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 A6WA201240390Angle · chafedANGLE ON L/E PANEL NR 421AL CHAFED. REMOVED ANGLE & INSTALLED SERVICEABLE ANGLE IAW SRM 51-42-06.SDR UALA2012022101064Heat Shield · looseLEFT NACELLE HEATSHIELD FOUND FOUR LOOSE FASTENERS WITH SEVEN BLIND FASTENERS INSTALLED. REMOVED AFT FAIRING FWD SECTIONS FOR SEAL REPLACEMENT REF MM. REMOVED NR 1 PAN CASTING FWD SEAL.SDR UALA2012022001006Web · crackedNR 2 PYLON FWD UPPER SPAR DRAIN WEB AT NAC STA 175.5 COMMON TO FUEL TUBE CUTOUT IS CRACKED AT NUT PLATE HOLE. TRIMMED OUT DAMAGE & ACP NDT FOR CRACKS, NONE FOUND. FABRICATED AND INSTALLED DOUBLER REPAIR PER EA PD67-54-020 & ECRA 5453-01048.SDR FDEA201202190617Stiffener · gougedNR 1 PYLON PANEL 413 CL HAS .50" GOUGE AT MILLED STIFFENER. COMPLIED WITH EA 6-5480-156100 NACELLES/ PYLONS INSTALLED REPAIR DOUBLER IAW SRM 54-52-51, FIG 202, SHEET 1, PGS 209-210.SDR FDEA201202190616Stiffener · crackedNR 2 ENGINE ANTI-ICE NOSE COWL DUCT TIE ROD SUPPORT BRACKET HAS 2 EA ELONGATED HOLES. COMPLIED WITH EA 6-5450-156097 NACELLES/PYLONS. REPAIRED NR 2 CANTILEVER BEAM AT RIB A7. R & R STIFFENER AT RIB A7 IAW SRM 51-72-10SDR AALA20120217013Web · crackedLEFT PYLON FORWARD UPPER WEB CRACKED. INSTALLED DOUBLER PER AARD 54-52-01-1.SDR UALA2012021500928Heat Shield · wornFOUND NR 1 HEAT SHIELD GAP COVER WORN INTO HEAT SHIELD I/B EDGE AND NR 2 GAP COVER O/B EDGE WORN INTO HEAT SHIELD. REPLACED HEAT SHIELD ASSY.SDR DALA1208459236Fastener · looseCW EA 02-476701-12AD INSPECTED PYLON SUPPORT FITTING FOR LOOSE OR MISSING FASTENERS. REMOVED & REPLACED FASTENERS IN ROW A PER OPN 0301 NR 1 PYLON.SDR DALA1208469236Fastener · looseCW PYLON SUPPORT FITTING FASTENER INSPECTION FOR LOOSE, DAMAGE OR MISSING FASTENERS CONDITION PER EA02-476701-12AD.SDR USAA2012021500020Pin · wornS2 CHECK - WORN 2 EA SLEEVE PINS ON NR 2 OUTBOARD PYLON AT RIB 12. REPLACED 2 EA SLEEVE PINS ON NR 2 OUTBOARD PYLON AT RIB 12 AT INBOARD & OUTBOARD WING TO PYLON FITTINGS IAW A330 MM 54-51-17.SDR HNAA2012021000571Angle · corrodedINBD NACELLE TO FORWARD SPAR CLOSING ANGLE IS CORRODED ON NR 1 NACELLE. REMOVED INBD CLOSING ANGLE, FABRACATED INBD SIDEWALL ANGLE IAW DWG 85710414. INSTALLED INBD SIDEWALL ANGLE IAW DWG 85710413.SDR DALA1207020139Fitting · defectiveNR 2 PYLON UPPER LINK PITCH LOAD FITTING T-CLIPS 112T7010-14 O/B AND 112T7010-16 I/B HAVE SHORT EDGE MARGIN AT FASTENER HOLES (NRC 52406).SDR DALA1207010139Fitting · defectiveNR 1 PYLON UPPER LINK PITCH LOAD FITTING T-CLIPS 112T7010-13 O/B AND 112T7010-15 I/B HAVE SHORT EDGE MARGIN (NRC 52405).SDR UALA2012020900787Sleeve · crackedNR 2 ENGINE, LT SIDE TRANSLATING SLEEVE HAS 2 INCH LONG CRACK ACCOMPANIED BY DELAMINATION MEASURING 1 INCH WIDE BY 2 INCHES, 8 O'CLOCK POSITION, 2 FOOT AFT. ACCOMPLISHED INTERIM REPAIR PER SRM, PARA F.