JASC 5720
Service difficulty reports · 13,637
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 CALA2023032700897Tape · wornSPEED TAPE COMING OFF BOTTOM OF RIGHT WING NEAR TIP PERFORMED INTERIM REPAIR PER ECRA 5739-02601, PERMANENT REPAIR TO BE ACCOMPLISHED WITHIN 10 DAYS, OK FOR SERVICE. PERFORMED INTERIM REPAIR PER ECRA 5739-02601, PERMANENT REPAIR TOMC-APPROVAL FROM SC1ELBYC COMSDR FDEA202303240766Web · misalignedAFTER REMOVED BUSH INSTALLED ON CWB(CENTER WING BOX) FR44 BEAM RH CUTOUT DOUBLER(Y-212), FOUND HOLE ECCENTRICITY DEVIATION REAMED AND INSTALLED THE BUSH TO THE DAMAGE HOLE, INSTALLED WITH NEW FASTENER I.A.W FEDEX EA NO:T6-5710-T0303307 A PART.3, SEQ NO:808SDR ABXA2023032841Unknown · unknownDURING C CHECK FOUND WEB STRINGER L-16 CORRODED AND LOCATED AT STA 314.3. 767-200 SRM 57-00-03 DENIES MAINTENANCE TO REPAIR IT AT THIS LOCATION DUE TO THIS REPAIR CANNOT BE COMBINED WITH OR BE INSTALLED WITHIN 10 INCHES (254 MM) OF SKIN AND/OR STRINGER REPAIRSSDR SWAA2023042820018Angle · crackedCRACK ON ANGLE SUPPORT FRONT SPAR WEB LOCATED IFSS 121 FORWARD BOOST PUMP UPPER AREA AT RT WING 2023-200274<[01] TOOL USED: DIGITAL CALIPER; P/N:500-193-30; S/N:0000291; DUE DATE: 12-OCT-23.;[02] FAULT RESOLVED ON OTHER FAULT TTG8Q00JXBL4;[03] FAULT RESOLVED OSDR SWAA2023042720252Support · crackedCRACK ON ANGLE SUPPORT FRONT SPAR WEB LOCATED IFSS 121 FORWARD BOOST P UMP UPPER AREA AT LT WING 2023-200278<[01] FAULT RESOLVED ON OTHER FAULT TTG8Q00JX8UR;[02] FAULT RESOLVED ON OTHER FAULT TTG8Q00JX8URSDR VNAA202302040011Channel · corrodedCORROSION ON SEAL RETAINER STRIP (NUTS STRIP) ON LH/RH WING-TO-FUSELAGE SEAL (VIEW FROM WHEEL WELL AREA) ON WING TRAILING EDGE SEALS. (AYP)
SEAL RETAINER STRIP (NUTS STRIP) ON LH/RH WING-TO-FUSELAGE SEAL WERE REPLACED PER
PER EA 23-C9-57-0305 REV A. SECTISDR SWAA2023042619412Panel · damagedPANEL 521KB DISBONDED AT FWD I/B CORNER.<OUT OF ALLOWABLE LIMITS IAW SRM 57-41-01-1A-1 PARA 4.A.(5).REMOVED DAMAGED PLIES. CLEANED AND PREPARED PANEL IAW SRM 51-70-05-2R-6 PARA 4.A-D.;[02] MEASUREMENT TABLE UPDATED. FABRICATED REPAIR PLIES USING BMS 5-129 TY2 SDR AALA202304044959Link · looseAIRCRAFT IN BASE MAINTENANCE: LEFT WING FLAP TRACK NUMBER 2 AFT FAIRING FITTING BEARING IS LOOSE. REMOVED AND REPLACED WORN NUMBER 2 OUTBOARD FLAP INBOARD TRACK AFT FAIRING SUPPORT LINK.SDR SWAA2023041919289Bracket · elongatedELONGATED HOLE TRAILING EDGE ON SUPPORT BRACKET LOCATED ORSS 273 AT LT WING 2023-191910<[01] REPLACED SUPPORT BRACKET LOCATED ON TRAILING EDGE ORSS 273 AT LT WING IAW B737-700 