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 CA021115022Mount · broken(CAN) UPON ENGINE COWLING REMOVAL DURING A SCHEDULED MAINTENANCE EVENT THE O/B UPPER ENGINE MOUNT TRUSS TUBE WAS FOUND BROKEN.SDR 2002UALA01708Mount · chafed#1 ENGINE FORWARD MOUNT CHAFED. AFT SIDE OF FWD ISOLATOR BEARING JOURNAL. MAJOR REPAIR ACCOMPLISHED.INSTALLED NEW FWD MOUNT.SDR 044910Truss · crackedWHILE PERFORMING AN "H" CHECK ON LT ENGINE TRUSS, MAINT FOUND A CRACK AT THE OUTBOARD COWLING ATTACH BRACKET. MAINT R & R WITH ANOTHER TRUSS. UPON RECEIPT OF OLD TRUSS, VENDOR DID A REPORT. REPORT REVEALED THAT A CRACK AT BOTH UPPER COWLING BRACKETS AND CHASDR 2002UALA01685Isolator · wornNR 1 ENGINE FWD MOUNT ISOLATOR JOURNAL ON MOUNT BEAM IS WORN AND DISCOLORED. MAJOR REPAIR ACCOMPLISHED. REPLACED ENGINE MOUNT BEAM.SDR AUS20021300Housing · cracked(AUS) LH ENGINE REAR MOUNT HOUSING CRACKED. RH ENGINE REAR MOUNTHOUSING REWORKED.SDR CA021105008Mount · cracked(CAN) ENGINE MOUNT CRACKED AT RT TOP AT THE WELDED JOINT.SDR AUS20021262Mount · deteriorated(AUS) ENGINE MOUNT RUBBERS BADLY DETERIORATED. AIRCRAFT HAS OPERATEDFOR 20.7 HOURS SINCE PERIODIC INSPECTION. PERSONNEL/MAINTENANCE ERROR.SDR QH52002F00002Bolt · crackedCRACK IN THE HEAD OF THE BOLT.SDR QXEA0201808Truss · chafedPDX - RIGHT HAND SIDE TRUSS MOUNT, LOWER TUBE IS CHAFED NEXT TO IGNITION EXCITERS AND TRANSMITTER. REPAIRED IAW RD 8-54-036.SDR CA021028005Mount · worn(CAN) FOUND BALL BEARING WORN AND MOUNT GOUGED AT C CHECK, BEARING REPLACED AND BLEND DONE. TOTAL AIRCRAFT TIME 13,073 HRS6,295CYCLESSDR 2002F00989Truss · crackedAIRCRAFT 166 WAS IN FOR A STRUCTURAL INSPECTION. WHILE IN MAINTENANCE, THE RT TRUSS WAS DISCOVERED TO HAVE A CRACK AT THE INBOARD AND OUTBOARD UPPER COWLING SUPPORT BRACKETS. REMOVED AND REPLACED THE RT TRUSS. REPORT STATES THAT VENDOR FOUND THE TRUSS CRACKED SDR 2002F00990Truss · crackedAIRCRAFT 123 WAS IN FARMINGTON NEW MEXICO FOR A STRUCTURAL INSPECTION. WHILE IN MAINTENANCE, THE RIGHT TRUSS WAS FOUND TO BE CRACKED ON THE INBOARD AND OUTBOARD COWLING SUPPORT BRACKETS. THE CORRECTIVE ACTION WAS THAT THEY REMOVED AND REPLACED THE RIGHT TRUSS.SDR AUS20021201Beam · cracked(AUS) LH ENGINE CROSSOVER BEAM CRACKED. FURTHER INVESTIGATION FOUND THAT THE LH MOUNTS DROPPED IN MOUNT BRACKETS AND PUT OUTWARD LOAD ON THE ENGINE LONGITUDINAL BEAMS.SDR GTIA021045Isolator · corrodedDTW - NR 2 ENGINE FORWARD LOWER VIBRATION ISOLATOR