(1).(B). REMOVED MOISTURE AND SEALED AREA WITH SPEED TAPESDR DALA1206830139Bushing · migratedNR 1 PYLON LWR AFT FITTING BUSHING MIGRATED AND REPAIRED PER B767-300 SRM 54-51-90 REPAIR 4 FIG 201.SDR A6WA201240345Seal · chafedRT LOWER NOSE COWL HAS CHAFED T/E SEAL. R & R RT NOSE COWL T/E SEAL IAW CMM 71-14-01, SRS 091.SDR ABXA20120207204Flange · chafedNR 1 PYLON PNL 437ELX LWR ATTACH FLANGE INSIDE PYLON STRUCTURE CHAFED THROUGH. REMOVED AND REPLACED ATTACH FLANGE IAW B767-200 SRM 51-40-02 & B. DWG #311T1380. #3 FITTING TO BE INSTALLED ON NR 0961.SDR EE4Y201202070014Strap · wornNR 2 ENGINE, NOSE COWLING, CAPPING STRAP WITH WORN AT 11 O`CLOCK. THE CAPPING STRAP WAS REPAIRED IAW SRM VRS2792 NR 030 PROCEDURE.SDR DALA1209440139Fastener · missingNR 1 PYLON HAS FASTENER MISSING. FASTENER INSTALLED ACCOMPLISHED AS PER VA81913AD REV A.SDR ABXR2012020400026Access Panel · crackedDURING INSPECTION, FOUND NR 2 PYLON ACCESS PANEL 446 BL CRACKED AROUND NUT PLATES. REPAIRED IAW REA B564-59630 AND SRM.SDR ABXR2012020400020Channel · crackedDURING INSPECTION, FOUND LT AND RT CHANNELS CRACKED ON T/E OF NR 2 PYLON. REPAIRED IAW SRM.SDR UALA2012020300677Seal · damagedNR 1 ENG NR 1 HEAT SHIELD REMOVED AND FOUND RT CORNER SEAL DAMAGE. REPLACED SEAL AND INSTALLED HEAT SHIELD REF AVO 1123.SDR DALA1205631603Panel · wornNR 1 PYLON PNL 436CL (1EA) AFT BOLT HOLE WORN AT AFT UPPER AREA.SDR DALA1205550674Fitting · damagedNR 2 PYLON FWD SPAR TENSION CLIP P/N 012N8886-2 HOLE NR 1 JOB CARD 06-070332-03 0228 PANEL 2 STEP 6 REQUIRES SPOTFACE .8125 HOLE HAS MINIMUM EDGE DISTANCE. ITEM ADDRESSED ON N/R 43117 AND ER/A 489934-14.SDR EE4Y201202010003Channel · crackedNR 2 ENGINE PYLON UPPER SECTION AT NR 7 RIB, INBD SIDE CHANNEL WITH CRACK. REPAIRED IAW SRM 54-52-12, FIG 208.SDR EE4Y201202010002Channel · crackedNR 1 ENGINE PYLON UPPER SECTION AT RIB NR 7 INBD SIDE CHANNEL CRACKED. REPAIRED IAW SRM 54-52-12, FIG 208.SDR EE4Y201202010001Channel · crackedNR 2 ENGINE PYLON UPPER SECTION AT RIB 8, RT SIDE CHANNEL CRACKED. REPAIRED IAW SRM 54-52-12, FIG 208.SDR NSVA2011429Structure · damagedCONTROL #343-55 RT FORWARD COWLING FORWARD HORSEWCOLLAR FRONT ATTACH POINT HOLES ELONGATED AND CHAFED. COMPLETED DOUBLER REPAIR IAW TD 340-54-11-37.SDR NSVA2011428Structure · damagedCONTROL #343-48 LT FORWARD COWLING FORWARD HORSECOLLAR FRONT