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 UIEA2024052600451Support Rod · corrodedLHW T/E UPR FIXED PANEL RIB SUPPORT ROD LOWER FITTING P/N : 69B11633-13 FOUND CORROSION(<P>LHW T/E UPR FIXED PANEL RIB SUPPORT ROD LOWER FITTING P/N: 69B11633-13 AND BRACKET P/N: 65B81991-41 REPLACED AND INSTALLED IAW RI-57-00-16905 REV A. NO FURTHER DEFECTS NSDR SWAA2024071690029Angle · crackedCRACK ON SUPPORT ANGLE LOCATED ORSS 251 AREA OF DEFLECTION CONTROL RIB AT LT TRAILING EDGE 2024-345552<[01] REPLACED SUPPORT ANGLE LOCATED ORSS 251 AREA OF DEFLECTION CONTROL RIB AT LT TRAILING EDGE IAW B737-700 SRM 51-10-02; B737-700 SRM 51-40-02 AND DRAWING SDR UIEA2024052300421Vent · misinstalledRIGHT WING MAIN, TANK, BETWEEN RIB 19 AND RIB 18, FUEL DUCT VENT, LOCKWIRE MISSING ON BOTH NUT RETAINER(<P>RIGHT WING MAIN TANK, BETWEEN RIB 19 AND RIB 18, FUEL DUCT VENT, LOCKWIRE WAS INSTALLED CORRECTLY IAW AMM 20-10-23-420-801 REV 142, APR 22,2023; TORQUE ASDR SWAA2024070290037Web · crackedR/W T/E UPPER SURFACE PANEL AT ORSS 280 LOWER TRANSVERSE WEB CRACKED AT O/B UPPER FASTENER<[01] REMOVED AND REPLACED TRANSVERSE WEB AT R/W T/E UPPER SURFACE PANEL AT ORSS 280 IAW SRM 51-40-02 0G-0 PARA. 4.;[02] VERIFIED CORRECTIVE ACTION #1SDR SWAA2024062889890Angle · crackedCRACK ANGLE TRAILING EDGE ORSS 271 RT WING 2024-341118<[01] REPLACED ANGLE LOC. TRAILING EDGE ORSS 271 RT WING IAW B737-700 SRM 51-40-02; SRM 51-10-02 Ï¿½TEM 9 AND DWG 115A2930 SHEET: 8 REV: -<BR>SEE INDIVIDUAL SIGNS OFF BELOW.;[02] REPLACED ANGLE LOC. TRAILINSDR SWAA2024062889891Angle · crackedCRACK ANGLE TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA LT WING 2024-341119<[01] REPLACED ANGLE LOC. TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA LT WING IAW B737-700 SRM 51-40-02; SRM 51-10-02 Ï¿½TEM 9 AND DWG 115A2930 SHEET: 7 REV: -.<BR>SEE INDSDR SWAA2024062889888Support Bracket · crackedCRACK SUPPORT BRACKET ORSS 271 DEFLECTION CONTROL RIB AREA LT WING 2024-341120<[01] REPLACED SUPPORT BRACKET LOC. ORSS 271 DEFLECTION CONTROL RIB AREA LT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02;[02] REPLACED SUPPORT BRACKET LOC. ORSS 271 DEFLECTSDR SWAA2024062889892Angle · crackedCRACK ANGLE TRAILING EDGE ORSS 297 LT WING 2024-341121<[01] REPLACED ANGLE ON TRAILING EDGE ORSS 297 LT WING IAW BU737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG: 115A3700 SHEET: 38 REV - SEE INDIVIDUAL SIGNOFFS BELOW;[02] CORRECTED STEP 1 <BR>REPLACED ANGLSDR SWAA2024070189083Support Angle · crackedUPPER FIXED TRAILING EDGE PANEL I/B OF #5 SPOILER LOWER ANGLE BRACKET CRACKED. REMOVED DEFLECTION RIB CLIP FROM AIRCRAFT I.A.W SRM 51-40-02.. LOCATED AND DRILLED NEW DEFLECTION RIB CLIP I.A.W SRM 51-40-05. INSTALLED DEFLECTION RIB CLIP I.A.W SRM 51-40-02SDR SWAA2024062589194Plate · damagedLH WING DEFLECTOR RIB ATTACH SERRATED PLATE HOLES ELONGATED<[01] REMOVED BOLTS AT L/H WING DEFLECTOR CONTROL RIB UPPER TAB IN REF B737-700 SRM 51-40-02-0G-0; AFTER FURTHER INSPECTION FOUND NO ENLONGATED HOLES; AND NO SERRATED PLATES DAMAGE; REPLACED BOLTS IN RSDR SWAA2024062589196Bracket · corrodedEVIDENCE OF CORROSION UNDER SEALANT AT LEFT AFT BOOST PUMP BONDING STRAP<[01] REMOVED AND REPLACED BOTH UPPER AND LOWER BONDING STRAPS/BRACKETS AT LEFT WING AFT BOOST PUMP IAW SRM 51-40-02-0G-0; AIPC 28-22-41-05; AMM 20-10-44-400-801. PERFORMED ELECTRICAL RESISDR A6WA202405238752Bracket · corrodedCORROSION ON BRACKET AT WS 48.30 AT LH TE WING. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED BRACKET AT WS 48.30 AT LH TE WING REF. CRJ-200 SRM 51-42-06 AND 51-42-20 REV. 39. RESTORED PROTECTIVE FINISH. ALL WORK PERFORMED UNDER AERSALE WORK ORDER SDR SWAA2024062688507Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED IRSS 215 AT RT WING 2024-335908<[01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED IRSS 215 AT RT WING I.A.W B737-800 SRM 51-10-02;[02] CORRECTED STEP 1 REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED IRSS 215 AT SDR SWAA2024053188344Web · crackedR/H WING VERTICAL WEB LOCATED JUST INBOARD OF DEFLECTION RIB AT WS 278.5 IS CRACKED AT OUTBOARD HOLE.<[01] REMOVED CRACKED VERTICAL WEB PER SRM 51-40-02. DRILLED REPLACEMENT WEB PER SRM 51-40-05.;[02] 02 - INSPECTED PER [SRM 51-40-02-0G-0-B00069 (GENERAL - FASSDR CALA2024052201555Angle · crackedCENTER WING RBL VAPOR BARRIER AROUND RBL 04 SUPPORT ANGLE HAS A CRACK REF AAR N/R 9888725 CUTOUT DAMAGED VAPOR BARRIER ANGLE AT RBL 04 TO RBL 17 STA 663 AND INSTALLED REPAIR REF B737 SRM 57-10-10-2R-5 REPAIR 5SDR SWAA2024061186760Bracket · crackedPANEL 551GB HAS A BULB SEAL RETAINING BRACKET CRACKED ON THE OUTBOARD CORNER.<[01] REMOVED AND REPLACED BULB SEAL RETAINING BRACKET PER SOPM 20-50-01.;[02] INSPECTION C/WSDR SWAA2024061186730Bracket · corrodedRH WING FUEL GAUGE MOUNT BRACKET HAS CORROSION AT #1 TANK GAUGE (MARKED)<[01] REPLACED R/H WING REFUELING PANEL; PANEL.& INSTALLED PER MM 28-41-61 & WDM 28-44-11;[02] VERIFIED REPLACED R/H WING REFUELING PANEL; PANEL.& INSTALLED PER MM 28-41-61 & WDM 28-44-11SDR IXXA2024051701Bracket · corrodedHYDRAULIC LINE BLOCK CLAMP BRACKET CORRODED.SDR 2024FA0000864Stiffener · crackedL/H WING I/B FWD TOP SKIN, FWD STIFFENER CRACKEDSDR SWAA2024060686536Support Bracket · damagedELONGATED HOLE SUPPORT BRACKET LOCATED IB LEADING EDGE AT LEVEL IFSS 151 AT LT WING 2024-318209<[01] REPLACED SUPPORT BRACKET LOCATED IB LEADING EDGE AT LEVEL IFSS 151 AT LT WING IAW B737-800 SRM 51-40-02 AND SRM 51-40-04.;[02] REPLACED SUPPORT BRACKET LOCATEDSDR SWAA2024061398186Support Beam · wornL/H WING TRAILING EDGE; DEFLECTION SUPPORT BEAM HAS WEAR MARKS AT THE TAB ATTACHED TO THE UPPER TRAILING EDGE PANEL.<[01] REMOVED DAMAGE ON LH WING INBD FIXED T/E DEFLECTION CONTROL RIB AND INBD SUPPORT BEAM MATERIAL LOSS .045; MAX ALLOWED .040; FOUND TO BE OUSDR SWI2024F00594Bracket · crackedRIGHT WING SLAT TRACK 1-3 CANNISTER BRACKET APPEARS CRACKED. HN00160033 (C-CHECK RO 7/17/2024) PERFORMED REPAIR TO RH WING SLAT TRACK CANNISTER. REF REO 670-57-42-577 REV -- DATED 2016-12-02. NO LEAKS NOTED AND COMPLIED WITH TASK CARD 51-900-1002-SKY.SDR VNAA20240523007Canister · crackedDISCREPANCY: CRACK IN CANISTER, WELDED NO.3 IN STA. WS148 OF INTERNAL LH MAIN FUEL TANK. CRACK IN CANISTER, WELDED NO.3 IN STA. WS148 OF INTERNAL LH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577 REV --SDR SWAA2024060684946Angle · crackedCRACK ANGLE TRAILING EDGE ORSS 280 DEFLECTION CONTROL RIB AREA LT WING 2024-318124<[01] REPLACED ANGLE ON TRAILING EDGE ORSS 280 DEFLECTION CONTROL RIB AREA LT WING IAW B737-800 SRM 51-40-02-0G AND DWG 115A6200 SHEET 24 REV A;[02] COMPLETED TASK CERTIFIEDSDR SWAA2024060684945Angle · crackedCRACK ANGLE TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA LT WING 2024-318123<[01] REPLACED ANGLE LOC. ON TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA LT WING IAW B737-800 SRM 51-40-02-0G-0 AND DWG 115A2930 SHEET 17 REV -. MEASURES OF THE CRACK ARE:SDR IXXA2024051106Bracket · cracked#6 SLAT CLOSE OUT PANEL BRACKET CRACKED.SDR IXXA2024051103Bracket · crackedSLAT BRACKET CRACKED RT LE STA. 270SDR IXXA2024051102Bracket · crackedRW LE STA. 278 HAS CRACKED BRACKETSDR IXXA2024051101Bracket · crackedRW LE BRACKET CRACKED.SDR UIEA2024050800363Bracket · corrodedLEFT WINGLET, RIB BRACKET CORROSION WBL 1243.750(<P>1. REMOVE DAMAGE PART IAW SRM 51-40-02-0G-0 REV 100. 2. INSTALL NEW PART IAW SRM 51-40-02-0G-0 REV 100 AND DWG 11245700 SHEET 1 REV C 3. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)SDR SWAA2024060483457Angle · crackedCRACK BRACKET ANGLE LOCATED ACCESS PANEL 651FB AT RT WING 2024-293939<[01] REPLACED BRACKET LOCATED ON ACCESS PANEL 651FB AT RT WING IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 PARAGRAPH 9.;[02] CORRECTED STEP 1: <BR>REPLACED BRACKET LOCATED ON ACCESS PANEL 651SDR SWAA2024050983281Strake · crackedLEFT VENTRAL STRAKE HAS A CRACK PROPAGATING APPROX 1.5 INCHES FROM THE TRAILING EDGE<[01] REMOVED AND REPLACED LEFT WING VENTRAL STRAKLET PER AMM 57-22-01.SDR SWAA2024052982745Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED ORSS 267 RT WING. REPLACED ANGLE ON TRAILING EDGE LOCATED ORSS 267 IAW SRM 51-40-02;SRM 51-10-02 AND DWG 115A2930 SHEET: 8 REV. -. MEASURES OF CRACK IS : L=1.062 INCH.SDR SWAA2024052982817Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS450 TO ORSS472 AT LT WING. REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS450 TO ORSS472 AT LT WING IAW SRM 51-10-02 ITEM 9 AND INSTALLED FASTENERS IAW SRM 51-40-02 AND DRAWING # 115A3760 REV -.SDR SWAA2024052982820Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED DEFLECTION CONTROL RIB AREA ORSS269 AT LT WING. REPLACED ANGLE TRAILING EDGE LOCATED DEFLECTION CONTROL RIB AREA ORSS269 AT LT WING IAW B737-700 SRM 51-10-02; B737-700 SRM 51-40-02 AND DRAWING 115A2930 SH 8; REV -.SDR SWAA2024052982815Angle · crackedCRACK ANGLE TE LOCATED DEFLECTION CONTROL RIB AREA ORSS 275 AT LT WING. REPLACED ANGLE AND FASTENERS TRAILING EDGE LOCATED DEFLECTION CONTROL RIB IAW SRM 51-40-02; SRM 51-10-02,ITEM 9 AND DWG 115A6200 SHEET 11 REV B. MEASURE OF CRACK IS: L 1.727.SDR SWAA2024052982819Web · crackedCRACK WEB TE LOCATED DEFLECTION CONTROL RIB AREA ORSS 272 AT LT WING. REPLACED WEB AND FASTENERS TRAILING EDGE LOCATED DEFLECTION CONTROL RIB AREA ORSS 272 AT LT WING IAW SRM 51-40-02, SRM 51-10-02, ITEM 9 & DWG 115A2512, SHEET 14, REV A. MEASURE OF CRACK ISSDR SWAA2024052982746Web · corrodedCORRODED WEB, FUEL INDICATOR LOCATED INTERNAL CAVITY LE AT RT WING. PERFORMED PERMANENT REPAIR ON