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 SWAA2024082616736Angle · cracked#2 ENGINE OIL ACCESS DOOR AFT SHIELD CRACKED<[01] REMOVED AND REPLACED ANGLE ON #2 ENGINE OIL ACCESS DOOR IAW SRM 51-40-02.;[02] VERIFIED MEASUREMENTSSDR SWAA2024082616737Shield · cracked#1 ENGINE OIL ACCESS DOOR AFT SHIELD CRACKED<[01] REMOVED AND REPLACED ANGLE ON #1 ENGINE OIL ACCESS DOOR IAW SRM 51-40-02.;[02] VERIFIED MEASUREMENTSSDR SWAA2024072515600Web · cracked#1 PYLON AFT WEDGE FWD WEB HAS A CRACK EXTENDING 1.6 INCHES FROM FWD WEB OVERLAP ACROSS RADIUS TO O/B FRAME.<[01] C/W EA 24-154-02004 ON #1 ENG PYLON AFT WEDGE FWD WEB.SDR SWAA2024072515601Web · cracked#2 PYLON AFT WEDGE FWD WEB HAS A CRACK EXTENDING 1 INCH FROM FWD WEB OVERLAP TO RADIUS.<[01] COMPLIED WITH EA M-23-154-01884 ON #2 ENGINE PYLON AFT STRUT SUPPORT FAIRINGSDR SWAA2024080514246Frame · crackedCRACK LOCATED AFT ZEE FRAME UPPER POSITION ON FAN COWL O/B AT ENGINE 1 2024-402203<[01] REPLACED AFT ZEE FRAME UPPER POSITION ON FAN COWL O/B AT ENGINE 1 IAW B737-800 SRM 51-40-02 AND GOODRICH AEROSTRUCTURES CMM 71-13-30 PAGE 10062.<BR>SEE INDIVIDUAL SIGN-OFF SDR SWAA2024082313794Bracket · elongatedELONGATED HOLE BRACKET ANGLE LOCATED OUTBOARD THRUST REVERSER AFT UPPER EDGE ON ENGINE 2 2024-443746<[01] REPLACED BRACKET ANGLE LOCATED OUTBOARD THRUST REVERSER AFT UPPER EDGE ON ENGINE 2 IAW B737-700 SRM 51-10-02 PARAGRAPH 9 AND SRM 51-40-02.;[02] TASK CARD SDR NACA2024070900003Angle · cracked"L" ANGLES CRACK ON RH NACELLE NAC.STA.278.52 AT WBL.204 REPAIRED CRACK IAW SRM 51-40-02SDR SWAA2024072509195Shield · cracked#1 ENGINE I/B FAN COWL OIL TANK ACCESS DOOR SHIELD CRACKED<[01] REMOVED AND REPLACED ACCESS DOOR SHIELD IAW SRM 51-40-02.;[02] PARTS REMOVED / INSTALLED;[03] REJECTION OF CORRECTIVE ACTION 1 AND STEP 1: 1EA BAD RIVET AT LOWER END OF #1 ENGINE I/B FAN COWL OIL SDR SWAA2024080507774Bracket · crackedCRACK SUPPORT BRACKET ON O/B FAN COWL ENGINE 1 2024-402146<[01] REPLACED SUPPORT BRACKET ON O/B FAN COWL ENGINE 1<BR>IAW B737-800 SRM 51-40-02 AND AND GOODRICH AEROSTRUCTURES CMM 71-13-30 PAGE 10050;[02] REPLACED SUPPORT BRACKET ON O/B FAN COWL ENGINE 1<BR>IAWSDR IXXA2024080403Beam · chafed#1 PYLON AFT FAIRING ASSY, INBD LATCH BEAM CHAFED EDGE DAMAGE DUE TO CONTACT WITH BROKEN HOLD OPEN RODSDR IPXA2024070896004Shield · bentPYLON NR 2 RIB 12 SHIELD PANEL EDGE BENT. FABRICATED, LOCATED AND DRILLED NEW #2 PYLON RIB 2 SHIELD PANEL ON TRAVELER# T24/1764214. TREATED AND PRIMED NEW SHIELD PANEL IAW SRM 51-21-10 VERIFIED JOB IN STEP #6. JOB COMPLETE REVIEWEDSDR SWI202408260775Bracket · bentL/H UPPER TRANSCOWL INBD "A" BRACKET STANDOFF IS BENT AND NOT SEATING PROPERLY (C-CHECK RO 8/24/2024) INSTALLED 1 EA. NEW INBD. STANDOFF P/N CN 624-2082-201 ON L/H UPPER TRANS COWL, REF. REO 670-54-21-971, REV. B. 2023-11-28. COMPLIED WITH STEPS 1-3, ASDR SWI202408260774Bracket · crackedL/H UPPER TRANSCOWL OTBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 8/24/2024) INSTALLED 1 EA. NEW OTBD. STANDOFF P/N CN 624-2082-201 ON L/H UPPER TRANS COWL, REF. REO 670-54-21-971, REV. B, 2023-11-28. COMPLIED WITH STEPS 1-3, AND COMPLIED WITH 51-90SDR SWAA2024061400310Shield · cracked#1 ENG I/B FAN COWL SHIELD; LOCATED ON FAN COWL INNER SURFACE JUST AFT OF THE OIL SERVICE DOOR OPENING; HAS A 1.3 CRACK ON THE UPPER O/B CORNER.