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 USAA2010093092146Fuse Pin · corrodedCLT - Q6 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON RIGHT ENGINE INBOARD FUSE PIN. REPLACED RIGHT ENGINE INBOARD FUSE PIN IAW AMM 54-10-01.SDR USAA2010093092145Fuse Pin · corrodedCLT - Q6 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON LEFT ENGINE INBOARD FUSE PIN. REPLACED LEFT ENGINE INBOARD FUSE PIN IAW AMM 54-10-01.SDR USAA2010093092144Fuse Pin · corrodedCLT - Q6 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON LEFT ENGINE OUTBOARD FUSE PIN. REPLACED LEFT ENGINE OUTBOARD FUSE PIN IAW B737 AMM 54-10-01.SDR DALA1021993101Mount · gougedDURING M-CHECK FOUND GOUGE IN AFT MOUNT FITTING OF AFT RT ENGINE PYLON MOUNT ADJACENT TO SAFETY WIRE HOLE FOR INBD ATTACH BOLT. REPAIRED IAW ERA 484250-14 SECTION I, SECTION II REQUIRES MFG APPROVAL OF REPAIR WITHIN 6 MONTHS.SDR DALA1021983101Mount · gougedDURING M-CHECK FOUND GOUGE IN AFT FLANGE OF RT ENGINE PYLON MOUNT INBD SIDE AT FWD BOLT HOLE. REPAIRED IAW ERA 484250-14 SECTION I, SECTION II REQUIRES AIRBUS APPROVAL OF REPAIR WITHIN 6 MONTHS.SDR C2XA10TY121Mount · crackedTYS - A/C CURRENTLY IN A C-CHECK STATUS WHEN INSPECTION FOUND THE NR 2 FWD LOWER YOLK CRACKED. MAINTENANCE REMOVED AND REPLACED THE YOLK IAW EC5450-01028. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.SDR C2XA10TY120Mount · crackedTYS - A/C CURRENTLY IN A C-CHECK STATUS WHEN INSPECTION FOUND THE NR 1 ENGINE LOWER YOLK MOUNT CRACKED. MAINTENANCE REMOVED AND REPLACED THE YOLK IAW EC5440-01028. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.SDR SIMA201024303Yoke · crackedDURING MAINTENANCE BASE VISIT FOUND A CRACK ON THE LEFT FORWARD LOWER PYLON ENGINE YOKE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED FITTING IAW EO EM-54MR-354. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR DALA1019909876Attach Angle · crackedDURING LINE CHECK FOUND CRACK IN LT ENGINE PYLON INSP PANEL 8103 ATTACH ANGLE. REPAIRED IAW SRM 54-01.SDR DALA1019899876Attach Fitting · crackedDURING LINE CHECK FOUND CRACK IN LT PYLON CLOSURE WEB UPPER CLIP INBD SIDE. REPAIRED IAW SRM 54-20-0.SDR DALA1019889876Attach Angle · crackedDURING LINE CHECK FOUND CRACK IN LT PYLON FAIRING SUPPORT RIB ATTACH ANGLE. REPAIRED IAW DWG 9915500.SDR FDEA201008193054Fitting · corrodedE.O. F-5450-7-5003 P4 CODE B, FASTENER ON RT WING I/B SIDE LOAD FITTING , I/B AFT FASTENER HOLE FOUND CORRODED AFTER REAMING TO CALLED OUT OVER SIZE. COMPLIED WITH EA F-5720-139200, MAJOR REPAIR.SDR FDEA201008132993Attach Angle · crackedNR 1 PYLON-TO-ENGINE FWD ATTACH MOUNT, INBD UPPER ATTACH ANGLE IS CRACKED. R & R NR 1 PYLON TO