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 96ZZZX459Truss · crackedSPI - DURING VISUAL INSPECTION OF AREA 'A' AS REQUIRED BY AD 95-12-18, A CRACK WAS FOUND. THE RIGHT ENGINE TRUSS WAS REPLACED WITH SERVICEABLE.SDR 96ZZZX247Support · crackedSUPPORT REMOVED FOR SMALL CRACK IN UPPER FLANGE. UPON REMOVAL OF CABIN AIR INLET DUCT FROM FORWARD BULKHEAD, FOUND SUPPORT COMPLETELY SEVERED AT POINT SUPPORT PASSES THROUGH TUNNEL ASSY AND ATTACHES TO KEEL. SAME CONDITIONS FOUND ON RT SIDE ALTHOUGH NOT AS OSDR 96ZZZX246Support · severedSUPPORT REMOVED FOR SMALL CRACK IN UPPER FLANGE. UPON REMOVAL OF CABIN AIR INLET DUCT FROM FORWARD BULKHEAD, FOUND SUPPORT COMPLETELY SEVERED AT POINT SUPPORT PASSES THROUGH TUNNEL ASSY AND ATTACHES TO KEEL. SAME CONDITIONS FOUND ON RT SIDE ALTHOUGH NOT AS OSDR CA970311028Support Channel · cracked(CAN) CRACKS FOUND IN UPPER FLANGE BEND RADIUS, FORWARD ENGINE ATTACHMENT. LOWER ROOF BEAM WEB P/N 206-031-200-019 CRACKED.SDR 96ZZZX163Mount · crackedDURING A ROUTINE ENGINE CHANGE, THE ENGINE MOUNT WAS FOUND CRACKED AT THE RT LOWER ATTACHMENT TO FIREWALL, AS WOULD BE VIEWED FROM BEHIND AIRCRAFT.SDR 96ZZZX67Mount · brokenMOUNT WAS FOUND BROKEN IN 2 PLACES; BOTH OUTBOARD AND BELOW THE UPPER LEFT MOUNTING FLANGE. A SMALL AMOUNT OF INTERNAL CORROSION WAS DETECTED, BUT IT DID NOT APPEAR TO BE A CONTRIBUTING FACTOR. THE BROKEN AREAS WERE NOT ON WELD JOINTS, IT APPEARS THAT THE SUSDR CA951221013Mount · cracked(CAN)WHILE CARRYING OUT ROUTINE INSPECTION, BOTH REAR ENGINE MOUNTS WERE FOUND CRACKED. CRACKS WERE APPROXIMATELY ONE INCH LONG. NEW MOUNTS INSTALLED AND AIRCRAFT RETURNED TO SERVICE.SDR UPS505121Fuse Pin · crackedWHILE ON GROUND, MAINT FOUND RT ENGINE O/B FUSE PIN CRACKED. REMOVED AND REPLACED BOTH FUSE PINS ON RT ENG IAW EO B757-440-0431. ENG OPS AND LEAK CKS GOOD.SDR 95ZZZX6768Bolt · rustedENGINE MOUNT UPPER ATTACH POINTS TO FIREWALL; FOUND FRETTING CORROSION IN AREA. BOLTS HAD WORKED LOOSE AND BOLTS WERE RUSTING AND HAD SERIOUS PITTING.SDR CA951209104Diffuser Housing · cracked(CAN)ON DAILY INSPECTION IT WAS FOUND THAT THE PAN HAD CRACKED AROUND THE INSERT.SDR CA951209103Diffuser Housing · cracked(CAN)ON DAILY INSPECTION IT WAS FOUND THAT THE PAN HAD CRACKED AROUND THE INSERT.SDR 95ZZZX6685Bracket · crackedDURING INSPECTION, FOUND ENGINE LT REAR MOUNT BRACKET CRACKED. TCM REP STATES NO FAILIURE HISTORY ON THIS PART.SDR CA951122004Strut · cracked(CAN)REAR ENGINE MOUNT STRUT #2 ENGINE INBOARD FOUND CRACKED JUST BELOW MID POINT CROSSBRACE BOLT HOLE. STRUT WAS MODIFIED AS PER MOD 8/1763 AND AD CF-92-14.SDR 96ZZZM76Truss · crackedSPW - DURING ROUTINE INSPECTION (REQUIRED BY AD95-02-18), MAINTENANCE