JASC 5714
Service difficulty reports · 1,451
Reports filed under 5714 · Wing, Center Box, 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 = '5714' 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 = '5714' 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 AALA202302163000Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR SHEAR FITTING LOCATED AT BS 540 AND RBL 32.40. REPLACED SHEAR FITTING PER EA 342233.SDR AALA202302165316Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR SHEAR FITTING LOCATED AT BS 540 AND LBL 54.60. REPLACED SHEAR FITTING PER EA 342233.SDR AALA202302165062Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR SHEAR FITTING LOCATED AT BS 540 AND RBL 15.04. REPLACED SHEAR FITTING PER EA 342233.SDR DALA2023030301589None · noneSHIP 1200 THE CABIN CENTER SECTION UPPER SURFACE CORROSION AT BL 0 AND STA 955.1;REF TO CPCP TASK:53-494-00. CORRECTIVE ACTION: REPAIRED THE CORRODED OF THE CABIN CENTER SECTION UPPER SURFACE AT BL 0 AND STA 955.1 AS PER PRI 605104-14 REV 0 AND PRI 605104- 14 SDR DALA2023020700952None · noneSHIP 3308 CRACK FOUND AT FRAME 40 VERTICAL WEB ABOVE THE CENTER WING BOX LOWER P ANEL AT HOLE H263 RH SIDE. AA 5716-01017. SB A330-57- 3115 REV 02. AD 2019-16-07. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR ON HOLE H263 RH LOC. ON FR40 VERTICAL WEB ABOVE CENSDR DALA2023020700970None · noneSHIP 3308 CRACK FOUND AT FRAME 40 VERTICAL WEB ABOVE THE CENTER WING BOX LOWER P ANEL AT HOLE H260 RH SIDE. AA 5716-01017. SB A330-57- 3115. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR ON HOLE H260 LOC. ON FR40 VERTICAL WEB ABOVE CENTER WING BOX LOWER PANEL SDR DALA2023020700969None · noneSHIP 3308 CRACK FOUND AT FRAME 40 VERTICAL WEB ABOVE THE CENTER WING BOX LOWER P ANEL AT HOLE H263 LH SIDE. AA 5716-01017. SB A330-57- 3115. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR ON HOLE H263 LH LOC. ON FR40 VERTICAL WEB ABOVE CENTER WING BOX LOWER PANSDR DALA2023020700968None · noneSHIP 3308 CRACK FOUND AT FRAME 40 VERTICAL WEB ABOVE THE CENTER WING BOX LOWER PANEL AT HOLE H260 LH SIDE. AA 5716-01017. SB A330-57-3115 REV 02. AD 2019-16-07. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR ON HOLE H260 LOC. ON FR40 VERTICAL WEB ABOVE CENTER WSDR DALA2023020700959None · noneSHIP 3308 DURING HCK AT AEROMAN (SAL) AND INSPECTION PER EM 5716-01017, HO LE 263 RH WAS FOUND CRACKED. A REPAIR WAS ACCOMPLISHED PER SECT IV OF ERA 604913-14AD. CORRECTIVE ACTION: ACCOMPLISH THE SECT VII INSPECION OF HOLE 263 RH AT A THRESHOLD OF 26,579 TOTALSDR DALA2023020700958None · noneSHIP 3308 DURING HCK AT AEROMAN (SAL) AND INSPECTION PER EM 5716-01017, CRACK WAS FOUND AT HOLE 263 LH. A REPAIR WAS ACCOMPLISHED PER SECT II OF ERA 604913-14AD. CORRECTIVE ACTION: ACCOMPLISH THE SECT VI INSPECTION OF HOLE 263 LH AT A THRESHOLD OF 21,409 