JASC 5415
Service difficulty reports · 1,305
Reports filed under 5415 · Nacelle/Pylon, Attach Fittings, 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 = '5415' 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 = '5415' 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 RAAA98B1001Fitting · crackedDURING SCHEDULED AD 89-23-17 INSPECTION, FOUND NR 1 ENGINE AFT MOUNT SUPPORT FITTING CRACKED AT BS 1243, LBL 60. TWO CRACKS APPROX 1 IN EACH IN FITTING FWD SIDE UPPER FLANGE AND RADIUS. REPLACED AFT MOUNT SUPPORT FITTING PER S/B 727-54-0017 AND DWG 65C34829,SDR CA980317004Rivets · sheared(CAN) RIGHT HAND NACELLE SURGE DAMPER ATTACH BRACKET RIVETS SHEARED. AIRCRAFT TT: 18,688 HOURS.SDR DL757972354Fitting · mismanufacturedTHE CONDUCTIVITY INSPECTION OF THE DIAGONAL DRAG BRACE FITTING ON THE NR 2 ENGINE PYLON GAVE READINGS OUTSIDE THE CONDUCTIVITY REGION FOR 7075-T76. THE FITTING WAS ALLOWED TO CONTINUE IN SERVICE WITH LETTER CHECK INSPECTIONS PER ER/A 363151-14.SDR P5CA9701590Fuse Pin · corrodedLEVEL 2 CORROSION ON NR 4 PYLON OUTBOARD FUSE PIN INSERT. REPLACED FUSE PIN PER BAC MM 54-10-03.SDR P5CA9701570Panel · crackedCRACK ON PANEL NR 462EL ON NR 2 PYLON. FABRICATED AND INSTALL REPLACEMENT PANEL PER BAC SRM 51-30-02.SDR 97ZZZX4661Casting · crackedWHILE ACCOMPLISHING A FLEET-WIDE INSPECTION OF AIRCRAFT, A CASTING CRACK WAS FOUND ON A SECOND UNIT WITHIN FLEET.SDR 97ZZZX4662Casting · crackedWHILE ACCOMPLISHING PRE-FLIGHT, CREW NOTICED MORE MOVEMENT IN THE RIGHT (NR 2) JET THAN THE LEFT. FURTHER INVESTIGATION BY MAINTENANCE REVEALED A CRACK EXTENDING HORIZONTALLY THROUGH THE P/N 513485 FORWARD JET PYLON MOUNT CASTING.SDR 97UAL900610Fitting · crackedTHE NR 1 PYLON RIGHT-HAND TRUSS FITTING IS CRACKED. THE CRACKS PROPAGATE FROM THREE FASTENER HOLES. THE CRACKS ARE NOT CONTINUOUS AND DO NOT EXTEND INTO FILLET RADIUS. *S/D* INSTALLED INTERIM REPAIR PER EVA SFO-1503 AND ALERT BULLETIN A54-99/A54-103. THE SDR ABXA9701384Fitting · corrodedWHILE COMPLYING WITH 'D' INSPECTION, FOUND THE LEFT ENGINE PYLON UPPER BEAVERTAIL FITTING CORRODED. REMOVED AND REPLACED LEFT BEAVERTAIL FITTING AND REPAIRED AREA IAW ABX REA D954-20135-MR AND DC-9 SRM CHAPTER 51-30-5.SDR ABXA9701387Fitting · corrodedWHILE COMPLYING WITH 'D' INSPECTION, FOUND THE LEFT ENGINE PYLON LOWER BEAVERTAIL FITTING CORRODED. REPAIRED LEFT LOWER BEAVERTAIL IAW ABX REA D954-20074 AND DC-9 SRM CHAPTER 53-04, FIGURE 13.SDR ABXA9701386Fitting · corrodedWHILE COMPLYING WITH 'D' INSPECTION, FOUND THE RIGHT ENGINE PYLON LOWER BEAVERTAIL FITTING CORRODED. REPAIRED