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 VNAA202504020020Rub Strip · worn"WEAR FOUND ON UPPER/LOWER AFT EDGE RUB STRIP OF FWD CORE COWL AT RH ENGINE. UPPER/LOWER AFT EDGE RUB STRIP OF FWD CORE COWL AT RH ENGINE WERE REPLACED PER CRJ900 SRM 54-23-00-201-006-A01"SDR SWAA2025041419414Bracket · cracked040-001 BRACKET ON AFT SIDE OF # 1 ENGINE O/B COWL IS WORN AND CRACKED. HAS STREAMER ATTACHED.<[01] REMOVED WORN AND CRACKED BRACKET ON AFT SIDE OF #1 ENG O/B COWL AND REPLACED WITH NEW BRACKET; PN 314-2264-7 ATAG A307566; IAW SRM 51-40-02-0G-0 AND CMM 71-13-3SDR SWAA2025042408271Door · cracked#1 ENGINE INBOARD FAN COWL WEB AFT OF OIL SERVICE DOOR IS CRACKED. (MARKED) <[01] #1 ENGINE INBOARD FAN COWL REPLACED ON TTG8Q00S5GXN.; [02] INSPECTED WORK PERFORMED.SDR SWAA2025042408272Door · cracked#2 ENGINE OUTBOARD FAN COWL; WEB AFT OF OIL SERVICE DOOR IS CRACKED. (MARKED) <[01] REMOVED AND REPLACED #2 ENGINE OUTBOARD FAN COWL ON TTG8Q00S5GXN.SDR IXXA20250329001Bracket · cracked#1 PYLON UNDER DOOR #437BL HYDRAULIC VENT LINE SUPPORT BRACKET IS CRACK.SDR HALA20250317018Fairing · cracked2 1/2 INCH CRACK ON AFT SECTION OF R/H PYLON LOWER FAIRING. REPAIRED PER E105-373018-INISDR HALA20250317017Fairing · cracked2 INCH CRACK ON AFT SECTION OF L/H PYLON LOWER FAIRING. REPAIRED PER E105-373016-INI.SDR DALA2025031501994Fitting · corrodedSHIP 3276 DISC: CORROSION SPIGOT FITTING RECEPTACLE BORE ON LH PYLON. C/A: REPLACED LOWER FITTING SPIGOT ON LH PYLON AS PER A320 SRM 54-51- 12-300-001 AND PERFORMED DETAIL VISUAL INSPECTION ON AREA AND NOTFOUND ADDITIONAL DAMAGE AS PER AIRBUS NTM 51-90-00, ANDSDR SWAA2025041404586Stiffener · crackedPANEL 414 COWL ASSY - FAN - #1 ENGINE INBOARD - STIFFENER AT OIL SERVICE DOOR CRACKED<[01] FAN COWL TO BE REPLACED ON TTG8Q00S5HJNSDR IXXA20250411001Angle · cracked#2 PYLON INBD ACCESS HYDRAULIC BAY AFT OTBD STRUCTURE CLIP CRACKED. REF HAECO WO 320011 NON ROUTINE 34843SDR AALA202503204834Fitting · 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.SDR SWIA202507210219Web · crackedLEFT PYLON SS WEB HAS MULTIPLE CRACKS RADIATING FROM AROUND THE FITTING FOR THE ENGINE DRIVEN PUMP PRESSURE LINE, UNDER PANEL 281AZ. (MARKED) (C-CHECK RO 07/18/2025)REMOVED AND INSTALLED NEW FIREWALL WEB ON LH ENGINE PYLON BETWEEN FS 1069 AND FS 1088 PER REF SDR SWIA20250428210Stand Off · crackedR/H UPPER TRANSCOWL INBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 04/26/2025)INSTALLED NEW R/H UPPER TRANSCOWL I/B "A" BRACKET (PN CN624-2082-201) REF REO# 670-54-21-971, REV B, DATED 11/28/23. COMPLIED FULLY W/SKYCARD 51-900-1002-SKY. SEE CONTINUATION SHESDR YENA2025021100150Plate · wornDURING HEAVY MAINTENANCE: WEAR RIB 8 REINFORCING PLATE ON LH PYLON; REF AEROMAN WO 2025 25/1 NR 2025-76346 