TOTALSDR DALA2023020700957None · noneSHIP 3308 DURING HCK AT AEROMAN (SAL) AND DURING INSPECTION PER EM 5716-01 017, HOLE 260 LH AND RH WERE FOUND CRACKED. REPAIRS WERE ACCOMPL ISHED PER SECT I AND III OF ERA 604913-14AD. CORRECTIVE ACTION: ACCOMPLISH THE SECT IV OF ERA 604913-14 AT HOLE 260 LH ASDR SWAA2023032098614Stiffener · crackedCRACK STIFFENER FLOOR STRUCTURE LOCATED BS 540 BETWEEN BL 0 AND RBL 24.5 WL 208.1 CENTER SECTION 2023-106058<[01] REPLACED STIFFENER FLOOR STRUCTURE LOCATED BS 540 BETWEEN BL 0 TO RBL 24.5 WL 208.1 CENTER SECTION IAW B737-700 #DWG-143A0060 SHEET= 36 REV= A ANDSDR SWAA2023030697675Stiffener · crackedCRACK STIFFENER FLOOR STRUCTURE LOCATED BS540 BTW LBL24.8 AND BL0.0 CENTER SECTION 2023-99103<[01] REPLACED STIFFENER FLOOR STRUCTURE LOCATED BS540 BTW LBL24.8 AND BL0.0 CENTER SECTION IAW B737-700 SRM 51-10-02 Ï¿½TEM 9 AND SRM 51-40-02 SEE INDIVIDUAL SIGNOFFSSDR SWAA2023030697674Structure · crackedCRACK STIFFENER FLOOR STRUCTURE LOCATED BS540 BTW RBL24.8 TO BL0.0 CENTER SECTION 2023-99104<[01] REPLACED STIFFENER FLOOR STRUCTURE LOCATED BS540 BTW RBL24.8 TO BL0.0 CENTER SECTION IAW B737-700 SRM 51-10-02 Ï¿½TEM 9 AND SRM 51-40-02 SEE INDIVIDUAL SIGNOFFS BSDR SWAA2023031396386Intercostal · crackedIN THE MAIN CABIN FLOOR AREA AT STATION 540; THERE IS A CRACK AT THE FLEXIBLE INTERCOSTAL AT LBL 2. (SEE ATTACHED PICTURE)<[01] R/R INTERCOSTAL IAW SRM 51-40-02.;[02] C/W INSPSDR SWAA2023021696618Stiffener · crackedLOWER FUSELAGE CENTER WING REAR SPAR BULKHEAD STA 663.75 VAPOR BARRIER SUPPORT STIFFENER CRACKED @ LOWER RADIUS RBL 28 MKD DOT<[01] REMOVED SUPPORT STIFFENER FOR CRACK AT STA 663.75 RBL28 LOWER VAPOR BARRIER SRM 51-40-02-0G-0;[02] RECEIVED NEW STIJJENER PN. 11SDR SWAA2023021696617Stiffener · crackedLOWER FUSELAGE CENTER WING REAR SPAR BULKHEAD STA 663.75 VAPOR BARRIER SUPPORT STIFFENER CRACKED @ LOWER RADIUS LBL 28 MKD DOT<[01] REMOVED STIFFENER AT LOWER FUSELAGE CENTER REAR SPAR BULKHEAD STA 663.75 LBL 28 FOR CRACK SRM 51-40-02-0G-0;[02] RECEIVED NEW PASDR AALA202301267047Angle · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN WING CENTER SECTION REAR SPAR VAPOR BARRIER SUPPORT ANGLE LOCATED AT BS 663 AND RBL 9. REPAIRED ANGLE PER SRM 51-40-02 AND SRM 57-10-10-2R-5.SDR SWAA2023022294289Angle · crackedCRACK SUPPORT ANGLE LOCATED AT BS 695 RBL 24.5 WL 208.1 CENTER SECTION 2023-83568<[01] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 01-FEB-24; TEMPERATURE CONTROLLER: P/N: 48VFL11; S/N: AE-31448; DUE DATE: 14-JUN-23.;[02] SDR SWAA2023022294288Structure · crackedCRACK STIFFENER FLOOR STRUCTURE LOCATED AT BS 540 BETWEEN BL0 AND LBL 24.5 WL208.1 CENTER SECTION 2023-83569<[01] REPLACED STIFFENER FLOOR STRUCTURE AND FASTENERS BS540 BETWEEN BL0 TO LBL24.5 IAW B737-700 SRM 51-40-02 AND DRAWING 143A0060 SHEET 43 REV ?.SEE INSDR SWAA2023020894470Fitting · crackedR/W REAR SPAR LOWER T/E PANEL 651GB FWD WIGGLE FITTING CRACKED ; SHEARED FASTENERS<[01] LOCATED AND DRILLED NEW R/W REAR SPAR LOWER T/E PANEL 651GB FWD WIGGLE FITTING AS PER B737-700 SRM 51-40-05-0G-0;[02] VALIDATED STEP 1<BR><BR><BR>OK TO INSTALL NEW UNIT;[03SDR SWAA2023021693905Intercostal · crackedIN THE MAIN CABIN FLOOR AREA AT STATION 540; THE FLEXIBLE INTERCOSTAL HAS A CRACK AT BL 0.