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 R61A201303130269Grill · crackedWHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE REPLACED THE NUMBER ONE ENGINE PYLON INBOARD EXHAUST GRILL. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE ENGINE PYLON INBOARD EXHAUST GRILL IAW EMB ETD2013-190-004333. THE AIRCRAFT WAS RETURNED TO SERVICE 3/14SDR DALA13011675806Support Angle · crackedAFT UPPER PYLON SUPPORT ANGLE CRACKED IN PYLON JUST AFT OF CORE COWLS. REMOVED OLD SUPPORT ANGLE. DRILLED NEW ANGLE NW 5B54-41985-1. OK TO INSTALL. INSTALLED SKATE ANGLE IAW DWG 311N3570.SDR V0XR2013031200002Bracket · chafedLEFT NACELLE TOP OF FINGERNAIL DECK JUST AFT OF WHEEL WELL CUTOUTS IN CENTER BRACKET CHAFED THROUGH AFT PART, XN 263. REPAIRED CHAFE MARK AT XN 263 ON LEFT NACELLE, TOP OF FINGERNAIL IAW DEHAVILLAND RD8-54-177, REPAIR NR 1, BY REMOVING CHAFED MATERIAL AND INSSDR V0XR2013030700008Structure · crackedCRACKS IN INTERIOR PIPE SURFACE OF RIGHT EXHAUST FINGERNAIL. REPAIRED CRACKS IN INTERIOR PIPE SURFACE OF RIGHT EXHAUST FINGERNAIL IAW DASH 8-100 SRM 54-78-11, 51-40-07, 51-40-11 AND DHC DRAWING 85411373. W/O 50335, W/C 4279SDR UALA2013030601330Plate · wornNR 1 PYLON CNA ANTI CHAFING PLATE WORN AT RIB 5. INSTALLED ANTI-CHAFING PLATE PER SRM 54-51-12 FIG 202.SDR FDEA201303030493Splice Plate · corrodedNR 1 NACELLE STRUT PYLON STRUCTURE UPPER WEB INBD SPLICE PLATE AT PP 170.0, FOUND WITH CORROSION. REMOVED AND REPLACED IAW DWG 311N5040 REV.N. REPAIR IS MAJOR.SDR AALA20130308008Fitting · crackedRIGHT PYLON: SHEARED OUTBOARD LOWER FASTENER THROUGH THE VERTICAL FLANGE OF THE DIAGONAL BRACE FITTING OF THE AFT BULKHEAD. HFEC INSPECTION OF THE FASTENER HOLE INDICATED EVIDENCE OF A CRACK. REAMED HOLE. HFEC REINSPECTION CONFIRMED NO CRACK. REINSTALLED SDR IXXA201304120002Channel · crackedNR 1 PYLON INBD CHANNEL ABOVE ARROWHEAD PANEL HAS A 2.00" CRACK. REPLACED INBD CHANNEL ON NR 1 PYLON IAW SRM 57-40-02.SDR KCSA201302280033Stiffener · crackedNR 4 PYLON HAS CRACKED STIFFENER ON MID SPAR WEB AT NAC STA 187.SDR SWAA2013030613361Rub Strip · crackedCRACK ON RUBSTRIP ON NACELLE STRUT ACCESS PANEL 57700L ENGINE NR 1. REMOVED AND REPLACED RUBSTRIP IAW SRM.SDR SWAA2013031413626Attach Angle · crackedNR 2 PYLON INSIDE ACCESS PANEL 440JB VERTICAL ATTACH ANGLE CRACKED. REMOVED AND REPLACED ANGLE PER SRM.SDR SWAA2013030413282Rub Strip · crackedCRACK ON RUBSTRIP LOCATED ON STRUT ACCESS PANEL 58720R ENGINE NR 2. REMOVED AND REPLACED RUBSTRIP IAW SRM AND DWG.SDR QXEA2013022500421Intercostal · crackedWHILE WORKING LT NACELLE MOD TC 6-54-441/LT FOUND INTERCOSTAL, CRACKED AT XN197.81. REMOVED INTERCOSTAL IAW SRM 51-42-05-02-01, 51-40-15-02-01, REV 12. MATCH DRILLED NEW