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 CHQA20141102311Access Door · openA HUMMING NOISE FROM THE LOWER LT NOSE AREA DURING CLIMB. THE CREW ELECTED TO RETURN TO FIELD & LANDED WITHOUT FURTHER INCIDENT. FOUND THE GPU ACCESS PANEL TO BE OPEN. THE DOOR WAS CLOSED & NO FURTHER DEFECTS WERE NOTED.Nov 2, 2014 · N258JQ · Emb EMB145LR · Service DoorsSDR CHQA20141029318Floor Support · corrodedDURING INSPECTION THE LT OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED. THE OMEGA BEAM WAS REPAIRED IAW SRM 51-40-02.Oct 29, 2014 · N286SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20141028314Floorbeam · corrodedDURING INSPECTION THE CTR FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 20. THE CTR FLOORBEAM WAS REPLACED IAW SRM 51-40-02.Oct 28, 2014 · N286SK · Emb EMB145LR · Fuselage Main, Floor BeamSDR CHQA20141028315Floor Support · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE RT RAMP FLOOR SUPPORT AT FRAME 19 THROUGH FRAME 20. THE CTR RAM FLOOR SUPPORT WAS REPLACED IAW SRM 51-40-02.Oct 28, 2014 · N286SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20141028322Fitting · crackedDURING INSPECTION THE SHEAR CLIP AT FRAME 62 & STRINGERS 6R & 8R WAS FOUND TO BE CRACKED. THE SHEAR CLIP WAS REPLACED IAW SRM 53-31-04.Oct 28, 2014 · N271SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20141028325Floor Support · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE CTR OMEGA BEAM AT FRAME 20 UNDER THE RAMP ANGLE. THE CTR OMEGA BEAM WAS REPAIRED IAW SRM 51-40-02.Oct 28, 2014 · N271SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20141027310Light · inoperativeDURING INSPECTION THE EMER FLOOR PROXIMITY LIGHT STRIP AT ROW 9A WAS FOUND TO BE INOPERATIVE. THE LIGHT WAS DEFERRED. THE DEFERRAL WAS CLEARED ON 10/28/2014 WHEN MX REPLACED THE NR 4 EMER LIGHT PROXIMITY STRIP.Oct 27, 2014 · N579RP · Emb EMB145LR · Emergency LightingSDR CHQA20141027313Fitting · crackedDURING INSPECTION THE SHEAR CLIP AT THE APU FIREWALL & STRINGER 11R WAS FOUND TO BE CRACKED. THE SHEAR CLIP WAS REPLACED IAW SRM 51-40-02.Oct 27, 2014 · N286SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20141027316Doubler · corrodedDURING INSPECTION THE RT FLOORBEAM REPAIR DOUBLER AT FRAME 23 WAS FOUND TO BE CORRODED. THE REPAIR DOUBLER WAS REPLACED IAW SRM 53-21-10.Oct 27, 2014 · N286SK · Emb EMB145LR · Fuselage Main, Floor BeamSDR CHQA20141027317Gusset · corrodedDURING INSPECTION THE CTR FLOORBEAM GUSSET FROM FRAME 20 TO FRAME 23 WAS FOUND TO BE CORRODED. THE CTR FLOORBEAM GUSSET WAS REPLACED IAW SRM 51-40-02.Oct 27, 2014 · N286SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20141027319Fitting · crackedDURING INSPECTION THE SHEAR CLIP AT THE APU FIREWALL & STRINGER 10R WAS FOUND TO BE CRACKED. THE SHEAR CLIP WAS REPLACED IAW SRM 51-40-02.Oct 27, 2014 · N286SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20141027323Doubler · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE LT OMEGA BEAM PREVIOUS REPAIR AT THE CARBON CROSS MEMBER. THE REPAIR DOUBLER WAS REPLACED IAW SRM 53-00-10 & 51-40-02.Oct 27, 2014 · N271SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20141027324Support · crackedDURING INSPECTION THE LT WING BOX ANGLE SUPPORT WAS FOUND TO BE CRACKED BETWEEN