# Rolls-Royce AE-3007C - Type: Engine model (FAA registry) - Registry code: 54572 - Manufacturer (registry): ROLLS-ROYC - Model: AE 3007C - Engine type: Turbo-fan - Power: 6,442 lb thrust - Data sheet: [TCDS TE6CH](https://openairdocs.org/tcds/TE6CH) (OpenAirDocs) - Holder: Rolls-Royce Corporation - Installed in: 16 registered aircraft - Page: https://openairdocs.org/engine/rolls-royce-ae-3007c 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 2017-26-06](https://openairdocs.org/ad/2017-26-06): Turbine/turboprop Engine, Turbine · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1/1 and 7 more. Effective Jan 31, 2018 - [AD 2017-11-05](https://openairdocs.org/ad/2017-11-05): Turbine/ turboprop Engine, Turbine Section · Rolls-Royce AE 3007C and AE 3007C1. Effective Jul 18, 2017 - [AD 2015-02-08](https://openairdocs.org/ad/2015-02-08): Turbine wheels · Rolls-Royce AE 2100D2, AE 2100D2A, AE 2100D3 and 11 more. Effective Mar 11, 2015 - [AD 2009-24-04](https://openairdocs.org/ad/2009-24-04): Fan spinner · Rolls-Royce AE 3007A1, AE 3007A1E, AE 3007A1P and 5 more. Effective Dec 28, 2009 - [AD 2007-24-05](https://openairdocs.org/ad/2007-24-05): Engine oil temperature · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1/1 and 8 more. Effective Jan 2, 2008 - [AD 2001-25-05](https://openairdocs.org/ad/2001-25-05): Compressor Cone Shafts · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1P and 4 more. Effective Jan 23, 2002 - [AD 2001-19-03](https://openairdocs.org/ad/2001-19-03): High Pressure Turbine 1st to 2nd Stage Turbine Spacer · Rolls-Royce AE 3007A and AE 3007C. Effective Oct 29, 2001 - [AD 2001-17-31](https://openairdocs.org/ad/2001-17-31): Second Stage High Pressure Turbine Wheel · Rolls-Royce AE 2100A, AE 2100C, AE 2100D3 and 2 more. Effective Oct 5, 2001 - [AD 2000-18-06](https://openairdocs.org/ad/2000-18-06): Digital Electronic Controls · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1P and 5 more. Effective Sep 22, 2000 - [AD 2000-13-01](https://openairdocs.org/ad/2000-13-01): Turbine Wheels · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1P and 5 more. Effective Sep 1, 2000 - [AD 2000-11-22](https://openairdocs.org/ad/2000-11-22): Critical Life-Limited Parts · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1P and 5 more. Effective Aug 7, 2000 - [AD 98-11-32](https://openairdocs.org/ad/98-11-32): Sump Magnetic Chip Collector Plug · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1P and 5 more. Effective Jun 18, 1998 Historical (superseded or no longer in force): - [AD 2000-09-05](https://openairdocs.org/ad/2000-09-05) (historical): Cone Shafts · AE 3007A, AE 3007A1, AE 3007A1P and 4 more. Effective Jul 5, 2000 - [AD 