INTERCOSTAL IAW SRM 51-40-07-02-01, REV 12. OK TO INSTALL NEW INTERCOSTAL. INSTALLED INTSDR FDEA201302220419Ferrule · crackedNR 2 PYLON FERRULE CRACKED AT FWD ATTACH POINT OF PNUEMATIC DUCT. CRACK IS 0.50 LONG. COMPLIED WITH EA 6-5450-T0300088 AND SB 54-2028. R & R FERRULE HALVES AND SPLICES.SDR FDEA201302210405Fitting · crackedNR 2 PYLON FERRULE CRACKED AT FWD OTBD UPPER CORNER AND AT FWD ATTACH POINT OF PNUEMATIC DUCT. CRACK A IS 1' LONG AND CRACK B IS 0.50 LONG. COMPLIED WITH EA 6-5450-T0300088 AD SB 54-2028. R & R FERRULE HALVES AND SPLICES.SDR FDEA201302190368Shim · migratedNR 1 PYLON UPPER SPAR FITTING, SHIM MIGRATED, UPPER AND LOWER SHIMS AFTER FURTHER EVALUATION FOUND VERTICAL SHIM MIGRATION UPPER = 0.150 AND LOWER =0.009 (FWD & AFT). HORIZONAL SHIM NO MIGRATION NOTED, FOUND WITHIN LIMITS IAW SRM 54- 50-90 PAGE 201, FIG 201 RSDR FDEA201302190367Shim · migratedNR 2 PYLON LOWER MID-BULKHEAD LOWER FLANGE SHIMS MIGRATING ON BOTH SIDES AFTER FURTHER EVALUATION 3 EA LOCATIONS LT FWD AND AFT AND RT AFT WERE FOUND TO BE IN LIMITS IAW SRM 54-50-90, FIG 201. REPAIR NR 7 STEP 4D. TRIMMED THE EXPOSED PLIES AND SEALED IAW SSDR AALA20130219005Shim · migratedLEFT ENGINE PYLON MID BULKHEAD INBOARD LOWER FORWARD ATTACH SHIMS MIGRATING. HIGH FREQUENCY EDDY CURRENT INSPECTION REVEALED CRACK INDICATIONS ON BOTH HOLES. REPAIRED AFT FASTENER LOCATION AND INSTALLED NEW SHIMS AT BULKHEAD TO CHORD ATTACH POINT PER AARD 54SDR UALA2013021800978Panel · damagedNR 2 AFT O/B PYLON PANEL DAMAGED. PERFORM INTERIM REPAIR IAW ECRA 5454-01067 PART 1. THIS REPAIR IS ACCEPTABLE UNTIL 11-19-13 WITH AN HFEC INSPECTION TO VERIFY A CRACK FREE CONDITION WITHIN 125 FLIGHT HOURS.SDR SWAA2013022513078Rub Strip · crackedCRACK ON RUBSTRIP INBOARD POSITION LOCATED ON UPPER PYLON SIDE STRUCTURE AT NAC STA 196.840 INTERNAL CAVITY OF PYLON ACCESS PANEL 5747L ENGINE NR 1. REPLACED RUBSTRIP IAW B737-500 SRM AND DRAWING.SDR HNAA2013021500073Angle · crackedRT NACELLE FINGERNAIL OTBD LOWER AFT HEAT SHIELD ANGLE IS CRACKED. R & R LOWER AFT ANGLE IAW SRM 51-42-05.SDR HNAA2013021500068Angle · crackedLEFT INBD AND OTBD UPPER ANGLE IS CRACKED. REPAIRED BOTH LT AND RT UPPER ANGLES IAW SRM 51-42-45.SDR HNAA2013021500067Stiffener · crackedTWO STIFFENERS AND ONE CHANNEL WAS FOUND CRACKED ON RT NACELLE HEAT SHIELD. REPAIRED STIFFENERS AND CHANNEL ON RT NACELLE HEAT SHIELD AD IAW RD8-54-1153 AND RD8-54-3195.SDR IPXA3M77503Intercostal · crackedINSPECTION TYPE:4C, NR 2 ENGINE PYLON LT INTERCOSTAL CRACKED BELOW NR 4 BANJO FITTING AT UPPER FWD RADIUS. REPAIRED NR 2 ENGINE PYLON LT REAR CENTER SPAR TO REAR SPAR LOWER PANEL REF STASA EA 011-5530-01-A4471 REV I/R, EO MD11-5530-50139-A.SDR SWAA2013021912774Support