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 SWAA2023041314334Structure · cracked#1 ENGINE I/B FAN COWL OIL ACCESS DOOR SHEILD STRUCTURE IS CRACKED<[01] REPLACED SHEILD STRUCTURE ON #1 ENGINE I/B FAN COWL OIL ACCESS DOOR IAW SRM 51-40-02-0G-0 PAR.4 AND 5;[02] REMOVED AND REPLACED SHEILD STRUCTURE ON #1 ENGINE I/B FAN COWL OIL ACCESS DOOR ISDR SWAA2023040711703Web · brokenBROKEN WEB OUTBOARD FAN COWL ON RT ENGINE 2023-142964<[01] REPLACED WEB AND FASTENERS LOCATED OUTBOARD FAN COWL ON RT ENGINE; IAW BOEING 737-700 SRM 51-40-02 AND BOEING 737-700 CMM 71-13-30 FIGURE 3 (SHEET 5 OF 8).;[02] REPLACED WEB AND FASTENERS LOCATED OUTBOSDR SWAA2023032010758Rib · crackedNO-1 ENG INB FAN COWL INT.INTERCOSTAL RIB CRACKED AT EDGE AT ENG OIL SERVICE DOOR AREA MKD DOT<[01] REMOVED AND REPLACED INT; INTERCOSTAL RIB AT EDGE ON #1 ENGINE I/B FAN COWL AT ENGINE OIL SERVICE DOOR AREA. PER SRM 51-40-02-0G-O;[02] VERIFIED REPLACEMENTSDR SWAA2023031505672Bracket · cracked#2 ENGINE; O/B FAN COWL; ENG. OIL ACCESS DOOR; INTERNAL SUPPORT BRACKET IS CRACKED.<[01] REMOVED OLD FAN COWL AND INSTALLED NEW FAN COWL PER AMM 71-11-02.;[02] VERIFIED REMOVED OLD FAN COWL AND INSTALLED NEW FAN COWL PER AMM 71-11-02.SDR SWAA2023021603436Stiffener · elongated#1 ENG AFT STRUT FAIRING; HORIZONTAL STIFFENER OUTBOARD LOWER HOLE IS ELONGATED #1 ENG AFT STRUT FAIRING HORIZONTAL STIFFENER OUTBOARD LOWER HOLE IS ELONGATED<[01] COMPLIED WITH EA- 23-154-00539SDR SWAA2023031000744Shield · broken#2 ENGINE O/B FAN COWL INNER SHIELD IS BROKEN IN BEND RADIUS.<[01] REMOVED AND REPLACED #2 ENGINE O/B FAN COWL INNER SHIELD IAW SRM 51-40-02-0G-0 AND CMM 71-13-30;[02] VERIFIED CORRECTIVE ACTION 1.SDR SWAA2023021000316Wedge · cracked#2 ENGINE AFT PYLON TE WEDGE CRACKED ON FWD WEB MEASURING 1 AND EXTENDING BEYOND RADIUS<[01] ACCOMPLISHED EA 23-154-00430.SDR SWAA2023020697716Fairing · cracked#2 PYLON AFT STRUT FAIRING CRACKED<[01] COMPLIED WITH EA-GENERAL 23-154-00375.SDR SWAA2023022897766Shield · crackedNO-1 ENG I/B FAN COWL INTERNAL INTERCOSTAL CRACKED @ UPPER EDGE AFT OF ENG SERVICE OIL ACCESS DOOR MKD DOT<[01] REMOVED 1EA DAMAGED SHIELD FROM NO-1 ENG I/B FAN COWL PER SRM 51-40-02;[02] VERIFIED STEP 1;[03] LOCATED AND DRILL 1E/A SHIEL <BR><BR><BR><BR><BR>LOSDR SWAA2023022897765Shield · crackedNO 2 ENG O/B FAN COWL INTERNALINTERCOSTAL CRACKED @ UPPER EDGE AFT ENG SERVICE OIL ACCESS DOOR MKD DOT<[01] REMOVED 1 OFF E/A DAMAGED SHIEL FROM NO2ENG O/B FAN COWL PER SRM 51-40-02;[02] LOCATED AND DRILL NEW SHIELD PER SRM 51-40-05;[03] CORRECTION: REMOVED 1 SDR SWAA2023031396332Web · crackedPANEL 424 COWL ASSY - FAN - #2 ENGINE OUTBOARD OIL SERVICE DOOR OPENING; THE AFT REINFORCEMENT WEB IS CRACKED. (MARKED)<[01] REMOVED