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 SWAA2023121222224Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE ORSS 261 AT RT WING 2023-694304<[01] REPLACED CORRUGATED PLATE TRAILING EDGE ORSS 261 AT RT WING I.A.W B737-700 SRM 51-40-02-0G-0 AND B737-700 SRM 51-10-02-0G-0 PARAGRAPH 9.;[02] REPLACED CORRUGATED PLATE TRAILING EDGE ORSSSDR SWAA2023121222009Angle · crackedCRACK TRAILING EDGE ANGLE INTERNAL STRUCTURE AREA ACCESS PANEL 661AB AT RT WING 2023-694299<[01] REPLACED ANGLE AND FASTENERS LOCATED TRAILING INTERNAL STRUCTURE AREA ACCESS PANEL 661AB AT RT WING. <BR>IAW B737-700 SRM 51-10-02 ITEM 9 ;SRM 51-40-02 AND DWG: 11SDR JR2R11132023774Angle · crackedLH WING STUB ANGLE CRACKEDSDR R61A2023120400714Support · crackedDURING HEAVY CHECK, LOWER AILERON CABLE FAIRLEAD SUPPORT AT FRAME 31 IN FWD CARGO CRACKED. CRACKED LOWER AILERON CABLE FAIRLEAD SUPPORT AT FRAME 31 IN FORWARD CARGO REMOVED & REPLACED WITH NEW PART IAW ERJ 170/175 SRM 51-41-01.SDR SWAA2023121319700Plate · crackedLT WING REAR SPAR LOWER CHORD AT APPROX. ORSS 264 WIGGLE PLATE IS CRACKED. 124-005<[01] REMOVED LT WING REAR SPAR LOWER CHORD AT APPROX. ORSS 264 WIGGLE PLATE REF: SRM 51-40-O2-OG-0;[02] STEP 1 ENTERED IN ERROR;[03] REMOVED AND REPLACED WIGGLE PLATE AT LT WINGSDR SWAA2023121219669Angle · crackedCRACK ANGLE TRAILING EDGE DEFLECTION CONTROL RIB LOCATED ORSS 271 AT LT WING 2023-694056<[01] FAULT GENERATED BY ERROR DUE TO FAULT WAS DUPLICATED. SEE [ TTG8Q00PJ8RB ];[02] CORRECTED STEP 1; <BR>REPLACED ANGLE TRAILING EDGE LOCATED AT LEVEL ORSS 271 AT LT WINSDR SWAA2023121219667Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED AT LEVEL ORSS 271 AT LT WING 2023-694054<[01] REPLACED ANGLE TRAILING EDGE LOCATED AT LEVEL ORSS 271 AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9; B737-700 SRM 51-40-02 AND DRAWING 115A2930 REV - MEASURE OF CRACK IS L=0.730' TOSDR SWAA2023121219668Angle · crackedCRACK BRACKET ANGLE TRAILING EDGE LOCATED AT LEVEL ORSS 271 AT LT WING 2023-694055<[01] REPLACED BRACKET ANGLE TRAILING EDGE LOCATED AT LEVEL ORSS 271 AT LT WING IAW B737-700 SRM 51-40-02-0G-0 ;SRM 51-10-02-0G-0 AND DWG 115A2930 SHEET 6 REV- . SEE INDIVIDUAL SSDR SWAA2023121219670Angle · crackedCRACK ANGLE TRAILING EDGE DEFLECTION CONTROL RIB LOCATED ORSS 280 AT RT WING 2023-694057<[01] REPLACED ANGLE LOCATED ON TRAILING EDGE DEFLECTION CONTROL RIB LOCATED ORSS 280 AT RT WING IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DRAWING 115A6200 SHEET 1SDR SWAA2023121319348Plate · crackedRT WING FIXED T/E AT REAR SPAR LOWER CHORD APPROX ORSS 322 WIGGLE PLATE IS BENT AND PHENOLIC SUPPORT IS CRACKED. 124-002<[01] REMOVED AND INSTALLED NEW WIGGLE PLATE AT R/W FIXED T/E REAR SPAR LWR CHORD APPROX ORSS 322 AS-PER SRM 51-40-02-0G-0;[02] VERIFIED PLASDR SWAA2023120719068Plate · crackedCRACK CORRUGATED PLATE INBOARD TRAILING EDGE IRSS 215 LT WING 2023-682292<[01] REPLACED CORRUGATED PLATE INBOARD TRAILING EDGE IRSS 215 LT WING IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02. MEASURE OF CRACK IS: L: 0.400 INCH;TOOL USED: CALIPER P/N:500-196-30SDR SWAA2023120718675Angle · crackedCRACK ANGLE ACCESS PANEL 551GB AT LT WING 2023-682227<[01] REPLACED ANGLE ACCESS PANEL 551GB AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 TOOL USED<BR>ELECTRONIC CALIPER S/N: 500-196-30; S/N: B22072476 DUE DATE: 14-JUL-2024. CRACK LENGTHS: 1.970 ISDR SWAA2023121318353Angle · crackedCRACK ANGLE LOCATED BS 695 LBL 24.75 AT CENTER WING BOX 2023-689200<[01] TOOL USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 25-JAN-24; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N:112820025; DUE