# BMW Rolls BR700-715A130

- Type: Engine model (FAA registry)
- Registry code: 09499
- Manufacturer (registry): BMW ROLLS
- Model: BR700-715A130
- Engine type: Turbo-fan
- Power: 18,710 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-br700-715a130

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)

- [N886BC](https://openairdocs.org/aircraft/N886BC): [Delta Air Lines Inc](https://openairdocs.org/faa-owner/DELTA%20AIR%20LINES%20INC), [Atlanta, GA](https://openairdocs.org/faa-place/GA/Atlanta), S/N 55191

## NTSB investigations

None matched to aircraft with this engine model.

## FAA accident and incident reports

None matched to aircraft with this engine model.

## Service difficulty reports (358, newest 50)

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

- [SDR DALA2026102005747](https://openairdocs.org/sdr/DALA2026102005747), Oct 19, 2026: ENGINE. FAILED. DECLARED AN EMERGENCY AND DIVERTED TO BNA DUE TO RIGHT ENGINE FAILURE. INSPECTED RIGHT ENGINE CHIP DETECTOR AND FOUND METAL DEBRIS. R & R ENGINE #2 IAW AMDS JIC
- [SDR DALA2026082104770](https://openairdocs.org/sdr/DALA2026082104770), Aug 19, 2026: FMU. FAULTED. ABORTED TAKEOFF AT 110 KTS DUE TO LT ENGINE UNABLE TO MAKE TAKEOFF POWER. R & R NR 1 ENGINE FMU IAW AMM 73-21 AND R & R NR 1 ENGINE FUEL PUMP IAW AMM 73-12. (92
- [SDR DALA2026072804383](https://openairdocs.org/sdr/DALA2026072804383), Jul 26, 2026: COMPRESSOR. STALLED. ATB- RETURNED TO ATL DUE TO RIGHT ENGINE COMPRESSOR STALL. CORRECTIVE ACTION: RIGHT ENGINE FAILED HPC BORESCOPE. REPLACED NR 2 ENGINE. (9087110) AIRCRAFT GROUND
- [SDR DALA2026071304130](https://openairdocs.org/sdr/DALA2026071304130), Jul 10, 2026: O-RING. LEAKING. NR 1 ENGINE FUEL LEAK ON WALK AROUND STRONG FUEL ODOR ON APU AIR. R & R O-RING IAW AIPC 73-12-05-22. (8831910) (AIRCRAFT GROUNDED)
- [SDR ASAA2026063065628](https://openairdocs.org/sdr/ASAA2026063065628), Jun 30, 2026: COMPRESSOR. STALLED. RETURN TO AIRPORT -LEFT ENGINE COMP STALL ON TAKEOFF DOUBLE BANG AT GEAR RETRACTION - RAN AT IDLE. GROUNDED - YES. PERFORME EEC BITE & FAULT REVIEW - NO FAULTS.
- [SDR DALA2026042302606](https://openairdocs.org/sdr/DALA2026042302606), Apr 23, 2026: ACOUSTIC LINER. DAMAGED. DURING SERVICE CHECK FOUND DAMAGE IN #1 ENG INLET COWEL ACOUSTIC LINER. REPAIRED DAMAGE IN #1 ENG INLET COWEL ACOUSTIC LINER PER B717 SRM 54-10-01 (7985278) (AI
- [SDR DALA2026041702450](https://openairdocs.org/sdr/DALA2026041702450), Apr 14, 2026: ENGINE. FIRE. FIRE- DURING RIGHT ENGINE START, TGT ROSE RAPIDLY ALONG WITH AUDIBLE STALL. ENGINE SHUTDOWN AND FIRE BOTTLE DISCHARGED. PERFORMED BORESCOPE INSPECTION OF LPC AN
- [SDR DALA2026040102117](https://openairdocs.org/sdr/DALA2026040102117), Mar 30, 2026: COMPRESSOR. STALLED. CREW REJECTED TAKEOFF AT 70 KNOTS DUE TO RIGHT ENGINE COMPRESSOR STALL. PERFORMED BORESCOPE INSPECTION OF RIGHT ENGINE AND FOUND MULTIPLE HPC BLADES DAMAGED. RE
