, 2005
- [AD 2000-25-51](https://openairdocs.org/ad/2000-25-51): High Pressure Turbine Disks · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Feb 20, 2001

Historical (superseded or no longer in force):

- [AD 2012-26-14](https://openairdocs.org/ad/2012-26-14) (historical): High-pressure (HP) compressor stages 1 to 6 rotor disc assembly · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Jan 10, 2013
- [AD 2009-07-01](https://openairdocs.org/ad/2009-07-01) (historical): High Pressure (HP) Turbine · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Apr 27, 2009

## Registered aircraft (1)

- [N608AT](https://openairdocs.org/aircraft/N608AT): [Delta Air Lines Inc](https://openairdocs.org/faa-owner/DELTA%20AIR%20LINES%20INC), [Atlanta, GA](https://openairdocs.org/faa-place/GA/Atlanta), built 2000, S/N 55081

## 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 20110829020559I](https://openairdocs.org/incident/20110829020559I), Aug 29, 2011: Boeing 717-200 (N608AT), Orlando, FL, Substantial damage. On aug 29, 2011 at 10:55AM flight trs 491 (717-200, N975AT) was struck by a bird during a 5 mile final approach to runway 17L at Orlando International Airport…

## Service difficulty reports (59, newest 50)

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

- [SDR DALA2026031001643](https://openairdocs.org/sdr/DALA2026031001643), Mar 8, 2026: VALVE. BINDING. SHIP 9522 CREW REPORTS STRONG DIRTY SOCK SMELL IN BACK OF AIRCRAFT. CORRECTIVE ACTION: FOUND #2 ENG SOURCE R/R #2 ENG BUFFER AIR VALVE FOUND IT BINDING & STIFF 
- [SDR DALA2026020900919](https://openairdocs.org/sdr/DALA2026020900919), Feb 2, 2026: FMU. FAULTED. ON TAKEOFF AROUND 700 - 1000 FT, HEARD A BANG AND RECEIVED LT ENG COMP STALL MESSAGE. MSG CLEARED 30 SECONDS LATER, RAN QRH AND ALL ENGINE INDICATIONS APPEARED 
- [SDR DALA2026012700606](https://openairdocs.org/sdr/DALA2026012700606), Jan 24, 2026: COMPRESSOR. STALLED. RETURNED TO BDL DUE TO LEFT ENGINE COMPRESSOR STALL. PERFORMED BORESCOPE INSPECTION OF THE ENTIRE LT ENGINE, NO DEFECTS FOUND. REPLACED N2 SPEED PROBE AND RETUR
- [SDR DALA2026010500069](https://openairdocs.org/sdr/DALA2026010500069), Jan 1, 2026: EEC. FAULTED. ATB TO DTW DUE TO LEFT ENGINE COMPRESSOR STALL ON CLIMB OUT. PERFORMED BORO INSP NO DAMAGED FOUND. REPLACED EEC, OPS CHECK NORMAL. (8071484)
- [SDR DALA2025122309342](https://openairdocs.org/sdr/DALA2025122309342), Dec 20, 2025: PRESSURE SWITCH. FAULTED. ATB - RIGHT ENGINE SYSTEM FAIL MESSAGE ALONG WITH A RIGHT ENGINE FUEL FILTER MESSAGE ON CLIMB OUT. INSPECTED FILTERS WITH NO DEBRIS NOTED. BOTH HIGH AND LOW PRE
- [SDR DALA2025122309344](https://openairdocs.org/sdr/DALA2025122309344), Dec 20, 2025: PUMP. FAULTED. THE CREW REPORTED LT HYDRAULIC QTY LOW MESSAGE, FOLLOWED QRH AND LANDED WITH SYSTEM PRESSURE AND QUANTITY. MAINTENANCE REPLACED THE LEFT ENGINE DRIVEN HYDRAULIC