RIGHT PYLON LOWER BEAVERTAIL IAW ABX REA D954-19607-MR.SDR P5CA9701330Fitting · corrodedLEVEL 1 CORROSION, UPPER LINK FORWARD FITTING (ON PYLON) BORE CORRODED NR 4 PYLON. REMOVED CORROSION IAW SB 54-2164. NON ROUTINE CARD S/N 6002.SDR 97ZZZX2966Fuse Pins · crackedDURING C-CHECK INSPECTION, DISCOVERED NR 1 PYLON INBOARD/OUTBOARD STRUT ATTACH FUSE PINS CRACKED (FUSE PINS HAD 3,814 CYCLES). REPLACED FUSE PINS WITH (15-5PH) P/N 311N5217-1 FUSE PINS.SDR ABXA9701113Fitting · crackedDURING C-CHECK, FOUND THE RIGHT ENGINE PYLON REAR SPAR UPPER FITTING CRACKED AT THE FWD INBD CORNER. REPLACED FITTING IAW DC9 SRM.SDR EIAA970164Fitting · gougedHKG - DURING C5/D-CHECK INSPECTION, DISCOVERED NR 3 PYLON UPPER LINK WING ATTACH FITTING OUTBOARD HALF WAS GOUGED AND CORRODED. REPAIRS ACCOMPLISHED IAW RS 57-04-33335 AND BOEING TELEX EVR-HKG-97-0096RE, REWORKED. (M)SDR EIAA970162Fitting · damagedHKG - DURING C5/D-CHECK INSPECTION, DISCOVERED NR 2 PYLON FRONT SPAR UPPER LINK INBOARD FITTING HAS TOOL MARKS. REPAIRS ACCOMPLISHED IAW RS 57-04-33343 AND BOEING TELEX EVR-HKG-97-0114RE, REWORKED. (M)SDR EIAA970161Fitting · damagedHKG - DURING C5/D-CHECK INSPECTION, DISCOVERED NR 1 PYLON FRONT SPAR UPPER LINK OUTBOARD FITTING HAS TOOL MARKS. REPAIRS ACCOMPLISHED IAW RS 57-04-33352 AND BOEING TELEX EVR-HKG-97-0103RE, REWORKED. (M)SDR IXXA9700132Attach Fitting · crackedDURING ROUTINE C-CHECK INSPECTION, THE NR 3 PYLON FOOTSTOOL FITTING WAS FOUND TO BE CRACKED. THE FITTING WAS REMOVED AND REPLACED IN ACCORDANCE WITH THE DOUGLAS STRUCTURE REPAIR MANUAL 51-3-0, 51-1-20D AND 51-1-21.SDR P5CA9700432Heatshield · crackedNR 1 PYLON - STRUT HEATSHIELD CRACKS AND ELONGATED HOLES. REMOVED HEATSHIELD AND FABRICATED PER BOEING SRM 51-30-02.SDR P5CA9700411Skin · damagedNR 4 PYLON NAC STA 160 LEFT SIDE HAD ELONGATED HOLE. REPAIRED PER BOEING SRM 51-40-02.SDR P5CA9700401Pylon · crackedNR 4 PYLON FIXED AFT FAIRING CRACKED AT FWD ATTACH SUPPORT. REPAIRED, REWORKED PER BOEING SRM 51-10-02.SDR P5CA9700400Skirt · crackedNR 1 PYLON SKIRT CRACKED NUTPLATE STRIP. REPAIRED PER BOEING SRM 51-10-01.SDR NYBA971Support Assy · corrodedSUPPORT ASSY IS CORRODED. SUPPORT REPLACEDSDR RAAA97E8004Angle · crackedDURING SCHEDULED NR 2 CHECK, FOUND NR 1 NACELLE OUTBD SKATE ANGLE CRACKED 1 INCH AT NAC STA 111. REPAIRED PER SRM 54-2-6 FIG 7.SDR DL757962731Bushing · wornDURING ACCOMPLISHMENT OF INSPECTION PER OPN 8201, OUTBOARD MIDSPAR FITTING BUSHING ON THE NR 2 ENGINE WAS FOUND TO HAVE MIGRATED .150 AND WAS LOOSE. THIS ER/A AUTHORIZES REPLACEMENT OF THE BUSHING PER BACO S/B 