AND REPLACED REINFORCEMENT WEB PER SRM 51-40-02.;[02] OKSDR SWAA2023012795333Fairing · cracked#1 ENGINE AFT STRUT FAIRING AFT FITTING CRACKED<[01] MEASUREMENT FIELD COMPLETED.;[02] INSTALLED #1 ENG AFT STRUT FAIRING END CAP IAW SRM 51-40-02.;[03] COMPLIED WITH AFT STRUT FAIRING FITTING ASSY REMOVAL AND REPLACEMENT PER SRM 51-40-02. REMOVED AND REINSTALSDR V0XD2022300002Angle · crackedRH ENGINE LOWER COWLING HAS A CRACKED INTERNAL RIB. CORRECTIVE ACTION: CUT OUT DAMAGED RIB Z ANGLE SECTION, FABRICATED REPAIR PARTS AND INSTALLED REPAIR PARTS IAW EMB 145 SRM 54-10-03. SEE AVMAX W/O: 81031 W/C: 4122SDR UIEA2023011800057Support Beam · crackedCRACK EVIDENCE OF FAN COWL SUPPORT BEAM FITTING OF LH ENGINE / STRUT(<P>FAN COWL SUPPORT BEAM FITTING P/N 311T2114-7 WAS REPLACED PER DRAWING TRE6754167 AND IPC 54-50-53-02 REQUIREMENTS </P>)SDR SWAA2023030694126Flange · broken#1 ENGINE PYLON OUTBOARD AFT FIRE SEAL CLIP HORIZONTAL FLANGE IS BROKEN<[01] REMOVED #1 ENGINE PYLON O/B AFT FIRE SEAL CLIP AND FIRE SEAL BRACKET COMMON TO THE CLIP IAW SRM 51-40-02-0G-0.;[02] CERTIFIED ACTION 1;[03] UPDATED PARTS REMOVED / INSTALLED;[04] INSTSDR SWAA2023012593938Fairing · crackedCRACK; #1 ENGINE PYLON AFT STRUT SUPPORT FAIRING ASSB.<[01] REMOVED AND REPLACED #1 ENGINE PYLON AFT. STRUT SUPPORT FAIRING ASSB.PER SRM 51-40-02.SDR IXXA2023012102Channel · crackedPYLON WEB FRAME CHANNEL CRACKEDSDR SWAA2023012494623Bracket · brokenNO. 1 ENGINE R/H FAN COWLING LOWER GUIDE BRACKET ASSEMBLY IS BROKEN.<[01] REPLACED LOWER GUIDE BRACKET ASSEMBLY PER POWER PLANT BUILD UP MANUAL 71-00-02.SDR 2023FA0000062Firewall · crackedLEFT ENGINE FIREWALL FOUND CRACKED DURING ENGINE CHANGE.SDR SWAA2023012391978Web · cracked#2 ENGINE AFT STRUT FAIRING TE WEDGE WEBB CRACKED. TOTAL CRACK LENGTH 1.6 EXTENDS .6 BEYOND RADIUS<[01] C/W EA 23-154-00165SDR SWAA2023021689405Bracket · broken#2 ENGINE PYLON INBOARD AFT FIRE WALL BRACKET HORIZONTAL FLANGE IS BROKEN<[01] REMOVED #2 ENGINE PYLON INBOARD AFT FIRE WALL BRACKET IAW SRM 51-40-02-0G-0 STEP 5.;[02] #2 ENGINE PYLON INSTALLED SERVICEABLE INBOARD AFT FIRE WALL BRACKET IAW SRM 51-40-02-0G-0 STSDR IPXA2023012090080Web · crackedINSPECTION TYPE:1C, PYLON PANEL 413BL INTERNAL WEB CRACKED AT CORNER. FABRICATED DOUBLER IAW SRM 54-52-51 AND INSTALLED IAW SRM 51-40-21.SDR SWAA2023021087162Panel · crackedCRACK HOLES ACCESS PANEL 561BB TRAILING EDGE AT LT WING 2022-708471<[01] TOOL USED: CALIPER P/N: 500-197-30; S/N: A21041924; DUE DATE: 24-SEP-23.;[02] TOOL USED HOT BONDER PN: HCS9200B-AV; SN: 18185781; DUE DATE: 16/JAN 23.;[03] TOOL USED. SCALE PN: SPX621; SNSDR SWAA2023020885195Bracket · brokenBROKEN BRACKET LOWER STRUT BOX INBOARD AND OUTBOARD SIDE AT RT