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 MASA98077Truss Bolts · looseFLT 5330 - JAX-PBI - IN FLIGHT, CREW NOTICED THE RIGHT COWLING WAS LOOSE. CREW REDUCED POWER TO THE RT ENGINE AND RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE FOUND THE UPPER INBOARD TRUSS BOLT WAS LOOSE. REMOVED AND REPLACED THE ENGINE TRUSS AND BOLTSDR CA980407008Mount · cracked(CAN) ENGINE MOUNT ARM FROM LOWER LEFT FIREWALL TO NOSE GEAR CRACKED AT FIREWALL. POSSIBLY DUE TO CROSS WIND LANDING. REPAIRED.SDR 98ZZZX1484Bracket · displacedFOUND LEFT LOWER ENGINE MOUNT BRACKET DISPLACED FROM NORMAL POSITION. THIS MAY HAVE OCCURRED DURING UNDOCUMENTED REPAIR IN AREA BY PERSONS UNKNOWN.SDR 98ZZZX1551Mount · crackedDURING ANNUAL INSPECTION, FOUND ENGINE MOUNT CRACKED ON RT SIDE. CRACK IS LOCATED WHERE NLG HYDRAULIC ACTUATOR ATTACHES TO MOUNT. DESIGN REQUIRES ACTUATOR TO BE POSITIONED SUCH THAT IT STRESSES THE MOUNT.SDR 98ZZZX3101Support · mismanufacturedENGINE MOUNT SUPPORT REJECTED, NEW OUT-OF-BOX. FAILED DIMENSIONAL CHECK. AREA NR 2 EXCEEDS LIMITS AT 13.98 MM. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.SDR 98ZZZX1462Bracket · crackedLOWER RIGHT FIREWALL ENGINE MOUNT BRACKET FOUND CRACKED INTO TWO PIECES. UPPER LEFT AND RIGHT BRACKETS FOUND TO HAVE SIMILAR CRACKS, BUT NOT AS EXTENSIVE. AREA IS DIFFICULT TO INSPECT AS ENGINE MOUNT BOLTS NEED TO BE REMOVED AND BRACKETS ARE OFTEN COVERED UPSDR 98ZZZX1461Bracket · crackedLOWER RIGHT FIREWALL ENGINE MOUNT BRACKET FOUND CRACKED INTO TWO PIECES. UPPER LEFT AND RIGHT BRACKETS FOUND TO HAVE SIMILAR CRACKS, BUT NOT AS EXTENSIVE. AREA IS DIFFICULT TO INSPECT AS ENGINE MOUNT BOLTS NEED TO BE REMOVED AND BRACKETS ARE OFTEN COVERED UPSDR AALA980522Mount · damagedTUL - FOUND LIGHT DAMAGE ON RT ENGINE PYLON FORWARD ATTACH FITTING LOWER FWD RT SIDE. BLENDED PER ESO 30595, DATED 3-16-98 AND FLAPPER PEENED WORK AREA PER SRM 51-29-00 (AA SPECIFICATION PAGE 16-19) PRIMED AND PAINTED. (M)SDR 98ZZZX1466Bracket · crackedCRACK RADIATING FROM ENGINE MOUNT BOLT HOLE. THIS IS THE SECOND CESSNA 175 SUBMITTER FOUND WITH CRACKED BRACKETS. VISUAL INSPECTION IS SATISFACTORY TO IDENTIFY CRACKS, BUT GAINING ACCESS TO BRACKET MAY REQUIRE REMOVAL OF ENGINE MOUNT BOLT/NUT AND WAHSERS.SDR 98ZZZX1465Bracket · crackedCRACK RADIATING FROM ENGINE MOUNT BOLT HOLE. THIS IS THE SECOND CESSNA 175 SUBMITTER FOUND WITH CRACKED BRACKETS. VISUAL INSPECTION IS SATISFACTORY TO IDENTIFY CRACKS, BUT GAINING ACCESS TO BRACKET MAY REQUIRE REMOVAL OF ENGINE MOUNT BOLT/NUT AND WAHSERS.SDR 98ZZZX1464Bracket · crackedCRACK RADIATING FROM ENGINE MOUNT BOLT HOLE. THIS IS THE SECOND CESSNA 175 SUBMITTER FOUND WITH CRACKED BRACKETS. VISUAL INSPECTION IS SATISFACTORY TO IDENTIFY CRACKS, BUT GAINING ACCESS TO BRACKET MAY REQUIRE REMOVAL