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 UALA2011111006137Bushing · migratedNR 2 ENG AFT ENGINE MOUNT SHOWS BUSHING MIGRATION AT 3RD BOLT INBD FROM OTBD SIDE, LOWER ROW. SAMC TEXT: WHATEVER HARDWARE IS REMOVED, SEND TO ENG MOUNT SHOP WITH EG-ALERT TAG, FOR FAILURE INVESTIGATION. NEED TO BE SURE THAT EVERYTHING THAT MAY HAVE CONTRIBSDR I5EA20111105Support Fitting · corrodedDURING HFEC INSPECTION OF THE SIDE ENGINE FWD MOUNT SUPPORT FITTING FASTENER INSPECTION REQUIRED BY SB 727-54A0010. SURFACE CORROSION WAS FOUND. INFORMATION HAS BEEN SUBMITTED TO ENGINEERING FOR REVIEW AND DISPOSITION.SDR JR2R2011114100561Mount · corrodedRIGHT ENGINE FRONT MOUNT YOKE NICKED AT LOWER ENG ATTACHMENT. REPAIRED LOWER LUG ON RT ENG FRONT MOUNT YOKE IAW RO CRJ9-71-0093 AS ON WO 1007307-4200-0062 AND WO 711014235.SDR UALA2011102405755Bolt · brokenNR 2 ENGINE UPPER FWD ENGINE MOUNT HAS A LOWER ISOLATOR BOLT BROKEN. REPLACED BOLT.SDR VGCA2011101400001Mount · crackedDURING INSPECTION, A CRACK WAS DISCOVERED IN THE NR 3 AFT ENGINE MOUNT.SDR CA110930018Mount · debonded(CAN) RT AFT ENGINE MOUNT, PN 9912480-2 (PN LM-451-SA2) BONDED RUBBER INSERTS DEBONDED AND MIGRATED OUT PAST THE BOLTHEAD ON FRONT SIDE AND THE NUT ON THE AFT SIDE. THE REPLACEMENT SCHEDULE IS EVERY SECOND ENGINE CHANGE WHICH IN THIS CASE WOULD BE 10,000 HRS.SDR JR2R2011092800433Mount Fitting · gougedNR 2 ENGINE YOKE MOUNT FITTING GOUGED. COMPLETED PRP BLENDED DAMAGE IAW RO CRJ7-53-046.SDR CA101104012Mount · broken(CAN) BOTH MOUNTS BROKEN. CUSTOMER CALLED AND ASKED IF SB 719 APPLIES TO AIRCRAFT SN 448107057. THEY WERE ADVISED THAT ALTHOUGH IT IS NOT REQUIRED TO DO SB 719 ON AIRCRAFT, IT IS ADVISED TO CHECK AFFECTED AREAS FOR CRACKS WHEN INSPECTING PER MFG SB 937. CRACKSSDR SWIA201127661Link · corrodedLEFT ENGINE YOKE LINK HAS GALLING INSIDE BUSHING. (ENGINE CHANGE) REPLACED LEFT ENGINE YOKE LINK ASSEMBLY.SDR SWIA201127625Mount · corrodedRIGHT ENGINE YOKE MOUNT SPHERICAL BUSHINGS PITTED. (ENGINE CHANGE) REPLACED RIGHT ENGINE YOKE MOUNT.SDR SWIA201127462Spherical Bearin · damagedFORWARD YOKE LINK SPHERICAL BEARING PITTED. (ENGINE CHANGE) REPLACED RIGHT ENGINE FORWARD YOKE LINK ASSEMBLY.SDR SWIA201127367Mount · corrodedLEFT ENGINE FORWARD YOKE MOUNT BEARINGS ARE CORRODED. (ENGINE CHANGE) INSTALLED A SERVICEABLE FORWARD YOKE MOUNT ASSEMBLY ON THE LEFT ENGINE DURING THE ENGINE CHANGE.SDR SWIA201127382Link Assy · corrodedLEFT ENGINE FORWARD YOKE UPPER LINK AND CLAMP UP BUSHING HAVE PITTING CORROSION. (ENGINE CHANGE) REPLACED THE LEFT ENGINE FORWARD YOKE UPPER LINK ASSEMBLY.SDR CA110826011Mount · cracked(CAN) ENGINE