# Rolls-Royce AE-3007A - Type: Engine model (FAA registry) - Registry code: 54162 - Manufacturer (registry): ROLLS-ROYC - Model: AE 3007A - Engine type: Turbo-fan - Power: 7,580 lb thrust - Data sheet: [TCDS TE6CH](https://openairdocs.org/tcds/TE6CH) (OpenAirDocs) - Holder: Rolls-Royce Corporation - Installed in: 1 registered aircraft - Page: https://openairdocs.org/engine/rolls-royce-ae-3007a 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 2020-16-13](https://openairdocs.org/ad/2020-16-13): Turbine Engine Compressor Section · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1/1 and 5 more. Effective Aug 14, 2020 - [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 2013-26-06](https://openairdocs.org/ad/2013-26-06): High-pressure turbine (HPT) stage 2 wheels · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1/1 and 5 more. Effective Feb 7, 2014 - [AD 2011-22-03](https://openairdocs.org/ad/2011-22-03): Low-cycle fatigue cracks · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1/1 and 4 more. Effective Nov 17, 2011 - [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 2004-04-05](https://openairdocs.org/ad/2004-04-05): Engine oil system · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1P and 4 more. Effective Mar 9, 2004 - [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 99-03-03](https://openairdocs.org/ad/99-03-03): Full Authority Digital Engine Control (FADEC) · Rolls-Royce AE 3007A and AE 3007A1/1. Effective Feb 16, 1999 - [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 2010-19-01](https://openairdocs.org/ad/2010-19-01) (historical): High pressure turbine · Rolls-Royce AE 3007A. Effective Oct 27, 2010 - [AD 2009-08-51](https://openairdocs.org/ad/2009-08-51) (historical): High-pressure turbine · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1/1 and 6 more. Effective May 27, 2009 - [AD 2008-26-06](https://openairdocs.org/ad/2008-26-06) (historical): High-pressure turbine (HPT) · AE 3007A. Effective Jan 8, 2009 - [AD 2008-19-51](https://openairdocs.org/ad/2008-19-51) (historical): AE 3007A, AE 3007A1, AE 3007A1E and 5 more - [AD 2001-08-15](https://openairdocs.org/ad/2001-08-15) (historical): Oil System · AE 3007A, AE 3007A1, AE 3007A1P and 4 more. Effective May 14, 2001 - [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 ## Registered aircraft (1) - [N145DB](https://openairdocs.org/aircraft/N145DB): [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 2008, S/N 14501045 ## 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 (3,309, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR