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 IPXA10561564Channel · chafedINSPECTION TYPE:C2, NAC-STRUT NR1 STA 203.85 INBD SIDE VERTICAL CHANNEL HAS EXTERIOR SURFACE CHAFED. R & R NAC STRUT INBD SIDE VENT CHANNEL.SDR IPXA10561537Splice · chafedINSPECTION TYPE:C2, CHAFING ON NR 2 PYLON STRUCTURE AT UPPER INBD CORNER OF AFT MATING SURFACE FOR NR 2 PYLON FAIRING NR 441AT REMOVED, FABRICATED AND REPLACED IAW SRM 51-40-02, SRM51-40-08.SDR WGFY2010FA0751004Stiffener · crackedPYLON NR2 STRAP STA 250 BETWEEN STIFFENER NR 2 & STIFFENER NR 3 WAS CRACKED.SDR WGFY2010FA0751003Stiffener · crackedPYLON NR 2 STIFFENER NR 3 AND STRAP, STA 248 WAS CRACKED.SDR WGFY2010FA0751002Strap · crackedPYLON NR1, STA 248.00 STRAP WAS CRACKED.SDR WGFY2010FA0751001Stiffener · crackedPYLON NR 1 STIFFENER NR3, STA 243 & 248 WAS CRACKED.SDR IPXA10561462Angle · crackedINSPECTION TYPE:C2, NR1 ENGINE PYLON: CUTOUT FOR PANEL 435AR FWD LOWER CORNER ANGLE IS CRACKED. R & R WITH NEW PART IAW SRM 51-40-02-0G.SDR IPXA10561443Striker · wornINSPECTION TYPE:C2, 1 ENGINE PYLON: CUTOUT FOR PANEL 435AL FWD LATCH STRIKER PLATE IS WORN ON FRONT AND BACK SIDE. R & R STRIKER LATCH IAW SRM 51-40-02-0G AND AMM 54-53-02-5.SDR FDEA201007132506Support · crackedNR2 PYLON UPPER RT SIDE PANEL SUPPORT STRUCTURE VERTICAL BRACKET FOUND CRACKED AT PP STN 185. R & R IAW SRM 51-40-02, REV 100. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR DALA1020190662Support Fitting · damagedWHILE ACCOMPLISHING EA 06-070332-03, AD REV J, SPOTFACE DEPTH FOR HOLES MARKED 3 AND 4 ON NEW SUPPORT FITTING PN 012N8888-1 WAS EXCEEDED TO ATTAIN 100 PERCENT SPOTFACE.SDR USAA2010081391662Pin · corrodedCLT - Q1 - MAJOR REPAIR - RIGHT OUTBOARD FUSE PIN IS CORRODED ON HEAD AT NAC STA 276.6, WL132.15. REPLACED RIGHT O/B FUSE PIN IAW EO 5410-01012.SDR USAA2010081391661Pin · corrodedCLT - Q1 - MAJOR REPAIR - RIGHT INBOARD FUSE PIN IS CORRODED UNDER HEAD OF PIN AT NAC STA 276.6, WL132.15. REPLACED RIGHT INBOARD FUSE PIN IAW EO 5410-01012.SDR IPXA10M61222Angle · crackedINSPECTION TYPE:3C, NR3 PYLON UPPER ANGLE ON VERTICAL WEB IS CRACK ABOVE PRECOOLER. REMOVED ANGLE, FABRICATED AND INSTALLED ANGLE IAW DWB AUB7564.SDR IPXA10561265Channel · chafedINSPECTION TYPE:C2, PANEL 445BL IS CHAFED ON INNER SURFACE. R & R INNER SURFACE CHANNEL IAW SRM51-40-02-0G.SDR VGQY2010062300038Stiffener · wornNR 3 PYLON - ADP LT MOUNT BUSHING MISSING. COMPLIED WITH EN 1101-10, REPAIR FOR NR 3 PYLON NAC STA 365.51 BULKHEAD STIFFENER 65B90413-42 ELONGATED HOLE.SDR FDEA201006292222Plate · crackedFOUND 2 EA BOLTS SHEARED AT NR 1 ENG PYLON AT LOWER TOMBSTONE FITTING. R & R LOWER PLUG PLATE, NUT RETAINER AND BOLTS ON THE NR1 ENG. LOWER TOMBSTONE FITTING IAW AMM 54-00-01-4.SDR NSVA2010107Structure · damagedPERFORMED PERMANENT REPAIR FOR ELONGATED HOLE ON THE LT NACELLE OUTBOARD SIDE APPROXIMATELY AT STA 203 USING TD 340-54-10-09.SDR CA100628003Channel · crackedCHANNEL P/N 109-910045-28 CRACKED AT BEND RADIUS. CRACK NON-CRITICAL JUST CONTRIBUTES TO GRADUAL DEGRADATION OF THE COWL ASSY. PART REPLACED WITH NEW SAME P/N.SDR