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 KCSA071468Stiffener · crackedNR 3 PYLON STIFFENER HORIZONTAL FLANGE CRACKED AT NAC STA 132, NAC WL 164.SDR KCSA071456Stiffener · gougedNR 2 PYLON I/B STIFFENER CHORD OF CLOSURE WEB AT NAC STA 272, NAC WL 180 IS GOUGED.SDR KCSA071449Stiffener · wornNR 3 PYLON LOWER SPAR I/B STIFFENER WORN AT PNEUMATIC. DUCT ANTI-ROTATION CLIP BETWEEN NAC STA 180 AND 219.SDR KCSA071448Stiffener · wornNR 3 PYLON LOWER SPAR O/B STIFFENER WORN AT PNEUMATIC. DUCT ANTI-ROTATION CLIP BETWEEN NAC STA 180 AND 219.SDR KCSA071450Stiffener · wornNR 3 PYLON LOWER SPAR I/B STIFFENER WORN AT PNEUMATIC. DUCT ANTI-ROTATION CLIP BETWEEN NAC STA 180 AND 219.SDR WRLA2007105Retainer · damagedDURING C-CHECK, FOUND NR 3 PYLON AFT LOWER FAIRING RETAINER DAMAGE. 10-29-07 ACCOMPLISHED ERA NUMBER 07-54-107. REPLACED NR 3 PYLON AFT LOWER FAIRING RETAINER.SDR ABXR070388Attach Angle · crackedRIGHT LOWER PYLON ATTACH WAS CRACKED AND MISSING MATERIAL AT THE FORWARD OUTBOARD CORNER ATTACH POINT LOCATION FOR PANEL 8212A. REPAIRED AREA IAW ABX DC9 SSRM DGW K05683.SDR KCSA071395Web · crackedNR 2 PYLON NAC STA 202 LOWER WEB IS CRACKED .5 INCH.SDR 07FDEA04261Angle · crackedNR 2 ENG INLET DUCT HOUSING FRAME-TO-VERTICAL STAB LEADING EDGE ATTACH CLIP IS CRACKED. LOCATED ON LT SIDE STA 1233. REMOVED CRACKED ATTACHED BRACKET, FABRICATED NEW ATTACH CLIP AND INSTALLED. REF BOEING DOCUMENT NR 69-14476 AND SRM 51-30-02. CLASSIFIED ASSDR ABXA070325Angle · crackedNR 1 PYLON STRUCTURE CRACKED FORWARD OF CONNECTOR. REPAIRED NR 1 PYLON STRUCTURE FORWARD OF CONNECTOR IAW DC9 SSRM DWG K05159.SDR 07FDEA03594Fitting · chafedDEEP CHAFING MARK FOUND ON PYLON NR 1SPIGOT FITTING FWD PYLON TO ENGINE MOUNT REPAIR PERFORMED BY BLEND OUT TO ELIMINATE SHARP EDGES IAW EA 6-5451-112496 AND RAS 053455/005/2007 ISS A.SDR 07FDEA03593Fitting · chafedDEEP CHAFING MARK FOUND ON PYLON NR 1SPIGOT FITTING FWD PYLON TO ENGINE MOUNT REPAIR PERFORMED BY BLEND OUT TO ELIMINATE SHARP EDGES IAW EA 6-5451-112496 AND RAS 053455/005/2007 ISS A.SDR DHL2007363500Gusset · crackedNR 2 ENG PYLON AT COWL HINGE FITTING O/B SIDE HAS A CRACK APPROX 3/4" ABOVE T BRACKET AT RIB 4. REMOVED AN REPLACED GUSSET HINGE FITTING AN T BRACKET AT NR 2 ENG PYLON O/B SIDE RIB 4 IAW A300 SRM 51-30-30 AN A300 SB A300-54-068.SDR 07FDEA03442Plate · chafedCHAFING DAMAGE (10 BY 1.5 MM) ON PYLON REINFORCING PLATE, RT WING AT FWD OUTBOARD EDGE, RIB 9. REPAIR PERFORMED BY BLEND OUT AND NDT INSPECTION IAW EA 6-5720-95909 AND RAS/BAE/1002261/2006.SDR FDKA200709495Structure · bentTHE METAL LIP ON NR 2 ENGINE NOSE COWL IS BENT/DAMAGED. THE DAMAGED PART WAS REMOVED, FABRICATED AND REPLACED.SDR EIA2007157Stand Off · brokenNR 4 ENGINE NACELLE I/B INSIDE 3RD ACCESS DOOR UPPER ROW, HYD STAND OFF BRACKET IS BROKEN AT BOTTOM WITH FASTENERS PULLED THROUGH WEB FRAME. REMOVED AND REPLACED HYD STAND-OFF BRACKET AND REPLACED WEB WHERE FASTENERS PULLED THROUGH WEB FRAME ON NR 4 ENGINE NASDR ABXA070284Angle · crackedNR 2 PYLON WEB ANGLE ABOVE FORWARD EDGE OF PANEL 8206A INSIDE PYLON CRACKED. REPAIRED ANGLE IAW DC9 SSRM K05159. PO 421513435. INSTALLED WITH HI-LOKS IAW DC9 SRM 51-30-5.SDR COEA0729821Angle · corrodedFOUND DURING HEAVY CHECK, LT NACELLE OUTBOARD SKATE ANGLE CORROSION FORWARD AND AFT AREAS ON PREVIOUS BLENDS. REMOVED CORROSION PER SRAS DO/TS-3852/070-09218, SHEET REF DO/TS 3852/07. (M)SDR COEA0723821Skate Angle · corrodedFOUND DURING HEAVY CHECK. FOUND LEVEL 2 CORROSION, RT NACELLE OB SKATE ANGLE. REMOVED AND REPLACED WITH NEW SKATE ANGLE. (K)SDR 2007UALA03397Skate Angle · damagedNR 1 PYLON AFT SKATE ANGLE CRACKED OUT OF OUTBOARD ATTACH FASTENER AFT OF AFT ENG MOUNT. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED NEW SKATE ANGLE REPAIR.SDR UPS07450578Stiffener · crackedINSPECTION TYPE:C NR 2 PYLON RIGHT UPPER STIFFENER FOUND CRACKED JUST AFT OF FWD ENGINE MOUNT NR 13 HOLE AT INTERNAL ANGLE (1.125 INCH APPROX). NR 2 PYLON AFT OF RIGHT FWD ENGINE MOUNT NR 13 HOLE UPPER STIFFENER REPAIRED AS PER HX RS R54-50-35861 DETAIL VISUASDR KCSA071310Stiffener · crackedNR 2 PYLON LOWER I/B STIFFENER AFT BULKHEAD AT NAC STA 267 HAS 1.5 INCH CRACK.SDR UPS07450579Angle · crackedINSPECTION TYPE:C NR 2 PYLON REAR ENG MOUNT BULKHEAD ATTACHMENT UPPER LINK BEAM AFT SIDE O/B ANGLE CRACKED AS MARKED (CRACK LENGTH .75 INCH). NR 2 PYLON REAR ENG MOUNT BULKHEAD ATTACHMENT UPPER LINK BEAM AFT SIDE O/B ANGLE REPAIRED AS PER SRM 54-14-03 FIG B &SDR UPS07450511Fitting · crackedINSPECTION TYPE:C NR 3 PYLON REAR ENG MOUNT BULKHEAD UPPER LINK BEAM ATTACHMENT BATH FITTING FOUND SUSPECTED CRACK. CRACK LENGTH .3125 INCH. NR 3 PYLON REAR ENG MOUNT BULKHEAD UPPER LINK BEAM ATTACHMENT BATH FITTING REPLACED AND INSTALLED AS PER SRM 51-10-01SDR UPS07450493Fitting · crackedINSPECTION TYPE:C NR 1 PYLON REAR ENGINE MOUNT BULKHEAD UPPER LINK BEAM ATTACHMENT BATH FITTING FOUND CRACKED (CRACK LENGTH .375 INCH). NR 1 PYLON REAR ENGINE MOUNT BULKHEAD UPPER LINK BEAM ATTACHMENT BATH FITTING REPLACED AND INSTALLED AS PER SRM 51-10-01 PGSDR UPS07450492Fitting · crackedINSPECTION TYPE:C NR 4 PYLON