- [SDR DALA2026031701819](https://openairdocs.org/sdr/DALA2026031701819), Mar 14, 2026: ENGINE. BIRD INGESTION. IFSD - APPROXIMATELY 13 MINUTES FROM LANDING IN STL, BIRD STRIKE RIGHT ENGINE WITH VIBES. CREW PERFORMED IFSD. REPLACED #2 ENGINE.
- [SDR DALA2026020900918](https://openairdocs.org/sdr/DALA2026020900918), Feb 2, 2026: BLADES. DAMAGED. RTO- APPROXIMATELY 25 KNOTS DUE TO A LT ENGINE COMPRESSOR STALL MESSAGE ALONG WITH AN AUDIBLE STALL. PERFORMED BORESCOPE INSPECTION OF LT ENGINE AND FOUND MULTI
- [SDR DALA2026012200496](https://openairdocs.org/sdr/DALA2026012200496), Jan 17, 2026: FADEC. FAULTED. FLIGHT CREW DIVERTED TO ATL DUE TO RIGHT ENGINE FADEC ALTERNATE MODE CAUSING FLIGHT TO BE REMOVED FROM CAT 1/2/3 AND RVSM. REMOVED AND REPLACED RIGHT ENGINE P20
- [SDR DALA2025111808427](https://openairdocs.org/sdr/DALA2025111808427), Nov 14, 2025: ENGINE. SURGES. ATB- RETURNED TO MSP DUE TO LEFT ENGINE SURGING. REDUCED THRUST AND SURGING STOPPED. REPLACED LEFT ENGINE. OPS CHECK NORMAL. (8225854).
- [SDR DALA2025090206467](https://openairdocs.org/sdr/DALA2025090206467), Aug 27, 2025: COMPRESSOR. STALLED. ATB TO ORD DUE TO LT ENGINE COMPRESSOR STALL. REPLACED LEFT ENGINE. (7851686)
- [SDR HALA20250716038](https://openairdocs.org/sdr/HALA20250716038), Jul 14, 2025: COMPRESSOR. STALLED. LEFT ENGINE COMPRESSOR STALL ON TAKEOFF. PERFORMED B717 FIM TASK 72-00 TASK 801 AND AMM 72-00-00-200-801 UP TO STEP 2(E)4 21794. REMOVED AND REPLACED #1 ENG. OK
- [SDR DALA2025071405285](https://openairdocs.org/sdr/DALA2025071405285), Jul 12, 2025: ENGINE. FAULTED. SHIP 9558 - RTO - CREW REPORTED WITH AUTO-THROTTLE ENGAGED AT 60KNTS RIGHT THROTTLE RETARDED. P30 FAULT, INSPECTED FOR LEAKS/BLOCKAGE WITH NO FINDINGS. REPLACED
- [SDR HALA20250627035](https://openairdocs.org/sdr/HALA20250627035), Jun 24, 2025: COMPRESSOR. STALLED. DIVERSION TO HNL - LT ENG COMPRESSOR STALL AT 400 FT, 2 LOUD THUDS BEFORE FOLLOWING PHASE 1'S. NO MORE THUDS TO FOLLOWS LEVEL 2 MESSAGE COMPRESSOR STALL. FOUND 
- [SDR HALA20250218008](https://openairdocs.org/sdr/HALA20250218008), Feb 16, 2025: PUMP. FAULTED. "INFO TO MX" RTO;BTB TAKEOFF AND THROTTLE ADVANCE LEFT ENGINE N1 STAGNANT. L ENGINE N1 AT 25 WHEN R ENGINE AT N1 55. REMOVED AND REPLACED FUEL PUMP ENG #1 REF A
- [SDR HALA20250213006](https://openairdocs.org/sdr/HALA20250213006), Feb 12, 2025: COMPRESSOR. STALLED. LVL 2- ENG L COMP STALL ON EAD DURING LANDING ( NO OTHER INDICATIONS). PERFORMED FIM 72-00 TASK 803, REMOVED AND REPLACED LH ENG N2 SHARED SPEED PROBE PER AMM 7
