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 REXA201100218Yoke · scratchedRIGHT FORWARD ENGINE MOUNT YOKE HAS FOUR SCRATCHES AT TOP FORWARD LUG ON FORWARD FACE. TWO SCRATCHES MEASURE .156 INCH LONG AND UP TO 0.025 INCH DEEP. TWO SCRATCHES MEASURE 0.375 INCH LONG AND UP TO 0.007 INCH DEEP. REPAIRED IAW BOMBARDIER REO 601R-71-21-04SDR KGBR20110411341Mount Fitting · delaminatedLEFT WING UPPER OUTBOARD ENGINE MOUNT FITTING HAS START OF DELAMINATION, FWD SIDE OF FRONT SPAR.SDR KGBR20110411340Mount · delaminatedLEFT WING, UPPER INBOARD ENGINE MOUNT ON FWD SIDE OF FRONT SPAR IS DELAMINATEDSDR KGBR20110411339Mount · delaminatedRIGHT WING UPPER INBOARD ENGINE MOUNT ON FWD SIDE OF FRONT SPAR IS DELAMINATEDSDR CA110411003Mount · failed(CAN) DURING THE ACCEPTANCE FLIGHT OF ACFT 313, A VIBE WAS DETECTED ON NR 1 ENG & PROP. INVESTIGATION BY MTCE PERSONNEL, POST FLIGHT QUICKLY REVEALED THAT THE NR 1 ENG TOP MOUNT HAD FAILED DUE TO DISBOND. THE TOP MOUNT PN LM-431-83-V, SN LK0014 WAS INSTALLEDSDR SWIA201125937Mount · corrodedRIGHT ENGINE AFT THRUST MOUNT HAS CORROSION ON THE BALL END. (ENGINE CHANGE) REPLACED RT ENGINE AFT THRUST MOUNT ASSEMBLY.SDR MTNA03281100003Mount Bracket · brokenDURING A ONE YEAR AND TWO YEAR INSPECTION THE NUMBER TWO ENGINE LEFT AFT LATERAL AIRFRAME MOUNT BRACKET WAS FOUND BROKEN.SDR SWIA201125860Mount · corrodedLEFT ENGINE FORWARD MOUNT ASSEMBLY IS PITTED. (ENGINE CHANGE) REPLACED LEFT ENGINE FORWARD MOUNT ASSEMBLY PER AMM.SDR UALA2011032501442Acoustic Liner · tornTHREE SMALL TEARS IN THE ACOUSTIC MATERIAL INSIDE THE NUMBER ONE ENG COWLING. SAMC TEXT: REF MT 71-006. TEAR IN SKIN 3.5 INCHES LONG. EXCEEDS MT LIMITS. ACP REPAIR NR 1 PER MT 71-006.SDR SWIA201125864Mount · corrodedLEFT ENGINE FORWARD YOKE MOUNT ASSEMBLY CORRODED. (ENGINE CHANGE) REPLACED LEFT ENGINE FORWARD YOKE MOUNT ASSEMBLY PER AMM.SDR A6WA201140225Mount · chafedUPON INSTALLATION OF ANTI-ICE DUCT, FOUND CHAFING ON LT ENG FWD MOUNTS ATTACH STRUCTURE. REPAIR LT FWD ENG MOUNTS ATTACH STRUCTURE IAW REO 601R-54-51-102.SDR SWIA201125807Mount · corrodedRIGHT ENGINE AFT MOUNT HAS PITTING. (ENGINE CHANGE) REPLACED THE RIGHT ENGINE AFT THRUST MOUNT.SDR MASA2011031402144Cover · bentNR 2 ENG I/B COWL LATCH COVER BENT UP. MX R2 COWL LATCH COVER.SDR GUUA93371030711ATruss · crackedDURING MAG PARTICLE INSP, DISCOVERED ENGINE TRUSS TUBE WELD AREA CRACK. (OPEN)SDR UALA2011030401074Bearing · migratedNR 2 ENG AFT ENG MOUNT CENTER BEARING OF CENTER LINK ASSY. BEARING MIGRATED AFT APPROX 7-16 