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 SWAA2022030366151Angle · crackedCRACK ANGLE LOCATED BS695 AND LBL24 AT CENTER WING BOX 2022-55487 / [01] REPLACED ANGLE LOC. BS 695 AND LBL 24 AT CENTER WING BOX IAW B737-700 SRM 51-40-02 AND DWG 273A9110. REV A.;[02] CORRECTED STEP 1<BR>REPLACED ANGLE LOC. BS 695 AND LBL 24 AT CENTER WING BSDR SWAA2022030266064Splice Angle · crackedLEFT HAND PACK BAY; HORIZONTAL ANGLE COMMON TO LOWER SIDE OF CENTER FUEL TANK AT STATION 663 LBL 10 IS CRACKED 3RD FASTENER OUTBOARD OF KEEL BEAM VERTICAL ANGLE. MARKED. / [01] REMOVED ALL FASTENERS IN REPAIR AREA AND CUT OUT DAMAGED SECTION OF ANGLE LBL6-17 ISDR SWAA2022030266065Angle · crackedRIGHT HAND PACK BAY; HORIZONTAL ANGLE COMMON TO LOWER SIDE OF CENTER FUEL TANK AT STATION 663 RBL 10' IS CRACKED 3RD FASTENER OUTBOARD OF KEEL BEAM VERTICAL ANGLE. MARKED. / [01] REPLACED RH HORIZONTAL ANGLE COMMON TO LOWER SIDE OF CENTER FUEL TANK STA 663 RBLSDR SWAA2022030266063Angle · crackedRIGHT HAND PACK BAY; HORIZONTAL ANGLE COMMON TO LOWER SIDE OF CENTER FUEL TANK AT STATION 663 RBL 34' IS CRACKED. / [01] REMOVED DAMAGED ANGLE RBL6-65 IAW SRM 57-10-10-2R-5;[02] PERFORMED DETAILED INSPECTION OF REPAIR AREA; NO DEFECTS NOTED IAW SRM 57-10-10-2RSDR SWAA2022020365492Angle · crackedSUPPLEMENTAL INFORMATION: A125-03 - CRACK NOTED AT FASTENER - BS663; RBL08 - ECS BAY AFT BULKHEAD; UPPER ANGLE / [01] CUT AND REMOVED DAMAGE IAW SRM 57-10-10-2R-5 REPAIR 5;[02] PERFORMED DVI OF REPAIR AREA AND UNDERLYING STRUCTURE. NO DEFECTS NOTED IAW SRM 57-SDR SWIA202265197None · damagedDEFECTS NOTED IN THE RH LWR WING PLANK FWD & AFT ATTACHMENT HOLES FOR THE RH WING DRAIN LOCATED BETWEEN WS0.00 + THE RH BOOST PUMP AND BETWEEN STR5 - STR7. (C-CHECK RO 3-25-22) REPAIRED DEFECTS IN THE RH LWR WING PLANK FWD & AFT ATTACHMENT HOLES FOR THE RSDR SWIA202265196None · damagedDEFECTS NOTED IN THE LH LWR WING PLANK FWD & AFT ATTACHMENT HOLES FOR THE LH WING DRAIN LOCATED BETWEEN WS0.00 + THE LH BOOST PUMP AND BETWEEN STR5 - STR7. (C-CHECK RO 3-25-22) REPAIRED DEFECTS IN THE LH LWR WING PLANK FWD & AFT ATTACHMENT HOLES FOR THE LSDR SWAA2022031165318Web · crackedCRACK HORIZONTAL PRESSURE WEB LOCATED BS 663 AND LBL32 APPROX. AT CENTER WING BOX 2022-67659 / [01] TOOL USED P/N:NORTEC 600D S/N:210138503 CAL DUE DATE:05-MAR-22;[02] TOOL USED ;P/N: FPK-PRO-104 ; S/N: PRO-3446 ; DUE DATE: 12-JAN-23;[03] REPAIRED PRESSURE WEBSDR SWAA2022020365493Angle · crackedCRACK NOTED AT FASTENER, BS 663, LBL 8, ECS BAY AFT BULKHEAD, UPPER ANGLE. CUT AND REMOVED DAMAGE IAW SRM 57-10-10-2R-5 REPAIR 5. PERFORMED DVI OF REPAIR AREA AND UNDERLYING STRUCTURE. NO DEFECTS NOTED IAW SRM 57-10-10-2R-5 REPAIR 5. COMPLETED NDT INSP FOSDR SWAA2022021663924Gusset · crackedGUSSET CRACKED IN FWD CARGO BS500I STR19R. / [01] REMOVED; LOCATED AND DRILLED NEW GUSSET