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 SIMA20131031003Plug · inoperativeLEFT NR 1 ENGINE HAS EXHAUST SMOKE FROM TAIL PIPE AFTER SHUTDOWN AND ODOR OF BURNING OIL. R & R LT ENGINE SHAFT PLUG IAW EO-EM-7200-139. PERFORMED ENGINE RUNS, NO SMOKE NOTICED ON LT ENGINE SHUTDOWN.SDR CHQA20131023400Support Bracket · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE AILERON TORQUE TUBE SUPPORT BRACKET AT FRAME 13 BETWEEN STRINGERS 20-21R. SUPPORT BRACKET WAS REPLACED IAW SRM 51-40-02.SDR CHQA20131023401Support Bracket · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE AILERON TORQUE TUBE SUPPORT BRACKET AT FRAME 12 BETWEEN STRINGERS 20-20L. SUPPORT BRACKET WAS REPLACED IAW SRM 51-40-02.SDR CHQA20131023402Stringer · corrodedDURING INSPECTION, CORROSION WAS FOUND ON STRINGER 21R AT FRAME 13. THE STRINGER WAS REPLACED IAW SRM 51-40-02.SDR CHQA20131023403Frame · crackedDURING INSPECTION, A CRACK WAS FOUND ON THE LT SILL FRAME 20 AT STRINGER 3L. THE SILL FRAME 20 WAS REPLACED IAW SRM 51-40-02.SDR CHQA20131023404Shear Tie · crackedDURING INSPECTION, A CRACK WAS FOUND ON THE SHEAR TIE AT FRAME 24 BETWEEN STRINGERS 16R AND 15R. THE SHEAR TIE WAS REPLACED IAW SRM 51-40-02.SDR CHQA20131023405Shear Tie · crackedDURING INSPECTION, A CRACK WAS FOUND ON THE SHEAR TIE AT FRAME 61 BETWEEN STRINGERS 6L AND 7L. THE SHEAR TIE WAS REPLACED IAW SRM 51-40-02.SDR CHQA20131023406Shear Tie · corrodedDURING INSPECTION, A CRACK WAS FOUND ON THE SHEAR TIE AT FRAME 62 BETWEEN STRINGERS 7L AND 8L. THE SHEAR TIE WAS REPLACED IAW SRM 53-31-04.SDR SIMA20130924006Compressor · stalledCREW REPORTED THAT ON INTIAL CLIMB, NR 2 ENGINE HP VIBRATIONS MAXED CLIMBING THROUGH 2000 FT. FELT COMPRESSOR STALL. IMMEDIATELY BROUGHT ENGINE TO IDLE AND INDICATIONS RETURNED TO GREEN. DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. LANDED WITHOUT INCISDR SIMA20130826004Engine · power lossCREW REPORTED DURING CRUISE FLT, NR 1 ENGINE FUEL IMPELLER BYPASSED ILLUMINATED ON EICAS. NR 1 ENGINE WOULD NOT PRODUCE FULL POWER AND ENGINE WAS SPUTTERING LIKE IT WAS STARVED OF FUEL. DECLARED AN EMERGENCY AND DIVERTED. LANDED WITHOUT INCIDENT. ACFT RESDR CHQA20130817321Shear Tie · crackedDURING INSPECTION, A CRACK WAS FOUND ON THE SHEAR TIE, FRAME 68 BETWEEN STRINGERS 6 AND 7L. SHEAR TIE REPLACED IAW SRM 51-40-02.SDR CHQA20130817322Shear Tie · crackedDURING INSPECTION, A CRACK WAS FOUND ON THE SHEAR TIE, FRAME 72 BETWEEN STRINGERS 6 AND 8R. SHEAR TIE REPLACED IAW SRM 51-40-02.SDR CHQA20130817323Shear Tie · crackedDURING INSPECTION, A CRACK WAS FOUND ON THE SHEAR TIE, FRAME 73, BETWEEN STINGERS 8 AND 9L. SHEAR TIE REPLACED IAW SRM 51-40-02.SDR SIMA20130814011Engine · odorCREW REPORTED DURING DESCENT FROM 4000' MSL, AN OILY ODOR ENTERED COCKPIT AND F/A STATION, DISSAPATED AFTER A FEW