SRM 51-40-02 AND DWG 115A5300; SHEET 20; REV A. SEE INDIVIDUAL SIGNS-OFF BELOW.;[02]SDR KCSA202303211023Fitting · crackedR/H O/B AILERON WING FITTING HAS EVIDENCE OF CRACKING AT WS1485SDR KCSA202303211022Hinge Fitting · crackedL WING O/B T/E CHORD @ APPROX WS 1488 HAS MARKED CRACKSDR SWIA202305030030Unknown · crackedL/ WING WS 48.3 UPPER FWD BATT ANGLE CRACKED . (C-CHECK RO 4/30/2023) REPLACED L/ WING WS 48.3 UPPER FWD BATT ANGLE WITH NEW PN 600-10204-27 PO# T60652 REF CRJ 200 SRM 51-42-06 AND BOMBARDIER DWG 600-10204 REV M .COMPLIED WITH SKY CARD 51-900-1003 SKY SDR SWAA2023050318382Web · corrodedCORROSION FUEL BOOST PUMP WEB LOCATED IFSS115 AND WS108 AT RT WING 2023-208279<[01] TOOL USED EDDY CURRENT EQUIPMENT P/N NORTEC 600D; S/N 60009161631 DUE DATE 31/JAN/24;[02] ULTRASONIC THICKNESS GAGE P/N:45MG; S/N: 130066701; DUE DATE: 08-APR-23.;[03] EVALUATESDR SWAA2023041918331Bracket · crackedCRACK REAR SPAR BRACKET ORSS 270 AT LT WING 2023-191821<[01] TOOL USED: SOLAR POWER CALIPER; P/N:500-454; S/N: 15045599; DUE DATE: 05-APR-23.;[02] REPLACED REAR SPAR BRACKET AND FASTENERS LOCATED ORSS 270 AT LT WING IAW B737-700 DWG 115A2930 SHEET 7; REV. ? ; SDR SWAA2023041918377Spar · crackedCRACK REAR SPAR AFT POSITION ORSS 270 AT LT WING 2023-191829<[01] REPLACED REAR SPAR AFT POSITION ORSS 270 AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02.;[02] TASK CARD COMPLETEDSDR SWAA2023041918378Bracket · crackedCRACK REAR SPAR AFT POSITION BRACKET ORSS 270 AT RT WING 2023-191838<[01] REPLACED REAR SPAR AFT POSITION BRACKET ORSS 270 AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02.;[02] REPLACED REAR SPAR AFT POSITION BRACKET ORSS 270 AT RT WING IAW B737-7SDR SWAA2023050117997Fitting · crackedL/W REAR SPAR PANEL 551GB WIGGLE FITTING CRACKED INB OF FLAP TRACK NO-3 MKD DPT<[01] REMOVED AND REPLACED L/W REAR SPAR PANEL 551GB WIGGLE FITTING CRACKED INB OF FLAP TRACK NO-3 AS PER SRM 51-40-02-0G-0.;[02] CORRECTION TO STEP 1;<BR>REMOVED AND REPLACED L/W RSDR VNAA202304270025Retainer · corrodedCORROSION ON RETAINER SEALS AT ACCESS PANEL 583AB, 583BB, 683AB, 683BBSDR VNAA202302040010Support Angle · corrodedCORROSION ON MLG ELECTRICAL/HYDRAULIC PROTECTIVE COVER SUPPORT ANGLE (SETTLEMENT AREA OF ACCESS PANEL 642AZ/542AZ) ON LH/RH MLG WHEEL WELL