OF ENGINE MOUNT BOLT/NUT AND WASHERS.SDR CALA9800414Bolts · looseINSPECTION FOUND NR 3 ENGINE FORWARD ENGINE MOUNT TRUSS BOLTS LOOSE AT TRUSS TO PYLON BOX INTERSECTION LOWER SURFACE. THE BOLTS WERE RETORQUED IAW SERVICE BULLETIN A54-99.SDR AU980281Mount · worn(AUS) LT ENGINE MOUNT TOP RT DIAGONAL BRACE HAD A HOLE WORN THROUGH BY THE TOP OF THE SWITCH ON THE ANTI-ICE VALVE P/N 319980-13-1. SIZE OF HOLE APPROXIMATELY 4.762MM (0.1875 INCH).SDR 98ZZZX1329Beam Assy · crackedDURING PHASE INSPECTION, UPPER OUTBOARD AFT VERTICAL WEB MEMBERS OF AFT BEAM ASSEMBLIES WERE FOUND CRACKED. THIS AFFECTED BEAMS IN BOTH NACELLES. SUBMITTER SUSPECTS CAUSE WAS HARD LANDING. AIRCRAFT REMOVED FROM SERVICE PENDING REPAIRS.SDR 98ZZZX1325Beam Assy · looseDURING PHASE INSPECTION, SEVERAL LOOSE AND WORKING RIVETS WERE FOUND IN TOP OF INBOARD ENGINE MOUNT BEAM APPROXIMATELY 6 INCHES AFT OF AFT ENGINE MOUNT BRACKET. SUBMITTER STATED POSSIBLY CAUSED BY HARD LANDING OR TURBULENCE.SDR CA980303007Mount · cracked(CAN) ENGINE MOUNT CRACKED NEAR BOTTOM RIGHT ENGINE MOUNT BUSHING. REPAIRED.SDR 98FDEA00123Fitting · looseNR 1 ENG FWD ENG MOUNT TRUSS FITTING HAS 25 TO 30 BOLTS LOOSE AND 1 SHEARED LT AND RT. *S/D* COMPLIED WITH EA 8-5410-35982 PYLON FORWARD ENG MOUNT TRUSS FITTING. FITTING BOLTS FOUND UNDER TORQUE (2) DURING PYLON INSP.SDR 98ZZZX1577Bushing · wornENGINE MOUNT BUSHING'S ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.SDR 98ZZZM346Arm · brokenDURING 'A' CHECK, FOUND LEFT ARM OF NR 4 ENGINE MOUNT ASSEMBLY BROKEN IN THE THREADED AREA AND NUT MISSING, REF DACO IPC 71-20-0 FIG 16 ITEM 65 AND 30). REPLACED AFT ENGINE MOUNT ASSEMBLY AND RETURNED AIRCRAFT TO SERVICE. (M)SDR 98ZZZX1122Mount · crackedWHILE INVESTIGATING A ROUGH ENGINE, FOUND AN ENGINE MOUNT TUBE CRACKED THROUGH ON LT ENGINE INBOARD, UPPER CLUSTER, LOWER TUBE. INSTALLED DIFFERENT REPAIRED TRUSS.SDR EIAA98053Bushing · wornHKG - DURING 'C5/D' CHECK INSPECTION, NR 3 PYLON AFT UPPER MOUNT HAS WORN ATTACH BUSHING AND SIDE PLAY. ENGINE UPPER MOUNT BUSHING REPLACED IAW OHM 20-50-03. (M)SDR EIAA98052Bushing · wornHKG - DURING 'C5/D' CHECK INSPECTION, NR 4 PYLON AFT UPPER MOUNT HAS WORN ATTACH BUSHING AND SIDE PLAY. THRUST LINK END FITTING WORN. ENGINE UPPER MOUNT BUSHING REPLACED IAW OHM 20-50-03, THRUST LINK BEARING REPLACED IAW OHM 20-50-03. (M)SDR 98ZZZX904Bearing · wornHKG - DURING C5/D-CHECK INSPECTION, NR 4 PYLON AFT UPPER MOUNT HAS WORN ATTACH BUSHING AND SIDE PLAY. THRUST LINK END FITTING WORN. ENGINE UPPER MOUNT BUSHING REPLACED IAW OHM 20-50-03, THRUST LINK BEARING REPLACED IAW OHM 20-50-03. REFERENCE: OPERATOR CONSDR 98ZZZM333Bearing · wornHKG - DURING 'C5/D' CHECK INSPECTION, NR 4 PYLON AFT UPPER MOUNT HAS WORN ATTACH BUSHING AND SIDE PLAY. THRUST LINK END FITTING WORN. ENGINE