# Service difficulty reports: Allison AE-3007A1/3

A list on [Allison AE-3007A1/3](https://openairdocs.org/engine/allison-ae-3007a1-3.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 5 · 228 reports

- [SDR HNAA2026012300074](https://openairdocs.org/sdr/HNAA2026012300074.md): Engine · auto shutdown · Jan 22, 2026 · N677AE · Emb EMB145LR · Engine Emergency Shutdown System
  > NR 2 ENGINE FAILED ON CLIMBOUT AT 91 PERCENT N1. NR 2 ENGINE WAS R & R.
- [SDR 4DPA2025041500001](https://openairdocs.org/sdr/4DPA2025041500001.md): Engine · failed · Apr 15, 2025 · N252JX · Emb EMB135LR · Engine (Turbine/Turboprop)
  > CREW REPORTED- ENGINE 1 FAILED AT 90 KTS ON TAKEOFF ROLL. EXTREMELY LOUD BOOM HEARD ACROSS THE AIRPORT, MULTIPLE MESSAGES APPEARED WHILE REJECTING INCLUDING WARNING FOR E1 ENGINE OUT AS WELL AS RUDDER AP HARD OVER FAIL, E1 SHORT DISPATCH, AND A FEW OTHERS. STR
- [SDR FJTA2024080205311](https://openairdocs.org/sdr/FJTA2024080205311.md): Metering Unit · failed · Jul 29, 2024 · N531CN · Emb EMB135KL · Engine Fuel Pump
  > 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) TO BE FAILED. THE FPMU WAS REMOVED AND REPLACED, AND OPS CHECKED GOOD.
- [SDR 2024FA0000196](https://openairdocs.org/sdr/2024FA0000196.md): Engine · auto shutdown · Nov 16, 2023 · N1023C · Emb EMB135LR · Engine (Turbine/Turboprop)
  > 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 THE CREW IMMEDIATELY WITNESSED THE #1 ENGINE SPOOL DOWN RAPIDLY RESULTING IN LOSS OF ENGINE #1. THE F
- [SDR 2022FA0000137](https://openairdocs.org/sdr/2022FA0000137.md): None · none · Feb 24, 2022 · N712A · Emb EMB135LR · Landing Gear Brake System
  > # 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.md): Duct · broken · Dec 13, 2021 · N262JX · Emb EMB135LR · Engine (Turbine/Turboprop)
  > 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, AND EVEN AFTER LANDING ITT SHOWS 720 ON ENGINES IDLE. AMT'S DISCOVERED DISCHARGE TUBE ASSY BROKEN OF
- [SDR 4DPA2021071300001](https://openairdocs.org/sdr/4DPA2021071300001.md): O-Ring · damaged · Jul 9, 2021 · N259JX · Emb EMB135LR · Engine Bleed Air System
  > 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 COMPLETED BLEED LEAK OPS CHECK GOOD
- [SDR 4DPA202105300001](https://openairdocs.org/sdr/4DPA202105300001.md): Fuel Filter · dirty · May 30, 2021 · N258JX · Emb EMB135LR · Engine Fuel Distribution
  > 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.md): Transducer · failed · Jan 17, 2020 · N812AE · Emb EMB135KL · Engine Anti-Icing System
  > 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 PRESS. TRANDUCER IAW EMB 140 AMM 30-21-06 AND REMOVED AND REPLACED E2 HARNESS IAW 71-51-01 OPS CHEC
- [SDR SIMA201911276001](https://openairdocs.org/sdr/SIMA201911276001.md): Anti-Ice Valve · malfunctioned · Nov 26, 2019 · N812AE · Emb EMB135KL · Engine Anti-Icing System
  > 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 ACTION C/W
- [SDR SIMA201910310003](https://openairdocs.org/sdr/SIMA201910310003.md): Bleed Valve · failed · Oct 30, 2019 · N843AE · Emb EMB135KL · Compressor Bleed Valve
  > 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 VALVE OPS CHECK GOOD IAW AMM 36-11-05.
- [SDR SIMA201906175002](https://openairdocs.org/sdr/SIMA201906175002.md): Engine · fire · Jun 15, 2019 · N800AE · Emb EMB135KL · Engine (Turbine/Turboprop)
  > 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-ABI-02406"-C/A-REMOVED AND REPLACED #1 ENGINE IAW WORK CARD 71-000-00 LEAK CHECK GOOD OPS CHECK GOOD
- [SDR SIMA201902221003](https://openairdocs.org/sdr/SIMA201902221003.md): Anti-Ice Valve · failed · Feb 21, 2019 · N813AE · Emb EMB135KL · Engine Anti-Icing System
  > 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 EMB 140 AMM 30-21-01, OPS CK GOOD, MEL RESTORED
- [SDR V8XA201901260001](https://openairdocs.org/sdr/V8XA201901260001.md): Electronic Unit · faulty · Jan 25, 2019 · N234BZ · Emb EMB135LR · Landing Gear Position and Warning
  > 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 45 AFTER LANDING MESSAGE PERSISTED ON EICAS POWER AIRCRAFT DOWN THEN POWERED UP LG AIR/GND WENT AWA
- [SDR SIMA201812043003](https://openairdocs.org/sdr/SIMA201812043003.md): Anti-Ice Valve · failed · Dec 3, 2018 · N824AE · Emb EMB135KL · Engine Anti-Icing System
  > 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. OPC DONE IAW EMB 140 AMM 30-00-00 ICE AND RAIN PROTECTION ADJ/TEST. NO DEFECTS NOTED.
