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 SIMA201105203Fitting · crackedDURING MAINTENANCE BASE VISIT FOUND THE LEFT ENGINE FORWARD LOWER YOKE FITTING CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT ENGINE FORWARD YOKE FITTING IAW AEA EO-EM-54MR-382. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR DALA1114929878Angle · crackedNR 1 PYLON LE PANEL UPPER ATTACH ANGLE REPAIR CRACKED REMOVED CRACKED ANGLE REPAIR IAW SRM 51-30-2. FABRICATED NEW ANGLE REPAIR IAW SRM 54-04 FIGURE 10. LOCATED AND DRILLED IAW SRM 51-10-4. PRIMED IAW SRM 51-10-3. INSTALLED NEW REPAIR ANGLE IAW SRM 51-30-2SDR FDEA201102170596Mount · corrodedNR 2 ENGINE PYLON FWD MOUNT MATING SURFACE FOUND WITH CORROSION. CORROSION REMOVED AS PER SRM 51-74-10 REV 74 AND FOUND EXCEEDED LIMITS PER SRM 54-51-81 FIGURE 104 REV 74. MATERIAL ORIGINAL THICKNESS = 0.780", MATERIAL REMOVED = 0.018", MATERIAL REMAINING SDR IPXA1564978Attach Bracket · corrodedINSPECTION TYPE:C3, ATTACH BRACKET FOR PANEL NR 442AL IS GOUGED AND CORRODED ON OTBD SURFACE, NR 2 PYLON 1" AFT OF CUTOUT FOR PANEL 443CL. REMOVED, FABRICATED AND INSTALLED IAW SRM 51-40-02-0G, AND DWG NR 313N3100.SDR C2XA11SH044Yoke · crackedSHV - DURING C-CHECK LT FORWARD LOWER ENGINE YOKE CRACKED. REMOVED AND REPLACED LT FWD LOWER ENGINE YOKE IAW EC5450-01028. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR IPXA1564950Fitting · corrodedINSPECTION TYPE:MOD, NR 1 PYLON MID SPAR FITTING ON THE ACFT INBD SURFACE AROUND THE BUSHING IS PITTED AND WORN. REPAIRED FITTING IAW EO B757-5440-41606-A, DATED 24 FEB 2011 AND ATS ER 11-01495, DATED 23 FEB 11.SDR IPXA1564949Fitting · gougedINSPECTION TYPE:MOD, NR 1 PYLON INBD MID SPAR FITTING ON ACFT INBD AND OTBD SURFACE AROUND THE BUSHING ARE WORN AND GOUGED. REPAIRED FITTING IAW EO B757-5440-41606-A AND ER 11-01495.SDR USAA2011020890579Pin · corrodedSAL - MAJOR REPAIR - S5 CHECK - CORROSION ON BOTH ATTACH PINS FOR THE PYLON TO WING ATTACH FITTINGS BETWEEN WS 6465 AND WS 7063, BETWEEN RIB 3 AND RIB 5. REPLACED BOTH ATTACH PINS FOR THE PYLON TO WING ATTACH FITTINGS BETWEEN WS 6465 AND WS 7063, BETWEEN RIB SDR DALA1108139857Attach Angle · crackedNR 2 PYLON REAR SPAR WEB ATTACH ANGLE CRACKED. REMOVED ATTACH ANGLE IAW SRM 51-30-5 AND ORIG MATERIAL .040 TITANIUM IAW SRM DWG 9915500, REV K, FABRICATED ATTACH ANGLE IAW DWG 9915500. INSTALLED ATTACH ANGLE IAW DWG 9915500.SDR FDEA201101300419Fitting · gougedNACELLE STRUT NR 2 AFT BULKHEAD STA 201.02 INBD AND OUTBD LOWER SIDES SURFACE HAS A GOUGE. REPAIR DISPOSITION WAS REJECTED. REFERENCE "REWORK" NON-ROUTINE N01498. W/O 00049340, FOR CORRECTIVE ACTIONS.SDR FDEA201101300420Fitting · chafed(997FD/ 473AC) LT PYLON REAR BULKHEAD, LT LOWER CORNER IS CHAFED. COMPLIED WITH EA F-5450-146255: NACELLES/PYLONS-AD2003-18-05, EO F-5450-7-5010, NR 1 ENGINE STRUT AFT BULKHEAD REPAIR USING PARTS FABRICATED. REPAIR IS CLASSIFIED AS A CAT. "A" MAJOR.SDR SIMA201103103Fitting · crackedDURING THE MAINTENACE BASE VISIT FOUND THE RIGHT FORWARD LOWER PYLON YOKE INNER LUG FITTING CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLIED WITH EO EM-54MR-380 FOR REPAIRS. