JASC 5420
Service difficulty reports · 3,949
Reports filed under 5420 · Nacelle/Pylon Miscellaneous Structure, 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 = '5420' 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 = '5420' 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 ASAA0440065Bushing · wornGYR - NR 2 PYLON LOWER SPAR FITTING INBOARD BUSHING MIGRATED. REMOVED AND REPLACED LOWER SPAR FITTING BUSHINGS. (M)SDR 04FDEA00541Support · missingNR 2 ENG CORE COWL FWD LT AND RT HINGE LINK/ROD SUPPORT FOUND MISSING. ALSO FOUND CRACKS AT LT AND RT VERTICAL STIFFENERS AT HINGE FITTING CUTOUTS FOR LINK ATTACHMENT. REPLACED LINK ASSY AND WELDED CRACKS. SUSPECT CRACKS CAUSED DUE TO MISSING ROD.SDR SWIA200413037Frame · crackedDISCOVERED DURING C-CHECK INSPECTION, RIGHT PYLON UPPER ACCESS PANEL 422AB STIFFENER FRAME CRACKED. REPLACED STIFFENER IAW SHORTS CMM 20-40-11, 20-42-06, 20-27-11 & 20-27-11.SDR SWIA200413036Fairing · crackedDISCOVERED DURING C-CHECK INSPECTION, RIGHT PYLON LOWER STANG FAIRING 444BB CRACKED ON INBOARD SIDE. REPAIRED DAMAGE IAW SHORTS CMM 78-30-00, SRS 049.SDR ABXA040080Angle · crackedLEFT PYLON UPPER ATTACH ANGLE WAS CRACKED AT STA 1019. REPAIRED AREA IAW DC-9 SRM 54-04.SDR 6521Beam · crackedDURING VISUAL INSPECTION OF BOTH LT AND RT NACELLE STRUCTURES, CRACKS WERE OBSERVED ON BOTH NACELLE, AFT BEAMS ON THE TOP AND AFT, OB AREAS. FOLLOWING EVALUATION OF THIS STRUCTURE BY THIS INSPECTION CREW AND A LOCAL DER, IT WAS DETERMINED THAT REPAIR OF THIS SSDR 04047637Web · crackedDURING INSPECTION THE RIGHT HAND ENGINE SUPPORT BEAM LOWER OUTBOARD WEB WAS FOUND CRACKED. THE BEAM WAS TEMPORARILY REPAIRED IN ACCORDANCE WITH MANUFACTURERS DATA. AIRCRAFT WAS RETURNED TO SERVICE UPON COMPLETION OF INSPECTION.SDR SWIA200412981Clip · crackedRIGHT WING OUTBOARD OF NACELLE 1ST FUEL PANEL OUTBOARD MIDDLE LOWER CLIP CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED SHEAR TIE RIGHT WING (MIDDLE LOWER). NO LEAKS NOTED.SDR CALA0400082Attach Angle · crackedINSPECTION FOUND A .5 INCH CRACK IN ATTACH ANGLE I/B OF NR 2 PYLON JUST AFT OF MIDSPAR ATTACH BOLT. REPAIRED ANGLE IAW SRM 51-70-12.SDR ASAA0440019Housing · wornNR 1 ENGINE PYLON SPHERICAL BEARING OUTER RACE IS LOOSE IN HOUSING UPPER SPAR ATTACHMENT FITTING FOR UPPER LINK. REMOVED AND REPLACED NR 1 ENGINE PYLON SPHERICAL BEARING, PYLON CROWN BEAM, IAW ASA EA 5440-01011, TYPICAL REPAIR. (M)SDR QXEA200400115Clip · crackedPDX - UPPER FORWARD INBOARD NACELLE CENTER STRUCTURE ATTACHMENT CLIP CRACKED AT LEFT HAND NACELLE. REPAIRED IAW HORIZON AIR EA 6-54-283.SDR QXEA200400114Clip · crackedPDX - UPPER FORWARD INBOARD NACELLE CENTER STRUCTURE ATTACH CLIP