IAW SRM 51-40-02. INSTALLATION STILL REQUIRED.;[02] INSTALLED GUSSET IAW SRM 51-40-02.;[03] INSPECTION COMPLETE ON CORRECTIVE ACTION #2 FOR GUSSET REPLACEMENT.SDR SWAA2022021763342Stiffener · crackedCRACK STIFFENER FLOOR STRUCTURE LOCATED AT BS 540 BETWEEN BL0 AND LBL 24.88 CENTER SECTION ; 2022-58102 / REPLACED STIFFENER FLOOR STRUCTURE LOCATED AT BS 540 BETWEEN BL0 AND LBL 24.88 CENTER SECTION IAW B737-700 SRM-51-10-02-0G-0 ITEM 9 AND SRM-51-40-02 PART SDR SWAA2022021772410Stiffener · crackedCRACK STIFFENER FLOOR STRUCTURE LOCATED AT BS 540 BETWEEN BL0 AND LBL 24.88 CENTER SECTION 2022-58102 / [01] REPLACED STIFFENER FLOOR STRUCTURE LOCATED AT BS 540 BETWEEN BL0 AND LBL 24.88 CENTER SECTION IAW B737-700 SRM-51-10-02-0G-0 ITEM 9 AND SRM-51-40-02 PASDR SWAA2022021772409Stiffener · crackedCRACK STIFFENER FLOOR STRUCTURE LOCATED BETWEEN BL0 AND RBL24.88 BS540 CENTER SECTION 2022-58101 / [01] REPLACED STIFFENER FLOOR STRUCTURE LOCATED BETWEEN BL0 AND RBL24.88 BS540 CENTER SECTION IAW B737-700 SRM-51-10-02-0G-0 ITEM 9 AND SRM-51-40-02; PART USED: SDR SWAA2022012562370Attach Angle · crackedCRACK FOUND IN RT AC BAY UPPER ATTACH ANGLE AT BS 663 RBL 8. CRACK VERIFIED WITH HFEC. CUT & REMOVED ATTACH ANGLE IAW SRM 57-10-10-2R-5 FIG 202 SHEET 4; PERFORMED DVI OF REPAIR AREA & UNDERLYING STRUCTURE. NO DEFECTS NOTED IAW SRM 57-10-10-2R-5 REPAIR 5; FSDR SWAA2022013162169Panel · crackedFLOOR STRUCTURE 143A5240 AT BS537.5 IS CRACKED AT LBL0 ; / [01] REMOVED FLOOR PANEL AT BS 520 TO 540 LBL 25 TO RBL 25 FOR ACCESS IAW SRM 51-40-02-0G.; [02] REMOVED CRACKED SUPPORT BREAK IAW SRM 51-40-02-0G; [03] VERIFIED NEW PART AS PART# 143A5240-35. IAW B737SDR SWAA2022021560857Structure · crackedCRACK ANGLE FLOOR STRUCTURE AT LEVEL OF LBL 24.75 BS 695 AT PASSENGER CABIN ; 2022-12358 / [01] REPLACED ANGLE OF FLOOR STRUCTURE LOCATED AT LEVEL OF LBL24.75 BS695 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG# 273A9110; SHEET: 6; REV. ?A?; AND DWG# 27SDR SWAA2022011260404Angle · crackedSUPPLEMENTAL INFORMATION: A125-01 - CRACK NOTED AT BS663; RBL 09 AT AFT UPPER AC BAY BULKHEAD ATTACH ANGLE TO CENTER TANK ;LOWER SKIN. / [01] REMOVED FASTENER AT BS663 RBL 09 AT AFT UPPER AC BAY BULKHEAD ATTACH ANGLE TO CENTER TANK LOWER SKIN I/A/W SRM 51-40-0SDR SWAA2022020459963None · crackedSUPPLEMENTAL INFORMATION: MAIN CABIN CENTER WING BOX UNDER FLOOR PANEL CENTER AISLE FLOOR SUPPORT BREAK CRACKED @ STA 540 LBL 1 ; / [01] REMOVED MAIN CABIN FLOOR SUPPORT BREAK AT STA 540 BETWEEN BL 0 AND LBL 24 REF B737-700 SRM 51-40-02-0G-0.; [02] LOCATED ANDSDR SWAA2022021559561Angle · crackedCRACK ANGLE FLOOR STRUCTURE AT LEVEL OF BS 695 AND BL 0 AT PASSENGER CABIN ; 2022-12266 / [01] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 21-JAN-22; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 21SDR SWAA2022021559559Angle · crackedCRACK ANGLE FLOOR STRUCTURE AT LEVEL OF RBL 24.75 AND BS 695 AT PASSENGER CABIN ; 2022-12265 / [01] REPLACED ANGLE OF FLOOR STRUCTURE LOCATED AT LEVEL OF RBL24.75 BS695 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG# 273A9110; SHEET: 6; REV. ?A?; AND DWGSDR SWAA2022020860338Bracket · brokenPANEL 192E SUPPORT BRACKETS BROKEN OFF AT STA 552 AT LBL 5 AND RBL 5 ; / [01] REMOVED SUPPORT BRACKETS AT PANEL 192EOFF STA 552 LBL 5 AND RBL 5 PER SRM 51-40-02-0G; [02] LOCATED AND DRILLED NEW (2EA) SUPPORT BRACKETS FOR PANEL 192E BS 552 ; LBL 5 AND RBL 5 IAWSDR SWAA2022021159172Angle · crackedCRACK ANGLE LOCATED BS 693 BL 0 WL 208.1 AT CENTER WING BOX ; 2022-11223 / [01] REPLACED ANGLE LOCATED BS 693 BL 0 WL 208.1 AT CENTER WING BOX IAW B737-700 SRM 51-10-02 AND DRAWING 273A9110 SHEET 6 REV A; [02] REPLACED ANGLE LOCATED BS 693 BL 0 WL 208.1 AT CENSDR SWAA2022021159175Angle · crackedCRACK ANGLE LOCATED BS 693 LBL 25 WL 208.1 AT CENTER WING BOX ; 2022-11222 / [01] REPLACED ANGLE LOCATED BS 693 LBL 25 WL 208.1 AT CENTER WING BOX IAW B737-700 SRM 51-10-02 AND DRAWING 273A9110 SHEET 6 REV A SEE INDIVIDUAL SIGN-OFF BELOW; [02] REPLACED ANGLE LSDR SWAA2022021159176Angle · crackedCRACK ANGLE LOCATED BS 693 RBL 25 WL 208.1 AT CENTER WING BOX ; 2022-11226 / [01] REPLACED ANGLE LOCATED BS 693 RBL 25 WL 208.1 AT CENTER WING BOX IAW B737-700 SRM 51-10-02 AND DRAWING 273A9110 SHEET 6 REV A SEE INDIVIDUAL SIGN-OFF BELOW; [02] REPLACED ANGLE LSDR SWAA2022021159173Angle · crackedCRACK ANGLE LOCATED BS 693 BL 0 TO RBL 2 WL 208.1 AT CENTER WING BOX ; 2022-11225 / [01] REPLACED ANGLE LOCATED BS 693 BL 0 TO RBL 2 WL 208.1 AT CENTER WING BOX IAW B737-700 SRM 51-10-02 AND DRAWING 273A9110 SHEET 6 REV A; [02] REPLACED ANGLE LOCATED BS 693 BLSDR SWAA2022021458387Angle · crackedCRACK ANGLE LOCATED BS695 AND LBL24 AT CENTER WING BOX ; 2021-585102 / [01] CORRECTED CORRETIVE ACTION.REPLACED ANGLE LOCATED AT BS695 AND LBL24 AT CENTER WING BOX IAW B737-700 SRM 51-10-02 ITEM 9 AND B737-700 SRM 51-40-02 AND DWG 273A9110; REV: A<BR>SEE INDIVSDR SWAA2022021458388Angle · crackedCRACK ANGLE LOCATED BS695 AND BL0 AT CENTER WING BOX ; 2021-585101 / [01] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 21-JAN-22; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 21-JAN-22; TEMPERATURE SDR SWAA2022021458389Angle · crackedCRACK ANGLE LOCATED BS695 AND RBL24 AT CENTER WING BOX ; 2021-585099 / [01] REPLACED ANGLE LOCATED AT BS695 AND LBL24 AT CENTER WING BOX IAW B737-700 SRM 51-10-02 ITEM 9 AND B737-700 SRM 51-40-02 AND DWG 273A9112; REV: -.