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR E4GR6002Fitting · crackedRT FWD LOWER PYLON YOKE FITTING CRACKED IN THE UPPER FWD RADIUS.SDR E4GRFitting · crackedLT PYLON FWD LOWER YOKE FITTING CRACKED IN UPPER FWD RADIUS.SDR DALA1105479864Attach Angle · crackedNR 2 ENG PYLON FWD LOWER ATTACH ANGLE FOR PANEL 8220NW HAS APPROX 1 IN CRACK AT FWD END. REMOVED & FABRICATED NEW ANGLE IAW SRM 54-04, FIG 10 PRIMED IAW SRM 51-10-3 INSTALLED IAW SRM 51-30-5 & 54-04 FIG 10 & 51-30-2. REQUIRED INSP COMPLETED.SDR A6WA201140046Attach Fitting · wornFWD AND AFT DIVIDER CLIP ARE DAMAGED ON PANEL 422BT. R & R WITH NEW FWD AND AFT DIVIDER CLIPS.SDR A6WA201140047Attach Fitting · worn100 PERCENT MATERIAL LOSS WORN ALL THE WAY THROUGH FWD DIVIDER CLIP ON PANEL 412BF. DAMAGE R & R WITH NEW CLIP.SDR USAA2010123093276Attach Fitting · corrodedSAL - MAJOR REPAIR - S5 CHECK - CORROSION ON THE RIGHT WING TO PYLON AFT ATTACH FITTING AT RIB 10. REPLACED THE RIGHT WING TO PYLON AFT ATTACH FITTING AT RIB 10 IAW TASK CARD 26C40054026.SDR USAA2010122293219Attach Fitting · corrodedBFM - S2 - MAJOR REPAIR - CORROSION ON RIGHT PYLON WING TO ATTACH FITTING ON OUTBOARD SIDE WHERE LOWER ATTACH BOLT INSTALLS AT RIB 12. REMOVED CORROSION ON RIGHT PYLON WING TO ATTACH FITTING. FOUND TO BE WITHIN LIMITS IAW EA 134330A.SDR USAA2011011090156Fitting · corrodedSAL - S5 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON LEFT PYLON SPIGOT FITTING BORE BETWEEN LEFT PYLON STA 6465 TO STA063. REPLACED LEFT PYLON SPIGOT FITTING BETWEEN LEFT PYLON STA 6465 TO STA 063 IAW A320 SRM 54-51-12.SDR EE4Y100562Fitting · cracked(EE4Y) ENGINE NR1, PYLON BOX STA 648 RIB09 FITTING WITH CRACK. NOTE: THE FITTING'S CRACK REQUIRES A MAJOR REPAIR.SDR USAA2010121793173Fuse Pin · corrodedMCN - MAJOR REPAIR - C20 CHECK - CORROSION ON NR 1 PYLON FUSE PIN AT NAC STATION 257.25. REPLACED NR 1 PYLON FUSE PIN AT NAC STATION 257.25.SDR USAA2010121793172Fuse Pin · corrodedMCN - MAJOR REPAIR - C20 CHECK - CORROSION ON NR 2 PYLON FUSE PIN AT NAC STATION 257.25. REPLACED NR 2 PYLON FUSE PIN AT NAC STATION 257.25.SDR USAA2010120992938Sleeve · corrodedBFM - S2 - MAJOR REPAIR - FRETTING CORROSION ON RIGHT PYLON RIB 12 PYLON TO RIB ATTACH FITTING OUTBOARD LOWER ATTACH SLEEVE UNDER HEAD FLANGE AT WS 6261. REPLACED RIGHT PYLON RIB 12 PYLON TO RIB ATTACH FITTING OUTBOARD LOWER ATTACH SLEEVE UNDER HEAD FLANGE ATSDR USAA2010122893262Pin · corrodedBFM - MAJOR REPAIR -S2 CHECK - LEVEL 2 GALVANIC CORROSION ON LT PYLON TOP SLEEVE (PIN) OF PYLON TO WING ATTACH FITTING. REPLACED LT PYLON TOP SLEEVE (PIN) OF PYLON TO WING ATTACH FITTING IAW A330 AMM 54-51-17.SDR FDEA201011284504Bracket · crackedNR1 ENG OTBD FAN COWL UPPER HINGE HEAT SHIELD COVERS 4 EA FOUND WITH CRACKS. CRACKED