PYLON (2 EA) 2022-707341<[01] REPLACED BRACKET LOWER STRUT BOX INBOARD AND OUTBOARD SIDE AT RT PYLON (2 EA) IAW B737-700 SRM 51-40-02 AND DRAWING 311A2683 REV -;[02] TASK COMPLETEDSDR CALA2022122103458Panel · missingENG 2 PANEL 443JL(PRECOOLER THERMAL SWITCH) MISSING. PDA LOGPAGE TO BE PROCESSED AS PER GMM 02-30-95. LIM MX WORKED ITEM. ENG 2 PANEL 443JL(PRECOOLER THERMAL SWITCH) MISSING. SECURED BLA 6 TOTAL AIRFRAME FLIGHT CYCLES. THIS IS A 2 CYCLE ECRA 5450-0279 NKING PLSDR AALA2023013101827Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING PYLON SPIGOT FITTING RECEPTACLE BETWEEN PYLON STATION 495 AND 679, BETWEEN PYLON RIBS 4 AND 5. MAINTENANCE REPLACED THE PYLON SPIGOT FITTING PER SRM 54-51-12.SDR SWAA2023013080806Support Angle · crackedCRACK INBOARD FAN COWL SUPPORT ANGLE AFT LOWER POSITION ON ENGINE 1 2022-691670<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600D; S/N: 210138003; DUE DATE: 22-FEB-23.;[02] PERFORMED REPAIR LOCATED INBOARD FAN COWL SUPPORT ANGLE AFT LOWER POSITION OSDR SWAA2022121380681Fairing · delaminatedNR 1 ENGINE PYLON STRUT FAIRING PANEL DELAMINATED ON THE OTBD AFT CORNER. REMOVED AND REPLACED THE STRUT FWD FAIRING IAW AMM 54-52-01.SDR ASAA2022120941103Latch · looseIN FLIGHT PAX REPORTED #1 ENGINE LATCH ON TOP OF PYLON WAS POSSIBLY LOOSE. CREW COULD NOT VERIFY STATUS. GROUNDED - YES. DIVERSION - PERFORMED LATCH CLOSING FORCE FOUND TO BE LESS THEN REQUIRED (12LB). REF B737-800 AMM TASK 54-52-01-410-801. REMOVED FWD ENG #1SDR SWAA2022120176659Fairing · damagedFOUND 2 LOCK FASTENER HOLES ON THE LT STRUT FAIRING ELONGATED ON THE LT SIDE. REPAIRED THE DAMAGEIAW EA 22-154-03528.SDR FDEA202211292863Fairing · cracked#3 ENGINE PYLON HAS CRACKED PANEL,LOCATED AT LOWER SURFACE AFT OF EXUAST NOZZLE AND FORWARD OF V PANEL. REPAIRED PYLON PANEL ASREQUIRED IAW SRM 54-00-01 FIG. 2B SHEET 2.SDR SWAA2022121276182Web · crackedNO-2 ENGINE. OUB FAN COWL INTERIOR INTERCOSTAL WEB CRACKED @ ENG OIL SERVICE DOOR MKD / [01] REMOVED AND REPLACED NO-2 ENGINE. OUB FAN COWL INTERIOR INTERCOSTAL WEB @ ENG OIL SERVICE DOOR IRW SRM 51-40-02-0G-0;[02] VERIFIED STEP 1SDR SWAA2022121276183Web · crackedNO-1 ENG INB FAN COWL INT INTERCOSTAL WEB CRACKED AREA OF ENG OIL SERVICE ACCESS PANEL MKD DOT / [01] REMOVED AND REPLACED NO-1 ENG INB FAN COWL INT INTERCOSTAL WEB; AREA OF ENG OIL SERVICE ACCESS PANEL IRW SRM 51-40-02-OG-0;[02] VERIFIED STEP 1SDR SWAA2022112975540Fitting · damaged#1 ENGINE NACELLE SUPPORT INBOARD FITTING I/B SIDE HOLE ELONGATED. COMPLIED WITH 22-157-03484-WIP1, COMPLIED WITH 22-157-03484-WIP2, COMPLIED WITH 2-157-03484-WIP1, COMPLIED WITH 22-157-03484-WIP2.SDR R61A2023010400006Angle · corrodedCRACK FOUND ON NR 2 ENG AFT FIXED FAIRING