FRAME 44 & 45. THE SUPPORT WAS REPLACED IAW SRM 51-40-02.Oct 27, 2014 · N271SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20141027326Floor Support · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE CTR OMEGA BEAM SUPPORT FROM FRAME 44 TO 50. THE SUPPORT WAS REPLACED IAW SRM 51-40-02.Oct 27, 2014 · N271SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20141027327Fitting · crackedDURING INSPECTION THE SHEAR CLIP AT FRAME 80 & STRINGER 8L WAS FOUND TO BE CRACKED. THE SHEAR CLIP WAS REPLACED IAW SRM 51-40-02.Oct 27, 2014 · N271SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR ASOA20141027113Blade · separatedENGINE NR 1 FAILED AT 2200 MSL. R & R NR 1 ENGINE, OPS CHECKED GOOD, ACFT RELEASED AND RETURNED TO SERVICE. NO N2 ROTATION. 6TH STAGE COMPRESSOR BLADE HAD LIBERATED.Oct 24, 2014 · N16571 · Emb EMB145LR · Turbine Engine Compressor SectionSDR CHQA20141022300Ballast · defectiveELECTRICAL BURNING ODOR WAS PRESENT IN THE CABIN IN FLIGHT. THE LIGHTING BALLAST AT SEAT 1A WAS FOUND TO BE CAUSING THE ODOR & WAS DEFERRED. THE DEFERRAL WAS CLEARED ON 10/26/2014 WHEN MX REPLACED THE LIGHTING BALLAST. OPERATIONAL CHECKS WERE GOOD WITH NO FOct 22, 2014 · N568RP · Emb EMB145LR · Passenger Compartment LightingSDR CHQA20141022301Connector · dirtyDURING INSPECTION THE EMER LIGHTS AFT OF ROW 12 WERE FOUND TO BE INOPERATIVE. CLEANED THE CONNECTIONS TO EMER LIGHT BATTERIES 3 & 4. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Oct 22, 2014 · N573RP · Emb EMB145LR · Light System WiringSDR CHQA20141022302Connector · dirtyDURING INSPECTION THE EMER LIGHTS AFT OF ROW 12 WERE FOUND TO BE INOPERATIVE. CLEANED THE CONNECTIONS TO EMER LIGHT BATTERIES 3 & 4. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Oct 22, 2014 · N573RP · Emb EMB145LR · Light System WiringSDR CHQA20141020299Isis · faultyRECEIVED A STANDBY ATTITUDE INDICATION FAILURE IN FLIGHT. DIVERTED THE ACFT & LANDED WITHOUT INCIDENT. REPLACED THE ISIS. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Oct 20, 2014 · N258JQ · Emb EMB145LR · Integrated Flight SystemSDR CHQA20141018297Battery · dischargedDURING INSPECTION THE NR 2 EMER LIGHT BATTERY WAS FOUND TO BE INOPERATIVE. THE BATTERY WAS REPLACED. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Oct 18, 2014 · N578RP · Emb EMB145LR · Emergency LightingSDR CHQA20141018298Transducer · faultyON CLIMB THE NR 1 ENG OIL TEMP WAS READING HIGH. RETURNED TO FIELD & LANDED WITHOUT INCIDENT. REPLACED THE ENG 1 OIL PRESS & TEMP TRANSDUCER. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Oct 18, 2014 · N565RP · Emb EMB145LR · Engine Oil TemperatureSDR ASOA20141017085Bleed Valve · faultyTHE CREW REPORTED AFTER STARTING APU, RECEIVED A STRONG FUEL ODOR IN COCKPIT, WHICH DISSIPATED. MAINTENANCE INSPECTED AND REPLACED THE APU BLEED VALVE. OPS CHECKED GOOD.Oct 17, 2014 · N48901 · Emb EMB145LR · Compressor Bleed ValveSDR CHQA20141017306Door Sill · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE LT FLOOR SILL BETWEEN FRAMES 19 & 20. THE SILL WAS REPLACED IAW SRM 51-40-02.Oct 17, 2014 · N281SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20141015307Skin · crackedDURING INSPECTION THE FUSELAGE SKIN WAS FOUND TO BE CRACKED AT FRAME 79 & STRINGERS 5L & 6L. THE SKIN WAS REPAIRED IAW ETD 2014-145-086559.Oct 15, 2014 · N281SK · Emb EMB145LR · Fuselage Main, Plate/SkinSDR CHQA20141013296Inverter · malfunctionedDURING INSPECTION THE LT EMER EXIT AFT IDENTIFIER SIGN WAS FOUND TO BE INOPERATIVE. RESET THE LT OVERWING INVERTER AT ROW 12A. