JASC 7120
Service difficulty reports · 3,030
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 SWIA200820553Mount · corrodedDURING C-CHECK, RIGHT ENGINE AFT THRUST MOUNT CORRODED. REPLACED PER AMM.SDR 08FDEA03996Mount · corrodedNR 1 PYLON, ENGINE AFT ATTACHMENT BEAM LOWER SURFACE INBD AND OUTBD FAYING SURFACES HAVE CORROSION. ABRASIVE BLASTED ENGINE MOUNT IAW AIRBUS A310-200 SRM 51-74-10; PG 208. CONTINUED BLENDING TO REMOVE CORROSION IAW AIRBUS A310-200 SRM 51-74-10. FOUND TO BE SDR SWIA200820523Mount · corrodedDURING C-CHECK, RIGHT ENGINE THRUST MOUNT CORRODED. REPLACED PER AMM.SDR SWIA200820522Mount · corrodedDURING C-CHECK, LEFT ENGINE THRUST MOUNT CORRODED. REPLACED PER AMM.SDR SWIA200820521Mount · corrodedDURING C-CHECK, LEFT ENGINE AFT THRUST MOUNT CORRODED. REPLACED PER AMM.SDR SWIA200820520Mount · corrodedDURING C-CHECK, RIGHT ENGINE THRUST MOUNT CORRODED. REPLACED PER AMM.SDR SWIA200820498Link · corrodedDURING C-CHECK, RIGHT ENGINE FORWARD MOUNT UPPER LINK CORRODED. REPLACED PER AMM.SDR SWIA200820497Fitting · corrodedDURING C-CHECK, LEFT ENGINE AFT THRUST FITTING CORRODED. REPLACED PER AMM.SDR SWIA200820496Fitting · corrodedDURING C-CHECK, RIGHT ENGINE AFT THRUST FITTING CORRODED. REPLACED PER AMM.SDR V0J2008F00001Support · damagedELECTRICAL ARC FROM GROUNDING STUD ON ENGINE SUPPORT FRAME TO SUPPORT FRAME ITSELF. THE SUPPORT FRAME WAS REPLACED WITH NEW IMPROPER BONDING BETWEEN LUG AND SUPPORT FRAME APPEARS TO BE THE CAUSE OF THE ARCING DAMAGE TO THE FRAME. (K)SDR CA080908001Mount · cracked(CAN) CRACKS WHERE TUBES ARE WELDED TO NOSE STRUT. CHAFING WHERE AERO DUCT HOSE TOUCHED MOUNT.SDR SWIA200820452Fitting · corrodedC-CHECK, LEFT ENGINE THRUST FITTING CORRODED. REPLACED PER AMM.SDR SWIA200820451Fitting · corrodedC-CHECK, RIGHT ENGINE THRUST FITTING CORRODED. REPLACED PER AMM.SDR SWIA200820425Fitting · corrodedC-CHECK, LEFT ENGINE THRUST FITTING BEARING AND BALL WORN AND CORRODED, REPLACED.SDR SWIA200820424Fitting · corrodedC-CHECK, RIGHT ENGINE AFT THRUST FITTING BALL CORRODED, REPLACED.SDR KCSA081402Mount · damagedNR 2 PYLON AFT ENG MOUNT HAS 9 HOLES ELONGATED AT WL 145, LAL 1 TO RBL 9 FOR AFT ENG MOUNT BULKHEAD WEB FRAMES ATTACH AT NAC STA 221.9. (S)SDR SWIA200820411Fitting · corrodedC-CHECK, RIGHT ENGINE AFT THRUST FITTING ASSEMBLY CORRODED IN BEARING AREA, REPLACED.SDR SWIA200820458Mount · corrodedC-CHECK, RIGHT ENGINE AFT THRUST MOUNT FITTING CORRODED. REPLACED PER AMM.SDR COMA086353Support Beam · crackedRT UPPER WEB-ENG SUPPORT BEAM ASSEMBLY CRACKED. COMPLIED WITH REPAIR TO UPPER WEB-ENG SUPPORT. BEAM ASSEMBLY BETWEEN BL 27.5 AND 36.2 PER REO601R-53-61-569. (S)SDR COMA086352Support Beam · crackedLT UPPER WEB-ENG SUPPORT BEAM ASSEMBLY CRACKED. COMPLIED WITH REPAIR TO UPPER WEB-ENG SUPPORT. BEAM ASSEMBLY BETWEEN BL27.5 AND 36.2 PER REO601R-53-51-569. (S)SDR SWIA200820403Fitting · corrodedC-CHECK, RIGHT ENGINE THRUST FITTING CORRODED, REPLACED.SDR SWIA200820402Bushing · corrodedC-CHECK, LEFT ENGINE FORWARD MOUNT YOKE FLANGED BUSHING CORRODED, REPLACED.SDR SWIA200820401Bushing · corrodedC-CHECK, RIGHT ENGINE FORWARD MOUNT YOKE FLANGED BUSHINGS CORRODED, REPLACED.SDR SWIA200819925Bushing · corrodedLT ENGINE FWD MOUNT LINK AND BUSHINGS ARE CORRODED. REPLACED LT ENGINE LINK AND BUSHINGS IAW AMM 71-00-00.