JJBA20260819014](https://openairdocs.org/sdr/JJBA20260819014), Aug 16, 2026: ENGINE. FAILED. E1 OUT IN FLIGHT AT FLIGHT LEVEL 300. OCCURRED AT 30000, IT WAS SMOOTH AND THEN SEEMED LIKE TURBULENCE AND #1 ENGINE SHUTDOWN WITH EICAS MESSAGE. ATTEMPTED #1 E - [SDR HNAA2026072200600](https://openairdocs.org/sdr/HNAA2026072200600), Jul 20, 2026: ENGINE. HUNG START. NUMBER 2 ENGINE HAD HUNG START WITH WHITE SMOKE AND A FUEL ODOR IN FLIGHT DECK AND CABIN. PERFORMED ENGINE 2 START ON BOTH FADEC CHANNELS IAW MM 72-00-00-860-80 - [SDR HNAA2026052700436](https://openairdocs.org/sdr/HNAA2026052700436), May 26, 2026: ENGINE. FAILED. NR 2 ENGINE FAIL IN FLIGHT ALT 1700. R & R ENGINE IAW WC 71-00-00. OPS AND LEAK CHECK GOOD OK FOR SERVICE. - [SDR HNAA2026052600434](https://openairdocs.org/sdr/HNAA2026052600434), May 23, 2026: BLEED VALVE. FAILED. E1 HSV FAIL ON EICAS FACT 23MAY26 17:19 GSO. R & R NR 1 HSV IAW AMM 36-11-02. OPS AND LEAK CHECK GOOD. - [SDR JJBA20260527029](https://openairdocs.org/sdr/JJBA20260527029), May 23, 2026: ENGINE. FAILED. NR 1 ENGINE FAILED IN FLIGHT, DURING CLIMB AT 26,000 FT. REMOVED AND REPLACED LH ENGINE. OPS/LEAK CHECK SAT. - [SDR JJBA20260115025](https://openairdocs.org/sdr/JJBA20260115025), Jan 12, 2026: ENGINE. FAILED. ON CLIMBOUT HEARD A BIG BANG FROM NR 1 ENGINE AND NR 1 ENGINE SHUTDOWN. ALL INDICATORS WERE IN THE NORMAL ON TAKE OFF. DID ATTEMPT ANOTHER ENGINE RESTART IN FLI - [SDR HNAA2025071700469](https://openairdocs.org/sdr/HNAA2025071700469), Jul 16, 2025: BLEED VALVE. ABNORMAL. BLD 1 LEAK WARNING MESSAGE APPEARED DURING CLIMB. AFTER RUNNING QRH INSCRIPTION MESSAGE WENT AWAY. REMOVED AND REPLACED PNEUMATIC CROSS BLEED VALVE IRT AMM 36-1 - [SDR 4DPA2025053000001](https://openairdocs.org/sdr/4DPA2025053000001), May 30, 2025: GARLOCK SEAL. LEAKING. CREW REPORTED- ENGINE OIL LOW PRESSURE FOLLOWED BY QRH DIRECTIONS ENGINE NUMBER 1 SHUT DOWN . LANDED IN LAX WITHOUT FURTHER INCIDENT. CORR ACTION- MX TROUBLESHO - [SDR HNAA2025051900356](https://openairdocs.org/sdr/HNAA2025051900356), May 17, 2025: BLEED AIR SYS. LEAKING. BLD 1 LEAK MSG APPEARED ON EICAS DURING FLIGHT FACT 18MAY25 20:54 TYS R+R ORINGS/JOINTS AT POSITIONS 3,5,9,15,17 AND 23 IAW AMM 36-11-10-04. PERFORMED OPS CHECK - [SDR HNAA2025040800197](https://openairdocs.org/sdr/HNAA2025040800197), Apr 9, 2025: ENGINE. BIRD INGESTION. BIRD STRIKE ON #2 ENGINE. #2 ENG CHANGE. SEE W/C 71-00-00 ON WORK PACKAGE. - [SDR HNAA2025040300192](https://openairdocs.org/sdr/HNAA2025040300192), Apr 2, 2025: SENSOR. FAULTED. IN THE CLIMB FROM CLT E1 OIL TEMPERATURE WENT INTO THE RED FOR