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 SWIA200719156Bearing · corrodedRIGHT ENGINE MOUNT THRUST SHAFT AND INNER BEARINGS ARE CORRODED, FOUND AT C-CHECK. REPLACED RIGHT ENGINE THRUST SHAFT AND INNER BEARINGS IAW CRJ200 AMM 71-00-00. Oct 13, 2007 · N941SW · Cndair CL6002B19SDR SWIA200718785Bushing · corrodedRIGHT ENGINE FORWARD MOUNT LINK BUSHING IS CORODED. INSTALLED NEW LINK WITH NEW BUSHING IAW MM 71-00-00. Oct 13, 2007 · N368CA · Cndair CL6002C10SDR WRNA200700066Bolt · corrodedDURING ACCOMPLISHMENT OF CPCP C54-400-03-00 AT M96 CHECK LEVEL II CORROSION WAS FOUND ON 4 HORIZONTAL BOLTS OF NR 2 ENGINE AFT MOUNT. REMOVED AND REPLACED 4 HORIZONTAL MOUNT BOLTS IAW MM 20-21-17 AND MM 70-00-00.Oct 11, 2007 · N510TA · Airbus A300B4203SDR SWIA200719123Box Beam · crackedRIGHT SIDE OF ENGINE BOX BEAM SHOWS SIGNS OF CRACK AT ACCESS HOLE, FOUND AT C-CHECK. INSTALLED REPAIR PARTS IAW REO 601R-53-61-358 PG 1-4 REV A.Oct 7, 2007 · N910EV · Cndair CL6002B19SDR SWIA200719134Support Beam · crackedRIGHT LOWER WEB AT FORWARD CORNER OF ACCESS OPENING ON ENGINE SUPPORT BEAM IS CRACKED, FOUND AT C-CHECK. COMPLIED WITH REO 601R-53-01-358 REV B TO REPAIR WEB. Oct 6, 2007 · N915EV · Cndair CL6002B19SDR 07FDEA04434Mount · gougedNR 2 PYLON TO ENGINE FORWARD INBD MOUNT PLATE HOLE GALLED INSIDE, FORWARD MOUNT. BLENDED AREA IAW A310-200 SRM 54-51-81. HOLE SIZE IS .842 WITHIN LIMITS IAW A310-200 SRM 54-51-81. CADIMUM PLATED IAW A310-200 SRM 51-21-10. ADHESION TEST PASSED IAW FEDEX A31Oct 1, 2007 · N451FE · Airbus A310222SDR 07FDEA04433Mount · gougedNR 2 PYLON TO ENGINE FWD MOUNT PLATE, AFT INBD HOLE GOUGED. BLENDED AREA IAW A310-200 SRM 54-51-81. HOLE SIZE IS .842 WITHIN LIMITS IAW A310-200 SRM 54-51-81. CADMIUM PLATED IAW A310-200 SRM 51-21-10. ADHESION TEST PASSED IAW FEDEX A310-200 SRM 51-21-10.Oct 1, 2007 · N451FE · Airbus A310322SDR 1214834612170Mount · chafedNR 2 ENGINE "Z" MOUNT TUBE 7 CHAFED. REPAIRED BY BLENDING AND FOUND TO BE WITHIN LIMITS PER ATR SRI DO/TS-3777/07-9189.Sep 29, 2007 · N14834 · Aerosp ATR42320SDR 1218345121707Mount · chafedNR 2 ENGINE AFT "Z" MOUNT TUB NR 2 CHAFED. CHAFE REPAIRED BY BLENDING OUT IN ACCORDANCE WITH ATR SRT DO/TS-3777/07-9189 SRAS 4238. BLEND OUT WITHIN LIMITS.Sep 28, 2007 · N14834 · Aerosp ATR42320SDR CO1Y200700007Truss Fitting · corrodedON ENGINE NR 1 FORWARD TRUSS FITTING, FOUND 4EA HOLES WITH CORROSION.Sep 14, 2007 · N702BC · Doug MD11SDR CO1Y200700006Truss Fitting · corrodedON ENGINE NR 3 FORWARD TRUSS