Allison AE-3007A
Service difficulty reports · 3,309
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 = 'AE3007A' 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 = 'AE3007A' 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 C2XA04TY116Sill · corrodedDURING A SCHEDULED 4C INSPECTION CORROSION WAS FOUND ON THE FWD SERVICE DOOR SILL. MAINT. REMOVED AND REPLACED THE FWD DOOR SILL IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL, BE REL. UPON COMPLETION OF ALL 4C WORK.SDR C2XA04TY117Sill · corrodedDURING A SCHEDULED 4C INSPECTION,CORROSION WAS FOUND ON THE AFT SERVICE DOOR SILL. MAINT REMOVED AND REPLACED THE AFT DOOR SILL IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE REL. UPON COMPLETION OF ALL 4C WORK.SDR C2XA04TY119Cap · corrodedDURING A SCHEDULED 4C INSPECTION, CORROSION WAS FOUND ON THE RIVETS AT THE CENTER LAV TOP CAP. MAINT REMOVED AND REPLACED THE LAV TOP CAP IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE REL. UPON COMPLETION OF ALL 4C INSPECTION.SDR RAIA00407016Fadec · malfunctionedNO DISPATCH MESSAGE, NR 1 ENGINE. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE FADECS.SDR C2XA04TY121Floor Support · corrodedDURING A SCHEDULED 4C INSPECTION, CORROSION WAS FOUND ON THE FLOORBOARD SUPPORT FROM LAV TO CARGO. MAINT. REMOVED AND REPLACED THE SUPPORT FROM THE LAV TO THE CARGO IAW SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE REL. UPON COMPLETION OF ALL WORK.SDR C2XA04TY122Floor Support · corrodedDURING A SCHEDULED 4C INSPECTION THE CENTER OMEGA BEAM UNDER THE LAV FLOOR WAS CORRODED. MAINTENANCE CLEANED UP THE DAMAGE AREA, BLENDED, ALODINED, PRIMED AND PAINTED IAW SRM 51-10-02;03 AND CPM 51-21-04 AND 51-21-05. ALL WORK WAS ACCOMPLISHED AND WILL BESDR C2XA04TY120Support · corrodedDURING A SCHEDULED 4C INSPECTION, CORROSION WAS FOUND ON THE RT FWD FLOORBOARD SUPPORT SILL IN THE LAV MAINT. REMOVED AND REPLACED THE FLOOR BOARD SILL IAW SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE REL. UPON COMPLETION OF THE 4C INSPECTION.SDR CHQA000521Odor · detectedDURING CRUISE, AT 10,000 FT, NOTICED A STRONG ELECTRICAL ODOR COMING FROM UNDER THE CAPTAINS PFD. ONCE ON THE GROUND DETERMINED THAT THE CAPTAINS PFD WAS CONSIDERABLY HOTTER THAT THE OTHER TUBES. TURNED OFF THE AVIONICS AND THE HEAT SUBSIDED. INSPECTED AVIOSDR C2XA04SH467Beam · corrodedDURING C CHECK THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR CHQA000520Carbon Seal · leakingCREW REPORTS ON CLIMB OUT AT HIGH POWER THEY EXPERIENCED A BURNING ODOR IN THE AIRCRAFT. THE POWER WAS DECREASED AND THE ODOR DISSIPATED. AS POWER WAS INCREASED THE BURNING ODOR CAME BACK. RAN BOTH ENGINES AT 98 PERCENT FOR 5 MINUTES AND AT GROUND IDLE FOR SDR C2XA04TY113Attach Bracket · bentDURING A 4C INSPECTION THE CARGO DOOR RAMP ANGLE SUPPORTS AT FR.66 AND FR.67 WERE FOUND BENT. MAINT. REMOVED AND REPLACED THE CARGO DOOR RAMP ANGLE SUPPORTS IAW SRM 51-40-02.SDR C2XA04TY114Plate · corrodedDURING A SCHEDULED 4C INSPECTION AT FR 59 STR 19R,THE WATER SERVICE BASE PLATE, CORROSION WAS FOUND ON THE RIVETS. MAINTENANCE CLEANED THE EFFECTED AREA, BLENDED, ALLODINED, PRIMED, PAINTED AND APPLIED CORROSION INHIBITOR COMPOUND. ALL WORK WAS ACCOMPLISHED SDR C2XA04SH465Floorbeam · corrodedDURING (C) CHECK THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW SRM 53-21-10, STEP 2 FIG. 201. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH466Battery · dischargedDURING C-CHECK THE NR 4 EMERGENCY LIGHT BATTERY WAS FOUND TO BE DISCHARGED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY, THE ENSUUING OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04BT079Power Supply · faultyMAINTENANCE REPORTED, DURING SERVICE CHECK, LT FRONT FAIRING WING FUSELAGE EMERGENCY LIGHT INOPERATIVE AND NR 1 AISLE PATH EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED NR 1 BATTERY POWER SUPPLY IAW EMB145 NR 33-50-04, OPS. CHECKED SYSTEM GOOSDR RAIA00407012Engine · malfunctionedDEN - LEFT ENGINE HIGH ITT UPON SETTING T/O TRUST. MAINTENANCE INSPECTED NR 1 ENGINE AND PERFORMED ENGINE RUN. ALL INDICATIONS NORMAL IAW ROLLS ROYCE MM 72-00-00.SDR C2XA04SH464Floorbeam · corrodedDURING C CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR CHQA000528Filler · missingEMERGENCY FLOOR PROXIMITY LIGHTS STRIPS ARE MISSING FILLER STRIPS. INSTALLED FLOOR PROXIMITY FILLER STRIPS IAW AMM 33-50-12.SDR C2XA04IA088Light · inoperativeDURING PREFLIGHT INSPECTION THE CREW FOUND THE EMERGENCY LIGHT STRIP AT ROW 9 TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, OPERATIONALLY TESTED THE LIGHTING AND CLEARED THE DISCREPANCY.SDR MASA200400415Light · inoperativeDURING MAINTENANCE, FOUND 1ST SECTION OF FLOOR EMERGENCY LIGHTING STRIP WOULD NOT ILLUMINATE. DEFERRED IAW MEL 33-50-00-2. MAINTENANCE REPLACED THE LIGHTING STRIP ON 7/20/04. OPS CHK GOOD.SDR MASA200400414Pitch Control · malfunctionedRETURNED TO THE FIELD DUE TO A PITCH TRIM 1 AND 2 INOPERATIVE AND CAS MISCOMPARE MSG. MECHANIC RESET THE PITCH TRIM SYSTEM AND IT OPERATED NORMALLY. ALL MESSAGES CLEARED AND A/C DEPARTED WITHOUT FURTHER INCIDENT.SDR MASA200400412Priority Valve · inoperativeSUP/CLOSED -ASH 2701 FROM CAE-PHL. THE LANDING GEAR WOULD NOT RETRACT DURING CLIMBOUT. IAW CFM CREW MADE 2ND ATTEMPT AND GEAR RETRACTED NORMALLY. MX TAKING A/C TO HANGER FOR TROUBLESHOOTING. MAINTENANCE REPLACED PRIORITY VALVE.SDR C2XA04IA087Battery Pack · dischargedPILOT REPORTED THAT THE EMERGENCY LIGHTING DID NOT WORK WHEN TESTED DURING PREFLIGHT INSPECTION. THE ENGINES WERE RUN TO RECHARGE THE BATTERY PACKS AND AN OPERATIONAL CHECK OF THE LIGHTING SYSTEM WAS ACCOMPLISHED. THE EMERGENCY LIGHTS TESTED GOOD AND THE DISCRSDR SIMA200420101Pitot System · contaminatedDUIRNG CRUISE FLIGHT, NR 1 ENGINE LOST POWER, REGAINED POWER TWO TIMES, THEN RAN NORMALLY. AFTER LANDING NR 1 ENGINE EXPERIENCED AN UNCOMMANDED SHUTDOWN. PERFORMED TROUBLESHOOTING IAW FAULT ISOLATION MANUAL AND FOUND WATER IN BOTH PITOT SYSTEMS. DRAINED PITSDR C2XA04BT078Light · inoperativeCREW REPORTED, (STRIP OF EMERGENCY AISLE PATH LIGHTS NOT WORKING.) MAINTENANCE RELEASED THE AIRCRAFT IAW MEL NR 33-50-00/02 CATEGORY C-PLACARD NR 044167 AND RETURNED THE AIRCRAFT TO SERVICE. ON IAD RON 07/16/2004 MAINTENANCE TROUBLESHOT AND REMOVED AND REPLASDR C2XA04CL072Carbon