757-54-0026. DIA OF OUTBOARD LUG PRIOR TO REWORKSDR P5CA9600376Mount Bracket · crackedNR 3 ENGINE CLAMP MOUNTING BRACKET IS CRACKED FOUR INCHES FORWARD OF R-RAIL AT 6 O'CLOCK POSITION. FABRICATED NEW BRACKET AND INSTALLED IAW MM 70-50-00.SDR P5CA9600354Fitting · crackedFOUND NR 4 PYLON FORWARD FAIRING OUTBOARD LATCH 'U' FITTING CRACKED. REMOVED AND REPLACED FORWARD FAIRING RETAINER FITTING IAW SRM 54-10-03 AND MM 54-32-01.SDR DHL96721119Fitting · crackedAT C-CHECK, NR 1 ENG MOUNT SUPPORT FITTING CRACKED AT LOWER I/B CORNER. REMOVED CRACKED MEMBER ON NR 1 ENGINE AFT MOUNT PER BOEING INSTRUCTIONS 32-9430.SDR COMA9610161Fitting · crackedLT NACELLE FLAP HINGE ATTACH FITTING FOUND CRACKED DURING INSPECTION. REPLACED CRACKED FITTING.SDR 9609646623Fitting · crackedDURING P-CHECK, FOUND A .3750 INCH CRACK IN THE NR 3 PYLON STRUT TO DIAGONAL BRACE ATTACH FITTING. REPLACED FITTING.SDR IXXA9652Plank · crackedDURING ROUTINE C-CHECK INSPECTION, THE NR 1 OUTBOARD PYLON REMOVABLE PLANK WAS FOUND CRACKED. THE PLANK WAS REMOVED, REPAIRED, AND REINSTALLED IAW AIRCRAFT SRM 54-2-2 AND SRM 5-1-21. (X)SDR UPS96805986Fitting · brokenWHILE IN FOR C-CHECK, MAINTENANCE REPORTED EO DC8-5710-40-80-E, WING FRONT SPAR PYLON SUPPORT FITTING REPLACEMENT OF NR 2 PYLON. REPAIRED NR 2 PYLON FOOTSTOOL, T-DOUBLER, SKATE ANGLE IAW UPS EO DC8-57-0660.SDR 9603289605Fitting · crackedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE RIGHT PYLON AFT SPAR UPPER FORWARD INBOARD FITTING APPROXIMATELY FS 1038. REPLACED FITTING PER SRM 51-30-25.SDR UPS805064Fitting · crackedWHILE IN FOR D-CHECK, MAINTENANCE FOUND FLANGE ON FITTING CRACKED L/E AT PYLON NR 3. REMOVED, FABRICATED AND INSTALLED FITTING PER UPS SRM 51-1-20D, 51-1-20, 51-1-21 AND DOUG DWG 5754705.SDR 9517696635Fitting · crackedDURING PERIODIC CHECK, FOUND A .375 INCH CRACK IN THE NR 3 PYLON STRUT TO DIAGONAL BRACE ATTACH FITTING. REPLACED FITTING PER EA 5440-01025.SDR DL76L954518Fitting · gougedRT WING I/B MID SPAR STRUT SUPPORT FITTING WAS GOUGED IN THREE PLACES. THE LEADING EDGE OF THE LUG IN THE TRANSITION AREA TO THE WING SKIN ATTACH FLANGE WAS GOUGED APPROX 18 INCHES DEEP ACROSS THE LUG THICKNESS. ALSO, TWO SMALL GOUGES APPROX .15 INCH IN DIAMSDR DL76L954517Fittings · damagedTHE RT PYLON MID SPAR SUPPORT FITTING BUSHINGS WERE FOUND DAMAGED, REQUIRING REPLACEMENT. THE FITTINGS WILL BE REWORKED TO ACCEPT OVERSIZE BUSHINGS, PER DL ERA 272105-14.SDR DL76L954516Fittings · damagedTHE RT PYLON STRUT SUPPORT UPPER LINK FITTING BUSHINGS WERE FOUND DAMAGED, REQUIRING REPLACEMENT. THE FITTINGS WILL BE