MLG ELECTRICAL/HYDRAULIC PROTECTIVE COVER SUPPORT ANGLES SETTLEMENT AREA OF ACCESS PANELS 642AZ/542AZ ON LH/RH MLG WHESDR SWAA2023041715723Panel · crackedCRACK ACCESS PANEL 661CB HOLES AT RT WING 2023-185255<[01] TOOL USED: CALIPER P/N:500-197-30 S/N:B20189416 DUE DATE:19-DEC-23;[02] TOOL USED: HOT BONDER P/N: HCS9200B-AV S/N: 18175478 DUE DATE: 24/SEP/23.;[03] TOOL USED: SCALE P/N: SPX621 S/N:8340225441 DUE DASDR SWAA2023031516328Flap Track · looseLEFT WING OUTBOARD AFT FLAP #4 TRACK LOOSE AT AFT ATTACH POINT<[01] REMOVED AND REPLACED LH WING OUTBD AFT FLAP TRACK #4 PER AMM 27-51-26SDR SWAA2023031414508Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED AT FIXED ACCESS PANEL LOWER AREA AT LT WING 2023-119652<[01] TOOL USED CALIPER P/N: 500-196-30:; S/N: A21126170; DUE DATE: 09-NOV-23.;[02] REPLACED ANGLE AND FASTENERS LOCATED ON TRAILING EDGE LOCATED AT FIXED ACCESS PANEL LOWSDR FDEA202303060382Former · crackedRIGHT WING, @ WING STA. 441 CRACKED LEADING EDGE NOSE FORMER. REMOVED AND REPLACED FORMER WITH B67-57-002-02. REF FEDED DRAWING SR67-57-002.SDR SWAA2023032412546Angle · corrodedCORROSION TRAILING EDGE ANGLE LOCATED ORSS 375 UPPER SIDE AT LT WING 2023-165201<[01] REPLACED TRAILING EDGE ANGLE LOCATED ORSS 375 UPPER SIDE AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02.<BR>SEE INDIVIDUAL SIGNOFF BELOW;[02] TASK COMPLETED <BRSDR SWAA2023032412545Angle · corrodedCORROSION TRAILING EDGE ANGLE LOCATED ORSS 407 UPPER SIDE AT LT WING 2023-165200<[01] REPLACED TRAILING EDGE ANGLE LOCATED ORSS 407 UPPER SIDE AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02;[02] CORRECTED STEP 1. REPLACED TRAILING EDGE ANGLE LOCASDR SWAA2023032412553Angle · corrodedCORROSION TRAILING EDGE ANGLE LOCATED ORSS 459 UPPER SIDE AT RT WING 2023-165212<[01] REPLACED TRAILING EDGE ANGLE AND FASTENERS LOCATED ORSS 459 UPPER SIDE AT RT WING IAW B737-700 SRM 51-10-02 ITEM ITEM 9 AND DRAWING # 115A3551 REV - SEE INDIVIDUAL SIGNOFFS BSDR SWAA2023032412555Angle · corrodedCORROSION TRAILING EDGE ANGLE LOCATED ORSS 404 UPPER SIDE AT RT WING 2023-165214<[01] REPLACED ANGLE AND FASTENERS LOCATED ORSS 404 UPPER SIDE AT RT WING IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 SEE INDIVIDUAL SIGN-OFF BELOW;[02] REPLACED ANGLE AND FASDR SWAA2023032412556Angle · corrodedCORROSION TRAILING EDGE ANGLE LOCATED ORSS 287 UPPER SIDE AT RT WING 2023-165216<[01] REPLACED ANGLE AND FASTENERS LOCATED ORSS 287 UPPER SIDE AT RT WING IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 SEE INDIVIDUAL SIGN-OFF BELOW.;[02] REPLACED ANGLE AND FSDR SWAA2023032412544Angle · corrodedCORROSION TRAILING EDGE ANGLE LOCATED ORSS 468 UPPER SIDE AT LT WING 2023-165199<[01] REPLACED ANGLE AND FASTENERS LOCATED ORSS 468 UPPER SIDE AT LT WING IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 