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 USAA2011011990262Pin · corrodedSAL - S5 - MAJOR REPAIR - CORROSION ON PIN OF NR 2 ENGINE AFT ENGINE MOUNT LOWER OUTBOARD POSITION BETWEEN PYLON STA 6465 TO STA 7063 & BETWEEN RIB 3 TO RIB 5. REPLACED PIN OF NR 2 ENGINE AFT ENGINE MOUNT LOWER OUTBOARD POSITION IAW A320 AMM 71-22-11-0401.Dec 21, 2010 · N624AW · Airbus A320231SDR C2XA10SH433Yoke · crackedSHV - DURING C-CHECK NR 2 ENGINE LOWER FWD YOKE CRACKED. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE LOWER FWD YOKE IAW EC5450-01028. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Dec 19, 2010 · N14902 · Emb EMB145LRSDR GUUA94071121710ABracket · crackedDURING MAGNETIC PARTICLE INSP, DISCOVERED ENGINE TRUSS COWL BRACKET WELD AREAS CRACKED. PERFORMED WELD REPAIR TO ENGINE TRUSS COWL BRACKET WELD AREA CRACKS. FOUND DURING MAGNETIC PARTICLE INSP.Dec 17, 2010 · N16540 · Beech 1900DSDR CA101213007Mount · damaged(CAN) DURING UNSCHEDULED MAINTENANCE INSPECTION, IT WAS NOTED THAT THE ENGINE MOUNT BULKHEADS WERE WORKING. THE ENGINE MOUNTS WERE REMOVED AND IT WAS OBSERVED THAT BOTH THE LH AND RH KEEL BULKHEAD SKINS WERE SHATTERED FROM YEARS OF WORK HARDENING. THERE IS CDec 13, 2010 · Cessna U206GSDR CA110104010Tube · mismanufacturedDURING BUILD-UP OF A METRO 2 ENGINE AS A SPARE FOR A "QUICK CHANGE", THE TECHNICIAN NOTICED THE ADEL CLAMPS WOULD NOT HOLD SECURELY TO THE MOUNT. FURTHER INVESTIGATION REVEALED THAT 2 TUBES WERE UNDER THE MANUFACTURERS MINIMUM DIMENSIONS. THE MOUNT WILL BE SDec 9, 2010SDR FDEA201012054582Mount · gougedNR1 PYLON FWD ENGINE MOUNT FITTING CTR GUIDE PIN HOLE HAS A GOUGE ON INNER DIAMETER. (SPIGOT GUIDE HOLE). REMOVED NR1 PYLON FWD MOUNT FITTING IAW SRM 51-40-21, PG 7 AND SRM 54-51-81, FIG 1, PG 202. REPAIRED NR1 PYLON FWD MOUNT FITTING (SPIGOT GUIDE HOLE BY Dec 5, 2010 · N660FE · Airbus A300F4605RSDR SWIA201025257Housing · corrodedRIGHT PYLON AFT ENGINE MOUNT HOUSING HAS PITTING. (ENGINE CHANGE) REPLACED RIGHT PYLON AFT ENGINE MOUNT HOUSING WITH SERVICABLE PART.Dec 4, 2010 · N944SW · Cndair CL6002B19SDR USAA2010120892925Shear Pin · corrodedSAL - MAJOR REPAIR - S5 - CORROSION WAS FOUND BETWEEN RIB 4 AND RIB 5 ON INNER PIN, LOCATED AT LEFT UPPER FROM LINK PIN ASSY OF AFT ENGINE MOUNT (ENGINE NR 1). REPLACED INNER PIN BETWEEN RIB 4 AND RIB 5 LOCATED AT LEFT UPPER FROM LINK PIN ASSY OF AFT ENGINE MDec 3, 2010 · N628AW · Airbus