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 C2XA09TY257Yoke · crackedNR 1 ENGINE FWD LOWER INBD YOKE HAS A CRACK. REMOVED AND REPLACED THE YOKE IAW EMB EC5450-01028.SDR SWIA200922494Pin · corrodedBOTH FORWARD MOUNT PINS AND YOKE BEARINGS FOR LEFT ENGINE HAVE PITTING CORROSION. (SVC CHECK) REPLACED PINS.SDR ABXR200908240010Support Fitting · damagedDURING THE REPETITIVE NR 3 ENG SUPPORT FITTING INSP IAW SB 2000-5410A01, AD 2005-19-24, HOLES I, J, K AND L WERE VISUALLY FOUND ELONGATED AND THE HOLES WERE FOUND PREVIOUSLY OVERSIZED TO MAX ALLOWABLE DIA. 0.2817 INCH. FABRICATED FREEZE PLUGS FROM 15-5PH H1025SDR CA090818006Bolt · brokenWHILE THE ENGINEER WAS CARRYING OUT A DAILY INSP, FOUND HALF A BOLT WITH NUT ATTACHED ON ENG DECK. FURTHER INVESTIGATION REVEALED THAT BOLT (ONE OF TWO) WAS PART OF THE ATTACHMENT OF THE PILLOW BLOCK ASSY TO THE ENG BIPOD MOUNT ASSY. PART OF THE BOLT APPEARESDR CA090721003Mount · cracked(CAN) NOTICED WORKING ENGINE MOUNT. INSPECTED ATTACHMENT BOLT FOR TORQUE AND FOUND IT PROPERLY TORQUED. LIFTED AFT END OF ENGINE AND FOUND MOVEMENT ON FIREWALL ATTACHMENT SIDE OF ENGINE MOUNT LEG AND UNDER CLOSER INSP FOUND IT CRACKED TWICE TO BOLT HOLE. REPLSDR C2XA09SH201Mount · crackedDURING C-CHECK ENG NR 2 FWD YOKE LWR MOUNT CRACKED. MX PERFORMED AND COMPLETED REPAIR OF NR 2 FWD YOKE LWR MOUNT IAW EC5450-01027. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR CA090714006Mount · corroded(CAN) UPON ENG CHANGE AND GOING THROUGH THE INSP OF ALL PARTS THAT WILL BE RE-INSTALLED WITH NEW ENG IT WAS DISCOVERED THAT THE AFT ISOLATOR MOUNT WAS BADLY FRET. FURTHER INVESTIGATION REVEALS THAT THESE UNITS HAVE 3 BOLTS WITH SAME DIAMETER AND 2 DIFFERENT LSDR NWAA092463251Mount · gougedDURING "M" CHECK FOUND GOUGE IN NR 1 ENGINE AFT MOUNT. REPAIRED PER EA 32-216283 SECTION I. SECTION II DAMAGE TOLERANCE ANALYSIS FOR REPETITIVE INSPECTIONS TO BE ACCOMPLISHED BY AIRBUS BY DEC 06, 2009.SDR 2009FA0000552Mount · corrodedRT LWR OTBD ENGINE MOUNT WING FITTING IS CORRODED- INSTALL SERVICEABLE PART.SDR C2XA09TY120Fastener · looseNR 2 ENGINE FWD MOUNT YOKE O/B PLATE HAS SEVERAL LOOSE FASTENERS. REMOVED AND REPLACED 13 LOOSE JO-BOLTS IAW EMB 145 SRM 51-40-02. AIRCRAFT RELEASED AND RETURNED TO SERVICE.SDR SWIA200921795Link · corrodedRIGHT ENGINE UPPER YOKE LINK AND BUSHING CORRODED. (ENG CHG) REPLACED LINK AND BUSHING.SDR HALA2009061500251Isolator · gougedGOUGE ON NR 2 ENGINE FWD UPPER ISOLATOR. REMOVED AND REPLACED NR 2 FWD UPPER ISOLATOR PER TASK 71-20-05-000-801, 71-20-05-400-801.SDR CA090526007Pedestal · corroded(CAN) 2 CORRODED LINES WERE FOUND IN THE CONICAL AREA. ONE ON THE RT SIDE FOR 50 PERCENT OF THE CIRCUMFERENCE AND ONE ON THE LT SIDE FOR 33 PERCENT OF THE CIRCUMFERENCE.SDR CA090522002Tripod · cracked(CAN) WELD ON LEG OF ENGINE MOUNT CRACKED (SHORT LEG)SDR SWIA200921621Mount · corrodedRIGHT ENGINE FORWARD MOUNT CORRODED. ENG CHANGE, REPLACED MOUNT.SDR DL76G090868Mount · damagedDURING IFSD INSP FOUND THE FWD OTBD ENGINE MOUNT DAMAGED. REPLACED ENGINE MOUNT.SDR CA090521003Tripod · cracked(CAN) WELD ON LEG OF ENGINE MOUNT CRACKED.SDR 2009FA0000361Mount · corrodedENGINE