CRACKED ON RIGHT HAND NACELLE. REPAIRED IAW HORIZON AIR EA 6-54-283.SDR QXEA200400113Clip · crackedPDX - UPPER FORWARD OUTBOARD NACELLE CENTER STRUCTURE ATTACH CLIP CRACKED ON RIGHT HAND NACELLE. REPAIRED IAW HORIZON AIR EA 6-54-283.SDR DHL2004745011Seal · looseNR 3 DETECTOR CIRCUIT GROUND LIGHT ILLUMINATED IN FLIGHT, THIS IS A REPEAT ITEM. DEFERRED NR 3 FIRE WARNING GROUND FAULT DETECTOR PER MEL 29-9-1, DMI 15580, PLACARDS INSTALLED. REF. DMI 15580 (NR 3 DETECTOR CIRCUIT GROUND LIGHT ILLUMINATED IN FLIGHT). OPENESDR SWIA200412975Bracket · crackedINTERIOR BRACKET CRACKED AT LEFT NACELLE OUTBOARD OF WHEEL WELL SUPPORT. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED IAW SRM 54-10-03 FIG 201. P/N 120-41419-001.SDR UPS04441811Web · crackedINSPECTION TYPE: C, NR 2 PYLON - LWR WEB CRACKED THRU AFT RT LONGITUDINAL STIFFENER APPROX 15 INCHES FWD OF AFT MOUNT, CRACK RUNS LATERALLY. LWR SPAR WEB 5 LOCATIONS CRACK END BY STOP HOLE PRILLED AS PER SRM 54-10-03 FIG 2. NDT INSP NIL CRACKS AND PERFORMED SDR ASAA0410021Structure · chafedOKC - DURING SCHEDULED D-CHECK, FOUND THE NR 2 ENGINE PYLON AT FAIRING STATIONS 40 AND 62 CHAFED. REPAIRED PYLON PER EA. (M)SDR QXEA200400010Clip · crackedPDX - NR 1 NACELLE THE LEFT HAND FORWARD SPINE COWL CLIP IS CRACKED ON FORWARD LEG OF CLIP BY BOLT HEAD. REPAIRED IAW HORIZON AIR EA 6-54-282 AND SRM 51-42-65.SDR C2XA04SH004Stiffener · chafedSHV- DURING C-CHECK THE NUMBER 2 ENGINE LOWER COWLING AFT STIFFENER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STIFFENER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASAA0340354Support · gougedGYR - DURING SI CHECK, FOUND NR 2 ENGINE PYLON OUTBOARD FAN COWL SUPPORT INBOARD AND OUTBOARD CHORD GOUGED. REPAIRED IAW EA. (M)SDR F3LA200300159Web · crackedDURING C-CHECK, INSPECTION REPORTED NR 2 ENGINE PYLON LOWER AFT STRUT FAIRING WEB CRACKED AND PULLED FASTENERS AT STIFFENER. REPLACED WEB ON NR 2 ENGINE PYLON LOWER AFT STRUT FAIRING PER SRM 51-40-02 AND EA B3-54R-10217.SDR ABXA030467Stiffener · crackedNR 1 PYLON INTERNAL UPPER HORIZONTAL STIFFENER CRACKED ON INBOARD END, ABOVE FUEL LINE SHROUD. REPAIRED AREA NOTED IAW DC-9 SSRM K05159 AND DC-9 SRM 51-30-5.SDR QXEA200301491Bracket · chafedPDX- LT NACELLE WHEEL WELL TOP OB GRAVEL GUARD BRACKET IS CHAFED. REPAIRED IAW DHC-8 SRM 51-20-11 AND 51-40-11.SDR QXEA200301490Bracket · chafedPDX- LT NACELLE WHEEL WELL BOTTOM OB GRAVEL GUARD BRACKET IS CHAFED. REPAIRED IAW DHC-8 SRM 51-20-11 AND 51-40-11.SDR CALA0300657Web · crackedINSPECTION FOUND A 3 INCH CRACK IN WEB AT NR 1 PYLON STRUT. REPAIRED IAW ECRA 5421-01002.SDR CALA0300656Strap · crackedINSPECTION FOUND A 6 INCH CRACK IN O/B STRAP ON NR 