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 SWAA2014051928120Support Angle · crackedRIGHT WING NR 2 PYLON OTBD UPPER TE SUPPORT ANGLE CRACKED. R & R ANGLE IAW SRM.SDR FDEA201405041118Plate · gougedRIGHT PYLON OTBD TR OPENING ACTUATOR FITTING DOUBLER GOUGED. REMOVED ACTUATOR FITTING FOR ACCESS IAW SRM 51-40-21. REMOVED DAMAGED DOUBLER, SHIM PLATE. FABRICATED NEW SHIM PLATE IAW STAM TRAVELER T14 1070228 USING 321A 063SS BATCH NR 0001839735 PO MST0094141SDR FDEA201405020915Hinge Fitting · wornLEFT PYLON INBD C DUCT AFT HINGE FITTING DAMAGED. COMPLIED WITH EA 6-5450-T0307765 EA. TITLE, NACELLES & PYLONS, PYLON STRUCTURES & NICKS AT INBD HINGE FITTING OF LT PYLON MAJOR IAW GMM6-2-100.SDR SWAA2014060228607Plate · crackedNR 2 ENG COWL ACCESS PANEL PLATE CRACKED OTBD FAN COWL. R & R PLATE IAW DWG & SRM.SDR SWAA2014052728326Structure · crackedLEFT PYLON STRUT ACCESS 5764L CRACKED. REPAIRED STRUT IAW EA.SDR HYIA05032014007Beam · chafedDURING SCHEDULED INSPECTION, CHAFE DAMAGE WAS NOTED AT RT NACELLE OTBD ENG BEAM AFT OF CORRESPONDING ENG MOUNT. THIS DAMAGE WILL BE REPAIRED IAW REPAIR DEFINITION SUPPLIED & SUBSTANTIATED BY DER. A SUPPLEMENT TO THIS SDR WILL BE FORWARDED SEPARATELY FURTHER SDR HYIA05032014006Beam · chafedDURING SCHEDULED INSPECTION, CHAFE DAMAGE WAS NOTED AT LT NACELLE OTBD ENG BEAM AFT OF CORRESPONDING ENG MOUNT. THIS DAMAGE WILL BE REPAIRED IAW REPAIR DEFINITION SUPPLIED & SUBSTANTIATED BY DER. A SUPPLEMENT TO THIS SDR WILL BE FORWARDED SEPARATELY FURTHERSDR UHLA2014043000355Bracket · crackedLEFT ENGINE PYLON PANEL 419QR AFT RETAINING BRACKET CRACKED. R & R IAW SRM 51-43-01, AND 51-43-02.SDR FDEA201404290884Fitting · crackedNUMBER 1 PYLON UPPER INBD HOLE OF VERTICAL FLANGE OF STRUT TO DIAGONAL BRACE FITTING HAS A CRACK INDICATION. ACCOMPLISHED EA F-5450-T0306349, NACELLES & PYLON, PYLONS STRUCTURES DEVIATION TO EO F-5450-7-5006, DUE TO CRACK IN BULKHEAD AT BRACE FITTING MOUNT HOSDR A6WA201441502Retainer · crackedSEAL RETAINER CRACKED ON PANEL 412AT. R & R WITH SERVICEABLE PN 601-37003-39 IAW SRM 51-40-11 & 51-42-06.SDR CALA2014042590898Seal · wornNR 1 PYLON BOTTOM METAL SEAL WORN. REMOVED STRAP & CHAFE PLATE ON LOWER SPAR. MATERIAL LOSS ON LOWER SPAR .005. BLENDED CHAFE MARK SMOOTH. HFEC IAW NTM 51-10-20 PB6 NO CRACKS. FABRICATED EXTENDED ANTI-CHAFING PLATE IAW SRM 54-51-12 FIG 202. INSTALLED REPSDR CALA2014042590897Seal · wornNR 2 PYLON BOTTOM METAL SEAL WORN. REMOVED WORN CHAFE STRIP & STRAP. MATERIAL LOSS <.002 ON LOWER SPAR. NR 2 PYLON LOWER SPAR REPAIRED WITH EXTENDED CHAFE PLATE.SDR DALA14025000188Web · crackedNR 2 PYLON STRUT INBD MID SPAR FITTING LOWER WEB FOUND CRACKED. REPAIRED IAW ERA 524403-14.SDR CALA2014041700471Web · corrodedNR 1 PYLON AFT FAIRING LOWER FWD WEB CORRODED. REMOVED & INSTALLED NEW NR 1 PYLON AFT FAIRING LOWER FWD WEB IAW DWG 313A2713 REV A.SDR CALA2014041790849Strip · crackedNR 1 ENG AFT FAIRING FIRE SHIELD GAP COVER STRIP HAS 1.5 INCH CRACK ON THE THIRD FIRE SHIELD SEGMENT. REMOVED DAMAGE CALCULATED LOSS IS .1085 SQ INCHES. ACCOMPLISHED HFEC OF EFFECTED AREA, NO CRACK INDICATIONS NOTED. NEED TO ACCOMPLISH FINAL DISPOSITION.SDR CALA2014041700469Angle · corrodedNR 2 PYLON AFT FAIRING LOWER FWD INBD ANGLE HAS SURFACE CORROSION & CORROSION IN AFT ATTACH HOLE. INSTALLED NEW ANGLE IAW SRM 51-40-02.SDR CALA2014041700470Web · corrodedNR 2 PYLON AFT FAIRING LOWER FWD WEB HAS CORROSION AT FWD END INSTALLED NEW WEB IAW SRM 51-40-02.SDR AALA20140416004Stiffener · crackedLEFT PYLON OTBD SIDE, STIFFENER CRACKED AT STATION 285. ACCOMPLISHED REPAIR IAW AARD 54-52-02-2.SDR CALA2014041490807Strip · crackedNR 1 ENG AFT FAIRING FIRE SHIELD GAP COVER STRIP HAS 1.5 INCH CRACK ON THE THIRD FIRE SHIELD SEGMENT. REMOVED DAMAGE CALCULATED LOSS IS .1085 SQ INCHES. ACCOMPLISHED HFEC OF EFFECTED AREA, NO CRACK INDICATIONS NOTED. NEED TO ACCOMPLISH FINAL DISPOSITION. ASDR CALA2014040890780Seal · wornNUMBER 1 PYLON BOTTOM METAL SEAL WORN. REMOVED STRAP & CHAFE PLATE ON LOWER SPAR. MATERIAL LOSS ON LOWER SPAR .005 INCHES. BLENDED CHAFE MARK SMOOTH. HFEC IAW NTM 51-10-20 PB6 NO CRACKS. FABRICATED EXTENDED ANTI-CHAFING PLATE IAW SRM 54-51-12 FIG 202. INSTSDR CALA2014040890776Seal · wornNUMBER 2 PYLON BOTTOM METAL SEAL WORN. REMOVED WORN CHAFE STRIP & STRAP. MATERIAL LOSS <.002 INCHES ON LOWER SPAR. HFEC OF WORKED AREA IAW NTM 51-10-20 PB6 NO CRACKS FOUND. FABRICATED EXTENDED ANTI-CHAFING PLATE IAW SRM 54-51-12 FIG 202. INSTALLED EXTENDESDR ABXA20140403195Beam · crackedNR 1 ENG, AFT PYLON SECTION, RT LOWER BEAM IS CHAFED & CRACKED FWD END. R & R BEAM IAW SRM 51-40-02. SDR INFO PN 313T1380-243, SN NSN, PART NAME BEAM, CRACKED 2 INCHES, FS & BS LOCATION NAC STATION 35334. ACFT WAS GNDED.SDR SWAA2014042927511Angle · crackedANGLE CRACKED LOCATED INTERNAL AREA ACCESS