<BR>SEE INDIVIDUAL SIGNOFF BELLOW; [02]SDR DALA2022010800153None · noneSHIP 185 FOUND CTR TANK UPPER SKIN CORROSION AT STA889. RBL88. CORRECTIVE ACTION: CORROSION REMOVED AND ACCOMPLISHED AS PER PRI 596167-14. (2074574)SDR SWAA2022012057299Support · crackedCABIN FLOOR BOARD SUPPORT CRACKED AT FASTENER STA.540 1'LBL. ; / [01] R&R SUPPORT PER SRM 51-40-02-0G-0SDR SWAA2022020754493Angle · crackedL/H FUS. FWD WING-TO-BODY FAIRING SUPPORT ANGLE CRACKED @ FIXED L/E FRONT SPAR END MKD DOT 001 ; / [01] REMOVED SUPPORT. ANGLE AT L/H FUS FWD WING TO BODY FAIRING L/E FROM. SPAR B 737 -700 SRM 51 40-02-0G -0; [02] LOCATED AND DRILLED. NEW SUPPORT. ANGLE B737-7SDR SWAA2022020754494Angle · crackedR/W FWD WING TO BODY FAIRING SUPPORT ANGLE CRACKED @ FASTENER'S TAIL INB FRONT SPAR FIXED L/E END INB. MKD DOT 002 ; / [01] REMOVED SUPPOR ANGLE AT R/W FWD WING TO BODY FAIRING B 737-700 SRN 51-40-02-0G-0; [02] VERIFIED STEP 1; [03] LOCATED AND DRILLED NEW SUPSDR SWAA2022013154582Bracket · crackedCRACK BODY STATION 540 SUPPORT BRACKET OF THE BLEED DUCT ON INTERNAL AREA OF ACCESS PANEL 192CL AT LOWER FUSELAGE ; 2021-577193 / [01] REPLACED FRONT BRACKET OF THE BLEED DUCT ON INTERNAL AREA OF ACCESS PANEL 192CL IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM B737SDR SWAA2022013154583Angle · crackedCRACK ON ANGLE LOCATED BS663 AND RBL 10 APPROX AIR CONDITIONING COMPARTMENT AREA AT LOWER FUSELAGE ; 2021-577198 / [01] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811020 DUE DATE: 21-JAN-22; [02] REPLACED ANGLE LOCATED BS663. BTW RBL 65.00 ANDSDR SWAA2022013154389Bracket · crackedCRACK BODY STATION 540 SUPPORT BRACKET OF THE BLEED DUCT ON INTERNAL AREA OF ACCESS PANEL 192CR AT LOWER FUSELAGE (1 EA) ; 2021-567190. / [01] REPLACED BRACKET OF THE BLEED DUCT ON INTERNAL AREA OF ACCESS PANEL 192CR AT LOWER FUSELAGE I.A.W B737-700 SRM 51-10-SDR SWAA2021122053188Angle · crackedLT A/C BAY BS 663, LBL 8, LOWER FUEL TANK ANGLE COMMON THE VAPOR BARRIER IS CRACKED AT FASTENER JUST OUTBD OF LH KEELBEAM. REPLACEMENT ANGLE FABRICATED IAW W/O 43057-5000-0001. SPLICE ANGLE FABRICATED ON W/O 43057-5000-0002, REPLACEMENT ANGLE TO BE .063' 20SDR CALA2021121002315Pressure Blkhd · crackedCENTER WING REAR SPAR VERTICAL PRESSURE WEB AT STA 663.75 HAS 2 EA CRACKS AT APPROX LBL 42 ENTERED FOR SFR REPORT PERFORM HFEC INSP AT 36000 FLT CYCLES REF 737 SRM 57-10-10-2R-3 REPAR 3 TABLE 206 PAGE 8 OF 34 VERIFIED SOURCE DOCUMENT AND DIP REQUIREMENTS.SDR SWAA2022012050795Angle · crackedCRACK ANGLE LOCATED BS695 AND BL0 AT PASSENGER CABIN ; 2021-557791 / [01] REPLACED ANGLE LOCATED BS695 AND BL0 AT PASSENGER CABIN I.A.W B737-700 SRM 51-40-05; DRAWING 273A9112 REV - ; AND B737-700 SRM 51-30-01 SEE INDIVIDUAL SIN-OFF BELOW; [02] REPLACED ANGLE SDR SWAA2022012050796Angle · crackedCRACK ANGLE LOCATED BS695 AND LBL24 AT PASSENGER CABIN ; 2021-557792 / [01] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 22-JAN-22; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 22-JAN-22.; [02] REPSDR SWAA2021122251093Structure · crackedLT A/C BAY, BS 663, LBL 9.5; LOWER CHORD IS CRACKED. REMOVED