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 ASOA04979Support Beam · crackedDURING HANGAR MAINTENANCE IN BTR, THE ENGINE SUPPORT BEAM LOWER WEB, BL 36.20 RT AND LT SIDE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS PERFORMING A TEMPORARY REPAIR TO THE ENGINE SUPPORT BEAM LOWER WEB, BL 36.20 RT AND LT SIDE IAW BOMBARDIER RO NRSDR ASOA04949Support Beam · crackedDURING A C-CHECK IN MCN, THE RT ENGINE SUPPORT BEAM AT BL 36.20 INBOARD FORWARD CORNER WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE RIGHT ENGINE SUPPORT BEAM AT BL 36.20 IAW ASA EO 600-53-0070. (M)SDR ASOA04955Support Beam · crackedDURING A C-CHECK IN MCN, THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 IAW ASA EO 600-53-0072. (M)SDR ASOA04956Support Beam · crackedDURING A C-CHECK IN MCN, THE ENGINE SUPPORT BEAM AT BL 36.20 LT/RT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE ENGINE SUPPORT BEAM AT BL 36.20 LT/RT IAW ASA EO 600-53-0070. (M)SDR SWIA200414176Yoke · corrodedLEFT ENGINE FORWARD MOUNT YOKE CORROSION FOUND ON BEARING SURFACES. REMOVED AND REPLACED FORWARD LEFT ENGINE YOKE MOUNT ASSEMBLY REF 71-21-01.SDR CA041103010Mount · cracked(CAN) DURING A 100 HR INSPECTION AN AME WAS PERFORMING A VISUAL INSPECTION ON THE ENGINE MOUNTS AND FOUND AN AREA ON THE RT MOUNT THAT LOOKED SUSPICIOUS. UPON FUTHER INVESTIGATION (LIGHT SANDING) IT WAS DETERMINED THAT THERE WERE CRACKS & HOLES IN 2 AREAS OF TSDR ASOA04828Support Beam · crackedDURING A C-CHECK, THE ENGINE SUPPORT BEAMS AT BL 36.20 ON THE LT AND RT SIDES WERE FOUND TO BE CRACKED AT THE AFT IB CORNERS UNDER THE ACCESS PANEL BEYOND LIMITS. MAINTENANCE IS REPAIRING THE ENGINE SUPPORT BEAMS AT BL 36.20 ON THE LT AND RT SIDES IAW EO 600-SDR CA041019003Mount · chafed(CAN) AT ENGINE REPLACEMENT, THE CLAMP WAS FOUND TO BE LOOSE AROUND THE ENGINE MOUNT TUBING. THE CLAMP HAD CHAFFED INTO THE TUBE SIGNIFICANTLY. THE MOUNT WAS REMOVED AND SENT FOR REPAIR IAW THE SRM FOR THE C208B. THE CLAMP AND HARDWARE WAS REPLACED AND SECUREDSDR 04FDEA02711Bearing · migratedNR 3 ENGINE AFT MOUNT O/B VERTICAL LINK HAS BOTH BEARINGS MIGRATING. REMOVED UNSERVICABLE NR 3 AFT ENGINE MOUNT, INSTALLED SERVICEABLE NR 3 AFT ENGINE MOUNT ASSEMBLY IAW DC10-30 MM 71-20-01-03.SDR GTIA040787Isolator · out of limitsDTW - VERIFY LOWER FORWARD VIBRATION ISOLATOR ALIGNMENT MARKS ARE WITHIN LIMITS. REMOVED AND REPLACED FORWARD LOWER NR 1 ENGINE ISOLATOR MOUNT. (M)SDR UPS04243180Bushing · corrodedINSPECTION TYPE:C, ENGINE NR 1 FWD MOUNT FITTING, REPAIR BUSHINGS IN BOTH O/B HOLES HAVE MIGRATED. REPAIRED IAW