Allison AE-3007A1/3
Service difficulty reports · 228
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 = 'AE3007A13' 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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR CHQA20140820268Skin · damagedDURING INSPECTION A LIGHTNING STRIKE REPAIR WAS COMPLETED ON NR 1 FRAME 27 - 28 AT STRINGER 21L & FRAME 28 AT STRINGER 18L - 19L. THE REPAIR WAS MADE IAW SRM 53-22-01.SDR CHQA20140820270Skin · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE SKIN AT FRAME 25 & STRINGERS 20 - 21L. THE SKIN WAS REPAIRED IAW SRM 53-22-01.SDR CHQA20140807241Threshold · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE LOWER CARGO DOOR SILL. THE DOOR SILL THRESHOLD WAS REPLACED IAW SRM 51-40-02.SDR CHQA201408042340Door Frame · corrodedDURING INSPECTION THE PAX DOOR LOWER FRAME WAS FOUND TO BE CORRODED. THE PAX DOOR FRAME WAS REPAIRED IAW ETD-2014-145-061530.SDR SIMA20140730010Engine · failedIAW ITEM NR 1 ON LOG PAGE 3529025 OIL FOUND NR 2 ENG DURING BORESCOPE INSPECTION. R & R NR 2 ENG IAW WC 71-000-00. OPERATIONS CHECKED GOOD & LEAK CHECKED GOOD.SDR CHQA20140712224Sensor · inoperativeTHE CREW REPORTED THAT THEY RECEIVED A BLD 2 OVERTEMP MSG IN FLIGHT WHEN ENTERING ICING CONDITIONS. AFTER FOLLOWING THE GRH BY CLOSING THE BLD 2 SYS & OPENING THE CROSSBLEED VLV, THE CREW REPORTED THAT A BLEED 1 LOW TEMPERATURE MSG APPEARED. THE CREW DIVERTESDR CHQA20140708208Air Filter · dirtyTHE CREW REPORTED THAT DURING CLIMB THEY RECEIVED A BLEED 2 OVERTEMP MSG IN ICING CONDITIONS. THE ACFT WAS DIVERTED & LANDED WITHOUT FURTHER INCIDENT. MX CLEANED DEBRIS FROM THE ENG 2 FAN AIR VLV FILTER. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS SDR CHQA20140624193Battery · dischargedDURING INSPECTION, THE EMER DOOR LIGHTS & A FLOOR STRIP WERE FOUND TO BE INOPERATIVE. MX REPLACED THE NR 3 EMER LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA20140622191Battery · 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.SDR CHQA20140604185Electronic Unit · faultyCREW REPORTED THAT THEY RECEIVED A LG AIR & GND FAIL MSG AFTER TAKEOFF & THAT THE LG WOULD NOT RETRACT. THE CREW RETURNED TO FIELD & LANDED WITHOUT INCIDENT. THE ACFT WAS FERRIED FOR FURTHER MX. MX REPLACED THE LG ELECTRONICS UNIT & THE NLG WEIGHT ON WHEELSSDR CHQA20140604186Proximity Switch · faultyCREW REPORTED THAT THEY RECEIVED A LG AIR & GND FAIL MSG AFTER TAKEOFF & THAT THE LG WOULD NOT RETRACT. THE CREW RETURNED TO FIELD & LANDED WITHOUT INCIDENT. THE ACFT WAS FERRIED FOR FURTHER MX. MX REPLACED THE LG ELECTRONICS UNIT & THE NLG WEIGHT ON WHEELSSDR CHQA20140602181Fuel Filter · cloggedCREW REPORTED THAT THEY RECEIVED ENG 1 & 2 FUEL IMPENDING BYPASS MSG FLIGHT. THE CREW RETURNED TO FIELD & LANDED WITHOUT FURTHER INCIDENT. MX REPLACED THE ENG 1 & 2 FUEL FILTERS. ENG RUNS WERE GOOD & NO FURTHER DEFECTS WERE NOTED.SDR CHQA20140601179Control Unit · faultyCREW REPORTED THAT UPON LANDING THAT THE BRAKING SYS SEEMED TO BE UNRESPONSIVE. THE BRAKING SYS WORKED NORMALLY AT LOW SPEEDS & THE ACFT TAXIED TO THE GATE UNEVENTFULLY. MX REPLACED THE BRAKE CONTROL UNIT. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTSSDR CHQA20140516149Battery · dischargedDURING INSPECTION, THE OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED THE NR 4 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA20140513148O-Ring · leakingTHE CREW REPORTED THAT THEY RECEIVED A BLEED 2 LEAK MSG IN FLIGHT. THE CREW FOLLOWED THE QRH & THE MSG CLEARED. THE CREW DIVERTED & LANDED WITHOUT FURTHER INCIDENT. REPLACED THE O RINGS AT JOINTS 20 & 26. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTSSDR CHQA20140403102Fire Loop · faultyCREW REPORTED THAT AFTER TAKEOFF, THEY RECEIVED AN ENG 1 FIRE DETECTION FAIL MSG. THE CREW DIVERTED THE ACFT & LANDED WITHOUT FURTHER INCIDENT. REPLACED THE ENG 1 PYLON FIRE LOOP. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA20140331101Battery · dischargedDURING INSPECTION, THE OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED THE NR 4 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA20140221064Light · inoperativeDURING INSPECTION, RT AFT EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MX REPLACED THE RT AFT EMERGENCY LIGHT. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR SIMA20140219005Control Tube · faultyIN CLIMB E2 WENT TO 903 DEGREE EVEN WITH THRUST LEVER PULLED BACK AN INCH, THE LT WAS RUNNING ABOUT 100 DEGREE WARMER. TRANSFERRED TO NRWC 820-DFW-01586. R & R CABV CONTROL TUBE IAW RR MM 75-00-00, OPERATIONS CHECKED GOOD.SDR CHQA20140213054Light · inoperativeDURING INSPECTION, THE FLOOR PROXIMITY EMERGENCY LIGHT STRIP AT ROW 3 WAS FOUND TO BE INOPERATIVE. THE LIGHT IS CURRENTLY ON DEFERRAL. REPLACED THE EMERGENCY LIGHT FLOOR PROXIMITY STRIP AT ROW 3. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR SIMA20140212006Sump · cokedWHILE CLIMBING THROUGH FL 330 E1 ITT WAS NOTED TO BE FLUCTUATING BETWEEN 600 - 800. N2 WAS FLUCTUATING +- 5%. N1 DROPPED BELOW 45% NO ENG LIMITATIONS WERE SEEN IN EXCEDENCE. ACFT WAS REMOVED FROM SERVICE. COMPLIED WITH ALL TROUBLE SHOOTING PROCEDURES FOUNDSDR SIMA20140131007Unknown · smokeNUMBER 1 ENG, CONSTANT STREAM OF ACRID SMOKE EXITING EXHAUST & SOMETIMES INTAKE OF ENG FOR TWENTY MINUTES, AND COUNTING, AFTER SHUT DOWN. NOT BILLOWING BUT CLOSE TO IT. PERFORMED GVI OF ENG NR 1 INLET & EXHAUST, FOUND NO EVIDENCE OF OIL LEAKING IAW ITEM NR 2SDR CHQA20140130050Housing · corrodedDURING INSPECTION, THE NLG BRACE STRUT BEARING HOUSING WAS FOUND TO BE CORRODED. THE NLG BRACE STRUT BEARING HOUSING WAS REPAIRED IAW ETD 2014-145-008736A.SDR CHQA20140130051Housing · corrodedDURING INSPECTION, THE NLG BRACE STRUT BEARING HOUSING WAS FOUND TO BE