JASC 5420
Service difficulty reports · 3,946
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 IPXA2026021574651Web · crackedNR 2 PYLON AFT FAIRING SURFACE WEB HAS CRACK WEB FAIRING SURFACE WAS REMOVED IAW A300/600 SRM 51-40-21 WEB WAS INSTALLED IAW A300/600 SRM 51-40-21SDR HNAA2026031000206Bracket · cracked54-2176 RH PYLON HAS CRACKED FORE PRECOOLER STRUCTURE BRACKET. RAR BRACKET IAW SRM 51-40-02SDR IPXA2026030223168Channel · crackedCRACKED CHANNEL, NR 1 PYLON AFT FAIRING PANEL 437DB INNER OTBD SIDE CHANNEL. INSTALLED A NEW BULKHEAD ANGLE IAW SRM 51-40-02-0G, REV 130 AND DWG 313T2362, SHT 4, REV B.SDR IPXA2026022523383Bracket · crackedCRACKED BRACKET, NR 2 PYLON INTERNAL RESERVOIR HYD TUBE SUPPORT BRACKET AT R/H SIDE UPPER HINGE BEAM AREA. (REPLACE). IAW SRM 51-40-02-0G REV. 130 AND AIPC 54-51-53-18 REV. 36 INSTALLED NEW BRACKET.SDR IPXA2026030411397Bracket · crackedCRACKED NR 4 PYLON HYD RESERVOIR BLEED VALVE MOUNTING BRACKET. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 105, & DWG 65B82300, SHT 4, REV B.SDR IPXA2026022410668Channel · crackedCRACKED CHANNEL, NR 1 PYLON AFT FAIRING INNER AFT BULKHEAD INBD SIDE CHANNEL. (REPLACE). INSTALLED NEW CHANNEL I.A.W SRM 51-40-02-0G REV. 130 AND BOEING DWG NO. 313T3380 SH. 5 REV. H AND 313T2362 SH. 4 REV. B. REVIEW COMPLETE.SDR IPXA2026022510717Channel · crackedCRACKED CHANNEL, NR 2 PYLON AFTER FAIRING PANEL 447DB INNER OUTBOARD CHANNEL CRACK. (REPLACE). INSTALLED NEW CHANNEL I.A.W SRM 51-40-02-0G REV. 130 AND BOEING DWG NO. 313T2362 SH. 4 REV. B. REVIEW COMPLETE.SDR IPXA2026022400346Support Bracket · crackedCRACKED SUPPORT BRACKET, NR 2 PYLON AFTER FAIRING INNER VANE TUBE SUPPORT NR 1 SUPPORT BRACKET (REPLACE). INSTALLED NEW BRACKET IAW SRM 51-40-02-0G REV. 130 AND DWG 272T0182 SH. 1 REV. A.SDR IPXA2026022400341Support Bracket · crackedCRACKED BRACKET, NR 2 PYLON AFTER FAIRING INNER VANE TUBE SUPPORT NR 2 SUPPORT BRACKET (REPLACE). INSTALL NEW BRACKET IAW SRM 51-40-02-0G REV. 130 AND DWG 272T0182 SH. 1 REV. A.SDR SWAA2026031668753Web · crackedCRACK ON WEB INBD FAN COWL ON ENGINE 1 2026-112370<[01] REPLACED WEB ON INBD FAN COWL ON ENGINE 1 IAW SRM 51-40-02-0G-0 AND CMM 71-13-30, REV 32, PAGE 10092.SDR SWAA2026030266698Bracket · crackedNUMBER 1 ENGINE INBD FAN COWL VERTICAL BRACKET JUST AFT OF OIL SERVICE DOOR IS CRACKED. NR 1 ENGINE FAN COWL REPLACED ON TTG8Q00S5HD9.SDR DALA2026020500826Web · abnormalAD / EM-EO TASK - FOUND NO.1 PYLON FWD UPPER WEB FOUND WITH AN EXISTING REPAIR AT NAC STA 221.250 TO NAC STA 237.500. REPAIRED THE WEB IAW ER/A 631985-14. (1425083)SDR IPXA2026021096944Stiffener · cracked# 2 PYLON ANGLE IS CRACKED INSIDE PANEL 445AL , ATA 54 STR. INSTALLED (1EA) NEW SPAR STIFFENER, (1EA) WEB CHANNEL (INBD) AND (1EA) WEB CHANNEL (OUTB) PREVIOUSLY REMOVED FOR ACCESS AT #2 PYLON INNER SIDE ABOVE EXHAUST IAW B757-200PF SRM 51-40-02-0G-0 PER E.A.