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 SWIA200717771Yoke · corrodedUPPER LINK ON FWD ENG MOUNT YOKE SHOWS SIGNS OF CORROSION INCLUDING BUSHING. REMOVED AND REPLACED HARDWARE ON YOKE IAW TASK CARD RII 72-400-1000.Jan 26, 2007 · N760SK · Cndair CL6002C10SDR 2007FA0000115Mount · corrodedPERFORMED ANNUAL INSPECTION ON ENGINE, FOUND BLACK (FRETTING) CORROSION BELOW CENTER 2 (LT AFT) ENGINE MOUNT BOLTS. BOLTS WERE LOOSE IN MOUNT, BUT THE NUTS WERE TIGHT ON BOLTS. PROBLEM IS THAT THE BOLTS ARE A LITTLE TOO LONG AND THE NUTS WERE RUNNING OUT OF Jan 11, 2007 · N1562F · Beech A36SDR SWIA200717853Beam · crackedFOUND LT UPPER OTBD BRACKET TOP WEB OF ENG BEAM TO FUSE SKIN. BRACKET CRACKED ON AFT RADIUS, DISCOVERED DURING C-CHECK INSPECTION. NEW ANGLE INSTALLED PER CRJ200 SRM 51-42-21.Jan 8, 2007 · N409SW · Cndair CL6002B19SDR DELR200700001Bolt · shearedAFTER REMOVAL OF SAFTY WIRE TO REMOVE BOLT, THE MOUNT BOLT WAS FOUND SHEARED AT THE NECK OF THE BOLT. THREADED SECTION OF BOLT WAS REMOVED WITH AN EASYOUT IAW CHAPTER 5 THIS ITEM IS LIFE LIMITED AT 20,000.00 HOURS.Jan 4, 2007 · N345RJ · Lear 55LEARSDR PIDA06128Bushing · migratedREPLACED THE FUSE PIN BUSHING IN THE LEFT ENGINE STRUT MID-SPAR ATTACH FITTING PER BOEING SB 737-54-1037 DUE TO BUSHING MIGRATION.Dec 20, 2006 · N737DX · Boeing 737400SDR SWIA200617707Support Beam · crackedENG SUPPORT BEAM LT LWR ACCESS PNL CUTOUT IS CRACKED AT FWD INBD CORNER, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS TO ENGINE SUPPORT BEAM LT LOWER WEB PER CRJ200 SRM 51-42-06 P11 AND 51-42-20 PG 23.Dec 11, 2006 · N445SW · Cndair CL6002B19SDR CA061211004Plug · missing(CAN) DURING OF C-CHECK INSPECTION FOUND THAT PLUG ASSY P/N 60137054-1 IS NOT INSTALLED AT THE AFT ENGINE TRUST FITTING P/N ASB18106-17 OF LT ENGINE. TO INSTALL THE PLUG ENGINE NEED TO BE REMOVED. (TC NR 20061211004)Dec 7, 2006 · Cndair CL6002B19SDR F3LA200600161Nut · looseDURING C-2 CHECK, INSPECTION REPORTED NR 1 ENGINE PYLON AFT UPPER THREADED SLEEVE AT RIB 10 LOCK WASHER NR 103 TANG SLIGHTLY ENGAGED IN NUT, AFT PYLON-TO-WING ATTACH FITTING. ENGAGED TANG ON NUT FOR NR 1 ENGINE PYLON AFT UPPER THREADED SLEEVE AT RIB 10 IAW AMNov 30, 2006 · N805FR · Airbus A318111SDR F3LA200600160Lockwasher · damagedDURING C-2 CHECK, INSPECTION REPORTED NR 2 ENGINE PYLON AFT UPPER THREADED SLEEVE AT RIB 10 NUT BACKING OFF AND LOCK WASHER NR 103 DAMAGED, AFT PYLON-TO-WING ATTACH FITTING. REMOVED DAMAGED LOCK WASHER IAW AMM 54-51-17, SUBTASK 54-51-17-481-050, AND INSTALLENov 30, 2006 · N805FR · Airbus A318111SDR YTRR112888Support · crackedON START THE PILOT NOTICED AND SMELLED OILY SMOKE IN CABIN. WHEN THE HEATER WAS TURNED OFF THE SMOKE DISAPATED. THE AIRCRAFT WAS SHUTDOWN. ON INSPECTION FOUND A CRACKED FRONT SUPPORT ON THE COMPRESSOR THAT WAS ALLOWING OIL INTO THE BLEED AIR HEATER. REMOVED ANov 20, 2006 · N595RL · Bell 407SDR QXEA200603084Mount · gougedC3 YYC - LEFT ENGINE FORWARD MOUNT LINK HAS 4 SMALL GOUGES ON THE CORNERS. REPAIRED IAW REO670-71-21-016.Nov 