FOUND THE ENGINE TRUSS CRACKED ON THE RIGHT SIDE NEAR THE LOWER BOLT HOLE. THE ENGINE TRUSS WAS REPLACED. (M)SDR EIAA9556Rod Assy · bolt missingJFK - LOG PAGE: E 07985 - NR 3 ENGINE AFT MOUNT THRUST LINK BOLT MISSING. REPLACED AFT ENGINE MOUNT IAW MM 71-23-03, PAGE 401, RII. BORESCOPED ENGINE AND PERFORMED ECRA 485-54-088-1 AND ECRA 485-54-089-1. REFERENCE OPERATOR CONTROL NR 95ZZZX6521. (X)SDR 95ZZZX6521Aft Mount · damagedJFK - LOG PAGE: E 07985 - NR 3 ENGINE AFT MOUNT THRUST LINK BOLT MISSING. REPLACED AFT ENGINE MOUNT IAW MM 71-23-03, PAGE 401, RII. BORESCOPED ENGINE AND PERFORMED ECRA 485-54-088-1 AND ECRA 485-54-089-1. REFERENCE OPERATOR CONTROL NR EIAA9556.SDR 95ZZZX6746Mount Bolts · looseDURING ANNUAL, FOUND LOWER ENGINE MOUNT BOLTS LOOSE.SDR CA951204027Mount · cracked(CAN)L/H MOUNT ASSEMBLY CRACKED.SDR 95ZZZX6903Engine Leg · defectiveWHEN INSTALLING LEGS TO AIR FRAME, FOUND UPPER END OF LEG AT WELD CONTACTS OTHER LEG.SDR 95ZZZX6642Truss · crackedSPW - DURING VISUAL INSPECTION OF AREA 'A' REQUIRED BY AD 95-02-18, THE TRUSS WAS FOUND CRACKED AT THE LT OUTBOARD SIDE AT THE WELD FOR THE COWL MOUNT. THE LT TRUSS WAS REPAIRED IAW BEECH KIT NR 129-9006.SDR 95ZZZX6641Truss · crackedSPW - DURING THE SCHEDULED VISUAL INSPECTION OF AREA 'A' OF THE LT ENGINE TRUSS AS REQUIRED BY AD 95-02-18, A SMALL CRACK WAS FOUND ON THE UPPER RT BRACKET THAT HOLDS THE COWL. THE CRACK WAS REPAIRED IAW BEECH KIT NR 129-9006.SDR CA951103003Bracket · cracked(CAN)UPON REMOVAL OF BRACKET TO COMPLY WITH SL 1656/95/ARL/27, THE BRACKET WAS FOUND TO BE CRACKED 1/2 WAY THROUGH. THE CRACK RUNS UP AND DOWN AND IS DIRECTLY IN CONTACT WITH THE SHARP SQUARE EDGE OF THE G EARBOX.SDR 95ZZZX6195Mount · improper weldENGINE MOUNT PAINT STRIPPED AND CLEANED FOR MAGNAFLUX TO PERFORM 1,200-HOUR INSPECTION. WELD JOINING TUBE TO LT MOUNT FITTING INCOMPLETE (MISSING .50 INCH OF WELD). REPAIRED BY WELDING.SDR CA951204028Mount · cracked(CAN)BOTH R/H AND L/H ENGINE MOUNTS FOUND CRACKED.SDR 9516249601Mount Assy · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN BOTH THE LEFT AND RIGHT PYLON FORWARD ENGINE MOUNT ISOLATOR HOUSINGS. REPLACED BOTH YOKE ASSEMBLIES PER MM 71-20-3.SDR 95ZZZX6749Mount · part missingDURING OIL CHANGE, FOUND THE CARBURETOR AIR BOX BROKEN FROM THE CARBURETOR. WHILE REMOVING AIR BOX, A 10 INCH PIECE OF THE LOWER ENGINE MOUNT WAS FOUND MISSING. IT DOES NOT SHOW SIGNS OF AN OLD CRACK AS BOTH SIDES ARE SHINEY. SUSPECT POSSIBLY A HARD NOSE WHSDR 95ZZZX6643Truss · crackedESC - DURING SCHEDULED VISUAL INSPECTION OF AREA 'A' AS REQUIRED BY AD 95-02-18, THE ENGINE TRUSS WAS FOUND CRACKED AT THE INBOARD TOP STRUT AT THE OIL PLUG. THE CRACK WAS REPAIRED