HEAT SHIELD NR 5 INBD ANGLE. REPLACED THE ANGLE IAW SRM 51-42-01.SDR SWAA2022121375150Web · crackedCRACKED WEB ON INBOARD FAN COWL, NR 1 ENGINE. REPLACED THE WEB IAW SRM 51-40-02-0G-0.SDR IXXA2022112702Fairing · cracked#2 ENG PYLON TO WING FAIRING 447DB HAS A CRACKED BULKHEAD. REF FAS WO FS220060 NON ROUTINE 00174SDR SWAA2022121374635Web · crackedCRACK WEB, OUTBOARD FAN COWL ON NR 2 ENGINE. REPLACED THE WEB IAW SRM 51-40-02-0G-0.SDR SWAA2022120773169Web · crackedCRACKED WEB OUTBOARD FAN COWL ON NR 2 ENGINE. REPLACED WEB IAW SRM 51-10-02, ITEM 9, AND CMM 71-13-30 FIGURE 3,SDR IXXA2022111602Fitting · damagedUPON REMOVAL OF # 2 PYLON INBOARD BATHTUB FITTING FOUND TO BE DAMAGED.SDR IXXA2022111601Channel · worn# 2 PYLON ANGLE CHANNEL COVER WORN SEVERAL AREAS.SDR SWAA2022121381126Web · crackedNR 2 ENGINE OTBD. FAN COWL, STRUCTURE BELOW HOLD OPEN ROD CRACKED. REMOVED AND REPLACED THE WEB IAW SRM 51-40-02.SDR SWAA2022120771250Intercostal · crackedCRACKED INTERCOSTAL AT OIL SERVICE DOOR OPENING, RIGHT OUTBOARD FAN COWL. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-40-02.SDR SWAA2022110367320Panel · crackedSUPPLEMENTAL INFORMATION: FOUND HALF INCH CRACK 5 INCHES FROM A FASTNER HOLE ON PANEL 434AR / [01] REPAIRED PANEL 434AR PER EA 22-154-03265;[02] APPLIED INTERIM REPAIR ON PANEL 434AR PER EA 22-154-03265SDR FDEA202211022715Attach Angle · cracked#2 PYLON AFT FAIRING O/B SIDE , FWD LOWER ATTACH CLIP IS CRACKED AT APPROX. NAC STA 206 REMOVED AND REPLACED CLIP AT #2 PYLON AFT FAIRING O/B SIDE , FWD LOWER AREA AT APPROX. NAC STA 206 IAW FEDEX EA : F-7120-T0371303 -P1SDR SWAA2022103165712Structure · crackedNO. 2 ENGINE STRUT AFT FAIRING STRUCTURE (PN: 313A2752-1) CRACKED. / [01] R&R NUMBER 2 ENG. STRUT FAIRING AFT STRUCTURE P/N 313A2752-1.<BR>PER SRM 51-10-02.;[02] RESTORED PROTECTIVE/DECORATIVE FINISH PER AMM 51-21-99.SDR FDEA202210282686Shim · corrodedNO. 2 ENGINE, INLET COWL, FWD PANEL LAND IS CORRODED BETWEEN 6 & 8 O'CLOCK POSITIONS REMOVED AND REPLACED 6 EA. SHIMS, NUMBER 2 ENGINE INLET COWL FWD LOWER LAND IAW BAC DWG 314N3010, REV. L AND B757 SRM 51-40-02-0G. CORROSION WAS FOUND TO BE ON PANEL LANSDR UIEA2022092101021Web · crackedLHW #2 PYLON O/B `D` FAIRING REAR WEB FOUND CRACK(<P>CRACK PREVIOUS WEB REPLACED AS PER RI NO: RI-57-41-15892 REV.A</P>)SDR SWAA2022103163749Structure · cracked#2 ENGINE STRUT AFT FAIRING STRUCTURE CRACK EXTENDS APPROXIMATELY .125' BEYOND THE RADIUS. / [01] FAULT RESOLVED ON ANOTHER FAULT REF TTG8Q00FPE1NSDR IPXA2022102587511Support · crackedINSPECTION TYPE:C, ENG #1 ARC WEB SUPPORT BETWEEN PRECOOLER AND BUTTERFLY PANELS HAVE CRACKS.INSTALLED ARC WEB IAW-AMM 54-52-61-0401
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