SEE INDIVIDUAL SIGN-OFF BELOW.;[02] CORRECTED STEP 1<BR>SDR SWAA2023032412554Angle · corrodedCORROSION TRAILING EDGE ANGLES LOCATED ORSS 416 UPPER SIDE AT RT WING 2023-165213<[01] REPLACED ANGLE AND FASTENERS LOCATED ORSS 416 UPPER SIDE AT RT WING IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 SEE INDIVIDUAL SIGN-OFF BELOW.;[02] REPLACED ANGLE AND SDR SWAA2023032412559Angle · corrodedCORROSION TRAILING EDGE ANGLE LOCATED ORSS 369 UPPER SIDE AT RT WING 2023-165215<[01] REPLACED ANGLE AND FASTENERS LOCATED ORSS 369 UPPER SIDE AT RT WING IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9.;[02] REPLACED ANGLE AND FASTENERS LOCATED ORSS 369 UPPESDR SWAA2023031312104Fitting · crackedDOT A24-55 #1 STRUT HYDRAULIC LINE CLAMP SUPPORT FITTING CRACKED JUST O/B OF AFT DIAGONAL BRACE FITTING.<[01] REMOVED SUPPORT FITTING I.A.W SRM 51-40-02-0G-0;[02] TRANSFERRED HOLES FROM OLD PART TO NEW P/N 272A9125-11 FITTING IAW SRM 51-40-05-0G-0 AND BOEING DSDR SWAA2023040711525Strap · corrodedCORROSION FRONT SPAR LOWER STRAP LOCATED OFSS463 AT RT WING 2023-142947<[01] TOOL USED USED EDDY CURRENT FLAW DETECTOR PN: NORTEC 600D; SN: 210138103 CAL DUE DATE: 11-APR-23<BR><BR>TOOL USED PN ULTRASONIC EQUIPMENT PN:45MG; SN: 130066701; DUE DATE: 08-APR-23;[SDR SWAA2023030711419Angle · crackedRT WING UPPER SURFACE MOST I/B PANEL SUPPORT BEAM; FWD ATTACH ANGLE CRACKED<[01] REMOVED AND REPLACED RT WING UPPER SURFACE MOST I/B PANEL SUPPORT BEAM; FWD ATTACH ANGLE REF B737-700 SRM 51-40-02-0G-0; AND DRAWING 115A2000;[02] VERIFIED STEP 1SDR SWAA2023031311073Bracket · crackedR/H WING; 'L' BRACKET CRACKED ON I/B SIDE OF MAIN FLAP ROLLERS CASTING BETWEEN I/B AND O/B MAIN FLAPS (MARKED)<[01] REMOVED AND REPLACED ?L? BRACKET I.A.W SRM 51-40-02.;[02] INSPECTED WORK PERFORMEDSDR SWAA2023040710048Panel · elongatedELONGATED HOLE ACCESS PANEL 621NB AT RT WING 2023-142654<[01] TOOL USED: CALIPER P/N: 500-464 S/N: B17030933 DUE DATE: 17-OCT-23.;[02] TOOL USED HOT BONDER P/N: HCS9200B-AV S/N: 18196021 DUE DATE: 24-JAN-24.;[03] TOOL USED: SCALE: P/N:SPX621 S/N:8340225441 DUESDR SWAA2023040710049Panel · crackedCRACK ACCESS PANEL 661BB ON HOLES AT RT WING 2023-142656<[01] TOOL USED: CALIPER P/N: 500-464 S/N: B17030933 DUE DATE: 17-OCT-23.;[02] TOOL USED HOT BONDER P/N: HCS9200B-AV S/N: 18196021 DUE DATE: 24-JAN-24.;[03] TOOL USED SCALE P/N: SPX621 S/N: 8340225441 DUESDR VNAA202302040013Web · corrodedCORROSION ON MACHINED SUPPORT ANGLE OF MAIN LANDING GEAR WHEEL BIN MOUNTING STRUCTURE AT RBL/LBL 16 ON RH/LH WHEEL WELL AREA.
