JASC 7120
Service difficulty reports · 3,029
Reports filed under 7120 · Engine Mount Section, newest first.
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 jasc_code = '7120' 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 jasc_code = '7120' 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 DALA2019050890004Link · damagedPD: WHILE INSPECTING THE PN 310T1032-3 LINK, DAMAGE WAS FOUND COMMON TOTHE BEARING BORE THAT WAS BEYOND THE LIMITS. CA:PRI 576880-14 WAS ISSUED TO MACHINE THE SUBJECT BORE TO COMPLETELY. REMOVE THE DAMAGE. PART WAS FPI'ED AND SLEEVES WERE MANUFACTURED AND INSTSDR ASOA201901307023Yoke · crackedNR 1 ENGINE FORWARD YOKE, LOWER FORWARD FITTING CRACKED ON RADIUS EDGE. REMOVED AND REPLACED YOKE FITTING. AIRCRAFT STILL IN C CHECK.SDR QEMY2019021300001Nut · looseINCOMING INSPECTION DEFECT REPORT FORM. AFT MOUNT LEFT HAND LINK INNER NUT BACKED OFF TO COTTER PIN. COTTER PIN EXHIBITS DAMAGE FROM THE NUT.SDR QEMY2019010700000Lock Nut · looseENGINE AT THE SHOP, ON INCOMING PROCESS OF THE ENGINE, 5 OUT OF 6 LOCKNUTS/COVERS FOUND TO BE HAND TIGHT ON DISASSEMBLY OF THE FRONT MOUNT SHACKLE FROM THE FHF.SDR FDEA201812283613Mount · corrodedNR 2 ENGINE FWD MOUNT , FORWARD INBOARD ATTA COMPLY WITH E..A. 6-5451-T0344330 REV NO. POS. P1 EA. T6-5451-T0344330. CORROSION REMOVAL OF OVER SIZE HOLE EA TO ADDRESS REPAIR. EXCEDED MAX OVER SIZE HOLE PER SRM.SDR CA190322007Bushing · missing(CAN) DURING MAINTENANCE IT WAS DISCOVERED A MISSING BUSHING AND DAMAGE TO THE FORWARD ENGINE MOUNT SYSTEM OF BR710 A2-20 ENGINE 13134 ON AIRCRAFT 9016 (RIGHT HAND SIDE). THE MISSING BUSHING WAS INFORMED TO BE PART NUMBER BRR15808. ROOT CAUSE: IT IS CONFIRMESDR 2020FA0000068Sealant · out of toleranceAFTER REMOVAL OF RIGHT HAND ESN 16030, IT WAS NOTED THAT THE FIREBOX COVER HAD WHAT LOOKS TO BE THE WRONG SEALANT PREVIOUSLY USED. THE CORRECT SEALANT TO BE USED IS MIL-S-38249 PS 700 PART B SEALANT COMPOUND, FIREWALL. THE ON-SITE TECHNICIAN REVIEWED THE ENGSDR AALA201812189025Mount · corrodedRIGHT ENGINE NR 2 AFT MOUNT HAD CORROSION. REPLACED THE ENGINE MOUNT IAW 71-22-11-0401-13, AND 71-22-11-400-010-A.SDR AALA201812089003Mount · corrodedAIRCRAFT WAS GROUNDED: LEFT ENGINE AFT MOUNT HAS EVIDENCE OF SURFACE CORROSION. REPLACED AFT MOUNT AS REQUIRED.SDR SIMA2018121016007Mount · crackedRH ENGINE PYLON FWD LOWER YOKE CRACKED-C/A-REMOVED AND REPLACED RH FWD LOWER YOKE IAW EO EM-54MR-698SDR ASOA201811147181Mount · crackedTYS A/C IS IN FOR A C-CHECK INSPECTION WHEN INSPECTORS FOUND THE NR 2 ENG. FORWARD LOWER YOLK CRACKED. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE LOWER FORWARD YOLK IAW ECTC EA 26-2014-063-01. A/C WILL BE RELEASED AT THE END OF THE CHECK.SDR SIMA201812050004Yoke · crackedRH PYLON FWD LOWER PYLON YOKE HAS CRACK.-C/A-REMOVED AND REPLACED RH PYLON FWD LOWER PYLON YOKE IAW ENVOY ERS-EM-54MR-698.SDR DALA2018120390008Mount · damagedONE OF THE TWO LUG BORE HOLES WAS FOUND TO MEASURE 1.484 INCHES AFTER THE DAMAGE CLEANUP IN ORDER TO REMOVE ALL DEFECTS. THIS EXCEEDS THE MAX. MANUFACTURER WAS CONTACTED AND PROVIDED INSTRUCTIONS TO CONTINUE REPAIR WITH AN OVERSIZED BUSHING. PRI 573062-14 WASSDR DALA2018112769007Mount · mismanufacturedPD:FORWARD ENGINE MOUNT BEAM WAS MACHINED BELOW THE REPAIRABLE LIMIT CA:NICKEL PLATE, MACHINE AND CHROME PLATE THE SHAFT END JOURNAL (REF BOEING MESSAGES DAL-DAL-18-2400-03B AND DAL-DAL-17-1932-04B) PER ER/A 572716-14SDR DALA2018110890006Mount · damagedPD:LINK ASSEMBLY, AFT MOUNT WAS FOUND WITH A THICKNESS OF 0.725 INCH WHICH IS BELOW THE MINIMUM THICKNESS ALLOWED OF 0.735 INCH CA:REPAIR PER ER/A 572417-14.SDR SIMA2018102926005Fitting · crackedLT ENG FWD YOKE LOWER FWD FITTING CRACKED. C/A-COMPLETE:ERS-EM-54MR-698 FOR CRACKED LT ENGINE FORWARD YOKE LOWER FORWARD FITTING SATISFACTORILY ACCOMPLISHED.SDR ASOA201809265285Fitting · corrodedRT ENGINE AFT PRODUCTION DUCT FRETTING. REPAIRED PER REO 601R-71-22-026 REV NC DATED 2004-10-05.SDR RAIA2018101210007Fitting · crackedNR 2 ENG PYLON YOKE LOWER FWD LINKAGE FITTING HAVE SIGNIFICANT CRACK INDICATION IN BEND RADIUS. DETAILS FOR THIS REPAIR HAVE BEEN EMAILED TO 9-AMC-SDR-PROGMGR@FAA.GOV, WITH SUBJECT 10156 SDR RAIA201809110007.SDR RAIA2018101210006Fitting · crackedNR 1 ENG PYLON YOKE LOWER FWD LINKAGE FITTING HAVE SIGNIFICANT CRACK INDICATION IN BEND RADIUS. DETAILS FOR THIS REPAIR HAVE BEEN EMAILED TO 9-AMC-SDR-PROGMGR@FAA.GOV, WITH SUBJECT 10156 SDR RAIA201809110006.SDR SIMA2018092611003Yoke · crackedR/H ENGINE FWD LOWER YOKE CRACKED. -C/A-REMOVED AND INSTALLED SERVICEABLE YOKE IAW EO EM-54MR-386SDR ASOA201809057160Yoke · crackedNR 1 ENGINE LOWER FORWARD YOKE HALF CRACKED. REMOVED AND REPLACED NR 1 ENGINE FOWARD LOWER YOKE FITTING IAW EA 26-2014-063.SDR ASOA201808257154Yoke · crackedDURING A C-CHECK INSPECTION FOUND THE L/H ENGINE UPPER FORWARD ENGINE YOKE CRACKED. MAINTENANCE REMOVED AND REPLACED THE YOLK FITTING IAW EC/TC EA 145-2018-125. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.SDR SIMA2018082715005Yoke · crackedLEFT ENGINE FWD LOWER PYLON YOKE WAS CRACKED. REMOVED AND REPLACED THE LT FORWARD LOWER PYLON YOKE FITTING IAW EO EM-54MR-386.SDR ASOA201808157148Yoke · crackedACFT WAS IN FOR AN A-CHECK WHEN INSPECTION FOUND THE NR 1 ENGINE FORWARD YOKE LOWER MOUNT ATTACH POINT FWD. FITTING CRACKED. MAINTENANCE REMOVED AND REPLACED THE ENGINE YOKE IAW EA 26-2014-063.ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECKSDR COEA2018082215805Fitting · damagedLT ENGINE INBOARD AFT MOUNT FITTING AT JUNCTION OF TUBES 1 & 2 WAS DAMAGED. REPAIED IAW ES-3657/18.13301.SDR GR4D20180711001Link Assy · crackedLEFT ENGINE TO FUSELAGE ENGINE MOUNT LINK ASSY WAS FOUND TO BE CRACKED DURING CMP G550 712137 DURING EDDY CURRENT INSPECTION P/N 1159BM51245-3 S/N J045312-001 REFERENCE DRAWING 1159P51300.SDR SIMA2018071910002Yoke · crackedLT ENGINE FORWARD NR 1 YOKE CRACKED LOWER END OUTBOARD SIDE. REMOVED AND REPLACED LT LOWER FORWARD YOKE FITTING IAW EO EM-54MR-386.SDR ASOA201806267115Fitting · crackedTYS A/C IS IN FOR A C-CHECK WHEN INSPECTION FOUND THE LEFT HAND ENGINE FWD LOWER YOLK FITTING CRACKED. MAINTENANCE R&R THE FITTING IAW CARD NUMBER EAZ6-2014-063. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.SDR DALA201806200001Mount · damagedDURING ACCOMPLISHMENT OF REPAIR 3-2 PER DAL CMM 310T1020-3 ATA 71-21-11, AFTER REMOVAL OF ALL DAMAGE BEARING LUG INDEX 14 WAS FOUND TO MEASURE 0.714 INCH, WHICH IS 0.021 INCH BELOW THE MINIMUM DIMENSION GIVEN IN FIGURE 601, SHEET 2. ADDITIONALLY, ATTACH LUG INSDR DALA201805239999Bushing · mismanufacturedDURING ACCOMPLISHMENT OF BOEING CMM 310T1020-3 (71-21-11) REPAIR 3-1, BUSHING REPLACEMENT, DTO WAS UNABLE TO ACHIEVE THE DIMENSIONAL REQUIREMENTS OF THE BUSHINGS. BOEING WAS CONTACTED FOR PART DISPOSITION AND RESPONDED WITH MESSAGE NUMBER DAL-DAL-18-0654-06B ISDR CHIR201805163302Mount · wornDURING RAMP CHECK, DISCOVERED THAT NR 1 ENGINE AFT LATERAL ENGINE MOUNT LINK ASSEMBLY HAD MOVEMENT ON THE OUTBOARD END RELATIVE TO THE AIRFRAME STRUCTURE. DETERMINED THAT THE AFT LATERAL ENGINE MOUNT TOP AND BOTTOM AIRFRAME ANGLES HAD ENGINE MOUNTING HOLES WHISDR DALA2018070390003Fitting · corrodedCORROSION FOUND. CORROSION REMOVED REF SHOP ORDER OG1103BCMM 310T1020-3, 71-21-11 REV 57 DTD 02/07/2018,OEM REV 32 DTD11/01/2017.SDR SIMA2018053109008Yoke · crackedLEFT ENGINE FWD LOWER YOKE WAS CRACKED. REPLACED THE LT ENGINE FWD LOWER YOKE IAW EO EM-54MR-386.SDR ASOA201804187066Mount · damagedDURING A C-CHECK, THE RT SIDE ENGINE YOLK FWD. UPPER AFT FITTING HAS MECHANICAL DAMAGE INSIDE THE HAT BUSHING OF THE YOLK FITTING. MAINTENANCE REMOVED AND REPLACED THE YOLK FITTING IAW EA48-2018-026.SDR ASOA201804107057Yoke · crackedNR 1 ENGINE FORWARD YOKE, FORWARD UPPER LUG INNER FITTING CRACKED. REMOVED AND REPLACED YOKE FITTING. AIRCRAFT STILL IN MAINTENANCE.SDR ASOA201804107056Yoke · crackedNR 2 ENGINE FORWARD YOKE, LOWER FORWARD LUG FITTING