Bracket · brokenSUPPORT BRACKET ON AFT END OF AFT STRUT LOWER FAIRING BROKEN. REMOVED AND REPLACED SUPPORT BRACKET PER SRM 51-40-02.SDR SWIA201332905Structure · crackedLEFT ENGINE PYLON TRAILING EDGE HAS CRACK AND DELAMINATION. (C-CHECK) REPAIRED CRACK AND DELAMINATION AT LEFT ENGINE PYLON TRAILING EDGE IAW STS EA.SDR HNAA2013020800042Stiffener · crackedTWO STIFFENERS AND ONE CHANNEL WAS FOUND CRACKED ON RT NACELLE SHIELD. FABRICATED HEAT SHIELD IAW RD 8-54-1153 AND RD8-54-3195.SDR HNAA2013020800040Structure · corrodedNR 2 NACELLE AFT ID CORRODED. REPAIRED RT AFT ID IAW RD8-54-020. NO DEFECTS NOTED.SDR SWAA2013021512709Rub Strip · crackedCRACK ON RUBSTRIP P/N 69-76746-5 LOCATED ON ACCESS PANEL 57710L OF ENGINE 1. REPLACED RUBSTRIP IAW SRM B737-300 51-40-02-0G-0, 51-10-02-0G-0 ITEM 8 AND DWG 65C27356.SDR DALA201302140332Acoustic Panel · damagedTHE LOWER INNER ACOUSTIC PANEL WAS FOUND WITH EXTENSIVE DAMAGE TO THE INNER AND OUTER SKINS. REPAIRED IAW ERA 510867-14 REV ORIG.SDR SWAA2013021912795Access Panel · crackedCRACK ON FWD CORNER OF ACCESS PANEL 57720L LOCATED ON LEFT NACELLE STRUT. REPAIRED ACCESS PANEL 57720L LOCATED ON LEFT NACELLE STRUT IAW B737-300 SRM 51-70-16-OG-0 REPAIR 7.SDR SWAA2013021112572Access Panel · delaminatedNR 2 ENGINE ACCESS PANEL 441AL, IS DELAMINATED. REPAIRED PER SRM.SDR USAA2013022500020Fitting · corroded3S CHECK - LEVEL 2 GALVANIC CORROSION ON LEFT PYLON SPIGOT FITTING INTERNAL AREA. REPLACED SPIGOT RECEPTACLE FITTING ON LEFT PYLON IAW A320 SRM 51-72-11 & 54-51-12 PAR. 5A & AIRBUS REPAIR DRAWING R54612042 & R54612043.SDR UIEA2013021900101Support Channel · crackedNR 4 PYLON CASE DRAIN MODULE SUPPORT CHANNEL, S/E SIDE FOUND CRACKED.NR 4 PYLON CORE DRAIN MODULE SUPPORT CHANNEL FABRICATED IAW BS NO R1-94-00-10147 AND REPLACED IAW SRM 51-10-02SDR UIEA2013020400066Skate Angle · crackedCRACK ON THE SKATE ANGLE OF NR 3 PYLON INBD FAIRING AT NAC STA 457. REPAIRED IAW EI NR T2013A54B-290, REV 00 AND REV 01.SDR QXEA2013020100239Intercostal · corrodedRT AFT NACELLE INTERCOSTAL HAS CORROSION AT STA XN305 BELOW HEAT SHIELD. REMOVED INTERCOSTAL IAW SRM 51-42-05-02-01 AND 51-40-15-02-01. MATCH DRILLED NEW INTERCOSTAL IAW SRM 51-40-07-02-01. INSTALLED NEW INTERCOSTAL IAW SRM 51-42-05-02-01 AND 51-40-15-02-01SDR SWAA2013020812438Support Angle · crackedCRACK ON SUPPORT ANGLE ON INTERNAL STRUCTURE OF ACCESS PANEL 5757L. REPLACED SUPPORT ANGLE LOC INTERNAL STRUCTURE OF ACCESS PANEL 5757L IAW B737-300 SRM 51-10-02 ITEM 8 DWG 313A1380, B737-300 SRM 51-40-02.SDR SWAA2013012811999Skate Angle · crackedNR 2 PYLON UPPER SKATE ANGLE CRACKED. TRIMMED OUT DAMAGED AREA PER BOEING DRAWING SG95530003.SDR R5KB2013012846170Structure · crackedCRACK ON