<[01] REMOVED AND REPLACED INTERCOSTAL WITH FASTENERS PER SRM 51-40-02.;[02] REMOVED AND REPLACED INTERCOSTAL WITH FASTENERS PER SRM 51-40-02.<BR>INSPECTION C/W.SDR SWAA2023020994117Support · crackedMAIN CABON CENTER WING BOX FLOOR SUPPORT BREAK CRACKED @ RBL-1 STA 540 WATER LINE 182<[01] REMOVED CABIN FLOOR PANEL 231UF FOR ACCESS AS PER 53-21-00-000-801.;[02] REMOVED MAIN CABIN CENTER WING FLOOR SUPPORT BREAK AT RBL-1 STA-540 IN REFERENCE B-737-700 SRM 5SDR AALA202301267481Angle · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN WING CENTER SECTION REAR SPAR VAPOR BARRIER SUPPORT ANGLE LOCATED AT BS 663 AND LBL 9. REPAIRED ANGLE PER SRM 51-40-02 AND SRM 57-10-10-2R-5.SDR SWAA2023021491842Bracket · crackedCRACK BODY STATION 540 LBL 19 BRACKET AT AIR CONDITIONING BAY 2023-38044<[01] REPLACED BRACKET LOCATED AT BODY STATION 540 LBL 19 AIR CONDITIONING BAY IAW B737-700 SRM 51-40-02 SEE INDIVIDUAL SINGOFFS BELOW.;[02] REPLACED BRACKET LOCATED AT BODY STATION 540 LBSDR SWAA2023021491843Angle · crackedCRACK BODY STA 663.75 ANGLE RBL 19 AT AIR CONDITIONING BAY 2023-38046<[01] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 112031023 DUE DATE: 01-FEB-23.;[02] REPLACED BODY STA 663.75 ANGLE RBL 19 AT AIR CONDITIONING BAY IAW B-737-700 SRM 51-40-02 ANDSDR SWAA2023021491844Angle · crackedCRACK BODY STA 663.75 ANGLE LBL 20 AT AIR CONDITIONING BAY 2023-38045<[01] TOOL USED: ET EQUIPMENT P/N: NORTEC 500D; S/N: N500X12101V022233; DUE DATE: 30-AUG-23;[02] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 112031023 DUE DATE: 01-FEB-23.;[03] RSDR AALA202302022956Pressure Deck · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN WING CENTER SECTION REAR SPAR VERTICAL PRESSURE DECK WEB LOCATED AT BS 663 AND RBL 40. REPAIRED WEB PER SRM 57-10-10-2R-3 ALTERNATIVE 2.SDR SWAA2023020890443Support Bracket · crackedLEFT ECS BAY HAS CRACKED DUCT SUPPORT BRACKET (212A1116) ACCESS PANEL 192CL BS540+6 LBL8.<[01] REMOVED LEFT ECS BAY HAS CRACKED DUCT SUPPORT BRACKET BS540+6 LBL8 IAW AMM TASK 20-50-11-910-801.;[02] REPLACED AND INSTALLED NEW DUCT SUPPORT BRACKET (212A1116) ACCSDR SWAA2023020890447Support Bracket · crackedRIGHT ECS BAY HAS CRACKED DUCT SUPPORT BRACKET (212A1116) ACCESS PANEL 192CR BS540+6 RBL8.<[01] REMOVED RIGHT ECS BAY HAS CRACKED DUCT SUPPORT BRACKET BS540+6 RBL8 IAW AMM TASK 20-50-11-910-801.;[02] REPLACED AND INSTALLED NEW DUCT SUPPORT BRACKET (212A1116) ASDR SWAA2023020790444Support · crackedWING CENTER SECTIONS PANEL SUPPORT TAB CRACKED BS540+12 RBL6 ACCESS PANEL 192E.