INCHES. REMOVED AFT MOUNT PER MM. REPLACED NR 2 ENG AFT LOWER ENG MOUNT PER MM. ACCOMPLISHED RII INSPECTION OF NR 2 ENG AFT LOWER ENG MOUNT PER MM. INSTALLATION ISDR SWIA201125701Bushing · corrodedRIGHT ENGINE FORWARD YOKE MOUNT LINK BUSHING CORRODED. (ENGINE CHANGE)REPLACED THE FORWARD YOKE LINK ASSEMBLY.SDR FDEA201102210642Mount · corrodedFWD NR 2 ENGINE MOUNT MATING SURFACE FOUND WITH CORROSION. CORROSION REMOVED AT NR 2 ENGINE FORWARD MOUNT MATING SURFACE AND FOUND WITHIN LIMITS AS PER CMM 71-20-04 REPAIR 5 FIGURE 504 REV 54. MATERIAL ORIGINAL THICKNESS= 0.765", MATERIAL REMOVED= 0.003", SDR FDEA201102210641Mount · corrodedAFT ENGINE MOUNT MATING SURFACE FOUND WITH CORROSION. CORROSION REMOVED AND CLEANED-UP PER CMM 71-20-05 REPAIR 3 TABLE 601 REV 50 AND FOUND WITHIN LIMITS AS PER CMM 71-20-05 FIGURE 501 REV 50. ORIGINAL MATERIAL THICKNESS= 0.125", MATERIAL REMOVED= 0.002"SDR FDEA201102210640Mount · corrodedNR 2 ENGINE PYLON - FWD ENGINE MOUNT BOLT HOLE FOUND WITH SPOT FACE CORRODED. COROSSION REMOVED AS PER SRM 51-74-10 REV 74 AND FOUND WITHIN LIMITS AS PER SRM 54-51- 81 FIGURE 104 REV 74. ORIGINAL MATERIAL THICKNESS: 0.078" , MATERIAL REMOVED: 0.017", MATERISDR FDEA201102170597Mount · corrodedNR 2 ENGINE PYLON - FWD ENGINE MOUNT BOLT HOLE SPOT FACE COROSSION FOUND. NR 2 ENGINE PYLON - FWD ENGINE MOUNT BOLT HOLE SPOT FACE COROSSION REMOVED IAW SRM 51-74-10, REV 74 AND FOUND WITHIN LIMITS IAW SRM 54-51-81, FIG 104, REV 74. ORIGINAL MATERIAL THICKNESDR SWIA201125606Housing · corrodedRIGHT ENGINE AFT MOUNT SPHERICAL BUSHING HOUSING HAS SOME PITTING. (ENGINE CHANGE) REPLACED RIGHT ENGINE SPHERICAL BUSHING HOUSING.SDR SWIA201125599Mount · corrodedRIGHT ENGINE FORWARD MOUNT LINK HAS CORROSION. (ENGINE CHANGE) REPLACED RIGHT ENGINE FORWARD MOUNT LINK.SDR ALGAR291144029Mount · crackedUPON DISASSEMBLY OF COMPRESSOR FOR 2000 HR INSP, FOUND CRACKING OF FWD FLANGE AT BOLT HOLES.SDR AALA20110208DFW01Bolt · brokenAIRCRAFT ARRIVED WITH CDL FOR LEFT WING LOWER FORWARD PYLON VIBRATOR ABSORBER MISSING. FOUND THE BOLT HEAD BROKEN OFF OF THE BOLT WHERE THE VIBRATOR ISOLATOR MOUNTS. THIS IS THE SAME BOLT THAT ATTACHES THE ENGINE MOUNT TO THE FRAME. REF IPC 71-20-00-04 FIGUSDR USAA2011020890580Pin · corrodedSAL - MAJOR REPAIR - S5 CHECK - GALVANIC CORROSION ON SOLID PIN AFT MOUNT LOWER OUTBOARD SIDE OF NR 2 ENGINE. REPLACED SOLID PIN AFT MOUNT LOWER OUTBOARD SIDE OF NR 2 ENGINE IAW A320 AMM 71-22-11.SDR CA110201010Mount · loose(CAN) VISUAL MOVEMENT CHECK REVEALED LOOSENESS OF ENGINE