18, 2006 · N613QX · Cndair CL6002C10SDR 2006FA0001096Mount · crackedCUSTOMER REPORTED THAT HYDRAULIC PUMP KENP CYCLING. INSPECTED LANDING GEAR ACTUATORS FOR LEAKS. FOUND NLG ACTUATOR ATTACH CRACKED ON ENGINE MOUNT. INSTALLING NEW ENGINE MOUNT IAW SB 1154A WILL SOLVE MALFUNCTION. (K)Nov 6, 2006 · N5215U · Piper PA46500TPSDR CA061107002Bolt · unsecure(CAN) AFT ENGINE MOUNT THRUST FITTING ATTACHMENT BOLTS ARE NOT SECURED (TORQUE IS UNKNOWN AND LOCKWIRE IS NOT INSTALLED) AT RH ENGINE. TO COMPLETE THE PROCEDURE IAW AMM 71-22-01 ENGINE TO BE REMOVED. (TC# 20061107002)Nov 3, 2006 · Cndair CL6002B19SDR SWIA200617477Support Beam · crackedENGINE SUPPORT BEAM LOWER WEB CRACKED AT RT ACCESS COVER OPENING. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR DOUBLER, WEB FILLER & STRAP IAW REO601R-61-358 REV A.Nov 2, 2006 · N443SW · Cndair CL6002B19SDR SWIA200617476Support Beam · crackedENGINE SUPPORT BEAM LOWER WEB CRACKED AT LT ACCESS COVER OPENING. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR DOUBLER, SHIM, STRAP AND WEB FILLER IAW CRJ200 REO 601R 53-61-358 SHEET 3 NOTE 7.Nov 2, 2006 · N443SW · Cndair CL6002B19SDR CA061030006Mount · cracked(CAN) THE TOP ENGINE MOUNT PAD, LOCATED ON THE GAS GENERATOR CASE, HAD A CRACK ON THE WELD LINE APPROX. 1.75 INCHES LONG. (TC# 20061030006)Oct 27, 2006 · Piper PA31TSDR MWEA060279Bolt · chafedLEFT UPPER FORWARD ENGINE MOUNT BOLT HAS CHAFED MARKED AT MID AREA SHAFT.Oct 25, 2006 · N812ME · Doug DC981SDR MWEA060278Bolt · gougedNUMBER ONE ENGINE LOWER YOKE ATTACH BOLT GOUGED.Oct 25, 2006 · N812ME · Doug DC981SDR MWEA060277Mount · corrodedRIGHT UPPER FORWARD ENGINE MOUNT YOKE INNER CUP HAS CORROSION AT THE 7 TO 9 O'CLOCK POSITION.Oct 24, 2006 · N812ME · Doug DC981SDR MWEA060281Bolt · chafedRIGHT LOWER FORWARD ENGINE MOUNT BOLT IS CHAFED. MARKS AT MID AREA OF SHAFT.Oct 23, 2006 · N812ME · Doug DC981SDR MWEA060280Bolt · corrodedRIGHT UPPER FORWARD ENGINE MOUNT BOLT HAS CORROSION ON SHAFT.Oct 23, 2006 · N812ME · Doug DC981SDR SWIA200617344Bearing · corrodedLT ENGINE YOKE LINK LOWER SPHERICAL BEARING IS CORRODED, DISCOVERED DURING ROUTINE MAINTENANCE. REPLACED YOKE LINK BEARING, P/N BA670-37071-1 P/N S10008-711.Oct 20, 2006 · N705SK · Cndair CL6002C10SDR DL76L060854Mount · crackedDURING ENG EXT HARDWARE INSP, FOUND AFT MOUNT RAILS CRACKED. REPLACED NR 1 ENG.Oct 15, 2006 · N193DN · Boeing 767332SDR DJFA2006329Mount · crackedWHILE PERFORMING A NON-DESTRUCTIVE TEST ON THE AIRCRAFT ENGINE MOUNTS, A CRACK WAS FOUND IN THE LT FWD UPPER ENGINE MOUNT. THE ENGINE MOUNT WAS REPLACED IAW THE MM.Oct 12, 2006 · N817TA · Raythn HAWKER800XPSDR SWIA200617529Support Beam · crackedENGINE SUPPORT BEAM WEB HAS EVIDENCE OF A CRACK RT SIDE MIGRATING FROM LOWER ACCESS PANEL FWD INBD CORNER, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR ON ENGINE SUPPORT BEAM LOWER WEB RT PER REO 601R 53-61-1968.Oct 11, 2006 · N442SW · Cndair CL6002B19SDR S9BA00606Mount · corrodedRIGHT ENGINE RIGHT ENGINE MOUNT PLATE HAS CORROSION. REMOVED AND