A320231SDR USAA2010120892924Shear Pin · corrodedSAL - MAJOR REPAIR - S5 - CORROSION WAS FOUND BETWEEN RIB 4 AND RIB 5 ON INNER PIN, LOCATED AT LEFT MIDDLE FROM LINK PIN ASSY OF AFT ENGINE MOUNT (ENGINE NR 1). REPLACED INNER PIN BETWEEN RIB 4 AND RIB 5 LOCATED AT LEFT MIDDLE FROM LINK PIN ASSY OF AFT ENGINEDec 3, 2010 · N628AW · Airbus A320231SDR USAA2010120892923Shear Pin · corrodedSAL - MAJOR REPAIR - S5 - CORROSION WAS FOUND BETWEEN RIB 4 AND RIB 5 ON INNER PIN, LOCATED AT RIGHT MIDDLE FROM LINK PIN ASSY OF AFT ENGINE MOUNT (ENGINE NR 1). REPLACED INNER PIN BETWEEN RIB 4 AND RIB 5 LOCATED AT RIGHT MIDDLE FROM LINK PIN ASSY OF AFT ENGIDec 3, 2010 · N628AW · Airbus A320231SDR USAA2010121793108Hinge Pin · corrodedSAL - S5 - MAJOR REPAIR - CORROSION ON INNER HINGE PIN FOR RIGHT AFT NR 1 ENGINE MOUNT AT PYLON STA 684. REPLACED RIGHT AFT NR 1 ENGINE MOUNT AT PYLON STA 684 IAW A320 AMM 71-22-11.Dec 1, 2010 · N628AW · Airbus A320231SDR USAA2010121793107Hinge Pin · corrodedSAL - S5 - MAJOR REPAIR - CORROSION ON INNER HINGE PIN FOR LEFT AFT NR 1 ENGINE MOUNT AT PYLON STA 684. REPLACED LEFT AFT NR 1 ENGINE MOUNT AT PYLON STA 684 IAW A320 AMM 71-22-11.Dec 1, 2010 · N628AW · Airbus A320231SDR USAA2010120892927Shear Pin · corrodedSAL - MAJOR REPAIR - S5 - CORROSION WAS FOUND BETWEEN WS 3758 TO WS 4067, BETWEEN RIB 7 AND RIB 8 ON INNER PIN, LOCATED AT RIGHT LOWER FROM LINK PIN ASSY OF AFT ENGINE MOUNT (ENGINE NR 1). REPLACED INNER PIN BETWEEN WING STATION 3758 TO 4067, BETWEEN RIB 7 ANDec 1, 2010 · N628AW · Airbus A320231SDR SWIA201025168Link Assy · damagedLEFT ENGINE FORWARD YOKE MOUNT LINK ASSEMBLY SCORED. (ENGINE CHANGE) REPLACED LEFT ENGINE FORWARD YOKE MOUNT LINK ASSEMBLY.Nov 14, 2010 · N937SW · Cndair CL6002B19SDR SWIA201025140Link · corrodedRIGHT ENGINE YOKE LINK CORRODED. (ENGINE CHANGE) INSTALLED SERVICEABLE LINK ASSEMBLY.Nov 3, 2010 · N941SW · Cndair CL6002B19SDR SWIA201025101Pin · scoredRIGHT ENGINE FORWARD MOUNT PIN SCORED. (ENGINE CHANGE) REPLACED RIGHT ENGINE FORWARD MOUNT PIN.Nov 1, 2010 · N938SW · Cndair CL6002B19SDR USAA2010110392471Mount · corrodedBFM - S2 - MAJOR REPAIR - FRETTING CORROSION ON NR 1 ENGINE FORWARD PYRAMID MOUNT FITTING ATTACH HOLES (4 EACH) & MATING SURFACES. REPAIRED NR 1 ENGINE FORWARD PYRAMID MOUNT FITTING IAW EA 134306.Oct 31, 2010 · N274AY · Airbus A330323SDR SWIA201025103Housing · corrodedRIGHT ENGINE AFT MOUNT HOUSING PITTED. (ENGINE