- [SDR HALA20250206004](https://openairdocs.org/sdr/HALA20250206004), Feb 5, 2025: BLEED VALVE. FAULTED. DIVERSION TO HNL. DURING FLIGHT LEFT BLEED FLUCTUATES FROM 8-67. WITH NO POWER CHANGES FLUCTUATIONS HAPPENING DURING ALL PHASES OF FLIGHT. REMOVED AND REPLACED 
- [SDR HALA20250121002](https://openairdocs.org/sdr/HALA20250121002), Jan 19, 2025: PUMP. FAULTED. BTB "HYD L PUMP FIL" AFTER ENG START . PERFORMED FAULT ISOLATION PROCEDURE 29-10 TASK 801, UP TO ND INCLUDING STEP 801. F. (3) 01/19/2025. REMOVED AND REPLACED 
- [SDR DALA2025010800167](https://openairdocs.org/sdr/DALA2025010800167), Dec 20, 2024: BLADES. DAMAGED. SHIP 9502 -ATB- THE CREW RETURNED THE AIRCRAFT TO PHL DUE TO MULTIPLE COMPRESSOR STALLS DURING CLIMB OUT. CORRECTIVE ACTION: INSPECTION PERFORMED BORESCOPE INSP
- [SDR HALA20241018054](https://openairdocs.org/sdr/HALA20241018054), Oct 17, 2024: COALESCER BAG. ODOR. AFTER #2 ENG START (AT THE GATE) + R PACK SWITCH ON ... FA REPORTED BURNING RUBBER SMELL IN FWD GALLEY. PILOT ASSITED WITH RUNNING #2 ENG AND RT PACK. ENGINE AM
- [SDR DALA2024062706579](https://openairdocs.org/sdr/DALA2024062706579), Jun 25, 2024: HPC. DAMAGED. SHIP 9538 -ATO- ABORTED TAKEOFF AT APPROXIMATELY 80 KNOTS DUE TO SUSPECTED RIGHT ENGINE SUSPECTED COMPRESSOR STALL. CORRECTIVE ACTION: PERFORMED BORESCOPE INSPE
- [SDR DALA2024060405771](https://openairdocs.org/sdr/DALA2024060405771), Jun 2, 2024: ENGINE. STALLED. SHIP 9546 -DIV/IFSD/DE- THE FLIGHT CREW NOTED THAT THE #1 ENGINE STALLED MULTIPLE TIMES IN FLIGHT WHICH RESULTED IN A "LT ENG SYS FAIL" MESSAGE. FLIGHT CREW SHU
- [SDR HALA20240528028](https://openairdocs.org/sdr/HALA20240528028), May 26, 2024: COMPRESSOR. STALLED. LEFT ENG COMPRESSOR STALL. REMOVED ENG1 BOOSTER BLEED VALVE (BBV) PER AMM 75-32-01 5/26/24 24713. INSTALLED BOOSTER BLEED VALVE IN SERVCABLE CONDITION ON #1 ENG
- [SDR HALA20240528027](https://openairdocs.org/sdr/HALA20240528027), May 25, 2024: COMPRESSOR. STALLED. ENG R COMP STALL IN CRUISE. COMPLIED WITH QRH PROCEDURE. "ENGINE VIB HI" AT HIGH POWER SETTINGS. PREPPED FOR BOROSCOPE INSP. PER AMM 72-00-00-200-801 TO STEP 2E
- [SDR HALA20240524026](https://openairdocs.org/sdr/HALA20240524026), May 23, 2024: COMPRESSOR. STALLED. ENG L COMP STALL ON TAKE OFF @ 1600' (ATB). PERFORMED EEC 1 BITE - FC 801105 STARTER AIR VALVE OUT OF POSITION. REPLACED #1 ENGINE START VALVE PER AMM 80-11-03.
- [SDR HALA20240521025](https://openairdocs.org/sdr/HALA20240521025), May 20, 2024: COMPRESSOR. STALLED. ATB - ENG L. COMP STALL @ APPX 1500' ON CLIMBOUT. CONDITION IMPROVED ON POWER REDUCTION. NORMAL LANDING PERFORMED. COMPLETED INSPECTION OF THE ENGINE AFTER HIGH
- [SDR HALA20240422021](https://openairdocs.org/sdr/HALA20240422021), Apr 19, 2024: EEC. FAULTED. ATB - ENG LEFT SYS FAIL. PERFORMED WIRE CHECK PER FIM 77-21 TASK 803 ENGINE 1 J8, PIN 42 AND 43 - AVERAGE 9.15 OHMS NO SHORT TO GROUND. J7, PIN 42 AND 43 - AVER