1 PYLON AT STA 363.5. INSTALLED SPLICE STRAPS IAW ECRA 5421-01002.SDR CALA0300655Strap · crackedINSPECTION FOUND A 6 INCH CRACK IN I/B STRAP ON NR 1 PYLON AT STA 363.5. REPAIRED IAW ECRA 5421-01002.SDR DHL2003802536Angle · crackedNR 4 PYLON UPPER PART ANGLE CRACKED 0.500, STA YN 188.000. REMOVED CRACKED ANGLE IAW SRM 51-1-20D PG 21. FABRICATED NEW ANGLE IAW SRM 54-2-0 PG 1. PERFORMED HEAT TREATMENT TO ANGLE IAW SRM 51-1-4 PG 1-3, SRM 51-1-1 PG 1-13, 17. CLEANED, TREATED AND PRIMED SDR SWIA200312678Channel · crackedLEFT ENGINE AFT OUTBOARD SUPPORT CHANNEL FOR AFT EXHAUST FAIRING CRACKED. STOP-DRILLED CRACK LEFT ENGINE AFT OUTBOARD SUPPORT CHANNEL. FABRICATED AND INSTALLED REPAIR DOUBLER PER EMB120 SRM 51-40-02, 51-70-04.SDR ASAA0340342Support · gougedGYR - DURING SI CHECK FOUND SUPPORT CHORD GOUGED ON NR 2 PYLON AT NAC 166.5 TO 196. REPAIRED IAW EA. (M)SDR QXEA200301362Angle · chafedSEALING ANGLE FOR LOWER COWL ABOVE OIL COOLER IS CHAFED ON INBOARD ANGLE SIDE. REPAIRED IAW DHC-8 RD 8-54-967.SDR 03FDEA01802Fitting · corrodedBFM CLOSER NR S 10 COMPLY WITH EA NR 6-5450-73844 PYLONS/NACELLES-NR 1 ENGINE PYLON FWD MOUNT CORROSION REPAIR. FACT 25OCT03 16:43 BFM U COMPLIED WITH EA NR 6-5450-73844- PYLONS/NACELLES - NR 1ENGINE PYLON FWD MOUNT CORROSION REPAIR. CLOSED ON 10/25/SDR QXEA200301365Structure · chafedPDX- LEFT HAND NACELLE GRAVEL GUARD LOWER ATTACHMENT POINTS HAVE CHAFE MARKS ON AFT WALL OF NACELLE. REPAIRED IAW DHC-8 SRM 51-20-11, 51-20-16, 51-20-36 AND 51-20-41.SDR EIA2003131Web · crackedNR 1 PYLON LOWER WEB CRACKED AT NAC STA 210 LT SIDE AFT OF STIFFER FOR PNEU. DUCT. STOP DRILLED CRACK AND FABBED AND INSTALLED REPAIR PLATE AND FILLERS IAW B747 SRM 54-10-03 FIG 2SDR F3LA200300152Support · crackedDURING C-5 CHECK, INSPECTION REPORTED ATTACH ANGLE CRACKED AT LOWER AFT END OF NR 1 PYLON. REPLACED DAMAGED SUPPORT IAW SRM 51-40-02.SDR SWIA200312579Bracket · crackedRIGHT HYD BAY CROSS BRACKET CRACKED AT INBOARD SIDE OUT OF LIMITS. DISCOVERED DURING C-CHECK. REMOVED AND REPLACED RIGHT HYD BAY CROSS BRACKET IAW SRM 51-10-02 & 51-40-00.SDR AWXA200301324Angle · crackedDURING C-17 CHECK A .5 INCH CRACK WAS FOUND ON NR 1 PYLON OUTBOARD ACCESS COVER ATTACH ANGLE, NAC STA 279.50. MAINTENANCE REMOVED CRACKED ATTACH ANGLE AT NAC STA 279.50, DURING REMOVAL FOUND SPLICE PLATE ATTACHED TO ANGLE WORN BEYOND LIMITS, REMOVED SPLICE PLSDR CALA0300593Channel · crackedINSPECTION FOUND A 1INCH CRACK IN LT PYLON RT SIDE VERTICAL CHANNEL THAT FORWARD END PANEL NR 5843R AND AFT END OF PANEL NR 5842R ATTACHES TO. A NEW SPLICE PLATE WAS INSTALLED IAW SRM 51-40-02.SDR C2XA03SH378Stiffener · chafedDURING C-CHECK THE INBOARD STIFFENER OF