<[01] REPAIRED PER EA 24-154-01593. STOP DRILLED CRACK AND APPLIED SPEED TAPE.SDR CALA2024061301791Bracket · crackedBRACKETS AT AFT UPPER SIDE OF LOWER SKIRT FAIRING WHERE THE STIN GER PANEL ATTACHES FOUND TO BE CRACKED #2 PYLON. REF AMES NR 170098-0600-0110 AND WORK SHEET 83 REMOVED AND REPLACED 2 BRACKET ON THE NO 2 PYLON AFT LOWER SKIRT FAIRING WITH NEWLY FABRICATED BRSDR SWAA2024060798832Cover · delaminated#1 ENGINE I/B PYLON HINGE BEAM FAIRING AERODYNAMIC SEAL COVER SECTION FLAPPING IN THE BREEZE #1 ENGINE HINGE BEAM FAIRING BLADE SEAL SAIL CLOTH COVER DELAMINATED/FRAYED TSR# 2024003859<[01] ACCOMPLISHED REPAIR PER EA 24-154-01540SDR CALA2024060501710Angle · crackedNR 1 PYLON AFT OB INTERNAL "L" ANGLE CRACKED AT MOST UPPER FASTENER,SDR HNAA2024070800533Gusset · corrodedE041241 RH UPPER ENGINE COWLING CENTER TRIANGLE GUSSET HAS CORROSION. REMOVED AND REPLACED RH UPPER ENGINE COWLING CENTER TRIANGLE GUSSET IAW EMB 145 SRM 51-40-02SDR IXXA2024053101Web · cracked#2 PYLON CLOSE OUT WEB CRACKEDSDR CALA2024053001647Angle · crackedGEN ITEM: EA 5700-03285 REV F OP 010 #2 PYLON OB AFT HYDRAULIC BAY "L" ANGLE IS CRACKEDSDR JJBA20240610011Bracket · crackedRH ENG PYLON PRECOOLER, FWD STRUCTURE BRACKET IS CRACKED. RH ENG PYLON PRECOOLER, FWD STRUCTURE BRACKET REMOVED FOR REPLACEMENT. RH ENG PYLON PRECOOLER FWD STRUCTURE BRACKET REPLACEDSDR UIEA2024052300414Stiffener · crackedNO.3 PYLON - I/B STIFFENER FOUND CRACK AT NAC STA 300(<P>NO.3 PYLON - I/B STIFFENER REPAIRED AS PER SRM 54-51-02-2R-2 REPAIR 2. NO FURTHER DEFECTS NOTED.</P>)SDR SWIA202408130683Stand Off · crackedL/H UPPER TRANSCOWL INBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 8/11/2024) INSTALLED 1 EA. NEW STANDOFF P/N CN624-2130-201 ON L/H UPPER TRANS COWL, REF. REO 670-54-21-971, REV. B, 2023-11-28, AND CRJ700 SRM 51-40-11-001-001-A01. COMPLIED WITH STEPSDR SWAA2024060686537Web · crackedCRACK WEB OUTBOARD FAN COWL ON ENGINE 2 2024-318208<[01] REPLACED WEB OUTBOARD FAN COWL ON ENGINE 2 IAW B737-800 SRM 51-40-02-0G-0 AND CMM 71-13-30;[02] REPLACED WEB OUTBOARD FAN COWL ON ENGINE 2 IAW B737-800 SRM 51-40-02-0G-0 AND CMM 71-13-30 TOOL USED CALIPESDR SWAA2024060686361Web · crackedCRACK WEB INBOARD FAN COWL INTERNAL AREA ON ENGINE 1 2024-318200<[01] REPLACED WEB LOCATED ON INBOARD FAN COWL INTERNAL AREA ON ENGINE 1 IAW B737-800 SRM 51-10-02 ITEM 9 AND GOODRICH AEROSTRUCTURES CMM 71-13-30. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED WEBSDR IPXA2024052554204Brace · chafedCHAFING - SURFACE , NO.4 PYLON DIAGONAL BRACE FORWARD 11:00 POSITION. (REPAIR) MEASURE REWORK AREA DEPTH=0.024", LENGTH=1.1", WIDTH=0.4" IT WAS ALLOWABLE I.A.W SRM 54-51-90-1A-3 FIGURE 101 DETAIL II REV:100. APPLY PROTECTIVE COATING AT REWORK AREA I.A.W SRM 5SDR SWAA2024061185255Plate · cracked#1 ENGINE IB FAN COWL WITH SIDE PLATE (BETWEEN ENGINE OIL ACCESS DOOR AND AFT HOLD OPEN ROD) CRACKED. REMOVED AND REPLACED SHIELD PLATE AT #1 ENGINE IB FAN COWL AS PER SRM 51-40-02-0G.;[02] VERIFIED STEP #1SDR SWAA2024050983962Fairing · cracked#2 ENGINE STRUT AFT FAIRING STRUCTURE CRACK. STARTED REMOVAL OF #2 ENGINE AFT FAIRING WEDGE PER SRM 51-40-02. R & R RT STRUT AFT FAIRING IB PANEL IAW SRM 51-40-02.SDR SWAA2024050983474Web · cracked#2 ENGINE AFT PYLON TE WEDGE FWD WEB CRACKED. CRACK TERMINATES AT EDGE OF MATERIAL AND UNDER OVERLAP; APPR 2.5 IN LENGTH<[01] 04 - REPAIRED PER EA-GENERAL 24-154-01241 (EA ATTACHED TO AN AIRCRAFT FAULT)]SDR YENA2024050700720Spigot · corrodedDURING HEAVY MAINTENANCE: CORROSION ON UPPER SPAR SPIGOT RECEPTACLE ON RH PYLON (CPCP RELATED MPD TASK 545117-01); REF AEROMAN WO# 2024 44/1 NR# 2024-149238. EVALUATED SPIGOT FITTING LOC. ON RH PYLON AND FOUND BEYOND OF LIMITS OF ADL ON A320 SRM, REPLACED SPIGSDR GTIA2024042938098Access Panel · damaged"DELAMINATED ACCESS PNL 481AL RAF-01 3316187-01 GENERATED-PERFORMED PERMANENT REPAIR ON RH PYLON ACCESS PANEL 481AL AS PER EC EA 5453-2419 AND EA#54-0082-24 REV 0."SDR IXXA2024042502Cover · delaminatedFIBERGLASS COVER SEPARATING #2 ENGINE.SDR AALA202405135476Spigot · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT PYLON SPIGOT RECEPTACLE BORE LOCATED BETWEEN WS 679 AND WS 706 AND RIB 4 TO RIB 5 ON LEFT-HAND PYLON. REPLACED LOWER SPIGOT FITTING PER SRM 54-51-12-300-002.SDR SWAA2024053078116Angle · corrodedCORROSION FWD STRUT FAIRING BONDING JUMPER SUPPORT ANGLE ON ENGINE 2 2024-270074<[01] REPLACED SUPPORT ANGLE AT FWD STRUT FAIRING BONDING JUMPER ON ENGINE 2 IAW B737-700 SRM 51-40-02.;[02] REPLACED SUPPORT ANGLE AT FWD STRUT FAIRING BONDING JUMPER ON ENGINE 2 SDR CALA2024042401219Angle · crackedNO 1 PYLON OB SIDE TE FAIRING UPPER WEB ATTACH ANGLE CRACKED. TAG NO 91007. REPORTED BY V930423 #1PYLON O/B SIDE TE FAIRING UPPER WEB ATTACH ANGLE WAS REMOVED AND REPLACED IAW B767 SRM 51-40-02 PARAGRAPH 7. DRAWING DOC #313T3380.ESFR 1035900.TRANSCRIBED FROM ASDR IXXA2024041701Strap · cracked#1 ENGINE AFT PYLON ATTACH STRAP CORRODED.SDR NACA2024041500003Angle · crackedTWO EA "L" ANGLES CRACK ON RH NACELLE NAC.STA.278.52 AT WBL.192 AND WBL.204SDR CALA2024041601105Angle · crackedGEN ITEM; 168798-0400-0017/// WHILE REMOVING NO 1 PYLON OB SIDE TE FAIRING UPPER WEB ATTACH ANGLE FOUND THE IB SIDE ALSO CRACKED . REPORTED BY REMOVED & REPLACED INBD ATTACH ANGLE ON NO 1 PYLON IAW B767 SRM 51-40-02 PARA 9 ESFR 1035806SDR COEA2024041213759Panel · crackedDURING A SCHEDULED MAINTENANCE INSPECTION, A CRACK WAS FOUND ON THE R/H ENGINE AFT OUTBOARD