- [SDR HALA20240403018](https://openairdocs.org/sdr/HALA20240403018), Apr 2, 2024: ENGINE. FAULTED. FLIGHT DECK CREW AND CABIN HEARD 2 LOUD POPS. ENG LEFT COMPRESSOR STALL ALERT CAME ON. CREW FOLLOWED QRH CHECKLIST, LEFT ENGINE WAS SHUT DOWN. ENG GAUGES SHOWED
- [SDR HALA20240405019](https://openairdocs.org/sdr/HALA20240405019), Apr 2, 2024: INDICATION SYS. FALSE INDICATION. HYD L TEMP HI INDICATION DURING TAXI ONTO RUNWAY EXIT RUNWAY RETURN TO GATE AFTER CYCLING FLIGHT CONTROLS AND INDICATION REMAINING. PERFORMED FIM 29-30 TASK 803
- [SDR HALA20240401017](https://openairdocs.org/sdr/HALA20240401017), Mar 30, 2024: BLADE. DAMAGED. #5 FAN BLADE #2 ENGINE MAJOR DAMAGE. REMOVED #2 ENG BLADE SET PER AMM72-38-15. 17601 3-29-24 PERFORMED INSPECTION OF #2 ENGINE FOR FOD PER AMM 72-00-00--200-809
- [SDR HALA20240102001](https://openairdocs.org/sdr/HALA20240102001), Dec 29, 2023: UNKNOWN. UNKNOWN. BTB L ENGINE COMPRESSOR STALL ON TAKEOFF ROLL AS SOON AS TAKEOFF POWER APPLIED LOUD BANG. REMOVED L/H ENG PER T/C E1128-717-71-003-REMOVAL W/O 280784
- [SDR HALA20231219051](https://openairdocs.org/sdr/HALA20231219051), Dec 19, 2023: COMPUTER. FAULTY. ATB - DUAL FMS FAIL INFLIGHT. PERFORMED FIM 34-63 TASK 830 "FMS DUAL FAIL". VIA 1 & 2 RTS PER AMM 31-43-00-741-803, TESTS OK. REMOVED AND REPLACED FCC-1 AS PREC
- [SDR HALA202310230046](https://openairdocs.org/sdr/HALA202310230046), Oct 20, 2023: UNKNOWN. UNKNOWN. AUDIBLE BANG. FLASH COMPRESSOR STALL EAD; RIGHT ENGINE. PERFORMED VISUAL INSPECTION OF INLET AND EXHAUST. LOOKS GOOD PER AMM 72-00-00-200-801. CHECKED CHIP DETE
- [SDR HALA2023081000037](https://openairdocs.org/sdr/HALA2023081000037), Aug 8, 2023: EEC. FAULTY. ATB - ENG L SYS FAIL. EE 2 FAULT REVIEW INDICATED NO DISPATCH FAULT CODES 732165 & 732166 (EEC BOX FAULT). REMOVED AND REPLACED EEC PER AMM 73-21-01.RTS OK. IDL
- [SDR HALA2023061400033](https://openairdocs.org/sdr/HALA2023061400033), Jun 13, 2023: UNKNOWN. UNKNOWN. ON CLIMBOUT LEFT ENGINE COMPRESSOR STALL. RETURNED BACK TO AIRPORT ATB. FOUND LEFT ENGINE NOSE CONE MISSING PROTECTIVE COATING. PERFOMED INSPECTION AFTER HIGH P
- [SDR HALA2022072500136](https://openairdocs.org/sdr/HALA2022072500136), Jul 23, 2022: NONE. NONE. ATO - L ENG COMPRESSOR STALL ON TAKEOFF.// L/H ENG REMOVED AND REPLACED PER TC E1128-717-72-003-REMOVAL AND 71-HWI-00-02. OK FOR SERVICE.
- [SDR HALA2022071400129](https://openairdocs.org/sdr/HALA2022071400129), Jul 14, 2022: PROBE. FAILED. ATB ENG L FADEC ALTN DISPLAYED. FAULTING 732116 P20/T20 PROBE. REMOVED AND REPLACED P20/T20 PROBE PER FIM 73-21 TASK 816. RTS TEST FPR P20/T20 PROBE FAILED. AS 