MOUNT FITTINGS P/N 50-980089-1. THERE ARE 4 PER NACELLE. THE LOWER PAIR WHERE FOUND LOOSE.SDR ALGAR1271145515Mount · crackedFOUND CRACKING OF FWD FLANGE OF REAR SUPPORT.SDR SIMA201102807Yoke · crackedDURING MAINTENANCE BASE VISIT FOUND THE LEFT ENGINE FORWARD INBOARD YOKE LUG FITTING FOUND TO HAVE A CRACK AT THE FORWARD INBOARD UPPER RADIUS 0.256" IN LENGTH AND CRACK IN THE LOWER YOKE AND FORWARD FITTING. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED ANSDR FDEA201101220333Mount · corrodedDURING NR 2 ENGINE PYLON MOUNT AFT HOLE CORROSION REMOVAL FOUND LOWER MATING FACE WITH CORROSION NEAR TO THE HOLE. REPAIRED IAW EA 6-5450-143832. DEEPEST REWORKED SURFACE: 0.019" AND MAXIMUM ALLOWABLE DEPTH: 0.0138" IAW SRM 54-51-81 CONFIGURATION 2, FIG 104,SDR C2XA11TY009Fitting · crackedTYS - A/C IS IN C-CHECK STATUS WHEN INSPECTION FOUND THE RT LOWER ENGINE YOLK, FWD MOUNT CRACKED. MAINTENANCE REMOVED THE FITTING AND REPLACED THE ENGINE IAW 5450-01028. A/C WILL BE RELEASED AT THE END OF THE CHECK.SDR EE4Y20110038Spar · damagedTHE FRONT SPARS ENGINES 1 AND 2, ENGINE MOUNTING HOLES WITH LIGHT NOTCHES.SDR ALGA1191144766Mount · crackedCRACK OF FWD FLANGE THROUGH BOLT HOLES AND DOUBLER PLATE.SDR SWIA201125478Bushing · corrodedRIGHT ENGINE AFT MOUNT SPHERICAL BUSHING HOUSING ASSEMBLY HAS SOME PITTING. (ENGINE CHANGE) REPLACED RIGHT ENGINE AFT MOUNT SPHERICAL BUSHING ASSEMBLY.SDR FDEA201101180279Mount · corrodedENGINE NR 2, PYLON FWD MOUNT AFT INBD HOLE LOWER AREA FOUND WITH CORROSION. AREA REWORKED AND FOUND WITHIN LIMIT IAW SRM 54-51-81, CONFIGURATION 2, FIG 202, REV 19. ORIGINAL HOLE DIAMETER: 0.9615", REWORKED HOLE DIAMETER: 0.9965" AND MAXIMUM HOLE DIAMETER: 0SDR FDEA201101180278Mount · corrodedENGINE NR 2, PYLON FWD MOUNT AFT OTBD HOLE LOWER AREA FOUND WITH CORROSION. REWORKED AND FOUND WITHIN LIMIT IAW SRM 54-51-81 CONFIGURATION 2, FIG 202, REV 19. ORIGINAL HOLE DIAMETER: 0.947", REWORKED HOLE DIAMETER: 0.9965" AND MAXIMUM HOLE DIAMETER: 0.997".SDR SWIA201125459Bearing · corrodedLEFT ENGINE FORWARD MOUNT LINK ASSEMBLY BEARING CORRODED. (ENGINE CHANGE) INSTALLED NEW FORWARD MOUNT LINK ASSEMBLY ON LEFT ENGINE.SDR SWIA201125463Bearing · corrodedLEFT ENGINE LINK ASSEMBLY HAS CORROSION ON THE BEARINGS. (ENGINE CHANGE) INSTALLED NEW LEFT ENGINE LINK ASSEMBLY.SDR GUUA94571011311AIsolation Mount · crackedDURING MAGNETIC PARTICLE INSP DISCOVERED LT LOWER ISOLATOR MOUNT WELD AREA CRACKS. PERFORMED WELD REPAIR TO ENGINE TRUSS TUBE WELD AREAS.SDR SWIA201125464Bearing · corrodedLEFT