APPROXIMATELY 1 MINUTE THEN RETURNED TO NORMAL 20 PSI INCREASE INDICATION OIL PRESSURE, OIL TEMPE - [SDR HNA2025F00002](https://openairdocs.org/sdr/HNA2025F00002), Apr 2, 2025: SENSOR. FAULTED. N THE CLIMB FROM CLT E1 OIL TEMPERATURE WENT INTO THE RED FOR APPROXIMATELY 1 MINUTE THEN RETURNED TO NORMAL 20 PSI INCREASE INDICATION OIL PRESSURE, OIL TEMPER - [SDR HNAA2025031000145](https://openairdocs.org/sdr/HNAA2025031000145), Mar 8, 2025: BLEED VALVE. ACTIVATION ERROR. ON TAKEOFF ENGINE BLEED VALVE FAIL ON EICAS, GOING 20 KNOTS AND REFKECTED TAKEOFF. FACT 08MAR25 18:48 CLT REMOVED AND REPLACED ENGINE BLEED AIR VALVE IRW AMM 36 - [SDR HNAA2025022400092](https://openairdocs.org/sdr/HNAA2025022400092), Feb 23, 2025: OIL SYSTEM. LOW. FAINT OIL LIKE ODOR IN FLIGHT DECK WHILE ON ENGINE BLEEDS DURING DESECENT LAST APPROX 30SECS FACT 23FEB25 13:56 PHL E1 1QT LOW. SERVICED E1 WITH 1QT AS REQUIRED - [SDR 4DPA2024112500001](https://openairdocs.org/sdr/4DPA2024112500001), Nov 25, 2024: FILTER. DIRTY. CREW REPORTED- E2 FUEL IMP BY MESSAGE ON DEPARTURE OUT OF LAX. RAN QRH AND DIVERTED TO BUR. CORR ACTION MX R&R'D FILTER CLEANED FUEL HOUSING OP LK CHECK GOOD - [SDR HNAA2024110101050](https://openairdocs.org/sdr/HNAA2024110101050), Oct 31, 2024: ENGINE. FAILED. CLIMBING THROUGH 3000FT HEARD A BANG AND NO. 1 ENGINE SUDDENLY FAILED. LOST ITT INDICATION. N1 CONTINUED TO SPIN AT 13 PRESENT. OIL PRESSURE ZERO. FACT 04NOV24 - [SDR 4DPA2024102700002](https://openairdocs.org/sdr/4DPA2024102700002), Oct 27, 2024: BLEED VALVE. LEAKING. CREW REPORTED- BLEED LEAK #1 ENGINE. LIGHT WENT OUT AFTER BLEED CLOSE BUT TOOK 2 MINS TO GO OUT. DIVERT TO BURBANK. CORR ACTION- MX TROUBLESHOT TO ENG 1 BLEED V - [SDR 4DPA2024102000001](https://openairdocs.org/sdr/4DPA2024102000001), Oct 20, 2024: CARBON SEAL. LEAKING. CREW REPORTED AT APPROX 400’ FA CALLED TO REPORT SMOKE IN THE AFT CABIN AND AN EXHAUST SMELL. SMOKE DISSIPATED BY THE TIME WE LANDED. EMERGENCY DECLARED. REPORT - [SDR HNAA2024100101050](https://openairdocs.org/sdr/HNAA2024100101050), Oct 18, 2024: SKIN. NONE. EXISTING DOUBLER REPAIR FOUND ON FUSELAGE SKIN BTW FR26~27, S-33R~35R COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, REPAIR IDENTIFICATION & TRACKING - [SDR 4DPA2024101700001](https://openairdocs.org/sdr/4DPA2024101700001), Oct 17, 2024: BEARING. LEAKING. CREW REPORTED- AT APPROX 400’ FA CALLED TO REPORT SMOKE IN THE AFT CABIN AND AN EXHAUST SMELL. SMOKE DISSIPATED BY THE TIME WE LANDED. EMERGENCY DECLARED, REPOR - [SDR HNAA2024092300834](https://openairdocs.org/sdr/HNAA2024092300834), Sep 21, 2024: FUEL