REPLACEMENT PYLON MOUNTING PLATE LOC SKIN LH WING IAW A320 SRM 57-21-11-300-005 AND A320 SRM 51-72-11-911-001 THIS REPAIR IS CATEGORY (A) NOT REQUIRED MOSDR AALA202502105871Shim · migratedAIRCRAFT IN BASE MAINTENANCE: NUMBER 2 PYLON AFT ENGINE MOUNT BULKHEAD ASSEMBLY TO CHORD SHIM IS MIGRATED. TRIM THE MIGRATED SHIM. PER D6-37239 737 NDT MANUAL, PART 6, CHAPTER 51-00-00, PROCEDURE 2 OR 19.SDR IPXA2025022192637Filler · corrodedNR 1 PYLON HAS SURFACE CORROSION AROUND FASTENER HOLES FOR PANEL 433CL. DOT 142-22.REMOVED CRACKED AND CORRODED STRAP (OUT OF LIMITS WITH EXFOLIATED CORROSION VISIBLE IAW SRM 51-10-08) IAW B757-200-51-40-02-OG.SDR SWI2025F01016Stiffener · shearedR/H LWR TRANSCOWL Z STIFFENER RIVETS ARE SHEARED (C-CHECK RO 07/18/2025)ON R/H LOWER TRANSCOWL, 3 EA. FASTENER HOLES COMMON TO ZED STIFFENER P/N CN624-2038-203 ON INNER SKIN FOUND TO BE CRACK FREE WITH NO DAMAGE NOTED. ENGINEERING REQUIRED FOR ALTERNATE METHSDR CALA2025020400288Intercostal · crackedSUPPORT TASK - NO.2 PYLON PNL #443CL CUTOUT INNER UPR INTERCOSTAL FOUND CRACK. NO.2 PYLON PNL NO.443CL CUTOUT INNER UPPER INTERCOSTAL REPLACED AS PER SRM 51-10-02 AND FASTENER INSTALLED AS PER SRM 51-10-02.SDR DALA2025013100747Fairing · crackedSHIP 3146 #1 PYLON OUTBOARD LATERAL FAIRING HAS A 1" CRACK LOWER AFT CORNER. CORRECTIVE ACTION: COMPLIED WITH ERA 624005-14. (0787395)SDR 2025F00026Rub Strip · gougedRUB PLATE GOUGED OUTBD FAN COWL PN 224-2202-507 2 ENGINESDR 2025FA0000056Shim · migratedFOUN SHIM MIGRATION, ENGINE #2 STRUT LOWER PANEL WING, NAC STA 354.090, NAC BL 1.792, NAC WL 160.140SDR SWAA2025021089767Fairing · crackedCR VB.... #2 PYLON AFT FAIRING HAS A CRACKED FRAME ON FWD SIDE<[01] REMOVED AND REPLACED PYLON #2 AFT FAIRING IAW BAC DWG 313A2752 REV J AND B737-800 SRM 51-40-02;[02] VERIFIED: REMOVED AND REPLACED PYLON #2 AFT FAIRING IAW BAC DWG 313A2752 REV J AND B737-800 SDR UIEA2025011600068Strip · corrodedENG 1, RH CORE COWL, UPPER STRIP WITH CORROSION. L: 2.500 IN, W: 1.000 IN.(<P>THE CORROSION METAL STRIP WAS REMOVED, THE NEW METAL STRIP WAS DRILLED AND WAS INSTALLED CORRECTLY. SRM 51-40-02-0G-0 REV 127 15DEC24 AND SRM 51-10-02-0G-0 PAR 9. LEVEL 1. NO FURTHERSDR UIEA2025011800086Support Angle · crackedBROKEN ENG 2, ACCESS PANEL 447DB, ANGLE SUPPORT WITH CRACK.(<P>THE BROKEN SUPPORT ANGLE WAS REMOVED, THE AREA WAS CLEANED, THE NEW SUPPORT ANGLE WAS DRILLED AND INSTALLED CORRECTLY. THE SUPPORT ANGLE WAS REPLACED WITH A NEW ONE. DWG 313T3360 SRM 51-40-02-OG-O SDR DALA2025012300563Shim · crackedSHIP 3422 #2 ENGINE NOSE COWL 12:00 POSITION TILTED SHIM IS CRACKED IN SEVERAL PLACES. CORRECTIVE ACTION: COMPLIED WITH ERA 623670-14 REV O. (0773751)SDR SWAA2025012387880Support · cracked#1 ENGINE AFT STRUT FAIRING FWD SUPPORT CRACKED AT 2ND FROM UPPER FASTENER<[01] REPAIRED #1 ENGINE AFT STRUT FAIRING FWD SUPPORT PER EA M-23-154-01884; SRM 51-10-02;[02] EDIT TO CHANGE STEP 3 TO 'YES'SDR IXXA20250122009Support · crackedNO. 