MINUTES. R & R NR 1 ENGINE IAW 71-000-00. NO DEFECTS NOTED. ACFT RETURNED TO SERVICE.SDR CHQA20130728197Engine · odorDURING FLIGHT THERE WAS AN OIL BURNING ODOR IN THE COCKPIT WHILE USING BLEED SYSTEM 1 AND BOTH PACK SYSTEMS TURNED ON. THE ODOR WAS ONLY PRESENT IN THE COCKPIT AND CLEARED ON THE GROUND WHILE USING THE APU AS A BLEED SOURCE. LANDED WITHOUT INCIDENT. MX REPSDR CHQA20130727193Unknown · odorDURING ALL PHASES OF FLIGHT, A SLIGHT OIL BURNING ODOR WAS PRESENT. MX RAN BOTH ENGINES WITH THE ENGINE BLEED AND PACK SYS TURNED ON. NO ODORS OR DEFECTS WERE NOTED AND ACFT RETURNED TO SERVICE.SDR SIMA20130722003Engine · failedDURING CRUISE FL 330, NOTICED OIL LEVEL WAS 7 QTS ON NR 1 ENGINE. NR 1 ENGINE ITT WENT INTO CAUTION SO THEY PULLED TL BACK HALFWAY. ITT CAME DOWN THEN SHOT INTO RED. NR 1 ENGINE SHUTDOWN ON ITS OWN AND THE COCKPIT FILLED WITH SMOKE. NO ENGINE FIRE INDICATIOSDR CHQA20130722184Ballast · failedAN ELECTRICAL BURNING ODOR IN CABIN NEAR ROW 2 DURING FLIGHT. MX FOUND THE SIDEWALL BALLAST AT ROW 1A TO BE AT FAULT. REPLACED BALLAST. OPS CHECKED GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA20130722185Windshield · failedDURING CRUISE, HEARD A LOUD POP IN COCKPIT AND CAPTAIN'S WINDSCREEN SHATTERED. DESCENDED AND DECLARED AN EMERGENCY. DIVERTED AND LANDED WITHOUT INCIDENT. REPLACED WINDSHIELD. OPS AND LEAK CHECKED GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA20130720183Connector · unsecureMX REPORTED THAT THE RT FORWARD WING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MX RESECURED CONNECTOR. OPS CHECKED GOOD, WITH NO FURTHER DEFECTS NOTED.SDR CHQA20130625136Bulb · inoperativeDURING INSPECTION, THE OVERHEAD COCKPIT EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MX REPLACED THE COCKPIT EMERGENCY LIGHT BULB. OPS CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR 7GMB0201306244991Flex Hose · chafedON DESCENT AT 14,000FT, HYD 2 QTY LOW MESSAGE APPEARED, THEN FOLLOWED SHORTLY BY ENG 2 HYD PUMP FAIL MESSAGE. THE CREW DIVERTED DUE TO RUNWAY REQUIREMENT AND LANDED SAFELY. DURING VISUAL INSPECTION, PN 145-31063-409 HOSE FROM NR 2 ENGINE DRIVEN HYDRAULIC PUMPSDR CHQA20130620221Battery Pack · dischargedDURING INSPECTION, THE OVERWING EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MX REPLACED THE NR 4 EMERGENCY LIGHT BATTERY. OPS CHECKED GOOD WITH NO FURTHER DEFECTS NOTED.SDR 7GMB2013006186181Tube · brokenNR 1 ENGINE ANTI-ICE PRESSURE TRANSDUCER TUBE FOUND BROKEN AT TRANSDUCER AND ENGINE AIR INTAKE ANTI-ICE DUCT. R & R WITH NEW. OPS CHECKED GOOD.SDR CHQA20130602193Light · inoperativeCREW REPORTED THAT THE FLIGHT DECK EMERGENCY LIGHT BULB WAS FOUND TO BE INOPERATIVE DURING PRE-FLIGHT INSPECTION. MX REPLACED THE FLIGHT DECK EMERGENCY LIGHT. OPS CHECKS WERE GOOD WITH NO FURTHER DEFECTS. NOTED.SDR