- [SDR DALA2025101707598](https://openairdocs.org/sdr/DALA2025101707598), Oct 14, 2025: IDG. FAULTED. SHIP 9547-MISC/DE- ON DESCENT THE CREW RECEIVED A "RT GEN OFF" MESSAGE WITH THE APU ON MEL. CORRECTIVE ACTION: MAINTENANCE REPLACED THE RIGHT IDG AND PERFORMED 
- [SDR DALA2025091606815](https://openairdocs.org/sdr/DALA2025091606815), Sep 11, 2025: COMPRESSOR. DAMAGED. ATB TO ATL DUE TO NR 1 ENGINE COMPRESSOR STALL ON CLIMB OUT. BORESCOPED LT ENGINE AND FOUND MULTIPLE BLADES IN HPC DAMAGED. REPLACED ENGINE.(7723471)
- [SDR DALA2025081105985](https://openairdocs.org/sdr/DALA2025081105985), Aug 8, 2025: COMPRESSOR. STALLED. SHIP 9505 GOING THRU 10,000 ON CLIMBOUT WE GOT COMPRESSOR STALL TGT HAD AN X OFF AND ON. CORECTIVE ACTION: EPLACED HARNESS PER B717 AMM 77-21. REPLACED ALL 6 TG
- [SDR DALA2025070104879](https://openairdocs.org/sdr/DALA2025070104879), Jun 30, 2025: EEC. FAULTED. SHIP 9505 -ATB- DUE TO LEFT ENGINE NOT MAKING EPR ON CLIMB OUT. CORRECTIVE ACTION: REPLACE EEC, FUEL FLOW TRANSMITTER, AND FMU. NO HELP, REPLACED FUEL PUMP AND 
- [SDR DALA2025030501715](https://openairdocs.org/sdr/DALA2025030501715), Mar 4, 2025: VALVE. STIFF. SHIP 9519 -ATB/FUME/DE- DURING CLIMB OUT AT ABOUT 10K FEET, THE FLIGHT CREW DECLARED AN EMERGENCY WITH ATC AND RETURNED TO MEM DUE TO UNKNOWN ODOR THROUGHOUT TH
- [SDR DALA2025022001287](https://openairdocs.org/sdr/DALA2025022001287), Feb 18, 2025: LOCK LINK ASSY. DAMAGED. SHIP 9524 -IFSD/DE- THE CREW RECEIVED A "LEFT REVERSER UNLOCK" MESSAGE. THE QRH WAS COMPLIED WITH, WHICH INCLUDED SHUTTING DOWN THE LEFT ENGINE. CORRECTIVE ACTI
- [SDR DALA2024121911830](https://openairdocs.org/sdr/DALA2024121911830), Dec 19, 2024: IDG. FAILED. SHIP 9579 -MISC/DE- THE FLIGHT CREW DECLARED AN EMERGENCY WITH ATC FOLLOWING THE "LEFT GENERATOR FAIL" MESSAGE DURING APPROACH INTO PHL. THE APU WAS ALREADY ON 
- [SDR DALA2024072507459](https://openairdocs.org/sdr/DALA2024072507459), Jul 24, 2024: PANEL. DAMAGED. DURING PILOT PRE-FLT WALKAROUND, NOTICED DAMAGE TO THE #2 ENGINGE UPPER THRUST REVERSER PANEL. 6-8 FOOT SECTION OF PANEL WAS MISSING. MAINTENANCE REPLACED THE #
- [SDR DALA2024040103938](https://openairdocs.org/sdr/DALA2024040103938), Mar 29, 2024: GENERATOR. FAILED. SHIP 9586 -DIV- THE FLIGHT WAS DIVERTED TO MCO FOLLOWING THE FAILURE OF THE RIGHT GENERATOR AFTER TAKEOFF, WHILE THE APU GENERATOR WAS ON MEL. THE CAPTAIN DECLA
- [SDR 2023F00200](https://openairdocs.org/sdr/2023F00200), Jun 12, 2023: DISC. CRACKED. MULTIPLE MICRO CRACKS FOUND ON OUTER AIR SEAL F THE LONGEST ONE HAS A RADIAL LENGTH 0.021 INCHES.