99-02-51](https://openairdocs.org/ad/99-02-51) (historical): Starter Shaft Seal · AE 3007A, AE 3007A1, AE 3007A1P and 5 more. Effective Apr 20, 1999 ## Information bulletins (advisory) (1) - [SAIB NE-11-22](https://openairdocs.org/saib/NE-11-22): Engine Controls. Issued Feb 23, 2011 ## Registered aircraft (16) - [N12195](https://openairdocs.org/aircraft/N12195): [United Airlines Inc](https://openairdocs.org/faa-owner/UNITED%20AIRLINES%20INC), [Chicago, IL](https://openairdocs.org/faa-place/IL/Chicago), built 2005, S/N 14500943 - [N12GG](https://openairdocs.org/aircraft/N12GG): [Lima Golf Investments LLC](https://openairdocs.org/faa-owner/LIMA%20GOLF%20INVESTMENTS%20LLC), [Bigfork, MT](https://openairdocs.org/faa-place/MT/Bigfork), built 2001, S/N 750-0140 - [N187CR](https://openairdocs.org/aircraft/N187CR): [Jaoo 187 LLC](https://openairdocs.org/faa-owner/JAOO%20187%20LLC), [Raleigh, NC](https://openairdocs.org/faa-place/NC/Raleigh), built 2000, S/N 750-0119 - [N199XX](https://openairdocs.org/aircraft/N199XX): [Cirrus Aviation LLC](https://openairdocs.org/faa-owner/CIRRUS%20AVIATION%20LLC), [San Bernardino, CA](https://openairdocs.org/faa-place/CA/San%20Bernardino), built 2002, S/N 750-0199 - [N200AP](https://openairdocs.org/aircraft/N200AP): [Wheels Up Partners LLC](https://openairdocs.org/faa-owner/WHEELS%20UP%20PARTNERS%20LLC), [New York, NY](https://openairdocs.org/faa-place/NY/New%20York), built 1996, S/N 750-0003 - [N200JT](https://openairdocs.org/aircraft/N200JT): [N200jt LLC](https://openairdocs.org/faa-owner/N200JT%20LLC), [Dallas, TX](https://openairdocs.org/faa-place/TX/Dallas), built 2000, S/N 750-0103 - [N230SM](https://openairdocs.org/aircraft/N230SM): [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 2001, S/N 750-0152 - [N405BS](https://openairdocs.org/aircraft/N405BS): [Radio Flyer LLC](https://openairdocs.org/faa-owner/RADIO%20FLYER%20LLC), [Granbury, TX](https://openairdocs.org/faa-place/TX/Granbury), built 1998, S/N 7500041 - [N480WT](https://openairdocs.org/aircraft/N480WT): [Whiskey Tango Foxtrot Motorsports LLC](https://openairdocs.org/faa-owner/WHISKEY%20TANGO%20FOXTROT%20MOTORSPORTS%20LLC), [Scottsdale, AZ](https://openairdocs.org/faa-place/AZ/Scottsdale), built 1996, S/N 750-0004 - [N621FP](https://openairdocs.org/aircraft/N621FP): [Raleighwood Aircraft LLC](https://openairdocs.org/faa-owner/RALEIGHWOOD%20AIRCRAFT%20LLC), [Raleigh, NC](https://openairdocs.org/faa-place/NC/Raleigh), built 1998, S/N 750-0045 - [N703DM](https://openairdocs.org/aircraft/N703DM): [Papa Grande Aviation LLC](https://openairdocs.org/faa-owner/PAPA%20GRANDE%20AVIATION%20LLC), [Fort Worth, TX](https://openairdocs.org/faa-place/TX/Fort%20Worth), built 