FITTING, FOUND 4EA HOLES WITH CORROSION.Sep 14, 2007 · N702BC · Doug MD11SDR CA070913009Mount · damaged(CAN) AFT ENGINE MOUNT. THE REVERSER THERMAL BLANKETS CONTACT THE MOUNT AND WITH ENGINE VIBRATION, CAUSE THE DAMAGE. THE MOUNT INSTALLED ON THE SPARE ENGINE SHOWED THE SAME TYPE OF DAMAGE. THE WEAR DAMAGE WAS APPROXIMATELY .080 IN TO .210 IN IN WIDTH X.600 INSep 13, 2007 · Emb ERJ190100IGWSDR DJFA2007099Mount · crackedDURING A SCHEDULED MAINTENANCE INSPECTION, TECH FOUND THE NR 1 ENGINE UPPER AFT ENGINE MOUNT CRACKED. THE MOUNT IS CRACKED AT THE RADIUS AT BOTH ENDS ON THE AFT SIDE OF THE MOUNT. CRACKS ARE APPROXIMATELY .75 INCHES. MAINTENANCE REPLACED THE UPPER AFT MOUNTAug 24, 2007 · N828LX · Raythn HAWKER800XPSDR 07FDEA03064Bearing Race · migratedNR 3 PYLON AFT MOUNT BEARING AFT FACE OUTER RACE FOUND MIGRATED. 08-31-07 REMOVED AND REPLACED AS PER FEDEX E.A. 1-5410-112388. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Aug 23, 2007 · N595FE · Doug MD11SDR SWIA200718747Spherical Bearin · corrodedFOUND AT C-CHECK, RIGHT ENGINE FORWARD MOUNT LINK HAS CORROSION ON SPHERICAL BEARING. UPPER FLOATING BUSHING IS CORRODED. REPLACED ENGINE FORWARD MOUNT LINK AND UPPER FLOATING BUSHING IAW CRJ MM 71-21-01-400-801. Aug 4, 2007 · N472CA · Cndair CL6002B19SDR SWIA200718744Beam · crackedFOUND AT C-CHECK, CRACK IN RADIUS OF ENGINE BEAM AT FS 640. COMPLIED WITH SB 601R-53-065. Aug 4, 2007 · N472CA · Cndair CL6002B19SDR SWIA200718772Fitting · corrodedFOUND AT C-CHECK, LEFT ENGINE THRUST FITTING IS CORRODED. INSTALLED NEW ENGINE THRUST FITTING PER CRJ200 AMM 71-22-01-400-801. Aug 2, 2007 · N907SW · Cndair CL6002B19SDR SWIA200718771Fitting · corrodedRIGHT ENGINE THRUST FITTING IS CORRODED, FOUND AT C-CHECK. REPLACED ENGINE THRUST FITTING PER CRJ200 AMM 71-22-01-400-801. Aug 2, 2007 · N907SW · Cndair CL6002B19SDR SWIA200718843Bolt · scoredRIGHT ENGINE FORWARD MOUNT BOLTS SHOW SIGNS OF SHANK SCORING BELOW HEAD OF BOLT, FOUND AT C-CHECK. REPLACED FORWARD ENGINE MOUNT BOLTS PER CRJ200 AMM SUBTASK 71-00-00-420-001 PARA A ITEMS 15-20. Jul 27, 2007 · N403SW · Cndair CL6002B19SDR SWIA200718842Mount · corrodedLEFT ENGINE AFT MOUNT FITTING BALL BEARING IS CORRODED, FOUND AT C-CHECK. REPLACED LEFT ENGINE AFT MOUNT FITTING PER CRJ200 AMM 71-22-01-000-801.Jul 27, 2007 · N403SW · Cndair CL6002B19SDR SWIA200718841Mount · corrodedRIGHT ENGINE AFT MOUNT THRUST FITTING BALL RACE IS CORRODED, DISCOVERED AT C-CHECK. REPLACED RIGHT ENGINE AFT MOUNT THRUST FITTING ASSEMBLY IAW