UPPER MOUNT BUSHING REPLACED IAW OHM 20-50-03, THRUST LINK BEARING REPLACED IAW OHM 20-50-03. (M)SDR EIAA98048Bearing · rotatingHKG - DURING 'C5/D' CHECK INSPECTION, NR 4 PYLON THRUST LINK BEARING IS ROTATING IN THE HOUSING. BEARING REPLACED IAW OHM 20-50-03. (M)SDR CA980317024Nut · loose(CAN) DURING INSPECTION, FOUND FORWARD MOUNT BOLTS WITH BROKEN LOCKWIRE. LOW TORQUE VALUES WERE CONFIRMED. REPLACED RT AND LT MOUNT BOLTS AND NUTS. PART TT: 65,430 HOURS.SDR P5CA9800228Mount Bolt · looseNR 4 PYLON FWD MOUNT INBD BOLT WASHER ON HEAD SIDE LOOSE. REMOVED WEIGHT OF ENGINE FROM FWD MOUNT. RETORQUED LOOSE BOLD PER MM 71-21-01.SDR AU980118Mount · corroded(AUS) RH ENGINE MOUNTS BADLY CORRODED.SDR 98ZZZX854Bolt · seizedENGINE NR 1 WAS BEING REMOVED FOR MAINTENANCE. WHEN THE UPPER MOUNT BOLT, WHICH ATTACHES ENGINE TO AIR FRAME WAS BEING REMOVED, THE BOLT STOPPED TURNING AND WAS FROZEN SOLID INTO ENGINE MOUNT. BOLT HEAD WAS CUT OFF TO REMOVE ENGINE. BOLT IS MADE OF STAINLESSDR 98ZZZX853Bolt · seizedENGINES NR 1 AND NR 3 WERE BEING REMOVED FOR MAINTENANCE. WHEN THE UPPER MOUNT BOLTS, WHICH ATTACH ENGINES TO THE AIR FRAME, WERE BEING REMOVED THE BOLT STOPPED TURNING AND WAS FROZEN SOLID INTO ENGINE MOUNT. BOLT HEAD WAS CUT OFF TO REMOVE ENGINE. BOLT IS SDR 98ZZZX846Mount · crackedDISCOVERED CRACKED HORIZONTAL TUBE MEMBER ON ENGINE MOUNT. THE CRACKED MEMBER IS THE .50 INCH DIAMETER TUBE RUNNING FROM THE OUTSIDE .6250 INCH TUBE TO THE CENTER LANDING GEAR MOUNTING POSITION. THIS CONDITION WAS DISCOVERED DURING AN ANNUAL INSPECTION. NO SDR 98ZZZX995Bracket · failedDURING NORMAL ANNUAL INSPECTION, FOUND BOTH ENGINE MOUNTS BROKEN THROUGH THE MIDDLE. THIS CAUSED ENGINE TO LAY FARTHER DOWN ON ITS LEFT SIDE CAUSING FURTHER DAMAGE TO VALVE COVERS, COWLING, INTAKE MANIFOLD. MOUNTS HAD BROKEN SINCE LAST OIL CHANGE APPROXIMATESDR HEEA0012738Bearing Rod End · wornROD END HAS TOO MUCH PLAY ON NEW BEARING.SDR EIAA98021Bushing · wornHKG - DURING 'C5/D' CHECK INSPECTION, NR 1 PYLON FORWARD UPPER ENGINE MOUNT HANGERS MOUNT BUSHING WORN. BUSHINGS REPLACED IAW OHW 20-50-03. (M)SDR 98ZZZX714Mount · crackedCRACK FOUND DURING ANNUAL INSPECTION AT UPPER FRONT ELBOW OF ENGINE MOUNT SUPPORT BRACKET. PREVIOUS UNRECORDED REPAIR HAD BEEN MADE, BUT CRACK HAS CONTINUED TO PROGRESS. CAUSE UNKNOWN. LEFT SUPPORT SHOWS NO STRESS.SDR AU980020Bolt · loose(AUS) LH LOWER ENGINE MOUNT BRACKET BOLTS LOOSE. SUSPECT BOLTS INCORRECTLY TORQUED AT MANUFACTURE.SDR 98ZZZX896Mount Bracket · crackedDURING ANNUAL INSPECTION, NOTICED RT REAR ENGINE MOUNT BRACKET RIVETS WERE LOOSE. AFTER REMOVAL OF ENGINE, FOUND BOTH REAR MOUNTS WERE CRACKED AT FORWARD EDGE OF REAR SUPPORT MEMBER. TOTAL TIME OF AIRCRAFT WAS A CONTRIBUTING FACTOR, BUT EXTRA CARE SHOULD BE SDR DL72K980064Nut · missingFOUND