# Allison AE-3007A1/3

- Type: Engine model (FAA registry)
- Registry code: 03036
- Manufacturer (registry): ALLISON
- Model: AE 3007A1/3
- 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: 9 registered aircraft
- Page: https://openairdocs.org/engine/allison-ae-3007a1-3

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 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 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 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 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 2003-25-08](https://openairdocs.org/ad/2003-25-08): 1st and 2nd stage turbine spacers · Rolls-Royce AE 3007A1, AE 3007A1E, AE 3007A1P and 3 more. Effective Jan 21, 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 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 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 2008-19-51](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 (9)

- [N12145](https://openairdocs.org/aircraft/N12145): [United Airlines Inc](https://openairdocs.org/faa-owner/UNITED%20AIRLINES%20INC), [Chicago, IL](https://openairdocs.org/faa-place/IL/Chicago), built 2003, S/N 145745
- [N135SX](https://openairdocs.org/aircraft/N135SX): [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 2003, S/N 145728
- [N254JX](https://openairdocs.org/aircraft/N254JX): [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 2000, S/N 145275
- [N825AE](https://openairdocs.org/aircraft/N825AE): [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 2002, S/N 145589
- [N836AE](https://openairdocs.org/aircraft/N836AE): [Corporate Flight Management Inc DBA](https://openairdocs.org/faa-owner/CORPORATE%20FLIGHT%20MANAGEMENT%20INC%20DBA), [Smyrna, TN](https://openairdocs.org/faa-place/TN/Smyrna), built 2002, S/N 145635
- [N837AE](https://openairdocs.org/aircraft/N837AE): [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 2002, S/N 145647
- [N838AE](https://openairdocs.org/aircraft/N838AE): [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 2002, S/N 145651
- [N840AE](https://openairdocs.org/aircraft/N840AE): [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 2002, S/N 145656
- [N856AE](https://openairdocs.org/aircraft/N856AE): [Avi Sales & Leasing Services LLC](https://openairdocs.org/faa-owner/AVI%20SALES%20%26%20LEASING%20SERVICES%20LLC), [Muskegon, MI](https://openairdocs.org/faa-place/MI/Muskegon), built 2003, S/N 145748

## NTSB investigations (2)

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 WPR09LA255](https://openairdocs.org/ntsb/WPR09LA255), May 21, 2009: Embraer EMB-135 (N843AE), Los Angeles, CA, substantial damage. Probable cause: The flight crew's failure to adequately monitor and maintain clearance from a parked aircraft while taxiing. Contributing to the accident was an improperly parked airplane that encroached upon the…
- [NTSB NYC03LA135](https://openairdocs.org/ntsb/NYC03LA135), Jun 24, 2003: Embraer EMB-135-KL (N839AE), Boston, MA, substantial damage. Probable cause: The tug driver's failure to maintain directional control of the tug, which caused the tug to impact the airplane.

## FAA accident and incident reports (8)

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 20190925013679I](https://openairdocs.org/incident/20190925013679I), Sep 25, 2019: Embraer EMB-135KL (N855AE), Jamaica, NY, Minor damage. As passengers were boarding the aircraft a cleaning van operated by airways cleaners drove into the right wing, causing damage to the right flap and aileron.…
- [Incident 20140730014529I](https://openairdocs.org/incident/20140730014529I), Jul 30, 2014: Embraer EMB-135KL (N837AE), Flushing, NY, No damage. Envoy air, flight 3340, N837AE, was operating a revenue flight from laguardia airport, NY (lga) to knoxville, TN (tys). According to air carrier reports,…
- [Incident 20140728011679I](https://openairdocs.org/incident/20140728011679I), Jul 28, 2014: Embraer EMB-135KL (N856AE), Champaign, IL, No damage. Smoke in cabin and lav. Lav smoke indicator on eicas. Declared emergency and returned cmi.
- [Incident 20130204001899I](https://openairdocs.org/incident/20130204001899I), Feb 4, 2013: Embraer EMB-145XR (N12145), Chicago, IL, No damage. Flight departed ord and while climbing out of 700 feet, both pilots "noticed smoke billowing into the cockpit". Crew declared an emergency and requested an…
- [Accident 20090521007209A](https://openairdocs.org/incident/20090521007209A), May 21, 2009: Emb EMB135KL (N843AE), Los Angeles, CA, Minor damage. (-23) American eagle #3085 (lax-san) N843AE active aircraft was pushed back from terminal by ground crew and disconnected from tow bar. Reporting inspector…
- [Incident 20050313009459I](https://openairdocs.org/incident/20050313009459I), Mar 13, 2005: Emb EMB135KL (N825AE), Buffalo, NY. (-23) On 03/13/2004 at 0959 edst an Emb-135-KL, operated by sima, while on approach to buf entered icing conditions. When the ice protection systems cycled on,…
- [Incident 20030907032179I](https://openairdocs.org/incident/20030907032179I), Sep 7, 2003: Emb EMB135KL (N838AE), Syracuse, NY. (-23) On September 7, 2003, an American eagle, Emb-135, flt. 4320, diverted into Syracuse airport, Syracuse, NY due to smoke in the cockpit. The ARFF responded…
- [Accident 20030624012029A](https://openairdocs.org/incident/20030624012029A), Jun 24, 2003: Emb EMB135KL (N839AE), Boston, MA, Substantial damage. (-23) Date: June 24, 2003 Logan international airport Boston ma (bos) 15:15 EDT ASI: donald e. small N839AE Embraer Emb-135-KL s/n 145653 FSDO-01 Tuesday…

