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.

SDR CA100819012Mount · crackedENGINE MOUNT SENT IN FROM JCAB REGISTERED ACFT. ENGINE MOUNT IS CURRENT REVISION OF THE 89137-002 ENGINE MOUNT WITH "1 PIECE" ACTUATOR ATTACHMENT PIECE. ACFT IS NOT INCLUDED IN INSP IAW SB 1103C. REF FAILURES OF PARTS 89137-002, 89137-02, 89137-41, 84010-02,Jan 6, 2010 · Piper PA46350PSDR SWIA201023414Mount · corrodedLEFT ENGINE FORWARD LINK AND BUSHING PITTED. (ENG CHANGE) REPLACED YOKE LINK AND BUSHING.Jan 6, 2010 · N913SW · Cndair CL6002B19SDR SWIA201023420Mount · corrodedLEFT ENGINE MOUNT UPPER YOKE LINK AND BUSHING CORRODED. (ENG CHANGE) REPLACED LEFT ENGINE MOUNT UPPER YOKE LINK AND BUSHING.Jan 3, 2010 · N752SK · Cndair CL6002C10SDR C2XA10TY001Fitting · crackedNR 1 ENGINE FWD LWR YOKE WEBBING IS CRACKED. REMOVED AND REPLACED FWD YOKE LWR LINKAGE FITTING IAW EC5450-01028.Jan 1, 2010 · N15574 · Emb EMB145LRSDR SWIA200923395Mount · gougedLEFT ENGINE MOUNTS PITTED AND GOUGED. (ENG CHANGE) REPLACED MOUNTS AND BUSHINGS AS REQUIRED.Dec 27, 2009 · N750SK · Cndair CL6002C10SDR SWIA200923356Mount · corrodedUPPER FORWARD ENGINE MOUNT CORRODED. (ENG CHANGE) REPLACED UPPER FORWARD ENGINE MOUNT ASSEMBLY.Dec 20, 2009 · N748SK · Cndair CL6002C10SDR SWIA200923301Mount · corrodedRIGHT ENGINE FORWARD MOUNT, BEARING SURFACES ARE CORRODED. (ENG CHG) REPLACED RIGHT ENGINE FORWARD MOUNT.Dec 18, 2009 · N403SW · Cndair CL6002B19SDR SWIA200923264Mount Fitting · corrodedFORWARD ENGINE MOUNT LINK AND BUSHING CORRODED. (ENG CHANGE)REPLACED LINK AND BUSHING PER AMM.Dec 14, 2009 · N821SK · Cndair CL6002D24SDR SWIA200923181Mount · corrodedLEFT ENGINE FORWARD ENGINE MOUNT PITTED AND CORRODED. (ENG CHANGE) REPLACED MOUNT PER AMM.Dec 1, 2009 · N941SW · Cndair CL6002B19SDR SWIA200923159Bushing · corrodedRIGHT ENGINE YOKE MOUNT LINK BUSHINGS CORRODED. (ENGINE CHANGE) REPLACED RIGHT ENGINE YOKE MOUNT LINK BUSHING PER AMM.Nov 24, 2009 · N457SW · Cndair CL6002B19SDR C2XA09SH435Mount · crackedSHV - DURING C-CHECK, RT ENG FWD LOWER MOUNT CRACKED. REMOVED AND REPLACED RT ENG FWD LOWER MOUNT IAW EC 5450-01028. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Nov 22, 2009 · N19966 · Emb EMB145LRSDR CA091117004Mount · broken(CAN) FOUND ON ANNUAL INSPECTION, FORWARD END OF LOWER RT ENGINE MOUNT TUBE MEMBER BROKEN COMPLETELY AROUND TUBE AT DATA PLATE ATTACH RIVETS LOCATION. FAILURE LOOKS LIKE IT BEGAN AT THE FORWARD END OF THE DATA PLATE ATTACHING RIVETS. MAY HAVE CRACKED FROM RINov 16, 2009 · Beech 3NMSDR SWIA200923067Mount Fitting · corrodedRIGHT ENGINE FORWARD MOUNT LINK AND BUSHING CORRODED. (ENG CHANGE) REPLACED MOUNT LINK AND BUSHING PER AMM.Nov 14, 2009 · N751SK · Cndair CL6002C10SDR FDEA200911123935Mount · corrodedNR1 ENG PYLON FWD ENG MOUNT PAD CORRODED. REMOVED CORROSION AT NR 1 ENG PYLON FWD LWR WEB (MOUNT) IAW SRM 54-50-01. ORIG MAT THICKNESS AT FWD BLENDOUT AREA .263, AFTER REWORKED .261, AND AT MIDDLE BLENDOUT AREA ORIG MAT THICKNESS .264, AFTER REWORKED .261, ANNov 12, 2009 · N907FD · Boeing 7572B7SDR SWIA200923027Bearing · corrodedLEFT ENGINE FORWARD YOKE BEARINGS AND LINK CORRODED. (ENG CHANGE) REPLACED YOKE AND LINK PER AMM.Nov 3, 2009 · N408SW · Cndair CL6002B19SDR C2XA09SH394Mount · corrodedSHV - DURING C-CHECK RT ENGINE FRONT MOUNTING FLANGE HAS ON CORRODED (LEVEL 2 LOCAL) BOLT HOLE. MAINTENANCE CLEANED, REAMED AND POLISHED ONE CORRODED HOLE AT RT ENGINE FRONT MOUNTING FLANGE IAW EMB-145 RR AE3007A; 72-25-30. THE AIRCRAFT WAS APPROVED FOR RETUOct 31, 2009 · N16963 · Emb EMB145LRSDR C2XA09SH393Mount · corrodedSHV - DURING CHECK LT ENG FRONT MOUNTING FLANGE HAS 24 CORRODED (LEVEL 2 LOCAL) BOLT HOLES. MAINTENANCE CLEANED, REAMED AND POLISHED UP TO 0.306 CORRODED HOLES AT 24 LT ENG MOUNTING FLANGE BOLT HOLES IAW EMB-145 RR AE3007A; 72-25-30. THE AIRCRAFT WAS APPROVEOct 31, 2009 · N16963 · Emb EMB145LRSDR CA091027009Bolt · loose(CAN) DURING ANNUAL INSPECTION, THE MAIN ENGINE MOUNT THROUGH BOLTS WERE FOUND TO BE LOSSENED OFF ACCORDING TO THE WITNESS MARKINGS. ONE BOLT INDICATED LESS THAN30 FT LBS OF TORQUE, THE REQUIRED TORQUE VALUE IS 80 FT LBS. ALL 8 BOLTS WERE FOUND LOOSENED. THE BOct 23, 2009 · Gruman FIRECATSDR 2009FA0000853Mount · corrodedSEVERE INTERNAL CORROSION FOUND IN THE MOUNT ASSEMBLY TUBING DUE TO INGRESS OF MOISTURE CAUSED BY LACK OF INTERNAL CORROSION PROTECTION AND LACK OF EXTERNAL SEALING.Oct 20, 2009 · N901AH · Agusta A109ESDR 2009FA0000869Mount · corrodedSEVERE INTERNAL CORROSION FOUND IN THE MOUNT ASSEMBLY TUBING DUE TO INGRESS OF MOISTURE CAUSED BY LACK OF INTERNAL CORROSION PROTECTION AND LACK OF EXTERNAL SEALING.Oct 16, 2009 · N907AH · Agusta A109ESDR 2009FA0000868Mount · corrodedSEVERE INTERNAL CORROSION FOUND IN THE MOUNT ASSEMBLY TUBING DUE TO INGRESS OF MOISTURE CAUSED BY LACK OF INTERNAL CORROSION PROTECTION AND LACK OF EXTERNAL SEALING.Oct 16, 2009 · N907AH · Agusta A109ESDR 2009FA0000867Mount · corrodedSEVERE INTERNAL CORROSION FOUND IN THE MOUNT ASSEMBLY TUBING DUE TO INGRESS OF MOISTURE CAUSED BY LACK OF INTERNAL CORROSION PROTECTION AND LACK OF EXTERNAL SEALING.Oct 16, 2009 · N907AH · Agusta A109ESDR 2009FA0000866Mount · corrodedSEVERE INTERNAL CORROSION FOUND IN THE MOUNT ASSEMBLY TUBING DUE TO INGRESS OF MOISTURE CAUSED BY LACK OF INTERNAL CORROSION PROTECTION AND LACK OF EXTERNAL SEALING.Oct 16, 2009 · N905AH · Agusta A109ESDR 2009FA0000865Mount · corrodedSEVERE INTERNAL CORROSION FOUND IN THE MOUNT ASSEMBLY TUBING DUE TO INGRESS OF MOISTURE CAUSED BY LACK OF INTERNAL CORROSION PROTECTION AND LACK OF EXTERNAL SEALING.Oct 16, 2009 · N905AH · Agusta A109ESDR 2009FA0000864Mount · corrodedSEVERE INTERNAL CORROSION FOUND IN THE MOUNT ASSEMBLY TUBING DUE TO INGRESS OF MOISTURE CAUSED BY LACK OF INTERNAL CORROSION PROTECTION AND LACK OF EXTERNAL SEALING.Oct 16, 2009 · N905AH · Agusta A109ESDR 2009FA0000863Mount · corrodedSEVERE INTERNAL CORROSION FOUND IN THE MOUNT ASSEMBLY TUBING DUE TO INGRESS OF MOISTURE CAUSED BY LACK OF INTERNAL