CHANGE) REPLACED RIGHT ENGINE AFT MOUNT HOUSING.Oct 28, 2010 · N479CA · Cndair CL6002B19SDR SWIA201025102Bushing · corrodedRIGHT ENGINE AFT MOUNT BUSHING PITTED. (ENGINE CHANGE) REPLACED AFT MOUNT SPHERICAL BUSHING.Oct 28, 2010 · N479CA · Cndair CL6002B19SDR USAA2010110392470Mount · corrodedBFM - S2 - MAJOR REPAIR - FRETTING CORROSION ON NR 2 ENGINE FORWARD PYRAMID MOUNT FITTING ATTACH HOLES (4 EACH) & MATING SURFACES. REPAIRED NR 2 ENGINE FORWARD PYRAMID MOUNT FITTING IAW EA 134308.Oct 28, 2010 · N274AY · Airbus A330323SDR CA101028004Truss · damaged(CAN) MAINTENANCE FOUND THAT THE ANTI-ICE VALVE HAD BEEN RUBBING UP AGAINST THE ENGINE TRUSS, CAUSING A SCREW ON THE ELECTROMAGNETIC RECEPTACLE ASSEMBLY TO COME LOOSE, WHICH THEN WORE A HOLE THROUGH THE ENGINE TRUSS. THE IPC LISTS 319980-6-1 (PRE SB 75-009) AOct 27, 2010 · Swrngn SA226TCSDR REXA201000223Bushing · missingCOMPANY DISPATCH RECALLED THE AIRCRAFT WHEN IT WAS SUSPECTED THAT A BUSHING MIGHT HAVE BEEN LEFT OUT OF THE UPPER CLEVIS MOUNT OF THE RIGHT ENGINE. THE RIGHT ENGINE HAD BEEN INSTALLED ON 10/24/2010. THE FLIGHT CREW ADVISED MIAMI ATC AND ASKED TO RETURN TO KAOct 27, 2010 · N147PQ · Cndair CL6002D24SDR C2XA10SH356Yoke · crackedSHV - DURING C-CHECK NR 1 ENGINE FWD LWR ENGINE YOKE CRACKED. MAINTENANCE REMOVED AND REPLACED NR1 ENGINE FWD LWR ENGINE YOKE IAW EC5450-01028 REV ORIG. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Oct 25, 2010 · N15948 · Emb EMB145ERSDR SWIA201025064Bushing · corrodedRIGHT ENGINE AFT MOUNT SPHERICAL BUSHING ASSEMBLY PITTED. (ENGINE CHANGE) REPLACED RIGHT ENGINE AFT MOUNT SPHERICAL BUSHING ASSEMBLY.Oct 23, 2010 · N932SW · Cndair CL6002B19SDR SWIA201025036Link · corrodedRIGHT ENGINE FORWARD YOKE MOUNT LINK AND BUSHING CORRODED AND PITTED. (ENGINE CHANGE) REPLACED FORWARD YOKE MOUNT LINK AND BUSHING.Oct 19, 2010 · N926SW · Cndair CL6002B19SDR SWIA201025035Pin · damagedRIGHT ENGINE FORWARD YOKE MOUNT PINS ARE SCORED. (ENGINE CHANGE) REPLACED FORWARD YOKE MOUNT PINS.Oct 19, 2010 · N926SW · Cndair CL6002B19SDR SWIA201025041Link · corrodedRIGHT ENGINE LINK ASSEMBLY CORRODED. (ENGINE CHANGE) INSTALLED SERVICEABLE LINK ASSEMBLY.Oct 17, 2010 · N408SW · Cndair CL6002B19SDR COEA2010101501899Mount · crackedGEG PHASE INSPECTION: MAJOR REPAIR: DURING MAINTENANCE INSPECTION FOUND ONE CRACK .250" IN LENGTH ON LT ENGINE MOUNT RING ASSEMBLY. MAINTENANCE REMOVED AND REPLACED ENGINE MOUNT