MOUNT SHOWED PIN HOLES ON LOWER OUTER TUBE. REMOVED PAINT AND FOUND CORROSION. REPAIRED 13 TUBES. (K)SDR CA090430002Mount · cracked(CAN) THE ENGINE MOUNT WAS FOUND CRACKED IN THE UPPER RT MOUNT TO ENGINE ATTACH AREA.SDR UALA2009042401193Mount · shearedNR 1 ENG LOWER ISOLATION PACK BOLT SHEARED OFF AND LAYING ON UNISON RING. TRIED TO REMOVE SHEARED BOLT FROM MOUNT UNABLE TO ACP. SHIM PACK AND SHEARED BOLT HEAD PACKAGED AND ON FLIGHT DECK. REPLACED NR 1 ENG LOWER FWD ENG MOUNT. ACP'D INSP OF FWD ENG MOUNTSDR DLM88090672Mount · chafedNUMBER ONE AFT LOWER MOUNT LUG CHAFING. REPAIRED PER ERA 46119-14 REV ORG BY BLENDING AND HFEC INSPECTION OF NACELLE REAR SPAR LOWER CAP AT STATION 1380. REMAINING MATERIAL .232 AND .231.SDR FDEA200904151301Mount · corrodedNR 2 PYLON ENGINE FWD MOUNT BOTH AFT FASTENER HOLES CORRODED, 6 SQ IN REMOVED LEVEL 1 CORROSION. FABRICATED AND INSTALLED REPAIR BUSHINGS ON NR 2 PYLON FWD MOUNT AFT FASTENER HOLES IAW FEDEX EA6-5450-124253. RELEASE DATE 8 APRIL, 2009SDR DLM88090657Mount · wornTHE NACELLE REAR SPAR LOWER CAP AT FS 1380, NR 2 ENGINE AFT MOUNT LUG WAS FOUND WITH CHAFING ON THE FACES. THE WEAR WAS BLENDED AND FOUND ACCEPTABLE TO BOEING.SDR DLM88090656Mount · wornTHE NACELLE REAR SPAR LOWER CAP NR 1 ENGINE AFT MOUNT LUG WAS FOUND WITH CHAFING. THE CHAFING WAS BLENDED AND FOUND TO BE ACCEPTABLE TO BOEING.SDR CA090513003Mount · corroded(CAN) AT INSPECTION THE NR 2 AND 3 POSITION OTBD LOWER ENGINE TRUSS MOUNTS WERE FOUND TO HAVE CORROSION PITTING BEYOND ACCEPTABLE LIMITS. THE UNITS WERE REPLACED IAW THE MFG MM INSTRUCTIONS.SDR DL757090654Mount · gougedNR 2 PYLON FWD OTBD ENG MOUNT HOLE INNER BORE IS DAMAGED GOUGED AT HOLE OPENING LWR SIDE AND HAS GROOVE (RING) IN CENTER OF BORE. C/W AT SAA - SAT ON N/R 118549 SAA JOB 82635410001 COMPLIED WITH ER/A 473675-14 REV 0.SDR SWIA200921956Pin · failedRIGHT ENGINE FORWARD MOUNT PINS FAIL DIMENSION CHECK. (C-CHECK) REPLACED PER AMM.SDR 2009FA0000284Mount · crackedTROUBLESHOOTING A TRACKING DISCREPANCY, IT WAS FOUND THAT THE RT FWD MOUNT LOCATION OF THE PYLON HAD CRACKED AS WELL AS THE GUSSET. THE CRACK WAS NOT VISIBLE THROUGH THE UPPER SIDE PANELS JUST BELOW THE FUEL TANKS. THE CRACK WAS NOT FOUND UNTIL THE FUEL TANKSDR SWIA200921348Bushing · corrodedFLT 6097 - LEFT ENGINE LINK ASSEMBLY BUSHINGS CORRODED. REPLACED PER AMM.SDR 22AA20090501Mount · damagedFOUND AT AFT SECTION EXTENSIVE DAMAGE IN AFT PYLON AND NACELLE STRUCTURE, BY DEBRIS FROM ENGINE. REMOVED AND REPLACED AT AFT ENGINE MOUNT, TAIL PYLON TORQUE BOX IAW DC-10 DRAWING AVB7050 AND AVB 7326. REPLACED FASTENERS IAW DC-10 SRM 51-31-00 PAGE 1 TO 15 RESDR UALA2009032500884Clevis · wornNR 2 ENGINE AFT ENGINE MOUNT OUTBOARD CLEVIS HAS A WORN AREA ON INNER, AFT SURFACE. CONTINUED INSTALLATION OF AFT ENGINE MOUNT. NEED TO COMPLETE TORQUE AND SAFETY OF ALL MOUNT BOLTS.SDR 2009FA0000248Mount · debondedDURING NR 1 ENGINE REMOVAL FROM ACFT, FOUND NR 1 ENGINE ISOLATOR MOUNT ALIGNMENT PUCK DEBONDED AND SEPARATED FROM THE MAIN BODY OF THE ISOLATOR. (K)SDR USAA2009032490669Mount · corrodedPHL - ENGINE CHANGE - MAJOR REPAIR - NR 1 ENGINE AFT MOUNT AFT MOUNT