MOUNT TUBE CRACKED AT NOSE GEAR OLEO UPPER ATTACH POINT- RT SIDE DIAGONAL TUBE FROM RT LOWER ENGINE MOUNT, TOO UPPER NOSE GEAR ATTACH POINT, AND LT LOWER DIAGONAL TUBE FROM LOWER LT FIRE WALL ATTACH POINT TO LOWER NOSE GEAR ATTACH POINT. (CRACKED SDR UALA2011082304506Bolt · unsecureFOUND AFT INBD BOLT ON ENG AFT MOUNT NOT SEATED. REPLACED ALL AFT MOUNT BOLTS AND AFT MOUNT ON SMB W-US Q0508E & Y1556H.SDR 29GA94971081911ATruss · damagedREPORT: DURING MAGNETIC PARTICLE INSPECTION DISCOVERED ENGINE TRUSS TUBE DAMAGED. PERFORMED ENGINE TRUSS REPAIR IN ACCORDANCE WITH FAA APPROVED DATA CONTAINED IN DRAWING 1005272-7, 8110-3, DERT-510208-CE.SDR 29GA94771081911ATruss · damagedREPORT: DURING MAGNETIC PARTICLE INSPECTION DISCOVERED ENGINE TRUSS TUBE DAMAGED. PERFORMED ENGINE TRUSS REPAIR IN ACCORDANCE WITH FAA APPROVED DATA CONTAINED IN DRAWING 1005272-5, 8110-3, DERT-510208-CE.SDR 29GA94071081911ATruss · damagedREPORT: DURING MAGNETIC PARTICLE INSPECTION DISCOVERED ENGINE TRUSS TUBES DAMAGED. PERFORMED ENGINE TRUSS REPAIR IN ACCORDANCE WITH FAA APPROVED DATA CONTAINED IN DRAWING 1005272-4,8110-3, DERT-510208-CE.SDR 29GA94071081911Truss · damagedREPORT: DURING MAGNETIC PARTICLE INSPECTION DISCOVERED ENGINE TRUSS TUBES DAMAGED. PERFORMED ENGINE TRUSS REPAIR IN ACCORDANCE WITH FAA APPROVED DATA CONTAINED IN DRAWING 1005272-4,8110-3, DERT-510208-CE.SDR CA110817004Isolator · separated(CAN) UPON INSPECTION OF THE ENGINE MOUNT ISOLATORS THAT MAKEUP AN ASSY, IT WAS NOTED THAT IT WAS SEPARATED WHEN THE ASSY WAS TAKEN APART. THE ASSY HAS 3 ISOLATORS IN 1 HSG SN OF ALL 3 ISOLATORS FROM THE SAME.SDR SWIA201127216Spherical Bearin · corrodedRIGHT ENGINE, AFT MOUNT SPHERICAL BUSHING AND HOUSING ARE PITTED. (ENGINE CHANGE) REPLACED RIGHT ENGINE, AFT MOUNT SPHERICAL BUSHING AND HOUSING.SDR FDEA201108103181Mount · corrodedNR 2 PYLON FWD ENG MOUNT STRUT FITTING WITH CORROSION ON LOWER SURFACE FWD AND AFT MOUNT MATING. REMOVED CORROSION BY BLENDING AREA PER SRM-54-51-90 PG.104 FIG.101 DET.VII, REMOVED AND REPLACED FWD. STRUT MOUNT FITTING, PER SRM-51-40-02.SDR UIEA2011072800394Mount · crackedDURING INSP OF THE NR 4 PYLON REAR ENGINE MOUNT NAC STA 270 BULKHEAD, 1 CRACK WAS FOUND ON THE SUBJECT UPPER SIDE RT BULKHEAD CHORD (PN 65B94107-54) FROM THE MOST INBD FLANGE TOWARDS THE SECOND FASTENER HOLE. THE CRACK IS APPROX 1.72" LONG. (THE DAMAGE WAS RESDR C2XA11TY107Yoke · crackedTYS - A/C IS IN C-CHECK WHEN INSPECTION FOUND THE NR 1 ENGINE FWD LWR YOKE WAS CRACKED. MAINTENANCE REMOVED AND REPLACED THE NR 1 FWD LWR YOKE FITTING IAW EC 5450-01028. A/C WILL BE RELEASED AT THE END OF THE CHECK.SDR 