- [SDR DALA2023051803951](https://openairdocs.org/sdr/DALA2023051803951), May 15, 2023: UNKNOWN. UNKNOWN. SHIP 9567 -HYD/DE- THE FLIGHT CREW NOTICED A LOSS OF HYDRAULIC FLUID INDICATION WITH THE LEFT SYSTEM. THE QRH WAS COMPLIED WITH AND THE LEFT ENGINE DRIVEN HYDRA
- [SDR DALA202303094717D](https://openairdocs.org/sdr/DALA202303094717D), Mar 8, 2023: DISC. CRACKED. 1 AXIAL CRACK IN AIR SEAL F AREA (ABOVE DIA 15-2) MEASURING ~0.340 INCH 1 CIRCUMFERENTIAL CRACK IN AIR SEAL F AREA (BELOW DIA 15-2) MEASURING ~0.100 INCH
- [SDR HALA2019121900523](https://openairdocs.org/sdr/HALA2019121900523), Dec 18, 2019: IO CARD. FAILED. IN CRUISE FLIGHT ENG L SYS FAIL MESSAGE. // TROUBLESHOOT PER FIM 71-00 TASK 802. RECEIVED EEC-1 CURRENT FAULT 732177 IOP BOX FAULT. REMOVED AND REPLACED LH ENG 
- [SDR HALA2019082600355](https://openairdocs.org/sdr/HALA2019082600355), Aug 22, 2019: PROBE. MALFUNCTIONED. INFLIGHT, RT ENG SYS FAIL. TROUBLESHOT FAULT THROUGH MCDU EEC-2 AND FOUND FAULT TO BE N2 PROBE ELECTRICAL CH-B. REMOVED AND REPLACED N2 SPEED PROBE PER FIM 77-1
- [SDR DALA2019080504575](https://openairdocs.org/sdr/DALA2019080504575), Aug 3, 2019: PACKING. DAMAGED. APPROX 40 MINUTES AFTER TAKEOFF, THE LAT FUEL UNBAL MESSAGE ANNUNCIATED. REBALANCED FUEL TRANSFER AND DIAGNOSED LEFT FUEL SYSTEM WAS LOSING FUEL. MAINTENANCE FO
- [SDR DALA2018070404366](https://openairdocs.org/sdr/DALA2018070404366), Jul 3, 2018: COWLING. CRACKED. CRACKS ON INLET COWL BULLNOSE AROUND FASTENERS IN INTERIOR MARKED. REPLACED NR 1 ENGINE INLET COWL REF AMM 71-11-05.
- [SDR DALA2017122108917](https://openairdocs.org/sdr/DALA2017122108917), Dec 20, 2017: ENGINE. ODOR. ODOR PREVALENT AFTER TAKEOFF AND THROUGHOUT FLIGHT. ODOR STRONGEST FROM RT PACK ON THE NR 2 ENGINE BLEED. NO CONTAMINATION WAS FOUND. FOUND TURBINE OIL ODOR ISO
- [SDR DALA2017121108490](https://openairdocs.org/sdr/DALA2017121108490), Dec 9, 2017: ENGINE. SURGES. SHIP 9573 - THE CREW EXPERIENCED AN ENGINE SURGE AND HIGH EXHAUST TEMPERATURES WITH THE #2 ENGINE SO THE FLIGHT DIVERTED TO CAE. THE PILOT DID REDUCE POWER ON T
- [SDR HALA2017111000278](https://openairdocs.org/sdr/HALA2017111000278), Nov 10, 2017: ENGINE. MALFUNCTIONED. NR 2 ENGINE COMPRESSOR STALL. REMOVED AND REPLACED NR 2 ENGINE.
- [SDR DALA2016121509877](https://openairdocs.org/sdr/DALA2016121509877), Dec 9, 2016: ENGINE. OVERHEATED. THE CREW DIVERTED, FOLLOWING AN OVERHEAT OF THE LEFT ENGINE BEARING AND ASSOCIATED ROLLBACK. THE ENGINE WAS REPLACED.
- [SDR ZZDA2016F00063](https://openairdocs.org/sdr/ZZDA2016F00063), Feb 16, 2016: VANE. LOOSE. DURING UNSCHEDULED NON-ROUTINE CHECK, INBD FLAP FORWARD MOVABLE VANE HAS PLAY AT TORQUE TUBE.