UNIT. FAULTED. IN FLT FUEL 1 LOW LEVEL MASTER WARNING FOLLOWED BY LOSS OF ALL FUEL INDICATIONS FACT 21SEP24 01:04 ROA FOUND CMC MESSAGE "FUEL 1 LOW LEVEL FAIL". R/R'D FUEL CON - [SDR HNAA2024080600637](https://openairdocs.org/sdr/HNAA2024080600637), Aug 5, 2024: VALVE. FAULTED. ON T/O AFTER THRUST LEVERS ADVANCED, BLD 2 VLV FAIL MSG APPEARED. REJECTED T/O. MSG DISAPPEARED WHEN THRUST LEVERS RETARDED. R & R HIGH STAGE VALVE PRESS SWITCH - [SDR HNAA2024080600636](https://openairdocs.org/sdr/HNAA2024080600636), Aug 5, 2024: VALVE. FAULTED. ON T/O AFTER THRUST LEVERS ADVANCED, BLD 2 VLV FAI MSG APPEARED. REJECTED T/O. MSG DISAPPEARED WHEN THRUST LEVERS RETARTED. R & R HIGH STAGE VALVE PRESS SWITCH - [SDR HNAA2024070200500](https://openairdocs.org/sdr/HNAA2024070200500), Jul 1, 2024: CONNECTOR. FAULTED. ENG 2 ANTI ICE VALVE FAILED. R&R PLUG P0973 ON E2 ANTI-ICE VALVE IRT SWPM 20-50-00, ALSO R&R RELAY KO536 IRT AMM 20-13-02. OPS TEST GOOD AT THIS TIME - [SDR HNAA2024032800235](https://openairdocs.org/sdr/HNAA2024032800235), Mar 27, 2024: WIRE HARNESS. DAMAGED. #2 ENG HUNG START WITH HEAVY FUEL SMELL (ONLY 0N FADEC 2A). MEL 28MAR24 06:10 RIC B08803 74-1 IGNITION SYSTEM CHANNELS. FOUND DAMAGED/BENT PIN ON PMA A PLUG PIN - [SDR HNAA2024022900166](https://openairdocs.org/sdr/HNAA2024022900166), Feb 28, 2024: COMPUTER. FAULTED. BLEED 2 VALVE FAIL DURING ICING DISPLAYED ON EICAS. R/R INTEGRATED COMPUTER IC600 NO. 2 IAW AMM 31-42-01 OPS CHECK GOOD. A/C OK FOR SERVICE. - [SDR HNAA2022113000313](https://openairdocs.org/sdr/HNAA2022113000313), Nov 29, 2022: ENGINE. FAILED. ON TAKEOFF ROLL AT APROX 10 KNOTS OIL PRESSURE ROSE AND A POP WAS HEARD. ENGINE ROLLED BACK WITH E1 OUT AND E1 NO DISPATCH MESSAGES DISPLAYED. ENGINE REMOVED AN - [SDR JJBA20221026017](https://openairdocs.org/sdr/JJBA20221026017), Oct 22, 2022: ENGINE. FAILED. #2 ENGINE FAILURE AT CRUISE. REMOVED AND REPLACED RH ENGINE. OPS AND LEAK CHECK GOOD. - [SDR JJBA20221007001](https://openairdocs.org/sdr/JJBA20221007001), Oct 4, 2022: CARBON SEAL. LEAKING. SUPPLEMENTAL (NEW) INFORMATION: REMOVED AND REPLACED #1 PACK HEAT EXCHANGER. OPS AND LEAK CHECK GOOD. REMOVED AND REPLACED HEPA FILTERS 1 AND 2. INSTALLED FLOOR - [SDR HNAA2021081900387](https://openairdocs.org/sdr/HNAA2021081900387), Aug 18, 2021: BLEED VALVE. FAULTED. BLD 1 VALVE CLOSED MSG IN FLT AND WOULD NOT CLEAR UNTIL STARTED APPROACH. R & R BLD 1 VLV REGULATOR IAW AMM 36-11-05.NO FIX. CONTINUE T/S. R/R PANEL ASSY AIR CO - [SDR HNAA2021062100265](https://openairdocs.org/sdr/HNAA2021062100265), Jun 18, 2021: ENGINE. ODOR. BURNING OIL SMELL