JASC 5720
Service difficulty reports · 13,633
Reports filed under 5720 · Wing 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 = '5720' 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 = '5720' 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 SWAA2023092196988Faceplate · corrodedR/W REFUEL PANEL FACEPLATE HAS CORROSION.<[01] REMOVED AND REPLACED P15 REFUEL PANEL I/A/W BOEING AMM 28-21-00-000-801 & 28-21-00-400-801; OPS CHECKS FOUND NORMAL;[02] VERIFIED STEP:1 SYSTEM TEST FOUND NORMALSDR SWAA2023091396179Bracket · crackedRIGHT HAND STA 663 GROUD DISCONNECT BRACKET IS CRACKED<[01] VERIFIED NEW BRACKET AS PART # 276A9183-2 I.A.W BOEING DWG 111A1001<BR><BR>DRILLED NEW BRACKET I.A.W SRM 51-40-05-0G-0 AND BOEING DWG 111A1001;[02] A TAG # FOR BRACKET A201950;[03] INSTALLED BRACKET ISDR SWAA2023100394734Plate · crackedR/H WING T/E WIGGLE PLATE IS CRACKED AT IRSS 220. MRKD<[01] REMOVED; DRILLED UP AND INSTALLED NEW WIGGLE PLATE PER SRM 51-40-02.SDR SWAA2023100394743Angle · crackedR/H WING T/E DEFLECTION CONTROL RIB I/B SIDE L-ANGLE IS CRACKED AT ATTACH FASTENERS. MRKD<[01] REMOVED CRACKED ANGLE.;[02] REJECT: CORRECTIVE ACTION #1 DOES NOT CONTAIN A REFERENCE USED FOR THE WORKED PERFORMED AS REQUIRED PER MPM 51.03.01. SEE FAULT TTG8Q00NBSDR IPXA2023092174790Angle · corroded*** SUPPLEMENTAL SDR *** FAULT - WTB UNDER PANEL 191CL AFT STRUCTURE WITH CORROSION MARKED IN RED APPLIED CIC ON THE REPAIR AREA IAW B757 AMM 51-24-03-377-008. ACCOMPLISHED REPAIR IAW EO-88197-REQ1 AND VT MAE EA 757-5340-27-A3367 REV-. REVIEWED.SDR IPXA2023092074790Angle · unknown**SDR FILED OPEN**FAULT - WTB UNDER PANEL 191CL AFT STRUCTURE WITH CORROSION MARKED IN RED IN REFERRENCE TO STEP 21: VERIFIED PERFORMED DVI IAW B757 SRM 51-10-08, VERIFIED NO ADDITIONAL DAMAGE FOUNDSDR IPXA2023090794114Doubler · crackedINSPECTION TYPE:2CL/H WING FIXED L/E BEADED DOUBLER AT STA XORS= 772 HAS A CRACKED.REPAIRED CRACKED BEADED DOUBLER AT THE L/H WING FIXED L/E AT STA XORS=772 IAW SRM 57-40-02 REPAIR 15 FIG 205 (MAJOR)SDR DALA2023083007072Unknown · unknownSFIP 3330 CRACK SUPPORT BRACKET ATTACHMENT TO SLAT TRACK 1 RH WING. CORRECTIVE ACTION: REPLACED SUPPORT BRACKET ATTACHMENT ON SLAT TRACK 1 RH WING AS PER A330 SRM 51-42 AND SRM 51-72 AND AS PER A330 AMM 27-84. (2943569)SDR DALA2023083007071Unknown · unknownSHIP 3330 CRACK SUPPORT BRACKET ATTACHMENT TO SLAT TRACK 1 ON LH WING. CORRECTIVE ACTION: REPLACED SUPPORT BRACKET ATTACHMENT ON SLAT TRACK 1 LH WING AS PER A330 SRM 51-42 AND ARM 51-72. (2943584)SDR SWAA2023092694504Plate · brokenLEFT WING LOWER TRAILIING EDGE WIGGLE PLATE @RSS 261 ABOVE #1 PYLON AFT TIP O/B FASTENER BROKEN<[01] REMOVED AND REPLACED WIGGLE PLATE AT ORSS 261 IAW SRM 51-40-02-0G-0; AIPC 57-50-00-30 ITEM 345 & BAC DRAWING #115A2001 SH29.