ATTACH POINT HOLES ELONGATED AND CHAFED. COMPLETED DOUBLER REPAIR IAW TD 340-54-11-37.SDR DALA1204829210Fastener · unknownDURING PSV VISIT ACCOMPLISHING OPN NR 0101 ME01 (PYLON SUPPORT FITTING UPPER FASTENERS) EA 02-476701-12AD REVE REPLACED FASTENERS IN ROW A WITH FASTENER PART #: FWD HLT 141-8-5 MID HLT 141-8-5 _AFT HLT 141-8-5 NO FASTENERS REPLACED IN ROW B. NO FASTENERS WERESDR DALA1204819210Fastener · unknownDURING PSV VISIT ACCOMPLISHING OPN NBR 0301 (PYLON SUPPORTING UPPER FASTENERS) ME O3 EA 02-476701-12AD. REPLACED FASTENERS IN ROW A WITH FASTENER PART # HLT 41-8-5 - HLT 41-8-5 - HLT 41-8-5. NO FASTENERS REPLACED ON ROW B.SDR NSVA2011418Repair · crackedCONTROL #343-15: CRACK IN REPAIR PATCH ON RIGHT O/B NACELLE. COMPLETED PERMANENT REPAIR IAW TD 340-54-10-25.SDR NOCA201201291312Support Angle · crackedBRACKET CRACKED, FAIRING 447DB INTERNAL SUPPORT ANGLE CRACKED. REMOVED 447DB INTERNAL SUPPORT ANGLE AND INSTALLED NEW 447DB INTERNAL SUPPORT ANGLE AS PER BOEING DRAWING 015T1499.SDR AALA20120128AFW02Web · crackedCRACK IN PYLON AT PASS THROUGH FOR INTEGRATED DRIVE GENERATOR FEEDER CABLES. REPAIRED PER AARD 54-52-01-1.SDR AALA20120128TUL01Fitting · damagedTWO LOOSE FASTENERS FOUND ON THE VERTICAL FLANGE OF THE DIAGONAL BRACE FITTING. ACCOMPLISHED INTERIM REPAIR TO LEFT PYLON VERTICAL FLANGE DIAGONAL BRACE FITTING PER EA B757-54-015408.SDR AALA20120128AFW03Web · crackedLEFT PYLON LOWER TORQUE BOX SKIN AT GENERATOR FEEDER CABLE PASS THROUGH HAS A POSSIBLE CRACK ON THE INBOARD FORWARD CORNER. INSTALLED DOUBLER REPAIR PER EA COMP767-54-021544.SDR A6WA201240143Stand Off · crackedRT JETPIPE FAIRING FIRE LOOP FWD SHIELD FWD STANDOFF HAS A CRACKED ATTACHMENT ANGLE. R & R ATTACHMENT ANGLE PN 228-50181-285 AND STANDOFF PN WSI4A12-5 IAW SRM 51-24-06.SDR UALA2012012600536Strip · crackedNR 1 ENG PYLON 3 GAP STRIP CRACKED. REPAIRED PER MT 54-UA2 FINAL DIMENSIONS TOP MIDDLE OF GAP STRIP 4.125 IN LONG BY .15625 IN DEEP. REPAIR STARTS 8.25 INCHES FROM INBD EDGE. ACP. HFEC OF AREA, NO CRACKS DETECTED, REF NDT MANUAL, PT.6, 51-10-06. REF AD2006-SDR R61A20120063Fastener · corrodedWHILE AIRCRAFT WAS IN FOR HEAVY CHECK, LEVEL 2 CORROSION WAS FOUND ON THE RT ENGINE PYLON PANEL 429DT HARDWARE. MAINTENANCE REMOVED AND REPLACED THE HARDWARE ON THE RT ENGINE PYLON PANEL 429DT IAW EMB 170/175 AMM 20-10-07. REF: P/N'S PE21114-3C8 BOLT & PE211SDR UALA2012012500511Fastener · looseNR 1 ENG AFT STRUT LOWER FWD HEAT SHIELD SEAL HAS 4 LOOSE ATTACHMENT FASTENERS. REPLACED WITH BLIND BOLTS PER MT 54-UA1 ** MF6158 CREATED TO MONITOR **^21JUL OPB INF- :PER