- [SDR HALA2022052300104](https://openairdocs.org/sdr/HALA2022052300104), May 22, 2022: NONE. NONE. ATB- ENG L FADEC ALTERNATE (AIRBORNE) WOULD NOT RESET // PERFORMED FIM 71-00 TASK 812. NO FAULTS FOUND. RAN #1 ENG TWICE. BOTH RUNS NO DEFECTS NOTED. OK FOR SVC
- [SDR DALA2022050503143](https://openairdocs.org/sdr/DALA2022050503143), May 5, 2022: COMPRESSOR. STALLED. SHIP 9585 - THE CREW ABORTED THE TAKE-OFF AT 103 KNOTS FOLLOWING THE #2 ENGINE COMPRESSOR STALL AFTER INGESTING A MYLAR BALLOON FLOATING OVER THE RUNWAY. CORREC
- [SDR HALA2021120800183](https://openairdocs.org/sdr/HALA2021120800183), Dec 7, 2021: ENGINE. INOPERATIVE. CREW REPORTED THAT INBND TO OGG THEY HAD ENG1 BRG OVHT MSG, PER FCOM PROCEDURES CREW SHUT DOWN AFFECTED ENG // MX TROUBLESHOOTING, FOUND METAL FINDINGS FROM OIL
- [SDR HALA2021080300094](https://openairdocs.org/sdr/HALA2021080300094), Aug 3, 2021: SENSE LINE. CRACKED. ATB - LEFT ENGINE COMPRESSOR STALL FOLLOWED BY ENG L SYS FAIL IN FLIGHT. // FAULT CODE 732178. PERFORMED FIM 73-21 TASK 873, FOUND P30 SENSE LINE P/N BRH17623 C
- [SDR HALA2020092800188](https://openairdocs.org/sdr/HALA2020092800188), Sep 26, 2020: EEC. DEFECTIVE. ATB AT CRUISE JUST PRIOR TO DESCENT "SELECT FADEC ALTN" MSG CAME ON LT ENGINE PERFORMED QRH PROCEDURE. ATB TO HNL ADVISED BY MOC. PERFORMED BITE TEST OF EEC1, P
- [SDR HALA2020073000160](https://openairdocs.org/sdr/HALA2020073000160), Jul 29, 2020: PROBE. MALFUNCTIONED. RIGHT ENGINE IGNITER INTERMITTENTLY COMES ON IN IDLE DURING DESCENT. PERFORMED FIM 72-00, TASK 803, REMOVED & REPLACED N2 SPEED PROBE IAW AMM 77-12-01, OPS & LE
- [SDR HALA2020061000124](https://openairdocs.org/sdr/HALA2020061000124), Jun 9, 2020: UNKNOWN. UNKNOWN. IN FLIGHT - ENG L FUEL PRESS FUEL LINES IN FUEL PAGE WERE GREEN. NO DEVIATIONS ON ENGINE INDICATIONS. FROM OTHER ENGINE. CREW DECLARED AN EMERGENCY. PERFORMED F
- [SDR HALA2020013110023](https://openairdocs.org/sdr/HALA2020013110023), Jan 30, 2020: WARNING MESSAGE. ILLUMINATED. ENGINE LEFT FUEL PRESSURE ON STATUS PAGE., OK TO CONTINUE, DEFERED PER MEL 73-33-01
- [SDR HALA2020011400014](https://openairdocs.org/sdr/HALA2020011400014), Jan 11, 2020: EEC. MALFUNCTIONED. DURING CLIMB OUT, "ENG L FADEC ALT" ALERT DISPLAYED. WOULD NOT RESET - ATB. PERFORMED FIM 73-21 TASK 814. OPS CHECK GOOD. FAULT CLEARED. OK FOR SVC. REMOVED AND
- [SDR HALA2019102100429](https://openairdocs.org/sdr/HALA2019102100429), Oct 19, 2019: EEC. FAULTED. ATB - SEL FADEC ALTN MSG FL210 FOR #2 ENGINE.// UPON FURTHER INVESTIGATION, FOUND FAULT CODES 732115, 732116. REMOVED AND REPLACED P20/T20 PROBE PER FIM 73-21-0
- [SDR HALA2019100400400](https://openairdocs.org/sdr/HALA2019100400400), Oct 3, 2019: OIL SYSTEM. OVERSERVICED. SMELL IN CABIN AND COCKPIT-DESCRIBED AS BURNING PLASTIC, OILY, VOMIT 2-3 MINUTES AFTER TAKEOFF. SMELL LASTED 1-2 MINUTES. // FOUND ENGINE 1 AND 2 OIL OVER SERVI