1999, S/N 750-0080 - [N719XJ](https://openairdocs.org/aircraft/N719XJ): [Rllt Jet LLC](https://openairdocs.org/faa-owner/RLLT%20JET%20LLC), [Auburn, AL](https://openairdocs.org/faa-place/AL/Auburn), built 2002, S/N 750-0179 - [N750CX](https://openairdocs.org/aircraft/N750CX): [Textron Aviation Inc](https://openairdocs.org/faa-owner/TEXTRON%20AVIATION%20INC), [Wichita, KS](https://openairdocs.org/faa-place/KS/Wichita), built 1993, S/N 703 - [N78ZE](https://openairdocs.org/aircraft/N78ZE): [Staff-Up LLC](https://openairdocs.org/faa-owner/STAFF-UP%20LLC), [Dallas, TX](https://openairdocs.org/faa-place/TX/Dallas), built 1996, S/N 750-0005 - [N85AV](https://openairdocs.org/aircraft/N85AV): [Montgomery, AL](https://openairdocs.org/faa-place/AL/Montgomery), built 1999, S/N 7500085, Sale reported, pending cancellation - [N92TH](https://openairdocs.org/aircraft/N92TH): [Goshawk Consulting LLC](https://openairdocs.org/faa-owner/GOSHAWK%20CONSULTING%20LLC), [Belgrade, MT](https://openairdocs.org/faa-place/MT/Belgrade), built 1999, S/N 750-0097 ## 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 ERA23LA176](https://openairdocs.org/ntsb/ERA23LA176), Apr 1, 2023: Cessna 750 (N85AV), Wall Township, NJ, substantial damage. Probable cause: The pilots’ loss of directional control while landing in gusting wind conditions which resulted in a runway excursion. Also contributing was the flight crew’s decision to land at an airport where… ## FAA accident and incident reports (5) 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. - [Accident 20230401020889A](https://openairdocs.org/incident/20230401020889A), Apr 1, 2023: Cessna 750 (N85AV), Wall Township, NJ, Substantial damage. During repositioning flight operating under 14 CFR part 91, aircraft landed runway 32 at Monmouth county executive airport with approaching line of… - [Incident 20201031020559I](https://openairdocs.org/incident/20201031020559I), Oct 31, 2020: Cessna 750 (N719XJ), Minor damage. Upon intercepting the LOC for the ILS RWY15 (circle RWY6) hit a bird (canadian goose). Both crew and passengers heard a loud thump from the lower front chin of… - [Incident 20190317001569I](https://openairdocs.org/incident/20190317001569I), Mar 17, 2019: Cessna 750 (N777KT), Seattle, WA, Minor damage. On March 17 at approximatly 1755, local time, N777KT (Cessna 750) was on final approach to runway 32L when it struk 2 or 3 birds. The pilots did not feel any… - [Incident 20160410007389I](https://openairdocs.org/incident/20160410007389I), Apr 10, 2016: Cessna 750 (N719XJ), Oakland, CA, Minor damage. Aircraft N719XJ, a Cessna citation 750, was being repositioned from san francisco international airport to Oakland