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 HNAA0200031Strut · crackedDURING ROUTINE INSPECTION FOUND #2 ENGINE AFT OUTBOARD ENGINE MOUNT VERTICAL STRUT CRACKED AT THE HORIZONTAL STRUT ATTACH POINT. REPLACED VERTICAL STRUT.SDR HEEA078210Mount · damagedENGINE MOUNT HAS MECHANICAL DAMAGE ON ONE LEG BEYOND MAINTENANCE MANUAL LIMITS.SDR LR7A02024Mount · crackedDURING SCHEDULED C3 INSPECTION FOUND NR 2 ENGINE FS 517 INBOARD TRUSS MOUNT LUG CRACKED AT DIAGONAL TUBE ATTACH HOLE, CWS 179L, WL 275. REPLACED TRUSS MOUNT IAW SRM SMP 583 51-10, PG 4.SDR LR7A02014Mount · crackedDURING SCHEDULED C3 INSPECTION PER JOB CARD HSP53118 FOUND NR 2 ENGINE FS 517 OUTBOARD TRUSS MOUNT LUG CRACKED AT FWD DIAGONAL TUBE ATTACH HOLE, CWS 216L, WL 275. REPLACED TRUSS MOUNT IAW SRM SMP 583 51-10 PG 4.SDR DL72E020269Mount · crackedDURING INSPECTIONS OF THE FORWARD ENGINE MOUNT SUPPORT FITTING ON THE NR 3 ENGINE PYLON PER AD 97-05-08, A CRACK INDICATION WAS NOTED IN HOLE C AS REFERENCED IN BAC S/B 727-54A0010. THE HOLE WAS OVERSIZED TO REMOVE THE CRACK WITH AN ADDITIONAL INSURANCE CUT. SDR 2002FA0000454Bolt · brokenUPON INSPECTION, FOUND RIGHT TOP ENGINE MOUNT BOLT BROKEN AT FIREWALL.SDR HEEA078147Tube · damagedENGINE MOUNT TUBE DAMAGED BEYOND LIMITS. TUBE WAS FULL OF WATER UPON REMOVAL FROM AIRCRAFT.SDR HEEA078125Mount · wornENGINE MOUNT BEARING WORN.SDR QH52002F00000Mount · crackedMOUNT HAS A .500 INCH CRACK AS MARKED ON PART.SDR DL72W020156Mount · crackedHFEC BOLT HOLE INSPECTION OF THE FWD ENGINE MOUNT ON THE NR 3 PYLON PER AD 97-05-08 INDICATED CRACKS IN HOLES -C- AND -D- OF BAC S/B 727-54A0010. THE HOLES WERE OVERSIZED WITH A .0312 INCH ADDITIONAL INSURANCE CUT TO REMOVE ALL CRACKS. LARGER DIAMETER FASTENSDR 2002FA0000226Beam · corrodedFOUND RT OUTBOARD ENGINE BEAM CORRODED BEYOND LIMIT, CANTED BULKHEAD WAS ALSO CORRODED BEYOND LIMITS. SUGGEST SHORTER INTERVAL BETWEEN INSPECTIONS.SDR HEEA077806Bearing · wornENGINE BIPOD MOUNT HAS BOTTOM BEARINGS WORN.SDR CA020131001Nut · missing(CAN) SCHEDULED MAINTENANCE DURING REGULAR SCHEDULED OVERNIGHT MAINTENANCE; AD:99-26-07 (A)(2),INSPECTION OF NR 1 ENGINE AFT MOUNT CONE BOLT SECONDARY SUPPORT, WESTJET ENGINEER FOUND THE SECONDARY SUPPORT NUT, P/N:84821CD-524 MISSING. MAINTENANCE REPLACED THE SDR USAA020054Mount · scoredPIT - FOUND ENGINE MOUNT SCORING AND LUG CHAMFER BEARING LUG. BLENDED TO DEPTH .051, UNIT MPI ACCOMPLISHED. ROTOPEENED BLENDED AREA PER EA 73271. (M)SDR F3LA200200027Mount · wornDURING C-7 CHECK, INSPECTION REPORTED EXCESSIVE PLAY IN NR 2 ENGINE YOKE TO WING MOUNT. REPLACED ENGINE MOUNT FITTINGS AND YOKE PER MM 54-51-41.SDR F3LA200200026Mount · wornDURING C-7 CHECK, INSPECTION REPORTED SEVERE MOVEMENT IN NR 2 ENGINE AT YOKE IN PYLON, INBOARD SIDE. REPLACED NR 2 ENGINE MOUNT YOKE