ENGINE FWD ATTACH MOUNT, INBD UPPER ATTACH ANGLE SHEET IAW SRM 51-40-21, PARA 5 AND SRM 51-72-10.SDR FDEA201008112938Attach Angle · crackedNR 1 PYLON-TO-ENGINE FWD ATTACH MOUNT OTBD UPPER ATTACH ANGLE IS CRACKED. REMOVED BLEED AIR DUCT, LOWER NR 1 PYLON TO GAIN ACCESS. R & R NR 1 PYLON OTBD FWD ATTACH MOUNT, UPPER ATTACH ANGLE SHEET IAW SRM 51-40-21. REINSTALLED BLEED AIR VALVE IAW AMM 20-21SDR A6WA201040743Bracket · crackedRT INBD FLAP INBD HINGE MIDDLE INBD FLAP FAIRING BRACKET/ANGLE CRACKED. R & R WITH DUPLICATED PART IAW SRM.SDR FDEA201008042810Attach Angle · crackedNR 2 PYLON; RT SIDE PANEL VERTICAL ATTACH ANGLE FOR ACCESS PANELS 422DR & 424 CR IS CRACKED AT THE UPPER EDGE. REMOVED CRACKED BRACKET AND INSTALLED NEW CRACKED BRACKET PN A5461132150500, PO 688783.1 IAW SRM 51-72-10 PARA 5 AND 6.SDR IPXA10561461Attach Angle · crackedINSPECTION TYPE:C2, NR 2 ENGINE: PANEL 445AR CUTOUT FWD LWR ATTACH ANGLE IS CRACKED. R & R ANGLE IAW SRM 51-40-02-0G.SDR DALA1020250662Fitting · crackedFOUND 1 EA HOLE WITH POSSIBLE CRACK EXTENDING FROM IT INSIDE FUEL TANK. HOLE IDENTIFIED ON LWR R WING PYLON SIDE LOAD FITTING AREA AS A-24 / ACCOMPLISHED ER/A 484133-14AD REV A AT SAA.SDR USAA2010071491418Fastener · shearedCLT - C2 - MAJOR REPAIR - FASTENER SHEARED AT RIGHT PYLON OUTBOARD UPPER VERTICAL FLANGE FOR STRUT TO DIAGONAL BRACE FITTING AT PPS209.5. REPLACED DAMAGED FASTENER IAW EA 102029A.SDR FDEA201007122480Fitting · corrodedNR 2 PYLON PYRAMID FITTING BASE PLATE UPPER SURFACE HAS CORROSION AROUND 4 EA MOUNT HOLES (APPROX 6 SQ IN TOTAL) REMOVED CORROSION FROM NR 2 PYLON PYRAMID FITTING BASE PLATE UPPER SURFACE. AROUND 4 EA HOLES IAW SRM 54-51-81 PAGE 101-102 FIG 104 NDT CHECK C/WSDR USAA2010072291478Pin · corrodedSAL - Q4 - MAJOR REPAIR - REPLACE MID-SPAR FUSE PIN ENG 1 OUTBOARD SIDE DUE CORROSION WAS FOUND. REPLACED MID-SPAR FUSE PIN ENG 1 OUTBOARD SIDE IAW ENGINEERING JOB CARD E5M54001.SDR USAA2010072291477Pin · corrodedSAL - Q4 - MAJOR REPAIR - CORROSION ON OUTBOARD MID-SPAR FUSE PIN AT ENGINE NR 2. REPLACED OUTBOARD MID-SPAR FUSE PIN AT ENGINE NR 2 IAW ENGINEERING JOB CARD E5M54001.SDR USAA2010072291476Pin · corrodedSAL - Q4 - MAJOR REPAIR - CORROSION ON INBOARD MID-SPAR FUSE PIN AT ENGINE NR 2. REPLACED INBOARD MID-SPAR FUSE PIN AT ENGINE NR 2 IAW ENGINEERING JOB CARD E5M54001.SDR USAA2010072291475Pin · corrodedSAL - Q4 - MAJOR REPAIR - CORROSION ON INBOARD MID-SPAR FUSE PIN AT ENGINE NR 1. REPLACED INBOARD MID-SPAR FUSE PIN AT ENGINE NR 1 IAW ENGINEERING JOB CARD E5M54001.SDR IPXA10561096Bracket · crackedINSPECTION TYPE:C4, ENG NR 2 NAC-STRUT STA 203.85 BULKHEAD OTBD LOWER CHORD ANGLE BRACKET IS CRACKED. REPLACED