UPS EO B727-5440-11592-A.SDR GTIA040765Isolator · out of limitsDTW - FOUND NR 1 UPPER ISOLATOR REQUIRES CHANGE, OUT OF LIMITS. REMOVED AND REPLACED NR 1 UPPER FORWARD VIBRATION ISOLATOR. (M)SDR 2004FA0000752Bracket · crackedTHE FUSELAGE UPPER ENGINE MOUNT BRACKETS WERE DISCOVERED TO BE CRACKED AT MOUNTING HOLES. PN 0513132-11 FOR UPPER LT AND UPPER RT. NEW REPLACEMENT PARTS WERE NOTED TO BE SLIGHTLY THICKER AND MADE FROM SAME MATERIAL. SUGGEST ENGINE MOUNT REMOVAL FOR INSPECTISDR CA040915010Tube · cracked(CAN) ENGINE MOUNT LT LONGITUDINAL TUBE CRACKED AND DEFORMED AT THE REAR ATTACH CLUSTER. DAMAGE CONSISTENT WITH THAT FOUND AFTER A HARD LANDING, AIRFRAME AND ENGINE INSPECTED FOR RELATED DAMAGE AND NONE FOUND. NO REPORT OF A HARD LANDING FORTH COMING FROM FLSDR 2004UALA00818Hanger Assy · corrodedNR 3 ENGINE AFT MOUNT HANGER PITTED AROUND BOLT HOLE I/B SIDE & O/B SIDE. NR 3 ENGINE AFT MOUNT REPLACED.SDR GTIA040776Isolator · out of adjustNR 2 ENGINE PYLON FORWARD LOWER ISOLATOR, ALIGNMENT MARKS ARE OUT OF LIMITS. REMOVED AND REPLACED LOWER FORWARD ISOLATOR. (M)SDR CA040827003Rail · cracked(CAN) THE LT UPPER ENGINE RAIL WAS FOUND TO BE CRACKED DURING SCHEDULED MAINTENANCE. PN 0513132-3 WAS REPLACED WITH NEW PART. NEW HARDWARE WAS INSTALLED.SDR AALA20040884Mount · corrodedRIGHT HAND OUTBOARD AFT ENGINE MOUNT BOLT COUNTER BORE CORRODED. CORROSION REMOVED AND COUNTER BORE TREATED, PRIMED, AND PAINTED PER ESO 30595.SDR AALA20040883Mount · corrodedRT IB AFT ENGINE MOUNT BOLT COUNTER BORE CORRODED. CORROSION REMOVED AND COUNTER BORE TREATED, PRIMED, AND PAINTED IAW ESO 30595 DATED 8/18/04. (CLOSED)SDR 04FDEA02499Mount · corrodedCOMPLY WITH EA8-7120-79336 ENGINE MOUNTS ALIGNMENT PIN MINOR CORROSION REPAIR. COMPLIED WITH EA 8-7120-79336.SDR CA040825001Bracket · cracked(CAN) CHANGED LT UPPER ENGINE RAIL BRACKET. PN 0411281-6 REPLACED WITH NEW PART. NEW HARDWARE USED.SDR GTIA040732Isolator · shiftedRSW - FOUND FORWARD LOWER ISOLATOR FOUND SHIFTED ON NR 2 PYLON. REPLACED FORWARD LOWER ISOLATOR. (M)SDR SD92004F00000Mount · brokenENGINE MOUNT TUBE BROKEN BELOW RT ISOLATOR. DISCOVERED DURING 100 HOUR INSPECTION.SDR 2004FA0000755Mount · brokenENGINE MOUNT TUBE BROKEN BELOW TOP RT ISOLATOR. DISCOVERED DURING 100 HR INSPECTION. (WP07200420174)SDR UPS04242985Crossover Tube · crackedINSPECTION TYPE: C, DURING NDT OF NR 2 ENGINE MOUNTING COMPONENTS THE CROSSOVER STRUT WAS FOUND TO BE CRACKED. REPLACED CROSSOVER STRUT IAW SRM 51-30-02.SDR CA040803008Casting · separated(CAN) ENGINE WAS FOUND SAGGING. UPON INVESTIGATION THE UPPER ENGINE