CORRECTIVE ACTION:
MACHINED SUPPORT ANGLES WERE REPAIRED PER REO 690-53-83-068 REV.-ASDR EE4Y2023022417260Skin · damagedDURING THE ACCOMPLISHMENT OF SB 190-57-0056, AT LH WING LOWER SKIN AFT AREA WITH FASTENER HOLE WITH AN EXISTING COUNTERSINK BUSHING THROUGH THE LOWER SKIN AND THE INTERNAL RIB.WAS REPAIRED FOLLOWING EMBRAER INSTRUCTIONS UNDER ETD2022-190-037529 REV / AND APPROSDR EE4Y2023022417259Skin · damagedDURING THE ACCOMPLISHMENT OF SB 190-57-0056 AT LH WING LOWER SKIN AFT AREA,FASTENER HOLE WITH AN EXISTING FLANGED BUSHING THROUGH THE LOWER SKIN AND THE INTERNAL RIB.WAS REPAIRED FOLLOWING EMBRAER REOAIR INSTRUCTIONS UNDER ETD2022-190-037521 REV / AND APPROVEDSDR EE4Y2023022417247None · noneDURING THE ACCOMPLISHMENT OF SB, RH WING REINFORCEMENT PREPARATION, WAS FOUND A WEAR AT UPPER REAR SKIN STGR 9, WAS REPAIRED FOLLOWING EMBRAER REPAIR INSTRUCTIONS UNDER ETD2022-190-036251 AND APPROVED ON ANAC F-200 FORM PROVIDED BY EMB.SDR VNAA202302040012Intercostal · corrodedCORROSION ON TIRE BURST COVER INTERCOSTAL (2 EAS, INB/OUTB FACE OF INTERCOSTAL) ON SUPPORT STRUCTURE OF ACCESS PANNEL 642AZ/542AZ ON WHEEL WELL AREA RH/LH. TIRE BURST COVER INTERCOSTAL LH WAS EVALUATED WITHIN OF LIMITS PER CRJ-900 SRM 53-00-00-101-001-A01 ANDSDR SWAA2023022709396Plate · crackedAFT OF 2 ENG PYLON FIXED PANEL WAFFLE PLATE CRACKED<[01] REMOVED AND REPLACED WAFFLE PLATE <BR>REF SRM 51-40-02SDR DALA2023022301358None · noneSHIP 5810 EVIDENCE OF POSSIBLE LIGHTNING STRIKE ON LT WINGLET IN ZONE 6 23 " FROM WINGLET JOINT. CORRECTIVE ACTION: FOUND ONLY FASTENER DAMAGED. REPLACED DAMAGED FASTENER PER APB SRM 57-31 AND REAPPLIED TOPCOAT PER APB SRM 57-31. (2641470)SDR SWAA2023040709426Angle · crackedCRACK ANGLE TRAILING EDGE SEAL LOCATED DEFLECTOR CONTROL RIB AT LT WING 2023-142545<[01] REPLACED ANGLE TRAILING EDGE LOCATED DEFLECTOR CONTROL RIB AT LT WING IAW B737-700 SRM 51-10-02; B737-700 SRM 51-40-02 AND DRAWING 115A2930 SHEET 7; REV. -;[02] REPLACED ASDR SWAA2023040709427Angle · crackedCRACK ANGLE TRAILING EDGE SEAL LOCATED DEFLECTOR CONTROL RIB IRSS 271 AT RT WING 2023-142546<[01] REPLACED ANGLE TRAILING EDGE LOCATED DEFLECTOR CONTROL RIB IRSS 271 AT RT WING IAW B737-700 SRM 51-10-02; B737-700 SRM 51-40-02 AND DRAWING 115A2930 SHEET 8; REV.SDR SWAA2023022705613Support · crackedLH WING T/E FLAP WELL SEAL SUPPORT IS CRACKED BEHIND #1 PYLON FOR INBD FLAP OTBD SIDE<[01] REMOVED AND REPLACED L/H WING T/E FLAP SEAL SUPPORT PER SRM 51-40-02.;[02] REMOVED AND REPLACED L/H WING T/E FLAP SEAL SUPPORT PER SRM 51-40-02.SDR VNAA202302221112None · noneMILLED RIB/FITTING CRACKED NEAR LOWER ROW OF FASTENERS IN FITTING. AFT SIDE OF MLG REAR SPAR (APPROX RH WS 49.00, INBOARD SIDE OF RH INBOARD MOST SPOILER RIGHT WING) / CONSTANT AVIATION PERFORMED TEMP REPAIR CLASSIFIED AS A MAJOR REPAIR IAW MHIRJ REO 690-57-21SDR IXXA2023040103Skin Panel · gougedRH WING LWR SKIN HAS SEVERAL GOUGES OUTBOARD OF PYLONSDR SWAA2023032003903Attach Angle · crackedLEFT WING TRANSVERSE WEB O/B ATTACH ANGLE CRACKED AT MAIN FLAP PROGRAM ROLLER SUPPORT ARM ATTACH POINT<[01] REMOVED LEFT WING TRANSVERSE WEB O/B ATTACH ANGLE CRACKED AT MAIN FLAP PROGRAM ROLLER SUPPORT ARM ATTACH POINT IAW SRM 51-40-02-0G-0;[02] LOCATED AND DR
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