ACCESSORY PANEL. A TEMPORARY REPAIR WAS PERFORMED ON THE R/H ENGINE AFT OUTBOARD ACCESSORY PANEL PER TEXTRON DOCUMENT REF: DQ428170M2. REPLACED THE R/H ENGINE AFT OUTBSDR SWAA2024041970372Shield · cracked#2 ENGINE OUTBOARD FAN COWL OIL TANK ACCESS DOOR SHIELD IS CRACKED<[01] #2 ENGINE OUTBOARD FAN COWL REMOVED AND REPLACED OIL TANK ACCESS DOOR SHIELD IKAW AMM 51-40-02-0G-0 STEPS 4 AND 5;[02] VERIFIED TASK COMPLETESDR SWAA2024041970373Shield · cracked#1 ENGINE INBOARD FAN COWL OIL TANK ACCESS DOOR SHIELD IS CRACKED<[01] MEASUREMENTS FIELD UPDATED.<BR><BR>REMOVED AND REPLACED #1 ENGINE INBOARD FAN COWL OIL TANK ACCESS DOOR SHIELD PER CMM 71-13-30 AND SRM 51-40-02-0G-0. NO FURTHER ACTION REQUIRED.;[02] VERIFSDR SWAA2024042668639Strut · corrodedCUSTOMER REQUEST-CORROSION ON AFT STRUT FAIRING INBOARD SIDE AT LT PYLON 2024-195942<[01] TOOL USED IN STEP 4: ULTRASONIC THICKNESS GAGE; P/N: 45MG; S/N: 130064101 DUE DATE: 13-DIC-24;[02] TOOL USED IN STEP 5: EDDY CURRENT INSTRUMENT P/N: NORTEC 600D; S/N: 210SDR SWAA2024042668638Strut · corrodedCUSTOMER REQUEST-CORROSION ON AFT STRUT FAIRING INBOARD SIDE AT RT PYLON 2024-195943<[01] TOOL USED: ULTRASONIC THICKNESS GAUGE; PN: 45MG; SN:221861811; DUE DATE: 30-NOV-24;[02] TOOL USED: EDDY CURRENT EQUIPMENT; PN: NORTEC 600D; SN: 210138503; DUE DATE: 21-JUSDR SWAA2024032868095Web · crackedLH ENGINE; INBOARD FAN COWL WEB AFT OF THE OIL SERVICE DOOR CRACKED. LH ENGINE INBOARD FAN COWL WEB AFT OF THE OIL SERVICE DOOR CRACKED.<[01] CRACK MEASURES 1 INCH. ENGINEERING NOTIFIED.;[02] ACCOMPLISHED EA 24-154-00815;[03] ACCOMPLISHED EA 24-154-00815SDR IXXA2024032701Stiffener · crackedINTERNAL STIFFENER CRACKEDSDR SWAA2024040566507Shield · cracked#1 ENGINE INBOARD FAN COWL OIL TANK ACCESS DOOR SHIELD IS CRACKED<[01] #2 ENGINE INBOARD FAN COWL REMOVED AND REPLACED THE OIL TANK ACCESS DOOR SHIELD IAW SRM 51-40-02-0G-0 STEPS 4. AND 5.;[02] EDIT CORRECTIVE ACTION STEP 1: #1 ENGINE INBOARD FAN COWL REMOVED SDR IXXA2024041401Stiffener · gouged#1 PYLON, HYDRAULIC BAY, BILGE AREA, 2EA WEB STIFFENERS ARE GOUGEDSDR SWAA2024041063996Strap · damagedENGINE #1 UPPER OUTER INLET COWL STRAP P/N 314-2154-2 AT 3 O' CLOCK POSITION #3 HOLE FROM FWD END ELONGATED<[01] REMOVED AND PARTIALLY REPLACED STRAP AT ENGINE #1 UPPER OUTER INLET COWL AS PER SRM 51-40-020G-0 & CMM 71-11-22.;[02] CORRECTION TO STEP #1 <BR>STRSDR YENA2024031200402Plate · corrodedDURING HEAVY MAINTENANCE: RETAIINING PLATE WAS FOUND WITH CORROSION ON LH PYLON SPIGOT (1EA); REF AEROMAN W.O. 2024 41/1 NR 55041 - REMOVED AND REPLACED SPIGOT ON LH PYLON (1EA) IAW A320 SRM A320 54-51-12-300-002. THIS REPAIR IS CATEGORY A. NO REQUIRED FURTHERSDR SWAA2024031161256Fairing · cracked#2 ENGINE PYLON AFT FAIRING CRACK<[01] REPAIRED PER SRM 54-50-70-2R-7.;[02] REVIEWED THE FAULT AND VERIFIED THE REFERENCE USED HAS THE CORRECT FOLLOW ON INSPECTIONS.
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