#:SDR IPXA2026022652366Bracket · crackedNR 2 PYLON, INBD SIDE AT RIB 8, BRACKET CRACKED. REMOVED BRACKET I.A.W. A300-600 SRM 51-40-21. INSTALLED BRACKET I.A.W. A300-600 SRM 51-40-21.SDR IPXA2026021552275Bracket · crackedNR 2 PYLON, AFT FAIRING LOWER SURFACE, OTBD BRACKET CRACKED. THE BRACKET WAS REMOVED IAW SRM 51-40-21 & INSTALLED IAW SRM 51-40-21.SDR IPXA2026021552250Bracket · crackedNR 2 PYLON, AFT FAIRING LOWER SURFACE, INBD BRACKET CRACKED. THE BRACKET WAS R & R IAW SRM 51-40-21.SDR JJBA20260120041Seal · tornRIGHT ENGINE PYLON LOWER FAIRING HAS SEAL TORN. REMOVED BLADE SEAL AND INSTALLED RT ENGINE PYLON LOWER FAIRING SEAL.SDR IPXA2026021200748Angle · damaged475AL HAS MISSING HALF L ANGLE AT BOTTOM OF 7TH RIB FROM FWD END. REMOVED L ANGLE IAW SRM 51-40-21, WHEN REMOVING FOUND LOWER LONGERON WITH CRACK INSTALLED PANEL 475AL IAW AMM 54-55-00/401SDR DALA2025123109553Web · crackedFOUND NR 1 PYLON UPPER WEB CRACKED AT OTBD SIDE OF PYLON TO WING INBD MID SPAR FITTING. REPAIRED AS PER PRI 630868-14 (1368270)SDR SWAA2025122253468Fairing · damagedFAN FAIRING; FWD OF FAN OGV HAS ELONGATED FASTENER HOLE AT 5 OCLOCK POSITION. REMOVED AND REPLACED SPLITTER FAIRING IAW AMM 72-21-03.SDR SWAA2025122253583Bracket · crackedRIGHT ENGINES O/B AFT STRUT FIRE SEAL BRACKET IS CRACKED. PICTURE ADDED.<[01] 01 - REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-A00729 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)]SDR SWAA2025123052809Bracket · crackedNR 1 ENGINE OTBD SIDE 2 EA. COOLING BRACKETS CRACKED. REMOVED AND REPLACED THE NR 1 ENGINE COOLING BRACKET IAW AMM 75-24-03-000-802-G00, STEP 5.G 1 THRU 5.SDR SWAA2025123052811Bracket · crackedNR 1 ENGINE IB SIDE 2 EA. COOLING BRACKETS CRACKED. REMOVED AND REPLACED NR 1 ENGINE COOLING BRACKETS IAW AMM 75-24-03-000-802-G00, STEP 5, G 1 TO 5.SDR SWAA2025123052810Bracket · crackedNUMBER 2 ENGINE INBD SIDE 1 EA. COOLING BRACKET CRACKED. REMOVED AND REPLACED THE NR 2 ENGINE 9 O'CLOCK COOLING BRACKET IAW AMM 75-24-03-000-802-G00 STEP 5.G 1 THRU 5.SDR SWAA2025120841318Support · crackedNUMBER 1 PYLON AFT FAIRING, AFT WEDGE CRACKED AT T/E SUPPORT. EVALUATED DAMAGED AFT WEDGE ASSEMBLY AND FOUND COMPONENT UNSERVICEABLE IAW SRM 54-50-90-1A-1. REMOVED AND REPLACED NR 1 ENGINE PYLON AFT WEDGE ASSY IAW SRM 51-40-02-0G-0, AND DWG 313A2752, SHEET 0SDR SWAA2025123040175Angle · crackedNR 1 ENGINE INBD FAN COWL VERTICAL ANGLE AFT OF OIL SERVICE DOOR CRACKED UPPER END. NR 1 ENGINE INBD FAN COWL TO BE REMOVED, REPLACED