Allison AE-3007A1
Service difficulty reports · 321
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 = 'AE3007A1' 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 = 'AE3007A1' 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 SIMA20140329004Engine · malfunctionedSTRONG OIL SMELL NOTED IN COCKPIT & CABIN DURING APPROACH & TAXI IN. IAW NRWC 613-DFW-01774 R & R NR 1 ENG IAW WORK CARD 71-000-00, OPERATIONS & LEAK CHECKED NORMAL.SDR CHQA20140319088Battery · dischargedDURING INSPECTION THE OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MX REPLACED THE NR 4 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR SIMA20140302001Engine · malfunctionedAFTER TAKEOFF AT 1500 FEET LAVATORY SMOKE WARNING ON EICAS. RETURNED TO KCMH. FLIGHT ATTENDANT REPORTED SMOKE IN LAST 3 ROWS. ACCOMPLISHED FIM ASK 21-20-00, FOUND SMALL AMOUNT OF DEICING FLUID AT NR 2 ENG AIR INLET. CLEANED AS REQUIRED, RUN ENG IAW ETN-EM-SDR ASOA20140226023Engine · contaminatedCREW REPORTED SMOKE IN COCKPIT IMMEDIATELY AFTER TAKEOFF AND PERFORMED AIR TURN BACK. MAINTENANCE INSPECTED ACFT AND DETERMINED THE ACFT WAS DE-ICED PRIOR TO TAKEOFF AND FOUND DE-ICE FLUID IN BOTH ENGINE INLETS. MAINTENANCE REMOVED FLUID AND RAN ENGINES AND PSDR SIMA20140131008Carbon Seal · failedON POST FLIGHT NR 1 ENG SMOKING AFTER SHUTDOWN FOR 15 MINUTES. IAW ETN-EM-79-015 REV 5 SHAFT PLUG WAS CHANGED 22.13 HRS AGO. IAW ETN STEP 13 THE RTBS & THE THIRD STAGE BLADES ARE DRY. R&R THE ENGINE DUE TO A NR 7 CARBON SEAL. REMOVED AND REPLACED LT ENG SSDR SIMA20140130002Engine · malfunctionedAFTER TAKEOFF FLIGHT ATTENDANT CALLED UP & REPORTED STRONG BURNING ODOR, PAX COMPLAINED AS WELL. TAKEOFF WAS ALT TO 1, CLB LANDED UNDER MAX WT. R & R LT ENG IAW WORK CARD 71-000-00, OPERATIONS & LEAK CHECKED GOOD.SDR SIMA20140110011Accelerometer · failedDURING CLIMB THROUGH FL260 TGE NR 1 ENG BEGAN TO SURGE. CREW TURNED THEN ENG IGNITION ON & THE N1 SURGING WENT AWAY. CREW DECLARED AN EMERGENCY & DIVERTED TO IND. DURING MAINTENANCE INSPECTION ON FLIGHT 3745 FOUND ALT TO 1 AT SJT RIGHT HP WENT TO THE BOTTOMSDR SIMA20131014005Engine · vibrationDURING CLIMBOUT MID 20K IN ALTITUDE, NR 1 ENGINE HP VIBRATION GAUGE JUMPED INTO THE AMBER, ABOUT .33 -.5 UP. VIBRATION CHANGED WITH REDUCTION INCREASED WITH ADVANCEMENT. SEEMED WORSE BETWEEN FL 250 AND FL 320. R & R NR 1 ENGINE IAW 71-000-00. OPS & LEAK CHSDR SIMA20130920004Engine · odorTHE CREW REPORTED THAT DURING THE TAKEOFF ROLL THE NOTICED A BURNING ODOR IN THE COCKPIT. THE CREW ABORTED THE TAKEOFF. CONFIRMED ODOR IN CABIN. THE ACFT WAS REMOVED FROM SERVICE. R & R THE LT ENGINE IAW WC 71-000-00. OPS AND LEAK CHECKED GOOD IAW MM 72-0SDR SIMA20130905005Carbon Seal · leakingHEAVY OIL ODOR THRU ENVIROMENTAL SYS AFTER ADDING THRUST DURING DESCENTS AND CLIMB. FOUND OIL TO BE LEAKING FROM NR 1 ENGINE CARBON SEAL. REMOVED AND REPLACED THE CARBON SEAL IAW MM 72-25-25. OPS CHECKED GOOD. PERFORMED ETN ETN-EM-72-034. NO DETECTABLE ODOR SDR SIMA20130829002Engine · leakingDURING TAKEOFF, BELOW 80KTS, AFTER POWER SET, NOTICED SMOKE IN COCKPIT, F/A ADVISED