<BR>UPDATED PART REQUIREMENT.;[02] SDR SWAA2023092694617Support Angle · crackedRIGHT WING UPPER FIXED T/E PANEL BETWEEN #7 AND #8 SPOILERS; LOWER SURFACE SUPPORT ANGLE IS CRACKED AT TRANSVERSE WEB LOWER ATTACH POINT<[01] REMOVED AND REPLACED RIGHT WING UPPER FIXED T/E PANEL BETWEEN #7 AND #8 SPOILERS; LOWER SURFACE SUPPORT ANGLE CRACKED SDR SWAA2023092694619Support Angle · crackedLEFT WING; UPPER T/E PANEL BETWEEN SPOILERS #5 AND #6; LOWER SURFACE SUPPORT ANGLE IS CRACKED AT TRANSVERSE WEB LOWER ATTACH POINT<[01] REMOVED AND REPLACED RIGHT WING UPPER FIXED T/E PANEL BETWEEN #5 AND #6 SPOILERS; LOWER SURFACE SUPPORT ANGLE CRACKED AT TRASDR SWAA2023092694615Support Angle · crackedLEFT WING; T/E COVE SEAL SUPPORT ANGLE CRACKED AT UPPER ATTACH POINT ABOVE #1 PYLON AFT TIP<[01] REMOVED AND REPLACED LT WING T/E COVE SEAL SUPPORT ANGLE ABOVE #1 PYLON IAW MM 20-50-11-910-801<BR>CAL TOOL ID#PER2331 DUE 03/2024; PER2300 DUE 09/2023;[02] VERIFISDR FDEA202308281513Stiffener · crackedRIGHT WING - LEADING EDGE COMPARTMENT LOWER SUPPORT STIFFENER AT STATION XOS 542 FOUND CRACK. RIGHT WING - LEADING EDGE COMPARTMENT LOWER SUPPORT STIFFENER AT STATION XOS 542 REMOVED AND FABRICATED STIFFENER PER DOUGLAS DRAWING ARB2918 REVISION G. INSTALSDR SWIA20230906827Unknown · gougedRH. WING FIXED LEADING EDGE HAVE GOUGING ON UPPER SURFACE AT RIB 32. (C-CHECK RO 9/3/2023) REPAIRED GOUGE IN R/H WING FIXED LEADING EDGE BY WAY OF CUTTING OUT DAMAGE AND INSTALLING FILLER, SHIM AND DOUBLER REF EMB ETD2023-170-021618. WEIGHT OF REPAIR PASDR SWAA2023100393945Retainer · crackedLT WING UNDER FIXED T/E I/B OF DEFLECTION CONTROL RIB VERTICAL SEAL RETAINER IS CRACKED. 124-014<[01] REMOVED AND REPLACED AT LT WING UNDER FIXED T/E I/B OF DEFLECTION CONTROL RIB VERTICAL SEAL RETAINER REF 51-40-02-0G -0;[02] VERIFIED 1.SDR SWAA2023100393946Support Bracket · crackedLT WING FIXED T/E I/B OF DEFLECTION CONTROL RIB SEAL RETANER SUPPORT BRACKET IS CRACKED. 124-016<[01] REMOVED AND REPLACED LT WING FIXED T/E I/B OF DEFLECTION CONTROL RIB SEAL RETANER SUPPORT REF SRM 51-40-02-0G-0;[02] VERIFIED 1.SDR SWAA2023100393944Support Bracket · crackedLT WING FIXED T/E LATERAL SUPPORT PANEL O/B BRACKET IS CRACKED AT DEFLECTION CONTROL RIB ATTACHMENT. 124-013<[01] REMOVED AND REPLACED DAMAGE BRACKET AT LT WING FIXED T/E LATERAL SUPPORT PANEL SRM51-40-02-0G-0 AND DWG115A6200;[02] VERIFIED CORRECTIVE ACTION.SDR SWAA2023100301094Bracket · corrodedREFUELING PANEL P15 LIGHT CORRISION AROUND REFUELING QTY INDICATORS OPENINGS<[01] REMOVED REFUEL PANEL (P15) AS PER REF AMM 28-21-00-000-801. REPLACED P15 INDICATOR FACEPLATE/BRACKET ASSY PER TASK 28-41-61-000-801 AND AMM 28-41-61-400-801. REPLACED CENTER DEFUSDR SWAA2023100292625Plate · crackedIB AND OB SEAL STRIKE PLATES CRACKED IB AND OB SEAL STRIKE PLATES CRACKED. #1 