- [SDR SIMA201810085001](https://openairdocs.org/sdr/SIMA201810085001.md): Engine · contaminated · Oct 5, 2018 · N813AE · Emb EMB135KL · Engine (Turbine/Turboprop)
  > 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 AND REPLACED TURBO LT ENG IAW W/W 71-00-00 OPC/LEAK CHECK GOOD, COMPLIED WITH ODOR EVENT ETN-EM-72-034
- [SDR V8XA2018061500000](https://openairdocs.org/sdr/V8XA2018061500000.md): Vhf Comm · intermittent · Jun 13, 2018 · N234BZ · Emb EMB135LR · VHF Communications System
  > 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 TRANSPONDER DISPLAYED DASHES, TCAS DISPLAYED DASHES. ATC REQUESTED IDENT FOR TRANSPONDERS CREW SWITCHED
- [SDR FJTA201806129191](https://openairdocs.org/sdr/FJTA201806129191.md): Warning Message · activated · Jun 7, 2018 · N16919 · Emb EMB145LR · Engine Anti-Icing System
  > 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. STARTED DECENT BACK TO DEPARTURE, LEFT ICING CONDITIONS. THE ANTI TURNED OFF AND THE RIGHT OIL TEM
- [SDR SIMA201806076008](https://openairdocs.org/sdr/SIMA201806076008.md): Engine · vibration · Jun 6, 2018 · N840AE · Emb EMB135KL · Engine (Turbine/Turboprop)
  > 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 ENGINE AT ABOUT 3000 FT. REMOVED AND REPLACED THE NR 2 ENGINE ASSY IAW WC 71-000-00, OPS AND LEAK
- [SDR SIMA20180221005](https://openairdocs.org/sdr/SIMA20180221005.md): Igniter · failed · Feb 21, 2018 · N849AE · Emb EMB135KL · Spark Plug/Igniter
  > 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 RT ENGINE IGNITOR A IAW AMM 74-24-01. OPS CHECKED GOOD, NO DEFECTS NOTED.
- [SDR SIMA20171113001](https://openairdocs.org/sdr/SIMA20171113001.md): Engine · odor · Nov 13, 2017 · N856AE · Emb EMB135KL · Engine (Turbine/Turboprop)
  > 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 REPORTED THE SMOKE ODOR DISAPATED BY THE TIME OF FINAL APPROACH. REMOVED AND REPLACED BOTH ENGIN
- [SDR ASOA201701234002](https://openairdocs.org/sdr/ASOA201701234002.md): Engine · flamed out · Jan 23, 2017 · N15527 · Emb EMB135LR · Engine (Turbine/Turboprop)
  > 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 ENGINE, OPERATIONALLY TESTED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR 4DPA201611040001](https://openairdocs.org/sdr/4DPA201611040001.md): Cabin Pressure · malfunctioned · Oct 31, 2016 · N251JX · Emb EMB135LR · Cabin Pressure Control System
  > 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 PRESSURIZATION SYSTEM AND THE BLEEDS AND PACKS. FOUND THE CONFIGURATION OF THE AIRCRAFT TO BE SET PROPERLY FOR
- [SDR ASOA201610164074](https://openairdocs.org/sdr/ASOA201610164074.md): Fadec · malfunctioned · Oct 11, 2016 · N15527 · Emb EMB135LR · Engine (Turbine/Turboprop)
  > 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 FAIL, AND RUD HDOV PROT FAIL MESSAGES. THE AIRCRAFT RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDEN
- [SDR ASOA201610164075](https://openairdocs.org/sdr/ASOA201610164075.md): Fadec · inoperative · Oct 11, 2016 · N15527 · Emb EMB135LR · Engine (Turbine/Turboprop)
  > 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 FAIL, AND RUD HDOV PROT FAIL MESSAGES. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDEN
- [SDR ASOA201610164076](https://openairdocs.org/sdr/ASOA201610164076.md): Metering Unit · inoperative · Oct 11, 2016 · N15527 · Emb EMB135LR · Engine (Turbine/Turboprop)
  > 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 FAIL, AND RUD HDOV PROT FAIL MESSAGES. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT
- [SDR 4DPA20160923](https://openairdocs.org/sdr/4DPA20160923.md): Cabin Pressure · malfunctioned · Sep 21, 2016 · N252JX · Emb EMB135LR · Cabin Pressure Control System
  > 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 PRESSURIZATION SYSTEM AND THE BLEEDS AND PACKS. FOUND THE CONFIGURATION OF THE AIRCRAFT TO BE SET PR
- [SDR CICB2016FA0000208](https://openairdocs.org/sdr/CICB2016FA0000208.md): Tire · separated · May 3, 2016 · N1023C · Emb EMB135LR · Tire
  > 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 GEAR DOOR CONNECTING ROD. NO DAMAGE TO ANY OTHER STRUCTURE. INVESTIGATION SHOWS THAT THE TREAD SE
- [SDR SIMA20150908003](https://openairdocs.org/sdr/SIMA20150908003.md): Engine · smoke · Sep 8, 2015 · N838AE · Emb EMB135KL · Engine (Turbine/Turboprop)
  > 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 DEFECTS NOTED AT THIS TIME.
