Allison AE-3007A1/2
Service difficulty reports · 289
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 = 'AE3007A12' 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 = 'AE3007A12' 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 V0XR20101223025Gusset · corroded(V0XR) CTR GUSSET AT FR 59-61 IS CORRODED BEYOND LIMITS. R & R GUSSET. W/C 2087SDR V0XR20101223026Gusset · corroded(V0XR) LT GUSSET AT FR 59-61 IS CORRODED BEYOND LIMITS. R & R GUSSET. W/C 2088SDR V0XR20101223027Gusset · corroded(V0XR) LT SILL AT FR 29-35 IS CORRODED BEYOND LIMITS. R & R GUSSET. W/C 2112SDR V0XR20101223028Gusset · damaged(V0XR) CO-PILOTS LOWER AFT SIDEWALL PANEL IS DAMAGED. R & R SIDEWALL. W/C 2117SDR V0XR20101223029Seat Track · corroded(V0XR) LEFT SEAT TRACK A-3 IS CORRODED BEYOND LIMITS. R & R LT SEAT TRACK. W/C 2121SDR V0XR20101223030Seat Track · corroded(V0XR) RIGHT SEAT TRACK D-3 IS CORRODED BEYOND LIMITS. R & R RT SEAT TRACK. W/C 2133SDR V0XR201012230033Bushing · corroded(V0XR) BUSHINGS AT FWD RUDDER AT PCU-2 CORRODED BEYOND LIMITS. R & R LT SEAT TRACK. W/C 3059SDR C2XA10TY185Inlet · dentedTYS - A/C WAS DESENDING INTO TYS WHEN A BIRD STRUCK THE NR 1 ENGINE INLET. THE CREW CHANGED A/C TO A/C 909 AND CONTINUED ON. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE INLET AFTER BOROSCOPING THE ENGINE. BOROSCOPE REVEAL NO DAMAGE TO THE ENGINE CORE. SDR V0XR201012020001Attach Fitting · cracked(V0XR) LT WING TO BODY FAIRING ATTACHMENT STRIP AT STA 17445.0 - 16143.5 IS CRACKED. REMOVED AND REPLACED STIP. W/C 5063SDR V0XR201012020002Attach Fitting · cracked(V0XR) RT UPPER WING TO BODY FAIRING ATTACHMENT STRIP AT STA 16143.0 - 14967.0 IS CRACKED. R & R STIP. W/C 6009SDR V0XR201012020003Attach Fitting · cracked(V0XR) RT WING TO BODY FAIRING UPPER AFT STRIP IS CRACKED. R & R STIP. W/C 6010SDR CHQA201000219Hose · deterioratedDURING CLIMBOUT FROM CMH THE FLIGHT CREW REPORTED A BLEED 1 OVER TEMP MESSAGE WHILE IN ICING CONDITIONS. THE FLIGHT RETURNED TO CMH WHERE IT LANDED WITHOUT INCIDENT. DURING TROUBLESHOOTING MAINTENANCE FOUND THE RUBBER FLEX LINE GOING TO THE FAN AIR VALVE THESDR V0XR201011290001Sill · corroded(V0XR) SILL AT FRAME 36-42L IS CORRODED BEYOND LIMITS. R & R SILL. W/C 1073SDR V0XR201011290002Sill · corroded(V0XR) SERVICE DOOR SILL IS CORRODED BEYOND LIMITS. R & R SERVICE SILL. W/C 1074SDR V0XR201011290003Sill · corroded(V0XR) LT SILL AT FRAME 19-23L IS CORRODED BEYOND LIMITS. R & R SILL. W/C 1077SDR V0XR201011290004Sill · corroded(V0XR) RIGHT SILL SERVICE DOOR AT FRAME 19-20 IS CORRODED BEYOND LIMITS. R & R SILL. W/C 1084SDR V0XR201011290005Gusset · corroded(V0XR) CENTER FLOOR GUSSET AT FRAME 36-40 IS CORRODED BEYOND LIMITS. R & R GUSSET. W/C 2153SDR V0XR201011290006Seat Track · corroded(V0XR) SEAT TRACK POSITION B BETWEEN FRAME 19-24 IS CORRODED BEYOND LIMITS. R & R SEAT TRACK. W/C 2172SDR V0XR201011260001Gusset · corroded(V0XR) GUSSET AT FRAME 17-18 Y0.0 - LY 479.0 IS CORRODED BEYOND LIMITS. R & R GUSSET. W/C 1087.SDR V0XR201011240001Gusset · corroded(V0XR) CTR GUSSET AT FRAME 19-23 Y0.0 IS CORRODED OUT OF LIMITS. R & R CTR GUSSET. W/C 1081SDR V0XR201011240002Floor Support · corroded(V0XR) RT OMEGA BEAM AT RY 479.0 FRAME 19-25 IS CORRODED OUT OF LIMITS. R & R BEAM. W/C 1082SDR V0XR201011240003Doubler · corroded(V0XR) DOUBLER AT RY 479.0, FRAME 20-22 IS CORRODED OUT OF LIMITS. R & R DOUBLER. W/C 1083SDR V0XR201011240004Floor Support · corroded(V0XR) FWD DIGITAL PLATE AT FRAME 14-16 IS CORRODED OUT OF LIMITS. R & R DIGITAL PLATE. W/C 1086SDR V0XR201011240005Gusset · corroded(V0XR) CTR GUSSET AT FRAME 59-61 IS CORRODED OUT OF LIMITS. R & R GUSSET. W/C 1089SDR