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Oct 13, 2014 · N293SK · Emb EMB145LR · Emergency LightingSDR CHQA20141013304Floor Support · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE CTR OMEGA BEAM AT FRAME 20. THE CTR OMEGA BEAM WAS REPAIRED IAW SRM 51-40-02.Oct 13, 2014 · N281SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20141013308Skin · crackedDURING INSPECTION THE FUSELAGE SKIN WAS FOUND TO BE CRACKED AT FRAME 75 & STRINGER 2R. THE SKIN WAS REPAIRED IAW ETD 2014-145-086559.Oct 13, 2014 · N281SK · Emb EMB145LR · Fuselage Main, Plate/SkinSDR CHQA20141012303Floor Support · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE INBD SIDE OF THE LT OMEGA BEAM AT FRAME 20. THE BEAM WAS REPLACED IAW SRM 51-40-02.Oct 12, 2014 · N281SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20141012309Floor Support · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE LT OMEGA BEAM AT FRAME 59. THE BEAM WAS REPAIRED IAW ETD 2014-145-087054.Oct 12, 2014 · N281SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20141010305Fitting · crackedDURING INSPECTION THE SHEAR CLIP AT FRAME 80 & STRINGER 5L WAS FOUND TO BE CRACKED. THE SHEAR CLIP WAS REPLACED IAW SRM 51-40-02.Oct 10, 2014 · N281SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20140928282Light · inoperativeDURING INSPECTION AN AFT FLOOR PROXIMITY EMER LIGHT STRIP WAS FOUND TO BE INOPERATIVE. REPLACED THE FLOOR PROXIMITY EMER LIGHT STRIP. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Sep 28, 2014 · N577RP · Emb EMB145LR · Emergency LightingSDR CHQA20140927281Wire Harness · damagedTHE CREW REPORTED THAT THERE WAS AN ELEC SMELL IN THE FWD CABIN. REPLACED THE CEILING LIGHT HARNESS ASSEMBLY AT ROW 8. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Sep 27, 2014 · N273SK · Emb EMB145LR · Light System WiringSDR CHQA20140925283Angle · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE RAMP ANGLE AT FRAME 20. THE RAM ANGLE WAS REPLACED IAW SRM 51-40-02.Sep 27, 2014 · N272SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20140927286Fitting · crackedDURING INSPECTION THE AFT FUSELAGE END CLIP AT THE APU FIREWALL INSIDE ACCESS AT FRAME 81 & STRINGER 9R WAS FOUND TO BE CRACKED. THE END CLIP WAS REPLACED IAW SRM 51-40-02.Sep 27, 2014 · N567RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20140927287Fitting · crackedDURING INSPECTION THE AFT FUSELAGE END CLIP AT THE APU FIREWALL INSIDE ACCESS AT FRAME 81& STRINGER 8R WAS FOUND TO BE CRACKED. THE END CLIP WAS REPLACED IAW SRM 51-40-02.Sep 27, 2014 · N567RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20140925284Profile · corrodedDURING INSPECTION THE PROFILE FWD OF THE RAMP ANGLE AT FRAME 20 WAS FOUND TO BE CORRODED. THE PROFILE WAS REPAIRED IAW SRM 53-21-10.Sep 25, 2014 · N272SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20140925285Support · corrodedDURING INSPECTION THE RT RAMP SUPPORT WAS FOUND TO BE CORRODED. THE RT RAMP ANGLE WAS REPLACED IAW SRM 51-40-02 & ETD 2014-145-08-1412.Sep 25, 2014 · N272SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20140920277Floor Support · corrodedDURING INSPECTION THE CTR OMEGA BEAM WAS FOUND TO BE CORRODED FROM FRAME 19 - 23. THE OMEGA BEAM WAS REPLACED IAW SRM 51-40-02.Sep 20, 2014 · N566RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20140920279Skin · crackedDURING INSPECTION A HIGH FREQUENCY EDDY CURRENT INSPECTION FOUND THE SKIN TO CRACKED AT 1 FASTENER ABOVE STRINGER 6R & 1 BELOW STRINGER 6R AT FRAME 79. THE SKIN WAS REPAIRED IAW ETD 2014-145-079864.Sep 20, 2014 · N566RP · Emb EMB145LR · Fuselage Main, Plate/SkinSDR CHQA20140919274Discharge Tube · crackedCREW REPORTED THAT DURING FLIGHT THE ENG 2 ITT WAS SHOWING HIGH. RETURNED TO FIELD & LANDED WITHOUT INCIDENT. REPLACED THE COMPRESSOR AIR DISCHARGE TUBE ON THE ENG 2 RT SIDE. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Sep 19, 2014 · N573RP · Emb EMB145LR · Engine Cooling SystemSDR CHQA20140912275Skin · gougedDURING INSPECTION THE RT FUSELAGE SKIN WAS FOUND TO BE GOUGED AT THE INSIDE PYLON ACCESS PANEL 424DB AT FRAME 67 & STRINGER 9R. THE SKIN WAS REPAIRED IAW ETD2014-145-079860.Sep 19, 2014 · N566RP · Emb EMB145LR · Fuselage Main, Plate/SkinSDR CHQA20140919276Skin · damagedDURING HEAVY MX A LIGHTNING STRIKE REPAIR WAS COMPLETED ON THE SKIN AT FRAME 17 & STRINGER 17R IAW ETD2014-145-015228A.Sep 19, 2014 · N566RP · Emb EMB145LR · Fuselage Main, Plate/SkinSDR CHQA20140919278Skin · damagedDURING HEAVY MX A LIGHTNING STRIKE REPAIR WAS COMPLETED ON THE SKIN AT FRAME 25 & STRINGER 15R IAW ETD2014-145-015228A.Sep 19, 2014 · N566RP · Emb EMB145LR · Fuselage Main, Plate/SkinSDR CHQA20140919280Skin · damagedDURING HEAVY MX A LIGHTNING STRIKE REPAIR WAS COMPLETED ON THE SKIN AT FRAME 24 & STRINGER 15R IAW ETD2014-145-015228A.Sep 19, 2014 · N566RP · Emb EMB145LR · Fuselage Main, Plate/SkinSDR CHQA20140916259Ahrs · faultyTHE ACFT WAS TO BE FERRIED FOR MAINTENANCE DUE TO AN AHRS 1 INOPERATIVE MSG. BEFORE THE FLIGHT THE AHRS 1 WAS SWAPPED WITH THE AHRS 2. DURING THE FERRY FLIGHT THE CREW REPORTED THAT AFTER TAKEOFF THEY RECEIVED AN AHRS 1/2 INOPERATIVE MSG. RETURNED TO FIELD Sep 16, 2014 · N298SK · Emb EMB145LR · Integrated Flight SystemSDR CHQA20140914259Light · inoperativeDURING INSPECTION THE FLOOR PROXIMITY EMER LIGHT STRIP AT ROW 5A WAS FOUND TO BE INOPERATIVE. REPLACED THE LIGHT STRIP. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Sep 14, 2014 · N273SK · Emb EMB145LR · Emergency LightingSDR CHQA20140914258Battery · dischargedDURING INSPECTION THE AFT EMER EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED THE NR 4 EMER LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Sep 14, 2014 · N273SK · Emb EMB145LR · Emergency LightingSDR CHQA20140914272Gusset · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LT OMEGA GUSSET AT FRAME 16 TO 19. THE GUSSET WAS REPAIRED IAW ETD2014-145-077627A.Sep 14, 2014 · N564RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20140914273Skin · gougedDURING HEAVY MX A PERMANENT REPAIR OF THE BAGGAGE DOOR SKIN NEAR THE FWD VENT FLAP WAS REPAIRED IAW ETD2013-145-040730.Sep 14, 2014 · N564RP · Emb EMB145LR · Cargo/Baggage Doors
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