SMOKE IN CABIN, ABORTED TAKEOFF TURNED OFF BOTH ACFT PACKS AND RECIRCULATION FANS. SMOKE DISSIPATED, RAN GROUND EVAC CHECKLIST. PERFORMED ETN-EM-72-034 ENGINE ODOR EVENT TROSDR SIMA20130707008Carbon Seal · leakingFOUL ODOR WHEN NR 1 PACK WAS SELECTED AND ON ENGINE BLEED SOURCE ODOR IS LESS WITH APU BLEED SOURCE, AND GONE WITH THE PACK OFF. THE ACFT WAS REMOVED FROM SERVICE. PERFORMED ETN-EM-72-034 AND DETERMINED ENGINE NR 1 BLEED TO BE THE SOURCE OF ODOR. FOLLOWING THSDR RAIA201306130001Engine · shutdownDURING CRUISE, FLIGHT CREW RECEIVED A NR 2 ENGINE TEMPERATURE SPIKE. PULLED THROTTLE BACK AND ENGINE AUTO SHUTDOWN. DIVERTED. MX INSPECTED AND R & R NR 2 ENGINE. OPS CHECKED GOOD.SDR RAIA201305100006Support · corrodedDURING SCHEDULED MAINTENANCE, FOUND CORROSION AROUND TRANSPONDER. MX R & R THE SUPPORT ASSY AROUND THE TRANSPONDER ANTENNA.SDR SIMA20130227006Engine · failedFLIGHT 4132, CREW REPORTED JUST AFTER VR, FUMES AND HAZE BECAME EVIDENT IN COCKPIT. BY APPROX. 500FT, FLIGHT ATTENDANT CHIMMED AND NOTIFIED CREW OF SMOKE IN CABIN. EICAS LAVATORY SMOKE WARNING ILLUMINATED. EMERGENCY PROCDURES PERFORMED PER AOM - 1. FLIGHSDR SIMA20130127006Engine · failedFLIGHT 3917. DURING CRUISE ALTITUDE FL 360, NR 2 ENGINE ITT ON EICAS SPIKED TWICE, AND TEMP AS HIGH AS 1015 DEGREES. WITH THE SPIKES TWO SEPARATE VIBRATIONS WERE FELT. NR 2 ENGINE THEN HAD AN UN-COMMANDED SHUTDOWN. OIL SHOWED TO BE 4 QUARTS. AT DEPARTURSDR CHQA20121126444Strut · lowCREW REPORTED, RECEIVED A LANDING GEAR AIR/GROUND FAIL MESSAGE IN FLIGHT. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE SERVICE THE LEFT, RIGHT, AND NOSE LANDING GEAR STRUTS. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA20121126445Strut · lowCREW REPORTED, RECEIVED A LANDING GEAR AIR/GROUND FAIL MESSAGE IN FLIGHT. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE SERVICE THE LEFT, RIGHT, AND NOSE LANDING GEAR STRUTS. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA20121126446Strut · lowCREW REPORTED, RECEIVED A LANDING GEAR AIR/GROUND FAIL MESSAGE IN FLIGHT. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE SERVICE THE LEFT, RIGHT, AND NOSE LANDING GEAR STRUTS. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA20121123430Battery · dischargedDURING INSPECTION, THE LEFT FUSELAGE EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA20121122432Threshold · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CARGO DOOR THRESHOLD BETWEEN FRAMES 65 AND 67. THE THRESHOLD WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.SDR CHQA20121121443Fitting · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LATERAL L SHAPE FRAME 65 LOWER AT THE CARGO DOOR REST PLACED. MAINTENANCE REPLACED THE SHEAR CLIP IN ACCORDANCE WITH ETD 2012-145-016935.SDR DJFA20121118001Ballast · failedCREW REPORTED STRONG ODOR OF HOT ELECTRICAL OR RUBBER IN CABIN. MX FOUND BALLAST FOR PASSENGER LIGHTING BAD.SDR CHQA20121027438Angle · damagedDURING HEAVY MAINTENANCE A PERMANENT REPAIR WAS COMPLETED ON THE RIGHT LOWER WING TRAILING EDGE IN ACCORDANCE WITH ETD 2012-145-015393B.SDR CHQA20121115440Fitting · crackedDURING INSPECTION, A CRACK WAS FOUND ON THE SHEAR CLIP AT FRAME 68 BETWEEN STRINGERS 6L AND 7L. MAINTENANCE REPLACED THE UPPER SHEAR CLIP AND REPAIRED THE LOWER SHEAR CLIP IN ACCORDANCE WITH SRM 51-40-02.SDR CHQA20121115441Fitting · crackedDURING INSPECTION, A CRACK WAS FOUND ON THE SHEAR CLIP AT FRAME 68 BETWEEN STRINGERS 6L AND 7L. MAINTENANCE REPLACED THE UPPER SHEAR CLIP AND REPAIRED THE LOWER SHEAR CLIP IN ACCORDANCE WITH SRM 51-40-02.SDR CHQA20121115439Skin · damagedDURING HEAVY MAINTENANCE A PERMANENT REPAIR WAS COMPLETED OF A LIGHTNING BURN ON FRAME 23 ABOVE STRINGER 20L IN ACCORDANCE WITH ETD2012-145-007041. PART INFORMATION WILL BE SUBMITTED AS A SUPPLEMENT TO THIS REPORT.SDR CHQA20121115442Frame · damagedDURING HEAVY MAINTENANCE A PERMANENT REPAIR OF A LIGHTNING BURN AT FRAME 13 ON STRINGER 19L WAS COMPLETED IN ACCORDANCE WITH ETD2012-145-007033.SDR CHQA201211/14431Stringer · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE EDGE OF STRINGER 21R AT FRAME 11 THROUGH 12. THE STRINGER WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.SDR CHQA20121113421Connector · disconnectedDURING INSPECTION, THE FLOOR PROXIMITY STRIP LIGHTS AT ROW 12 AND AFT WERE FOUND TO BE INOPERATIVE. MAINTENANCE RE-SCURED CONNECTOR P8532 TO THE NUMBER 6 INVERTER. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA20121113422Light · inoperativeDURING INSPECTION, THE MAIN ENTRY DOOR EMERGENCY LIGHT ON THE DOOR HINGE WAS FOUND TO BE INOPERATIVE. THE MAIN ENTRY DOOR EMERGENCY LIGHT WAS RELAMPED. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOETD.SDR CHQA20121010408Fuel Cap · unsecureCREW REPORTED THAT THE RIGHT FUEL CAP CAME OFF DURING FLIGHT. THE AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE RE-SECURED THE RIGHT OVERWING FUEL CAP AS REQUIRED. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA20121109407Control Lever · faultyCREW REPORTED THAT DURING CLIMB, WHEN THE LANDING GEAR LEVER WAS SELECTED UP, THAT THE LANDING GEAR DID NOT RETRACT AND A LANDING GEAR LEVER DISAGREE MESSAGE APPEARED. THE CREW MOVED THE LANDING GEAR LEVER DOWN AND THE LANDING GEAR SHOWED DOWN AND LOCKED. THSDR CHQA20121108425Doubler · damagedDURING INSPECTION, THE LEFT SIDE COCKPIT BULK HEAD BAYONET RECEPTACLE UPPER REPAIR WAS FOUND TO BE DAMAGED. THE UPPER PLATES WERE REPLACED IN ACCORDANCE WITH SRM 51-40-00.SDR CHQA20121108426Doubler · damagedDURING INSPECTION, THE LEFT SIDE COCKPIT BULK HEAD BAYONET RECEPTACLE LOWER REPAIR WAS FOUND TO BE DAMAGED. THE LOWER PLATE WERE REPLACED IN ACCORDANCE WITH SRM 51-40-00.SDR CHQA20121108428Seat Track · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LEFT OUTBOARD SEAT TRACK AT FRAME 23 THROUGHT FRAME 28. THE SEAT TRACK WAS REPLACED IN ACCORDANCE WITH AMM 53-01-06.SDR CHQA20121108429Support Bracket · corrodedDURING INSPECTION, THE COCKPIT UNDERFLOOR AILERON QUADRANT RIGHT SUPPORT BRACKET WAS FOUND TO BE CORRODED. THE SUPPORT BRACKET WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.SDR CHQA20121108435Support · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE SUPPORT