CRACKED. REMOVED AND REPLACED CRACKED YOKE FITTING. AIRCRAFT STILL IN MAINTENANCE.SDR ASOA201803247036Yoke · cracked#1 ENGINE PYLON LOWER FORWARD YOKE CRACKED. REMOVED AND REPLACED FORWARD YOKE. AIRCRAFT STILL IN C CHECK.SDR FDEA201803070626Mount · corrodedNR 1 ENG FWD PYLON MOUNT HAS CORROSION IN BOLT HOLES. CLEANED NR 1 FWD ENGINE MOUNT HOLES IAW AMM 12-21-11-00, NO DAMAGE NOTED, REAMED AFT OUTBD HOLE TO DIA. 0.957" AND REMOVED CORROSION FOUND TO BE IN LIMITS IAW SRM 54-51-86 FIG 104, REPAIRED AFT INBD HOLE IASDR CHIA201803073174Support Angle · crackedDURING ENGINE REPLACEMENT, CRACK WAS FOUND IN AFT ENGINE SUPPORT ANGLE, NR 2 ENGINE.SDR SIMA20180208003Yoke · crackedLEFT ENGINE FORWARD YOKE I RADIUS CRACKED. COMPLIED WITH EO-EM-54MR-386.SDR ASOA201802054007Link · crackedDURING A MAINTENANCE INSPECTION, THE RIGHT FWD PYLON, FORWARD LOWER YOKE LINK WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LINK AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR RAIA201801240002Yoke · crackedLEFT PYLON, FWD LOWER ENGINE YOKE, FWD BRACKET IS CRACKED. R & R THE YOKE FITTING.SDR AALA201801249001Mount · corrodedCORRODED AFT ENGINE MOUNT SHEAR PINS. REPLACED AFT ENGINE MOUNT IAW AMM 71-22-11-400.SDR RAIA201801120002Mount · crackedRIGHT ENGINE FWD YOKE LOWER FWD FITTING CRACKED. R & R THE RT ENGINE FWD YOKE LOWER FWD FITTING.SDR ASOA201801267003Yoke · crackedDURING INSPECTION AT TYS, THE NR 2 ENGINE FWD PYLON UPR LINKAGE FITTING WAS FOUND CRACKED. THE CRACK MEASURED .20" IN LENGTH LOCATED ALONG THE INNER FLANGE, NEAR THE WEB RADIUS. REPLACED UPR FWD YOKE FITTING FOR THE NR 2 ENGINE.SDR YENA201712161010Mount · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE NR 2 ENGINE AFT MOUNT. CORRODED INNER BORE OF FOUR OUTER PINS. R & R THE AFT ENGINE MOUNT AND PINS IAW IAW AMM 71-22-11.SDR YENA201712161009Mount · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE NR 1 ENGINE AFT MOUNT. CORRODED ON INNER BORE OF FOUR OUTER PINS. R & R THE NR 1 ENGINE AFT MOUNT AND THREE INNER AND OUT PINS IAW AMM 71-22-11.SDR RAIA201711290003Yoke · crackedRH ENG FWD MOUNT LOWER YOKE FITTING IS CRACKED. R & R RH ENG FWD MOUNT LOWER YOKE FITTING.SDR RAIA201711290002Yoke · crackedLH ENG FWD MOUNT LOWER YOKE FITTING IS CRACKED. R & R LH ENG FWD MOUNT LOWER YOKE FITTING.SDR DALA2017113008384Pin · damagedDURING ACCOMPLISHMENT OF CMM 310A2020 ON THE ENGINE MOUNT ASSY PIN HAD TO BE GROUND TO 0.862 INCH 0.0025 INCH BELOW MINIMUM IN-PROCESS OF 0.8645 INCH IN ORDER TO REMOVE PREVIOUS PLATING AND TWO ADDITIONAL PAWL PINS HAD TO BE GROUND TO 1.235 INCHES, 0.003 I
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