RING ASSY IAW CESSNA 208 MM.Oct 15, 2010 · N899FE · Cessna 208BSDR SWIA201025030Bushing · corrodedLEFT ENGINE SPHERICAL BUSHING AND HOUSING HAS SOME PITTING AND GALLING. (ENGINE CHANGE) REPLACED LEFT ENGINE THRUST MOUNT SPHERICAL BUSHING AND HOUSING.Oct 13, 2010 · N932SW · Cndair CL6002B19SDR SWIA201025029Link · corrodedLEFT ENGINE FORWARD MOUNT LINK ASSEMBLY PITTED. (ENGINE CHANGE) REPLACED LEFT ENGINE FORWARD MOUNT LINK ASSEMBLY.Oct 13, 2010 · N814SK · Cndair CL6002D24SDR CA101007014Mount · crackedUPON ROUTINE SERVICING, MX FOUND LT LOWER ENGINE FRAME TO BE CRACKED THROUGH BOTH INBD AND OTBD, PART WAS REMOVED FOR REPAIR. ALMOST IDENTICAL TO INCIDENT ON SEPT 30TH, 2010. REF SDR 20101007013.Oct 7, 2010 · Swrngn SA226ATSDR SWIA201025157Fitting · corrodedRIGHT ENGINE AFT THRUST MOUNT FITTING ASSEMBLY HAS CORROSION. (C-CHECK) INSTALLED NEW RIGHT AFT THRUST MOUNT FITTING ASSEMBLY.Oct 4, 2010 · N693BR · Cndair CL6002B19SDR SWIA201024979Link · corrodedRIGHT ENGINE FORWARD MOUNT LINK ASSEMBLY PITTED. (ENGINE CHANGE) REPLACED RIGHT ENGINE FORWARD MOUNT YOKE LINK ASSEMBLY PER AMM.Oct 3, 2010 · N443SW · Cndair CL6002B19SDR SWIA201024978Bolt · damagedRIGHT ENGINE FORWARD MOUNT BOLT IS SCORED. (ENGINE CHANGE) REPLACED ONE RIGHT ENGINE FORWARD MOUNT BOLT PER AMM.Oct 3, 2010 · N443SW · Cndair CL6002B19SDR SWIA201024977Shaft · damagedRIGHT ENGINE AFT THRUST SHAFT SCORED. (ENGINE CHANGE) REPLACED RIGHT ENGINE AFT MOUNT THRUST SHAFT PER AMM.Oct 3, 2010 · N443SW · Cndair CL6002B19SDR CA101007013Frame · crackedUPON ROUTINE ENG SERVICING, FOUND RT LOWER ENGINE FRAME ASSY TO BE CRACKED THROUGH MAIN BAR ON BOTH INBD AND OTBD.Sep 30, 2010 · Swrngn SA226TCSDR CA100930009Washer · misinstalledWASHERS ARE INSTALLED AT THE FACTORY UNDER THE HEADS OF THE 4 BOLTS THAT MOUNT THE BARRY MOUNTS, PN 93880-13 TO THE ENGINE. THROUGH COMMUNICATIONS WITH THE MOUNT AND ACFT MFG, DISCOVERED THAT THE WASHERS SHOULD NOT BE INSTALLED. THE WASHERS CAUSE THE BOLTS TSep 30, 2010 · Airtrc AT802ASDR SWIA201024951Bushing · corrodedLEFT ENGINE FORWARD MOUNT ASSEMBLY BUSHING PITTED. (ENGINE CHANGE) REPLACED LEFT ENGINE FORWARD YOKE MOUNT ASSEMBLY PER AMM.Sep 29, 2010 · N423SW · Cndair CL6002B19SDR ABXA201011150151Mount · corrodedNR 1 ENG AFT MOUNT HAS SURFACE CORROSION. REMOVED AND REPLACED NR 1 ENGINE AFT MOUNT FROM STEP G1 TO G3 IAW AMM 71-2-04.Sep 28, 2010 · N774AX · Boeing 767281SDR CA100928012Mount · brokenAIRFLOW MODULATOR WAS REMOVED. TIME EXPIRED FOR O/H (2400 HRS) 1 OF THE 3 MOUNT ATACHMENT WAS FOUND BROKEN.Sep 27, 2010 · Snias AS350B2SDR ABXR201009250043Mount · corrodedDURING FERRY FLIGHT PREP FOUND NR2 PYLON AFT ENGINE MOUNT CORRODED. R AND R AFT MOUNT ASSY IAW MM.Sep 25, 2010 · N934AX · Doug DC933FSDR ABXR201009250042Isolator · corrodedDURING FERRY FLIGHT PREP FOUND NR1 PYLON UPPER VIBRATION ISOLATOR RUSTED AND PITTED. R & R NR1 PYLON UPPER VIBRATION ISOLATOR IAW MM.Sep 25, 2010 · N934AX · Doug DC933FSDR ABXR201009250041Isolator · corrodedDURING FERRY FLIGHT PREP FOUND NR 1 PYLON YOKE LOWER ISOLATION ABSORBER RUSTED AND PITTED. R & R LOWER ISOLATION ABSORBER IAW MM.Sep 25, 2010 · N934AX · Doug DC933FSDR ABXR201009250040Mount · corrodedDURING FERRY FLIGHT FLIGHT, PREP FOUND NR1 PYLON AFT MOUNT RECEIVER RUSTED AND PITTED. R & R NR1 PYLON AFT MOUNT IAW MM.Sep 25, 2010 · N934AX · Doug DC933FSDR ABXR2010092400039Link · corrodedDURING FERRY FLIGHT, PREP FOUND NR1 PYLON AFT MOUNT UPPER INBD "H" DOG BONE AND OTBD BOLT RUSTY. R & R BOLT AND MOUNT LINK IAW MM.Sep 24, 2010 · N934AX · Doug DC933FSDR CA101014003Tube · mismanufacturedDURING BUILD-UP OF ENGINE AS A SPARE FOR A "QUICK CHANGE" THE TECH NOTICED THE ADEL CLAMPS WOULD NOT HOLD SECURELY TO THE MOUNT. FURTHER INVESTIGATION REVEALED THAT 2 TUBES THAT WERE REPLACED AT O/H WERE IN FACT UNDER THE MINIMUM MFG DIMENSIONS. THE MOUNT WISep 23, 2010SDR SWIA201024935Mount · corrodedBOTH LEFT ENGINE FORWARD MOUNT PINS NEED REPLACED DUE TO PITTING. (ENGINE CHANGE) REPLACED BOTH LEFT ENGINE FORWARD MOUNT PINS PER AMM.Sep 23, 2010 · N925SW · Cndair CL6002B19SDR SWIA201024934Yoke · corrodedLEFT ENGINE YOKE LINK ASSEMBLY CORRODED. (ENGINE CHANGE) REPLACED YOKE LINK ASSEMBLY PER AMM.Sep 22, 2010 · N927SW · Cndair CL6002B19SDR SWIA201024915Mount · corrodedFORWARD MOUNT BOLTS ON LEFT ENGINE HAVE SMALL AREA PITTED AND SHANK DIAMETER ON AREA 2 OUT OF LIMITS PER AMM. (ENGINE CHANGE) REPLACED LEFT ENGINE FORWARD MOUNT PINS.Sep 21, 2010 · N445SW · Cndair CL6002B19SDR CA100920008Mount · cracked(CAN) DURING A 50 HR INSP ON THE NR 1 ENGINE, A CRACK WAS FOUND ON THE NR 1 ENGINE MOUNT FRAME. WHILE INSPECTING THE FRAME IAW SB 719, A FRAME PN 86212-02 THAT WAS REPAIRED IAW SB 1033 WAS INSTALLED IN ITS PLACE AND THE REMOVED FRAME WAS SENT IN EXCHANGE.Sep 17, 2010 · Piper PA44180T
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