1 ENG OTBD CORE COWL UPPER FAIRING AFT SEAL SUPPORT STRUCTURE CRACKED.SDR IXXA20250116004Tie Clip · crackedNO. 2 ENG PYLON AFT FAIRING ASSY NAC STA 377 INBD INTERNAL CLIP IS CRACKED.SDR IPXA2025012821114Plate · cracked#2 ENG PYLON TOP AREA RH RIB 3 LATERAL PANEL SKIN CORNER CRACKED-DOT 139/18-MR/139. NSTALLED PLATE AT #2 ENG PYLON TOP AREA RH RIB 3 LATERAL PANEL SKIN CORNER IAW A300-600 SRM 51-40-21. FASTENER PN:NAS1200M4-7, BN:0004171072, PN:MS21060-3, BN:0004201914, PN:CCSDR CALA2025012100150Fitting · corrodedLEFT PYLON SPIGOT BEARING RETAINER PLATE,RECEPTACLE FITTING AND SLEEVE HAVE CORROSION. . REMOVED & REPLACED #1 PYLON SPIGOT BEARING FITTING IAW A320 SRM 54-51-12-300-002. REPLACED SPIGOT SLEEVE IAW AMM 57-26-12-400-00 2-A.SDR CALA2025012100147Fitting · corrodedRIGHT PYON SPIGOT BEARING RECEPTACIE FITTING AND SLEEVE HAVE CORROSION. REMOVED & REPLACED #2 PYLON SPIGOT FITTING IAW A320 SRM 54-51-12 -300-002. REPLACED SPIGOT SLEEVE IAW AMM 57-26-12-400-002-A.SDR IPXA2025013155554Bracket · crackedNR 1 ENG PYLON NAC STA.149.5 FRAME I/B HAS ELONGATED HOLES AND 0,5 CRACK. EA-62. INSTALLED NEW FRAME ANGLE ON #1 PYLON. IAW SRM 51-40-02-0G. INSTALLED NEW BRACKET ON FRAME ANGLE OF PYLON #1. IAW SRM 51-40-02-0G.SDR IPXA2025020465996Angle · crackedNR 2 ENG STRAP AT NAC STA. 149.5 HAS CRACK AT HI-LOCK.DOT 69-003. EL-69. INSTALLED FRAME ANGLE IAW SRM 51-40-02-0G. AUDIT COMPLETE.SDR IPXA2025020465427Bracket · crackedFAULT:STR-Z400 #1 ENG PYLON HYD LINE BRACKET DAMAGED AT STRAP.NAC STA 149.5. DOT 69-001. EL-69. INSTALLED NEW FRAME ANGLE ON #1 PYLON. IAW SRM 51-40-02-0G. INSTALLED NEW BRACKET ON FRAME ANGLE OF PYLON #1. IAW SRM 51-40-02-0G.SDR REXA2025020500148Angle · crackedCRACK ON ANGLE SUPPORT OF LEFT PYLON ON FS1031 ANGLE SUPPORT OF LEFT PYLON ON FS1031 WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-- 42-21-001-001-A01SDR DALA2024123012079Web · gougedSHIP 3145 GOUGE WEB LOC. UPPER AREA BTW RIB08 TO RIB09 ON RH PYLON. CORRECTIVE ACTION: REPAIRED PER ER/A 622411-14. (0731701)SDR DALA2024122712039Support Web · crackedSHIP 3308 RH PYLON LAPF NO.2 SUPPORT WEB. CORRECTIVE ACTION: STOP DRILL AT THE CRACK END AND APPLY DOUBLER REPAIR WITH MATERIAL 2024-0-0.063" AS PER PW CMM 54-56-11. (0726441)SDR DALA2024122311924Web · crackedSHIP 3308 LH PYLON LAPF NO.1 SUPPORT WEB CRACK. CORRECTIVE ACTION: COMPLIED WITH ERA 541163-14. (0724567)SDR AALA202412249120Bracket · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK BRACKET INBOARD AND OUTBOARD SIDE AFT TORQUE BOX AT LT PYLON. REPLACED BRACKET LOCATED AT INBOARD AND OUTBOARD SIDE AFT TORQUE BOX AT LEFT PYLON. PER B777-200 SRM 51-40-02-0G AND DWG 311W5531.SDR SWAA2024122374124Bracket · crackedPANEL 414 FAN COWL ASSY. #1 ENGINE INBOARD: OIL DOOR WIND DEFLECTOR BRACKET IS CRACKED. MARKED. PANEL 414 FAN COWL ASSY. #1 ENGINE INBOARD: OIL DOOR WIND DEFLECTOR BRACKET IS CRACKED. MARKED.