JASC 7120
Service difficulty reports · 3,029
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 AALA2020012959004Pin · seizedAIRCRAFT IN BASE MAINTENANCE: NR 2 ENGINE AFT MOUNT INNER PIN SEIZED. REPLACED AFT ENGINE MOUNT IAW AMM 71-22-11-400.SDR IPXA2020012435291Shackle · corrodedINSPECTION TYPE:C#1 ENG PYLON I/B, O/B SHACKLE CORRODED AROUND BUSHINGREPLACED SHACKLE WITH NEW PART (A54610042020, S/N MEC206) PER IPC 54-51-71-01-630. INSTALLATION C/W ON T.C# 572179-02-1-512.`SDR IPXA2020012451292Shackle · corrodedINSPECTION TYPE:C#1 ENG I/B, I/B SHACKLE CORRODED AROUND BUSHINGREPLACED SHACKLE WITH NEW PART (A5461004200200, S/N 59750) PER IPC 54-51-71-01-630. INSTALLATION C/W ON TC#572179-02-1-512SDR IPXA2020012451297Shackle · no testINSPECTION TYPE:CINBRD SHACKLE OF #2 PYLON INBRD SIDE HAS CORROSION AROUND CUT OUT HOLES REPLACED INBRD SHACKLE PART #A5461004200200 S/N UP61336 OF #2 PYLON, IAW SRM 54-51-71 SRM 51-72-10SDR IPXA2020012435289Shackle · crackedOTBD SHACKLE ON #2 PYLON INBD SIDE HAS CORROSION AROUND CUTOUT HOLESREPLACED OB SHACKLE PART #A5461004200200 SER#UP48205 OF #2 PYLON IAW SRM 51-72-10SDR IPXA2020012251240Mount · corrodedINSPECTION TYPE:SEG, NR 1 ENG TO PYLON MOUNT HAS CORROSION AROUND WASHER& ENG FORWARD MOUNT BOLT HEADS LEFT AND RIGHT SIDECLEAN SURFACE AREA AROUND FWD MOUNT BOLT HOLES IAW AMM 51-74-10. NO DAMAGE NOTED.SDR RAIA2020012910003Mount · cracked# 1 ENGINE FWD YOKE MOUNT LOWER FWD LINKAGE FITTING HAS CRACK AT FWD RADIUS- R&R #1 ENGINE FWD YOKE MOUNT LOWER FWD LINKAGE FITTING.SDR IPXA2020012745338Attach Fitting · corrodedINSPECTION TYPE:A300#1 ENGINE PYLON OB SHACKLE ATTACH FITTING HAS TORQUE WEAR NEAR BUSHINGS O/B SIDEBLENDED AREA FOUNBD WITHIN LIMITS IAW A300-600 SRM 54-51-71 FIG 102.SDR IPXA2020012745337Attach Fitting · corrodedNR 1 ENG PYLON OTBD SHACKLE ATTACH FITTINGS CORRODED BETWEEN THE TWO NEAR BUSHINGS. BLENDED AREA WITHIN LIMITS IAW SRM 54-51-71, FIG 102.SDR IPXA2020012451295Shackle · corrodedINSPECTION TYPE:C, CORROSION ON #1 ENG PYLON OUTBRD SHACKLE INBRD SIDEREPLACED OUTBRD SHACKLE, PART #A5461004200200 S/N MEC150 OF #1 PYLON, IAW SRM 51-72-10SDR IPXA2020012451294Shackle · corrodedINSPECTION TYPE:CCORROSION ON OUTBRD, ONTBRD SIDE OF #1 ENG PYLONREPLACED SHACKLE, O/B PART #4561004200200 S/N UP61336 IAW SRM 51-72-10SDR AALA202001219011Bearing · excess playAIRCRAFT WAS GROUNDED: WHILE ACCOMPLISHING TASK CARD 26T41571002 RIGHT ENGINE AFT MOUNT OUTBOARD LINK UPPER BEARING HAS EXCESSIVE PLAY AND WEAR. REPLACED AFT ENGINE MOUNT ASSEMBLY PER AMM 71-22-11.SDR IPXA2020012451296Mount · deterioratedINSPECTION TYPE:C, NR 1 ENG PYLON AFT MOUNT FITTING BEAM ASSY PROTECTIVE FINISH DETERIORATEDRESTORED HIGH HEAT PRIMER @ #1 ENG PYLON AFT MOUNT FITTING IAW A300 SRM 54-51-00SDR