## Service difficulty reports (228, newest 50)

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

- [SDR HNAA2026012300074](https://openairdocs.org/sdr/HNAA2026012300074), Jan 22, 2026: ENGINE. AUTO SHUTDOWN. NR 2 ENGINE FAILED ON CLIMBOUT AT 91 PERCENT N1. NR 2 ENGINE WAS R & R.
- [SDR 4DPA2025041500001](https://openairdocs.org/sdr/4DPA2025041500001), Apr 15, 2025: ENGINE. FAILED. CREW REPORTED- ENGINE 1 FAILED AT 90 KTS ON TAKEOFF ROLL. EXTREMELY LOUD BOOM HEARD ACROSS THE AIRPORT, MULTIPLE MESSAGES APPEARED WHILE REJECTING INCLUDING WAR
- [SDR FJTA2024080205311](https://openairdocs.org/sdr/FJTA2024080205311), Jul 29, 2024: METERING UNIT. FAILED. CREW REPORTED E2 FADEC SWITCHING FROM A TO B WITH UN-COMMANDED THROTTLE ADVANCE. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE FUEL PUMP METERING UNIT (FPMU)
- [SDR 2024FA0000196](https://openairdocs.org/sdr/2024FA0000196), Nov 16, 2023: ENGINE. AUTO SHUTDOWN. N1023C DEPARTED MMSD AT 1530 LOCAL TIME IN CABO, MEXICO. ENROUTE TO KVNY AT APPROXIMATELY 1647 (1HOUR, 47 MINUTES) INTO THE FLIGHT, A LOUD BANG WAS HEARD, AND T
- [SDR 2022FA0000137](https://openairdocs.org/sdr/2022FA0000137), Feb 24, 2022: NONE. NONE. # 2 ENG. SN: CAE312165 TT: 28158:12 TC: 25262. DESCRIPTION - CAPTAIN REPORTED THAT UPON LANDING SHE HAD NO BRAKES.
- [SDR 4DPA2021121300001](https://openairdocs.org/sdr/4DPA2021121300001), Dec 13, 2021: DUCT. BROKEN. ISSUE-CREW REPORTED ENGINE 2 ITT WENT TO RED LIMIT RIGHT AFTER V1 ON TAKEOFF ROTATION, AFTER ACCELERATION ALTITUDE REDUCED THE POWER AND DIVERTED BACK TO KBUR, 
- [SDR 4DPA2021071300001](https://openairdocs.org/sdr/4DPA2021071300001), Jul 9, 2021: O-RING. DAMAGED. RTF DUE TO BLD 1 LK(PACK 2 WAS ALREADY ON MEL) DISC: BLD 1 LEAK MESSAGE CORR ACTION: FOUND O-RING IN JOINTS 9, 15,17,19 BROKEN REMOVED AND REPLACED O-RINGS COMP
- [SDR 4DPA202105300001](https://openairdocs.org/sdr/4DPA202105300001), May 30, 2021: FUEL FILTER. DIRTY. E1 FUEL IMPENDING BYPASS MESSAGE ENROUTE RNO. QRH CONSULTED DIVERTED BACK TO BUR. R&R'D FILTER E1 RESET IMP BYPASS INDICATOR LEAK AND OPS TEST GOOD
- [SDR SIMA2020012317010](https://openairdocs.org/sdr/SIMA2020012317010), Jan 17, 2020: TRANSDUCER. FAILED. ICE COND A-ICE INOP IN FLIGHT. E2 A/ICE FAIL PRESENTED WITH OVERRIDE KNOB SELECTED TO ALL. "TRANSFERRED TO NRWC 812-DFW-03218" -C/A- REMOVED AND REPLACED E2 A/I
- [SDR SIMA201911276001](https://openairdocs.org/sdr/SIMA201911276001), Nov 26, 2019: ANTI-ICE VALVE. MALFUNCTIONED. E2 A/ICE FAIL INFLIGHT RAN QRH AND LIGHT DID NOT GO OUT UNTIL WE EXITED ICING CONDITIONS-C/A-AT THIS TIME DEFERREWD # 2 ENGINE ANTI-ICE VALVE AS PER MEL MTX ACT