CORRODED. THE NLG BRACE STRUT BEARING HOUSING WAS REPAIRED IAW ETD 2014-145-008736A.SDR CHQA20140128034Battery · dischargedDURING INSPECTION, THE EMERGENCY LIGHT ON THE MAIN ENTRY DOOR WAS FOUND TO BE INOPERATIVE. REPLACED THE NR 1 EMERGENCY LIGHT BATTERY. OPERATIONS CHECKED GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA20140128049Plate · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE BOTTOM FWD CARGO DOOR STRIKER PLATE AT FRAME 65. THE BOTTOM FWD CARGO DOOR STRIKER PLATE ON FRAME 65 WAS REPAIRED IAW SRM 53-31-04.SDR CHQA20140128052Fitting · crackedDURING INSPECTION, A CRACK WAS FOUND ON THE SHEAR CLIP AT FRAME 26 BETWEEN STRINGERS 15R & 16R. THE SHEAR CLIP WAS REPLACED IAW SRM 51-40-02.SDR CHQA20140126023Proximity Switch · damagedCREW REPORTED THAT DURING CRUISE FLIGHT, THEY RECEIVED A LG AIR GND FAIL MESSAGE. THE CREW REPORTED THAT THEY RECEIVED ASSOCIATED ENG 1 & 2 THRUST REVERSER DISAGREE MESSAGES. DIVERTED & LANDED WITHOUT INCIDENT. REPLACED THE NLG WEIGHT ON WHEELS PROXIMITY SWISDR CHQA20140126048Skin · gougedDURING INSPECTION, THE FWD FUSELAGE NOSE SKIN WAS FOUND TO BE GOUGED AT FRAME 8. THE SKIN WAS REPAIRED IAW SRM 53-11-01.SDR CHQA20140124019Control Unit · faultyCREW REPORTED THAT THEY RECEIVED A BRAKE DEGRADED MESSAGE ON THE EICAS DURING LANDING & REPORTED THE BRAKES AS INTERMITTENT. THE ACFT TAXIED TO THE GATE WITHOUT FURTHER INCIDENT. REPLACED THE BRAKE CONTROL UNIT, OPERATIONS CHECKED GOOD WITH NO FURTHER DEFECTSDR CHQA20140120018Control Unit · faultyCREW REPORTED THAT ON LANDING, THE ACFT PULLED SLIGHTLY TO THE RT & HAD DIFFICULTY STOPPING. THE CREW TAXIED TO THE GATE WITHOUT FURTHER INCIDENT. REPLACED THE BRAKE CONTROL UNIT, OPERATIONS CHECKED GOOD WITH NO FURTHER DEFECTS NOTED.SDR SIMA20140119003Engine · bird ingestionDECLARED EMERGENCY LEFT ACCT BIRD STRIKE FOLLOWED BY ENG 1 FAILURE. FLT LANDED WITHOUT FURTHER INCIDENT. AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED LEFT ENGINE IAW WC 71-000-00.SDR CHQA20140109005Proximity Switch · dirtyCREW REPORTED THAT THE ACFT HAD A SLIGHT UNINTENDED ROLL TO THE LT DURING DESCENT. THE CREW FURTHER REPORTED THAT THE SPOILERS SHOWED OPEN WITH THE HANDLE IN THE CLOSED POSITION. THE SITUATION WAS REMEDIED & THE ACFT LANDED WITHOUT FURTHER INCIDENT. PERFORMSDR SIMA20131222013Seal · damagedDURING MAINTENANCE INSPECTION ON FLIGHT 3503 FOUND OPS REPORTS E1 SMOKING AFTER SHUTDOWN. AIRCRAFT WAS REMOVED FROM SERVICE. REMOVE AND REPLACE REAR SHAFT PLUG SEAL IAW WORK CARD 72-200-03 AND R&R THE AGB BREATHER SEAL IAW RR MM 72-63-10. OPS CK GOOD.SDR CHQA20131122432Fitting · damagedLEFT AILERON PCA FITTING HOLES WERE FOUND TO BE ELONGATED. THE LT AILERON PCA FITTING WAS REPLACED IAW SRM 51-40-02.SDR CHQA20131121433Fitting · damagedRIGHT AILERON PCA FITTING HOLES WERE FOUND TO BE ELONGATED. THE RT AILERON PCA FITTING WAS REPLACED IAW