- [SDR DALA2014091505043](https://openairdocs.org/sdr/DALA2014091505043), Sep 14, 2014: O-RING. LEAKING. ON APPROACH, LOST RT HYD SYS. PERFORMED ALT EXTEND AND DOORS WERE EXTENDED ON TOUCHDOWN. REPLACED O-RING ON RT THRUST REVERSER ACCUMULATOR. REPLACED NR 2 EDP AN
- [SDR SWAA2014082131063](https://openairdocs.org/sdr/SWAA2014082131063), Aug 18, 2014: O-RING. FAULTY. APPROACHING AIRPORT NOTICED AN IMBALANCE OF 900LBS LT TANK LOW. R & R O RING IAW MM.
- [SDR SWAA2014052828420](https://openairdocs.org/sdr/SWAA2014052828420), May 26, 2014: COMPRESSOR. DAMAGED. DIVERSION COMPRESSOR STALLED ON CLIMB OUT. FOUND STAGE 4 HPC DAMAGE OUT OF LIMITS NR 1 ENG. R & R THE NR 1 ENG ASSEMBLY.
- [SDR SWAA2014030625799](https://openairdocs.org/sdr/SWAA2014030625799), Mar 6, 2014: COMPRESSOR. STALLED. AIR TURN BACK, ON DEPARTURE LT ENG COMPRESSOR STALL 2 TIMES WITHIN 3 MINUTES BETWEEN COMPRESSOR STALLS. R & R NR 1 ENG IAW TASK CARD.
- [SDR CA140303018](https://openairdocs.org/sdr/CA140303018), Mar 3, 2014: TUBE. WORN. (CAN) IFSD FUEL SHUTOFF CABLE ENGAGEMENT BR715, ESN 13195 SHUTS DOWN DURING AIRCRAFT`S APPROACH PHASE, IFSD, FUEL SHUTOFF VALVE WAS ENGAGED THROUGH ITS CABLE/HA
- [SDR SWAA2014012824651](https://openairdocs.org/sdr/SWAA2014012824651), Jan 23, 2014: COMPRESSOR. STALLED. DIVERSION RT ENG SURGED, COMPRESSOR STALLED ENROUTE. R & R NR 2 ENG IAW MT.
- [SDR SWAA2013121123170](https://openairdocs.org/sdr/SWAA2013121123170), Dec 8, 2013: COMPRESSOR. STALLED. AIR TURN BACK DECLARED EMERGENCY RT ENG COMPRESSOR STALL ALERTS INCLUDED COMPRESSOR STALL & ENG RT SYSTEM FAIL. ENG BROUGHT TO IDLE, NOT SHUT DOWN. R & R NR 2 E
- [SDR SWAA2013111922553](https://openairdocs.org/sdr/SWAA2013111922553), Nov 13, 2013: ENGINE. FAILED. DECLARED EMERGENCY, SEVERAL COMPRESSOR STALLS ON DESCENT RAW CHECK LIST. COMPRESSOR STALL ON FINAL APPROACH WITH THROTTLE AT IDLE RT ENGINE ONLY. R & R NR 2 ENG
- [SDR SWAA2013102821552](https://openairdocs.org/sdr/SWAA2013102821552), Oct 28, 2013: COMPRESSOR. STALLED. AIR TURN BACK, AT 12K FEET IN CLIMB LOUD BANG MOMENTARILY COMPRESSOR STALL ALERT. R & R NR 2 ENGINE IAW TC.
- [SDR CA130911012](https://openairdocs.org/sdr/CA130911012), Sep 11, 2013: TURBINE. DAMAGED. (CAN) ACFT HAD AN LPT FAIRING RELEASE IN SERVICE, PRELIMINARY INVESTIGATION REVEALS THAT SOME SCREWS ARE MISSING AND OTHERS ARE STILL INSTALLED, HOLES ARE ELONG
- [SDR SWAA2013050815841](https://openairdocs.org/sdr/SWAA2013050815841), May 7, 2013: COMPRESSOR. STALLED. AIR TURNBACK - AFTER TAKEOFF NR 2 ENGINE COMPRESSOR STALL. REMOVED AND REPLACED NR 2 ENGINE PER TC AND MM.
- [SDR SWAA2013050115387](https://openairdocs.org/sdr/SWAA2013050115387), Apr 28, 2013: COMPRESSOR. STALLED. INFLIGHT SHUTDOWN/AIR RETURN/DECLARED EMERGENCY. NR 2 ENGINE COMPRESSOR STALL DURING CLIMBOUT. REMOVED AND REPLACED NR 2 ENGINE PER TC.