IAW BEECH REPAIR KIT 129-9006.SDR CA951103004Mount · cracked(CAN)BOTH R/H MOUNT P/N 350A21-1066-05 AND L/H MOUNT P/N 350A21-1066-06 WERE FOUND CRACKED.SDR CA951103101Tripod Mount · cracked(CAN)TRIPOD ENGINE MOUNT INSIDE LEG BROKEN WHERE LEG IS WELDED TO THE UPPER BEARING MOUNT. REPLACEMENT TRIPOD INSTALLED AND A MISALIGNMENT WAS NOTED AT THE ATTACHMENT POINT CAUSING A PRELOAD ON THE MOUNT.SDR 9514739949Mount · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE RIGHT ENGINE AFT MOUNT. REPLACED MOUNT PER MM 71-20-2.SDR 95ZZZX6121Truss · crackedSPW - DURING ROUTINE INSPECTION REQUIRED BY AD 95-02-18, MAINTENANCE FOUND THE LT TRUSS CRACKED ALONG THE TOP COWLING ATTACH BRACKETS BOTH INBOARD AND OUTBOARD. THE TRUSS WAS REPLACED.SDR 95ZZZX5959Mount · corrodedFOUND MOUNT CORROSION BETWEEN PLATE AND CAST BEAM ON ALL FOUR SIDES. AREA BETWEEN PLATE AND BEAM CAN HOLD MOISTURE. RECOMMEND REMOVE PLATES, CLEAN CORROSION. FILL WITH PRC AND REASSEMBLE. REPAIR WILL REQUIRE DER.SDR 95ZZZX5958Mount · corrodedFOUND MOUNT CORROSION BETWEEN PLATE AND CAST BEAM ON ALL FOUR SIDES. AREA BETWEEN PLATE OF BEAM CAN HOLD MOISTURE. RECOMMEND REMOVE PLATES, CLEAN CORROSION, FILL WITH PRC, AND REASSEMBLE. REPAIR WILL REQUIRE DER.SDR 95ZZZX5767Mount · corrodedCORROSION BETWEEN PLATE AND CAST BEAM ALL FOUR SIDES. AREA BETWEEN PLATE AND BEAM CAN HOLD MOISTURE. CORROSION LOCATED UNDER P/N 62003211 BLOCK. RECOMMEND REMOVE PLATES, CLEAN CORROSION. FILL WITH PRC AND REASSEMBLE. REPAIR WILL REQUIRE DER APPROVAL.SDR 95ZZZX5766Mount · corrodedCORROSION BETWEEN PLATE AND CAST BEAM ALL FOUR SIDES. AREA BETWEEN PLATE AND BEAM CAN HOLD MOISTURE. CORROSION LOCATED UNDER PN 62003211 BLOCK. RECOMMEND REMOVE PLATES, CLEAN CORROSION, FILL WITH PRC AND REASSEMBLE. REPAIR WILL REQUIRE DER APPROVAL.SDR 95ZZZX6118Truss · chafedSPW - DURING A ROUTINE INSPECTION, MAINTENANCE FOUND RT TRUSS INBOARD UPPER TUBE CHAFED. THE CHAFE WAS REPAIRED BY WELDING IAW REPAIR NR 2 OF BEECH KIT 129-9006-1.SDR 95ZZZX6120Truss · chafedSPW - DURING ROUTINE INSPECTION REQUIRED BY AD 95-02-18, MAINTENANCE FOUND THE RT ENGINE TRUSS TOP INBOARD TUBE IN AREA 'A' CHAFED. THE CHAFE WAS REPAIRED BY WELDING IAW REPAIR NR 2 OF BEECH KIT 129-9006-1.SDR 95ZZZX6068Tube · crackedDURING ANNUAL INSPECTION, THE TUBE USED TO MOUNT ENGINE OIL TANK FOUND CRACKED AT THE RIGHT REAR TANK MOUNTING POINT. THE CRACK ENCIRCLED THE TUBE, BUT DID NOT MEET. DURING REPAIR, NO EVIDENCE OF INTERNAL CORROSION ON TUBING OTHER THAN AT CRACK AREA.SDR 95ZZZM514Truss · chafedSPW - DURING ROUTINE INSPECTION, MAINTENANCE FOUND THE RT ENGINE TRUSS CHAFED IN AREA 'B' AS DESCRIBED IN BEECH SB 2255R7 AND AD 95-02-18, THE DAMAGE WAS