IS CORRODED AND PLATING IS FLAKING OFF ON INNER CONICAL AREA. REMOVED AND REPLACED NR 2 ENGINE FORWARD LOWER VIBRATION ISOLATOR (CLOSED 10/15/02). (M)SDR GTIA021037Isolator · defectiveDTW - FOUND LOWER NR 1 ENGINE ISOLATOR DOES NOT HAVE ANTI-ROTATION MARK. REMOVED AND REPLACED NR 1 ENGINE LOWER ISOLATOR, CLOSED 10/10/02. (M)SDR GTIA021036Isolator · defectiveDTW - FOUND UPPER NR 1 ENGINE ISOLATOR DOES NOT HAVE ANTI-ROTATION MARK. REMOVED AND REPLACED NR 1 ENGINE UPPER ISOLATOR, CLOSED 10/10/02. (M)SDR CA021010003Mount · cracked(CAN) ENGINE MOUNT ASSEMBLY CRACKED AT LOWER CROSS MEMBER RT SIDE.SDR DLM90021374Strut · wornA THRUST STRUT WAS FOUND TO HAVE WEAR DAMAGE BEYOND CMM LIMITS. A DER PROVIDED A BLEND REPAIR FOR THE ONE AREA OF DAMAGE. A DTA ASSESSMENT IS REQUIRED FOR CONTINUED SERVICE BEYOND THE TIME LIMITED REPAIR LIMIT.SDR DLM90021373Strut · wornA THRUST STRUT WAS FOUND TO HAVE THREE AREAS OF WEAR DAMAGE BEYOND CMM LIMITS. A DER APPROVED BLEND REPAIR WAS PROVIDED. A DTA ASSESSMENT IS REQUIRED FOR CONTINUED SERVICE BEYOND THE TIME LIMITED REPAIR LIMIT.SDR DLM90021372Strut · wornTHE THRUST STRUT WAS FOUND TO HAVE WEAR DAMAGE IN TWO PLACES ON THE STRUT BODY. A TIME LIMITED BLEND REPAIR WAS APPROVED BY A DER. A DTA ASSESSMENT IS REQUIRED TO AUTHORIZE CONTINUED SERVICE BEYOND THE TIME LIMITED REPAIR.SDR USAA020371Mount · wornPIT - FOUND ENGINE MOUNT CROSSBEAM WORN LUG, LUG BORE ON ENGINE MOUNT. MACHINE INSIDE DIAMETER OF LUG BORE TO OVERSIZE BEARING PER TYPICAL REPAIR 550-19 REV B. (M)SDR AMWA5Truss · crackedWHILE PERFORMING AND "H" CHECK ON THE RT TRUSS IN, MECHANICS DISCOVERED A CRACK LOCATED ON THE UPPER RT COWLING BRACKET. THE CRACK WAS ON THE OUTBOARD SIDE OF THE TRUSS. THE CORRECTIVE ACTION WAS THAT THEY REMOVED AND REPLACED THE TRUSS. UPON RECEIPT OF THE TRSDR CA021028006Link · cracked(CAN) DURING AN INSPECTION (AD 2001-20-09), THE RT TRUNNION LINK BUSHING WAS FOUND LOOSE. UPON REMOVAL OF THE TRUNNION LINK ASSYEMBLY, IT WAS NOTED THAT THE FORWARD BEARING END (RACE) HAD AN APPROXIMATLEY 2 INCH CRACK ALONG IT'S VERTICAL AXIS. NOTE: TSN IS UNSDR CA021016032Mount · cracked(CAN) CRACK FOUND IN LOWER CORNERS OF ENGINE MOUNT RING.SDR AUS20021166Mount · cracked(AUS) ENGINE MOUNT CRACKED IN SEVERAL AREAS. FURTHER INSPECTION FOUND BOTH LOWER ENGINE MOUNT BRACKETS LOCATED BEHIND THE FIREWALL ALSO CRACKED. LH AND RH TOP FUSELAGE SKINS REMOVED FOR INSPECTION ANDLH TOP