<[01] REMOVED SUPPORT ON WING CENTER SECTIONS PANEL BS540+12 RBL6 ACCESS PANEL 192E IAW SRM 51-40-02-0G-0-A;[02] INSTALLED NEW SUPPORT AT BS540+12 RBL6 ACCESS PANEL 192E PER REF SRMSDR SWAA2023021489752Angle · crackedCRACK ANGLE FLOOR STRUCTURE BS 685 PLUS 6 INCHES AT BL 0 AT PASSENGER CABIN 2023-37824<[01] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 01-FEB-23; TEMPERATURE CONTROLLER: P/N: 48VFL11; S/N: AE-31448; DUE DATE: 14-JUN-23.;SDR SWAA2023021489753Angle · crackedCRACK FLOOR STRUCTURE ANGLES LOCATED ON BS 540 BTW LBL 24.75 TO RBL 24.75 AT PASSENGER CABIN (2 EA) 2023-37825<[01] REPLACED FLOOR STRUCTURE ANGLES LOCATED ON BS 540 BTW LBL 24.75 TO RBL 24.75 AT PASSENGER CABIN (2 EA) IAW B737-700 SRM 51-40-02 AND DWG 143A006SDR SWAA2023021088581Angle · crackedCRACK ANGLE FLOOR STRUCTURE LOCATED BS 540 BTW BL 0 TO LBL 24.75 CENTER SECTION 2022-708632<[01] REPLACED STIFFENER (ANGLE) FLOOR STRUCTURE LOCATED BS 540 BTW BL 0 TO LBL 24.75 CENTER SECTION I.A.W B737-700 SRM 51-40-02-0G-0 AND DWG 143A0060 SHEET 36 REV A.;[0SDR SWAA2023020186624Bracket · crackedLOWER CENTER WING L/H A/C BAY STA 540 CROSS-OVER DUCT I/B SUPPORT BRACKET CRACKED MKD DOT<[01] REMOVED LOWER CENTER WING L/H A/C BAY CROSS OVER DUCT I/B SUPPORT BRACKET RED BOEING 737 ARM 51-40-02-0G-0;[02] VERIFIED STEP #1.;[03] OK TO INSTALL NEW SUPPORT BRACSDR DALA2022122108284Skin · corrodedSHIP 659 CORROSION ON UPPER SKIN CENTER TANK WING BOX STA 960 AND 940 LBL65. CORRECTIVE ACTION: SUMMARY OF NRC 00553. AREA WAS REPAIRED PER ER/A 603710-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 603710-14 REV 5. (2547416)SDR SWAA2023020883714Support Bracket · crackedCRACK BODY FAIRING SUPPORT BRACKET OF BLEED AIR DUCT AT LEVEL STA540 LT SIDE AT LOWER FUSELAGE 2022-697217<[01] REPLACED BODY FAIRING SUPPORT BRACKET OF BLEED AIR DUCT AT LEVEL STA540 LT SIDE AT LOWER FUSELAGE I.A.W B737-700 SRM 51-10-02 AND DWG 212A1110 SHEETSDR SWAA2023020883723Angle · crackedCRACK BODY FAIRING INTERNAL STRUCTURE ANGLE LOCATED AT LEVEL OF STA661.96 AND RBL6.0 AND WL145.8 AT LOWER FUSELAGE 2022-697233<[01] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 112031023 DUE DATE: 01-FEB-23;[02] REPLACED ANGLE LOCATED ON BODY FAIRISDR DALA2022121308023Floorbeam · crackedA CRACK WAS FOUND IN FLOORBEAM STA 735 X=-58 AT WING BOX AREA (WB), WHILE PERFORMING AMDS 5310-01436-01C. SUMMARY OF NRC 00249: BEAM STA 735 X=-58 AT WING BOX AREA (WB) WAS REPLACED PER B717-200 SRM 51-41-03-0G PAR 11, 51-41-02-0G, 51-41-01-0G, 51-41-02-0G PARSDR SROM110220223None · chafedCHAFING DAMAGE ON RH INBOARD FLAP, OUTBOARD WING TANK CAN (P/N 85714630-004. DAMAGE IS BEYOND MANUFACTURES LIMITS; PART REQUIRES REPLACEMENT.SDR