PER MM 54-41-11, 4C - J, PAGES 41 AND 402.SDR HEEA077721Mount · mismarkedENGINE MOUNT LEG IS MISIDENTIFIED BY PART NUMBER.SDR DL733020062Support Fitting · damagedFWD ENGINE MOUNT SUPPORT FITTING WAS FOUND WITH OVERSIZED MOUNT HOLES. REPAIR PER ER/A 410877-14AD.SDR DL733020061Support Fitting · damagedFWD ENGINE MOUNT SUPPORT FITTING WAS FOUND WITH OVERSIZED MOUNT HOLES. REPAIR PER ER/A 410878-14AD.SDR 2002FA0000134Shock Mount · missingFOUND RIGHT FORWARD ENGINE VIBRATION ISOLATOR MOUNT AND ATTACH HARDWARE MISSING FROM RIGHT ENGINE.SDR 2002FA0000198Washer · wrong partDURING A ROUTINE INSPECTION, FOUND THE ENGINE MOUNT BOLTS HAD AN960616L WASHERS INSTALLED UNDER BOLT HEADS (12 BOLTS ) TOTAL. THIS TYPE BOLT MUST HAVE MS20002C6 WASHERS.SDR CA020117002Support · cracked(CAN) FOUND CRACK ON THE ENGINE SUPPORT BEAM. ENGINE SUPPORT BEAM REPAIRED.SDR GTIA020127Bolt · missingFTW - FOUND NR 2 ENGINE FORWARD MOUNT CONE BOLT THROUGH BOLT HAS MISSING ALIGNED BOLT ON ANTI-ROTATION ASSY. REMOVED AND REPLACED TOP FORWARD CONE BOLT PER MD80 MM 71-20-01. (M)SDR GTIA020151Isolator · out of positionFOUND LEFT ENGINE FORWARD LOWER VIBRATION ISOLATOR ROTATION MARKS ARE MISMATCHED. REMOVED LEFT LOWER VIBRATION ISOLATOR. INSTALLED LOWER LEFT VIBRATION ISOLATOR IAW MD80 MM 71-20-02. (M)SDR GTIA020150Isolator · out of positionFTW - RIGHT ENGINE FORWARD LOWER VIBRATION ISOLATOR ROTATION IND MARKS ARE MISMATCHED. REMOVED RIGHT ENGINE FORWARD LOWER VIBRATION ISOLATOR IAW MD80 MM 71-20-02. INSTALLED RIGHT LOWER VIBRATION ISOLATOR. (M)SDR QXEA0200016Strut · chafedPDX - NR 2 ENGINE MOUNT LOWER OUTBOARD STRUT HAS TWO CHAFED SPOTS ON INBOARD SIDE. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36.SDR RASFTYRK195Mount Bracket · crackedCRACK FOUND IN LT FORWARD ENGINE MOUNT BRACKET WHILE PERFORMING FLUORESCENT PENETRANT INSPECTION AS PER RAYTHEON AIRCRAFT SAFETY COMMUNIQUE NR 189.SDR UPS02237548Mount · corrodedINSPECTION TYPE:C+SI NR 3 ENGINE FWD MOUNT FWD OUTBOARD HOLE HAS PITTING CORROSION ON INSIDE OF BORE.SDR UPS02237534Mount · corrodedINSPECTION TYPE:C=SI NR 1 ENGINE FWD TRUNNION MOUNT AFT OUTBOARD HOLE HAS PITTING CORROSION IN BORE OF HOLE.SDR JEM2002F00000Mount · crackedCONCERNING A VISUAL INSPECTION OF THE LT ENGINE CARRY THROUGH MOUNT BACKET FOR CRACKS ON MFG 400 NAD 400A. IT DOES NOT COVER THE MU-300 SERIES AIRCRAFT. WE IN SPECTED THIS AIRCRAFT AND FOUND A CRACKED MOUNT BRACKET. BUGGEST MFG EXPAND THE MODELS TO INCLUDE SDR HEEA077436Leg Assy · mismarkedPART NUMBER INCORRECT, PART MADE OF STEEL (MISIDENTIFIED) SHOULD BE 206064106001.SDR 2001FA0000606Mount · crackedENGINE TRUSS WELD ASSEMBY FOUND CRACKED AT STEERING ARM ATTACH POINT.SDR 2001FA0000605Mount · crackedENGINE TRUSS WELD ASSY FOUND CRACKED AT STEERING ARM ATTACH POINTSDR HEEA077428Bearing · wornBEARING WORN PREMATURELY.SDR AUS20011403Mount · cracked(AUS) LT AND RT REAR ENGINE MOUNT SUPPORT BRACKETS CRACKED FROM REAR INBOARD BEND RADIUS. NUMEROUS RIVETS IN SURROUNDING STRUCTURE FRETTING.SDR RASFTYRK198Mount Bracket · crackedWHILE PERFORMING A ROUTINE SCHEDULED INSPECTION, INSPECTORS NOTED THE LT FORWARD ENGINE MOUNT BRACKET TO BE CRACKED APPROX 75 PERCENT THROUGH THE LOWER HALF.SDR CA011128006Support · cracked(CAN) CRACK ON THE ENGINE SUPPORT BEAM. REPAIRED.SDR CA011128004Support · cracked(CAN) DURING INSPECTION PER SB A601R-53-059, ONE CRACK ON THE SUPPORT BEAM LOWER WEB INBOARD FORWARD CORNER (BL 36) WAS FOUND ON THE R/H SIDE AND THE L/H SIDE. REPAIR PER REO 601R-53-61-358 WAS CARRIED OUT.SDR CA011128003Support · cracked(CAN) DURING THE INSPECTION OF THE ENGINE SUPPORT BEAM IAW SB A601R-53-059, TWO CRACKS WERE FOUND. ONE ON THE UPPER WEB AT RBL 9.5 AND LEFT LOWARD ACCESS PANEL LEFT FORWARD CORNER.SDR CA011128002Mount · cracked(CAN) CRACKS FOUND ON THE RIGHT SIDE (2.5 INCHES) AND LEFT (TWO CRACKS = CUMULATIVE MEASUREMENT OF APPROXIMATELY 2 INCHES )ACCESS PANEL CUT-OUT.SDR HEEA077257Mount · inoperativeINOPERATIVE.SDR 2002FA0000524Mount · chafedDURING THE 100 HOUR INSPECTION, A FUEL LINE CLAMP WAS FOUND CHAFING ON THE ENGINE MOUNT. THE CLAMP HAD CHAFED APPROXIMATELY .006 INTO ONE OF THE ENGINE MOUNT TUBES. THE CLAMP FOR THIS LINE APPEARS TO BE TOO LONG, ALLOWING IT TO CONTACT THE MOUNT TUBE. THE ESDR HEEA077216Leg Assy · mismarkedMISIDENTIFIED. IT SHOULD BE 206-064-106-001.SDR COMA0160886Mount · corrodedDURING ENGINE CHANGE FOUND CORROSION/FRETTING ON RIGHT ENGINE THRUST MOUNT FITTING FROM 12 O'CLOCK POSITION, TO 6 O'CLOCK POSITION. REPAIRED DAMAGE PER REO 601R-54-50-034. RETURNED TO SERVICE.SDR HEEA077212Leg Assy · mismarkedPARTS MISIDENTIFIED.SDR RASFTYRK183Mount Bracket · crackedWHILE PERFORMING A ROUTINE SCHEDULED INSPECTION, INSPECTORS NOTED THE LT FORWARD ENGINE MOUNT BRACKET TO BE CRACKED APPROX 75 PERCENT THROUGH THE LOWER HALF.SDR RASFTYRK180Mount Bracket · crackedWHILE PERFORMING A ROUTINE SCHEDULED INSPECTION, INSPECTORS NOTED THE LT FORWARD ENGINE MOUNT BRACKET TO BE CRACKED APPROX 75 PERCENT THROUGH THE LOWER HALF.SDR RASFTYRK178Mount Bracket · crackedWHILE PERFORMING A ROUTINE SCHEDULED INSPECTION, INSPECTORS NOTED THE LT FORWARD ENGINE MOUNT BRACKET TO BE CRACKED APPROX 50 PERCENT THROUGH THE LOWER HALF.SDR RASFTYRK189Mount Bracket · crackedWHILE PERFORMING A ROUTINE SCHEDULED INSPECTION, INSPECTORS NOTED THE LT FORWARD ENGINE MOUNT BRACKET TO BE CRACKED APPROX 80 PERCENT THROUGH THE LOWER HALF.SDR 2002FA0000013Mount · crackedWHILE PERFORMING A ROUTINE SCHEDULED INSPECTION, INSPECTORS NOTED THE LT FORWARD ENGINE MOUNT TO BE CRACKED.
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