REWORKED TO ACCEPT OVERSIZE BUSHINGS, PER DL ERA 272106-14.SDR DL76L954511Fitting · damagedTHE RT PYLON STRUT SUPPORT CENTER FITTING BUSHINGS WERE FOUND DAMAGED, REQUIRING REPLACEMENT. THE FITTING WILL BE REWORKED TO ACCEPT OVERSIZE BUSHINGS. DAMAGE FROM LANDING GEAR COLLAPSE REPAIRED PER DL ERA 272109-14.SDR 95UAL900175Fitting · crackedNR 3 ENGINE PYLON FWD MOUNT TRUSS FITTING ASSY, PRIOR TO FURTHER FLIGHT, REPLACE AT LEAST ONE TRUSS FITTING ACCT RT FITTING PREVIOUSLY CRACKED AND REPAIRED. LT FITTING CRACKED AT HORIZ FLANGE INBD BOLT HOLE.SDR ABXA9600139Fitting · crackedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE LEFT ENGINE PYLON INTERIOR FITTING CRACKED AT FS 1038 ABOVE THE ELECTRICAL CONNECTORS. REPLACED FITTING IAW DC-9 SRM 51-30-1 AND 51-30-5.SDR 9514889855Fitting · crackedDURING H-CHECK, FOUND A 1.25 INCH CRACK IN THE RIGHT PYLON FITTING LOCATED FORWARD AND INBOARD OF THE UPPER AFT PYLON STRAP. REPLACED FITTING PER SRM 51-01 PARA 1C AND 51-30.SDR P5CA9500381Hinge · crackedCRACK ON BLOWOUT PANEL HINGE NR PYLON LEFT SIDE. REPLACED HINGE PER BOEING SRM 51-30-02.SDR 95ZZZX3156Fitting · crackedWHILE PERFORMING A C3 CHECK AND THE A.A.C.I.P. SB 3173, FOUND NR 2 AND NR 3 OVERWING FITTING CRACKED FORWARD OF FUSELAGE ATTACHMENT BOLT. INSTALLED NEW TYPE FITTING: NR 1, PYLON AT: ATT 51,029/ATC 20,325, FEB 91. NR 2 AND NR 3, ATT 52,324/ATC 20,629 MAY 9SDR 9510909995Yoke · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN THE FASTENER HOLE FOR THE RIGHT ENGINE YOKE ISOLATOR MOUNT AT THE FORWARD SPAR. REPAIRED YOKE PER EA 99-93566.SDR UPS502977Fuse Pin · crackedWHILE IN 'C' CHECK, MAINTENANCE PERFORMED INSPECTION OF FUSE PIN P/N 311N5217-1 PER SB 757-54A0019R5 ON P AND W AIRCRAFT. FOUND PIN TO BE CRACKED. REPLACED FUSE PIN PER UPS EO B757-5440-0431-H.SDR DLM88951317Angle · crackedFOUND DURING C-2 LETTER CHECK, NR 1 ENG PYLON UPPER SKIN TO FUSELAGE SKIN ATTACH ANGLE WAS FOUND CRACKED .5 INCHES. INSTALLED REPAIR PER SRM 54-04A.SDR DLM88951285Angle · crackedFOUND DURING D-1 LETTER CHECK, .75 INCH CRACK UPPER AFT LT PYLON TO FUSELAGE SKIN ATTACH ANGLE. REPAIRED PER SRM 54-04A.SDR DLL17951539Bushing · wornAT HMV, NR 3 PYLON O/B WING, PYLON MAIN ATTACH I/B BUSHING WAS WORN BEYOND LIMITS. REPAIRED PER SRM 54-11-00. ALSO, O/B WING, PYLON MAIN ATTACH CENTER BEARING IS GOUGED. REPAIRED PER SRM 54-11-00.SDR DLM88951198Angle · crackedFOUND DURING LETTER CHECK, NR 2 PYLON UPPER SKIN TO FUSELAGE ATTACH ANGLE WITH A .75 INCH CRACK. REPAIRED PER SRM 54-04 A FIG 4.
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