AND INSTALLED ON 7111-E-17063-NG.SDR SWIA2025112475755Structure · damagedT/E OF THE RT PYLON IS DELAMINATED AND MISSING COMPOSITE MATERIAL REPLACED AND INSTALLED NEW TRAILING EDGE ASSY, PYLON RT, PER DWG.601-37012 REV B AND REF.CRJ/200 SRM.51-42-10-00, 51-74-00-00. COMPLIED WITH SKYWEST TASKCARD 51-900-1003-SKY.SDR SWAA2025120832820Shield · crackedNR 1 ENGINE INBD FAN COWL OIL DOOR SHIELD HAS A CRACK IN IT. REMOVED AND REPLACED THE CRACKED NR 1 ENGINE INBD FAN COWL OIL DOOR SHIELD IAW SRM 51-40-02-0G-0.SDR SWAA2025112832026Web · crackedCRACK INBOARD FAN COWL SUPPORT WEB ON ENGINE 1. REPLACED SUPPORT WEB LOCATED INBOARD FAN COWL ENGINE 1 IAW SRM 51-10-02 ITEM 9 SRM 51-40-02 AND CMM 71-13-30 MEASURE OF CRACK IS L: 0.680 INCH;SDR DALA2025110608101Web · crackedFOUND NO.1 PYLON AFT UPPER WEB AT NSTA 290 CRACK. THE CLOSEOUT ANGLE REMOVED AND REPLACED AS PER B767-400 SRM 51-40-02 REV 76.00 AUG-29-2025. REFER TO ER/A 629817-14 (1277534)SDR IPXA2025103116091Web · crackedNR 1 PYLON AFT MEMBER BETWEEN RIB 18 AND RIB 21 CRACKED. JP-110. REMOVED AND REPLACED AFT MEMBER (WEB) IAW A300-600 SRM 51-40-21.SDR SWAA2025120429674Seal Plate · crackedCRACK SEAL PLATE LOCATED ON ACCESS PANEL 434CL ON LT PYLON. REPLACED SEAL PLATE ON ACCESS PANEL 434CL IAW SRM 51-10-02, ITEM 9, AND SRM 51-40-02.SDR IPXA2025110562627Fairing · crackedAFT FAIRING 485AL HAS A CRACK AT AFT I/B SIDE. PERFORMED WELDING AT CRACKED AREA AT AFT FAIRING 485AL AT AFT I/B SIDE. IAW SRM 54-55-51 AMS 4921 RED. VERIFIED PERFORED WELDING AT CRACKED AREA AT AFT FAIRING 485AL AT AFT I/B SIDE. IAW SRM 54-55-51 AMS 4921.SDR SWAA2025111328440Support Angle · cracked#1 ENGINE I/B FAN COWL OIL ACCESS DOOR 414AR INNER SUPPORT ANGLE CRACKED. REMOVED AND REPLACED INNER SUPPORT ANGLE PER SRM 51-40-02.SDR CALA2025102310431Fitting · crackedNR 1 PYLON AFT TRAILING EDGE FAIRING O/B FITTING CRACKED. REMOVED AND REPLACED NR 1 PYLON T/E FAIRING IAW SRM 51-40-02 AND DWG 313A2700 REV-.SDR AALA202510206602Panel · detachedAIRCRAFT WAS GROUNDED: FLIGHT CREW REPORTED THAT THE RIGHT ENGINE UPPER PYLON PANEL TO ENGINE FLEXIBLE SEAL / PANEL DETACHED IN FLIGHT AND IS MISSING. MAINTENANCE INSTALLED PANEL PER AMM 54-57-22.SDR IXXA20251008001Angle · cracked#2 PYLON INTERNAL I/B UPPER ANGLE CRACKED, SEEN THRU ACCESS HOLE 446AL..SDR IPXA2025103099591Web · crackedNR 1 PYLON RIB 3 UPPER WEB CRACKED. JP-110. INSTALLED PYLON #1 SUPPORT OF THE PRESSURE RELIEF DOOR, IAW-A300-AMM 54-52-62/401 ITEM (4).SDR SWAA2025100620748Stiffener · damagedNR 2 ENGINE AFT STRUT FAIRING STIFFENER HAS 4 EACH ELONGATED HOLES FORWARD SIDE. REAMED HOLES TO .328 AND INSTALLED OVERSIZED FATSENERS IAW EA 25-154-02693 REFERENCE TASK TTG8Q015HNDM.SDR