Seal · leakingTHE CREW REPORTED SMOKE IN THE COCKPIT AND CABIN ON CLIMB. THEY ALSO REPORTED A LAV SMOKE LITE WARNING. THE AIRCRAFT RETURNED TO EWR AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 1 ENGINE AND OPERATIONAL CHECKS WERE GOOD.SDR C2XA04BT076Light · burned outDURING 5A INSPECTION, MAINTENANCE FOUND EMERGENCY EXIT SIGN OVER SERVICE DOOR, NOT OPERATING. REMOVED AND REPLACED EMERGENCY EXIT SIGN LIGHT OVER SERVICE DOOR IAW AMM NR 33-50-06. OPS. CHECKED GOOD.SDR SIMA200419401Engine · failedON CLIMB-OUT CREW REPORTED A LOUD BANG. ENGINE NR 2 ROLL BACK AND UNCOMMANDED SHUTDOWN. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE IAW EMB MM. OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR MASA200400388Warning Light · illuminatedSUP/CLOSED- ASH 2811 IND. AIRCRAFT ABORTED TAKEOFF AND RETURNED TO GATE WITH A ENG 1 REV DISAGREE CAUTION MESSAGE DURING TAKE OFF ROLL. MAINTENANCE DEFERRED E1 T/R IAW MEL 78-34-00 AND CONTINUED OPS. 7/9/04 MX RE-RIGGED AND OPS CHK OK.SDR CA040629001Engine · making metal(CAN) PRELIMINARY REPORT, HIGH OIL TEMPERATURE, LOW OIL PRESSURE AND IMPENDING BYPASS MESSAGE. PILOT COMMANDED THE IFSD DURING CRUISE. EMERGENCY DECLARED AND UNEVENTFUL LANDING. REPORTED METAL DEBRIS ON OIL TANK CHIP DETECTOR AND NOT ABLE TO ROTATE FAN OR COSDR MASA200400370Control Unit · failedSUP/CLOSED - ASH 2818 CAE-DCA. ENG NR 1 TR DISAGREE ON T/O, ABORTED TAKEOFF. MX PLACED ON MEL MAINTENANCE REPLACED THE ICU.SDR MASA200400369Resistor · inoperativeSUP/CLOSED - ASH 2681 CLT-BHM. ENG NR 1 REVERSER DISAGREE ON TAKE OFF. ABORTED TAKEOFF MX PLACED ON MEL. MAINTENANCE REPLACED RESISTOR.SDR SIMA200417703Starter · brokenFLT 3712 - CVG - DURING TAKEOFF, 500 FT AIR CREW REPORTED E1 FIRE INDICATION FOLLOWED BY FIRE WARNING BELL ABOUT 1.5 MINUTES LATER. FOUND NR 1 ENGINE AIR TURBINE STARTER BROKEN OFF THE MOUNTING PAD SEVERING FLUID LINES IN THE AREA WHICH CAUSED FIRE. NR 1 ENGSDR CA040625007Engine · failed(CAN) PRELIMINARY REPORT THE CREW REPORTED THAT ON DESCENT, THE NR 2 ENGINE FAILED (UNCOMMANDED SHUT DOWN). THE AIRCRAFT LANDED WITHOUT INCIDENT. ON GROUND, THE FAN WOULD NOT ROTATE FREELY, BUT CORE COULD NOT BE ROTATED VIA PMA SHAFT. ENGINE ALLOCATED TO RRCSDR CHQA000506Light · inoperativeEXIT ROW MARKER ON FLOOR FOUND INOPERATIVE. REMOVED AND REPLACED EXIT ROW LIGHT STRIP IAW MM CH 33-50-00. OPS CHECK GOOD.SDR C2XA04IA073Engine · malfunctionedIAH - FLIGHT 2376 THE CREW REPORTED THAT THE NUMBER ONE ENGINE SHOWED LOW OIL PRESSURE, AND HIGH OIL TEMPERATURE WITH A SMELL OF SMOKE DURING CRUISE. THE CREW SHUT DOWN THE NUMBER ONE ENGINE AS A PRECAUTION, AND LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE RESDR CX2A04RI004Engine · fireCREW RETURNED ACFT TO THE GATE AFTER ENG NR 1 HUNG START AND AN ABORTED ENG NR 1 HOT START. PASSENGERS WERE DEPLANED. MAINTENANCE DISCOVERED NR 1 ENG SMOKING AND SUSPECTED ENGINE CORE FIRE. MAINTENANCE PROCEEDED WITH NR 1 ENG DRY MOTORING TO EXPEL RESIDUAL SDR SIMA200417002Fcu · inoperativeCREW A FLAP FAIL MESSAGE WHEN FLAPS WERE RETRACTED AFTER TAKEOFF. FLAPS REMAINED AT 9 DEGREES. FOLLOWED AOM PROCEDURES AND