AFT FLAP TRACK FAIRING #544BB<[01] STEP 1 COMPLETE;[02] STEP 2 COMPLETE;[03] VERIFIED STEP 2 COMPLETE.;[04] REMOVED AND REPLACED I/B AND O/B SEAL STRIKE PLATE ON #1 AFT FLAPTRACK FAISDR SWAA2023100292626Plate · crackedPANEL 543BB IB/OB MID SEAL STRIKE PLATES CRACKED<[01] PARTIAL UPDATE STEP 1;[02] STEP 2 COMPLETE;[03] VERIFIED STEPS 2 COMPLETE.;[04] REMOVED AND REPLACED I/B AND O/B SEAL STRIKE PLATE ON 543BB AFT FLAPTRACK FAIRING IAW AMM 27-51-28-820-802;[05] VERIFIED STEPSSDR SWAA2023092592890Angle · crackedCRACK ANGLE ON INBOARD AUXILIARY SLAT TRACK SLAT 8 AT RT WING 2023-530942<[01] REPLACED ANGLE ON INBOARD AUXILIARY SLAT TRACK SLAT 8 AT RT WING IAW B737-700 SRM 51-40-02; TOOL USED DIGITAL<BR>PN: 500-1096-30<BR>SN: A20227391<BR>DUE DATE: 11-OCT-23;[02] CORRECTSDR SWAA2023100392756Support Bracket · crackedR/W T/E ACCESS PANEL 651AT FWD PANEL SUPPORT BRACKET CRACK.<[01] REMOVED AND REPLACED CLIP (BRACKET); AT R/W T/E ACCESS PANEL 651AT FWD PANEL SUPPORT BRACKET.PER B737-700 SRM 51-40-02-0G-0;[02] VERIFIED STEP 1.SDR SWAA2023100392757Panel · corrodedCORROSION FOUND R/W REFUELING PANEL HAS SPOTS OF CORROSION.<[01] REMOVED REFUEL PANEL PER REF. AMM 28-21-00-000-801. TRANSFER COMPONENTS AND HARDWARE TO THE NEW METAL PANEL PER REF. AMM 20-50-11-910-801. INSTALLED REFUELING PANEL (P15) FOR R/W PER REF. AMM 28-SDR SWAA2023092692744Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS261 AT LT WING 2023-530894<[01] REPLACED CORRUGATED PLATE LOCATED ON TRAILING EDGE LOCATED ORSS261 AT LT WING IAW B737-700 SRM 51-40-02 AND DWG 115A2001; SHEET 32.;[02] COMPLETE TASK CERTIFIEDSDR SWAA2023092692745Support Bracket · crackedCRACK TRAILING EDGE SUPPORT BRACKET LOCATED ORSS272 AT LT WING 2023-530895<[01] REPLACED TRAILING EDGE SUPPORT BRACKET LOCATED ORSS272 AT LT WING I.A.W. B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02. DWG: 115A2930 SHEET:7 REV: -. DUE TO NOT FOUND ALLOWABLE DAMSDR SWAA2023092692746Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS241 AT LT WING 2023-530896<[01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS241 AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9. AND DRAWING # 115A2001 REV: A. SEE INDIVIDUAL SIGN OFF BELOW;[02] CORRECTED STSDR SWAA2023092592748Angle · crackedCRACK ON ANGLE BODY STATION 663 RBL 41.10 AT LOWER FUSELAGE 2023-530908<[01] TOOL USED ET EQUIPMENT: P/N: NORTEC 600D; S/N: 210138203; CAL DUE DATE: 09-JUN-24;[02] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 25-JAN-24.;[03SDR 2024FA0000026Stiffener · crackedFOUND RIGHT WING LOWER, INBOARD, FORWARD SKIN, AFT STIFFENER CRACKED. REPLACED
STIFFENERSDR 2024FA0000025Stiffener · crackedFOUND RIGHT WING LOWER, INBOARD, FORWARD SKIN, FORWARD STIFFENER CRACKED. REPLACED