PANEL 5757L STRUT TORQUE BOX ENG NR 1. R & R ANGLE IAW SRM & DWG.SDR SWAA2014042827443Angle · crackedANGLE CRACKED ON INTERNAL AREA ACCESS PANEL 5743L AFT STRUT FAIRING ENG NR 1. R & R ANGLE IAW SRM & DWG.SDR ABXA2014040179Stiffener · crackedNUMBER 2 PYLON INBD HYD BAY. AFT HORZ STIFFENER AT NAC 370 HAS DAMAGED HOLES COMMON TO THE LOWER DOOR FRAME CHANNEL. REMOVED DAMAGED STIFFENER IAW SRM 51-40-02. FABRICATED NEW STIFFENER IAW SRM 54-51-71 & 51-30-01, PERFORMED NDT IAW NDTM PART 6 51-00- 19, ASDR AALA20140406004Access Panel · wornNR 2 PYLON ACCESS PANEL 443 - FRAME HAS A WORN EDGE. FABRICATED & INSTALLED PANEL IAW AARD 20-00-00-1.SDR CALA2014032100379Web · corrodedNR 1 ENG PYLON AFT FAIRING, FWD WEB PN 313A2713-2 FOUND CORROSION. INSTALLED NEW FWD WEB ON NR 1 ENG PYLON AFT FAIRING IAW SRM 5 1-40-02 & DWG 313A2700.SDR CALA2014032100378Angle · corrodedNR 1 ENG PYLON AFT FAIRING OTBD FWD WEB ANGLE CORRODED. INSTALLED NEW OTBD FWD WEB ANGLE ON NR 1 ENG PYLON IAW SRM 51-40-02 & DWG 313A2700.SDR CALA2014032100377Angle · corrodedNR 1 ENG PYLON AFT FAIRING INBD FWD WEB ANGLE CORRODED. INSTALLED NEW INBD FWD WEB ANGLE ON NR 1 ENG PYLON IAW SRM 51-4 0-02 & DWG 313A2700.SDR CALA2014032100375Web · corrodedNR 2 ENG PYLON AFT FAIRING FWD WEB CORRODED. R & R NR 2 ENG PYLON AFT FAIRING FWD WEB IAW DWG 313A2700 & SRM 51-40-02.SDR CALA2014032100374Angle · corrodedNR 2 EMERGENCY PYLON AFT FAIRING OTBD WEB ANGLE CORRODED. R & R NR 2 ENG PYLON AFT FAIRING OTBD WEB ANGLE IAW DWG 313A2700 & SRM 51-40-02.SDR CALA2014032090654Seal · looseSTRIPPING LOOSE NR 1 ENG OTBD AFT PYLON, SECURED SEAL.SDR QXEA2014032400231Stiffener · crackedCRACK AND CHAFING FOUND ON PANEL 424AR. REPLACED STIFFENER IAW SRM 51-42-05, STEP 4D(3-10).SDR QXEA2014032400230Stiffener · crackedCRACK AND CHAFING FOUND ON PANEL 424AL. REPLACED STIFFENER IAW SRM 51-42-05 STEP 4D(3-10).SDR SWAA2014033126638Support Fitting · crackedRIGHT WING NR 2 PYLON UPPER INBD SUPPORT CLIP CRACKED. R & R CRACKED CLIP IAW SRM.SDR CALA2014032000360Fitting · corrodedNR 2 ENG PYLON AFT FAIRING AFT WEB CORRODED. R & R AFT WEB FITTING IAW SRM 51-40-02 & DWG 313A2700.SDR R61A201403130403Rub Strip · corrodedDURING FOR HEAVY CHECK, FOUND RT ENGINE OTBD HALF COWLING FAN ON FWD/AFT METALIC STRIP WORN AND CORRODED. MX R & R RT ENGINE OTBD HALF COWNING FAN ON FWD/AFT METALIC STRIP, PN 341-2221-503, AMM 71-11-02.SDR