DURING C-1 CHECK, UPPER ENGINE MOUNT CONE BOLT NUT MISSING AND BOLT BACKED OUT ABOUT .25 INCH. LOWER ENGINE MOUNT CONE BOLT NUT LOOSE, NO TORQUE STRIPS. DROPPED ENGINE AND REPLACED CONE BOLTS REF TRANS 4T216, OPN 5130, ERA 279520-14, SI 4-72242-12.SDR 98ZZZM830Yoke · chafedNR 4 PYLON MOUNT YOKE HAS THE PYLON DRAIN LINE CHAFING ON ITS RIGHT SIDE TOP SURFACE. REMOVED NR 4 PYLON ENGINE FRONT MOUNT YOKE. INSPECTED AND FOUND CHAFEAGE TO BE WITHIN 146 SRM 54-50-41 LIMITS. BLENDED AREA AND REINSTALLED MOUNT YOKE IAW MM 71-10-11. (MSDR 98ZZZM235Truss · crackedON INSPECTION, NR 1 ENGINE TRUSS INBOARD SIDE UPPER HAS CRACK. WELDED CRACK IAW MANUFACTURERS REPAIR INSTRUCTIONS CONTAINED IN KIT NR 114-9033-1, PARAGRAPH 16. (M)SDR 98ZZZX2742Mount · damagedATW - NR 3 PYLON SHOULDER COWL LORD MOUNT BRACKET CENTER RIVET HEAD SHEARED OFF. REPLACED NR 3 PYLON LORD MOUNT BRACKET CENTER FASTENER IAW BAE FAX PJN/1196R-92.SDR 98ZZZX2766Mount · corrodedNR 1 MOTOR YOKE ASSEMBLY HAS SLIGHT SURFACE CORROSION AT CENTER AREA OF YOKE. CLEANED AREA AND REMOVED SURFACE CORROSION FROM NR 1 ENGINE MOUNT YOKE IAW A46 SRM 51-20-11. COATED AREA. REF: 51-20-11.SDR 98ZZZX2739Mount · damagedATW - NR 1 PYLON LORD MOUNT ATTACH BRACKET CENTER RIVET SHEARED. INSTALLED BOLT AT CENTER LORD MOUNT RACKET POSITION. REF: FAX PJN/1196R-92. REPLACED BOTH LORD MOUNT RUBBER BUSHINGS.SDR DL72S980016Cone Bolt · brokenNR 1 ENG IDLES AT 1.2 EPR IN FLT. FOUND AFT ENG MOUNT CONE BOLT BROKEN. MTC IN PROGRESS REPLACING CONE BOLT AND ISOLATOR.SDR 98ZZZX2735Mount · corrodedATW - NR 2 PYLON YOKE HAS SLIGHT SURFACE CORROSION IN CENTER OF YOKE. REMOVED CORROSION FROM SURFACE OF NR 2 PYLON YOKE CENTER AND COATED SURFACE WITH CARBOLINE.SDR 98ZZZX173Mount · mismanufacturedUPON ARRIVAL OF A NEW ENGINE MOUNT, DISCOVERED TWO OF THE WELD JOINTS WERE DEFECTIVE. THE GUSSET PLATES ON BOTH UPPER BRACE ARMS WERE NOT WELDED DOWN, ONLY TACK-WELDED TO THE BRACE ARMS. THE MANUFACTURER SAID THAT ALTHOUGH IT WAS NOT CORRECT, SEVERAL UNITS HSDR AU971570Bracket · cracked(AUS) ENGINE MOUNT TO WING ATTACHMENT BRACKETS (3OFF) WERE FOUND CRACKED:1. LH LOWER INBOARD PNO 68-1.2027,2. RH UPPER INBOARD PNO 68-1.2025-1 AND 3. RH UPPER OUTBOARD PNO 68-1.2025-3. FOUND IAW AD/P68/28A3, SECTION 3.SDR 98ZZZX251Tube · corrodedDEFECT DISCOVERED DURING 1,750 HOURLY INSPECTION OF ENGINE MOUNTS. WHILE BORESCOPING INSIDE OF TUBE, CORROSION WAS FOUND THAT EXCEEDED LIMITS. INSIDE OF TUBE ASSEMBLY CORRODED AND PITTED. SUBMITTER SUGGESTED USING BETTER CORROSION PREVENTATIVE METHODS.SDR AU971575Mount · cracked(AUS) RH LOWER O/B ENGINE MOUNT CRACKED AT THE TURBOCHARGER MOUNT HOLE.SDR AU971574Mount · cracked(AUS) LH LOWER I/B ENGINE MOUNT CRACKED AT THE TURBOCHARGER MOUNT HOLE.
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