THE LEFT ENGINE COWLING WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR AWXA200301113Angle · crackedMCN - MAJOR REPAIR - DURING C-07 CHECK A CRACK WAS FOUND ON THE LEFT PYLON PANEL ATTACH ANGLE. (PROFILE). MAINTENANCE CUTOUT AFFECTED AREA, FABRICATED A REPAIR PARTS, SPLICE AND FILLER. IAW A320 SRM 54-52-12 PAGE 215-220 FIG.203 SHEET 1 AND 2.SDR AWXA200301114Fairing · corrodedDURING C-07 CHECK CORROSION WAS FOUND ON IB SIDE OF AFT PYLON FIXED FAIRING AT RIB 11 TO RIB 16. MAINTENANCE REMOVED AND REPLACED AFT FAIRING FIXED SKIN AT RT PYLON RIB 11-16 IAW A320 SRM 51-42-11 FIG. 8 PAGES 21 AND 22 AND SRM 54-54-11 FIG.1 PAGES 1-3 AND 51-SDR C2XA03SH347Stiffener · chafedDURING C CHECK MAINTENANCE FOUND THE NR 2 ENGINE UPPER COWLING AFT STIFFENER TO BE CHAFED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA03SH346Stiffener · chafedDURING C CHECK THE NR 2 ENGINE LOWER COWLING AFT STIFFENER WAS FOUND TO BE CHAFED ALONG THE ENTIRE RADIUS. MAINTENANCE REMOVED THE DAMAGED AFT STIFFENER AND REPLACED IT WITH A NEW AFT STIFFENER IAW WITH EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETUSDR SWIA200312445Structure · crackedLT ENGINE NACELLE DECK CRACKED BY ENGINE DRIVEN HYD LINE. (DISCOVERED DURING E005 INSPECTION) REPAIRED LEFT ENGINE NACELLE DECK CRACK IAW IC 2003-120/3178 2A AND SRM 51-40-00.SDR AWXA200301178Support Angle · crackedLCQ - MINOR REPAIR - DURING C-09 CHECK A .625 INCH CRACK WAS FOUND ON NR 1 ENGINE PYLON FORWARD OUTBOARD SUPPORT ANGLE. MAINTENANCE REMOVED CRACKED FORWARD OUTBOARD SUPPORT ANGLE; FABRICATED A NEW REPLACEMENT SUPPORT ANGLE PER DWG 311N5002; INSTALLED REPAIR PSDR 2003UALA00700Stiffener · crackedNR 3 PYLON AFT BULKHEAD STIFFENER CRACKED. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED STIFFENER.SDR C2XA03SH324Stiffener · gougedDURING C CHECK THE NUMBER 2 LOWER COWLING AFT STIFFENER WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STIFFENER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA03SH323Stiffener · chafedDURING C CHECK THE NUMBER 1 ENGINE LOWER COWLING AFT STIFFENER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STIFFENER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR AWXA200301046Clip · crackedDURING C-16 CHECK A .1250 CRACK WAS FOUND IN RADIUS OF NR 1 ENGINE LT FIXED FAIRING CLIP AT AFT END, 1ST RIB. MAINTENANCE REMOVED CRACKED CLIP ON NR 1 ENGINE LT FIXED FAIRING AFT END, 1ST RIB; FABRICATED A NEW REPLACEMENT CLIP IAW DWG 65-52263; INSTALLED REPAISDR ARWA20030905Angle · crackedDURING (A) CHECK INSPECTION THE FOLLOWING WAS FOUND; NR 2 PYLON STUB WING BELOW LT SPAR CAP (Z) ANGLE WITH CRACK.
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