Allison AE-3007A1P

Service difficulty reports · 849

Newest first. General aviation reporting is voluntary.

Query with SQL
duckdb -csv -c "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 = 'AE3007A1P'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR CHQA20140912257Wire Harness · faultyDURING INSPECTION THE MAIN ENTRY DOOR EMER LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED THE MAIN DOOR HARNESS W737. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Sep 12, 2014 · N573RP · Emb EMB145LR · Light System WiringSDR CHQA20140909248Switch · inoperativeDURING INSPECTION THE FLIGHT ATTENDANT EMER LIGHT SWITCH WAS FOUND TO BE INOPERATIVE. REPLACED THE FLIGHT ATTENDANT CONTROL PANEL. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Sep 9, 2014 · N290SK · Emb EMB145LR · Emergency LightingSDR SIMA20140908004Warning System · false activationLEFT ENG PPH WENT TO 0 & TURNED RED & BLINKED AT APPROX 120 IAS. ABORTED TAKEOFF WT APPROX 41K LBS. HAD CREW PERFORM HI POWER RUN. ALL INDICATIONS NORMAL IAW RR MM 72-00-00.Sep 8, 2014 · N653AE · Emb EMB145LR · Fuel Flow IndicatingSDR CHQA20140903247Light · inoperativeDURING INSPECTION THE LT OVERWING EXTERIOR EMER LIGHT WAS FOUND TO BE INOPERATIVE. RE-LAMPED THE LT OVERWING EMER LIGHT. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Sep 3, 2014 · N258JQ · Emb EMB145LR · Emergency LightingSDR CHQA20140829253Floor Support · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE CTR OMEGA BEAM AT FRAME 20. THE OMEGA BEAM WAS REPLACED IAW SRM 51-40-02.Aug 29, 2014 · N266SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20140829255Floor Support · corrodedDURING INSPECTION THE RT OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAME 59 & 60. THE BEAM WAS REPLACED IAW ETD 2014-145-073053.Aug 29, 2014 · N266SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20140828252Skin · chafedDURING INSPECTION THE CARGO DOOR INNER SKIN WAS FOUND TO HAVE CHAFE MARKS ON THE LOWER AFT END. THE SKIN WAS REPLACED IAW SRM 51-40-02.Aug 28, 2014 · N266SK · Emb EMB145LR · Cargo/Baggage DoorsSDR CHQA20140827254Firewall · crackedDURING INSPECTION THE APU FIREWALL WAS FOUND TO BE CRACKED UNDER THE UPPER LT SUPPORT ROD. THE APU FIREWALL WAS REPAIRED IAW SRM 53-32-13.Aug 27, 2014 · N266SK · Emb EMB145LR · Fuselage Main, BulkheadSDR CHQA20140826249Seat Track · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE LT OMEGA BEAM SEAT TRACK FROM FRAME 25 THROUGH FRAME 30. THE SEAT TRACK WAS REPLACED IAW AMM 53-01-06.Aug 26, 2014 · N266SK · Emb EMB145LR · Fuselage, Seat/Cargo Attach FittingsSDR CHQA20140826250Seat Track · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE CTR OMEGA BEAM SEAT TRACK FROM FRAME 25 - 30. THE SEAT TRACK WAS REPLACED IAW AMM 53-01-06.Aug 26, 2014 · N266SK · Emb EMB145LR · Fuselage, Seat/Cargo Attach FittingsSDR CHQA20140826256Doubler · corrodedDURING INSPECTION THE LT OMEGA BEAM REPAIR DOUBLER ON THE INBD SIDE WAS FOUND TO BE CORRODED AT FRAME 20. THE REPAIR DOUBLER WAS REPLACED IAW SRM 53-00-10.Aug 26, 2014 · N266SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20140825251Profile · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE LOWER PROFILE ON THE CARGO DOOR. THE PROFILE WAS REPLACED IAW SRM 51-40-02.Aug 25, 2014 · N266SK · Emb EMB145LR · Cargo/Baggage DoorsSDR CHQA20140818242Light · inoperativeDURING INSPECTION THE EMER FLOOR PROXIMITY STRIP WAS FOUND TO BE INOPERATIVE AT ROW 8. R & R THE LIGHT STRIP & ALL OPERATIONAL CHECKS WERE GOOD.Aug 18, 2014 · N567RP · Emb EMB145LR · Emergency LightingSDR CHQA20140815245Floor