IN COCKPIT ALSO CAUSING EYE IRRITATION. REMOVED AND REPLACE #1 ENGINE. OP CK AND LEAK CHECKS GOOD. - [SDR HNAA2021032500101](https://openairdocs.org/sdr/HNAA2021032500101), Mar 23, 2021: BLEED VALVE. MALFUNCTIONED. ON TAKE OFF ROLL W/ THRUST LEVERS ADVANCED BLEED 2 VLV FAIL APPEARS ON EICAS. R&R'D #2 ENGINE BLEED VALVE IAW EMB AMM 36-11-05-000-801-A AND 36-11-05-400-801-A. - [SDR HNAA2021022500061](https://openairdocs.org/sdr/HNAA2021022500061), Feb 23, 2021: BLEED VALVE. FAILED. PDIS 608 36-11 2329701 23FEB21 ROA CLOSE ENG 1 BLEED VALVE FAIL WHEN AT FULL POWER. EICAS MESSAGE CLEARS WHEN POWER AT IDLE. FACT 23FEB21 23:11 ROA. R & R'D HIG - [SDR HNAA2021020800046](https://openairdocs.org/sdr/HNAA2021020800046), Feb 7, 2021: ANTI-ICE VALVE. FAILED. NR 2 ENGINE ANTI ICE FAILED AFTER TAKEOFF. R & R THE NR 2 ENGINE ANTI-ICE VALVE IAW AMM 30-21-01-000/400-801A. PERFORMED OPS CHECK IN REF TO AMM 30-00-70-700-80 - [SDR HNAA2020052600158](https://openairdocs.org/sdr/HNAA2020052600158), May 23, 2020: RELAY. FAILED. E2 ATS SOV OPEN ON EICAS IN FLIGHT. R+R RELAY K0114 IAW AMM 20-13-02. RAN #2 ENGINE WITH #2 BLEED ON ABOVE 54% N2 FOR 20 MINUTES. MESSAGE DID NOT SHOW ON EICAS. - [SDR HNAA2020052600157](https://openairdocs.org/sdr/HNAA2020052600157), May 22, 2020: START VALVE. FAILED. #2 ATS SOV OPN MESSAGE APPEARED AFTER SMELLING AN UNKNOWN FUME FOR 2 MINUTES. (SMELL PERSISTED AFTER FOLLOWING QRH AND WOULD INCREASE AS THROTTLE INCREASED. OCC - [SDR HNAA2020042000143](https://openairdocs.org/sdr/HNAA2020042000143), Apr 17, 2020: CONNECTOR. LOOSE. PDIS 626 78-34 2222221 17APR20 PHL CLOSE E-1 REV DISAGREE MESSAGE ON TAKEOFF ROLL. 28574 00 PCS FACT 17APR20 23:17 ALB FOUND 2 PROX SWITCHES IN NLG TO BE LOOSE. - [SDR HNAA20200420144](https://openairdocs.org/sdr/HNAA20200420144), Apr 17, 2020: PROXIMITY SWITCH. UNSECURE. NR 1 ENGINE REVERSER DISAGREE MESSAGE ON TAKEOFF ROLL. FOUND 2 PROXIMITY SWITCHES IN NLG TO BE LOOSE. SECURED THE CONNECTORS IAW SWPM 20-50-00. OPS CHECKED GOOD - [SDR HNAA2020020700050](https://openairdocs.org/sdr/HNAA2020020700050), Feb 6, 2020: WARNING MESSAGE. ACTIVATED. AIRCRAFT RECEIVED LIGHTENING STRIKE. E1 OUT MASTER CAUTION FOLLOWED BY A HIGH SPIKE OF ITT ON ENG#1. THEN ENGINE 1 ROLL BACK AND SHUT OFF. AFTER LANDING E1 EXCE - [SDR ASOA2019121864066](https://openairdocs.org/sdr/ASOA2019121864066), Dec 16, 2019: ENGINE. FAILED. IAH - FLIGHT 4047 THE CREW REPORTED THAT INITIATED CLIMB OUT AT 5000FT WHEN THRUST LEVER WAS ADVANCED #2 ENGINE FLAMED OUT. EICAS MESSAGE PRESENTED SHORTLY AFTE - [SDR HNAA20191227001](https://openairdocs.org/sdr/HNAA20191227001), Nov 