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 CHQA201100273Wire · shortedDURING INSPECTION THE LEFT FORWARD EXTERNAL EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. UPON FURTHER INSPECTION, MAINTENANCE FOUND SHORTED WIRES TO THE LIGHTING ASSEMBLY. REPLACED THE LEFT FORWARD EXTERNAL EMERGENCY LIGHT ASSEMBLY AND THE NUMBER 1 EMERGENCYSDR CHQA201100293Seat Track · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LEFT OUTBOARD SEAT TRACK 5. MAINTENANCE REPLACED THE LEFT OUTBOARD SEAT TRACK 5 WITH NO FURTHER DEFECTS NOTED.SDR CHQA201100294Seat Track · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT OUTBOARD SEAT TRACK 4. MAINTENANCE REPLACED THE RIGHT OUTBOARD SEAT TRACK 4 WITH NO FURTHER DEFECTS NOTED.SDR CHQA201100295Seat Track · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE RIGHT INBOARD SEAT TRACK 1. MAINTENANCE REPLACED THE RIGHT INBOARD SEAT TRACK 1 WITH NO FURTHER DEFECTS NOTED.SDR CHQA201100296Seat Track · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT INBOARD SEAT TRACK 2. MAINTENANCE REPLACED THE RIGHT INBOARD SEAT TRACK 2 WITH NO FURTHER DEFECTS NOTED.SDR CHQA201100297Seat Track · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LEFT INBOARD SEAT TRACK 1. MAINTENANCE REPLACED THE LEFT INBOARD SEAT TRACK 1 WITH NO FURTHER DEFECTS NOTED.SDR CHQA201100277Buttstrap · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CENTER BUTT STRAP BETWEEN FRAMES 57-61. MAINTENANCE REPLACED THE CENTER BUTT STRAP BETWEEN FRAMES 57-61 IN ACCORDANCE WITH SRM 51-40-00.SDR CHQA201100271Sign · inoperativeDURING INSPECTION, THE SERVICE DOOR EMERGENCY EXIT SIGN WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE SERVICE DOOR EMERGENCY EXIT SIGN WITH NO FURTHER DEFECTS NOTED.SDR CHQA201100276Frame · crackedDURING INSPECTION, FRAME 10 LEFT SIDE WAS FOUND TO BE CRACKED ON THE UPPER INBOARD SIDE. MAINTENANCE REMOVED THE CRACKED FRAME AND INSTALLED THE NEW FRAME IN ACCORDANCE WITH SRM 51-40-02.SDR CHQA201100268Fitting · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LOWER FRAME BAGGAGE DOOR SHEAR CLIP. THE AIRCRAFT IS STILL IN INSPECTION AND THE FINAL CORRECTIVE ACTION WILL BE SUBMITTED AS A SUPPLEMENT TO THIS REPORT.SDR CHQA201100269Frame · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LEFT CHANNEL FRAME AT FRAME 65 BETWEEN STRINGER 15L AND 16L. THE CORRODED AREA MEASURED 2.9" BY 0.8". MAINTENANCE REPLACED FRAME 65 BETWEEN STRINGERS 15L AND 16L. THE NEW PART WAS INSTALLED WITH A SOLID RIVET ISDR CHQA201100270Beam · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LOWER CARGO DOOR THRESHOLD BEAM BETWEEN FRAMES 65 & 68 AND STRINGERS 14R AND 15R. MAINTENANCE REPLACED THE LOWER CARGO DOOR THRESHOLD BEAM WITH NO FURTHER DEFECTS NOTED.SDR CHQA201100278Floorbeam · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CENTER FLOORBEAM AT FRAME 15. MAINTENANCE REPLACED THE CENTER FLOORBEAM GUSSET AT FRAME 15 IN ACCORDANCE WITH SRM 53-21-10.SDR CHQA201100279Door Frame · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE SERVICE DOOR FRAME 22 BELOW THE LOWER DOOR STOP. MAINTENANCE REPLACED THE SERVICE DOOR FRAME 22 IN ACCORDANCE WITH SRM 51-40-02.SDR CHQA201100267Floor Support · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE MIDDLE TOILET