REPAIRED IAW REPAIR NR 2 OF BEECH KIT 129-9006-1. (M)SDR 95ZZZM515Truss · crackedSPW - DURING THE ROUTINE VISUAL INSPECTION REQUIRED BY AD 95-02-18, THE RIGHT TRUSS WAS FOUND CRACKED IN AREA 'A'. THE TRUSS WAS CHANGED AND ENGINE FUNCTIONAL TEST WAS SATISFACTORY.SDR 95FDEA01202Fitting · corrodedCENTER ENGINE REAR SUPPORT FITTING ASSEMBLY IS BADLY CORRODED. REMOVED AND REPLACED CENTER ENGINE REAR SUPPORT FITTING IAW FEDEX SRM 51-30-2, 51-30-4 AND FEDEX MM 71-21-1.SDR 95ZZZX5769Bolt · failedONE LOWER ENGINE MOUNT BOLT BROKE IN-FLIGHT, CONDITION WAS DISCOVERED BY OWNER WHILE CHECKING OIL. ENGINE MOUNT SPACER WENT OUT THROUGH PROPELLER CAUSING SIGNIFICANT DAMAGE TO PROPELLER. WHEN MFG WAS ASKED, THEY SAID NEW BOLTS ARE NOW INSTALLED AND SENT 4 NSDR 95ZZZM589Truss · crackedDURING A INSPECTION OF AREA 'A' ON THE RIGHT ENGINE TRUSS A .5 INCH CRACK. REPAIRED BY WELDING CRACK. (M)SDR 95ZZZM483Truss · crackedESC - DURING THE ROUTINE TRUSS INSPECTION REQUIRED BY AD95-02-18, A .75 INCH CRACK WAS FOUND NEAR THE LINSEED OIL PLUG OF THE INBOARD AREA 'A' OF THE RIGHT TRUSS. THE TRUSS WAS REPAIRED IAW BEECH KIT 129-9006, REPAIR NR 2.SDR 95ZZZX5045Mount · looseLOWER ENGINE MOUNT FOUND LOOSE ON LEFT SIDE AND BOLT HOLE ELONGATED. PART REPLACED. MANUFACTURER'S TORQUE IS 40 INCH/POUNDS AT THIS POINT. THE BOLT IS STAINLESS CLOSE TOLERANCE. THE STRUCTURE IS STAINLESS AND THE MOUNT IS STEEL. THIS SEEMS LIKE A LIGHT TOSDR 95ZZZX5526Mount · crackedFOUND CRACKED RT REAR MOTOR MOUNT. RADIAL CRACKS EMANATING FROM SHOCK MOUNT BUSHING BRACKET. (BUSHING P/N 785-000).SDR 95ZZZM487Truss · crackedSPW - DURING ROUTINE INSPECTION, MAINTENANCE FOUND THE OUTER LEFT ENGINE TRUSS CRACKED AT UPPER WELD ON COWL ATTACH BRACKET ON TUBE, APPROXIMATELY .5 INCH LONG ON OUTER AND .125 INCH LONG ON INNER. BOTH CRACKS WERE REPAIRED IAW BEECH KIT NR 129-9006.SDR UPS203971Cone Bolt · gougedWHILE IN SHANNON, IRELAND FOR C-CHECK, MAINTENANCE FOUND NR 2 ENGINE, LT FWD MOUNT CONE BOLT NOT SITTING PROPERLY. NEW CONE BOLT INSTALLED AND INSPECTION CARRIED OUT PER E.O. 95-10-003.SDR 95ZZZX4573Bracket · brokenWHILE C/W AD 91-15-20, FOUND RIGHT ENGINE LOWER NR 1 CYLINDER BRACKET BROKEN IN TWO. NOTE: AD 95-03-14, PN 630695, APPLIES TO LEFT LOWER BRACKET. THIS WAS RIGHT LOWER BRACKET. SUBMITTER STATED AD 95-03-14 SHOULD APPLY TO BOTH ENGINE MOUNT BRACKETS.SDR 95ZZZM490Truss · crackedESC - DURING INSPECTION OF AREA 'A' AS REQUIRED BY AD 95-02-18, THE RIGHT TRUSS WAS FOUND CRACKED. THE .5 INCH CRACK WAS CENTERED AT THE OIL PLUG ON THE UPPER LEFT FORWARD LEG. A WELD REPAIR WAS ACCOMPLISHED IAW BEECH REPAIR KIT NR 129-9006-1 REPAIR NR 2.
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