CALA2025100609638Plate · crackedNR 2 ENGINE, UPPER STRUT GAP PANEL LE CRACKED. REMOVED, FABRICATED AND REPLACED GAP PANEL SKIN IAW SRM 51-40-02 AND PER PRODUCTION CONTROL TRAVELER T25/1832479 SDR 200 4.SDR R612025F00004Plate · chafed#2 ENGINE OUTBOARD T/R CENTER THERMAL BLANKET CHAFE PLATE CHAFED.REMOVED DAMAGED CHAFE PLATE, FABRICATE REPAIR PATCH REF.NO. REPUBLIC AIRWAYS 170EA--78-31-0004MR_1 REV 2.SDR R61A2025101900471Plate · chafed#1 ENGINE INBOARD T/R CENTER THERMAL BLANKET CHAFE PLATE CHAFED.REMOVED DAMAGED CHAFE PLATE, FABRICATE REPAIR PATCH.REF.NO.REPUBLIC AIRWAYS 170EA-78-31-0004MR_1 REV 2.SDR SWAA2025100619024Angle · missingMISSING TWO ANGLES SUPPORT ON IDG ACCESS PANEL OUTBOARD FAN COWL ENG 1. INSTALLED TWO ANGLES SUPPORT AND FASTENERS ON IDG ACCESS PANEL OUTBOARD FAN COWL ENGINE 1 IAW SRM 51-40-02 AND CMM 71-13-30 FIGURE 2 SHEET 6 DETAIL P.SDR REXA2026052800850Rub Strip · wornOUT OF SCOPE': WEAR ON RUB STRIPS OF LOWER AND UPPER FORWARD CORE COWL AT RH ENGINE/LH ENGINE WEAR ON RUB STRIPS OF LOWER AND UPPER FORWARD CORE COWL AT RH ENGINE AND UPPER FORWARD CORE COWL LH ENGINE WERE REPLACED PER CRJ-900 SRM 54-23-00-201-006-A01, RUB STSDR REXA2026052800849Rub Strip · wornOUT OF SCOPE': WEAR ON RUB STRIPS OF LOWER AND UPPER FORWARD CORE COWL AT RH ENGINE/LH ENGINE WEAR ON RUB STRIPS OF LOWER AND UPPER FORWARD CORE COWL AT RH ENGINE AND UPPER FORWARD CORE COWL LH ENGINE WERE REPLACED PER CRJ-900 SRM 54-23-00-201-006-A01, RUB STRSDR AALA202510083644Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND PYLON SPIGOT FITTING RECEPTACLE BETWEEN PYLON RIBS 4 AND 5. REPLACED SPIGOT FITTING PER SRM 54-51-12-300-001SDR AALA202510084972Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT HAND PYLON SPIGOT FITTING RECEPTACLE BETWEEN PYLON RIBS 4 AND 5. REPLACED SPIGOT FITTING PER SRM 54-51-12-300-001.SDR AALA202510202607Fairing · corrodedAIRCRAFT IN BASE MAINTENANCE: #2 ENGINE AFT STRUT FAIRING TRAILING EDGE ASSEMBLY HAS CORROSION ON INBOARD SIDE. REPLACED TRAILING TRAILING EDGE ASSEMBLY REPLACED PER AARD 51-00-05-1.SDR SWAA2025100611311Web · crackedCRACK WEB ON OUTBOART FAN COWL ENGINE 2. REPLACED WEB LOCATED ON OUTBOARD FAN COWL OF ENGINE 2 IAW CMM 71-13-30, PAGE 10088, FIGURE 3, SHEET 1, DETAIL P, TABLE OF PAGE 10105, AND SRM 51-40-02-0G-0. MEASUREMENTS OF CRACK IS: 1.025 INCH.SDR VNAA202508280042Lug · gougedRIGHT UPPER C-DUCT INBOARD HINGE BEAM LUGS HAVE GOUGE / CHAFE DAMAGE. PERFORMED REPAIR BY COMPLYING WITH MHIRJ REO 670-54-22-114 REV: -- DATED: 2025-07-01- REPAIR FOR DAMAGED BOLT HOLE AND BLENDED CHAFE DAMAGE TO RH UPPER THRUST REVERSER HINGE BEAM LUGS. RE
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