IPXA2020020351753Fitting · gougedINSPECTION TYPE:3C#1 ENG. WING PYLON MOUNT I/B SIDE TRUSS FITTING IS GOUGED AT STA. YWN 200, ZWN=23 AND X=2.4.REPAIRED DAMAGED #1 ENG., WING PYLON I/B SIDE TRUSS FITTING AT NOTED LOCATION IAW VT-SAA EA 011-5410-01-A7976 REV. I/R AND UPS EO MD11-5410-75173-A. (SDR NACA2019122400157Fitting · crackedLEFT HAND ENGINE REAR ENGINE MOUNT HANGAR FITTING HAS PITTING CORROSION IN CONE BOLT MATING SURFACE. REPLACED #1 ENGINE REAR MOUNT HANGAR FITTING IAW B737-400 AMM 71-21-03 REV 90. SEE NDT REPORT NDT19-5645 FOR HANGAR BOLT INSPECTION. NO CRACKS FOUND. NEEDS PASDR DALA2019122427526Brace · corrodedLEFT ENG DRAG FITTING CLAMP & DIAG BRACE, STEP 27. CORROSION IN HOLES # 13, 14, AND 18, WAS FOUND. REPLACED PER ERA 583990-14AD REV. ORIG. SECTION 1 AND ETI-57-19-190 REV 13.SDR ASOA201912247139Yoke · crackedWHILE IN C CHECK, DISCOVERED THE RT ENGINE UPPER FORWARD PYLON YOKE CRACKED. REMOVED AND REPLACED YOKE FITTING. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE.SDR SIMA201912187001Yoke · crackedDURING HMBV INSPECTION, QC FOUND LH PYLON FWD LOWER YOKE FITTING CRACKED.-C/A-REMOVED AND REPLACED YOKE FITTING IAW ERS-EM-54MR-698.SDR ASOA2019121945118Yoke · crackedDURING MX INSPECTION THE #1 ENGINE FORWARD UPPER YOKE FITTING WAS FOUND CRACKED. MX R&R THE #1 ENGINE FORWARD UPPER YOKE FITTING IAW STS EA26-2014-063. A/C WAS APPROVED FOR RETURN TO SERVICE.SDR DALA2019121107227Fitting · corroded(AIRCRAFT 5645, L/P 1397114) CORROSION WAS FOUND ON HOLE #6 OF LH ENG DRAG FTG CLAMP-UP & DRAG BRACE IN REFERENCE TO WORK CARD 5720-01100-0101A-LH JOB #088-0001 STEP 26. CORRECTIVE ACTION: REPAIRED PER ER/A: 583471-14AD REV: ORIGINAL AND ETI-57-19-175 REV: 5.SDR DALA2019121107226Fitting · damaged(AIRCRAFT 5645, L/P 1396789) BROKEN PAINT AROUND OF FASTENER # 13 AT LH ENG DRAG FTG, ENGINE 1. CORRECTIVE ACTION: HOLE #13 WAS REPAIRED PER ER/A: 583471-14AD REV. ORIG. AND ETI-57-19-175 REV: 5. AND REPAIR APPROVAL IS LIMITED TO 24 MONTHS SERVICE ONLY TO NOV SDR 2019FA0000408Truss · crackedDURING SCHEDULED MAINTENANCE/ENGINE CHANGE, CONDUCTED THE SCHEDULED 1000 HOUR SPECIAL INSPECTION OF WELDS ON RH ENGINE TRUSS MOUNT ASSEMBLY (AAIP SPEC INSP #25). VERY SMALL (FINE) CRACK APPROX 3/4" LONG WAS OBSERVED WITH 16X MAGNIFYING GLASS PRIOR TO APPLICATISDR HNAA20191227001Yoke · crackedLEFT ENGINE FWD LOWER YOKE HAS CRACK ON FWD LOWER CORNER. R & R LH FWD YOKE FITTING AND GUSSET PLATE IAW EO1-71-19-0565.SDR ABXA201912104195Support Bracket · crackedCRACK IN THE LEFT PYLON AFT ENGINE MOUNT SUPPORT BULKHEAD, AFT SIDE UPPER BRACKET AT OUTBOARD SIDE FORWARD OF THE WIRE BUNDLE. THE BRACKET WAS REPLACED. THE AIRPLANE WAS GROUNDED.SDR AALA201910149014Bearing · wornAIRCRAFT IN BASE MAINTENANCE: NR 2 ENGINE