QXEA2010062800367Structure · crackedMOD - FRONT OTBD SPINE COWL CLIP ON LT ENGINE NACELLE IS CRACKED. R & R CRACKED CLIP REF RD 8/4-71-0032 PERMANENT REPAIR.SDR R61A20100273Stiffener · corrodedWHILE AC WAS IN FOR HEAVY CHECK, LEVEL TWO CORROSION WAS FOUND UNDER RT NUMBER THREE PYLON ENGINE HEAT SHIELD ON THE INTERNAL STIFFENERS. MAINTENANCE REMOVED AND REPLACED THE CORRODED INTERNAL STIFFENERS (P/N 170-39583-001 AND 170-39583-002) PER THE EMB SRM. SDR WRLA20100621395Web · crackedWHILE IN ATL DURING A-5 CHECK A SPECIAL INSPECTION (SI) WAS PERFORMED ON THE NR 3 PYLON AND THE UPPER WEB WAS FOUND CRACKED AT THE CORNER OF THE GENERATOR FEEDER CABLE PASS THROUGH CUTOUT LOCATED AT YUS 338. FOUND BY ATLANTA INSPECTOR. PERMANENT REPAIR MADE SDR WRLA20100615405Fitting · chafedCHAFING - FOUND PYLON-4 MID SPAR UNDER WING FITTING BUSHING OUTSIDE AROUND CHAFING (LT FITTING RT SIDE, RT FITTING RT SIDE). ACCOMPLISHED PYLON 4 MID SPAR UNDER WING FITTING REPAIRED REFERENCE JOB CARD ATTACHING SHEET 025857, 025858. CONDITION CHECK SATISFACSDR VGQY2010061400033Fairing · crackedPYLON NR 2 PYLON AFT FAIRING AFT OF AFT STRUT AFT LWR SIDE WITH CRACK. 01 EACH CRACK FOUND ON OUTER SKIN OF NACELLE NR 2 FIXED FAIRING ASSY P/N 65B90813-67 AT AFT LOWER EDGE HOLE. NO SPECIFIC SRM REPAIR AVAILABLE. COMPLIED WITH EN 1098-10 (REPAIR FOR 01 CRSDR C2XA10TY087Mount Flange · corrodedNR 1 ENG INLET MOUNTING FLANGE HOLES CORRODED. REPAIRED INLET HOLES IAW EC5420-01158. AIRCRAFT CURRENTLY IN C CHECK.SDR VGQY2010060900028Fitting · corrodedCORROSION / NR 4PYLON / UNDERWING DUAL SIDE BRACE FITTING / BORE. COMPLIED WITH SB 747-54A2218 FIGURE 9. REMOVED AND REPLACED 2 EACH BEARING AS PER BOEING SOPM 20-50-03 REV 90.SDR VGQY2010060900027Bearing · corrodedCORROSION NR 1 PYLON / UNDERWING DUAL SIDE BRACE FITTING/BORE. COMPLIED WITH SB 747-54A2218 FIGURE 9. REMOVED AND REPLACED 2 EACH BEARING AS PER SOPM 20-50-03 REV 90.SDR FDEA201006081866Ferrule · crackedNR 2 PYLON FERRULE HAS CRACKS AT FWD OTBD LOCATION AND HAS PREVIOUS REPAIRS ON IT. REPAIRED NR 2 PYLON FERRULE IAW EA6-548-135179 (NR 2 PYLON PRECOOLER DUCT FERRULE) AND SB 54-2028 NACELLES/PYLONS.SDR FDEA201006081865Ferrule · crackedNR 1 PYLON HAS A CRACKED FERRULE AT THE FWD INBD CORNER. REPAIRED NR1 PYLON FERRULE IAW EA6-548-135179, (NR1 PYLON PRECOOLER DUCT FERRULE) AND SB 54-2028, NACELLES / PYLONS.SDR WRLA20100607393Stiffener · wornNR 1 ENG RT CORE COWL HAS ANGLE WEAR NEAR SUPPORT ROD END. REMOVED DAMAGE PARTS AND FABRICATE NEW PARTS IAW EI W2010P548-1283 REV 00. RE-INSTALLED NEW PARTS IAW SRM 51-40-02 REV 76. JOB COMPLETED AND CONDITION CHECK NORMAL.SDR USAA2010062491259Fitting · corrodedSAL - S4 - MAJOR REPAIR - CORROSION ON BALL JOINT OF SPIGOT RIGHT PYLON. REPLACED BALL JOINT OF SPIGOT RIGHT PYLON IAW A319 AMM 54-51-41.SDR A6WA201040567Retainer · crackedSEAT RETAINER CRACKED ON PANEL 412AT. RETAINER REPAIRED IAW SRM 54-00-00, CRACK APPROX .030" IN LENGTH.SDR A6WA201040564Retainer · crackedRT PYLON 422BT SEAL RETAINER IS CRACKED. R & R SEAL RETAINER IAW AMM 54-63-01 IAW SRM 51-42-06. R & R.SDR