AT FRAMES 10 THROUGH 11. THE SUPPORT WAS REPAIRED IN ACCORDANCE WITH ETD 2012-145-016499A.SDR CHQA20121108436Support · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE SUPPORT AT FRAME 10 THROUGH 11 AT STRINGER 20R UNDERNEATH THE ELEVATOR QUADRANT. THE SUPPORT WAS REPAIRED IN ACCORDANCE WITH ETD 2012-145-016499A.SDR CHQA20121107427Floor Support · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LEFT SIDE OF THE CENTER OMEGA BEAM AT CARBON CROSSMEMBER FRAME 28. THE LEFT CENTER OMEGA BEAM AT FRAME 28 WAS REPAIRED IN ACCORDANCE WITH SRM 51-20-03.SDR CHQA20121107434Floor Support · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LEFT SIDE OF THE CENTER OMEGA BEAM AT CARBON CROSSMEMBER FRAME 24. THE LEFT CENTER OMEGA BEAM AT FRAME 24 WAS REPAIRED IN ACCORDANCE WITH SRM53-00-10.SDR CHQA20121107433Floor Support · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE INBOARD SIDE OF THE LEFT OMEGA BEAM AT CARBON CROSSMEMBER BETWEEN FRAMES 24 AND 25. THE INBOARD SIDE LEFT-HAND OMEGA BEAM WAS REPLACED IN ACCORDANCE WITH SRM 51-40-00.SDR CHQA20121106406Light · inoperativeCREW REPORTED THAT THE RIGHT OVERWING EXTERNAL EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE DEFERRED THE EMERGENCY LIGHT. THE DEFERRAL WAS CLEARED ON 11/7/2012 BY REPLACING THE RIGHT OVERWING EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECKS WERE GOOSDR CHQA20121103403Proximity Switch · faultyCREW REPORTED THAT AFTER TAKEOFF THE NOSE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NOSE LANDING GEAR WOW HARNESS (W019) AND THE NOSE LANDING GEAR WOW PROXIMITY SWITCH. OPERATIONAL CSDR CHQA20121103404Wire Harness · faultyCREW REPORTED THAT AFTER TAKEOFF THE NOSE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NOSE LANDING GEAR WOW HARNESS (W019) AND THE NOSE LANDING GEAR WOW PROXIMITY SWITCH. OPERATIONAL CSDR CHQA20121103405Sign · inoperativeDURING INSPECTION, THE EMERGENCY EXIT SIGN ABOVE SEAT 12F WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY EXIT SIGN AT ROW 12, OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA20121131409Seat Track · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT WALL SEAT TRACK FROM FRAME 53 THROUGH FRAME 57. THE RIGHT SIDE WALL SEAT TRACK FROM FRAME 53 THROUGH FRAME 57 WAS REPLACED IN ACCORDANCE WITH AMM 53-01-06.SDR CHQA20121031410Seat Track · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT SIDE WALL SEAT TRACK FROM FRAME 47 THROUGH FRAME 52. THE RIGHT SIDE WALL SEAT TRACK FROM FRAME 47 THROUGH FRAME 52 WAS REPLACED IN ACCORDANCE WITH AMM 53-01-06.SDR CHQA20121031411Seat Track · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LEFT SIDE WALL SEAT TRACK FROM FRAME 54 THROUGH FRAME 59. THE LEFT SIDE WALL SEAT TRACK FROM FRAME 54 THROUGH FRAME 59 WAS REPLACED IN ACCORDANCE WITH AMM 53-01-06.SDR CHQA20121031412Seat Track · corrodedDURING INSPECTION, THE CENTER OMEGA BEAM SEAT TRACK WAS FOUND TO BE CORRODED FROM FRAME 41 THROUGH FRAME 47. THE CENTER OMEGA BEAM SEAT TRACK FROM FRAME 41 THROUGH FRAME 47 WAS REPLACED IN ACCORDANCE WITH AMM 53-01-06.
Back to Allison AE-3007A1