MOUNT STRUCTURE FOUND CRACKED. LH RUDDER BAR ATTACHMESDR USAA020362Mount · wornPIT - FOUND BEARING BORE .005 INCH BEYOND LIMITS, UNIT HAS ONLY ONE BEARING FORWARD HOLE. OVERSIZED 0.005 INCH, MACHINED TO 1.445-1.4430 PER TYPICAL REPAIR 54-50-08 REV B. (M)SDR 2003F00381Truss · chafedAT SCHEDULED ROUTINE MAINTENANCE, CHAFING DAMAGE AT 3 INCHES AFT OF FIRE SEAL FLANGE ON INBOARD SIDE. PERFORMED TRUSS REPAIR TO CHAFED AREA IAW FAA APPROVED DATA CONTAINED IN RAYTHEON FIELD REPAIR FR-CO-00706 REV. (M)SDR PCAA0209104Strut · brokenDURING A LEVEL INSPECTION LEFT OUTBOARD AFT ENGINE STRUT WAS FOUND BROKEN. ENGINE STRUT WAS REPLACED IN ACCORDANCE WITH DEHAVILLAND DASH 8 MAINTENANCE MANUAL 71-20-00. AIRCRAFT RETURNED TO SERVICE.SDR UAO2002F00000Truss · brokenDURING A PHASE INSPECTION IT WAS NOTED THAT THE EXHAUST HEATSHIELD FORWARD OF THE TURBO COMPRESSOR HAD CHAFED AN AREA .1875 INCH X .3125 INCH THROUGH THE ENGINE MOUNT TRUSS. THIS WAS CAUSED BY THE HEATSHIELD MOUNT BREAKING ALLOWING THE HEATSHIELD TO DROP ONTOSDR CA020821002Isolation Mount · debonded(CAN) DURING A ROUTINE INSPECTION OF THE RT ENGINE. THE UPPER INBOARD VIBRATION ISOLATOR ENGINE MOUNT WAS FOUND TO BE DEBONDED, THE BACK HALF OF THE RUBBER WAS DEBONDED FROM THE METAL FACE PLATE. THE MOUNT WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE.SDR QXEA0201260Mount · chafedPDX - NR 2 ENGINE NACELLE LOWER INBOARD DIAGONAL MOUNT STRUT HAS CIRCULAR CHAFE AT MID SPAN ON OUTBOARD SIDE. REPAIRED IAW RD 8-54-036.SDR QXEA0201259Mount · gougedPDX - NR 2 ENGINE NACELLE UPPER INBOARD DIAGONAL MOUNT STRUT HAS GOUGE MID SPAN ON TOP SIDE. REPAIRED IAW RD 8-54-036.SDR CA020830016Mount · cracked(CAN) ENGINE MOUNT HAD BROKEN TUBE JUST ABOVE FISHMOUTH WELD 11 INCHES BELOW UPPER RT FUSELAGE ATTACH.SDR CA020918009Mount · chafed(CAN) FOLLOWING ENGINE MOUNT REPLACEMENT FOR SB 1103, IT WAS DISCOVERED THE MOUNT CHAFED ON ONE ENGINE MOUNT TUBE BECAUSE OF A PIECE OF THE PLENUM MAKING CONTACT. CORROSION HAD STARTED TO TAKE PLACE. THE PROBLEMATIC PART (A BOOT SEALING THE PLENUM AROUND AN SDR AUS20020793Mount · burned(AUS) RT ENGINE UPPER MOUNT HEAT DAMAGED. HEAT DAMAGE ALSO FOUND ON HOSES PN SS1001K000312 AND PN SS1001F0000100. NO CAUSE OF DAMAGE WAS FOUND BUT IT IS SUSPECTED THAT A FUEL LEAK HAD OCCURRED AT THE NR 10 FUEL NOZZLE FITTING ALTHOUGH THE FITTING WAS FOUND TOSDR USAA020283Mount · wornPIT - FOUND ENGINE MOUNT WORN BEYOND