29GA94971071111ATruss · crackedDURING MAGNETIC PARTICLE INSPECTION DISCOVERED ENGINE TRUSS COWLING ATTACH BRACKETS WELD AREA CRACKS AND FORWARD LOWER ENGINE MOUNT ATTACH POINTS WELD AREA CRACKS. PERFORMED WELD REPAIR TO ENGINE TRUSS ATTACH BRACKETS WELD AREAS AND FORWARD LOWER ENGINE MOUNTSDR 2011F00162Mount · crackedDURING EDDY CURRENT CHECK, PYLON NR 3 REAR ENGINE MOUNT BULKHEAD OTBD UPPER AFT FRAME FOUND WITH CRACK. CRACK LENGTH APPROX 10MM. FINDING DISCOVERED DURING 'C1 & C2' CHECK. (OPEN)SDR 2011F00160Mount · crackedCRACK DETECTED DURING LOW FREQUENCY EDDY CURRENT CHECK ON NR3 PYLON REAR ENGINE MOUNT BULKHEAD UPPER CAP SKIN STRAP ADJACENT TO FRONT SPAR FITTING. FINDING DISCOVERED DURING 'C1+C2' CHECK FROM 08 JUN 2011 TO 22 JULY 2011. (OPEN)SDR 2011F00159Mount · crackedCRACKS FOUND ON NR 2 PYLON REAR ENGINE MOUNT UPPER BULKHEAD INBD AND OTBD FRAME HORIZ FLANGE. EACH CRACK APPROX 0.500" IN LENGTH. FINDING DISCOVERED DURING 'C1 & C2' CHECK.SDR 29GA94671062911ATruss · crackedDURING MAGNETIC PARTICLE INSPECTION DISCOVERED ENGINE TRUSS COWLING ATTACH BRACKETS WELD AREA CRACKS AND RIGHT FORWARD LOWER ENGINE MOUNT ATTACH POINT WELD AREA CRACK. PERFORMED WELD REPAIR TO ENGINE TRUSS ATTACH BRACKETS WELD AREAS AND RIGHT FORWARD LOWER ENSDR 29GA94971062811ATruss · crackedDURING MAGNETIC PARTICLE INSPECTION DISCOVERED ENGINE TRUSS COWLING ATTACH BRACKETS WELD AREA CRACKS AND RIGHT FORWARD LOWER ENGINE MOUNT ATTACH POINT WELD AREA CRACK. PERFORMED WELD REPAIR TO ENGINE TRUSS ATTACH BRACKETS WELD AREAS AND RIGHT FORWARD LOWER ENSDR SWIA201126581Mount · corrodedRIGHT ENGINE FORWARD YOKE MOUNT HAS CORROSION ON SPHERICAL BUSHING. (ENGINE CHANGE) REPLACED FORWARD YOKE MOUNT ASSEMBLY ON RIGHT ENGINE.SDR SWIA201126495Link · corrodedTHE LEFT ENGINE FORWARD ENGINE MOUNT UPPER LINK ASSEMBLY IS PITTED. (ENGINE CHANGE) NEW LEFT ENGINE FORWARD MOUNT LINK ASSEMBLY INSTALLED DURING ENGINE INSTALLATION.SDR 2011F00142Mount · damagedLEFT AND RIGHT ENGINE, BOTH FRONT MOUNT UPPER HALVES COMPRESSED EXCESSIVELY. THE LT FRONT MOUNT ON THE LT AND RT ENGINE WERE EXPOSING .2500" OF INNER BARREL. SUBSEQUENTLY, THE LT ENGINE NR 6 CYLINDER HEADER TUBE RUBBED THE ENGINE BEAM EXTENSION. IT HAS NOT BESDR JR2R2011060300232Mount · gougedRIGHT FORWARD ENGINE MOUNT LUG GOUGED.SDR SWIA201126339Link · corrodedLEFT ENGINE FORWARD YOKE MOUNT LINK HAS PITTING. (ENGINE CHANGE) INSTALLED NEW FORWARD YOKE MOUNT LINK AT LEFT ENGINE.SDR SWIA201126313Yoke · corrodedRIGHT ENGINE YOKE MOUNT LINK ASSEMBLY IS CORRODED. (ENGINE CHANGE) REPLACED THE RIGHT ENGINE UPPER YOKE LINK ASSEMBLY.SDR SWIA201126299Link · galledLEFT