- [SDR SIMA201910310003](https://openairdocs.org/sdr/SIMA201910310003), Oct 30, 2019: BLEED VALVE. FAILED. PACK VALVE AND BLD VALVE CLOSED INFLIGHT ON #2. PACK 2 VALVE C/B POPPED.-C/A-REMOVED AND REPLACED #2 PACK VALVE IAW AMM 21-51-01. OPERATIONAL CHECK GOOD. #2 BLD
- [SDR SIMA201906175002](https://openairdocs.org/sdr/SIMA201906175002), Jun 15, 2019: ENGINE. FIRE. GROUND PERSONNEL OBSERVED FLAMES OUT OF BACK OF ENGINE #1 AND WHITE SMOKE COMING OUT OF FRONT AT SHUTDOWN. NO EICAS MESSAGES PRESENT. "TRANSFERRED TO NRWC 800-A
- [SDR SIMA201902221003](https://openairdocs.org/sdr/SIMA201902221003), Feb 21, 2019: ANTI-ICE VALVE. FAILED. E2 A ICE FAIL IN AUTO MODE WHILE IN ICE CONDITIONS. VALVE FAILED CLOSED-C/A-DEFFERED E2 ANTI ICE M PROCEDURE C/W. REMOVED AND REPLACED E2 ANTI-ICING VALVE IAW E
- [SDR V8XA201901260001](https://openairdocs.org/sdr/V8XA201901260001), Jan 25, 2019: ELECTRONIC UNIT. FAULTY. LG AIR/GND FAIL MESSAGE ON CLIMB OUT MESSAGE PERSISTED DESPITE CYCLING THE GEAR TWO TIMES DIVERTED TO KGPYT FOR LONG RUNWAYS FOLLOWED QRH PROCEDURE LANDED FLAPS
- [SDR SIMA201812043003](https://openairdocs.org/sdr/SIMA201812043003), Dec 3, 2018: ANTI-ICE VALVE. FAILED. PERFORMING IN AIR ICE TEST, RCVD E2 A/I FAIL. PER QRH CANNOT ENTER ICING CONDITION RTB-LGA-C/A-REMOVED AND REPLACED ENGINE A/I VALVE IAW EMB 140 AMM 30-21-01. O
- [SDR SIMA201810085001](https://openairdocs.org/sdr/SIMA201810085001), Oct 5, 2018: ENGINE. CONTAMINATED. ON DESCENT DIRTY SOCK SMELL IN COCKPIT AND CABIN A SLIGHT HAZE WAS VISABLE IN THE AIR. -C/A-FOUND OIL IN LT ENG FLOWPATH PER RRMM 72-30-00-200-803-A, REMOVED AN
- [SDR V8XA2018061500000](https://openairdocs.org/sdr/V8XA2018061500000), Jun 13, 2018: VHF COMM. INTERMITTENT. UPON CLIME OUT 4000 AGL NR 2 RMU DISPLAY, NR 2 COMM DISPLAYED DASHES, NR 2 TRANSPONDER DISPLAYED DASHES, NR 2 TCAS DISPLAYED DASHES. NR 1 RMU DISPLAY, NR 1 TRAN
- [SDR FJTA201806129191](https://openairdocs.org/sdr/FJTA201806129191), Jun 7, 2018: WARNING MESSAGE. ACTIVATED. CLIMBING THRU FL180, IN ICING CONDITIONS, THE ANTI ICE CAME ON THEN THE NR 2 OIL TEMP WENT TO 147C, BROUGHT THRUST LEVER BACK TO IDLE AND TEMP WENT TO 156 C. ST
- [SDR SIMA201806076008](https://openairdocs.org/sdr/SIMA201806076008), Jun 6, 2018: ENGINE. VIBRATION. AT 6000 FT, THE NR 2 ENGINE STARTED TO VIBRATE AND MADE A LOUD SOUND, EICASE INDICATED E2 CTL FAIL, FOLLOWED QRH PROCEDURES, STARTED THE APU AND RECOVERED THE E