International Airport on 04/10/2016 at… - [Incident 20130518007839I](https://openairdocs.org/incident/20130518007839I), May 18, 2013: Cessna 750 (N902VP), Costa Rico, No damage. On may 18, 2013, acft N902VP departed Costa Rico piloted by [privacy data omitted] (PIC) and [privacy data omitted] (SIC). The destination for this flight was… ## Service difficulty reports (793, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR CVGA20260207001](https://openairdocs.org/sdr/CVGA20260207001), Feb 6, 2026: COUPLING. LEAKING. ABORTED TAKE OFF DUE TO A LEFT ENGINE PYLON BLEED LEAK CAS MESSAGE AND SMOKE IN THE COCKPIT/ CABIN. UPON INVESTIGATION THE LT ENGINE OTBD PRECOOLER V-BAND COUPL - [SDR HNAA2024121101219](https://openairdocs.org/sdr/HNAA2024121101219), Dec 10, 2024: ENGINE. FAILED. AT FL320 E2 FAIL AFTER CREW HEARD BANG & POP WITH E2 UNCOMMANDED SHUTDOWN. R & R #2 ENG IAW WC 71-00-00. - [SDR HNAA2024120901168](https://openairdocs.org/sdr/HNAA2024120901168), Dec 7, 2024: CONTROL PANEL. FAULTED. BLEED #2 VALVE CLOSED MIDAIR FACT 08DEC24 02:24 PHL R&R PNEUMATIC CONTROL PANEL IRW AMM 20-13-10.OPS CHECKED IRW AMM 36-00-00 AND AMM 21-00-00. OPS CHECK GOOD. - [SDR HNAA2024120901165](https://openairdocs.org/sdr/HNAA2024120901165), Dec 6, 2024: EXCITER. FAULTED. E2 HUNG START AT 30%N2 ON FADEC A. CREW STOPPED START SEQ WHEN FUEL SMELLED IN A/C. FACT 06DEC24 21:38 PHL R&R E2 LEFT IGNITION EXCITER IAW RRM 74-13-10. STARTE - [SDR 3EJA2024080900001](https://openairdocs.org/sdr/3EJA2024080900001), Aug 9, 2024: WARNING MESSAGE. ILLUMINATED. ON TAKEOFF ROLL AMBER CAUTION MESSAGE ENG O’SPD SHUTDN L ILLUMINATED ON EICAS. - [SDR HNAA2023010400015](https://openairdocs.org/sdr/HNAA2023010400015), Jan 2, 2023: BLEED VALVE. FAILED. REJECTED TAKEOFF AT 60 KNOTS. BLEED 2 VALVE FAIL WITH TAKEOFF POWER SELECTED. R & R #2 ENGINE BLEED VALVE IRT AMM 36-11-05. OPS CHECK / LEAK CHECK GOOD. NO DEFE - [SDR HNAA2023010400017](https://openairdocs.org/sdr/HNAA2023010400017), Jan 2, 2023: ANTI-ICE SYSTEM. FAULTED. RETURN TO FIELD DUE TO ENG 2 ANTI ICE FAIL AT APPROX 14,000 FT WITH BLEED 1 OVERTEMP MESSAGE AND THEN SHORTLY AFTER WING ANTI ICE FAIL MESSAGE. R & R ENGINE PRE - [SDR HNAA2022122100318](https://openairdocs.org/sdr/HNAA2022122100318), Dec 18, 2022: PUMP. FAULTED. DURING TAKE OFF E2 LOW FUEL PRESS DISPLAYED ON EICAS WHEN OPERATING ON PUMP 2B. VERIFIED 2A AND 2C OPERATING NORMALLY... P/C C/B A4 ON LH DC DIST. BOX. T/S IAW - [SDR VQMA905VR121222R0](https://openairdocs.org/sdr/VQMA905VR121222R0), Dec 12, 2022: FAN. WARNING MESSAGE. ON MONDAY, DECEMBER 12TH 2022, CESSNA CITATION 750, REGISTRATION NUMBER N905, SERIAL NUMBER 750-0105 RECEIVED A FAN DAMAGE L WARNING INDICATION ALONG WITH