REAR ENG MOUNT BULKHEAD UPPER LINK BEAM ATTACHMENT BATH FITTING FOUND CRACKED. CRACK LENGTH .3125 INCH APPROX. NR 4 PYLON REAR ENGINE MOUNT BULKHEAD UPPER LINK BEAM ATTACHMENT BATH FITTING REPLACED AND INSTALLED AS PER SRM 51-10-SDR DL76S071065Fitting · crackedDURING HMV, ONE HOLE IN THE NR 2 PYLON BULKHEAD FITTING COMMON TO THE UPPER SPAR FITTING WAS FOUND CRACKED. CRACK WAS REPAIRED PER INSTRUCTIONS APPROVED BY BOEING.SDR SWAA074031Lug · corrodedDURING SCHEDULED BRDG CHECK, FOUND NR 2 ENGINE STRUT UPPER LINK FORWARD LUG CORRODED. REPAIRED LUG PER SWA EA.SDR KCSA071294Attach Angle · damagedCOMP DUCT ATTACH ANGLE DAMAGE O/B SIDE LOWER SURFACE OF NR 1 PYLON.SDR KCSA071293Attach Angle · damagedCOMP DUCT ATTACH ANGLE DAMAGE I/B SIDE LOWER SURFACE OF NR 1 PYLON.SDR KCSA071289Stiffener · wornNR 2 PYLON I/B LOWER WEB STIFFENER BY MAIN PNEUMATIC DUCT HAS WORN HOLE AT DUCT ATTACHMENT.SDR KCSA071288Stiffener · wornNR 2 PYLON O/B LOWER WEB STIFFENER BY MAIN PNEUMATIC DUCT HAS WORN HOLE AT DUCT ATTACHMENT.SDR USAA070599Angle · crackedNR 2 PYLON AFT I/B ANGLE CRACKED. INSTALLED FABRICATED REPAIR PART PER SRM 51-10-02; 51-20-01, BOEING DWG 65-26300-29, DEFECT SIZE: 2 INCHES.SDR CALA0700359Fitting · crackedINSPECTION FOUND A 1 INCH CRACK IN NR 2 ENGINE PYLON AFT HORSE COLLAR (FITTING). THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-10-02 AND 51-40-02.SDR EIA2007145Closeout Panel · gougedNR 3 PYLON INBOARD DOOR 473AL RING IS GOUGED INSIDE. REPAIRED NR 3 PYLON INBD ACCESS DOOR CUT OUT FOR ACCESS PANEL 473AL PER ECRA 488-54-018-2 PART 1.SDR FDKA200706317Bracket · crackedTHE LT PRE-COOLER FORWARD MOUNT ANGLE IS CRACKED AT THE TOP RIVET. REMOVED AND REPLACED DAMAGED PART.SDR UPS07550238Fairing · debondedINSPECTION TYPE:C NR 2 PYLON AFT FAIRING INBD AND OUTBD SKIN FORWARD END UPPER CORNER DISBONDED AND WORN SURFACE (PANEL RACK). REPAIRS ACCOMPLISHED PER FINAL EA NR 757-5451-27-A1704 AND UPS FILE NUMBER 757-54-20083, REPAIR WAS IDENTIFIED PER STEP NR 11 OF FINSDR UPS07650197Fitting · misinstalledINSPECTION TYPE:SIP LEFT PYLON AFT PITCH LOAD FITTING HAS SHORT EDGE MARGIN. FABBED RADIUS FILLER FROM 7075-T7351. LOCATED, DRILLED & REAMED TO FINAL SIZE. VERIFIED RADIUS FILLER LIES FLAT AS BACKUP FITTING. ALODINED & PRIMED RADIUS FILLER PER ER 07-2696. SDR DL76S070775Nut Clip · unknownDURING ACCOMPLISHMENT OF EA 01-074906-03AD, NEED TEE CLIPS ARE ATTACHED TO THE SUBJECT PITCH LOAD FITTINGS, HOWEVER THEY HAD SHORT EDGE MARGIN. BACO GAVE AMOC APPROVAL FOR THE SHORT EDGE MARGIN CONDITION. REFERENCE ER/A 