SIMA20130530003Engine · bird ingestionTHE PILOT REPORTED HE WAS UNAWARE OF A BIRDSTIKE THAT MUST HAVE OCCURRED. HE SAID THAT HE USED THE CAPTAIN’S FLASHLIGHT AND MISSED IT ON THE POST INSPECTION. WHILE TROUBLESHOOTING, SMOKE IN THE COCKPIT FOUND NR 2 ENGINE SMELLING LIKE A BIRD HAD GONE THROUGH ISDR CHQA20130524176Light · inoperativeDURING INSPECTION, THE THIRD AFT EMERGENCY FLOOR LIGHTING STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT STRIP. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA20130523174Proximity Switch · corrodedCREW REPORTED THAT AFTER TAKE-OFF THE LANDING GEAR WOULD NOT RETRACT AND THAT THEY RECEIVED A LANDING GEAR AIR/GROUND FAIL MESSAGE. THE CREW RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE AIRCRAFT SAFE FOR FERRY FLIGHT AND THE ASDR CHQA20130523175Connector · corrodedCREW REPORTED THAT AFTER TAKEOFF THE LANDING GEAR WOULD NOT RETRACT AND THAT THEY RECEIVED A LANDING GEAR AIR/GROUND FAIL MESSAGE. THE CREW RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE AIRCRAFT SAFE FOR FERRY FLIGHT AND THE AISDR CHQA20130504153Skin · damagedDURING INSPECTION, A TOOLING MARK ON THE INTERIOR BELLY SKIN WAS FOUND ADJACENT TO STRINGER 21L AND BETWEEN FRAMES 10 AND 11. THE SKIN WAS REPAIRED IN ACCORDANCE WITH ETD 2013-145-008436.SDR CHQA20130502143Light · inoperativeCREW REPORTED THAT THE EMERGENCY LIGHT IN THE FLIGHT DECK WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT LAMP. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA20130502161Support · damagedDURING INSPECTION, A MISDRILLED RIVET HOLE ON THE RIGHT CONTROL CABLE QUADRANT SUPPORT. THE SUPPORT BRACKETS AND QUADRANT SUPPORT WERE REPLACED IN ACCORDANCE WITH SRM 51-40-02 AND 51-20-03.SDR CHQA20130502162Frame · damagedDURING INSPECTION, AN ELONGATED RIVET HOLE WAS FOUND ON FRAME 12 BETWEEN STRINGERS 21R AND 20R. THE FRAME WAS REPAIRED IN ACCORDANCE WITH ETD 2013-145-008257.SDR CHQA20130501151Floor Support · corrodedDURING INSPECTION, CORROSION AND CRACKS WERE FOUND ON THE FLOORBOARD SUPPORT FLANGE OF THE LEFT OMEGA BEAM BETWEEN FRAME 24 AND FRAME 25. THE OMEGA BEAM WAS REPAIRED IN ACCORDANCE WITH SRM 53-00-10.SDR CHQA20130501156Stringer · corrodedDURING INSPECTION, CORROSION WAS FOUND ON STRINGER 21R BETWEEN FRAMES 13 AND 9. THE STRINGER WAS REPLACED IAW SRM 51-40-02.SDR CHQA20130501157Support · corrodedDURING INSPECTION, CORROSION WAS FOUND IN THE RIGHT AILERON QUADRANT SUPPORT WEB AT FRAME 12 AND 13 AND STRINGERS 20R AND 21R. THE RIGHT QUADRANT SUPPORT WAS REPAIRED IN ACCORDANCE WITH SRM 51-40-02.SDR CHQA20130501158Support · corrodedDURING INSPECTION, CORROSION WAS FOUND IN THE LEFT AILERON QUADRANT SUPPORT WEB AT FRAMES 12-13 AND STRINGERS 20L-21L. THE QUADRANT SUPPORT WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.SDR CHQA20130501159Stringer · corrodedDURING INSPECTION, CORROSION WAS FOUND ON STRINGER 21L BETWEEN FRAMES 13 AND 9. THE STRINGER WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.SDR CHQA20130430160Fitting · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE SHEAR CLIP AT FRAME 13 BETWEEN STRINGERS 21L AND 20L. THE SHEAR CLIP WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.SDR CHQA20130426146Doubler · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE REPAIR DOUBLER LEFT OMEGA FRAME 20. THE DOUBLER WAS REPLACED IN ACCORDANCE WITH SRM 53-00-10.SDR CHQA20130426147Bracket · crackedDURING INSPECTION, A CRACK WAS FOUND IN THE BRACKET BETWEEN FRAME 64 AND FRAME 65 AT STRINGER 5L. THE BRACKET WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02, 51-30-01, AND 53-31-02.SDR CHQA20130426148Fitting · crackedDURING INSPECTION, A CRACK WAS FOUND ON THE SHEAR CLIP AT FRAME 73 BETWEEN STRINGER 8L AND 9L. THE SHEAR CLIP WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.SDR CHQA20130426149Floor Support · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CENTER OMEGA AT THE CARBON CROSS MEMBER FRAME 27. THE OMEGA BEAM WAS REPAIRED IN ACCORDANCE WITH SRM 53-00-10.SDR CHQA20130426150Floor Support · corrodedDURING INSPECTION, CORROSION WAS FOUND AT THE SCREW HOLE ON THE CENTER OMEGA LEFT SIDE BETWEEN FRAMES 24 AND 25. THE CENTER OMEGA BEAM WAS REPAIRED IN ACCORDANCE WITH ETD 2013-145-008055.SDR CHQA20130426152Fitting · crackedDURING INSPECTION, A CRACK WAS FOUND ON THE SHEAR CLIP ON FRAME 66 BETWEEN STRINGERS 6L AND 7L. THE SHEAR CLIP WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.SDR CHQA20130426154Fitting · crackedDURING INSPECTION, A CRACK WAS FOUND ON THE SHEAR CLIP AT FRAME 73 BETWEEN STRINGER 8R AND 9R. THE SHEAR CLIP WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.SDR CHQA20130426155Fitting · crackedDURING INSPECTION, A CRACK WAS FOUND ON THE SHEAR CLIP AT FRAME 65 BETWEEN STRINGERS 7L AND 9L. THE SHEAR CLIP WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02 AND 53-31-04.SDR SIMA20130417003Engine · smokeFLIGHT 4439, DURING TAXI-OUT, COCKPIT AND CABIN FILLED WITH SMOKE & HAZE. RETURNED TO GATE AND DECLARED AN EMERGENCY. AIRCRAFT REMOVED FROM SERVICE. ODOR SMELLED LIKE ENGINE OIL. WHILE TROUBLESHOOTING FOUND NR 1 ENGINE TO BE SOURCE OF OIL ODOR & HAZE. SDR CHQA20130416124Door Frame · corrodedDURING INSPECTION, THE MAIN PASSENGER DOOR LOWER FRAME WAS FOUND TO HAVE CORROSION AT THE FASTENER HOLES. THE PASSENGER DOOR LOWER FRAME WAS REPAIRED IN ACCORDANCE WITH ETD 2013-145-007009.SDR CHQA20130416125Fitting · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CARGO DOOR CUTOUT LATERAL L SHAPE AT THE BOTTOM OF FRAME 65. THE SHEAR CLIP WAS REPLACED IN ACCORDANCE WITH SRM 53-31-04.
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