YAW D - [SDR HNAA2022110300299](https://openairdocs.org/sdr/HNAA2022110300299), Nov 2, 2022: CARBON SEAL. LEAKING. LAV SMOKE EICAS MSG APPEARED ON CLIMB 800FT STAYED ON FOR 3 TO 5 MINS. MAINTENANCE FOUND #2 ENGINE LEAKING OIL AND R&R'D THE ATS CARBON SEAL. THEY GROUND RAN TH - [SDR HNAA2022100500266](https://openairdocs.org/sdr/HNAA2022100500266), Oct 4, 2022: BLEED VALVE. FAULTED. BLEED 2 VALVE FAILURE ON T/O POWER ( C/W RMM 36-11-05) T/S FIM 36-11-00-810-806-A STEPS 1 2 3 20 21 AND 22 R/R #2 HIGH STAGE PRESSURE SWITCH IAW AMM 36-11-07. O - [SDR 4DPA2022082000001](https://openairdocs.org/sdr/4DPA2022082000001), Aug 20, 2022: METERING UNIT. FAILED. ISSUE- CREW REPORTED ON CLIMB OUT, APPROXIMATELY 2000 FEET, AIRCRAFT YAWED SLIGHTLY TO LEFT AND LEFT ENGINE N1 AND ITT BEGAN TO BOUNCE AROUND. ITT WAS UP AND DO - [SDR AJXA2022041100014](https://openairdocs.org/sdr/AJXA2022041100014), Apr 7, 2022: PUMP. LOW PRESSURE. DURING CRUISE THE PILOT RECEIEVED A CAS MESSAGE NOTING A FUEL IMBALANCE BETWEEN THE LH AND RH WING. THE FUEL FLOW FROM THE RIGHT HAND TRANSFER SYSTEM WAS NOT KE - [SDR HNAA2022030700118](https://openairdocs.org/sdr/HNAA2022030700118), Mar 3, 2022: NONE. NONE. PDIS 621 78-34 2697301 03MAR22 BTV CLOSE DURING T/O ROLL ENG 1 REV DISAGREE MESSAGE APPEARED ON EICAS FACT 06MAR22 03:58 PHL UNLOCKED #1 TR I.A.W AMM 78-31-01. - [SDR HNAA2021071300320](https://openairdocs.org/sdr/HNAA2021071300320), Jul 10, 2021: PIPE. LEAKING. BLEED 1 LEAK MSG DURING CLIMB. T/S IN REF W/FIM TASK 36-20-00-810-801-A. FOUND Y-PIPE AFTER #100 ENG BLD VLV TO BE DAMAGED. R&R'D Y-PIPE AFTER #100 ENG BLD VLV - [SDR HNAA2021060700234](https://openairdocs.org/sdr/HNAA2021060700234), Jun 4, 2021: COMPRESSOR. MAKING METAL. DURING CLIMB OUT WITH N1 AROUND 91%. LOUD BANG HEARD FROM ENGINE #1 FOLLOWED QUICKLY BY ENGINE SHUTDOWN. PERFORMED GVI OF #1 ENGINE. FOUND METAL FOD IN FIRST ST - [SDR HNAA2021040500129](https://openairdocs.org/sdr/HNAA2021040500129), Apr 5, 2021: ENGINE. MALFUNCTIONED. NO. 2 ENGINE WILL NOT START WITH 2 ATTEMPTS. HEAVY FUEL SMELL IN CABIN AND FLIGHT DECK. PERFORMED FIM TASK 72-33-33-810-824. ENIGNE RETURNED TO SERVICE DUE TO N - [SDR HNAA2020100500274](https://openairdocs.org/sdr/HNAA2020100500274), Oct 2, 2020: ANTI-ICE VALVE. SEIZED. PDIS 620 30-21 2453941 02OCT20 MDT. CLOSE E2 ANTI ICE FAIL WITH NO ICING CONDITION. FACT 03OCT20 20:29 MDT. DOWNLOADED CMC DATA, ENGINE 2 ANTI ICE VALVE FAIL OC - [SDR HALA2020091800183](https://openairdocs.org/sdr/HALA2020091800183), Sep 17, 2020: TUBE. BROKEN. ENG NR 2 LEFT SIDE 9 O'CLOCK POSITION VIEWING FROM REAR. RACEWAY TUBE ASSY FOR FIRE LOOP BROKEN/SHEARED. REPLACED NR 2 ENG RACEWAY TUBING AT 9 0'CLOCK POSITION - [SDR 