SDR SWIA200820357Bearing · corrodedC-CHECK, RIGHT ENGINE FORWARD YOKE MOUNT LINK BEARING CORRODED. REPLACED.SDR SWIA200820356Mount · corrodedC-CHECK, LEFT ENGINE FORWARD YOKE MOUNT LINK BEARING CORRODED. REPLACED.SDR SWIA200820334Fitting · corrodedC-CHECK, LEFT ENGINE THRUST FITTING CORRODED, REPLACED.SDR SWIA200820333Mount · corrodedDURING C-CHECK, RIGHT ENGINE THRUST MOUNT CORRODED, REPLACED.SDR 2008FA0000521Mount · crackedDURING A PHASE 2, 200 HR INSP, A CRACK WAS FOUND ON THE LT ENGINE MOUNT UPPER IB COWLING BRACKET. THE CRACK EXTENDED FROM THE TOP OF THE WELD AND WAS APPROXIMATELY 1 INCH IN LENGTH. THE ADJACENT AREAS DID NOT APPEAR DAMAGED.. TECH SUPPORT WAS CONTACTED AND SDR SWIA200820400Bushing · corrodedC-CHECK, LEFT ENGINE YOKE BUSHING CORRODED, REPLACED.SDR SWIA200820399Fitting · corrodedC-CHECK, LEFT THRUST FITTING CORRODED, REPLACED.SDR F3LA200800491Fitting · crackedDURING C-CHECK INSP NOTED THE NR 1 ENGINE PYLON PANEL NR 413CL MOUNTS STRUCTURE WAS CRACKED AT AFT UPPER SCREW HOLE. MAINT REPAIRED NR 1 ENGINE PYLON PANEL NR 413CL MOUNT STRUCTURE AT AFT UPPER HOLE IAW SRM 54-52-12 AND 51-42-11. UPON COMPLETION OF THE REPAIR SDR CA080710004Mount · deformed(CAN) DURING ENGINE INSPECTION NOTED THAT THE LT AND RT FORWARD ENGINE MOUNTS WERE SAGGING TO THE POINT THAT DURING TAKEOFF POWER ON ENGINE AND INTAKE PIPE HOSE CLAMP MADE CONTACT WITH THE UPPER PORTION OF ENGINE MOUNT. THE LORD MOUNT APPEARED TO BE SAGGING/DSDR DALA1120720922Latch · unknownENGINE UPPER COWL DOOR LATCH REPLACED IAW EA 09-056907-12, ME05.SDR SWIA200820263Bearing · corrodedLT FORWARD ENGINE MOUNT YOKE LINK ASSEMBLY CORRODED ON UPPER BEARING (C-CHECK). REPLACED MOUNT.SDR SWIA200820273Fitting · corrodedRIGHT ENGINE REAR MOUNT THRUST FITTING BALL END CORRODED (C-CHECK). REPLACED BALL END.SDR SWIA200820272Fitting · corrodedLEFT ENGINE REAR MOUNT THRUST FITTING SPHERICAL BALL END CORRODED (C-CHECK). REPLACED BALL END.SDR SWIA200820271Spherical Bearin · corrodedLEFT ENGINE FORWARD MOUNT UPPER LINK SPHERICAL BEARING IS CORRODED (C-CHECK). REPLACED BEARING.SDR 08FDEA02252Mount · corrodedNR 2 ENGINE FORWARD MOUNT SPIGOT HOLE CORRODED REMOVED LEVEL 1 CORROSION. ACCOMPLISHED BUSHING REPAIR ON NR 2 ENGINE FORWARD MOUNT SPIGOT HOLE PER FED EX EA6-5450-121268.SDR SWIA200819932Fitting · corrodedLT AND RT ENGINE AFT THRUST FITTINGS HAVE SIGNS OF CORROSION. (FOUND AT C-CHECK) REPLACED THRUST FITTINGS IAW AMM 71-22-01-400-801.