MT 54-UA1 INTERIM REPAIR WITH BLIND BOLTS IS ACCEPTABLE UNTIL 'C' CHECK. OPBLM TSENSDR UALA2012012600550Heat Shield · wornNR 2 ENG PYLON AFT FAIRING HEAT SHIELD GAP STRIPS NR 1, 2, 3 & 4 ARE WORN & ARE WEARING INTO HEAT SHIELDS. RMV'D FIVE HEAT SHIELDS FROM NR 2 ENGINE (BOLTS ATTACHED TO PYLON DOORS).SDR UALA2012012400499Pylon · gougedNR 1 ENG INBOARD PYLON HAS GAUGES FROM FLEXIBLE SEAL CONTACTING IT. SAMC TEXT: GOUGES ARE .031 MAX DEPTH & 2 3-4 INCH IN LENGTH. INSPECTED AREA: NO CRACKS. HAND BLENDED, REPAIR TO BE DETERMINED BY AIRBUS AT CONCLUSION OF FLT 498. CONTACT SFOLE FOR REPAIR SDR UALA2012012400493Seal · wornNR 2 ENGINE PYLON, NR 1 HEAT SHIELD SEGMENT BULB SEAL IS WORN ON FWD END OF SEGMENT. MAINT TEXT: THE COVER GAP STRIP ON NR 1 IS ALSO DAMAGED. REMOVED BULB SEAL AND COVER GAP STRIP FROM NR 1 SHIELD SEGMENT OF NR 2 ENGINE PYLON. ACP HFEC INSP OF HOLES AS NEEDSDR UALA2012011900417Seal · damaged54/EQ4498 HEAT SHIELD INSP, FOUND NUMEROUS LOOSE FASTENERS AND DAMAGED SEAL. 6 FASTENERS LOOSE ON LT PYLON FAIRING FWD HEATSHIELD SEAL 2,4,5,8,12, & 16 (NUMBERED INBD TO OTBD, REF EQ4498). REMOVED HEATSHIELD FWD SEAL ATTACH FASTENERS, BACB30VG6K7 HI-LOKS PERSDR UALA2012011900415Skate Angle · crackedNR 1 ENG PYLON SKATE ANGLES CRACKED. EG MANDATED SKATE ANGLE REPLACEMENT. PARTS IN HAND. IN FUEL TANK REMOVING ANGLES.
REF SMC1, INBD AFT SKATE ANGLE REMOVED FOR REPLACEMENT. STARTED PICKING UP FASTENER HOLES & INSTALLING NUT PLATES. REPLACED SKATE ANGLSDR UALA2012011600343Strip · damagedNR 2 ENG AFT PYLON HEAT SHIELD GAP STRIP NR 3 PREVIOUS REPAIR IS CRACKED WITH POSSIBLE HEAT SHIELD DAMAGE. SEE HISTORY FOR WORK PROGRESSION AND COMPLETION.SDR UALA2012011600342Strip · wornNR 2 ENGINE, NR 1 GAP STRIP WORN. REMOVED WORN GAP STRIP, DRILLED NEW STRIP TO NOMINAL SIZE. HOLES ON CASTING ARE OVERSIZED NEED PIN BACB30MC6A3 (PCN 754-8021) AOG# B1807. INSTALLED NEW GAP STRIP WITH OVERSIZED HI-LOKS. OVERSIZE FASTENERS OKAY REF BOEING PSDR UALA2012011600341Blanket · damagedREMOVED NR 2 AFT PYLON HEAT SHIELD DUE TO DAMAGE. REPLACED HEAT SHIELD BLANKET PER MM.SDR UALA2012011600330Fastener · looseLEFT STRUT FAIRING FORWARD SEAL, 7 EA FASTENERS LOOSE. REMOVED 7 EACH FASTENERS. INSTALLED 7 BLIND FASTENERS. NEEDS RE-CHECKED EVERY 3SVC AND PERMANENT BY NEXT C-CHECK.SDR UALA2012011100239Strip · damagedNR 1 ENGINE GAP STRIP DAMAGED. DAMAGE EXTENDED 1.7813 LONG BY .218 DEEP. TOTAL 4.843 DAMAGE LONG. ACCOMPLISHED HFEC INSPECTION PER MT54-UA2, NO CRACK NOTED. ACCOMPLISHED ECRA 5454-01 032.
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