- [SDR SIMA20180221005](https://openairdocs.org/sdr/SIMA20180221005), Feb 21, 2018: IGNITER. FAILED. DURING TAXI, TRIED TO START THE NR 2 ENGINE, HAD A HUNG START, RAN THE CHECK LIST HAD GAS FUMES , RAN CHECK LIST AND RETURNED TO GATE. REMOVED AND REPLACED THE 
- [SDR SIMA20171113001](https://openairdocs.org/sdr/SIMA20171113001), Nov 13, 2017: ENGINE. ODOR. MUSTY ODOR AFTER TL TO THRUST SET POSITION ON TAKEOFF ROLL. AT 500 FT HAD A LAVATORY SMOKE WARNING MESSAGE. FA REPORTED SMOKE IN CABIN, RETURNED FOR LANDING. FA
- [SDR ASOA201701234002](https://openairdocs.org/sdr/ASOA201701234002), Jan 23, 2017: ENGINE. FLAMED OUT. IAH - FLIGHT 4231, THE CREW REPORTED ENG NR 2 OUT IN FLIGHT. THE AIRCRAFT LANDED IN IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER 2 ENG
- [SDR 4DPA201611040001](https://openairdocs.org/sdr/4DPA201611040001), Oct 31, 2016: CABIN PRESSURE. MALFUNCTIONED. CLIMBING THROUGH 13000', THE CAPTAIN NOTICED THE CAB ALT READ 9900', IT HAD TURNED AMBER. HE SLOWED THE ASCENT AND CHECKED THE CONFIGURATION OF THE PRESSURIZATI
- [SDR ASOA201610164074](https://openairdocs.org/sdr/ASOA201610164074), Oct 11, 2016: FADEC. MALFUNCTIONED. FLIGHT 4193, THE CREW REPORTED THAT IMMEDIATELY AFTER TAKEOFF, THE NR 2 ENGINE SHUTDOWN, WITH NO N2 OR FUEL FLOW, AND RECEIVED E2 NO DISP, E2 CTL FAIL, SPOILER 
- [SDR ASOA201610164075](https://openairdocs.org/sdr/ASOA201610164075), Oct 11, 2016: FADEC. INOPERATIVE. FLIGHT 4193, THE CREW REPORTED THAT IMMEDIATELY AFTER TAKEOFF, THE NR 2 ENGINE SHUTDOWN, WITH NO N2 OR FUEL FLOW, AND RECEIVED E2 NO DISP, E2 CTL FAIL, SPOILER 
- [SDR ASOA201610164076](https://openairdocs.org/sdr/ASOA201610164076), Oct 11, 2016: METERING UNIT. INOPERATIVE. FLIGHT 4193, THE CREW REPORTED THAT IMMEDIATELY AFTER TAKEOFF, THE NR 2 ENGINE SHUTDOWN, WITH NO N2 OR FUEL FLOW, AND RECEIVED E2 NO DISP, E2 CTL FAIL, SPOILER 
- [SDR 4DPA20160923](https://openairdocs.org/sdr/4DPA20160923), Sep 21, 2016: CABIN PRESSURE. MALFUNCTIONED. CLIMBING THROUGH 15000 FT, THE CAPTAIN NOTICED THE CABIN ALTITUDE READS 9800 FT; IT HAD TURNED AMBER. HE SLOWED THE ASCENT AND CHECKED THE CONFIGURATION OF THE 
- [SDR CICB2016FA0000208](https://openairdocs.org/sdr/CICB2016FA0000208), May 3, 2016: TIRE. SEPARATED. THE NR 1 MAIN WHEEL ASSEMBLY HAD THE TIRE TREAD SEPARATED FROM THE TIRE AND DAMAGED THE LT MLG DOOR, THE LT AUXILIARY LANDING GEAR DOOR AND THE AFT MAIN LANDING
- [SDR SIMA20150908003](https://openairdocs.org/sdr/SIMA20150908003), Sep 8, 2015: ENGINE. SMOKE. SMOKE COMING OUT OF ENG 2, AFTER SHUTDOWN WITH A STRONG SMELL OF BURNED OIL. COMPLIED WITH ETN-EM-79-015 STEPS 1 - 9. RETURNED ENG TO SERVICE. NO FURTHER DEFECT