CORROSION PROTECTION AND LACK OF EXTERNAL SEALING.Oct 16, 2009 · N904AH · Agusta A109ESDR 2009FA0000862Mount · corrodedSEVERE INTERNAL CORROSION FOUND IN THE MOUNT ASSEMBLY TUBING DUE TO INGRESS OF MOISTURE CAUSED BY LACK OF INTERNAL CORROSION PROTECTION AND LACK OF EXTERNAL SEALING.Oct 16, 2009 · N904AH · Agusta A109ESDR 2009FA0000861Mount · corrodedSEVERE INTERNAL CORROSION FOUND IN THE MOUNT ASSEMBLY TUBING DUE TO INGRESS OF MOISTURE CAUSED BY LACK OF INTERNAL CORROSION PROTECTION AND LACK OF EXTERNAL SEALING.Oct 16, 2009 · N904AH · Agusta A109ESDR 2009FA0000860Mount · corrodedSEVERE INTERNAL CORROSION FOUND IN THE MOUNT ASSEMBLY TUBING DUE TO INGRESS OF MOISTURE CAUSED BY LACK OF INTERNAL CORROSION PROTECTION AND LACK OF EXTERNAL SEALING.Oct 16, 2009 · N903AH · Agusta A109ESDR 2009FA0000859Mount · corrodedSEVERE INTERNAL CORROSION FOUND IN THE MOUNT ASSEMBLY TUBING DUE TO INGRESS OF MOISTURE CAUSED BY LACK OF INTERNAL CORROSION PROTECTION AND LACK OF EXTERNAL SEALING.Oct 16, 2009 · N903AH · Agusta A109ESDR 2009FA0000858Mount · corrodedSEVERE INTERNAL CORROSION FOUND IN THE MOUNT ASSEMBLY TUBING DUE TO INGRESS OF MOISTURE CAUSED BY LACK OF INTERNAL CORROSION PROTECTION AND LACK OF EXTERNAL SEALING.Oct 16, 2009 · N903AH · Agusta A109ESDR 2009FA0000855Mount · corrodedSEVERE INTERNAL CORROSION FOUND IN THE MOUNT ASSEMBLY TUBING DUE TO INGRESS OF MOISTURE CAUSED BY LACK OF INTERNAL CORROSION PROTECTION AND LACK OF EXTERNAL SEALING.Oct 16, 2009 · N901AH · Agusta A109ESDR 2009FA0000854Mount · corrodedSEVERE INTERNAL CORROSION FOUND IN THE MOUNT ASSEMBLY TUBING DUE TO INGRESS OF MOISTURE CAUSED BY LACK OF INTERNAL CORROSION PROTECTION AND LACK OF EXTERNAL SEALING.Oct 16, 2009 · N901AH · Agusta A109ESDR 2009FA0000857Mount · corrodedSEVERE INTERNAL CORROSION FOUND IN THE MOUNT ASSEMBLY TUBING DUE TO INGRESS OF MOISTURE CAUSED BY LACK OF INTERNAL CORROSION PROTECTION AND LACK OF EXTERNAL SEALING.Oct 15, 2009 · N902AH · Agusta A109ESDR 2009FA0000856Mount · corrodedSEVERE INTERNAL CORROSION FOUND IN THE MOUNT ASSEMBLY TUBING DUE TO INGRESS OF MOISTURE CAUSED BY LACK OF INTERNAL CORROSION PROTECTION AND LACK OF EXTERNAL SEALING.Oct 15, 2009 · N902AH · Agusta A109ESDR 2009FA0000847Tube · corrodedDURING A DAILY INSPECTION, NR 1 ENGINE REAR SUPPORT LEG WAS FOUND SHEARED AT MIDPOINT. DAMAGE OCCURRED DUE TO SEVERE INTERNAL CORROSION OF THE STEEL TUBE. THE DAMAGE WAS HIDDEN BEHIND A CLAMP THAT SECURES A WIRE BUNDLE TO THE MOUNT LEG. AT LEAST 2 MORE IDENTOct 15, 2009 · N902AH · Agusta A109ESDR SWIA200923726Mount Bolt · out of toleranceRIGHT ENGINE MOUNT BOLT AND THRUST MOUNT OUT OF TOLERANCE. (C CHECK) REPLACED PER AMM.Oct 14, 2009 · N431SW · Cndair CL6002B19SDR SWIA200922862Bushing · corrodedRIGHT ENGINE FORWARD MOUNT LINK BUSHINGS AND BEARING CORRODED. (ENG CHG) REPLACED LINK AND BUSHINGS PER AMM.Oct 14, 2009 · N740SK · Cndair CL6002C10SDR SWIA200922863Bushing · corrodedLEFT ENGINE YOKE LINK BOLT BUSHING CORRODED. (ENG CHG) REPLACED BOLT BUSHING PER AMM.Oct 13, 2009 · N719SK · Cndair CL6002C10SDR C2XA09SH343Fitting · crackedDURING C-CHECK, NR 1 ENG FWD LOWER YOKE FITTING CRACKED. REMOVED AND REPLACED FWD LOWER YOKE FITTING IAW EC5450-01021. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Oct 13, 2009 · N14939 · Emb EMB145EPSDR FDEA200910063483Mount · corrodedNR 2 ENG PYRAMID FITTING HAS CORROSION ON LWR SURFACE AND AFT LT MOUNT HOLE. REAMED LT AFT MOUNT HOLE SRM 54-51-81; FIG 104; SHEET 2 TO 0.965 IN 4TH OVER-SIZE. REMOVED 0.002 IN PITTING CORROSION IN LT AFT MOUNT HOLE BY LOCAL BLEND OUT SRM 54-51-81; FIG 104; Oct 6, 2009 · N659FE · Airbus A300F4605RSDR SWIA200922728Bushing · corrodedLEFT ENGINE FWD MOUNT LINK BUSHINGS HAVE CORROSION PITTING. (ENGINE CHANGE) REPLACED LEFT ENGINE FWD MOUNT LINK BUSHINGS IAW AMM 71-21-01.Sep 29, 2009 · N738SK · Cndair CL6002C10SDR GUUA95271092809ATruss · crackedDURING MAGNETIC PARTICLE INSP, DISCOVERED 2 ENGINE TRUSS TUBES HAVE WELD AREA CRACKS. PERFORMED WELD REPAIR TO ENG TRUSS TUBES WELD AREAS.Sep 28, 2009 · N87552 · Beech 1900DSDR SWIA200922723Link · corrodedLEFT ENGINE FORWARD UPPER ENGINE MOUNT LINK FOUND CORRODED. (ENG CHANGE) REPLACED LEFT ENGINE FORWARD UPPER ENGINE MOUNT LINK ASSY IAW AMM 71-21-01.Sep 28, 2009 · N743SK · Cndair CL6002C10SDR YENA20090909117Shear Pin · crackedPLEASE DISREGARD SDR YENA20090909116 FOR AIRCRAFT N289JB MSN 19000002 DATE 09/18/09. DURING 6000 HR CHECK, A VISUAL INSPECTION OF THE LT PYLON AFT OUTBOARD PYLON TO WING ATTACH FITTING SHEAR PIN WAS FOUND CRACKED. REMOVED AND REPLACED THE OUTBOARD SHEAR PIN Sep 18, 2009 · N289JB · Emb ERJ190200IGWSDR YENA20090909119Shear Pin · crackedDURING 6000 HR CHECK AT EMBRAER AIRCRAFT MAINTENANCE SERVICES BNA, A VISUAL INSPECTION OF THE RT PYLON AFT INBOARD PYLON TO WING FITTING ATTACH SHEAR PIN FOUND CRACKED. REMOVED AND REPLACED THE INBOARD SHEAR PIN IAW EMBRAER IC 2009-190/07333A.Sep 18, 2009 · N289JB · Emb ERJ190100IGWSDR YENA20090909118Shear Pin · crackedDURING 6000 HR CHECK, A VISUAL INSPECTION OF THE LT PYLON AFT INBOARD PYLON TO WING ATTACH FITTING SHEAR PIN CRACKED. REMOVED AND REPLACED THE INBOARD SHEAR PIN ASSEMBLY IAW EMBRAER IC 2009-190/0733A.Sep 18, 2009 · N289JB · Emb ERJ190100IGWSDR YENA20090909116Shear Pin · crackedDURING 6000 HR CHECK, A VISUAL INSPECTION OF THE LT PYLON AFT OUTBOARD PYLON TO WING ATTACH PIN CRACKED. REMOVED AND REPLACED THE OUTBOARD AFT SHEAR PIN IAW EMBRAER IC 2009-190/07333A.Sep 18, 2009 · N289JB · Emb ERJ190100IGWSDR 2009F00083Shear Pin · brokenDURING HEAVY MX, A SHEAR PIN ON THE NR 2 ENG WAS OBSERVED TO BE BROKEN INTO 2 PIECES. THIS OBSERVATION MADE FOLLOWING THE DETECTION OF 2 BROKEN SHEAR PINS ON THE NR 1 ENG.Sep 17, 2009 · N289JB · Emb ERJ190200IGWSDR SWIA200922514Link · corrodedLEFT FORWARD ENGINE MOUNT LINK BUSHINGS AND SPHERICAL BEARING CORRODED. (SVC CHECK) REPLACED LEFT FORWARD ENGINE MOUNT LINK.Sep 5, 2009 · N812SK · Cndair CL6002D24
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