# Allison AE-3007C

- Type: Engine model (FAA registry)
- Registry code: 03047
- Manufacturer (registry): ALLISON
- 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: 2 registered aircraft
- Page: https://openairdocs.org/engine/allison-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 (2)

- [N104R](https://openairdocs.org/aircraft/N104R): [Air Play LLC](https://openairdocs.org/faa-owner/AIR%20PLAY%20LLC), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), built 1999, S/N 750-0095
- [N751XJ](https://openairdocs.org/aircraft/N751XJ): [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 750-0151

## 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 20240325003399I](https://openairdocs.org/incident/20240325003399I), Mar 25, 2024: Cessna 750 (N246JR), Greenville, MS, Minor damage. During landing approach pilot reported terrain induced, convective turbulance. Winds were reported se at 26 gusts to 41. In the transition to land, rnw 18, the…

## 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/allison-ae-3007c/reports.md

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