SWAA2022111764755Structure · corrodedWING CTR SECTION FLOOR STRUCTURE PRESS FLOOR;SHOW SIGNS OF UPPER SURFACE CORROSION AT STA 716 MINUS 2.50 INCHES LBL 65 WL 202.1 / [01] REMOVED CORROSION AT WING CTR SECTION FLOOR STRUCTURE PRESS FLOOR AT STA 716 MINUS 2.50 INCHES LBL 65 WL 202.1 IAW SRM 51-10-SDR DALA2022102506882None · noneSHIP 197 HFEC INSPECTION FOUND 01EA CRACK ON RH LOWER UNDER-WING LONGERON FITTING AS MARK, CORRECTIVE ACTION: RH LOWER UNDER WING LONGERON FITTING 01EA CRACK LENGTH:0.160" REMOVED AND REPLACED REF TO W/C:5711-01042-04. (2460160)SDR SWAA2022110358842Angle · crackedCRACK ANGLE FLOOR STRUCTURE LOC. BL0 TO LBL 24.75 AND BS 540 AT PASSENGER CABIN 2022-576381 / [01] REPLACED ANGLE FLOOR STRUCTURE LOC. BL0 TO LBL 24.75 AND BS 540 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND SRM 51-10-02; ITEM 9; REV -. SEE INDIVIDUAL SIGNSDR SWAA2022110358843Angle · crackedCRACK ANGLE FLOOR STRUCTURE LOC. BL0 TO RBL 24.75 AND BS 540 AT PASSENGER CABIN 2022-576376 / [01] REPLACED ANGLE FLOOR STRUCTURE LOC. BL0 TO RBL 24.75 AND BS 540 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND SRM 51-10-02; ITEM 9; REV -. SEE INDIVIDUAL SIGNSDR SWAA2022110458379Bracket · crackedCRACK BRACKET BS 685 AND LBL 42.75 AT CENTER WING BOX 2022-576229 / [01] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 01-FEB-23; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 01-FEB-23.;[02] REPLACEDSDR SWAA2022110458377Bracket · crackedCRACK BRACKET LOC BS 685 AND RBL 24.75 AT CENTER WING BOX 2022-576227 / [01] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 01-FEB-23; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 01-FEB-23.;[02] REPLSDR AALA202210132375Web · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK FOUND ON CENTER WING SECTION KEEL BEAM WEB AT STA 727 BETWEEN RIGHT BUTT LINE 31.83 AND RIGHT BUTT LINE 40.00. INSTALLED A REINFORCING MODIFICATION PER SRM 57-10-10-2R,SDR SWAA2022101116001Angle · cracked(CUSTOMER REQUEST) CRACK SUPPORT ANGLE LOC BS 663 LH SIDE AT CENTER WING BOX 2022-510772 / [01] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 112031023 DUE DATE: 01-FEB-23.;[02] REPLACED SUPPORT ANGLE LOC BS 663 LH SIDE AT CENTER WING BOX IAW B737-7SDR SWAA2022101046545Angle · brokenBROKEN SUPPORT ANGLE LOCATED BS540 AT LEVEL BL0 TO RBL24.75 AT PASSENGER CABIN 2022-466945 / [01] REPLACED SUPPORT ANGLE SUPPORT ANGLE LOCATED BS540 AT LEVEL BL0 TO RBL24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02. SEE INDIVIDUAL SSDR SWAA2022101046546Angle · brokenBROKEN SUPPORT ANGLE LOCATED BS540 AT LEVEL RBL24.75 TO RBL45.50 AT PASSENGER CABIN 2022-466946 / [01] REPLACED SUPPORT ANGLE LOCATED BS540 AT LEVEL RBL24.75 TO RBL45.50 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02. SEE INDIVIDUAL SIGN
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