MOUNT WAS FOUND BROKEN OFF. ALL 3 MOUNTS REPLACED AND CHECKED OK NOTE THESE MOUNTS WERE INVOLVED IN A SUDDEN STOPPAGE, 243 HOURS PRIOR.SDR G9C2004F00000Mount · crackedWHILE INSPECTING THE ENGINE MOUNT IAW THE INSTRUCTIONS OF PART 1, MFG SB 1103B, DATED NOV 11, 2003, CRACKS WERE DISCOVERED IN TWO OF THE ENGINE MOUNT TUBE MEMBERS ATTACHED TO THE RT NOSE GEAR ACTUATOR ATTACHMENT FOOT. THE SB SPECIFIES TO INSPECT THE ENGINE MSDR MPY2004F00000Heat Shield · gougedHEAT SHIELD PN 600429-503 WAS FOUND TO BE MAKING CONTACT WITH TUBULAR ENGINE MOUNT. THIS CONTACT CREATED A GOUGE APPROX .200 INCH LONG AND APPROX .045 INCH DEEP.SDR 2004FA0000549Heat Shield · gougedHEAT SHIELD WAS FOUND TO BE MAKING CONTACT WITH TUBULAR ENGINE MOUNT. THIS CONTACT CREATED A GOUGE APPROXIMATELY .200 INCH IN LENGTH AND APPROXIMATELY .045 INCH DEEP.SDR CA040708001Bushing · debondedA SERVICEABILITY INSPECTION WAS CARRIED OUT FOLLOWING THE LAST FLIGHT OF THE DAY AND IT WAS FOUND THAT THE LEFT ENGINE OUTBOARD MOUNT HAD VISIBLY DROPPED. THE ELASTOMER MATERIAL WAS COMPLETELY DEBONDED FROM THE METAL INNER PORTION OF THE MOUNT BUSHING P/N 105SDR CA040723006Mount · cracked(CAN) A SMALL CRACK (LESS THAN 2MM) WAS DISCOVERED ON THE ENGINE MOUNT DURING SERVICING. THE CRACK IS LOCATED ON THE LT SIDE, ON THE UPPER TUBING WHICH RUNS FORE AND AFT IN BETWEEN THE FORWARD AND REAR ENGINE MOUNT PADS. THE EXACT LOCATION IS ONE INCH FORWARD SDR GTIA040634Isolator · out of limitsMCO - FOUND FORWARD LOWER VIBRATION ISOLATOR OUT OF LIMITS, NR 1 ENGINE. INSTALLED FORWARD LOWER VIBRATION ISOLATOR. (M)SDR ASOA04432Support Beam · crackedDURING A C-CHECK IN MCN, THE ENGINE SUPPORT BEAM UPPER CENTER WEB AT BL 0 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 IAW ASA EO 600-53-0072. (M)SDR CA040624001Mount · mismanufactured(CAN) DURING ENGINE MOUNT REPLACEMENT IT WAS NOTICED THAT THE NEW MOUNTS WERE MANUFACTURED WITH THE BEVEL ON THE WRONG SIDE OF THE METAL PART OF THE CORE (R20700-11). THE CORE IS MADE OF RUBBER SANDWICHED BETWEEN TWO PIECES OF METAL. THE BEVEL IS THERE TO ALLSDR GTIA040591Isolator · corrodedFTW - FOUND RIGHT ENGINE PYLON AFT VIBRATION ISOLATOR CONCEAL SURFACE PITTED. REMOVED AFT VIBRATION ISOLATOR. INSTALLED SERVICEABLE AFT ISOLATOR. (M)SDR AUS20040496Truss · corroded(AUS) LT ENGINE LOWER LT ATTACHMENT TRUSS CORRODED.SDR 04158409Mount · corrodedDURING INSPECTION THE RIGHT HAND FORWARD ENGINE MOUNT WAS FOUND WITH LEVEL 2 CORROSION AND WAS REPLACED. AIRCRAFT WILL BE RETURNED TO SERVICE UPON COMPLETION OF INSPECTION.SDR CA040603002Bolt · fractured(CAN) AFTER