DAMAGED SECTION IAW SRM 57-10-10-2R-5. REPLACEMENT ANGLE FABRICATED & -2 SPLICE ANGLE FABRICATED IAW SRM 57-10-10-2R-5. PERFORMED DETAILED INSP OF REPAIR AREA AND UNDERLYING STRUCTURE, NO DEFECTS SDR SWAA2021122251099Angle · crackedA113-09 R/H A/C BAY STA 663; RBL 9.5; CENTER WING BOX LOWER CHORD IS CRACKED. ; / [01] REMOVED DAMAGED ATTACHED ANGLE FROM L/H SIDE OF STA 663. IAW SRM 57-10-10-2R-5.SDR SWAA2021122040179Vapor Barrier · crackedSUPPLEMENTAL INFORMATION: WING CENTER SECTION STA 663.75 RH LOWER PRESSURE WEB (VAPOR BARRIER) HAS A CRACK BETWEEN RBL 6.15 AND RBL 14 ; / [01] REMOVED R/H AIR MIX VALVE AND ADJACENT DUCTS FOR MAINTENANCE ACCESS AS REF B737 AMM 21-61-02-000-801 AND 36-13-01-00SDR CALA2021102501960Bulkhead · crackedRIGHT MAIN GEAR WHEEL WELL, CENTER WING BOX REAR SPAR VERTICAL WEB AT STA 663, RBL 42 , APROX 5" FROM CEILING, HAVE A CRACK INDICATION REF FLEETCYCLE LOG PAGE 9786602 INITIATED DIP TO PERFORM INSPECTIONS AS GIVEN IN TABLE FLIGHT CYCLE INTERVALS. INSPECTION METSDR CALA2021102501961Spar · crackedLEFT MAIN GEAR WHEEL WELL, CENTER WING BOX REAR SPA VERTICAL WEB, STA 663 LBL 34.83, AND APPROX. 4" FROM CEILING, HAVE A CRACK INDICATION REF FLEET CYCLE LP# 9786603. THIS LP IS FOR DIP AND ESFR ONLY. REPAIR DISCREPANCY REF SRM 57-10-10 2R-3 ALT 2. SEE LP# 978SDR SWAA2021112329055Stiffener · crackedCRACK STIFFENER FLOOR STRUCTURE LOCATED BS540 BTW BL0 TO RBL24.75 CENTER SECTION ; 2021-460684 / [01] TOOL USED:ELECTRONIC CALIPER P/N:2340A11;S/N:B17119106;DUE DATE:23/SEP/22.; [02] REPLACED STIFFENER FLOOR STRUCTURE LOCATED BS540 BTW BL0 TO RBL24.75 CENTER SSDR AALA202110082601Keelbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING SECTION KEEL BEAM LOCATED AT BS 663 AND LBL 40 TO LBL 45. REPAIRED PER SRM 57-10-10-2R-3.SDR DALA2021092305729None · noneSHIP 3250 CRACK INDICATION ON FRAME 36 ON OPEN HOLE ZONE 2 Y765 LOCATED ON FLOOR BEAM IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPAIRED PER PRI 593608-14AD, REV.0,1,2 AND ERA 593608-14AD REV.ORIGINAL (1957949)SDR DALA2021092305728None · noneSHIP 3250 CRACK INDICATION ON FRAME 36 ON OPEN HOLE ZONE 2 -765 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: PERFORMED REPAIR PER PRI 593608-14AD, REV.0,1,2 AND ERA 593608-14AD REV.ORIGINAL. (1957944)SDR DALA2021092305726None · noneSHIP 3250 CRACK INDICATION ON FRAME 36 ON OPEN HOLE ZONE 1 -Y765 LOCATED FLOOR BEAM FWD CARGO COMPT. CORRECTIVE ACTION: PERFORMED REPAIR PER PRI 593608-14AD, REV.0,1,2 AND ERA 593608-14AD REV.ORIGINAL. (1957933)SDR DALA2021092305725None · noneSHIP 3250 CRACK INDICATION ON FRAME 36 ON OPEN HOLE ZONE 1 -Y254 LOCATED ON FLOOR BEAM IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPAIRED PER PRI 593608-14AD, REV.0,1,2 AND ERA 593608-14AD REV.ORIGINAL. (1957923)
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