V0XR201011240006Gusset · corroded(V0XR) RT GUSSET AT FRAME 59-61 IS CORRODED OUT OF LIMITS. R & R GUSSET. W/C 1090SDR V0XR201011240007Support Angle · corroded(V0XR) SUPPORT ANGLES AT FRAME 19-23 LY 0.0 IS CORRODED OUT OF LIMITS. R & R ANGLE. W/C 1116SDR V0XR201011240008Sill · corroded(V0XR) LT SILL AT FRAME 60-65S CORRODED OUT OF LIMITS. R & R ANGLE. W/C 2108SDR V0XR201011240009Gusset · corroded(V0XR) LT GUSSET AT FRAME 59-61 LY-479.0S CORRODED OUT OF LIMITS. R & R ANGLE. W/C 2109SDR V0XR201011240010Sill · corroded(V0XR) RT SILL AT SERVICE DOOR AT FRAME 22-23 IS CORRODED BEYOND LIMITS. R & R SILL. W/C 1075SDR C2XA10CL184Fmu · faultyORD FLT 5933 THE CREW REPORTED 2 ENGINE SURGE FROM 35 PERCENT TO 75 PERCENT, ITT FLUCUATIONS BETWEEN 285 AND 777 DEGREES IN DESCENT WHEN POWER LEVERS BROUGHT BACK TO IDLE. SURGES ACCURED FOR APPROX 20-30 SECONDS. MAINTENANCE INSPECTED AND REPLACED THE NR 2 ESDR V0XR201011230001Angle · corroded(VOXR) ANGLE ON FRAME 23 RY780.0 POSITION CORRODED BEYOND LIMITS. R & R ANGLE. W/C 1054SDR V0XR201011230002Angle · corroded(VOXR) SCALLOPED ANGLE AT FRAME 23 BETWEEN CTR BEAM AND SILL IS CORRODED BEYOND LIMITS. R & R ANGLE. W/C 1055.SDR V0XR201011230003Sill · corroded(VOXR) SILL FROM FRAME 24-29 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED SILL. W/C 1056SDR V0XR201011230004Sill · corroded(VOXR) LT SILL FROM FRAME 23-29 IS CORRODED BEYOND LIMITS. R & R SILL. W/C 1057SDR V0XR201011230005Sill · corroded(VOXR) LT GUSSET FROM FRAME 23-29 IS CORRODED BEYOND LIMITS. R & R SILL. W/C 1058SDR V0XR201011230006Gusset · corroded(VOXR) GUSSET FROM FRAME 39-46 IS CORRODED BEYOND LIMITS. R & R SILL. W/C 1069SDR V0XR201011230008Floor Support · corroded(VOXR) FLOOR SUPPORT AT FRAME 19-20 IS CORRODED BEYOND LIMITS. R & R SUPPORT. W/C 1080SDR V0XR201011230009Profile · corroded(VOXR) FLOOR SUPPORT ANGLE AT FRAME 19-20 LY 4790. IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED PROFILE. W/C 1085SDR V0XR201011220001Sill · corroded(V0XR) LT SILL AT FRAME 41-48 IS CORRODED BEYOND LIMITS. R & R LT SILL. W/C 1066.SDR V0XR201011220003Gusset · corroded(V0XR)LT GUSSET AT FRAME 39-41 IS CORRODED BEYOND LIMITS. R & R LY GUSSET. W/C 1068SDR V0XR201011220004Sill · corroded(V0XR) RT SILL AT FRAME 36-41 IS CORRODED BEYOND LIMITS. R & R SILL. W/C 1072SDR V0XR201011220005Angle · corroded(V0XR) PAX DOOR ANGLE IS CORRODED BEYOND LIMITS. R & R ANGLE. W/C 1078SDR V0XR201011220006Angle · corroded(V0XR) PAX DOOR ANGLE IS CORRODED BEYOND LIMITS. R & R ANGLE. W/C 1078SDR V0XR201011220007Mount · corroded(V0XR) FWD GALLEY INBD MOUNTS ARE CORRODED BEYOND LIMITS. R & R FITTINGS. W/C 2085SDR V0XR201011220008Angle · corroded(V0XR) RT WING LOWER WING TO FAIRING ATTACHMENT BRACKET IS CRACKED. R & R ANGLE. W/C 6008SDR C2XA10IA309Bleed Valve · inoperativeIAH - FLIGHT 2586 CLIMBING THROUGH 10000 WHILE PERFORMING 2ND PART OF ICE TEST, THE CREW RECEIVED A BLEED 2 VALVE FAIL MESSAGE WITH A BLD 2 VALVE FAIL MESSAGE. THE CREW PERFORMED THE QRH WITH NO HELP, AND THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INSDR V0XR201011120001Frame · corroded(V0XR) SERVICE DOOR LOWER FRAME IS CORRODED BEYOND LIMITS. R & R SERVICE DOOR LOWER FRAME.SDR V0XR201011120002Channel · corroded(V0XR) FWD DIGITAL PLATE FROM RY780.0 - LY780.0 AT FRAME 14-17 IS CORRODED BEYOND LIMITS. R & R DIGITAL PLATE.SDR V0XR201011120003Angle · corroded(V0XR) FWD DIGITAL PLATE FROM RY780.0 - LY780.0 AT FRAME 14-17 IS CORRODED BEYOND LIMITS. R & R REINFORCEMENT ANGLE PLATE.SDR V0XR201011120004Profile · corroded(V0XR) PROFILE AT FRAME 17-18 OTBD OF LY 470.0 IS CORRODED BEYOND LIMITS. R & R PROFILE.
Back to Allison AE-3007A1/2