All 358: https://openairdocs.org/engine/bmw-rolls-br700-715a130/reports.md

## PMA parts (OpenAirDocs) (171, first 50)

Current parts manufacturer approvals (PMA): parts the FAA has approved companies to make as replacements or modifications. Each record lists its models as free text; OpenAirDocs matched them to this engine model on its data sheet, so check the FAA record before relying on it. Newest first.

- [AAP-3502129-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID118286979320251125143635.0001): Bearing. Approved Air Parts, LLC · PMA PQ4173NE · Replaces Honeywell 3502129-1 · Nov 6, 2025
- [AAP-3177068-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID118354953420241011133357.0001): Bearing. Approved Air Parts Co Inc · PMA PQ4173NE · Replaces Honeywell P/N 3177068-1 · Sep 23, 2024
- [TA027029JP-02](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID108231829620240301165900.0001): Clamp, Cushioned. Jet Parts Engineering Inc · PMA PQ1739CE · Replaces TA027029-02 · Dec 15, 2023
- [3505934-8](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID176205137120230907182128.0001): Air Turbine Starter. Honeywell International Inc. · PMA PQ1222NM · Replaces 3505934-8 · Mar 10, 2023
- [3291678-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID172459269620230907182117.0001): Valve, Start ER Air. Honeywell International Inc. · PMA PQ1222NM · Replaces 3291678-1 · Mar 10, 2023
- [3504779-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID170066912420230907182119.0001): Starter QAD Clamp. Honeywell International Inc. · PMA PQ1222NM · Replaces 3504779-1 · Mar 10, 2023
- [3504780-5](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID169412422320230907182120.0001): Starter QAD Adapter. Honeywell International Inc. · PMA PQ1222NM · Replaces 3504780-5 · Mar 10, 2023
- [3291678-2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID165416002120230907182116.0001): Starter, Air Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 3291678-2 · Mar 10, 2023
- [3505934-7](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID145208011220230907182134.0001): Air Turbine Starter. Honeywell International Inc. · PMA PQ1222NM · Replaces 3505934-7 · Mar 10, 2023
- [3505934-6](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID141655170020230907182121.0001): Air Turbine Starter. Honeywell International Inc. · PMA PQ1222NM · Replaces 3505934-6 · Mar 10, 2023
- [3505934-11](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID119992863620230907182129.0001): Air Turbine Starter. Honeywell International Inc. · PMA PQ1222NM · Replaces 3505934-11 · Mar 10, 2023
- [3291182-4](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID111758177320230907182118.0001): Air Starter Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 3291182-4 · Mar 10, 2023
- [EB100256D](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID161275015220220811183156.0001): Valve, Bleed Stage 5. Meggitt (North Hollywood) Inc · PMA PQ0550NM · Replaces EB100256D · Aug 1, 2022
- [ED100273B](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID158530101320220811183158.0001): Pipe, Stand Bleed Valve. Meggitt (North Hollywood) Inc · PMA PQ0550NM · Replaces ED100273B · Aug 1, 2022
- [EB100258D](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID138539631720220811183157.0001): Valve, Bleed Stage 8. Meggitt (North Hollywood) Inc · PMA PQ0550NM · Replaces EB100258D · Aug 1, 2022
- [EA101205B](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID137954118120220811183156.0001): Solenoid Handling Bleed Valve. Meggitt (North Hollywood) Inc · PMA PQ0550NM · Replaces EA101205B · Aug 1, 2022