LAST FLIGHT, DAILY INSPECTION WAS BEING CARRIED OUT ON THE AIRCRAFT, WHEN THE NR 1 ENG LT UPPER TIE BOLT WAS FOUND TO BE FRACTURED. THE OTHER TWO TIE BOLTS WERE REMOVED AND INSPECTED AND FOUND TO BE SERVICEABLE. THIS TIE BOLT ATTACHES THE ENGINESDR 04154632CSupport Beam · crackedDURING HEAVY CHECK THE ENGINE SUPPORT BEAM LOWER WEB LEFT HAND SIDE WAS FOUND CRACKED. THE WEB WAS REPAIRED PER MANUFACTURER INSTRUCTIONS AND AIRCRAFT WAS RETURNED TO SERVICE UPON COMPLETION OF INSPECTION.SDR UPS04242556Support · crackedINSPECTION TYPE: C, CENTER ENGINE LEFT AND RIGHT SUPPORT WEBS AT BS 1387 ARE CRACKED. WEBS REMOVED IAW SRM 51-30-02. NEW WEBS FABRICATED IAW BOEING DRAWING 65-17553, NEW WEBS INSTALLED IAW SRM 51-30-02.SDR AUS20040440Stiffener · cracked(AUS) RT FORWARD ENGINE MOUNT STIFFENER CRACKED THROUGH. CRACK MIGRATED INTO LATERAL FRAME AT STN 155.SDR HNAA0400057Mount · crackedNR 1 ENGINE INBOARD AFT ENGINE MOUNT STRUT IS CRACKED AT UPPER WELD AREA. REMOVED AND REPLACED STRUT.SDR GTIA040468Mount · inoperativeNR 1 ENGINE FWD LOWER VIBRATION MOUNT REQUIRES CHANGE. REMOVED AND REPLACED NR ENGINE FWD/ LWR VIBRATION MOUNT.SDR UPS04242438Mount · corrodedINSPECTION TYPE: C ENGINE NR 3 FWD MOUNT HOLE HAVE PITTING CORROSION IN BOTH I/B HOLES. HOLES REPAIRED IAW UPS EO B727-5440-11592.SDR UPS04242437Mount · corrodedINSPECTION TYPE:C NR 1 ENG FWD MOUNT HOLES HAVE PITTING CORROSION IN BOTH IB HOLES. HOLES REPAIRED IAW UPS EO B727-5440-11592.SDR KBM2004F00078Mount · crackedRT FWD ENGINE COWLING SUPPORT LEG CRACKED AT MGB DECK HWD IAW STANDARD PRACTICES. REPAIRED RT ENGINE SUPPORT LEG W/STAINLESS STEEL BRACKET DOUBLER W/ EXISTING.SDR ALG2004F00028Mount · wornDURING TIME CHANGE OF ENGINE ASSEMBLY. REAR ENGINE MOUNT BEARING ON THE SUPPORT HAS EXCESSIVE WEAR, ALSO THE BEARING HOUSING HAS EXCESSIVE PLAY WHICH IS BEYOND LIMITS.SDR BAQ2004F12345Bracket · crackedNR 1 ENGINE LT OB FORWARD ENGINE SUPPORT BRACKET FOUND CANCELLED DURING ROUTINE MAINTENANCE. PART IS VISABLE AFTER INSPECTION PANEL IS REMOVED INSIDE ENGINE COMPARTMENT. PANEL NR 109-0322-10-527.SDR CA060208010Mount · broken(CAN) AFTER LIFT-OFF IT WAS NOTICE A POWER LOSS ON THE RT TORQUE GAUGE. THE WEATHER CONDITIONS WERE VERY BAD THE POWER WAS REDUCED AND THAN THE A/C LANDED 2 MINUTES AWAY. WHEN THE A/C WAS SECURE AND ENGINE SHUT OFF IT WAS NOTICED THAT THE ENGINE MOUNTS ON THESDR SWIA200413302Support Beam · crackedENGINE SUPPORT BEAM LOWER WEB RBL 38 CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED WEB IAW CRJ REO 601R-53-61-366, REV ''D''.
Back to JASC 7120