BRACKET IAW SRM 51-40-02-0G, SRM 51-40-05-0G, SRM 54-51-71-1A 1, SRM 51-10-02-0G STEP 8C.SDR IPXA10561220Bracket · crackedINSPECTION TYPE:C2, NR 2 PYLON RT FWD LWR BRACKET IS CRACKED AT NAC STA 205 UNDER PANEL AT 445AR. R & R BRACKET IAW SRM 51-40-05-0G AND SRM 51-40-02-0G.SDR FDEA201006242139Fitting · misalignedNR 2 PYLON MID BULKHEAD FWD RT BOLT HOLE MEASURES 0.4021 UPON REMOVAL OF EXISTING FASTNER. EO F-5450-7-5005 P2 WORK STEP 1.9 CALLS OUT A MAXIMUM REAM OF 0.3901- 0.3911 AND INSTALLATION OF 1/64 OVER SIZE FASTNER. ACCOMPLISHED EA NR F-5450-131189, CLASSIFIESDR FDEA201006242138Fitting · misalignedEO F-5450-7-5003, PT 3, FIG 8, PANEL 3, STEP 4, STATES TO REMOVED CODE I, 0.0374-0.375 IN FASTENER FROM L/E SUPPORT FITTING AREA, INCOMING FASTENER. REMOVED IS 0.437-0.438 IN DIA ACCOMPLISHED EA F-5450-131188, CLASSIFIED AS MAJOR REPAIR.SDR UALA2010062302218Sleeve · crackedNUMBER 1 PYLON AFT ATTACHMENT CENTER FITTING HAS CRACKED SLEEVE. RMV'D CRACK SLEEVE. INSTALLED NEW NR 1 ENG PYLON AFT SHACKLE CENTER PIN ASSY.SDR UALA2010062302221Sleeve · crackedNR 2 ENG PYLON AFT MOUNT LWR INBD SLEEVE CRACKED. REMOVED CRACKED SLEEVE PIN. INSTALLED NEW NR 2 PYLON AFT SHACKLE LWR INBD SLEEVE PIN.SDR UALA2010062302220Sleeve · crackedNR 1 PYLON AFT ATTACHMENT INBD FITTING SLEEVE CRACKED. REMOVED CRACKED SLEEVE. INSTALLED NEW NR 1 ENG PYLON AFT SHACKLE INBD PIN ASSY.SDR V0XR201006150004Bracket · cracked(V0XR) RT NACELLE INBD ATTACHMENT BRACKET IS CRACKED. R & R BRACKET. W/C 4072.SDR V0XR201006150003Attach Bracket · cracked(V0XR) LT NACELLE INBD ATTACHMENT BRACKET IS CRACKED. R & R BRACKET. W/C 4071.SDR AALA20100610AFW01Fitting · crackedCRACK AT THE AFT ENGINE MOUNT BULKHEAD AT MID SPAR FITTING. REPLACED FITTING IN ACCORDANCE WITH ASB 767-54A0101 INCLUDING INSPECTIONS SPECIFIED BY THE ASB.SDR C2XA10SH170Yoke · crackedSHV - DURING C-CHECK THE RT ENGINE FORWARD LOWER YOKE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED YOKE IAW EC 5450-01028. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR DL76L101179Bushing · wornNR 2 PYLON STRUT UPPER SPAR ATTACH FITTING BUSHING REPLACED IAW 54-53-90, FIG 201, REPAIR 2.SDR DL76L101178Bushing · wornNR 2 PYLON STRUT LWR SPAR FITTING ATTACH BUSHING REPLACED IAW SRM 54-53-90 FIG 201, REPAIR 4.SDR DL76L101177Bushing · wornNR 1 PYLON STRUT UPPER SPAR FITTING ATTACH BUSHING REPLACED IAW SRM 54-53-90, FIG 201, REPAIR 2.SDR DL76L101176Bushing · wornNR 1 PYLON STRUT LWR SPAR FITTING ATTACH BUSHING REPLACED IAW SRM 54-53-90 FIG 201, REPAIR 4.SDR WX0A070561Attach Angle · crackedLEFT EXTERNAL FUSELAGE AT CENTER FRAME 1463 PYLON UPPER ATTACH ANGLE CRACKED. TRIMMED OUT DAMAGED