16AA20191125001](https://openairdocs.org/sdr/16AA20191125001), Nov 25, 2019: HOSE. LEAKING. DURING TAKEOFF CREW DISCOVERED HYDRAULIC PRESSURE LOSS ON SYSTEM A. CREW DECLARED A EMERGENCY LANDING AND LANDED THE AIRCRAFT WITHOUT FURTHER INCIDENT. MANUFACT - [SDR CA190814006](https://openairdocs.org/sdr/CA190814006), Aug 7, 2019: LINE. CHAFED. (CAN) THE LH ELEVATOR HYDRAULIC LINE WAS CHAFFED AS A RESULT OF CONTACT WITH THE HORIZONTAL STAB INTERNAL STRUCTURE RESULTING IN FAILURE. DUE TO THIS FAILURE TH - [SDR CA190612012](https://openairdocs.org/sdr/CA190612012), Jun 10, 2019: DOOR. MALFUNCTIONED. (CAN) IN DECEMBER 2018 AIRCRAFT C750 C-XXXX HAD ADS-B MODIFICATION SB750-34-58R1 INSTALLED AT CESSNA/TEXTRON SERVICE CENTER. WE JUST BEGINNING A SCHEDULED INSPE - [SDR CA190227015](https://openairdocs.org/sdr/CA190227015), Feb 26, 2019: PUMP. FAILED. (CAN) REPLACING APU FUEL FILTER ON SCHEDULED TASK. THE FILTER AND FUEL IN THE FILTER BOWL WAS BLACK, AND VERY DIRTY, WITH PARTICLES FLOATING IN IT. ON INVESTIGA - [SDR 2020FA0000074](https://openairdocs.org/sdr/2020FA0000074), Nov 20, 2018: TUBE. CRACKED. HIGH PRESSURE BLEED AIR TUBE AT ENGINE INTERFACE CRACKED. - [SDR HNAA2018052500107](https://openairdocs.org/sdr/HNAA2018052500107), May 6, 2018: BLEED VALVE. FAILED. NR 2 BLEED VALVE FAILED EICAS MESSAGE DISPLAYED DURING TAKEOFF ROLL AFTER POWER LEVELS WERE ADVANCED. ABORTED THE TAKEOFF. - [SDR HNAA2018043000092](https://openairdocs.org/sdr/HNAA2018043000092), Apr 27, 2018: TUBE. FAILED. BLEED 1 LEAK EICAS MESSAGE DISPLAYED DURING CLIMBOUT. REMOVED AND REPLACED THE TUBES IAW AMM 36-13-00. PERFORMED A BLEED AIR LEAK CHECK IAW AMM 36-00-00. PERFOM - [SDR HNAA2017101600350](https://openairdocs.org/sdr/HNAA2017101600350), Oct 15, 2017: ENGINE. FIRE. GROUND CREW REPORTED A NR 1 ENGINE FIRE AT EXHAUST NOZZLE DURING TAXI. CREW REPORTED THE ENGINE WAS JUST PREVIOUSLY SHUTDOWN AND NO ABNORMAL INDICATIONS OR MESS - [SDR HNAA2017092100324](https://openairdocs.org/sdr/HNAA2017092100324), Sep 19, 2017: ENGINE. SMOKE. AFTER PREVIOUS FLIGHT, SMOKE WAS REPORTED COMING FROM THE INLET OF THE NR 1 ENGINE. GROUND RAN THE AIRCRAFT, ALL ENGINE INDICATIONS NORMAL. ON SHUTDOWN, NO SMOK - [SDR HNAA2017082100279](https://openairdocs.org/sdr/HNAA2017082100279), Aug 18, 2017: ENGINE. FIRE. GATE AGENT NOTICED FLAMES AND SMOKE EMINATING FROM THE NR 1 ENGINE WHILE ENGINE WAS SHUTDOWN. INSPECTED AND NO DAMAGE NOTED. GVI ENGINE INLET AND EXIT AND NACEL - [SDR HNAA2017081400272](https://openairdocs.org/sdr/HNAA2017081400272), Aug 13, 2017: FADEC. MALFUNCTIONED. NR 1 ENGINE SHORT DISPATCH ON FADEC A. DOWNLOADED CMC IAW W/C 45-90-00. FOUND MESSAGE ST-ENG1 MMV/CVG SYS. FIM 73-21-00-810-821 OPERATED ENGINES