- [ED100257B](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID122004898920220811183157.0001): Pipe, Stand Bleed Valve. Meggitt (North Hollywood) Inc · PMA PQ0550NM · Replaces ED100257B · Aug 1, 2022
- [9-217-49](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID150974614720220803181521.0001): Fuel Flow Transmitter. Eldec Corporation · PMA PQ0079NM · Replaces 9-217-49 · Jul 12, 2022
- [AAP-3502859- 1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID197353194120230331124852.0001): Bearing, Ball. Approved Air Parts Co Inc · PMA PQ4173NE · Replaces Honeywell P/N: 3502859-1 · Jun 2, 2021
- [AAP-3502689-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID183644830020230331124834.0001): Bearing, Ball. Approved Air Parts Co Inc · PMA PQ4173NE · Replaces Honeywell P/N: 3502689-1 · Jun 2, 2021
- [M58163-8](https://drs.faa.gov/browse/excelExternalWindow/D75531A7A50DF455862586010063CD06.0001): Ring-Piston. Jet Avion Corporation A HEICO Aerospace Company · PMA PQ1015CE · Replaces Collins Aerospace P/N 58163-8 · Sep 30, 2020
- [M58163-21](https://drs.faa.gov/browse/excelExternalWindow/A3D22A1662A60752862586010063CD49.0001): Ring-Piston. Jet Avion Corporation A HEICO Aerospace Company · PMA PQ1015CE · Replaces Collins Aerospace P/N 58163-21 · Sep 30, 2020
- [P3A1830](https://drs.faa.gov/browse/excelExternalWindow/15017AB6256A973D862584AB0076D8BB.0001): Rod End Assembly. REXNORD INDUSTRIES LLC, PSI BEARINGS DIVISION · PMA PQ1183NM · Replaces P3A1830 B0308015 · Mar 25, 2019
- [3177537-1JA](https://drs.faa.gov/browse/excelExternalWindow/281445797C582D00862581370060AFCA.0001): Clip-Retaining. Jet Avion Corporation A HEICO Aerospace Company · PMA PQ1015CE · Replaces Honeywell P/N 3177537-1 · May 25, 2017
- [3502689-1TA](https://drs.faa.gov/browse/excelExternalWindow/2A79CAB3069EF2E98625836A005030B7.0001): Bearing, Ball, Annular Supplement 129. Extex Engineered Products Inc · PMA PQ2203NM · Replaces 3502689-1 · Sep 7, 2016
- [GM9598](https://drs.faa.gov/browse/excelExternalWindow/6421F06CD315738A86257FAA0067F4D4.0001): Linear Transducer. Kavlico Corporation · PMA PQ1186NM · Replaces 1680-500 · Jan 12, 2016
- [CH34760-2](https://drs.faa.gov/browse/excelExternalWindow/0B22F1FE9C50B69286257F5C00549081.0001): Igniter Assembly. Champion Aerospace LLC · PMA PQ1287CE · Replaces CH34760-2 · Dec 2, 2015
- [GM9598](https://drs.faa.gov/browse/excelExternalWindow/8F3D3ED8957C171E86257EF4006453AC.0001): Linear Transducer. Kavlico Corporation · PMA PQ1186NM · Replaces 1680-500 · Sep 21, 2015
- [CV41-14-2](https://drs.faa.gov/browse/excelExternalWindow/B04D4AE53FD4AB2D86257E3C00823011.0001): Ejector and Float Valve. CIRCOR Aerospace, Inc. · PMA PQ1168NM · Replaces CV41-14-2 · May 3, 2015
- [CV41-14](https://drs.faa.gov/browse/excelExternalWindow/A5845832630338C986257E3C00822F7D.0001): Ejector and Float Valve. CIRCOR Aerospace, Inc. · PMA PQ1168NM · Replaces CV41-14 · May 3, 2015
- [CV99-221-1](https://drs.faa.gov/browse/excelExternalWindow/0CC0B2FF9FF6CBCF86257E3C00822F3A.0001): Valve, Check IDG. CIRCOR Aerospace, Inc. · PMA PQ1168NM · Replaces CV99-221-1 · May 3, 2015
- [3175325-1WD](https://drs.faa.gov/browse/excelExternalWindow/DA046E4759A29CA186257D69006A428F.0001): Bearing, Ball, Annular. Wencor LLC (formerly Dixie Aerospace LLC) · PMA PQ1630CE · Replaces 3175325-1 · Sep 21, 2014
- [NSL870 B1/2](https://drs.faa.gov/browse/excelExternalWindow/D02AEBC7008B811686257D19004F9761.0001): Sealant. Dedicated Packaging, LLC · PMA PQ4210CE · Replaces PRC-DeSoto Sealant Pro Seal 870 B1/2 · Jul 15, 2014