Support · corrodedDURING INSPECTION THE CTR OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. THE CTR OMEGA BEAM FROM FRAMES 16 TO 23 WAS REPLACED IAW SRM 51-40-02.Aug 15, 2014 · N258JQ · Emb EMB145LR · Fuselage Miscellaneous StructureSDR ASOA20140814107Engine · odorTHE CREW REPORTED A MUSTY ODOR WHEN EITHER BLEED ENGINE NR 1 OR NR 2 SELECTED BUT GOES AWAY WHEN APU IS SELECTED. MAINTENANCE R & R THE NR 1 ENGINE, OPS TESTED WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Aug 14, 2014 · N12922 · Emb EMB145LR · Engine (Turbine/Turboprop)SDR CHQA20140811246Skin · crackedDURING INSPECTION THE SKIN WAS FOUND TO BE CRACKED BELOW STRINGER 2L AT FRAME 75. THE SKIN WAS REPAIRED IAW ETD 2014-145-067832.Aug 11, 2014 · N258JQ · Emb EMB145LR · Fuselage Main, Plate/SkinSDR CHQA20140810243Floor Support · crackedDURING INSPECTION THE RT SIDE OMEGA BEAM SUPPORT AT FRAME 47 & 48 WAS FOUND TO BE CRACKED. THE RT OMEGA BEAM SUPPORT WAS REPLACED IAW SRM 51-40-02.Aug 10, 2014 · N258JQ · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20140810244Floor Support · corrodedDURING INSPECTION THE CTR OMEGA BEAM INBD FLANGE WAS FOUND TO BE CORRODED FRAME 23 - 24. THE OMEGA BEAM FLANGE WAS REPAIRED IAW SRM 53-00-10.Aug 10, 2014 · N258JQ · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20140808239Light · disconnectedDURING INSPECTION THE EMER FLOOR PROXIMITY STRIP WAS FOUND TO BE INOPERATIVE AT ROW 6. THE EMER LIGHT FLOOR STRIP WAS DEFERRED. THE DEFERRAL WAS CLEARED IN 8/8/14 WHEN MAINTENANCE RECONNECTED THE EMER LIGHT STRIP. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHERAug 8, 2014 · N265SK · Emb EMB145 · Emergency LightingSDR CHQA20140803238Unknown · smokeDURING DESCENT THERE WAS SMOKE IN THE COCKPIT. THE SMOKE DISSIPATED ON ITS OWN BEFORE LANDING. THE ACFT LANDED WITHOUT FURTHER INCIDENT AT ITS INTENDED DESTINATION. MAINTENANCE DEFERRED THE COOLING PACK 1 SYS. THE DEFERRAL WAS CLEARED ON 8/4/2014 WHEN OPERAug 3, 2014 · N370SK · Emb EMB145LR · Air Distribution SystemSDR ASOA20140802063Carbon Seal · wornPILOT REPORTED STRONG OIL ODOR IN COCKPIT AND CABIN DURING FLIGHT BECAME WORSE DURING APPROACH AND LANDING. ACFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED ACFT AND FERRIED ON 8/03/2014. MAINTENANCE R & R LT ENGINE "0" BEARING CARBON SEAL ASSEMBLY. PERFAug 2, 2014 · N11547 · Emb EMB145LR · Engine (Turbine/Turboprop)SDR CHQA20140728237Electronic Unit · faultyAFTER TAKEOFF WHEN THE LG WAS SELECTED UP, THEY RECEIVED A LANDING LEVER DISAGREE MSG & THE LT MLG DID NOT SHOW UP & LOCKED. DECLARED AN EMER & DIVERTED THE ACFT. WHEN THE LG WAS LOWERED THE LT MLG SHOWED DOWN & LOCKED. THE ACFT LANDED WITHOUT FURTHER INCIDJul 28, 2014 · N565RP · Emb EMB145LR · Landing Gear Retraction/Extension SystemSDR CHQA20140726236Battery · dischargedDURING INSPECTION THE EMER LIGHTS AFT OF ROW 12 WERE FOUND TO BE INOPERATIVE. REPLACED THE NR 3 EMER LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Jul 26, 2014 · N283SK · Emb EMB145LR · Emergency LightingSDR CHQA20140722235Tire · separatedTHE LT INBD TIRE SEPARATED ON TAKEOFF. DECLARED AN EMER & DIVERTED THE ACFT FROM ITS INTENDED FLIGHT PLAN. THE ACFT LANDED WITHOUT FURTHER INCIDENT. PERFORMED THE TREAD SEPARATION INSPECTION & CONFIRMED THE LT INBD TO BE AT FAULT. THE LT INBD TIRE, THE LT Jul 22, 2014 · N274SK · Emb EMB145LR · TireSDR CHQA20140714234Transducer · unsecureCREW REPORTED THAT UPON LANDING THAT THEY EXPERIENCED REDUCED BRAKING ACTION & THAT THE BRAKES SEEMED TO BE GRABBING. MX SECURED THE NR 4 WHEEL SPEED TRANSDUCER. NO FURTHER DEFECTS