AT MAX THRUST A - [SDR HNAA2017071000232](https://openairdocs.org/sdr/HNAA2017071000232), Jul 8, 2017: WARNING MESSAGE. FALSE ACTIVATION. NR 1 ENGINE ANTI ICE DISAGREE MESSAGE DISPLAYED ON EICAS. INSPECTED CMC, NO RELATED MESSAGES DISPLAYED. OPS CHECKED IAW AMM 30-21-00-700-804-A, OPS CHECKED GOOD - [SDR HNAA2017062100214](https://openairdocs.org/sdr/HNAA2017062100214), Jun 18, 2017: ENGINE. SMOKE. AFTER SHUTDOWN OF THE NR 1 ENGINE, SMOKE WAS SEEN COMING OUT OF THE FRONT AND BACK OF ENGINE. INSPECTED THE INTAKE AND EXHAUST. NO LEAKS NOTED. NO SMOKE NOTED. - [SDR ASOA201705104022](https://openairdocs.org/sdr/ASOA201705104022), May 10, 2017: ENGINE. LEAKING. THE CREW REPORTED SMOKE IN THE COCKPIT AFTER PACK ONE WAS USED. THE AIRCRAFT LANDED WITHOUT INCIDENT WHERE MAINTENANCE PLACED THE NR 1 PACK ON MEL 21-51-00-1 AN - [SDR SIMA20170401003](https://openairdocs.org/sdr/SIMA20170401003), Apr 1, 2017: ANTI-ICE VALVE. FAILED. HIGH SPEED ABORT PERFORMED AT APPROX 80 KTS DURING TO ROLL. RECEIVED AN ENGINE A/I DISAGREE CAUTION AND AN NR 2 ENGINE OPEN INSCRIPTION WITH ANTI-ICE OVERRIDE I - [SDR HNAA2017030800078](https://openairdocs.org/sdr/HNAA2017030800078), Mar 8, 2017: ENGINE. UNKNOWN. NR 2 ENGINE FAILED TO START. FIRST START, ENGINE DID NOT REACH 30 N2. SECOND START, ENGINE DID GET TO 30 N2, BUT THEN SHUTDOWN. NO WARNING OR CAUTION MESSAGE. S - [SDR DXTA2017021306371](https://openairdocs.org/sdr/DXTA2017021306371), Feb 13, 2017: VALVE. DEFECTIVE. UPON INITIATING DECENT, WHEN THE THROTTLES WERE REDUCED AND THE PAC HP VALVE OPEN L-R CAS MESSAGE APPEARS, THERE IS A STRONG ODOR OF BURNING RUBBER. REMOVED AND - [SDR AWKA201612230001](https://openairdocs.org/sdr/AWKA201612230001), Dec 21, 2016: LINE. FAILED. DURING A POST FLIGHT INSPECTION, THE FLIGHT CREW NOTED FUEL LEAKING FROM THE LT ENGINE GANG DRAIN AREA. A CONTRACTED MAINTENANCE TECHNICIAN FOUND A FIRE LOOP HA - [SDR HNAA2016092600297](https://openairdocs.org/sdr/HNAA2016092600297), Sep 26, 2016: O-RING. LEAKING. NR 2 ENGINE EMITTING SMOKE FROM TAILPIPE AREA 20 MINUTES AFTER SHUTDOWN. FOUND EVIDENCE OF OIL SEEPING FROM TURBINE SECTION. MAINTENANCE WAS DIRECTED TO REPLACE - [SDR SIMA20160825002](https://openairdocs.org/sdr/SIMA20160825002), Aug 25, 2016: FADEC. MALFUNCTIONED. NR 1 ENGINE N1 ROLL BACK UNCOMMANDED 90-60% FOR A FEW SECONDS, CAUTION YAW TO LEFT N2 RECOVERED 5 SECONDS LATER AT FL 320. LANDED NORMALLY. NO WEATHER, NO EXTEM - [SDR HNAA2016072500228](https://openairdocs.org/sdr/HNAA2016072500228), Jul 22, 2016: CONNECTOR. DIRTY. DOWNLOADED CMC AND FOUND ND ENG 2 COMM A AND B MESSAGES. TROUBLESHOT IAW FIM 77-44-00-810-807 AND ARRIVED AT BLOCK 09. CLEANED THE J2 CONNECTOR AND RECEPTACLES - [SDR