CRJ200 AMM 71-22-01-000-801 AND 71-22-01-400-801. Jul 27, 2007 · N403SW · Cndair CL6002B19SDR SWIA200718697Support Beam · crackedENGINE SUPPORT BEAM LOWER RIGHT WEB HAS INDICATION OF CRACK, FOUND AT C-CHECK. COMPLIED WITH REPAIR OF ENGINE SUPPORT BEAM LOWER RIGHT WEB IAW REO:601R-53-61-358 REV A.Jul 26, 2007 · N479CA · Cndair CL6002B19SDR CA070727006Web · cracked(CAN) CRACK FOUND AT LOWER WELD WEB LT SIDE. (TC NR 20070727006)Jul 23, 2007 · Cessna 172KSDR HNAA0700144Mount · brokenENGINE REMOVED FROM A/C 942 HA IN MDT ON 7-3-07 RECEIVED AT SBY MAINTANCE SHOP. FOUND TORQUE MOUNT END BROKEN OFF. ENG S/N 12-42.Jul 12, 2007 · N942HA · Dhav DHC8101SDR HNAA070144Mount · brokenENGINE WAS REMOVED FROM A/C IN MDT ON 7-3-07. RECEIVED IN SBY MAINTENANCE SHOP FOUND TORQUE MOUNT END BROKE OFF. ENGINE S/N 120042.Jul 12, 2007 · N942HA · Dhav DHC8102SDR SWIA200718643Mount · corrodedRIGHT FORWARD ENGINE MOUNT YOKE BEARING IS CORRODED, FOUND AT C-CHECK. REPLACED RIGHT ENGINE MOUNT BEARING, P/N 601-37015-8 S/N RJ/SLC/121806.Jul 2, 2007 · N407SW · Cndair CL6002B19SDR CA070711001Tube · cracked(CAN) ONE TUBE CRACKED NEAR RT REAR ENGINE LOAD MOUNT. NEW MOUNT INSTALLED. (TC NR 20070711001)Jun 5, 2007 · Cessna A185FSDR CA070528014Mount · cracked(CAN) THE AFT ENGINE MOUNT BRACKET WAS DISCOVERED TO BE CRACKED DURING A SCHEDULED ENGINE CHANGE. THE AFFECTED BRACKET WAS REPLACED WITH A SERVICEABLE UNIT. NO FURTHER ACTION NOTED. (TC NR 20070528014)May 27, 2007 · Saab SF340ASDR SWIA200718485Support Beam · crackedFOUND THE ENGINE SUPPORT BEAM UPPER ANGLE TO BE CRACKED, DISCOVERED AT C-CHECK. INSTALLED REPAIR ANGLE PER CRJ200 SRM 51-42-21 PG 17.May 22, 2007 · N928SW · Cndair CL6002B19SDR SWIA200718482Support Beam · crackedENGINE SUPPORT BEAM LOWER WEB IS CRACKED AT FORWARD, INBOARD CORNER OF LEFT ACCESS OPENING, DISCOVERED AT C-CHECK. INSTALLED REPAIR DOUBLER, WEB FILLER, SHIMS, STRAP AND ANGLE PER CRJ200 REO 601R 53-61-358.May 22, 2007 · N928SW · Cndair CL6002B19SDR SWIA200718481Support Beam · crackedENGINE SUPPORT BEAM LOWER WEB IS CRACKED AT FORWARD INBOARD CORNER OF RIGHT ACCESS OPENING, DISCOVERED AT C-CHECK. INSTALLED REPAIR PARTS PER CRJ REO 601R 53-61-258 REV A.May 22, 2007 · N928SW · Cndair CL6002B19SDR S9BA0907Adapter · corrodedOB ENGINE MOUNT ADAPTOR ON LT NACELLE IS CORRODED. REPLACED MOUNT ADAPTOR PLATE IAW RD6-54-006.May 16, 2007 · N251SA · Dhav DHC6SDR CA070508002Leg Assy · broken(CAN) ON STARTING A 200HR SCHEDULED INSPECTON FOUND LT ENGINE MOUNT LEG BROKEN IN (2) PIECES AND UPON REMOVAL FOUND SEVERE INTERNAL CORROSION THAT CAUSED THE WALL THICKNESS TO DEGRADE TO THE POINT OF COLLAPSE AND FAILURE. (TC NR 20070508002)May 7, 2007 · Bell 206L1SDR DLM88070487Mount · corrodedRT PYLON FRONT SPAR ENGINE MOUNT FITTING LOWER HOLE HAD CORROSION IN THE BORE AND SURROUNDING FORWARD FACE. REPAIRED PER ER/A 461312-14.May 7, 2007 · N944DL · Doug MD88SDR CA070507008Truss · cracked(CAN) DURING A PHASE 6 INSPECTION, A GAPING CRACK WAS FOUND ON THE RT ENGINE TRUSS MOUNT AT THE UPPER IB WELD JOINT OF THE FIREWALL ATTACH FITTING. (TC NR 20070507008)May 6, 2007 · Frchld SA227DCSDR 2007FA0000286Mount · brokenENGINE MOUNT RT FRONT CROSSOVER TUBE BETWEEN LT AND RT ENGINE SUPPORTS FOUND BROKEN AT THE WELD RT SIDE. ENGINE WAS CHANGED ABOUT 250 HRS AGO, NO MENTION OF ENGINE MOUNT DAMAGE. COULD HAVE BEEN A HARD LANDING, BUT NO OTHER SIGNS WERE NOTED. CONTACT WITH MFGMar 22, 2007 · N155CD · Cirrus SR20SDR CA070418003Mount · cracked(CAN) ENGINE MOUNT WAS INSTALLED NEW IAW STC SH99-11. POWER PLANT WAS ALIGNED IAW MM SUPPLEMENT. THE MM SUPPLEMENT INCLUDES AN INSP EVERY 100 HRS OR ANNUALLY. NOTE TO INSPECT ENGINE MOUNTS FOR CRACKS, DAMAGE, CORROSION AND SECURITY. THE CRACK STARTED BELOW THMar 21, 2007 · Bell 205A1SDR 07FDEA01061Bracket · crackedNR 2 ENG RT LOWER FORWARD FLANGE SHIP STAND ATTACHED POINT CRACK PAST STOP DRILL BOTH SIDES OF FLANGE. REMOVED GROUND HANDLING BRACKET IAW MD/DC 10 SRM 51-33-01 VOL 11. WELDED CRACK IN NR 2 ENG RT LOWER FORWARD FLANGE SHIP STAND IAW GE COMMERCIAL ENGINE STAMar 21, 2007 · N566FE · Doug MD1010FSDR CA070412001Mount · cracked(CAN) ON A ROUTINE ENGINE REPLACEMENT, IT WAS FOUND THAT THE LT LOWER ENGINE MOUNT WAS CRACKED AT THE ATTACH POINT. AFTER CLOSER INSPECTION THE MOUNT WAS COMPLETELY SEPARATED FROM THE AIRFRAME. THERE WAS NO INITIAL INDICATION OF A PROBLEM. IT WAS FOUND THAT THMar 20, 2007 · Bell 206BSDR CA070228006Mount · chafed(CAN) DURING ROUTINE MAINTENANCE A BLEED AIR LINE WAS FOUND CHAFING AN ENGINE TRUSS MOUNT TUBE. BLEED AIR LINE PN: 118-910033-93 TRUSS MOUNT PN: 129-910047-17. THE DAMAGE WAS FOUND TO BE WITHIN REPAIRABLE LIMITS IAW THE AIRCRAFT SRM. THE MOUNT WAS REPAIRED BY Feb 28, 2007 · Beech 1900CSDR GUUA94771022607ATube · chafedDURING INSP DISCOVERED ENGINE TRUSS TUBE PN 129-910032-101 HAD CHAFING DAMAGE AT 2.50 INCHES AFT OF FIRE SEAL FLANGE ON INBD SIDE. PERFORMED ENGINE TRUSS REPAIR TO CHAFED AREA, IAW FAA APPROVED DATA.Feb 26, 2007 · N69547 · Beech 1900DSDR SWIA200718118Yoke · corrodedLEFT ENGINE FORWARD MOUNT YOKE UPPER AND LOWER BEARINGS HAVE EVIDENCE OF PITTING CORROSION. LOWER BEARING IS FROZEN, DISCOVERED AT C-CHECK INSPECTION. REPLACED LEFT ENGINE FORWARD MOUNT YOKE P/N 601-37015-7.Feb 26, 2007 · N866AS · Cndair CL6002B19SDR GUUA02260701Truss · chafedAT SCHEDULED ROUTINE MAINTENANCE DISCOVERED ENGINE TRUSS TUBE PN 129-910032-101 CHAFING DAMAGE AT 2.5 INCHES AFT OF FIRE SEAL FLANGE ON IB SIDE. PERFORMED TRUSS REPAIR TO CHAFFED AREA IAW APPROVED DATA CONTAINED IN THE DWG NR 070226,DERT 510305-CE.Feb 26, 2007 · N69547 · Beech 1900DSDR UIEA200700086Mount · damagedNR 4 PYLON FWD ENGINE MOUNT FITTING BOTH I/B AND O/B LUG BORE HOLES FOUND OVERSIZED. REPAIRED ACCOMPLISHED AS PER BOEING SR ID NR 1-290193672-1 THRU -3 AND FAA FORM 8100-9.Feb 25, 2007 · N505MC · Boeing 7472D3BSDR SWIA200718044Mount · corrodedLT ENG FWD YOKE MOUNT HAS CORROSION IN BEARING, DISCOVERED DURING C-CHECK INSPECTION. REPLACED LEFT ENGINE FORWARD YOKE MOUNT P/N 601-37015-7 S/N RJ SWA/070301BTAC03.Feb 23, 2007 · N864AS · Cndair CL6002B19SDR SWIA200718043Mount · corrodedLT ENG FWD MOUNT UPPER LINK HAS CORROSION ON UPPER BEARING, DISCOVERED DURING C-CHECK INSPECTION. REPLACED LEFT ENGINE FORWARD MOUNT UPPER LINK P/N 601-37016-5 S/N 5064.Feb 23, 2007 · N864AS · Cndair CL6002B19SDR GUUA02190701Truss · chafedAT SCHEDULED ROUTINE MAINTENANCE DISCOVERED ENGINE TRUSS TUBE PN 129-910032-101 CHAFING DAMAGE AT 2.5 INCHES AFT OF FIRE SEAL FLANGE ON IB SIDE. PERFORMED TRUSS REPAIR TO CHAFFED AREA IAW APPROVED DATA CONTAINED IN THE MFG AIRLINER SERIES STRUCTURAL REPAIR MAFeb 19, 2007 · N81536 · Beech 1900DSDR CA070219005Mount · cracked(CAN) DURING INSPECTION A CRACK WAS DISCOVERED IN THE UPPER AFT OUTBOARD WELD ASSEMBLY ON THE ENGINE MOUNT TRUSS REQUIRING REPLACEMENT OF THE MOUNT ASSEMBLY. (TC NR 20070219005)Feb 18, 2007 · Swrngn SA227ACSDR WRNA200700007Mount · crackedDURING C-CHECK, WHILE ACCOMPLISHING ULTRASONIC INSPECTION OF NR 4 STRUT REAR ENGINE MOUNT THRUST LINKIAW 747 MM 71-21-03, THE FORWARD BORE HAD A CRACK INDICATION AT O/B LUG BORE EDGE.Feb 14, 2007 · N526UP · Boeing 747212BSDR CA070216004Spacer · sheared(CAN) A RATTLE NOISE WAS HEARD AT ENGINE START. CLOSE INSP OF THE ENGINE MOUNT ASSY REVEALED ALL 4 MOUNT SPACERS, P/N 829, HAD SHEARED THEIR ATTACHMENT RIVET HEADS. THIS AC WAS MODIFIED IN THE PAST WITH 180HP CONVERSION. DISASSEMBLY REVEALED THE USE OF VERY SOFeb 9, 2007 · Cessna 172E
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