WERE NOTED.Jul 14, 2014 · N574RP · Emb EMB145LR · Landing Gear Brake SystemSDR CHQA20140712223Electronic Unit · failedTHE CREW REPORTED THAT AFTER TAKEOFF THAT THE LG WOULD NOT RETRACT & THEY HAD A LG AIR & GND FAIL MSG. THE CREW ALSO REPORTED THAT THEY RECEIVED A SPOILER FAIL MSG, AN ENG 1 & 2 IDLE STOP FAIL MSG, GUST LOCK INOPERATIVE MESSAGE & THE THRUST REVERSER WAS NOT AJul 12, 2014 · N574RP · Emb EMB145LR · Landing Gear Position and WarningSDR CHQA20140711209Windshield · crackedTHE CREW REPORTED THAT ON CLIMB OUT, THE FIRST OFFICER`S WINDSHIELD CRACKED. THE ACFT WAS RETURNED TO FIELD & LANDED WITHOUT FURTHER INCIDENT. THE RT WINDSHIELD WAS REPLACED. NO FURTHER DISCREPANCIES WERE REPORTED.Jul 11, 2014 · N574RP · Emb EMB145LR · Flight Compartment WindowsSDR CHQA20140711210Light · inoperativeDURING INSPECTION, THE RT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MX RELAMPED THE EMERGENCY LIGHT. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Jul 11, 2014 · N268SK · Emb EMB145LR · Emergency LightingSDR SIMA20140710003Sensor · failedWHEN THRUST WAS ADVANCED ON TAKEOFF ROLL THE NR 2 ENG HP VIB INDICATOR PEGGED HIGH. NO MASTER CAUTION EVER OCCURRED. THE INDICATOR REMAINED PEGGED EVEN WHEN THRUST WAS REDUCED TO IDLE. TAKEOFF ABORT WAS LOW SPEED WITH VERY MINIMAL BREAKING. NO UNUSUAL SOUNDJul 10, 2014 · N663AR · Emb EMB145LR · Engine Vibration AnalyzerSDR CHQA20140708232Door Frame · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE PAX DOOR LOWER FRAME. THE DOOR FRAME SECTION WAS REPLACED IAW SRM 51-40-02.Jul 8, 2014 · N571RP · Emb EMB145LR · Passenger/Crew DoorsSDR CHQA20140705206Switch · faultyCREW REPORTED THAT DURING FLIGHT THEY RECEIVED A BLEED 1 VLV FAIL MSG. THE ACFT WAS DIVERTED & LANDED WITHOUT FURTHER INCIDENT. MX REPLACED THE BLEED SYS 1 PUSH BUTTON SWITCH. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Jul 5, 2014 · N272SK · Emb EMB145LR · Pneumatic Distribution SystemSDR CHQA20140705207Pump · leakingCREW REPORTED THAT THEY RECEIVED A HYD 1 LOW QTY MSG FOLLOWED BY A HYD SYS 1 FAIL MSG. THE CREW PERFORMED A MANUAL EXTENSION ON THE LG. THE ACFT LANDED WITHOUT FURTHER INCIDENT. MX REPLACED THE HYD SYS 1 ENG DRIVEN PUMP & PERFORMED THE LG FREE FALL CHECK. Jul 5, 2014 · N276SK · Emb EMB145LR · Hydraulic Pump (Electric/Engine), MainSDR CHQA20140704205Tat Probe · faultyCREW REPORTED THAT THEY RECEIVED A TAT 1 HEAT INOPERATIVE MSG IN FLIGHT. THE CREW RETURNED THE ACFT TO FIELD & LANDED WITHOUT FURTHER INCIDENT. MX REPLACED THE TAT 1 PROBE. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Jul 4, 2014 · N293SK · Emb EMB145LR · Outside Air Temperature Indicator/SensorSDR CHQA20140702227Floor Support · corrodedDURING INSPECTION, THE RT OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAME 59 & 60. THE OMEGA BEAM WAS REPAIRED IAW ETD2014-145-055968.Jul 2, 2014 · N571RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20140701203Light · burned outCREW REPORTED THAT THE BALLAST LIGHT BULB ABOVE ROW 6A BURNT OUT DURING FLIGHT & CAUSED A MINOR HAZE IN THE CABIN. THE ACFT LANDED AT ITS INTENDED DESTINATION WITHOUT FURTHER INCIDENT. MX DEFERRED THE LIGHT SOCKET. THE DEFERRAL WAS CLEARED ON 7/2/14 WHEN MXJul 1, 2014 · N274SK · Emb EMB145LR · Passenger Compartment LightingSDR CHQA20140701204Lamp Socket · defectiveCREW REPORTED THAT THE BALLAST LIGHT BULB ABOVE ROW 6A BURNT OUT DURING FLIGHT & CAUSED A MINOR HAZE IN THE CABIN. THE ACFT LANDED AT ITS INTENDED DESTINATION WITHOUT FURTHER INCIDENT. MX DEFERRED THE LIGHT SOCKET. THE DEFERRAL WAS CLEARED ON 7/2/14 WHEN MXJul 1, 