WEB IAW EA 24-157-01348 AND EA 24-157-01348-WIP1.SDR YENA2024050700713Grommet · corrodedDURING HEAVY MAINTENANCE: CORROSION DRY BAY LOCATED ON O/B GROMMET AREA AT RIB 5 ON FALSE SPAR B OX ON RH WING (CPCP RELATED MPD TASKS 575150-01); REF WO # 2024-44/1 NR # 2024-149245 REMOVED CORROSION AND EVALUATED REWORKED AREA LOC. ON HOLE BORE OF THE GEAR SSDR UATA202406105702Profile · crackedFOUND A CRACKED PROFILE ON THE AFT FALSE SPAR OF THE LH WING AT STA 2820. PROFILES AT FURTHER OUT STATIONS HAVE INSPECTIONS REQUIRED BY AN AD NOTE 98-12-28 WHICH DIDN'T COVER THIS PROFILE. THE CRACKED PROFILE WAS REMOVED AND ANOTHER PROFILE FABRICATED TO REPSDR FDEA202405030569Support Fitting · crackedAFTER INSPECTION AT L/H WING SKIN, DRAG FITTING O/B FOUND #5 AND #13 HOLE WITH CRACK INDICATION. ACCOMPLISHED EA # F-5730-T0378855 P1 TITLE: WINGS - PLATES AND SKINS - LH WING UPPER SKIN AT DRAG FITTING, HOLE #5 AND #13, CRACK REPAIRED *THIS EA DEVIATES FRSDR SWAA2024052981706Web · crackedLEFT WING DEFLECTOR RIB CONTROL FIXED PANEL LOWER HORIZONTAL BULB SEAL RETAINER WEB CRACKED @ O/B END. REMOVED AND INSTALLED NEW WEB RETAINER AT LEFT WING DEFLECTOR RIB CONTROL FIXED PANEL LOWER HORIZONTAL AS PER SRM-51-40-02-0G-0. VERIFIED STEP 1 FINAL AUDSDR SWAA2024052182018Strake · corrodedL/H WINGLET AREA; STRAKE HAS CORROSION AT THE TIP AREA.<[01] REMOVED CORROSION FROM AREA IAW B737-800 SRM 57-31-01. ORIGINAL THICKNESS IS .050'. REMOVED .039' OF MATERIAL. REMAINING THICKNESS IS .011'. FOUND TO BE OUT OF LIMITS. TOOL# T8224M CAL DUE: 07/NOV/24SDR SWAA2024050281465Retainer · crackedL/H WING SEAL RETAINER AT DEFLECTION RIB CRACKED.<[01] REMOVED AND REPLACED SEAL RETAINER IAW SRM 51-40-02.;[02] C/W INSPECTIONSDR SWAA2024052281441Angle · crackedR/W I/B FIXED L/E UPPER SKIN ANGLE FASTENER HOLE IS CRACKED AT KRAS 221<[01] REMOVED AND REPLACED ANGLE IAW SRM 51-40-02-0G-0 AND DWG. 116A4008.SDR SWAA2024050281012Web · crackedRIGHT WING UPPER TRAILING EDGE (BETWEEN SPOILERS 7 AND 8) PANEL SUPPORT ANGLE WEB CRACKED<[01] 01 - REMOVED AND REPLACED WEB PER [SRM 51-40-02-0G-0-B00069 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)]SDR SWAA2024050281011Support Angle · crackedLH WING ANGLE SUPPORT WEB UNDER UPPER TRAILING EDGE FIXED PANEL BETWEEN #5 AND #6 SPOILERS IS CRACKED.<[01] 01 - REMOVED AND REPLACED WEB PER [SRM 51-40-02-0G-0-B00069 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)]SDR SWAA2024052980940Support Angle · crackedBROKEN ACCESS PANEL 551FB SUPPORT ANGLE AT LT WING. REPLACED THE SUPPORT ANGLE ON ACCESS PANEL 551FB IAW SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG: 115A2710 SHEET: 7 REV -.SDR SWAA2024060480760Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED FWD BELLY FAIRING BS500D AND STR19L AT LT WING 2024-293817<[01] REPLACED SUPPORT ANGLE LOCATED FWD BELLY FAIRING BS500D AND STR19L AT LT WING IAW B737-700 SRM 51-40-02 AND DWG 116A3010 SHEET 1 REV H<BR>SEE INDIVIDUAL SIGN OFFS BESDR SWAA2024052080337Intercostal · crackedL/H WING TRAILING EDGE INTERCOSTAL IS CRACKED I/B OF DEFLECTION RIB<[01] FAULT RESOVLED ON N/R TTG8Q00T07WQ;[02] VERIFIED ITEM 1
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