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 SWIA201334349Bolt · galledLT ENGINE FWD MOUNT UPPER & LOWER BOLTS GALLED. SERVICE REPLACED.SDR SWIA201334348Bushing · scoredLT ENGINE UPPER & LOWER FWD MOUNT CLEVIS`S BUSHINGS HAVE SCORING. SERVICE REPLACED IAW PPBM.SDR DALA13040500953Bolt · corrodedDURING SCHEDULED MX INSPECTION, CORROSION WAS FOUND ON THE LOWER ENGINE MOUNT BOLT AT THE RT YOKE. (MRB 54-049-02). THE LOWER BOLT AT RT YOKE WAS REPLACED.SDR FDEA201308151932Mount · damagedNR 2 ENGINE AFT MOUNT LOWER HANGER FITTING BUSHING HOLES FOUND OVERSIZE AFTER EXISTING BUSHING REMOVAL. REPAIRED IAW EA F-7120 - 301912.SDR ASOA20130814203Mount · crackedDURING C-CHECK, NR 1 ENGINE FWD LOWER MOUNT CRACKED. MX R & R ENG NR 1 FWD LOWER YOKE FITTING IAW EC5450-01073. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20130719188Yoke · crackedDURING C-CHECK THE RT ENGINE FWD LOWER MOUNT YOKE WAS FOUND TO BE CRACKED AND VERIFIED WITH EDDY CURRENT. MX R & R THE YOKE IAW EC5450-01073. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR FDEA201307031473Strut · chafedNR 2 ENG STRUT OTBD SIDE STA 170 FIREWALL, CHAFED ON AFT SIDE.SDR REXA2013061601000Housing · gougedUPON REMOVAL OF LT ENGINE AFT THRUST MOUNT SPHERICAL BUSHING HOUSING, FOUND OTBD RIB HOUSING BORE GOUGED. REPAIRED LT ENG AFT THRUST MOUNT SPHERICAL BUSHING HOUSING ON OTBD RIB IAW REO 690-54-51-010 AND EO R54093.SDR CA130617007Mount · damaged(CAN) AFTER REPLACING TWO SHOCK MOUNTS AT THE LAST INSPECTION, 200HR. DURING THE NEXT INSPECTION, 50HR IT WAS FOUND THAT THE SAME MOUNTS THAT WERE REPLACED WERE AGAIN RIPPED AND COMPLETELY SEPARATED FROM THE ATTACHING BASE. THE ENGINE WAS INSPECTED FOR EXCESSDR HNAA2013060500327Mount · corrodedLEFT ENGINE HAD CORROSION UNDER ENGINE MOUNT. BLENDED FORWARD MOUNT IAW MM 72-10-00. ALODINE AREA IAW 72-00-00, PAGE 809.SDR FDEA201306041183Mount · corrodedNR 2 ENGINE PYLON FWD ENGINE MOUNT FITTING MATING SURFACE FOUND RUST. REWORKED IAW SRM 54-51-81, CONFIG 2, FIGURE 104, REV 23. REPAIR ACCOMPLISHED IAW EA 6-5450-167628 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 116.SDR FDEA201306041182Mount · corrodedNR 2 ENGINE PYLON FORWARD ENGINE MOUNT FITTING AFT OTBD BOLT HOLE SPOT FACE FOUND RUST. REWORKED AND FOUND WITH LIMITS IAW SRM 54-51-81, CONFIG 2, FIG 104, REV 23. REPAIR ACCOMPLISHED IAW EA NR 6-5450-167628, PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-1SDR FDEA201306041181Mount · corrodedNR 2 ENGINE PYLON FWD ENGINE MOUNT FITTING AFT INBD BOLT HOLE SPOT FACE FOUND RUST. REWORKED IAW SRM 54-51-81 CONFIG 2, FIG 104, REV 23. REPAIR ACCOMPLISHED IAW EA 6-5450-167628, PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 116.SDR ASOA06012013316Yoke · crackedACFT WAS IN FOR A 5A CHECK, WHEN INSPECTION FOUND NTHE LT FWD LWR ENGINE YOKE CRACKED. MX R & R THE ENGINE YOKE IAW EC 5450-01013. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.SDR ASOA20130530160VYoke · crackedDURING C-CHECK THE RT FWD ENGINE MOUNT LOWER YOKE WAS FOUND TO BE CRACKED. MX R & R THE YOKE IAW EC5450-01073. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ABXA20130506432Mount · corrodedNR 2 ENGINE AFT MOUNT HAS SEVERAL AREAS OF CORROSION. REMOVED AND REPLACED ENGINE MOUNT IAW B767 MM CH 71-21-02-4, ACFT WAS GROUNDED.SDR DALA13021139201Bushing · corrodedNR 2 ENGINE AFT MOUNT HAT BUSHINGS CORRODED. R & R NR 2 ENGINE AFT MOUNT BUSHINGS IAW CMM 71-20-14.SDR ABXA20130501433Mount · corrodedNR 1 ENGINE AFT ENGINE MOUNT HAS SURFACE CORROSION. REMOVED AND REPLACED AFT ENGINE MOUNT IAW B767 AMM 71-21-02-4, ACFT WAS GROUNDED.SDR 2013FA0000252Mount · chafedLOWER ENGINE MOUNT TUBE BETWEEN THE LOWER AFT MOUNTS WAS CHAFED APPROX HALFWAY THROUGH. INSPECTION REVEALED THAT AN OIL LINE ON THE BOTTOM REAR ENGINE THAT WAS ROUTED BETWEEN THE MOUNT AND THE FUEL CONTROL UNIT WAS THE CAUSE OF THE CHAFING. THERE IS SO LITTLESDR CA130425003Mount · cracked(CAN) COMPLETING SB1103D, FOUND CRACK IN NOSE GEAR ACTUATOR MOUNT OF ENGINE MOUNT.SDR USAA2013041200013Shear Pin · corrodedRON VISIT - INSPECTION OF RIGHT ENGINE CENTER OUTBOARD AFT MOUNT SHEAR PIN WAS FOUND TO HAVE CORROSION (PITTED AT 6 O`CLOCK POSITION). REPLACED RIGHT ENGINE CENTER OUTBOARD AFT MOUNT SHEAR PIN IAW A319 AMM 71-22-11-400.SDR 2013FA0000280Mount · erodedDURING LT AND RT ENGINE CHANGE THE LT AND RT ENGINE MOUNT TRUSSES WERE INSPECTED. SEVERE HEAT EROSION WAS FOUND ON THE LT BEAM BELOW THE FWD INDUCTION AIR BOX MOUNT BRACKET. THIS AREA IS NEAR THE LT EXHAUST ELBOW. BOTH MOUNTS SHOW THE SAME AMOUNT OF EROSIONSDR ASOA20130402119Yoke · crackedDURING C-CHECK, LT FWD LOWER ENGINE YOKE FWD FITTING CRACKED. REPAIRED IAW EC5450-01071. ACFT APPROVED FOR RETURN TO SERVICE.SDR QXEA2013033100719Strut · damagedCHAFE DAMAGE ON LT ENGINE A8 EMS STRUT AFT LOWER SIDE. REMOVED AND BLENDED DAMAGE IAW SRM 51-14-00-02-04, REV 12. CONFIRMED AFFECTED AREA CRACK FREE REF NTM 51-00-06-910-801, PT 1, REV 9. BLENDED FOUND TO BE OUT OF LIMITS IAW SRM 54-13-06-00-01, REV 12. MSDR FDEA201303220644Intake · crackedNR 2 ENGINE INTAKE DUCT RT ON PANEL NR 364RR STATION 2140, REAR CENTER SPAR TO REAR SPAR LOWER PANEL FOUND CRACKED. REPAIRED AS PER SRM 55-30-02 FIGURE 201 REPAIR 2 REVISION 52. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 116.SDR SIMA20130322010Yoke · crackedDURING MAINTENANCE INSPECTION FOUND THE LEFT ENGINE FORWARD LOWER YOKE CRACKED FORWARD SIDE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED A NEW SERVICEABLE LEFT ENGINE FORWARD LOWER YOKE IAW AEA EO EM-54MR-386. THE AIRCRAFT WAS RETURNED TO SERSDR QXEA2013031900628Strut · damagedSCRATCH DAMAGE ON LT ENGINE A2 EMS STRUT FWD OTBD SIDE. REMOVED CORRODED SIGN ANGLE IAW SRM REV 12 51-42-05-02-01. CORROSION DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 53-20-23-00-01. MATCH DRILLED NEW SKIN ANGLE IAW SRM 51-40-07-02-01, REV 12. INSTALLED NEWSDR QXEA2013031800646Strut · chafedCHAFE DAMAGE ON RT ENGINE F3 EMS STRUT LOWER SIDE NEAR AC GEN. REMOVED AND BLENDED DAMAGE IAW SRM REV 12 51-14-00-02-04. NO MATERIAL LOSS NOTED. CONFIRMED AFFECTED AREA CRACK FREE REF NTM 51-00-06-910-801, PT 1, REV 9. UPON FURTHER EVALUATION FOUND NO CHAFISDR ASOA20130309288TYoke · crackedACFT IS IN FOR A C-CHECK WHEN INSPECTION FOUND THE NR 1 ENGINE LOWER YOKE FWD KNUCKLE CRACKED. MX R & R THE FWD LOWER YOKE IAW EC 5450-01028, REV A. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF ALL CHECKS.SDR EBTR20130305007Lug · failedAPPROXIMATELY 1.5 HRS INTO FLIGHT, PILOT NOTED RT ENGINE MANIFOLD PRESSURE DROPPED AFTER SWITCHING FUEL TANKS ADJUSTED POWER, ENGINE MANIFOLD PRESSURE DROPPED AND SURGED, PILOT NOTICED OIL ON TOP OF RT ENG COWL AND OIL PRESSURE LOW AND SURGING, REDUCED POWERSDR CALA2013022500125Mount · corrodedNR 2 ENGINE AFT MOUNT PADS SHOW SIGNS OF PITTING CORROSION. CLEANED OFF SURFACE CORROSION, & PRIMED IAW SRM 54-50-02.SDR 2013F00047Mount · corrodedTHE LT FWD ENGINE MOUNT, CORRODED ALL THE WAY THROUGH UNDERNEATH THE CLAMSHELL DAMPER PIECE. A SMALL AMOUNT OF PLAY HAD BEEN FOUND IN THE ENG AND IT HAD BEEN DECIDED TO REPLACE THE LEG DUE TO THE PLAY. UPON REMOVING THE CLAMSHELL, THE LEG HAD RUSTED THROUGHSDR ASOA20130126066VFitting · crackedDURING C-CHECK THE NR 1 ENGINE FORWARD MOUNT YOKE LOWER FWD MOUNT FITTING WAS FOUND TO BE CRACKED. MX R & R THE CRACKED FITTING IAW EC5450-01028. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20130126065Fitting · crackedDURING C-CHECK, THE NR 2 ENGINE FORWARD MOUNT YOKE LOWER FWD MOUNT FITTING WAS FOUND TO BE CRACKED. MX R & R THE CRACKED FITTING IAW EC5450-01028. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR R5KB2013013150501Mount · corrodedNR 2 ENGINE, UPPER FORWARD MOUNT ASSY CORRODED.SDR CA130128022Rod End · worn(CAN) IN THE SUMMER OF 2011,PILOTS REPORTED THAT AT HIGH POWER SETTINGS IN CRUISE A HIGH FREQUENCY VIBRATION WAS FELT IN THE OTBD RUDDER PEDALS AND THE SEAT FRAMES. IT WAS ALSO NOTICED THAT THE OTBD STATIC WICKS OF THE LT ELEVATOR WOULD BE MISSING AFTER SOME FSDR FDEA201301260194Mount · unknownNR 2 ENGINE, AFT MOUNT SUPPORT, OTBD SIDE, AFT SIDE, EVIDENCE OF PREVIOUS BLEND OUT OF DAMAGE.SDR ASOA20130125244TYoke · crackedRT ENGINE LOWER FWD YOKE CRACKED IN CORNER OF FORWARD EAR. R & R YOKE.SDR YN8R201301230002Mount · crackedDURING HARD LANDING INSPECTION AND REPAIR, FOUND THE ENGINE MOUNT, CRACKED IN THREE WELD LOCATIONS AND ALSO WARPED. CRACKS FOUND BY MAG PARTICLE INSPECTION. LOWER RT ATTACHMENT LEG ALSO WARPED .7500" OUT OF ALIGNMENT.SDR ASOA20130119053Yoke · crackedDURING C-CHECK, NR 1 ENGINE FWD LOWER MOUNT YOKE FWD EAR HAS VISUAL INDICATION OF CRACK BEYOND STOP DRILL. MX R & R RT 1 ENGINE FWD LOWER MOUNT YOKE FWD EAR IAW EC5450-01028. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20130119034Fitting · crackedDURING C-CHECK DMI 0841573 - LT FWD LWR ENGINE YOKE FWD FITTING CRACKED. MX R & R LT FWD LWR ENGINE YOKE FWD FITTING IAW EC5450-01028. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR 2013FA0000039Isolator · failedDURING INSPECTION FOUND LT ENGINE, LT FORWARD AND LT REAR ENGINE MOUNT ISOLATOR DEFORMED, SAGGING AND JUMPED OUT OF AIRFRAME MOUNT. ALLOWS ENGINE TO SAG AND INTAKE MANIFOLD, AND EXHAUST PIPE TO CONTACT ACFT STRUCTURE. LT FORWARD ISOLATOR HAD BEEN INSTALLED SDR 2013FA0000084Mount · crackedDURING NDT INSPECTION OF ENGINE MOUNT, CRACK INDICATIONS FOUND.SDR CA121231004Mount · cracked(CAN) DURING INSPECTION A CRACK WAS DISCOVERED AT THE JUNCTION OF THE UPPER LT TUBES AND THE LT UPPER MOUNT. THE CRACK WAS APPROXIMATELY HALF WAY AROUND THE TUBE.SDR NOCA10112Mount · corrodedNR 2 ENGINE FWD ENGINE MOUNT HAS AREAS OF PITTING ON UPPER SURFACE. REMOVED AND REPLACED NR 2 FWD ENGINE MOUNT IAW AMM 71-21-01.SDR ASOA20121224184Fitting · crackedLT ENGINE FORWARD YOKE, LOWER FORWARD MOUNT FITTING CRACKED. MEASURED CRACK (.187") STOP DRILLED. PLACED ON 2 DMI'S ONE FOR 5000 FLIGHT CYCLES OR TILL NEXT C-CHECK FOR FINAL REPAIR. THE OTHER IS FOR A DETAILED VISUAL INSP EVERY 25 FLIGHT CYCLES.SDR ASOA20121224183Fitting · crackedRT ENGINE FORWARD YOKE, LOWER FORWARD MOUNT FITTING CRACKED. MEASURED CRACK (.187") STOP DRILLED. PLACED ON 2 DMI'S ONE FOR 5000 FLIGHT CYCLES OR TILL NEXT C-CHECK FOR FINAL REPAIR. THE OTHER IS FOR A DETAILED VISUAL INSPECTION EVERY 25 FLIGHT CYCLES.SDR CA121217001Truss · cracked(CAN) DURING A DAILY INSPECTION, THE RT ENGINE TRUSS WAS FOUND TO BE CRACKED ON THE RT UPPER BOLT FLANGE WELD. THE TRUSS WAS REPLACED.SDR CA121206010Mount · loose(CAN) FOUND DURING INSPECTION, THAT ATTACHMENT BOLTS, HAD COME LOOSE. THE INSPECTION WAS CARRIED OUT IAW INSTRUCTIONS FOR AIRWORTHINESS STC SH08-8. ALSO, THE HOLES HAD ELONGATED CAUSING THE FITTING TO MOVE INSIDE THE STRUT ASSEMBLY. MFG DART AEROSPACE, WAS NSDR FDEA201211214120Mount · corrodedNR 2 ENG PYLON FWD ENGINE MOUNT FITTING INBD AFT TENSILE BOLT HOLE HAS OXIDATION AND PITTING IN ITS BORE. REAMED NR 2 ENG FWD ENG MOUNT FITTING TO CLEAN OXIDATION AND PITTING TO 0.997 IAW SRM 54-51-81. INSP HOLE FOR CRACKS IAW NTM 51-60-00. REPROTECTED BORE IA
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