- [SDR SIMA20150204002](https://openairdocs.org/sdr/SIMA20150204002), Feb 4, 2015: ENGINE. FAILED. LAVATORY SMOKE AFTER TAKEOFF, AOM 1 PROCEDURE COMPLIED WITH. FLIGHT ATTENDANT REPORTS SMOKE & FUMES IN CABIN. R & R NR 2 ENGINE IAW WC 71-000-00. OPERATIONS CHE
- [SDR SIMA20150128004](https://openairdocs.org/sdr/SIMA20150128004), Jan 28, 2015: SKIN. CRACKED. RIGHT ENG TR LOWER DOOR SKIN HAS A CRACK AROUND A RIVET AT THE OTBD CORNER. REPAIRED IAW SRM 54-30-01 FIGURE 207.
- [SDR SIMA20150121003](https://openairdocs.org/sdr/SIMA20150121003), Jan 21, 2015: VALVE. FAILED. ABORTED TAKEOFF, AT LOW SPEED NR 2 ENGINE ATTCS NO MARGIN EICAS MESSAGE. NR 2 ENGINE EXCEEDENCE EICAS CAUTION. NR 2 ENGINE HAS VALVE FAIL EICAS MESSAGE. TROUBLE
- [SDR SIMA20141119004](https://openairdocs.org/sdr/SIMA20141119004), Nov 19, 2014: CONTROL PANEL. MALFUNCTIONED. PRIOR TO DECENT, NR 1 FUEL LOW PRESSURE ANNUNCIATION ILLUMINATED FOLLOWED BY CLICKING RELAYS. ABOUT THE SAME TIME RECEIVED AN ELECTRICAL BURNING ODOR BOTH IN TH
- [SDR CHQA20140923291](https://openairdocs.org/sdr/CHQA20140923291), Sep 23, 2014: TRUNNION. CORRODED. DURING INSPECTION THE RT MLG FWD TRUNNION FITTING WAS FOUND TO BE CORRODED. THE TRUNNION WAS REPAIRED IAW ETD 2014-145-080380.
- [SDR CHQA20140923292](https://openairdocs.org/sdr/CHQA20140923292), Sep 23, 2014: TRUNNION. CORRODED. DURING INSPECTION THE LT MLG FWD TRUNNION FITTING WAS FOUND TO BE CORRODED. THE TRUNNION WAS REPAIRED IAW ETD 2014-145-080380.
- [SDR CHQA20140922290](https://openairdocs.org/sdr/CHQA20140922290), Sep 22, 2014: TRUNNION. CORRODED. DURING INSPECTION THE RT MLG AFT TRUNNION FITTING WAS FOUND TO BE CORRODED. THE FITTING WAS REPAIRED IAW ETD 2014-145-080380.
- [SDR CHQA20140921293](https://openairdocs.org/sdr/CHQA20140921293), Sep 21, 2014: FLOOR SUPPORT. CORRODED. DURING INSPECTION CORROSION WAS FOUND ON THE CTR OMEGA BEAM AT FRAME 20. THE BEAM WAS REPLACED IAW SRM 51-40-02.
- [SDR CHQA20140921294](https://openairdocs.org/sdr/CHQA20140921294), Sep 21, 2014: FLOOR SUPPORT. CORRODED. DURING INSPECTION CORROSION WAS FOUND ON THE LT OMEGA BEAM AT FRAME 20. THE BEAM WAS REPLACED IAW 51-40-02.
- [SDR CHQA20140917295](https://openairdocs.org/sdr/CHQA20140917295), Sep 17, 2014: MOUNT BRACKET. WORN. DURING INSPECTION THE LT HORIZONTAL STABILIZER PIN ANTI-ROTATION PIN & MOUNTING BRACKET WAS FOUND TO BE WORN. THE BRACKET WAS REPLACED IAW SRM 51-40-02.
- [SDR SIMA20140908010](https://openairdocs.org/sdr/SIMA20140908010), Sep 8, 2014: ENGINE. FAILED. ABORTED TAKEOFF DUE TO SMOKE IN COCKPIT. BELOW 80 FTS OIL SMELL & VISIBLE SMOKE. PERFORMED BORESCOPE ON BOTH NR 1 AND NR 2 ENG. FOUND NR 1 ENG WET OF OIL COOL S