LIMITS. MACHINED, CHAMFER, MPI, ROTOPEEN PER TYPICAL REP 50-50-08 REV B. (M)SDR USAA020282Mount · wornPIT - FOUND ENGINE MOUNT STRUT WORN BEYOND LIMITS, ENGINE MOUNT MAIN SLEEVE REPAIR. REAMED, CHAMFERED, BLENDED AND ROTOPEENED THE FITTING BORE PER TYPICAL 54-50-10 REV A. (M)SDR GTIA020897Isolator · damagedFTW - FOUND RIGHT ENGINE FORWARD LOWER VIBRATION ISOLATOR INNER CORE ASSEMBLY CONTACTING OUTER RETAINER AND SLIPPAGE MARKS MORE THEN .5 INCH. REMOVED RIGHT ENGINE FORWARD LOWER VIBRATION ISOLATOR INNER CORE ASSEMBLY. INSTALLED RIGHT LOWER VIBRATION ISOLATOR.SDR QXEA0200969Support · chafedPDX - LT NACELLE UPPER INBOARD ENGINE SUPPORT TUBE IS CHAFED WHERE WIRE BUNDLE IS IN CONTACT APPROXIMATELY 12 INCHES FROM AT END OF TUBE. REPAIRED IAW RD 8-54-036 AND HORIZON AIR EA 2-54-147.SDR QXEA0200968Support · chafedPDX - LT NACELLE LOWER INBOARD ENGINE SUPPORT TUBE IS CHAFED APPROXIMATELY 22 INCHES FROM FORWARD END. REPAIRED IAW RD 8-54-036 AND HORIZON AIR EA 2-54-147.SDR ASOA02386Support · crackedDURING HANGAR MAINTENANCE IN MCN, A CRACK WAS FOUND IN THE BOX BEAM AREA OF THE LOWER RIGHT ACCESS PANEL ON THE INBOARD SIDE AS VIEWED THROUGHT THE LIGHTENING HOLE. MAINTENANCE REPAIRED THE CRACKED ENGINE SUPPORT BEAM IAW ASA EO 600-53-0070. (M)SDR QXEA0201023Strut · chafedPDX - LIGHT SURFACE CHAFING ON INBOARD SIDE OF LOWER RIGHT ENGINE STRUT, ON RIGHT NACELLE. REPAIRED IAW DHC-8 RD 8-54-036.SDR 2002F01074Mount Bracket · corrodedAT C-CHECK, FOUND NR 2 ENGINE, AFT VIBRATION ISOLATOR ASSEMBLY MOUNT BRACKET RUSTED AND CORRODED ON FRONT AND BACK SIDE. (M)SDR GTIA020793Isolation Mount · damagedFTW - NR 1 ENGINE AFT MOUNT ISOLATOR, INNER CONICAL SURFACE HAS NICKS, SCRATCHES AND WORN PLATING. REMOVED NR 1 ENGINE AFT MOUTN ISLOATOR. INSTALLED SVC, NR 1 ENGINE AFT MOUNT ISOLATER. (M)SDR HEEA080291Leg Assy · mismarkedENGINE MOUNT LEG ASSY IDENTIFIED AS LEFT HAND BUT IS ACTUALLY A RIGHT HAND.SDR HEEA080257Bipod Mount · wornENGINE BIPOD MOUNT WORN.SDR HEEA080256Bipod Mount · wornENGINE BIPOD MOUNT WORN.SDR HEEA080255Mount · wornENGINE BIPOD MOUNT WORN.SDR HEEA080130Tube · wornENGINE MOUNT TUBE HAS WORN BEARING. SCRAPPED.SDR GTIA020795Isolation Mount · wrong partFTW - FOUND LEFT ENGINE FORWARD UPPER AND LOWER VIBRATION ISOLATORS MISMATCH. REMOVED LEFT ENGINE FORWARD UPPER AND LOWER VIBRATION ISOLATORS. INSTALLED NEW UPPER AND LOWER ISOLATORS. (M)
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