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.

SDR KCSA071468Stiffener · crackedNR 3 PYLON STIFFENER HORIZONTAL FLANGE CRACKED AT NAC STA 132, NAC WL 164.Oct 14, 2007 · N707CK · Boeing 747246FSDR KCSA071456Stiffener · gougedNR 2 PYLON I/B STIFFENER CHORD OF CLOSURE WEB AT NAC STA 272, NAC WL 180 IS GOUGED.Oct 9, 2007 · N713CK · Boeing 7472B4BSDR KCSA071449Stiffener · wornNR 3 PYLON LOWER SPAR I/B STIFFENER WORN AT PNEUMATIC. DUCT ANTI-ROTATION CLIP BETWEEN NAC STA 180 AND 219.Oct 7, 2007 · N713CK · Boeing 7472B4BSDR KCSA071448Stiffener · wornNR 3 PYLON LOWER SPAR O/B STIFFENER WORN AT PNEUMATIC. DUCT ANTI-ROTATION CLIP BETWEEN NAC STA 180 AND 219.Oct 7, 2007 · N713CK · Boeing 7472B4BSDR KCSA071450Stiffener · wornNR 3 PYLON LOWER SPAR I/B STIFFENER WORN AT PNEUMATIC. DUCT ANTI-ROTATION CLIP BETWEEN NAC STA 180 AND 219.Oct 7, 2007 · N713CK · Boeing 7472B4BSDR 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.Oct 4, 2007 · N273WA · Doug MD11SDR 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.Oct 2, 2007 · N784TW · Doug DC915SDR KCSA071395Web · crackedNR 2 PYLON NAC STA 202 LOWER WEB IS CRACKED .5 INCH.Sep 24, 2007 · N713CK · Boeing 7472B4BSDR 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 ASSep 24, 2007 · N489FE · Boeing 727227SDR ABXA070325Angle · crackedNR 1 PYLON STRUCTURE CRACKED FORWARD OF CONNECTOR. REPAIRED NR 1 PYLON STRUCTURE FORWARD OF CONNECTOR IAW DC9 SSRM DWG K05159.Sep 22, 2007 · N967AX · Doug DC941SDR 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.Sep 12, 2007 · N733FD · Airbus A300B4605RSDR 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.Sep 12, 2007 · N733FD · Airbus A300B4605RSDR 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.Sep 8, 2007 · N363DH · Airbus A300B4203SDR 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.Sep 7, 2007 · N808FD · Airbus A310324SDR FDKA200709495Structure · bentTHE METAL LIP ON NR 2 ENGINE NOSE COWL IS BENT/DAMAGED. THE DAMAGED PART WAS REMOVED, FABRICATED AND REPLACED.Sep 5, 2007 · N856MJ · Emb EMB145LRSDR 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 NASep 5, 2007 · N486EV · Boeing 747212BSDR 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.Aug 30, 2007 · N960AX · Doug DC941SDR 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)Aug 24, 2007 · N821FX · Aerosp ATR72202SDR COEA0723821Skate Angle · corrodedFOUND DURING HEAVY CHECK. FOUND LEVEL 2 CORROSION, RT NACELLE OB SKATE ANGLE. REMOVED AND REPLACED WITH NEW SKATE ANGLE. (K)Aug 24, 2007 · N821FX · Aerosp ATR72202SDR 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.Aug 23, 2007 · N531UA · Boeing 757222SDR 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 VISUAAug 17, 2007 · N521UP · Boeing 747200SDR KCSA071310Stiffener · crackedNR 2 PYLON LOWER I/B STIFFENER AFT BULKHEAD AT NAC STA 267 HAS 1.5 INCH CRACK.Aug 16, 2007 · N709CK · Boeing 747132SDR 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 &Aug 14, 2007 · N521UP · Boeing 747200SDR 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 51-10-01Aug 14, 2007 · N521UP · Boeing 747200SDR 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 PGAug 14, 2007 · N521UP · Boeing 747200SDR 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-Aug 14, 2007 · N521UP · Boeing 747200SDR 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.Aug 13, 2007 · N129DL · Boeing 767332SDR SWAA074031Lug · corrodedDURING SCHEDULED BRDG CHECK, FOUND NR 2 ENGINE STRUT UPPER LINK FORWARD LUG CORRODED. REPAIRED LUG PER SWA EA.Aug 13, 2007 · N364SW · Boeing 7373H4SDR KCSA071294Attach Angle · damagedCOMP DUCT ATTACH ANGLE DAMAGE O/B SIDE LOWER SURFACE OF NR 1 PYLON.Aug 10, 2007 · N710CK · Boeing 7472B4BSDR KCSA071293Attach Angle · damagedCOMP DUCT ATTACH ANGLE DAMAGE I/B SIDE LOWER SURFACE OF NR 1 PYLON.Aug 10, 2007 · N710CK · Boeing 7472B4BSDR KCSA071289Stiffener · wornNR 2 PYLON I/B LOWER WEB STIFFENER BY MAIN PNEUMATIC DUCT HAS WORN HOLE AT DUCT ATTACHMENT.Aug 9, 2007 · N710CK · Boeing 7472B4BSDR KCSA071288Stiffener · wornNR 2 PYLON O/B LOWER WEB STIFFENER BY MAIN PNEUMATIC DUCT HAS WORN HOLE AT DUCT ATTACHMENT.Aug 9, 2007 · N710CK · Boeing 7472B4BSDR 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.Aug 7, 2007 · N425US · Boeing 737401SDR 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.Jul 15, 2007 · N69311 · Boeing 7373T0SDR 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.Jul 13, 2007 · N488EV · Boeing 747230BSDR FDKA200706317Bracket · crackedTHE LT PRE-COOLER FORWARD MOUNT ANGLE IS CRACKED AT THE TOP RIVET. REMOVED AND REPLACED DAMAGED PART.Jun 29, 2007 · N826MJ · Emb EMB145LRSDR 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 FINJun 29, 2007 · N402UP · Boeing 75724APFSDR 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. Jun 27, 2007 · N309UP · Boeing 76734AFSDR 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.Jun 22, 2007 · N127DL · Boeing 767332SDR 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.Jun 16, 2007 · N12313 · Boeing 7373T0SDR 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.Jun 15, 2007 · N387FE · Doug DC1010SDR 2007UALA01932Bushing · migratedLEFT PYLON INBOARD MIDSPAR FITTING, INBOARD LUG BUSHING MIGRATED. [08-08-07] REMOVED AND REPLACED BUSHINGS PER SRM 54-53-90, REPAIR 3.Jun 11, 2007 · N648UA · Boeing 767322SDR 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.Jun 11, 2007 · N648UA · Boeing 767322SDR 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.Jun 11, 2007 · N648UA · Boeing 767322SDR 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.Jun 11, 2007 · N648UA · Boeing 767322SDR 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.Jun 8, 2007 · N640DL · Boeing 757232SDR 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.Jun 8, 2007 · N640DL · Boeing 757232SDR 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. Jun 7, 2007 · N648UA · Boeing 767322SDR 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.Jun 7, 2007 · N640DL · Boeing 757232SDR 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.Jun 6, 2007 · N648UA · Boeing 767322
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