OMEGA BEAM 5 INCHES FORWARD OF FRAME 61. MAINTENANCE REPAIRED THE MIDDLE TOILET OMEGA BEAM IN ACCORDANCE WITH ETD 2011-145-101785 AND SRM 53-21-10.SDR CHQA201100263Support Bracket · crackedDURING INSPECTION, A CRACK WAS FOUND ON THE RIGHT SUPPORT BRACKET AT FRAME 8 AND STRINGER 9R IN THE FORWARD FUSE II SECTION. MAINTENANCE REPLACED THE RIGHT FORWARD FUSELAGE II FRAME 8 ANGLE SUPPORT ABOVE STRINGER 9R IN ACCORDANCE WITH SRM 51-0-02.SDR CHQA201100264Frame · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CHANNEL FRAME AT FRAME 65 BETWEEN STRINGERS 15L AND 16L. THE CORRODED AREA MEASURED 2.9" BY 0.8". MAINTENANCE REPLACED FRAME 65 BETWEEN STRINGERS 15L AND 16L. THE NEW PART WAS INSTALLED WITH A SOLID RIVET IN ACCSDR CHQA201100265Floor Support · crackedDURING INSPECTION, A CRACK WAS FOUND ON THE LEFT OMEGA BEAM BETWEEN FRAMES 23 AND 24 IN CENTER FUSE I. MAINTENANCE REPAIRED THE LEFT OMEGA BEAM BETWEEN FRAME 14 AND FRAME 25 IN ACCORDANCE WITH ETD2011-145-101741.SDR CHQA201100266Unknown · malfunctionedDURING CLIMB, THE FLIGHT CREW REPORTED THAT THE CABIN ALTITUDE BEGAN TO CLIMB. THE AIRCRAFT WAS LEVELED OFF BUT THE CREW WAS UNABLE TO MAINTAIN PRESSURE IN MANUAL MODE. THE QRH WAS FOLLOWED AND THE CREW DESCENDED TO 10,000FT AND WERE STILL UNABLE TO PRESSURISDR CHQA201100262Spar Cap · crackedDURING INSPECTION, A CRACK WAS FOUND ON THE RIGHT WING FRONT SPAR LOWER CAP FROM THE CAP EDGE THROUGH THE SCREW HOLE. THE AIRCRAFT IS CURRENTLY IN C-CHECK INSPECTION.SDR CHQA201100261Light · inoperativeDURING INSPECTION, THE LEFT HAND EXTERIOR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE THE LEFT AFT EXTERIOR EMERGENCY LIGHT WITH NO FURTHER DEFECTS NOTED.SDR CHQA201100260Check Valve · leakingDURING CLIMBOUT, THE FLIGHT CREW REPORTED A BLEED 2 LEAK MESSAGE. THE FLIGHT CREW DE-SELECTED THE NR 2 BLEED SYSTEM AND THE MESSAGE CLEARED. THE AIRCRAFT THEN DIVERTED TO KCMH AND LANDED WITHOUT INCIDENT. DURING TROUBLESHOOTING, MAINTENANCE FOUND THE GROUNDSDR CHQA201100281Frame · crackedDURING INSPECTION, A CRACK WAS FOUND AT FORWARD FUSELAGE II, LEFT AND RIGHT FRAME 10 AT THE INTERSECTION OF THE EMERGENCY ESCAPE HATCH LOWER BEAM. MAINTENANCE REPLACED THE FORWARD FUSELAGE II LEFT (PN: 145-02409-001) AND RIGHT (PN: 145-02409-002) FRAME 10 AT TSDR CHQA201100259Light · intermittentCREW REPORTED THAT UPON ENTERING THE AIRCRAFT THE MIDDLE SECTION OF EMERGENCY FLOOR PROXIMITY LIGHT STRIPS ILLUMINATED. AFTER CYCLING POWER AND PERFORMING AN OPS CHECK OF THE EMERGENCY LIGHTS, THE AFT MOST FLOOR PROXIMITY LIGHT STRIP WOULD ILLUMINATE THEN FADSDR CHQA201100280Skin · dentedDURING INSPECTION, THE RIGHT WING LEADING EDGE II WAS FOUND TO HAVE TWO DENTS ON THE SKIN COUPLED WITH A CRACK ON THE RIGHT LEADING EDGE II RIB. THE TWO DENTS ON THE RIGHT LEADING EDGE SKIN (PN:145-11450-604) COUPLED WITH THE CRACK ON THE RIGHT LEADING EDGE IISDR CHQA201100256Relay · burnedCREW REPORTED THAT DURING FLIGHT RECEIVED A PITOT 3 INOPERATIVE MESSAGE ON THE EICAS FOLLOWED SHORTLY BY AN UNUSUAL ODOR IN THE FLIGHT DECK. THE CREW DIVERTED TO KIAD AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE PITOT 3 CURRENT SENSOR RELAY K0057 AND SSDR CHQA201100250Unknown · malfunctionedCREW REPORTED THAT THE BRAKES FELT "SPONGY" AND THAT