LANDED WITH FLAPS AT 9 DEGREES AND OVERWEIGHT AT 42,800 AND 300 FPM. MAINTENANCE REMOVED AND REPLACED THE FLAP ELECTRONIC CONTROL UNITSDR C2XA04IA072Engine · failedTHE CREW REPORTED THAT ON DESCENT INTO IAH THE NUMBER TWO ENGINE FAILED (UNCOMMANDED SHUT DOWN). THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO ENGINE, OPERATIONAL CHECKED GOOD, AND THE AIRCRAFT WAS APPROVED SDR SIMA200416202Control Unit · malfunctionedDURING APPROACH CREW REPORTED FLAP FAIL AND SPS ADVANCE CAUTION MESSAGES ON EICAS. RESETING BREAKERS DID NOT HELP. MAINTENANCE RESET FLAP ELECTRIC CONTROL UNIT IAW MM. INDICATION RETURNED TO NORMAL AND ALL EICAS MESSAGES WERE CLEARED. AIRCRAFT WAS RETURNED SDR SIMA200415805Switch · inoperativeDURING TAKEOFF CREW REPORTED THE LANDING GEAR DID NOT RETRACT WHEN SELECTED UP. CREW NOTED A LDG AIR/GRD MESSAGE ON EICAS. CREW RETURNED TO DEPARTURE AIRPORT. MAINTENANCE DOWNLOADED CMC AND FOUND MULTIPLE FAILURES ON THE LT PROXIMITY SWITCH. THE LT WOW PROSDR SIMA200415801Engine · failedDURING CLIMB AT FL290, CREW REPORTED A NR 1 ENGINE VIBRATION FOLLOWED BY A PUFF OF SMOKE IN THE COCKPIT. POWER WAS REDUCED AND A/C WAS DIVERTED TO CLT. DURING APPROACH WHEN NR 1 WAS BROUGH OUT OF IDLE CREW REPORTED MAX VIBRATION AND LOSS OF OIL PRESSURE. ENSDR CA040602001Blade · failed(CAN) AC YAW AND LOUD BANG IN CLIMB AT 21,000 FT. ENGINE SHUTDOWN UNCOMMANDED. EMERGENCY DECLARED AND AC DIVERTED. ON GROUND INSP FOUND THAT N1 WOULD NOT ROTATE. DISASSEMBLY OF ENG AT RRC SHOWED SEVERE TURBINE DAMAGE. SULPHIDATION, PROBABLY CAUSED THE DESDR CA040602002Bevel Gear · failed(CAN) FLIGHT LOST POWER NOTICED SHORTLY AFTER TAKE OFF. NR 2 INDICATION WENT TO ZERO. THE CREW REPORTED THE NR 1 ENGINE SHUT DOWN IN FLIGHT. THE SHUT DOWN WAS UNCOMMANDED. THE AIRCRAFT RETURNED AND LANDED WITHOUT FURTHER INCIDENT. DISASSEMBLY OF THE ENGINE ASDR CA040602003Shaft · failed(CAN) IN CLIMB AT 8000 FT A LOUD BANG WAS HEARD AND UNCOMMANDED ENGINE SHUTDOWN AND AIR RETURN AND UNEVENTFUL LANDING OCCURRED. DISASSEMBLY OF THE ENGINE AT RRC REVEALED THAT NR 6 BEARING BEVEL DRIVING GEAR SYSTEM THAT DRIVE MODULE 05 ACCESSORY GEARBOX HAS FSDR CA040602006Bolt · loose(CAN) COMMANDED IFSD AND AIR RETURN. CREW REPORTED EMERGENCY WHEN ITT EXCEEDED 950C. UNEVENTFUL AIR RETURN. DISASSEMBLY OF ENGINE AT RRC SHOWED THAT OUTER MANIFOLD SERVICE ATTACHMENT BOLTS LOOSEN. BLEED AIR LEAKAGE CAUSED THERMAL DAMAGE TO THE SURROUNDING COMSDR C2XA04SH330Floorbeam · corrodedDURING C CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH331Stiffener · chafedDURING C CHECK THE T-REINFORCEMENT ON STRINGER 19R WAS FOUND TO BE CHAFED BETWEEN FRAMES 52 AND 53. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH332Skin · dentedSHV-DURING C CHECK THE EXTERNAL SKIN WAS FOUND TO BE DENTED AT FRAME 19A AND STRINGER 12L. MAINTENANCE PERFORMED A DOUBLER REPAIR TO THE AFFECTED AREA IAW EMB 145 SRM 53-22-01 STEP 6 FIGURE 206. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH323Stiffener · gougedSHV-DURING C CHECK THE T REINFORCEMENT ON EXTERNAL STRINGER 19L WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
Back to Allison AE-3007A