DXTA2016060306252](https://openairdocs.org/sdr/DXTA2016060306252), Jun 3, 2016: BRACKET. DAMAGED. DAMAGE FOUND IN TAILSTAND AREA WHILE INSTALLING TAIL STAND PRIOR TO MAINTENANCE. NO RECORD OF DAMAGE FOUND. REMOVED TAIL STAND BRACKET, PN 6712405-10 IAW SRM 51 - [SDR RAIA201602290003](https://openairdocs.org/sdr/RAIA201602290003), Feb 29, 2016: COUPLING. WORN. BLEED 2 LEAK EICAS MESSAGE IN FLIGHT. FOUND NR 2 ENGINE BLEED VALVE OUTLET COUPLING BAD, R & R BLEED COUPLING. OPS CHECK GOOD. INSPECTED BLEED DUCTS NO LEAKS NO - [SDR CWQR20160226008](https://openairdocs.org/sdr/CWQR20160226008), Feb 26, 2016: BULKHEAD. CRACKED. DURING THE DISASSEMBLY OF THE ENG INLET ASSEMBLY WE FOUND THIS BULKHEAD CRACKED IN NUMEROUS PLACES AT THE INLET LIP TO THROAT ATTACH FASTENERS. SUBMITTED DEFECT - [SDR CWQR20160226009](https://openairdocs.org/sdr/CWQR20160226009), Feb 25, 2016: CHANNEL. CRACKED. DURING THE DISASSEMBLY OF THE ENG INLET ASSEMBLY, WE FOUND THIS CHANNEL CRACKED IN NUMEROUS PLACES AT THE INLET LIP TO BULKHEAD ATTACH FASTENERS. SUBMITTED DEFE - [SDR DXTA2016020206176](https://openairdocs.org/sdr/DXTA2016020206176), Feb 3, 2016: BLADE. BENT. ON PREFLIGHT FOUND 4 BLADES ON PRIMARY FAN ARE BENT ON NR 1 ENG. ACCOMPLISHED FAN BLADE INSPECTION IAW MM 72-21-15-200-801. R & R 6 FAN BLADES IAW MM 72-21-15-0 - [SDR DXTA2016020306180](https://openairdocs.org/sdr/DXTA2016020306180), Feb 3, 2016: BLADE. DAMAGED. NUMBER 2 ENG HAS 5 BLADES DAMAGED & BENT. ACCOMPLISHED FAN BLADE INSPECTION IAW MM 72-21-15-200-801. R & R 5 FAN BLADES IAW MM 72-21-15-000-801 & 82-21-15-400-8 - [SDR DXTA2015111306129](https://openairdocs.org/sdr/DXTA2015111306129), Nov 23, 2015: PUMP. FAILED. DURING TAKEOFF THROUGH 3000 FEET WITH THROTTLE IN TAKE OFF, THE RT ENGINE N2 WENT TO 102 & INDICATED RED. THE FLYING PILOT FELT A POWER BUMP & THEN SLOWLY RETAR - [SDR DJFA20151120002](https://openairdocs.org/sdr/DJFA20151120002), Nov 20, 2015: WIRE HARNESS. DAMAGED. CREW REPORTED ENG POWER ROLL BACK INTERMITTENTLY. ACFT LANDED SAFELY. REPLACED THE ENG CONTROL B WIRE HARNESS. - [SDR DJFA20151114001](https://openairdocs.org/sdr/DJFA20151114001), Nov 14, 2015: FADEC. MALFUNCTIONED. DURING CLIMB, LT ENG POWER FLUCTUATED & ROLLED BACK 10 PERCENT 3 TIMES. AFTER THE THIRD ROLL BACK, FAN DAMAGE CAS MSG ILLUMINATED. ACFT LANDED SAFELY & NO ENG D - [SDR DJFA20150922001](https://openairdocs.org/sdr/DJFA20150922001), Sep 22, 2015: ENGINE. VIBRATION. ON CLIMB OUT, CREW FELT VIBRATION IN THE LT ENG & 20 SECONDS LATER RECEIVED A LT FAN DAMAGE CAS MSG. PERFORMED THEIR CHECKLIST, DECLARED AN EMER & DIVERTED BACK All 793: https://openairdocs.org/engine/rolls-royce-ae-3007c/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.