REPLACED RIGHT ENGINE MOUNT PLATE IAW RD-54-006.Oct 10, 2006 · N888PV · Dhav DHC6300SDR S9BA00506Mount · corrodedRIGHT ENGINE UPPER ENGINE MOUNT PLATE HAS CORROSION. REMOVED AND REPLACED UPPER ENGINE MOUNT PLATE IAW RD-54-006.Oct 10, 2006 · N888PV · Dhav DHC6300SDR CA061108002Mount · broken(CAN) DURING DAILY INSPECTION PILOT NOTICED UNUSUAL PIECE OF METAL IN THE ENGINE BAY. INVESTIGATION REVEALED BROKEN LOWER LT ENGINE MOUNT. (TC NR 20061108002)Sep 29, 2006 · Bell 206BSDR DL76S060792Fitting · fatiguedCRACK INDICATIONS WERE FOUND AT THE FORWARD OUTBOARD BOLT HOLE LOCATION OF THE AFT PITCH LOAD FITTING, NR 1 PYLON. CRACK IS IN LOWER WING SKIN ALSO, AND REQUIRED SUBJECT HOLE TO BE OVERSIZED AND BUSHED BACK TO DIAMETER.Sep 28, 2006 · N124DE · Boeing 767332SDR DL757060774Mount · corrodedDURING THE CURRENT HMV3 CHECK, THE NR 2 PYLON P/N 311N3211 -1 FORWARD ENGINE MOUNT FITTING WAS FOUND WITH FRETTING CORROSION ON THE LOWER SURFACE AROUND THE MOUNT HOLES. PERMANENT REPAIR WAS ACCOMPLISHED PER PRODUCTION PERMIT B757-54-25940PA AND ERA 457245-14Sep 22, 2006 · N632DL · Boeing 757232SDR DL757060773Mount · corrodedDURING THE CURRENT HMV3 CHECK, THE NR 1 PYLON P/N 311N3211-1 FORWARD ENGINE MOUNT FITTING WAS FOUND WITH FRETTING CORROSION ON THE LOWER SURFACE AROUND THE MOUNT HOLES. ACCOMPLISHED PERMANENT REPAIR PER PRODUCTION PERMIT B757-54-25939PA REF ERA 457244-14.Sep 22, 2006 · N632DL · Boeing 757232SDR DL757060772Mount · corrodedNR 2 ENGINE FORWARD LOWER MOUNT FITTING HAD PITTING, REMOVED BY BLENDING. ACCOMPLISHED PERMANENT REPAIR PER PRODUCTION PERMIT B757-71-25751 REF ERA 457048-14.Sep 22, 2006 · N632DL · Boeing 757232SDR DL757060771Mount · corrodedNR 1 ENGINE FORWARD LOWER MOUNT ON PYLON WAS BLENDED TO A DEPTH OF .003 INCHES TO REMOVE DAMAGE. ACCOMPLISHED PERMANENT REPAIR PER ACTS PRODUCTION PERMIT B757-71-25751. REFERENCE ERA 457046-14.Sep 22, 2006 · N632DL · Boeing 757232SDR CA060918004Bolt · broken(CAN) DURING ROUTING INSPECTION IT WAS NOTED THAT ONE OF THE BOLTS SECURING THE RT BOTTOM ENGINE MOUNT BRACKET ONTO THE CRANKCASE OF THE RT ENGINE WAS BROKEN AND THE OTHER BOLT WAS LOOSE. BROKEN TREADED BOLT PIECE WAS REMOVED FROM CRANKCASE AND A SERVICEABLE BSep 9, 2006 · Piper PA44180SDR 2006FA0000909Belt · fracturedULTRALIGHT FRACTURED ENGINE BELT REDUCTION BRACKET CAUSING IN-FLIGHT SHUTDOWN AND EMERGENCY LANDING. PROBABLE CAUSE: ENGINE BELT REDUCTION BRACKET STRESS/FATIGUE CRACK CAUSING HEAVY ENGINE VIBRATION AND SHUTDOWN. (K)Sep 7, 2006 · N56JH · Amtr WOODYPUSHERSDR 06FDEA03156Mount Fitting · corrodedPYLON NR 3 FWD ENG MOUNT FITTING WAS REPORTED WITH PITTING ON TRUSS P/N AUB7510-501 FWD AND AFT HOLES, AND ON TRUSS P/N AUB7510-502 FWD HOLES (FWD ENG MOUNT FITTING P/N AUB7508-1). CORROSION REMOVED AND FABRICATED BUSHINGS INSTALLED AS PER E.A.1-5450-102315, Aug 31, 2006 · N521FE · Doug MD11SDR UPS06247815Bushing · corrodedINSPECTION TYPE: C ENGINE NR 3 FWD MOUNT FITTING HAS PITTING CORROSION ON REPAIR BUSHING IN AFT OB HOLE FITTING REPAIR BUSHING REMOVED