AREA, FABRICATED ANGLE REPAIR AND INSTALLED AS PER SRM MD80 54-04.SDR QXEA2010042700286Plate · crackedPDX - MOD - THE MOUNTING PLATE FOR THE INBOARD AFT PORTION OF THE HORSE COLLAR ON THE RT ENGINE MOUNT STRUCTURE IS CRACKED APPROX .5 INCH FROM THE BOTTOM OF THE PLATE. CUT OUT DAMAGED AREA AND FABRICATED REPAIR SPLICE AND SEGMENT PER Q400 RD 8/4-54-289. FABSDR C2XA10SH152Fitting · crackedSHV - DURING C-CHECK NR 2 ENGINE FWD LOWER PYLON FWD YOKE FITTING MOUNT VISUAL INDICATION OF A CRACK. MAINTENANCE REMOVED AND REPLACED NR 2 ENG YOKE FWD LWR FITTING MOUNT IAW EC5450-01028. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA10SH151Fitting · crackedSHV - DURING C-CHECK NR 1 ENGINE FWD LOWER PYLON FWD YOKE FITTING MOUNT VISUAL INDICATION OF CRACK. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE FWD LOWER PYLON FWD YOKE FITTING IAW EC5450-01028. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR USAA2010051390957Fitting · corrodedSAL - S3 - MAJOR REPAIR - CORROSION ON LOWER SPIGOT FITTING AT RIGHT PYLON ENG NR 2. REPLACED LOWER SPIGOT FITTING AT RIGHT PYLON ENG NR 2 IAW A320 SRM 54-51-12.SDR IPXA10159613Attach Fitting · corrodedINSPECTION TYPE:10YR NR 2 PYLON RIB 18 AFT ATTACH FITTING BORE PITTED AND CORRODED. R & R RIB 18 ATTACH FITTING IAW AMM 54-51--75-04.SDR C2XA10SH137Fitting · crackedSHV - DURING C-CHECK NR 2 ENGINE FWD LOWER PYLON FWD YOKE FITTING MOUNT HAS VISUAL INDICATION OF A CRACK. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE YOKE FWD LOWER PYLON FITTING MOUNT IAW EC5450-01028. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR FDEA201004131174Fitting · looseNR 1 PYLON AFT BULKHEAD FITTING 6TH FASTENER FROM THE INBD SIDE UNDER THE CLEVIS IS LOOSE. COMPLIED WITH EA 8-5450-136646; REV "A"; "PYLONS - PYLON STRUCTURE - NR1 PYLON AFT BULKHEAD FASTENERS INSP".SDR FDEA201004121144Fitting · crackedCRACK INDICATION FOUND DURING ULTRASONIC INSP ON SECOND FASTENER HOLE ON LT SIDE PYLON CARRY THROUGH CAP COMMON TO AFT FLANGE OF NR 4 BANJO. REPAIR IAW EA 1-5530-137966 TITLE: "STABILIZERS - VERTICAL STABILIZER - NR 4 BANJO FITTING (REAR SPAR) AND CARRY THSDR QXEA2010041300258Attach Fitting · crackedC-CHECK FWD OTBD CLIP ON THE NACELLE SPINE COWL IS CRACKED. REMOVED CRACKED CLIP, FABRICATED NEW CLIP FROM T1-CP-70 MIL-T-9046 CP-1 0.025". INSTALLED NEW CLIP WITH NEW BOLTS AND SOLID RIVETS. REF RD 8/4-71-032.SDR USAA2010032990673Attach Fitting · corrodedSAL - C6 - MAJOR REPAIR - CORROSION ON LOWER SURFACE OF RIGHT FITTING BASE PLATE ATTACH ENGINE PYLON. REPAIRED LOWER SURFACE OF RIGHT FITTING BASE PLATE ATTACH ENGINE PYLON IAW EA 132934.
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