<[01] #1 ENGINE I/B (R/H) FAN COWL WAS REPLACED ON TASK CARD TTG8Q00SSDR JJBA20241209013Bracket · crackedON RH ENG PYLON BLEED AIR PRECCOLER REMOVED, FWD STRUCTURAL BRACKET FOUND CRACKED AND BENT. ON RH ENG PYLON BLEED AIR PRECOOLER FWD STRUCTURE BRACKET REMOVED AND REPLACEDSDR IPXA2024113024730Web · cracked#1 PYLON LOWER AFT AREA WEB P/N A54515063206 IS CRACKED. INSTALLED NEW WEB AT PYLON #1 LOWER IAW A300-600, SRM 51-40-21, WITH FASTENER: RIVET SOLID P/N:MS2615-4M5, BATCH# 0004090312, CR3523-4-04, BATCH# 0004176917, IAD 41R54610328 AND SRM 54-54-11 AND SRM 51-SDR IPXA2024112724730Web · crackedNR 1 PYLON LOWER AFT AREA WEB P/N A54515063206 IS CRACKED APPROVED.SDR CALA2024112702966Fairing · crackedNO.2 ENGINE AFT STRUT FAIRING CRACKED AT T/E INNER SURFACE REF AAR N/R 9917539 REMOVED AND REPLACED NO.2 ENG AFT STRUT FAIRING SKIN PANELS (T/E ASSY) PART NO.313A2752-2 AND 313A2752-3 REF B737 SRM 51-40-02-0G-0 AND DWG 313A2752 WORK ACCOMPLISHED BY V898225SDR SWAA2025010769892Shield · cracked#1 ENG I/B FAN COWL OIL ACCESS DOOR SHIELD CRACKED.<[01] REMOVED AND REPLACED #1 ENG I/B FAN COWL OIL DOOR SHIELD IAW SRM 51-40-02-0G-0 STEP 4 AND 5.;[02] VERIFIED CORRECTIVE ACTION #1SDR COEA2024112234757Panel · crackedWO 262870 NR 5 MINOR REPAIR/DISCREPANCY: L/H ENGINE INBOARD PLENUM PANEL CRACKED IN TWO LOCATIONS. CORRECTIVE ACTION: REPLACED L/H ENGINE INBOARD PLENUM PANEL IAW C408 MM 54-20-00.SDR SWAA2024121361747Channel · cracked#1 ENGINE I/B COWL; INTERCOSTAL CHANNEL CRACKED AFT OF ENGINE OIL ACCESS DOOR.<[01] #1 I/B FAN COWL REPLACED ON 7111-E-17063-NG (REP - RIGHT-HALF FAN COWL ASSEMBLY) [TTG8Q00S5HJF] LINE# 19;[02] C/W INSPECTIONSDR IXXA2024111901Support Web · cracked#1 PYLON BRACKET HAS SUPPORTING WEB CRACKED AROUND TIA DUCT SUPPORTSDR SWAA2024121060674Angle · elongatedELONGATED HOLE SUPPORT ANGLE OUTBOARD FAN COWL LOC. INTERNAL AREA ACCESS DOOR 424AR AT ENGINE 2 2024-715113<[01] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED OUTBOARD FAN COWL LOC. INTERNAL AREA ACCESS DOOR 424AR AT ENGINE 2 I.A.W B737-700 SRM 51-10-02; SRM 51SDR SWAA2024112160351Shield · crackedREJECT: #1 ENGINE I/B FAN COWL OIL ACCESS DOOR SHIELD; CRACK STILL EXISTS.<[01] REPLACED #1 ENGINE IB FAN COWL OIL ACCESS DOOR SHIELD AND OPENED/CLOSED IB FAN COWL PER AMM 71-11-02; SRM 51-40-02.;[02] VERIFIED MEASUREMENTS;[03] VERIFIED CORRECTIVE ACTION ITEM
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