AALA20140313014Fitting · damagedNUMBER 1 PYLON ONE FASTENER HOLE HAD A CRACK INDICATION DURING HFEC INSPECTION. THE SUBJECT HOLE WAS IN THE AFT FITTING, INBD SIDE, UPPER AFT HOLE. THE HOLE ON THE SKIN ONLY WAS OVERSIZED TO REMOVE DAMAGE & A FREEZE PLUG WAS INSTALLED.SDR SWAA2014040926949Fitting · crackedRIGHT PYLON INTERFACE FITTING CRACKED. REPAIRED FITTING IAW EA.SDR SWAA2014031025891Plate · crackedLT NACELLE SPLICE PLATE CRACKED AT BS 234, UPPER PYLON FRAME. R & R PLATE IAW SRM.SDR SWAA2014040726837Fitting · crackedRT PYLON AFT STRUT FAIRING T ANGLE FITTING CRACKED. REPAIRED FITTING IAW EA.SDR SWAA2014032426486Support Angle · crackedNR 1 ENG AFT STRUT ACCESS PANEL 5752L SUPPORT ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.SDR SWAA2014030425740Angle · crackedRT WING PYLON UPPER TE PANEL OTBD ANGLE CRACKED. R & R ANGLE IAW SRM.SDR ASOA2014032710190Fairing · crackedRT ENGINE UPPER HINGE LINE FAIRING AFT SECTION CRACKED. REMOVED HINGE LINE FAIRING DRILLED OF ATTACHING STIFFERS TO TRANFER TO NEW SKIN & TRANFERED HOLES TO NEW SKIN IAW SRM 51-42-06-001-001-A01. COUNTERSUNK NEW SKIN & ATTACHED STIFFENERS IAW SRM 51-42-06-00SDR ASOA2014032710189Fairing · crackedLT ENGINE UPPER HINGE LINE FAIRING AFT SECTION CRACKED. REMOVED LT ENGINE FARING AND REMOVED SKIN FROM ATTACHED STIFFENERS AND SEALS AND TRANSFERED TO NEW SKIN IAW SRM 57-42-06-001-001-A01 SDRWG GN624-4265. INSTALLED NEW RUB STRIP AND RESTORED A023 FINISH TOSDR KCSA201402221012Angle · wornNR 4 PYLON OTBD ANTI-ROTATION BRACKET ATTACH POINT REPAIR ANGLE WORN THRU.SDR KCSA201402221011Angle · wornNR 4 PYLON INBD ANTI-ROTATION BRACKET ATTACH POINT REPAIR ANGLE WORN THRU.SDR CALA2014022190405Blanket · tornRT NACELLE STRUT HEAT BLANKET TORN ABOVE NR 1 HEAT SHIELD. EVIDENCE OF HEAT DAMAGE TO STRUT STRUCTURE. REPLACED HEAT BLANKET IAW AMM 54-54-01. REPLACED LOWER SPAR WEB STRUCTURE IAW SRM 51-40-0 2. REPLACED CHORD, FRAME, & BULKHEAD IAW SRM 51-20-01 & DRAWINSDR SIMA20140219004Yoke · crackedLEFT ENG LOWER FWD YOKE IS CRACKED. R & R LT FWD LOWER YOKE IAW EO EM-54MR-386.SDR CALA2014021790399Structure · crackedLT 1 PYLON OTBD DRAIN HOLE AT NACELLE STATION 156 IS CRACKED. ALSO FOUND TWO EACH CRACKS AT THE INBD DRAIN HOLE, NACELLE STATION 156. STOP DRILLED ENDS OF CRACKS, FABRICATED TWO EACH DOUBLERS & FILLERS & INSTALLED IAW SRM 54-53-01, REPAIR 10.
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