29, 2019: YOKE. CRACKED. LEFT ENGINE FWD LOWER YOKE HAS CRACK ON FWD LOWER CORNER. R & R LH FWD YOKE FITTING AND GUSSET PLATE IAW EO1-71-19-0565. - [SDR LR7A2019112522214](https://openairdocs.org/sdr/LR7A2019112522214), Nov 22, 2019: ENGINE. FLAMED OUT. DURING SCHEDULED FLIGHT WHILE IN DESCENT #2 ENGINE FLAMEOUT AT 1700 FT. / INSPECTED NTS, 5TH & 10TH STAGE COMPRESSOR BLADES, INTAKE & EXHAUST, MAG PLUGS, SPEED - [SDR SIMA2019112219005](https://openairdocs.org/sdr/SIMA2019112219005), Nov 19, 2019: CARBON SEAL. FAILED. STRONG BURNING SMELL EACH TIME ANTI-ICEING CAME ON-C/A-REMOVED AND REPLACED RH ENGINE #0 CARBON SEAL IAW RRMM TASK 72-25-25-000-801 & 72-25-25-400-801 AND OPC I - [SDR HNAA2019112700367](https://openairdocs.org/sdr/HNAA2019112700367), Nov 17, 2019: WARNING MESSAGE. ILLUMINATED. E1 REV DISAGREE DURING TAKE-OFF (C/W TAKE 78-31-01-980-801).....FIX: MELD IAW 78-2 - [SDR HNAA2019111500365](https://openairdocs.org/sdr/HNAA2019111500365), Nov 14, 2019: IGNITER. FAILED. #2 ENG HUNG START AT 32% N2. FOLLOWE BY ODOR IN CABIN....FIX: R&RD B IGNITOR IAW MM 74-21-10 GROUND RUN A/C, OPS CHECK GOOD.OK FOR SERVICE - [SDR HNAA2019110400338](https://openairdocs.org/sdr/HNAA2019110400338), Nov 2, 2019: WARNING SYSTEM. ACTIVATED. PDIS 644 78-33 1997531 02NOV19 ROC ASSGN ENG 2 REV DISAGREE AFTER TAKE OFF EDGAR HISTORY: NONE MEL 02NOV19 16:17 ROC C30609 78-2 ENG 1 OR 2 REV DISAGREE MESSAGE - [SDR HNAA2019110400340](https://openairdocs.org/sdr/HNAA2019110400340), Nov 2, 2019: ENGINE. LEAKING. MDIS 657 72-13 2081341 02NOV19 CLT ASSGN OIL LEAK #2 ENG AFT END NEAR DIFFUSER. FIRE IN EXHAU ST FOR 1 TO 2 MINUTES 26631 00 EK ENGINE CHANGE IS CURRENTLY IN PR - [SDR SIMA2019103029004](https://openairdocs.org/sdr/SIMA2019103029004), Oct 29, 2019: MAGNETIC SEAL. LEAKING. PARKED AT THE GATE, SHUTTING DOWN ENGINE #2 PRODUCED WHITE SMOKE AND A VERY STRONG ODER IN THE COCKPIT DURING TAXI. T/S PER ETN-EM-79-015. FOUND LTP SHAFT SEAL - [SDR SIMA201908132001](https://openairdocs.org/sdr/SIMA201908132001), Aug 12, 2019: CLAMP. LOOSE. NR 1 ENG POWER FLUCTUATED N1,N2 AND ITT RISE ASSOCIATED WITH POWER CHANGES. MOST NOTICABLE AT MD RANGE POWER SETTINGS. FOUND BOTH LH ENG CHECK VALVE CLAMPS LOOS - [SDR HNAA2019081300225](https://openairdocs.org/sdr/HNAA2019081300225), Aug 9, 2019: WARNING MESSAGE. FALSE ACTIVATION. CREW CALLED WITH REJECTED TAKE-OFF, NR 2 BLEED VALVE FAILED MESSAGE. MESSAGE WENT AWAY AND CREW CONTENT WITH CONTINUING FLIGHT. All 3,309: https://openairdocs.org/engine/rolls-royce-ae-3007a/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.