461700-14AD.SDR CALA0700308Fitting · crackedINSPECTION FOUND A .5 INCH CRACK IN NR 2 PYLON AFT HORSE COLLAR (FITTING) AT LOWER I/B NUT PLATE, FORWARD OF NR 6 FLAP TRACK. A NEW FITTING WAS INSTALLED IAW SRM 51-40-02.SDR 07FDEA02136Web · wornON PYLON, NR 3 DEEP WEAR ON UPPER SURFACE OF HORIZONTAL WEB AT STA YN 200. REPAIRED IAW SRM 54-20-00 FIG 5.SDR 2007UALA01932Bushing · migratedLEFT PYLON INBOARD MIDSPAR FITTING, INBOARD LUG BUSHING MIGRATED. [08-08-07] REMOVED AND REPLACED BUSHINGS PER SRM 54-53-90, REPAIR 3.SDR 2007UALA01931Bushing · migratedRIGHT PYLON STRUT OUTBOARD MIDSPAR FITTING, OUTBOARDD LUG BUSHING MIGRATED. [08-08-07] REMOVED AND REPLACED BUSHINGS PER SRM 54-53-90, REPAIR 3. MID-SPAR FITTING OK FOR SERVICE.SDR 2007UALA01930Bushing · migratedRIGHT PYLON STRUT, INBOARD MIDSPAR FITTING, INBOARD LUG BUSHING MIGRATED. [08-08-07] REMOVED AND REPLACED BUSHINGS PER SRM 54-53-90, REPAIR 3. AIRCRAFT OK FOR RETURN TO SERVICE.SDR 2007UALA01929Bushing · migratedRIGHT STRUT, DIAGONAL BRACE ATTACH FITTING, INBOARD BUSHING MIGRATED. [08-08-07] REPLACED BUSHINGS PER MM 54-53-90, REPAIR 4. AIRCRAFT OK FOR RETURN TO SERVICE.SDR DU4R2007134Brace · out of limitsFOUND NR 1 DIAGONAL BRACE ID 2.003 OUT OF LIMITS. REPAIRED OVERSIZED LUG ON NR 1 DIAGONAL BRACE BY HONING, FABRICATING AND INSTALLING BUSHINGS IAW DELTA ERA 461664-14AD DATED 6/7/07 APPROVED BY FAA FORM 8100-9 WITH AMOC TO PARAGRAPH (A) OF AD 2003-18-05.SDR DU4R2007135Brace · out of limitsFOUND NR 2 DIAGONAL BRACE ID 2.003 (OUT OF LIMITS). REPAIRED OVERSIZED LUG ON NR 2 DIAGONAL BRACE BY HONING, FABRICATING AND INSTALLING BUSHINGS IAW DELTA ERA 461664-14AD DATED 6/7/07 APPROVED BY FAA FORM 8100-9 WITH AMOC TO PARAGRAPH (A) OF AD 2003-18-05.SDR 2007UALA01892Shim · migratedNR 2 PYLON LOWER AFT SPAR FITTING FOR THE DIAGONAL BRACE HAS SHIM MIGRATION. [08-08-07] REMOVED 4 EACH FASTENERS AT AFT LOWER SPAR FITTING PER SRM 51-40-02. NO GAP OR FURTHER SHIM MIGRATION NOTED. INSTALLED NEW FASTENERS PER MM 54-51-95 AND SEALED AREA. SDR DL757070698Brace · damagedDURING CURRENT HMV, THE NR 1 PYLON DIAGONAL BRACE REQUIRED OVERSIZING BEYOND THE EA LIMITS. AS SUCH, BOEING WAS CONTACTED FOR APPROVAL TO OVERSIZE BEYOND LIMITS DUE TO AD 2003-18-05, AND THE WORK IS DOCUMENTED IN ERA 461664-14AD.SDR 2007UALA01874Bushing · migratedNR 2 ENG, UPPER LINK INBOARD BUSHING MIGRATED AT FWD POINT. [08-07-07] REPLACED BUSHING DURING C-CHECK NR 12 VISIT. ALSO INSTALLED 2 EA REPAIR WASHERS. AIRCRAFT OK FOR RETURN TO SERVICE.
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