ENGINE FORWARD YOKE MOUNT SPHERICAL BEARINGS PITTED. (ENGINE CHANGE) REPLACED FORWARD YOKE MOUNT ON THE LEFT ENGINE.SDR SWIA201125408Link · corrodedRIGHT ENGINE FORWARD YOKE LINK HAS CORROSION. (ENGINE CHANGE) REPLACED RIGHT ENGINE FORWARD YOKE MOUNT LINK ASSEMBLY.SDR SWIA201125407Mount · corrodedRIGHT ENGINE FORWARD ENGINE MOUNT YOKE SPHERICAL BUSHINGS PITTED. (ENGINE CHANGE) REPLACED RIGHT ENGINE FORWARD YOKE MOUNT ASSEMBLY.SDR SWIA201125406Mount · damagedRIGHT ENGINE FORWARD THRUST MOUNT PINS SCORED. (ENGINE CHANGE) REPLACED RIGHT ENGINE FORWARD MOUNT PINS.SDR DALA1101259864Mount · crackedNR1 ENGINE PYLON APRON LOWER FRAME JUST AFT OF FWD MOUNT CRACKED. REMOVED FASTENERS AND SEVERAL PARTS TO GAIN ACCESS. CUT-OUT SECTION OF FRAME THAT WAS CRACKED. NDT TO VERIFY THAT DAMAGED WAS REMOVED. FABRICATED FORMER AND SPLICES IAW SRM 51-70-5. INSTALLESDR S9BA20110001Mount · failedON TAKEOFF, LT ENGINE SURGED AND WAS ONLY PRODUCING 24 TORQUE, ABORTED. UPON SHUTDOWN, UNABLE TO PULL LT PROP LEVER PAST FEATHER DETENT. AND PROP SPINNER SITTING LOW. FOUND UPPER MOUNT FAILED. R & R MOUNT ASSEMBLY IAW MM 71-20. INSPECTED ADJACENT MOUNTS, VERSDR 2011FA0000039Mount · damagedUPON REMOVAL, AN INSPECTION OF THE MOUNT WAS PERFORMED. DAMAGE WAS FOUND ON THE INBD MAIN SUPPORT CHANNEL. APPROX 10-12 INCHES FWD OF WHERE THE MOUNT ATTACHES TO THE FIREWALL. DAMAGE WAS ON THE INSIDE UPPER PART OF CHANNEL WITH A GROVE WORN APPROX .2500" INSDR GUUA94371010111AIsolator · crackedDURING MAGNETIC PARTICLE INSP DISCOVERED ISOLATOR MOUNT WELD AREA CRACKS. PERFORMED WELD REPAIR TO ENGINE TRUSS TUBE WELD AREAS.SDR SWIA201025383Yoke · corrodedLEFT ENGINE YOKE HAS CORROSION ON THE BUSHING FACES ON LINK ATTACH END. (ENGINE CHANGE) INSTALLED SERVICEABLE YOKE ASSEMBLY.SDR USAA2010123093275Pin · corrodedMAJOR REPAIR - S5 CHECK - CORROSION ON SOLID PIN AFT ENGINE MOUNT LOWER OUTBOARD POSITION ENG 2. REPLACED SOLID PIN AFT ENGINE MOUNT LOWER OUTBOARD POSITION ENG 2 IAW A320 AMM 71-22-11.SDR USAA2010123093274Pin · corrodedSAL - MAJOR REPAIR - S5 CHECK - CORROSION ON SOLID PIN AFT ENGINE MOUNT LOWER INBOARD POSITION ENGINE NR 2. REPLACED SOLID PIN AFT ENGINE MOUNT LOWER INBOARD POSITION ENGINE NR 2 IAW A320 AMM 71-22-11.SDR USAA2010123093273Pin · corrodedSAL - MAJOR REPAIR - S5 CHECK - CORROSION ON SOLID PIN AFT ENGINE MOUNT LOWER CENTER POSITION ENGINE NR 2. REPLACED SOLID PIN AFT ENGINE MOUNT LOWER CENTER POSITION ENGINE NR 2 IAW A320 AMM 71-22-11.
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