- [SDR CHQA20140908266](https://openairdocs.org/sdr/CHQA20140908266), Sep 8, 2014: TRUNNION. CORRODED. DURING INSPECTION CORROSION WAS FOUND ON THE RT MLG UPPER FWD TRUNNION. THE TRUNNION WAS REPAIRED IAW ETD 2014-145-075943A.
- [SDR CHQA20140908267](https://openairdocs.org/sdr/CHQA20140908267), Sep 8, 2014: TRUNNION. CORRODED. DURING INSPECTION CORROSION WAS FOUND ON THE LT MLG FWD UPPER TRUNNION. THE TRUNNION WAS REPAIRED IAW ETD 2014-145-075943A.
- [SDR CHQA20140827260](https://openairdocs.org/sdr/CHQA20140827260), Aug 27, 2014: FITTING. DAMAGED. DURING INSPECTION THE LT AILERON PCA OTBD FITTING WAS FOUND TO HAVE AN ENLARGED HOLE. THE LT AILERON PCA OTBD FITTING WAS REPLACED IAW SRM 51-40-02.
- [SDR CHQA20140827269](https://openairdocs.org/sdr/CHQA20140827269), Aug 27, 2014: BRACKET. CHAFED. DURING INSPECTION THE LT EMER EXIT DOOR WAS FOUND TO BE CHAFED & BENT ON THE BRACKET ON THE AFT SIDE. THE DOOR WAS REPAIRED IAW ETD 2014-145-073270.
- [SDR CHQA20140826265](https://openairdocs.org/sdr/CHQA20140826265), Aug 26, 2014: BEARING. CORRODED. DURING INSPECTION CORROSION WAS FOUND ON THE LT MLG UPPER AFT TRUNNION BEARING. THE TRUNNION BEARING WAS REPAIRED IAW ETD 2014-145-075943A.
- [SDR CHQA20140826264](https://openairdocs.org/sdr/CHQA20140826264), Aug 24, 2014: BEARING. CORRODED. DURING INSPECTION CORROSION WAS FOUND ON THE RT MLG UPPER AFT TRUNNION BEARING. THE TRUNNION BEARING WAS REPAIRED IAW ETD 2014-145-075943.
- [SDR CHQA20140824271](https://openairdocs.org/sdr/CHQA20140824271), Aug 24, 2014: SKIN. DENTED. DURING INSPECTION A DENT FROM STRIKE DAMAGE BETWEEN FRAME 70 - 72 & STRINGERS 13 - 14R WAS REPAIRED IAW ETD 2014-145-071479.
- [SDR CHQA20140822261](https://openairdocs.org/sdr/CHQA20140822261), Aug 22, 2014: REPAIR. CORRODED. DURING INSPECTION A PREVIOUS REPAIR ON THE LT OMEGA BEAM FLOOR FLANGE AT FRAME 20 WAS FOUND TO BE CORRODED. THE FLANGE WAS REPAIRED IAW SRM 53-00-10.
- [SDR CHQA20140822263](https://openairdocs.org/sdr/CHQA20140822263), Aug 22, 2014: FLOOR SUPPORT. CORRODED. DURING INSPECTION THE CTR OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. THE CTR OMEGA BEAM WAS REPLACED IAW SRM 51-40-02.
- [SDR CHQA20140820262](https://openairdocs.org/sdr/CHQA20140820262), Aug 20, 2014: REPAIR. CHAFED. DURING INSPECTION A PREVIOUS REPAIR WAS FOUND TO BE CHAFED BELOW ACCESS DOOR 113EL. THE PREVIOUS REPAIR DOUBLER WAS REPLACED IAW SRM53-11-01.

All 228: https://openairdocs.org/engine/allison-ae-3007a1-3/reports.md

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