NR1 ENGINE OTBD FAN COWL UPPER HINGE REPAIRED IAW EA F-7110-142348 (NR1 AND NR2 ENGINE FAN COWLING SHIELD HINGE BRACKET WELDING REPAIR). REPAIR IS CLASSIFIED AS MINOR IAWSDR DALA1101470659Fitting · damagedWHILE PERFORMING EA 06-074338-03, REV B, FOUND 1 EA INCOMING OVERSIZED HOLE ON NR 2 PYLON SPAR FITTING, NAC STA 127 LT SIDE. ACCOMPLISHED ERA 480632-14, REV ORIGINAL ON N/R CARD 183023.SDR DALA1101019855Attach Fitting · crackedPYLON REAR SPAR AFT MOUNT UPPER ATTACH FITTING CLIP CRACKED AT BOLT. REMOVED CRACKED CLIP IAW SRM 51-30-5. FABRICATED CLIP IAW DWG 9915500. INSTALLED NEW CLIP IAW SRM 51-30-5.SDR DALA1032049853Attach Angle · crackedDURING M-CHECK FOUND NR 2 ENGINE PYLON LOWER ATTACH ANGLE APPROX STA 1136 CRACKED. STOP DRILLED CRACK .25 AT EACH END IAW SRM 54-04, FIG 10, SHEET 2, HFEC INSPECTED STOP DRILL AREA IAW SPM 06-10-01.001 CRACK FOUND TO BE CONTAINED A2700 MAT ID FOR REPAIR ANGLE SDR C2XA10TY169Yoke · crackedNR 2 PYLON FWD YOKE LOWER FITTING CRACKED. REMOVED AND REPLACED LOWER FORWARD YOKE IAW EC5450-01028.SDR USAA2010110992567Fitting · corrodedSAL - S5 - MAJOR REPAIR - PITTING MARKS ON NR 2 ENGINE PYLON SPIGOT BALL JOINT AREA INSIDE BORE. REPLACED NR 2 ENGINE PYLON LOWER SPIGOT FITTING IAW A320 SRM 54-51-12 & EA 133144.SDR C2XA10SH372Fitting · crackedSHV - DURING C-CHECK NR 1 ENGINE FORWARD LOWER YOKE FORWARD FLANGE CRACKED. MAINTENANCE REMOVED AND REPLACED NR1 ENGINE FORWARD LOWER YOKE FITTING IAW EC5450-01028. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR USAA2010111092586Fitting · corrodedSAL - S5 - MAJOR REPAIR - PITTING MARKS ON NR 1 ENGINE PYLON SPIGOT BALL JOINT AREA INSIDE OF BORE. REPLACED NR 1 ENGINE PYLON LOWER SPIGOT FITTING IAW A320 SRM 54-51-12 & EA 133144.SDR USAA2010110592526Shear Tie · brokenMCN - C2 - MAJOR REPAIR - SHEAR TIE BROKEN ON NR 1 ENGINE STRUT TO SKIRT BEAM ASSEMBLY ON INBOARD SIDE AT NAC STA 240. REPLACED SHEAR TIE ON NR 1 ENGINE STRUT TO SKIRT BEAM ASSEMBLY ON INBOARD SIDE AT NAC STA 240 IAW B767 SRM 51-40-02.SDR USAA2010110392474Shear Tie · brokenMCN - C2 - MAJOR REPAIR - BROKEN SHEAR TIE AT NR 2 ENGINE PYLON STRUT TO SKIRT BEAM ASSEMBLY ON INBOARD SIDE AT NAC STA 240. REPLACED SHEAR TIE AT NR 2 ENGINE PYLON STRUT TO SKIRT BEAM ASSEMBLY ON INBOARD SIDE AT NAC STA 240 IAW B767 SRM 51-40-02.SDR QXEA2010101800644Attach Fitting · crackedRT NACELLE INBD REAR SPAR ATTACH FITTING, HAS 2 SUSPECTED CRACKS. PERFORMED A FPI INSP AND CONFIRMED 2 CRACKS. UPPER ONE IS APPROX .5" LONG AND LOWER ONE IS APPROX .6875" LONG. REPLACED RT NACELLE INBD REAR SPAR ATTACH FITTING IAW TC SB84-54-15.SDR USAA2010102192333Pin · corrodedBFM - MAJOR REPAIR - S2 - LEVEL 2 CORROSION ON PIN FLANGE AT NR 2 PYLON RIGHT INBOARD OF FORWARD PYLON TO WING ATTACH FITTING, RIB 12. REPLACED PIN FLANGE AT NR 2 PYLON RIGHT INBOARD OF FORWARD PYLON TO WING ATTACH FITTING, RIB 12 IAW A330 AMM 54-51-17.SDR DALA1025729886Attach Angle · crackedDURING M-CHECK