- [SDR SWAA2012030902016](https://openairdocs.org/sdr/SWAA2012030902016), Mar 8, 2012: FUEL FILTER. LEAKING. DIVERSION - FUEL LEAK RIGHT ENG NOTED AT CRUISE FL 340 AFTER DISPLAY OF LAT FUEL UNBAL ALERT. REMOVED AND REPLACED RT ENG FUEL FILTER ASSY PER MM.
- [SDR SWAA2012030802013](https://openairdocs.org/sdr/SWAA2012030802013), Mar 6, 2012: O-RING. LEAKING. FUEL/BURN WAS 1900 LBS MORE THAN FLIGHT PLANNED. CROSS FEED 15000 LBS. DURING FLIGHT, ON APPROACH A/C FOLLOWING NOTICED SOMETHING TRAILING THE NR 1 ENGINE. FOUN
- [SDR ZZDA2012034](https://openairdocs.org/sdr/ZZDA2012034), Dec 22, 2011: ENGINE. MALFUNCTIONED. LT ENGINE SHUT DOWN DUE TO OIL PRESS "0". REMOVED AND REPLACED LEFT ENG REF TASK CARD# 603 BR 700-715.
- [SDR CA111108002](https://openairdocs.org/sdr/CA111108002), Oct 12, 2011: BEARING. FAILED. (CAN) DURING TAXI IN, SIGNIFICANT VIBRATION WAS FELT IN THE ACFT WHILE STOPPED. ALL ENGINE INDICATIONS WERE NORMAL. ON SHUTDOWN, NR 1 ENGINE WAS VERY SMOKEY. RE
- [SDR CA111117001](https://openairdocs.org/sdr/CA111117001), Oct 12, 2011: BLADES. FAILED. (CAN) ENGINE RETURNED TO MFG FOR METAL DEBRIS IN TAIL PIPE. DISASSEMBLY OF ENGINE CONFIRMS 2 OFF, HP 1, TURBINE BLADE FAILURE BELOW, PLATFORM. ALL REMAINING STA
- [SDR ZZDA2011705](https://openairdocs.org/sdr/ZZDA2011705), Sep 9, 2011: ENGINE. FAILED. LEFT ENGINE FAILURE AT 22,000 FEET. REMOVED AND REPLACED NR 1 ENGINE ON W/O 247893, TASK CARD 603. OPS AND LEAK CHECK GOOD. AUTOLAND ACCOMPLISHED W/O 247893 TAS
- [SDR CA110929008](https://openairdocs.org/sdr/CA110929008), Aug 17, 2011: COMPRESSOR BLADE. BROKEN. (CAN) ENGINE BEING INDUCTED AT MFG. ENGINE REMOVED FOR HIGH TIME AND DURING BOROSCOPE OF ENGINE, HEAVY DAMAGE FOUND ON COMPRESSOR BLADES, STG 3, 4, 5, 6 AND 10.
- [SDR ZZDA2011402](https://openairdocs.org/sdr/ZZDA2011402), Apr 19, 2011: ENGINE. MALFUNCTIONED. RT ENG FAILURE ON TAKEOFF AT 300 FT. REMOVED AND REPLACED RT ENG PER TASK CARD 603.
- [SDR ZZDA2011009](https://openairdocs.org/sdr/ZZDA2011009), Jan 9, 2011: ENGINE. DAMAGED. LEFT ENGINE SEVERE DAMAGE. REMOVED AND REPLACED NR 1 ENGINE PER W/O 232308 AND TASK CARD 603, AUTOLAND ACCOMPLISHED ON TASK CARD 625 ALL OPS & LEAK CHECK GOOD.
- [SDR ZZDA2010656](https://openairdocs.org/sdr/ZZDA2010656), Dec 25, 2010: COMPRESSOR. STALLED. LEFT ENGINE COMPRESSOR STALL ALERT IN CLIMB THROUGH FL230. TRANSFERRED TO NRWC N082031 ITEM 1, ENGINE FAILED BORESCOPE, REF ITEM 3 LOG PAGE 1696965.
- [SDR ZZDA2010629](https://openairdocs.org/sdr/ZZDA2010629), Dec 10, 2010: LONGERON. CRACKED. LT FUSELAGE LONGERON, STA 1144 TO L21L, CRACKED. ACCOMPLISHED FUSELAGE LONGERON SPLICE REPAIR IAW EA 17-53-02784IR.

All 59: https://openairdocs.org/engine/bmw-rolls-br700-715c130/reports.md

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