ENGINE FORWARD MOUNT LINK ASSEMBLY GALLED. (ENGINE CHANGE) REPLACED LEFT ENGINE FORWARD MOUNT LINK ASSEMBLY.SDR REXA201100276Shaft · scoredRT ENGINE THRUST SHAFT SCORED APPROXIMATELY 0.002 INCH ON THREADED END AROUND ENTIRE SURFACE. REPAIRED IAW BOMBARDIER CMM CMM 71-22-05.SDR SWIA201126238Link · corrodedRIGHT ENGINE, YOKE MOUNT LINK ASSEMBLY IS CORRODED. (ENGINE CHANGE) REPLACED THE RIGHT ENGINE YOKE LINK ASSEMBLY.SDR CA110430001Isolator · corroded(CAN) DURING SCHEDULED 3600 HOUR REPLACEMENT OF ENGINE ISOLATORS, ISOLATOR WAS FOUND CORRODED ONCE REMOVED FROM THE AIRCRAFT. THE MOUNTING DESIGN OF THE ISOLATOR DOES NOT ALLOW A VISUAL INSPECTION OF THIS AREA OF THE ISOLATOR. IT COULD ONLY BE OBSERVED ONCE RESDR SWIA201126148Yoke · galledLEFT ENGINE FORWARD MOUNT YOKE ASSEMBLY HAVE GALLING. (ENGINE CHANGE) REPLACED LEFT ENGINE FORWARD MOUNT YOKE ASSEMBLY.SDR NX4R000013Mount · crackedDURING ROUNTINE MX, THE TECH WAS PERFORMING A PRELIMINARY/HIDDEN DAMAGE INSP OF THE AREA SURROUNDING THE AREA WHERE WORK WAS TO BE PERFORMED. NOTICED THE SMALL TUBE THAT IS WELDED TO THE LOWER ENGINE MOUNT TUBE THAT THE LOWER COWL IS MOUNTED TO, WAS MOVING SLISDR SWIA201126099Link · corrodedRIGHT ENGINE FORWARD THRUST MOUNT, UPPER LINK ASSEMBLY IS PITTED. (ENGINE CHANGE) REPLACED RIGHT ENGINE FORWARD, UPPER LINK ASSEMBLY.SDR SWIA201126089Link · corrodedLEFT ENGINE FORWARD YOKE MOUNT LINK IS CORRODED. (ENGINE CHANGE) REPLACED LEFT ENGINE FORWARD YOKE MOUNT LINK ASSEMBLY.SDR ABXR2011122200052Mount · corrodedNR 2 ENGINE AFT MOUNT CORRODED. INSTALLED NEW MOUNT IAW AMM 71-21-02.SDR FDEA201104141477Mount · corrodedNR 2 PYLON ENGINE FWD MOUNT LT FWD BOLT HOLE FOUND WITH CORROSION. REPAIRED AS PER E.A. 6-5450-150314 PART 1. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REVISION 112.SDR FDEA201104141479Mount · corrodedNR 2 PYLON ENG AFT MOUNT LT FWD BOLT HOLE FOUND WITH CORROSION. REWORKED AS PER E.A. 6-5450-143900 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 112.SDR FDEA201104141478Mount · corrodedNR 2 PYLON ENGINE FWD MOUNT LT AFT BOLT HOLE FOUND WITH CORROSION. REPAIRED AS PER E.A. 6-5450-150314 PART 1. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REVISION 112.SDR FDEA201104141476Mount · corrodedNR 2 PYLON ENGINE AFT MOUNT LT AFT BOLT HOLE FOUND WITH CORROSION. REWORKED AS PER E.A. 6-5450-143900 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 112.SDR SWIA201126018Link · corrodedRIGHT ENGINE FORWARD MOUNT UPPER LINK ASSEMBLY IS CORRODED. (ENGINE CHANGE) REPLACED RIGHT ENGINE FORWARD MOUNT UPPER LINK ASSEMBLY.
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