SHOWING SIGNS OF SURFACE CORROSION. REPAIRED NR 1 ENGINE AFT MOUNT IAW US AIRWAYS EA 112487.SDR USAA2009032490668Mount · corrodedPHL - ENGINE CHANGE - MAJOR REPAIR - NR 1 ENGINE FWD MOUNT MATING SURFACE SHOWING EVIDENCE OF CAD PLATING MISSING AND CORROSION. REPAIRED NR 1 ENGINE FWD MOUNT IAW US AIRWAYS EA 112487.SDR SWIA200921576Bearing · corrodedRIGHT ENGINE THRUST FITTING BEARING CORRODED ON INNER SURFACE. SB COMPLIANCE, REPLACED FITTING.SDR SWIA200921575Bearing · corrodedLEFT ENGINE THRUST FITTING BEARING CORRODED ON INNER SURFACE. SB COMPLIANCE, REPLACED FITTING.SDR CA090406001Pedestal · cracked(CAN) 2 CRACKS WERE FOUND IN THE (CRITICAL) CONICAL AREA. ONE LOCATED 2.125 IN AND THE OTHER AT 2.600 IN FROM THE TOP THREADED AREA.SDR TRBACPCP20090008Mount · corrodedFOUND CORROSION ON LT WING AT NR 1 ENG UPPER AFT INBD ENGINE MOUNT. ACCOMPLISHED EO NR E2-57MR-308 LT WING FWD SPAR LWR SLAT EXTERNAL CORROSION REPAIR AT RIB 10.SDR SWIA200921135Mount · corrodedFLT 6097-6 - UPPER AND LOWER FORWARD ENGINE MOUNTS CORRODED. REPLACED UPPER AND LOWER FORWARD ENGINE MOUNTS.SDR CA090304006Mount · cracked(CAN) ENGINE MOUNT CRACK FOUND ON 50HR INSP. CRACK WAS FOUND IN THE LOWER LT CLUSTER PERPENDICULAR TO THE WELD RUNNING A TOTAL OF .7500" ALONG THE VERTICAL TUBE.SDR ASOA200900263ABolt · looseSAFETIED LT ENG FWD MOUNT BOLTS IAW AMM 71-00-00-400-801 SUBTASK 71-00-00-420-001.SDR DLM90090330Fastener · looseENGINE AFT MOUNT SUPPORT FITTING FASTENER INSPECTION PER EA 02-469466-12AD. UPPER AFT FASTENER (AFT FASTENER ON ROW A) FAILED INSPECTION. REPLACED ALL 8 FASTENERS IN FITTING PER EA INSTRUCTIONS. REPLACEMENT OF DISCREPANT FASTENERS CONSTITUTES A MAJOR REPAIR SDR CA090309002Mount · corroded(CAN) DURING COMPLIANCE OF TB206-89-129 (REMOVAL OF ENGINE MOUNT LEG CLAMSHELL DAMPERS), IT WAS NOTICED AFTER THE REMOVAL OF THE CLAMSHELL DAMPERS AND THEIR PACKING MATERIAL, EXTREME CORROSION WAS FORMING UNDER THE PRIMER, WHICH WAS FOUND TO BE BEYOND LIMITS. SDR 2009FA0000101Mount · damagedDURING SCHEDULED INSP, FOUND RT FWD ENGINE MOUNT ATTACH BRACKETS, P/N 45A34361-004 AND P/N 45A34361-006, HAD UPPER PORTIONS CUT INTO BY REPAIR ANGLE INSTALLED ON RT ENGINE UPPER INBD COWL PANEL AND ADJACENT EDGE OF COWL PANEL EDGE CHANNEL. REPAIR ANGLE WAS INSSDR MTNA0903002Mount · chafedLEFT ENGINE MOUNT TUBE NR 1 HAS SMALL CHAFE MARK ON I/B SIDE OF THE TUBE. BLENDED OUT IAW ATR REPAIR REF DO/TS-677/09-11321.SDR SWIA200921391Mount · corrodedLEFT ENGINE AFT THRUST MOUNT CORRODED. SB COMPLIANCE, REPLACED MOUNT.SDR SWIA200921390Mount · corrodedRT ENGINE AFT THRUST MOUNT CORRODED. SB COMPLIANCE, REPLACED MOUNT.SDR CA090223014Mount · cracked(CAN) CRACK FOUND DURING A ROUTINE 400 HOUR INSP. REPLACEMENT PART ORDERED AND RECEIVED. CRACKED APPEARED TO BE NEW. TUBING CRACKED AND SEPARATED. CRACK APPEARED ON LWR PORTION OF ENGINE MOUNT WITHIN 1.5 CM OF WELD.SDR SWIA200921008Mount · corrodedLEFT ENGINE FORWARD YOKE MOUNT CORRODED. SERVICE BULLETIN COMPLIANCE CHECK, REPLACED MOUNT.SDR S9BA2009005Mount · corrodedRT WING, RT ENGINE MOUNT BRACKET CORRODED. REMOVED AND REPLACED RT ENGINE MOUNT ADAPTOR IAW RD6-54-006. (K)
Back to JASC 7120