TOP OF NR 1 PYLON OUTBD FASTENER HOLE"P" OF S/B 727-54A0010R6, FROM HOLE TO OTBD EDGE OF LOWER ANGLE.SDR DALA13005033272Support Angle · crackedDURING INSPECTION, FOUND CRACK ON SUPPORT ANGLE LOC AT RIB NR7 OTBD SIDE OF UPPER FWD PYLON ENGINE NR 1. REPLACED SUPPORT ANGLE LOC AT RIB NR 7 OTBD SIDE OF UPPER FWD PYLON ENGINE NR 1 IAW SRM 51-72-11 AND DWG D54630740.SDR R61A201301240098Cleat · crackedWHILE AIRCRAFT WAS IN FOR HEAVY CHECK MAINTENANCE REPORTED LT ENGINE, INBOARD FORWARD SPLINE COWL CLEAT IS CRACKED. MAINTENANCE REMOVED AND REPLACED THE INBOARD SPLINE COWL CLEAT IAW BOMBARDIER Q400 SRM 51-41-00-00-01 & 51-42-05-02-01. AIRCRAFT IS CURRENTLY SDR SPUY201301240003Angle · crackedDURING ROUTINE C-CHECK INSPECTION, NR 2 ENGINE. LT CORE COWL LOWER ANGLE CRACKED AT NAC STA 293.50, REF NR N0306.SDR DALA13004203213Fitting · corrodedDURING INSPECTION, FOUND NR 1 ENGINE SPIGOT RECEPTACLE FITTING BORE AT UPPER SPAR HAS FITTING CORROSION. REMOVED CORROSION IAW SRM 51-74-00 FINAL DIAMETER FOUND TO BE OUT OF LIMITS OF 4.345 ALLOWABLE DIA 4.335 IAW SRM 54-51- 12, FIG 101. REMOVED FITTING IAW SDR SWAA2013021512722Angle · crackedCRACK ON ANGLE LOCATED ON OUTBOARD SIDE PYLON NR 2 NAC STA 255.72. REPLACED ANGLE IAW SRM B737-300 51-10-02 ITEM 8 AND DRAWING 311A1680.SDR SWAA2013012912054Support Angle · crackedSUPPORT ANGLE CRACKED ON STRUCTURE OF OTBD SIDE OF PYLON RT ENG NR 2 WBL 198.6 AND FRONT SPAR INTERNAL CAVITY PYLON STRUT TORQUE BOX. R & R ANGLE IAW SRM AND DWG.SDR SWAA2013012811935Support Angle · crackedSUPPORT ANGLE CRACKED AT STRUCTURE I/N SIDE OF PYLON LEFT ENG NR 1 WBL 183.4 AND AT LEVEL OF FRONT SPAR INTERNAL CAVITY PYLON STRUT TORQUE BOX. REPLACED ANGLE IAW SRM AND DWG.SDR USAA2013012200018Slider · brokenMAINTENANCE REPORTED THE LEFT WING ENGINE PYLON AFT MOVEABLE FAIRING INBOARD SLIDER BROKEN. MAINTENANCE REPLACED LEFT WING ENGINE PYLON AFT MOVEABLE FAIRING INBOARD SLIDER IAW AMM 54-55-41.SDR R61A201301170060Grill · crackedWHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE REPLACED HEAT SHIELD GRILL NUMBER ONE ENGINE INBOARD AFT PYLON FAIRING. MAINTENANCE REMOVED AND REPLACED THE HEAT SHIELD GRILL IAW EMB ETD 2012-190-011648-B REV B. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.SDR DALA1303850125Web · misrepairedNR 1 PYLON LT UPPER WEB FOUND EXISTING REPAIR IAW ERA 267062-14 NOT IAW SRM AND UPON NDT INSPECTION FOUND CRACK AT ANTI-ICE DUCT CUT-OUT ON WEB. NR 1 PYLON UPPER SPAR WEB CRACKED AREA REPAIRED IAW PRI 510604-14, REV O AND REV 1. (ERA 267062-14)SDR UALA2013011100189Rub Strip · damagedNR 4 ENGINE INBRD CORE COWL L/E RUB STRIP DAMAGED. REMOVED AND REPLACED DAMAGED RUB STRIP.
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