SRM 51-40-02.SDR CHQA20131121434Fitting · damagedLEFT AILERON DAMPER LUG HOLES WERE FOUND TO BE ELONGATED. THE AILERON DAMPER FITTING WAS REPLACED IAW SRM 51-40-02.SDR CHQA20131118429Fitting · crackedCRACK WAS FOUND ON THE SHEAR CLIP AT FRAME 26 BETWEEN STRINGERS 15R & 16R. THE SHEAR CLIP WAS REPLACED IAW SRM 51-40-02.SDR CHQA20131107418Fitting · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE SHEAR CLIP AT FRAME 13 BETWEEN STRINGERS 21R & 20R. THE SHEAR CLIP WAS REPLACED IAW SRM 51-40-02.SDR CHQA20131107419Fitting · crackedDURING INSPECTION, THE SHEAR CLIP AT FRAME 24 BETWEEN STRINGERS 15R & 16R WAS FOUND TO BE CRACKED. THE SHEAR CLIP WAS REPLACED IAW SRM 51-40-02.SDR CHQA20131107420Fitting · crackedDURING INSPECTION, THE SHEAR CLIP AT FRAME 25 BETWEEN STINGERS 15R & 16R WAS FOUND TO BE CRACKED. THE SHEAR CLIP WAS REPLACED IAW SRM 51-40-02.SDR CHQA20131107421Fitting · corrodedDURING INSPECTION, THE SHEAR CLIP AT FRAME 23 BETWEEN STINGERS 16R & 15R WAS FOUND TO BE CRACKED. THE SHEAR CLIP WAS REPLACED IAW SRM 51-40-02.SDR CHQA20131107422Fitting · crackedDURING INSPECTION, A CRACK WAS FOUND IN THE SHEAR CLIP AT FRAME 68 BETWEEN STRINGERS 6L & 8L. THE SHEAR CLIP WAS REPLACED IAW SRM 53-31-04.SDR CHQA20131107424Stringer · corrodedDURING INSPECTION, CORROSION WAS FOUND ON STRINGER 21R BETWEEN FRAMES 12 & 13. THE STRINGER WAS REPLACED IAW SRM 51-40-02.SDR CHQA20131107425Support · corrodedCORROSION WAS FOUND ON THE AILERON TORQUE TUBE SUPPORT BRACKET BETWEEN STRINGER 20L & 21L AT FRAME 12. THE AILERON TORQUE TUBE SUPPORT BRACKET WAS REPLACED IAW SRM 51-40-02.SDR CHQA20131107426Support · corrodedCORROSION WAS FOUND ON THE AILERON TORQUE TUBE SUPPORT BRACKET BETWEEN STRINGER 20R & 21R AT FRAMES 12 & 13 13. THE SUPPORT BRACKET WAS REPLACED IAW SRM 51-40-02.SDR CHQA20131107427Skin · corrodedCORROSION WAS FOUND ON THE SKIN BETWEEN FRAMES 13 & 14 BETWEEN STRINGERS 20L & 20R. THE SKIN WAS REPAIRED IAW ETD 2013-145-057134.SDR CHQA20131106407Transducer · faultyCREW REPORTED THAT DURING STATIC TAKEOFF, RT BRAKE FAILED MOMENTARILY AND A BRAKE DEGRADED EICAS MESSAGE APPEARED. ABORTED TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE REPLACED THE BRAKE CONTROL UNIT AND THE NR 4 WHEEL SPEED TRANSDUCER. OSDR CHQA20131106408Control Unit · faultyCREW REPORTED THAT DURING STATIC TAKEOFF, THE RT BRAKE FAILED MOMENTARILY AND A BRAKE DEGRADED EICAS MESSAGE APPEARED. THE CREW ABORTED TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE REPLACED THE BRAKE CONTROL UNIT AND THE NR 4 WHEEL SPEED TRSDR SIMA20131103004Engine · failedRT ENGINE VIBRATION BY SOUND AND FEEL ON APPROACH AND SHUTDOWN. OIL DOWN TWO QUARTS ON TWO HOUR FLIGHT. AIRCRAFT LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REMOVED AND REPLACED RT ENGINE IAW W/C71-000-00. THE OPS CHECKED GOOD. NO LEAKS NOTED. ACF
Back to Allison AE-3007A1/3