- [NSL870 B2](https://drs.faa.gov/browse/excelExternalWindow/79754D781B68555386257D19004F9769.0001): Sealant. Dedicated Packaging, LLC · PMA PQ4210CE · Replaces PRC-DeSoto Sealant Pro Seal 870 B2 · Jul 15, 2014
- [NSL1428-B1/2](https://drs.faa.gov/browse/excelExternalWindow/F7183CB2BC43F62F86257D1000653FD7.0001): Sealant. Dedicated Packaging, LLC · PMA PQ4210CE · Replaces PRC-DeSoto Sealant PR-1428-B1/2 · Jun 30, 2014
- [NSL1428-B2](https://drs.faa.gov/browse/excelExternalWindow/36A26347DBF38ABB86257D1000653FD8.0001): Sealant. Dedicated Packaging, LLC · PMA PQ4210CE · Replaces PRC-DeSoto Sealant PR-1428-B2 · Jun 30, 2014
- [3503867-2WE](https://drs.faa.gov/browse/excelExternalWindow/A53D3D57B1B9B2AF86257CFD00649FC5.0001): Shaft-Drive Pump. Wencor LLC · PMA PQ1370NM · Replaces 3503867-2 · Jun 4, 2014
- [5500A13P002WE](https://drs.faa.gov/browse/excelExternalWindow/0861E490F8CC6B6986257CC3006047A0.0001): Packing Performed. Wencor LLC · PMA PQ1370NM · Replaces 5500A13P002 · Apr 3, 2014
- [514842-1](https://drs.faa.gov/browse/excelExternalWindow/4506964D0BA7661486257C70006366CE.0001): Stator, Alternator. Unison Industries LLC · PMA PQ0620NE · Replaces RR 514842-1 · Jan 28, 2014
- [114E6127G317](https://drs.faa.gov/browse/excelExternalWindow/EE7C6C281AAD352A86257C3D006DB5FE.0001): Engine Electronic Control. BAE System Controls Inc · PMA PQ2603CE · Replaces 114E6127G317 · Dec 5, 2013
- [114E6112G120](https://drs.faa.gov/browse/excelExternalWindow/C74B93265E0CE15686257C3D006DB5FC.0001): Engine Electronic Control. BAE System Controls Inc · PMA PQ2603CE · Replaces 114E6112G120 · Dec 5, 2013
- [114E6127G315](https://drs.faa.gov/browse/excelExternalWindow/B989CF353180452586257C3D006DB5FD.0001): Engine Electronic Control. BAE System Controls Inc · PMA PQ2603CE · Replaces 114E6127G315 · Dec 5, 2013
- [114E6112G118](https://drs.faa.gov/browse/excelExternalWindow/A07102F663FC87D486257C3D006DB5FA.0001): Engine Electronic Control. BAE System Controls Inc · PMA PQ2603CE · Replaces 114E6112G118 · Dec 5, 2013
- [114E7842G120](https://drs.faa.gov/browse/excelExternalWindow/84BC948133F018BD86257C3D006DB603.0001): Engine Electronic Control. BAE System Controls Inc · PMA PQ2603CE · Replaces 114E7842G120 · Dec 5, 2013
- [114E6127G417](https://drs.faa.gov/browse/excelExternalWindow/7A8C3BC1DE3EB27786257C3D006DB601.0001): Engine Electronic Control. BAE System Controls Inc · PMA PQ2603CE · Replaces 114E6127G417 · Dec 5, 2013
- [112E9321G2](https://drs.faa.gov/browse/excelExternalWindow/748E836396EA3C2D86257C3D006DB5F3.0001): Controller. BAE System Controls Inc · PMA PQ2603CE · Replaces 112E9321G2 · Dec 5, 2013
- [114E6127G319](https://drs.faa.gov/browse/excelExternalWindow/5FDB4EC78E7FA38F86257C3D006DB5FF.0001): Engine Electronic Control. BAE System Controls Inc · PMA PQ2603CE · Replaces 114E6127G319 · Dec 5, 2013
- [114E6127G419](https://drs.faa.gov/browse/excelExternalWindow/556E9C1F30B69CE486257C3D006DB602.0001): Engine Electronic Control. BAE System Controls Inc · PMA PQ2603CE · Replaces 114E6127G419 · Dec 5, 2013
- [114E6112G117](https://drs.faa.gov/browse/excelExternalWindow/4F27091C81C378B986257C3D006DB5F9.0001): Engine Electronic Control. BAE System Controls Inc · PMA PQ2603CE · Replaces 114E6112G117 · Dec 5, 2013
- [114E6112G115](https://drs.faa.gov/browse/excelExternalWindow/396AE2C83B2DB76B86257C3D006DB5F8.0001): Engine Electronic Control. BAE System Controls Inc · PMA PQ2603CE · Replaces 114E6112G115 · Dec 5, 2013

All of them: https://openairdocs.org/engine/bmw-rolls-br700-715a130/pma.md

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