FOUND CRACK IN PYLON CORNER ATTACH ANGLE UNDER PANEL 8205A AT AFT OTBD CORNER. REPAIRED IAW SRM 51-30-2, SRM 54-10-0 & SRM 51-10-4.SDR IPXA10563157Bracket · crackedINSPECTION TYPE:C4, NR 1 ENG LT COOLING AIR MANIFOLD INLET SUPPORT BRACKET CRACKED. R & R BRACKET IAW EM 72-52-03-300-003, REPAIR 003, FRS 5530.SDR USAA2010100192171Fuse Pin · corrodedCLT - RON - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON RIGHT OUTBOARD MID SPAR FUSE PIN. REPLACED RIGHT OUTBOARD MID SPAR FUSE PIN IAW B737 AMM 54-10-01.SDR FDEA201009303833Bracket · crackedRIGHT ENGINE RT FAN COWL PANEL TOP HINGE NR 4 SHIELD CRACKED A RADIUS. CRACKED TOP HINGE NR 4 SHIELD ON RIGHT ENGINE FAN COWL REPAIRED AS PER EA F-7110- 139358 (NR 1 AND NR 2 ENGINE FAN COWLING SHIELD HINGE BRACKET WELDING REPAIR). REPAIR IS CLASSIFIED AS MSDR FDEA201009303832Bracket · crackedRIGHT ENGINE RT FAN COWL PANEL TOP HINGE NR 3 SHIELD CRACKED AT RADIUS. RIGHT ENGINE CRACKED RT FAN COWL PANEL TOP HINGE NR 3 SHIELD REPAIRED AS PER EA F- 7110-139358 : NR 1 AND NR 2 ENGINE FAN COWLING SHIELD HINGE BRACKET WELDING REPAIR. REPAIR IS CLASSIFIESDR FDEA201009303831Bracket · crackedRIGHT ENGINE RT FAN COWL PANEL TOP HINGE NR 2 SHIELD CRACKED AT RADIUS. RT ENGINE RT FAN COWL TOP HINGE NR 2 SHIELD CRACK REPAIRED AS PER EA F-7110- 139358 : NR 1 AND NR 2 ENGINE FAN COWLING SHIELD HINGE BRACKET WELDING REPAIR). REPAIR IS CLASSIFIED AS MINOSDR FDEA201009303830Bracket · crackedRIGHT ENGINE RT FAN COWL PANEL TOP HINGE NR 1 SHIELD CRACKED AT RADIUS. CRACKED RIGHT ENGINE RT FAN COWL TOP NR 1 HINGE SHIELD REPAIRED AS PER EA F-7110-139358 (NR 1 AND NR 2 ENGINE FAN COWLING SHIELD HINGE BRACKET WELDING REPAIR). REPAIR IS CLASSIFIED AS MISDR USAA2010100192170Fuse Pin · corrodedCLT - RON - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON NR 1 ENGINE OUTBOARD FUSE PIN AT NAC STA 278, NAC WL 132. REPLACED NR 1 ENGINE OUTBOARD FUSE PIN AT NAC STA 278, NAC WL 132 IAW ENGINEERING CARD E5M54001 REV 2.SDR USAA2010092892134Fuse Pin · corrodedCLT - PYLON INSPECTION - MAJOR REPAIR - CORROSION ON LEFT OUTBOARD MID SPAR FUSE PIN. REPLACED LEFT OUTBOARD MID SPAR FUSE PIN IAW B737 AMM 54-10-01.SDR USAA2010092792108Fuse Pin · corrodedCLT - PYLON INSPECTION - MAJOR REPAIR - CORROSION ON HEAD OF LEFT INBOARD MIDSPAR FUSE PIN. REPLACED LEFT INBOARD MIDSPAR FUSE PIN IAW B737 AMM 54-10-01.SDR FDEA201009233662Fitting · misinstalledNR 1 PYLON AFT BULKHEAD FITTING HAS 12 EA FASTENERS ALONG THE UPPER FLANGE SPINNING. ACCOMPLISHED EA 8-5450-123559.SDR UALA2010092303536Attach Fitting · crackedNR 2 PYLON OTBD RIB 5 ATTACHING PLATE CRACKED. MAJOR REPAIR ACCOMPLISHED: REPLACED ATTACH ANGLE ON NR D4149Y AND INSPECTED BY LC38.SDR USAA2010093092147Fuse Pin · corrodedCLT - Q6 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON RIGHT ENGINE OUTBOARD FUSE PIN. REPLACED RIGHT ENGINE OUTBOARD FUSE PIN IAW AMM 54-10-01.
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