IAW SOPM 20-50-03. REPAIR CARRIED OUT IAW APPX B.Aug 15, 2006 · N942UP · Boeing 72722CSDR 06FDEA2885Mount · gougedGOUGE FOUND AT ENG MOUNT FWD BORE LOWER SURFACE AT RT TRUSS FITTING OF NR 1 PYLON.Aug 7, 2006 · N521FE · Doug MD11SDR 06FDEA2884Fitting · chafedCHAFE MARK (1 PLACE) AT RT TRUSS FITTING OF NR 1 PYLON.Aug 7, 2006 · N521FE · Doug MD11SDR 06FDEA2883Fitting · chafedCHAFE MARK (6 PLACES) AT LT TRUSS FITTING OF NR 1 PYLON.Aug 7, 2006 · N521FE · Doug MD11SDR 06FDEA2882Mount · chafedCHAFE MARK (2 PLACES) AT RT TRUSS FITTING OF NR 3 PYLON FWD ENG MOUNT.Aug 7, 2006 · N521FE · Doug MD11SDR 06FDEA2881Mount · chafedCHAFE MARK (4 PLACES) AT LT TRUSS FITTING OF NR 3 PYLON FWD ENG MOUNT.Aug 7, 2006 · N521FE · Doug MD11SDR DJFA2006297Bracket · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING AD 2002-01-23 A CRACK WAS DISCOVERED ON THE LT ENGINE CARRY THROUGH MOUNT BRACKET. THE LT ENGINE WAS REMOVED, AND THE LT AFT CARRY THROUGH BRACKET WAS REPLACED REFERENCING RAYTHEON ENGINEERING DRAWING 128-Aug 1, 2006 · N447LX · Beech 400ASDR 2006FA0000752Safety Wire · misinstalledALL 4 ENGINE VIBRATION ISOLATOR MOUNT BOLTS WERE SAFETY WIRED BACKWARDS. NO EVIDENCE OF DAMAGE. (K)Jul 20, 2006 · N2542T · Amtr LC41550FGSDR 2006FA0000946Attach Angle · brokenBOTH LT AND RT ENGINE MOUNTS TO FIREWALL ATTACH POINTS BROKE OUT AFT OF THE FIREWALL IN THE UPPER OB POINT. THIS BREAKAGE IS DIFFICULT TO DETECT DUE TO VISIBILITY ACCESS. THESE BRACKETS BROKE BECAUSE OF FLIGHT THROUGH TURBULENCE. (K)Jul 7, 2006 · N2009X · Beech 76SDR 2006FA0000945Mount · brokenBOTH LT AND RT ENGINE MOUNT TO FIREWALL ATTACH POINTS BROKE OUT AFT OF THE FIREWALL IN THE UPPER OB POINT. THIS BREAKAGE IS DIFFICULT TO DETECT DUE TO VISIBILITY ACCESS. THESE BRACKETS BROKE BECAUSE OF FLIGHT THROUGH TURBULENCE. (K)Jul 7, 2006 · N2009X · Beech 76SDR CA060717003Mount · cracked(CAN) DURING ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE FWD LT MOUNT PAD WAS CRACKED. THIS ENGINE MOUNT WAS INSTALLED 44.8 HRS AGO. REPLACED ENGINE MOUNT WITH SERVICEABLE P/N 075-1003-31, AIRCRAFT WAS RETURNED TO SERVICE. (TC NR 20060717003)Jul 6, 2006 · Cessna A185FSDR 2006FA0000599Gusset · crackedFOUND 2 OF 4 ENGINE MOUNT TO FIREWALL BRACKETS CRACKED. BRACKETS ARE LOCATED IN CABIN, ATTACHING AC SKIN TO FIREWALL. POSSIBLE CAUSE OF CRACKEING MAY BE OVERTORQUING OF ENGINE MOUNT TO FIREWALL BOLTS. (K)Jun 13, 2006 · N6540E · Cessna 175SDR 2006FA0000598Gusset · crackedFOUND 2 OF 4 ENGINE MOUNT TO FIREWALL BRACKETS CRACKED, BRACKETS ARE LOCATED IN CABIN, ATTACHING AC SKIN TO FIREWALL. POSSIBLE CAUSE OF CRACKING MAY BE OVERTORQUING OF ENGINE MOUNT TO FIREWALL BOLTS. (K)Jun 13, 2006 · N6540E · Cessna 175SDR 2006FA0000597Gusset · crackedFOUND 2 OF 4 ENGINE MOUNT TO FIREWALL BRACKETS CRACKED, BRACELETS ARE LOCATED IN CABIN, ATTACHING AC SKIN TO FIREWALL. POSSIBLE CAUSE OF CRACKING MAY BE OVERTORQUING OF ENGINE MOUNT TO FIREWALL BOLTS. (K)Jun 13, 2006 · N6540E · Cessna 175
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