THEY WERE NOT HOLDING WELL ON STATIC TAKEOFF. THE FLIGHT CONTINUED WITHOUT INCIDENT. MAINTENANCE PERFORMED OPERATIONAL CHECKS OF THE BRAKING SYSTEMS IAW AMM 32-49-03 AND 32-41-00. OPERATIONAL CHECKS WERE SDR CHQA201100247Yaw Damper · malfunctionedCREW REPORTED DURING CLIMB RECEIVED A RUDDER 1 AND 2 INOPERATIVE MESSAGE, FOLLOWED BY A YAW DAMPER AND AUTOPILOT FAIL MESSAGE ON THE EICAS. RETURNED TO KRDU AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED SUCCESSFUL OPERATIONAL CHECKS OF THE RUDDER SYSTEMSDR CHQA201100248Ahrs · faultyCREW REPORTED THAT DURING FLIGHT RECEIVED AND AILERON MISTRIM MESSAGE AND THAT THE AILERONS WERE BINDING WHILE ATTEMPTING TO TURN RIGHT. THE CREW FORCED THE AILERONS FREE AND THE AIRCRAFT FLEW NORMALLY THE REST OF THE FLIGHT. THE AIRCRAFT LANDED WITHOUT INCISDR CHQA201100246Light · inoperativeDURING INSPECTION, THE FORWARD RIGHT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE FORWARD RIGHT OVERWING EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA201100249Sill · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CABIN FLOOR STRUCTURE FORWARD SERVICE DOOR SILL. MAINTENANCE REPAIRED THE CABIN FLOOR STRUCTURE FORWARD SERVICE DOOR SILL IAW ETD2011-145/101400 WITH NO FURTHER DEFECTS NOTED. THE FINAL CORRECTIVE ACTION AND THE SDR CHQA201100230Recovery Unit · malfunctionedWHILE DESCENDING INTO KCAE ON AUTO PILOT, CREW RECEIVED AND AP MISS TRIM MESSAGE ON EICAS. WHEN THE QUICK DISCONNECT WAS PUSHED INITIALLY THE ROLL CONTROL WAS FROZEN. THE CREW THEN MANUALLY FORCED THE AILERONS OVER TO FREE THEM AND THE AIRCRAFT LANDED WITHOUSDR CHQA201100257Door Frame · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CARGO DOOR CUT OUT STRUCTURE FORWARD L-SHAPE. MAINTENANCE REPAIRED THE CARGO DOOR CUT OUT STRUCTURE FORWARD L-SHAPE IN ACCORDANCE WITH ETD 2011-145-101333. THE CRACKED SECTION OF SHEAR CLIP WAS REMOVED AND A NEW SDR CHQA201100258Floorbeam · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CARGO FLOOR STRUCTURE ENTRANCE AREA LOWER BEAM. MAINTENANCE REPLACED THE CARGO FLOOR STRUCTURE ENTRANCE AREA LOWER BEAM WITH NO FURTHER DEFECTS NOTED.SDR CHQA201100228Splice · brokenDURING INSPECTION THE AFT FLOOR PROXIMITY LIGHT STRIP WAS FOUND TO HAVE A BROKEN SPLICE. MAINTENANCE REPLACED THE SPLICE WITH NO FURTHER DEFECTS NOTED.SDR CHQA201100229O-Ring · leakingCREW REPORTED A BLEED 1 LEAK MESSAGE WHILE CLIMBING OUT OF KORD. THE AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE NR 1 BLEED SYSTEM AND FOUND THE O-RINGS AT JOINTS 5 AND 13 LEAKING. THE O-RINGS WERE REPLACED WITH NO FURTSDR CHQA201100227Actuator · malfunctionedDURING FLIGHT, THE FLIGHT CREW REPORTED THAT THE AILERONS LOCKED IN STRAIGHT AND LEVEL FLIGHT, FOLLOWED BY AILERON MIS-TRIM. THE CREW HAD TO FORCE THE AILERONS TO GET AUTO PILOT TO DISENGAGE. DURING APPROACH, THE AILERONS LOCKED AGAIN BUT THE CREW WAS ABLE TSDR CHQA201100226Windshield · undertorquedWHILE EN ROUTE TO MSY, THE CREW REPORTED A LOUD POP FOLLOWED BY AN EXTREMELY LOUD SQUEALING NOISE. THE CREW WAS NOT COMFORTABLE WITH CONTINUING DUE TO THE NOISE LEVEL, SO THE FLIGHT DIVERTED TO KCMH WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSSDR CHQA201100224Computer · malfunctionedWHILE DESCENDING THROUGH 5,000FT