2014 · N274SK · Emb EMB145LR · Passenger Compartment LightingSDR CHQA20140701211Floor Support · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CTR OMEGA BEAM Y=0.0 & FRAME 59. THE BEAM WAS REPAIRED IAW ETD 2014-145-055505.Jul 1, 2014 · N575RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20140701221Floor Support · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CTR OMEGA BEAM Y=0.0 BETWEEN FRAME 19 & 23. THE CTR OMEGA BEAM WAS REPLACED IAW SRM 51-40-02.Jul 1, 2014 · N575RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20140629212Repair · dentedDURING INSPECTION, A PREVIOUS REPAIR ON THE CARGO DOOR WAS FOUND TO BE DENTED AT THE LOWER AFT EDGE. THE DENT WAS REPAIRED IAW ETD 2014-145-055666.Jun 29, 2014 · N575RP · Emb EMB145LR · Cargo/Baggage DoorsSDR CHQA20140629214Fitting · crackedDURING INSPECTION, THE AFT FUSELAGE INSIDE ACCESS 312AR CLIP ON THE APU FIREWALL AT STRINGER 10L & FRAME 80 WAS FOUND TO BE CRACKED. THE APU FIREWALL CLIP AT FRAME 80 & STRINGER 10L WAS REPLACED IAW SRM 51-40-02.Jun 29, 2014 · N575RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20140629215Angle · crackedDURING INSPECTION, AFT FUSELAGE INSIDE ACCESS PANEL 312AR ANGLE ON THE APU FIREWALL AT STRINGER 10R & FRAME 80 WAS FOUND TO BE CRACKED. THE APU FIREWALL ANGLE WAS REPLACED IAW SRM 51-40-02.Jun 29, 2014 · N575RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20140629222Fitting · crackedDURING INSPECTION, THE AFT FUSELAGE INSIDE ACCESS 312AR FRAME 80 SHEAR CLIP WAS FOUND CRACKED AT STRINGER 1L. THE SHEAR CLIP WAS REPLACED IAW WITH SRM 51-40-02.Jun 29, 2014 · N575RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20140628217Fitting · crackedDURING INSPECTION, THE SHEAR CLIP AT FRAME 24 & STRINGER 15R WAS FOUND CRACKED. THE SHEAR CLIP WAS REPLACED IAW SRM 51-40-02.Jun 28, 2014 · N575RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20140628219Fitting · crackedDURING INSPECTION, THE SHEAR CLIP AT FRAME 24 & 16R WAS FOUND TO CRACKED. THE SHEAR CLIP WAS REPLACED IAW ACCORDANCE WITH SRM 51-40-02.Jun 28, 2014 · N575RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20140628220Rib · groovedDURING INSPECTION, A GROOVE WAS FOUND ON THE RT ELEVATOR NOSE RIB AT ELEVATOR STATION YH-1280.00 & HORIZONTAL & STAB YH=1310.00. THE RIB WAS REPLACED IAW SRM 51-40-02.Jun 28, 2014 · N575RP · Emb EMB145LR · Elevator, Spar/RibSDR CHQA20140627213Fitting · crackedDURING INSPECTION, THE SHEAR CLIP AT FRAME 26 AND STRINGER 16R WAS FOUND TO BE CRACKED. THE SHEAR CLIP WAS REPLACED IAW SRM 51-40-02.Jun 27, 2014 · N575RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20140627214Skin · dentedDURING HEAVY MX, A DENT BELOW & AFT OF ENG 2 ON THE FUSELAGE SKIN WAS REPAIRED IAW ETD 2014-145-054213.Jun 27, 2014 · N575RP · Emb EMB145LR · Fuselage Main, Plate/SkinSDR CHQA20140627218Fitting · crackedDURING INSPECTION, THE SHEAR CLIP AT FRAME 25 & STRINGER 16R WAS FOUND TO BE CRACKED. THE SHEAR CLIP WAS REPLACED IAW SRM 51-40-02.Jun 27, 2014 · N575RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20140627226Floor Support · corrodedDURING INSPECTION, THE CTR OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED. THE CTR OMEGA BEAM AT FRAME 20 WAS REPLACED IAW SRM 51-40-02.Jun 27, 2014 · N571RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20140625225Door Sill · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LT AISLE SILL AT FRAME 20. THE CORROSION WAS REMOVED IAW SRM 53-21-10.Jun 25, 2014 · N571RP · Emb EMB145LR · Fuselage Miscellaneous Structure
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