WRLA20100601403Bearing · wornWORN - FOUND PYLON -4 DIAGONAL BRACE FWD FITTING BEARING WORN. PER SRM 54-50-90 REPAIR 1 REV 76 REPAIRED PYLON -4 LOWER SPAR FITTING BEARING.SDR WRLA20100601402Bushing · corrodedCORROSION - FOUND PYLON -4 DIAGONAL BRACE AFT BUSHING CORROSION. PER OHM 54-00-01 REV 54, REPLACED DIAGONAL BRACE AFT BUSHING OF PYLON-4.SDR WRLA20100601400Bearing · wornWORN - FOUND PYLON -4 UPPER LINK AFT SIDE BEARING WORN. PER CMM 54-00-01 REV 54, REPLACED UPPER LINK AFT SIDE BEARING OF PYLON-4.SDR FDEA201006011753Fitting · crackedDURING ACCOPLISHMENT OF EO F-5450-7-5006 PT1, AT NR 1 ENGINE PYLON FOUND 1 EA HOLE CRACK ON BULKHEAD FITTING HORIZ FLANGE LOWER FWD OTBD. NR 1 ENG PYLON BULKHEAD HOLE REPAIR CARRIED OUT IAW EA NR F-5450-135851 (LT PYLON AFT BULKHEAD FITTING CRACK REPAIR). RESDR A6WA201040491Strip · chafedLT UPPER NOSE COWL AFT EDGE STRIP IS CHAFED. R & R STRIP ON LT ENGINE UPPER NOSE COWL AFT EDGE IAW BOM CMM 71-14-01.SDR A6WA201040373Angle · crackedCRACK ON ANGLE ON PANEL 422AT, BLENDED OUT CRACK ON PANEL 422AT IAW SRM 51-12-00.SDR 2010FA0000494Stiffener · crackedSUPPLEMENTAL INFORMATION:PYLON NR 1 STIFFENER NR 3 BEWEEN NAC STA.234-259 WAS CRACK +/- 25MMSDR A6WA201040495Retainer · crackedPANEL 422BT CRACKED SEAL RETAINER. REMOVED DAMAGED SEAL AND SEAL RETAINER AND INSTALLED NEW SERVICEABLE SEAL AND SEAL RETAINER IAW AMM 54-63-01 AND 51-41-02.SDR 2010FA0000485Stiffener · crackedPYLON NR 1 STIFFENER NR 3 BETWEEN NAC STA .234-259 WAS CRACK +/- 25MMSDR 2010FA0000478Stiffener · crackedPYLON NR 2 STIFFENER NR 3 CRACKSDR 2010FA0000477Stiffener · crackedPYLON NR 1 STIFFENER LOWER FLANGE NO.3 CRACK AT NAC. STA.256SDR IPXA10559984Brace · crackedINSPECTION TYPE: MOD, NR 1 PYLON AFT UNDERWING FAIRING STRUCTURE LT FWD BRACE IS CRACKED. R & R BRACE IAW SRM 51-40-02-0G.SDR A6WA201040356Separator · chafedDIVIDERS ON PANEL 422DB HAS CHAFING CONDITION. R & R 2 EA DIVIDER PANELS IAW SRM.SDR A6WA201040358Separator · chafedDIVIDER PLATES ARE KNIFE EDGED AND CHAFED, R & R DIVIDER PLATES PN 601R37138-27 AND 601R37138-25 IAW SRM 51-42-06, 51-42-13 AND 51-40-11.SDR SIMA201013405Fitting · crackedDURING MAINTENANCE BASE VISIT FOUND THE LEFT YOKE FORWARD SPAR LOWER LINKAGE FITTING CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED SERVICEABLE LEFT YOKE FORWARD SPAR LOWER LINKAGE FITTING IAW EO EM-54MR-338. THE AIRCRAFT WAS RETURNED SDR AALA20100512TUL06Angle · crackedTOP AFT END OF PYLON HAS CRACK IN ANGLE AT AFT END. INSTALLED ATTACH ANGLE DOUBLER PER AARD 54-20-00-1.SDR UALA2010051101595Web · crackedNR 1 PYLON INTERNAL MID TORQUE BOX UPPER WEB IS CRACKED AT LEFT DRAIN HOLE. MAJOR REPAIR ACCOMPLISHED. STOP DRILLED 2 EACH CRACKS AND FABRICATED A REPAIR DOUBLER AND FILLERS AND INSTALLED PER SRM.SDR FDEA201005101502Vane · crackedNR 2 ENGINE RT NACELLE STRUT ACCESS PANEL NR 443CR, AFT MOST (2) VANES LOWER PORTION CRACKED. REPAIR ON NR2 ENGING RT NACELLE STRUT ACCESS PANEL NR 443CR CARRIED OUT IAW NR F-5450-138560. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.
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