STIFFENERSDR SWAA2023092691991Panel · brokenBROKEN ANGLE ACCESS PANEL 651FB TRAILING EDGE AT RT WING 2023-530820<[01] REPLACED ANGLE LOCATED ON ACCESS PANEL 651FB TRAILING EDGE AT RT WING IAW B737-700 SRM 51-10- 02 ITEM 9;[02] CORRECTIVE ACTION CERTIFIEDSDR SWAA2023082490484Angle · crackedDOT A24-1 LH WING I/B L/E. LEADING EDGE / PANEL SUPPORT ANGLE CRACKED AT FORWARD LOWER CORNER FOR PANEL 195AL.<[01] VERIFIED <BR>AUDIT C/WSDR SWAA2023090690402Support Angle · crackedCRACK ON SUPPORT ANGLE ACCESS PANEL 191FR FORWARD UNDER WING RT 2023-491866<[01] REPLACED SUPPORT ANGLE ACCESS PANEL 191FR FORWARD UNDER WING RT IAW SRM B737-700 51-40-02; SRM 51-10-02 ITEM 9 AND DRWING 116A2300 SHEET 5 REV.- <BR>SEE INDIVIDUAL SIGN OFF BELOW.SDR SWAA2023090190773Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED ON ACCESS PANEL 651GB AT RT WING 2023-508530<[01] REPLACED NEW SUPPORT ANGLE LOCATED ON ACCESS PANEL 651GB AT RT WING IAW B737-700 SRM 51-10-02 PARAGRAPH 9; SRM 51-40-02;[02] REPLACED NEW SUPPORT ANGLE LOCATED ON ACCESS PANEL 651SDR SWAA2023083190365Angle · crackedRIGHT WING LOWER TRAILING EDGE PANEL 651EB SUPPORT ATTACH BRACKET CRACKED AT I/B FORWARD CORNER OF PANEL. (51-001)<[01] REMOVED AND REPLACED CRACKED SUPPORT ATTACH ANGLE AT RIGHT WING LOWER TRAILING EDGE PANEL 651EB AT I/B FORWARD CORNER AS PER SRM 51-40-02-0GSDR SWIA202310230001Unknown · damagedRIGHT WING LOWER WING PLANK ACCESS HOLE 640AB IS PITTED AND HS PIN HOLES. FLAGGED (C-CHECK RO 10/21/2023) BLENDED AROUND WING PLANK ACCESS HOLE 640AB AND COMPLIED WITH ALL STEPS OF REO 601R-57-21-030 REV-L DATE: 2014-02-05,BLEND IS WITHIN LIMITS, COMPLIEDSDR SWAA2023092589562Support · cracked(RIGHT WING) UPPER SURFACE PANEL BETWEEN #5 AND #6 SPOILERS; LOWER SURFACE SUPPORT GUSSETT IS CRACKED AT LOWER ATTACH FASTENER<[01] CORRECTION TO NRC; GUSSETT IS BETWEEN #7 AND 8 SPOILERS RIGHT WING;[02] REMOVED AND REPLACED (RIGHT WING) UPPER SURFACE PANEL BESDR SWAA2023090189305Angle · crackedCRACK INBOARD TRAILING EDGE TEE ANGLE LOCATED ON IRSS 211 AT RT WING 2023-508488<[01] REPLACED ANGLE LOCATED ON IRSS 211 AT RT WING.IAW. B737-700 SRM 51-10-02-0G-0 ITEM 9; SRM 51-40-02-0G-0 AND DWG 115A2001 SHEET 8 REV: . TOOL USED: ELECTRONIC CALIPER. P/N: 50SDR SWAA2023090189123Support Angle · crackedCRACK ANGLE TRAILING EDGE ORSS 261 PLUS 11 INCHES; AT DEFLECTION RIB AREA; RT WING 2023-508464<[01] REPLACED ANGLE TRAILING EDGE ORSS 261 PLUS 11 INCHES; AT DEFLECTION RIB AREA; RT WING IAW B737-700 SRM 51-10-02 Ï¿½TEM 9 AND DRAWING 115A2930 SHEET 8 REV -;[02]SDR SWAA2023090189118Angle · crackedCRACK ANGLE FRONT SPAR WEB LOCATED BOOST PUMP BONDING STRAP AT IFSS 121 AT LT WING 2023-508460<[01] REPLACED ANGLE FRONT SPAR WEB LOCATED BOOST PUMP BONDING STRAP AT IFSS 121 AT LT WING IAW B737-700 SRM 51-10-02.SEE INDIVIDUAL SIGN OFFS BELOW;[02] REPLACED ANGSDR SWAA2023090189122Web · crackedCRACK ANGLE FRONT SPAR WEB LOCATED BOOST PUMP BONDING STRAP AT IFSS 121 AT RT WING 2023-508461<[01] REPLACED ANGLE FRONT SPAR WEB LOCATED BOOST PUMP BONDING STRAP AT IFSS 121 AT RT WING IAW B737-700 SRM 51-10-02.SEE INDIVIDUAL SIGN OFFS BELOW;[02] JOB COMPLETESDR SWAA2023090188872Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED ORSS 261 PLUS 11 INCHES; DEFLECTION RIB AREA LT WING 2023-508425<[01] REPLACED ANGLE TRAILING EDGE LOCATED ORSS 261 PLUS 11 INCHES; DEFLECTION RIB AREA LT WING IAW B737-700 SRM 51-40-02-0G-0 AND SRM 51-10-02-0G Ï¿½TEM 9;[02] TSDR 2024FA0000023Stiffener · crackedFOUND RIGHT WING LOWER, INBOARD, FORWARD SKIN, AFT STIFFENER CRACKED. REPLACED
STIFFENERSDR SWAA2023082488450Plate · crackedRIGHT WING T/E LOWER WIGGLE PLATE CRACKED AT ORSS 260<[01] REMOVED CRACKED WIGGLE PLATE AT RIGHT WING T/E ORSS 260 AND BEGAN INSTALLATION OF NEW WIGGLE PLATE IAW SRM 51-40-02-0G-0;[02] COMPLETED INSTALLATION OF NEW WIGGLE PLATE; SEALANT AND RESTORATION OF PAINSDR SWAA2023082488449Plate · crackedLEFT WING T/E LOWER WIGGLE PLATE CRACKED AT ORSS 260<[01] REMOVED CRACKED WIGGLE PLATE ON L/W T/E AT ORSS 260 AND TEMPORARILY SECURED NEW WIGGLE PLATE IN PLACE WITH CLECOS IAW SRM 51-40-02-0G-0;[02] CONTINUED INSTALLATION OF NEW WIGGLE PLATE IAW SRM 51-40-02-0SDR IPXA2023081693926Support Bracket · crackedINSPECTION TYPE:3CL/H WING O/B FLAP I/B HINGE FOUND O/B SUPPORT BRACKET CRACKED AT STA XORS=538 .REMOVED, REPLACED CRACKED SUPPORT BRACKET AT THE L/H WING O/B FLAP I/B HINGE AT STA XORX=538 IAW SRM 51-31-01 AND AMM 20-50-02. (MINOR)SDR SWAA2023090787508Support Angle · crackedCRACK OUTBOARD TRAILING EDGE SUPPORT ANGLE LOCATED ORSS279 AT RT WING 2023-490657<[01] REPLACED SUPPORT ANGLE LOCATED OUTBOARD TRAILING EDGE ORSS279 AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 115A6200 REV. -; MEASURE OF CRACK IS: L= 0.81SDR SWAA2023090787701Support · crackedCRACK ANGLE TRAILING EDGE SUPPORT LOCATED ORSS 261 PLUS 11 INCHES ON DEFLECTION CONTROL RIB AREA AT LT WING 2023-490672<[01] REPLACE SUPPORT ANGLE ON TRAILING EDGE LOCATED ORSS 261 PLUS 11 INCHES ON DEFLECTION CONTROL RIB AREA AT LT WING IAW B737-700 SRM 51-40SDR SWAA2023090787707Support Angle · crackedCRACK SUPPORT ANGLE LOWER SURFACE REAR SPAR LOCATED TRAILING EDGE ORSS 261 PLUS 20 INCHES LT WING 2023-490679<[01] REPLACED SUPPORT ANGLE LOWER SURFACE REAR SPAR LOCATED TRAILING EDGE ORSS 261 PLUS 20 INCHES LT WING IAW B737-700 SRM 51-40-02 AND DWG 115A7112 RSDR SWAA2023082487322Support Bracket · crackedRT WING T/E PANEL 651FB FWD CENTER SUPPORT BRACKET IS CRACKED<[01] REMOVED AND REPLACED CRACKED FWD SUPPORT BRACKET ON PNL 651FB PER SRM 51-40-02-0G-0;[02] ADD REFERENCE SOPM 20-50-02;[03] VERIFIED CORRECTIVE ACTION #1.
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