AFT MOUNT INBOARD SIDE LINK BEARING MIGRATED. REPLACED LINK PER CMM 71-22-11-300-001.SDR DALA2019112390014Mount · damagedPD:DURING THE ACCOMPLISHMENT OF CMM 310T1020-3 ATA 71-21-11, REPAIR 3-2,ONE OF THE BEARING BORES WAS MACHINED TO THE MAXIMUM OVERSIZE &CORROSIO CA:AFTER REMOVAL OF THE CORROSION FINAL MEASUREMENTS WERE SENT TO BOEING.BOEING APPROVED OF THE DIMENSIONS AND PROVISDR YENA2019103010626Mount · crackedFT # 2601, BUF-JFK. FOUND CRACK ON PYLON LOWER LINK LUG ENG #1 INBD SIDE; REF LOGPAGE # 2482048-1 W/O# 1019537 FOR WORK PERFORMED. REF AEROMAN NR 2019-341092 WO 2019 35211 ACCOMPLISHED THE REPLACEMENT OF THE LH PYLON INBOARD UPPER SPAR WING USING ALTERNATE TOOSDR AALA201909169046Pin · corrodedAIRCRAFT WAS GROUNDED: #2 ENGINE AFT ENGINE MOUNT TOP OUTBOARD INNER PIN HAS PITTING. REPLACED PIN PER AMM 71-22-11-400-800.SDR FDEA2019080541796Mount · corrodedNR 2 ENGINE PYLON FORWARD ENGINE MOUNT, AFT BOLT HOLES HAVE EVIDENCE OF CORROSION. REPAIRED IAW EA 6-5451-T0348151SDR FDEA2023012701742Mount · corrodedNR 1 PYLON FORWARD ENGINE MOUNT AFT 2 HOLES HAVE EVIDENCE OF CORROSION. REPAIRED PER EA 6-5451-T0348198 P1.SDR FDEA2019073101742Mount · corroded#1 PYLON FORWARD ENGINE MOUNT AFT 2 HOLES HAVE EVIDENCE OF CORROSION. REPAIRED PER EA 6-5451-T0348198 P1SDR CA190730021Shock Absorber · failed(CAN) PAINT WAS FOUND MISSING ON PART OF THE SHORT SHAFT ATTACHED TO THE ENGINE, SUSPECTED CONTACT WITH FIREWALL. SHAFT INSPECTED AND FOUND SERVICEABLE, PAINT TOUCHED UP. SHOCK ABSORBER MOUNTS FOUND TO BE VERY WEAK ALLOWING THE BACK OF THE ENGINE TO SWAY BACK SDR ASOA201906287089Yoke · crackedDISCREPANCY: #2 FORWARD ENGINE YOKE CRACKED. CORRECTIVE ACTION: REMOVED AND REPLACED #2 FWD LOWER YOKE FITTING IN ACCORDANCE WITH EA 26-2014-06301.SDR QEMY20190625001Shackle · looseWHILE THE ENGINE IS IN THE INCOMING INSPECTION PROCESS, THE MAIN BEARING HOUSING OF THE FRONT MOUNT SHACKLE WAS LOOSE AND FREE TO ROTATE IN THE SHACKLE. THE BEARING HOUSING SHOULD NOT BE FREE TO ROTATE IN THE FRONT MOUNT SHACKLE.SDR CA190628005Bolt · missing(CAN) DURING INSPECTION, TECHNICIANS HAD FOUND DHC8-106 SN 324 WITH THE #1 ENGINE (P/N PW121 ENGINE S/N PCE-120144 MODULE S/N TM-120144) WITH THE FORWARD ENGINE MOUNT 2 TORQUE TUBE BOLTS HAVING FALLEN OUT.THERE DOES NOT APPEAR TO BE ANY VISUAL DAMAGE AND THE CSDR FXGA201906181949Mount · corrodedREPLACEMENT OF CORODED #2 ENGINE MOUNT FITTING. TO REPLACE CORRODED AFT ENGINE MOUNT FITTING AND TEE CHORDS AT #2 ENGINE POSITION. REMOVE AND REPLACE #2 ENGINE SUPPORT FITTING P/N 65-18670-1, CHORDS P/N 65-31281-3, 65-31281-4, 65-22913-5, 65-22913-6, AND WEBSDR REXA2019061501011Mount Fitting · nickedRT PYLON FWD ENGINE MOUNT FITTING AFT UPPER LUG IS NICKED AT THE AFT UPPER EDGE. REPAIRED IAW REO 601R-54-51-203 THIS IS A MAJOR REPAIR.SDR REXA2019061401001Yoke · nickedRT ENGINE YOKE HAS NICK ON THE IB FWD EDGE. REPAIRED IAW REO 601R-71-21-078.SDR ASOA201906117057Yoke · crackedA/C WAS IN C-CHECK WHEN INSPECTION FOUND THE NR 2 ENGINE LOWER YOLK CRACKED. MAINTENANCE REMOVED AND REPLACED THE #2 ENGINE YOLK IAW EA26-2014-06301. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.SDR SIMA2019062405008Yoke · crackedLT ENGINE FORWARD LOWER YOKE, FORWARD AFT RADIUS CRACKED (ERS-EM-54MR-698) -C/A-REMOVED AND REPLACED LH ENGINE FWD LOWER YOKE, FWD FITTING IAW ERS-EM-54MR-698.SDR DALA2019061790008Beam · wornPD:WHILE INSPECTING THE PN 221-0261-501 AFT MOUNT BEAM, DELTA FOUND WEARCOMMON TO THE SIDE WALL THAT IS BEYOND THE LIMITS OF CMM 71-20-05. THE CA:O/H PER CMM 221-0260-501, COMPLIED WITH ER/A 578346-14. DAMAGE WASCLEANED, VISUALLY AND FPI INSPECTED,BLENDED AND SDR DALA2019051603032Isolator · corroded(AIRCRAFT 682, L/P 1075071) HIDDEN CORROSION. AFTER ISOLATOR ASSEMBLY REMOVAL FROM FORWARD ENGINE MOUNT ISOLATOR A VISUAL INSPECTION WAS PERFORMED PER AMM 71-21-03-424-013-P00 PARAGRAPH E AND CORROSION WAS FOUND ON FORWARD ENGINE MOUNT BEAM. CORRECTIVE ACTION:SDR CA190503022Isolation Mount · torn(CAN) LH ENGINE, UPPER OUTBOARD ISOLATION MOUNT, FORWARD ISOLATOR FOUND COMPLETELY TORN AND UNSERVICEABLE. THE REMAINING THREE ISOLATOR MOUNTS ARE DETERIORATED AND REQUIRE REPLACEMENT. THERE WAS NO INDICATION OF FAULT OR ABNORMAL OCCURRENCES. (TC# 20190503022)SDR 2019FA0000119Mount · corrodedINTERNAL CORROSION OF THE ENGINE MOUNT ASSEMBLY P/N 20796-00.SDR REXA2019043011538Mount Fitting · gougedNR 1 ENG FWD MOUNT, AFT UPPER FITTING HAD TWO NICKS. COMPLIED WITH REO 601R-54-51-196, REMOVED THE NICK DAMAGE BY BLENDOUT, ROTOPEENED AND RESTORE FINISH.SDR MK1Y20190411008Strut · corrodedDEEP CORROSION FOUND ON LEFT ENGINE STRUT FRONT UPPER SPAR WEB, STA 230, LBL 8, WL 147.SDR DALA2019040902352Fitting · crackedSHIP 6702 DURING NDT ACCOMPLISHMENT OF PRI 576632-14, STEP #7, THE #2 ENGINE OUTBOARD DRAG FITTING WAS FOUND TO HAVE A CRACK-LIKE INDICATION, ON THE #14 HOLE, EXTENDING APPROXIMATELY 0.068" FROM THE HOLE ON THE UPPER SURFACE OF THE FITTING. CORRECTIVE ACTION: SDR CALA2019040500534Mount · crackedMETAL IS CRACKING AT INBOARD PYLON ENGINE ATTACH POINT ON NO.1ENG INE. TAPED ITEM 110 (MISSING) REF ECRA 5450-02357 PART 1D.SDR REXA2019042250466Mount · chafedNR 2 ENG FWD MOUNT FWD AFT AND UPPER LUG SMALL NICK AND MINOR CHAFF
C/W BOMBARDIER REO 601R-54-51-194 TO REMOVE CHAFE DAMAGE ROTO PEEN SURFACE FAND RESTORE FINISH (.003: MAX MATERIAL LOSS) AAR SM 39SDR AALA201903269021Spigot · gougedNR 2 ENGINE FORWARD MOUNT SPIGOT CENTER HOLE GOUGED. REPAIRED IAW EA A9-54R-34020.
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