INTO KDCA THE CREW REPORTED AN AILERON MIS TRIM MESSAGE ON EICAS. THE AUTO PILOT WAS THEN TURNED OFF AND REPORTED THAT THE AILERONS WERE LOCKED. THE CREW WAS ABLE TO FREE THE AILERONS BY FORCING THE AILERONS TO MOVE. THE AIRSDR CHQA201100225Feel Unit · malfunctionedDURING THE FLIGHT TO KSDF WITH THE AUTO PILOT ON MEL, THE FLIGHT CREW REPORTED THAT THE AILERONS LOCKED UP SEVERAL TIMES DURING FLIGHT. THE AIRCRAFT LANDED WITHOUT INCIDENT IN KSDF. MAINTENANCE INSPECTED THE AILERON CABLES AND FOUND NO DEFECTS. THE AILERON SDR C2XA11IA119Engine · malfunctionedIAH - CREW REPORTED, RECEIVED ERRONIOUS LAV SMOKE MESSAGE. WENT AWAY AFTER A MINUTE. MAINTENANCE DETERMINED NR 2 ENGINE CREATED IRREGULARITY. REMOVED AND REPLACED NR 2 ENGINE IAW TASK CARD 6271001. AIRCRAFT RETURNED TO SERVICE.SDR CHQA201100223Unknown · odorCREW REPORTED, SHORTLY AFTER TAKEOFF A SMOKE ODOR IN THE CABIN AND THE COCKPIT. A LAVATORY SMOKE INDICATION THEN APPEARED ON THE EICAS. REPORTED THAT AFTER APPROXIMATELY 30 SECONDS THE ODOR AND THE INDICATION BOTH WENT AWAY. THE AIRCRAFT LANDED WITHOUT INCISDR CHQA201100244Frame · crackedDURING INSPECTION, LEFT FRAME 10 WAS FOUND CRACKED AT THE INTERSECTION OF THE DIRECT VISION WINDOW'S LOWER BEAM IN FORWARD FUESLAGE II. MAINTENANCE REPLACED THE CRACKED LEFT FRAME 10 AT THE INTERSECTION OF THE DIRECT VISION WINDOW WITH NO FURTHER DEFECTS NOTESDR CHQA201100245Frame · crackedDURING INSPECTION, RIGHT FRAME 10 WAS FOUND CRACKED A THE INTERSECTION OF THE DIRECT VISION WINDOW'S LOWER BEAM IN FORWARD FUSELAGE II. MAINTENANCE REPLACED THE CRACKED RIGHT FRAME 10 AT THE INTERSECTION OF THE DIRECT VISION WINDOW WITH NO FURTHER DEFECTS NOTSDR CHQA201100222Autopilot Sys · malfunctionedCREW REPORTED THAT DURING CLIMB AT 22,000 FEET, RECEIVED AN AUTO-PILOT AILERON MISTRIM MESSAGE. THEN AT 27,000 FEET RECEIVED AN AUTO-PILOT FAIL MESSAGE. THE PILOT DISENGAGED THE AUTO-PILOT SYSTEM AND REPORTED HE COULD NOT MOVE THE AILERONS AND THAT THE AUTO-SDR CHQA201100253Frame · crackedDURING INSPECTION, THE FORWARD FUSELAGE II LEFT AND RIGHT FRAME 10 WAS FOUND TO BE CRACKED AT THE INTERSECTION OF THE DIRECT VISION WINDOW LOWER BEAM. MAINTENANCE REPLACED THE FORWARD FUSELAGE II LEFT AND RIGHT FRAME 10 AT THE INTERSECTION OF THE DIRECT VISIOSDR CHQA201100251Floor Support · crackedDURING INSPECTION A CRACK WAS FOUND ON THE MID OMEGA BEAM FLANGE ANGLE AT FR47. MAINTENANCE REPAIRED THE MID OMEGA BEAM FLANGE ANGLE AT FR47 IN ACCORDANCE WITH SRM 53-23-02.SDR CHQA201100252Floor Support · crackedDURING INSPECTION A CRACK WAS FOUND ON THE LEFT OMEGA BEAM FLANGE ANGLE AT FR47. MAINTENANCE REPAIRED THE LEFT OMEGA BEAM FLANGE ANGLE AT FR47 IN ACCORDANCE WITH SRM 53-23-02.SDR CHQA201100254Floor Support · crackedDURING INSPECTION, A CRACK WAS FOUND ON THE RIGHT OMEGA BEAM FLANGE ANGLE AT FR 47. MAINTENANCE REPAIRED THE RIGHT OMEGA BEAM FLANGE ANGLE AT FR47 IN ACCORDANCE WITH SRM 53-23-02.SDR CHQA201100255Frame · corrodedDURING INSPECTION, SURFACE CORROSION WAS FOUND ON THE LEFT WINDSHIELD AIRCRAFT FRAME ON THE LOWER OUTBOARD SIDE AROUND THE DOME NUT. MAINTENANCE REPAIRED THE LEFT WINDSHIELD AIRCRAFT FRAME, LOWER OUTBOARD SIDE IN ACCORDANCE WITH ETD2011-145-100872.
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