- [SDR SIMA20150204002](https://openairdocs.org/sdr/SIMA20150204002.md): Engine · failed · Feb 4, 2015 · N848AE · Emb EMB135KL · Engine (Turbine/Turboprop)
  > 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 CHECKED GOOD. LEAK CHECKED GOOD. PERFORMED ETN-EM-72-034 FOR NEW ENG. NO SMOKE OR ODOR PRESENT.
- [SDR SIMA20150128004](https://openairdocs.org/sdr/SIMA20150128004.md): Skin · cracked · Jan 28, 2015 · N856AE · Emb EMB135KL · Engine Thrust Reverser
  > 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.md): Valve · failed · Jan 21, 2015 · N836AE · Emb EMB135KL · Compressor Bleed Control
  > 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. TROUBLESHOT IAW FIM 72-00-00. R & R COMPRESSOR AIR DISCHARGER TUBE & COMPRESSOR ACCELERATION BLEED C
- [SDR SIMA20141119004](https://openairdocs.org/sdr/SIMA20141119004.md): Control Panel · malfunctioned · Nov 19, 2014 · N823AE · Emb EMB135KL · Fuel Controlling System
  > 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 THE COCKPIT & CABIN. RAN FUEL LOW PRESSURE, CABIN & COCKPIT FUMES CHECKLISTS. FUEL PUMP WAS ON 1A
- [SDR CHQA20140923291](https://openairdocs.org/sdr/CHQA20140923291.md): Trunnion · corroded · Sep 23, 2014 · N371SK · Emb EMB135KL · Main Landing Gear Attach Section
  > 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.md): Trunnion · corroded · Sep 23, 2014 · N371SK · Emb EMB135KL · Main Landing Gear Attach Section
  > 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.md): Trunnion · corroded · Sep 22, 2014 · N371SK · Emb EMB135KL · Main Landing Gear Attach Section
  > 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.md): Floor Support · corroded · Sep 21, 2014 · N371SK · Emb EMB135KL · Fuselage Miscellaneous Structure
  > 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.md): Floor Support · corroded · Sep 21, 2014 · N371SK · Emb EMB135KL · Fuselage Miscellaneous Structure
  > 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.md): Mount Bracket · worn · Sep 17, 2014 · N371SK · Emb EMB135KL · Horizontal Stabilizer Miscellaneous Structure
  > 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.md): Engine · failed · Sep 8, 2014 · N831AE · Emb EMB135KL · Engine (Turbine/Turboprop)
  > 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 SUMP AREA 6 O`CLOCK POS. ENG NR 1 ONLY REF ETN-EM-79-014. REMOVED AND REPLACED NR 1 ENGINE IAW W
- [SDR CHQA20140908266](https://openairdocs.org/sdr/CHQA20140908266.md): Trunnion · corroded · Sep 8, 2014 · N295SK · Emb EMB135KL · Main Landing Gear Attach Section
  > 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.md): Trunnion · corroded · Sep 8, 2014 · N295SK · Emb EMB135KL · Main Landing Gear Attach Section
  > 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.md): Fitting · damaged · Aug 27, 2014 · N295SK · Emb EMB135KL · Ailerons
  > 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.md): Bracket · chafed · Aug 27, 2014 · N295SK · Emb EMB135KL · Emergency Exits
  > 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.md): Bearing · corroded · Aug 26, 2014 · N295SK · Emb EMB135KL · Main Landing Gear Attach Section
  > 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.md): Bearing · corroded · Aug 24, 2014 · N295SK · Emb EMB135KL · Main Landing Gear Attach Section
  > 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.md): Skin · dented · Aug 24, 2014 · N295SK · Emb EMB135KL · Fuselage Main, Plate/Skin
  > 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.md): Repair · corroded · Aug 22, 2014 · N295SK · Emb EMB135KL · Fuselage Miscellaneous Structure
  > 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.md): Floor Support · corroded · Aug 22, 2014 · N295SK · Emb EMB135KL · Fuselage Miscellaneous Structure
  > 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.md): Repair · chafed · Aug 20, 2014 · N295SK · Emb EMB135KL · Fuselage Miscellaneous Structure
  > DURING INSPECTION A PREVIOUS REPAIR WAS FOUND TO BE CHAFED BELOW ACCESS DOOR 113EL. THE PREVIOUS REPAIR DOUBLER WAS REPLACED IAW SRM53-11-01.

Next page: https://openairdocs.org/engine/allison-ae-3007a1-3/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE engine_model_key = 'AE3007A13'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/allison-ae-3007a1-3/reports

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