SDR S9BA2008021Mount · failedRT SPINNER NOTED MISALIGNED. REMOVED AND REPLACED TOP ENGINE MOUNT INSPECTED ALL RIGGING AND WIRING. EMERGENCY MEASURES EXECUTED, RETURNED TO DOCK. AIRCRAFT GROUNDED, RETURNED TO SERVICE NEXT DAY. FLIGHT NR 189SDR T652008F00000Mount · damagedDURING AIRCRAFT CORROSION INSPECTION IT WAS NOTICED THAT THE AIR CONDITIONING CONDENSER DUCT CLAMP WAS CUTTING INTO THE ENGINE MOUNT ON THE LT TRUSS. THE TRUSS WAS ALSO RUBBING AGAINST THE CONDENSER DUCT. THERE ARE (4) CUTS MEASURING AS FOLLOWS: ( LENGTH 9/3SDR HNAA0800156Mount · wornNR 1 INBOARD AFT VERTICAL MOUNT STRUT BEARING WORN. INSP GENERATED BY RII CARD 71-20-03.SDR HNAA0800155Mount · brokenNR 1 ENGINE AFT OUTBOARD STRUT MOUNT FOUND TO BROKEN. INSP GENERATED BY INSPECTION CARD 71-20-03.SDR SWIA200819855Mount · corrodedLT ENGINE MOUNT THRUST FITTING IS CORRODED. (FOUND AT C-CHECK) REPLACED THRUST FITTING ON IAW AMM 71-22-01-400-801.
SDR SWIA200819854Mount · corrodedRT AFT ENGINE MOUNT THRUST FITTING IS CORRODED. (FOUND AT C-CHECK) REPLACED THRUST FITTING IAW AMM 71-22-01-400-801.
SDR 2008FA0000281Mount · crackedINSP FOUND UPPER LT BRACKET (0513132-11) WITH A SMALL CRACK ORIGINATING FROM THE LOWER EDGE OF THE ENGINE MOUNT BOLT WASHER. ONLY A SMALL BEND LINE WAS VISIBLE FROM THE COCKPIT SIDE OF THE BRACKET VIA BOROSCOPE. AFTER REMOVAL OF THIS BRACKET A CRACK WAS CLEASDR SWIA200819711Bushing · corrodedRT ENGINE MOUNT BUSHINGS ARE CORRODED. (FOUND AT C-CHECK) REPLACED BUSHINGS AS REQUIRED.SDR SWIA200819709Bushing · corrodedLEFT ENGINE FORWARD MOUNT BUSHINGS ARE CORRODED. (FOUND AT C-CHECK) REPLACED BUSHINGS ON MOUNT.SDR 2008FA0000202Mount · wrong partAN UNKNOWN AMOUNT OF AC FIREWALL ATTACH ASSEMBLIES (ENGINE MOUNTS) THAT WERE NOT FAA-PMA APPROVED. THE MIDO ATTEMPTED TO CONTACT THE OWNER OF MFG CONCERNING THIS MATTER, HOWEVER, ALL PHONE CALLS WERE NOT RETURNED, AND CERTIFIED LETTERS NOT ACCEPTED. AS OF THIS
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