DATE: 01-FEB-24.;[02] REPLACED ASDR SWAA2023121318354Angle · crackedCRACK ANGLE LOCATED BS 695 RBL 24.75 AT CENTER WING BOX 2023-689198<[01] TOOL USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 25-JAN-24; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N:112820025; DUE DATE: 01-FEB-24.;[02] REPLACED ASDR SWAA2023121318352Angle · crackedCRACK ANGLE LOCATED BS 695 BL0 LH SIDE AT CENTER WING BOX 2023-689199<[01] REPLACED ANGLE LOCATED ON BS 695 BL0 LH SIDE AT CENTER WING BOX IAW B737-700 SRM 51-10-02 STEP 9 AND DWG: 273A9110 REV: A. SEE INDIVIDUAL SIGN-OFF BELOW;[02] REPLACED ANGLE LOCATED ON BSDR SWAA2023113017633Bracket · crackedCRACK ON BRACKET LOCATED TRAILING EDGE INBOARD SIDE AT LH WING 2023-650227<[01] REPLACED BRACKET LOCATED ON TRAILING EDGE INBOARD SIDE AT LH WING IAW B737-800 SRM 51-40-02 AND DWG 115A2510 SHEET 2 REV A. SEE INDIVIDUAL SIGN OFF BELOW;[02] JOB COMPLETED; SEE INSDR CALA2023111503393Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STATION 540 AND RBL 6.14 IS CRACKED. SUPPORT TASK NSA EMX N/R 00074. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND RBL 6.14 00074 IAW B737-800 SRM 51-- 40-02 AND BAC DWG 111A2000 REV ORIGINAL SEE NSA EMX N/R 00074 AND HASDR SWAA2023110717602Support Beam · out of limitsSHELF PANEL SUPPORT BEAM REQUIRES SRM REPAIR 57-51-02 REPAIR 1 TO BE ACCOMPLISH WITH REPAIR 3<[01] FOUND THE SLOT IN THE EXISTING FIXED TRAILING EDGE SUPPORT BEAM EXCEEDS THE MAXIMUM DIMENSIONS ALLOWED. SUPPORT BEAM IS OUT OF LIMITS PER SRM 57-51-02-2R-1 PAR 4SDR SWAA2023120717190Angle · crackedCRACK ANGLE TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA LT WING 2023-682084<[01] REPLACED ANGLE LOCATED AT TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA LT WING IAW B737-700 SRM 51-10-02 AND SRM 51-40-02<BR>SEE INDIVIDUAL SIGN OFF BELOW;[02] TASK CSDR SWAA2023120717191Angle · crackedCRACK ANGLE TRAILING EDGE ORSS 280 DEFLECTION CONTROL RIB LT WING 2023-682085<[01] REPLACED ANGLE LOC TRAILING EDGE ORSS 280 DEFLECTION CONTROL RIB LT WING IAW B737-700 SRM 51-10-02 Ï¿½TEM 9 AND SRM 51-40-02;[02] CORRECTED STEP 1 <BR>REPLACED ANGLE LOC TRAILINSDR SWAA2023120517302Web · crackedRIGHT WING DEFLECTION CONTROL RIB WEB IS CRACKED AT THE O/B UPPER FASTENER CORNER (MARKED)<[01] UPDATED MEASUREMENTS; AND STEPS 1 & 2.;[02] REMOVED; REPLACED; AND INSTALLED A NEW R/W; T/E DEFLECTION CONTROL RIB WEB IAW SRM 51-40-02 AND BOEING DWG 115A2512. ALSSDR AALA202311063368Landing · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT HAND WING PANEL LANDING AT WS 512, RIB 17. REPLACED PANEL LANDING PER SRM 51-40-02-0G.SDR SWAA2023121116614Web · crackedWEB IB OF RIGHT WING DEFLECTION ROLLER CRACKED AT UPPER OB RIVET; MARKED.<[01] REMOVED AND REPLACED WEB PER SRM 51-10-02.;[02] COMPLIED WITH INSPECTION; REMOVED AND REPLACED WEB PER SRM 51-10-02.SDR SWAA2023120716617Plate · crackedRIGHT WING WIGGLE PLATE UNDER WING PANEL 651EB CRACKED AT RIVET; MARKED.<[01] REMOVED AND REPLACED THE WIGGLE PLATE UNDER RH WING PANEL 651EB PER SRM 51-40-02.SDR SWAA2023120516821Web · crackedLEFT WING DEFLECTION CONTROL PANEL LOWER WEB CRACKED<[01] REMOVED AND REPLACED LEFT WING DEFLECTION CONTROL PANEL LOWER WEB AS PER SRM 51-40-02-0G-0.;[02] VERIFIED STEP 1SDR SWAA2023121116116Web · crackedL-CLIP COMMON TO I/B SIDE OF DEFLECTION CONTROL RIB AND O/B END OF TRANSVERS WEB IS CRACKED RIGHT WING<[01] REMOVED AND REPLACED L-CLIP COMMON TO I/B SIDE OF DEFLECTION CONTROL RIB AND O/B END OF TRANSVERS WEB; P/N 115A6260-2 IAW SRM 51-40-02-0G-0 AND IPC 57-4SDR SWAA2023103115521Support Bracket · crackedRT. WING UPPER INBD FWD UPPER PANEL SUPPORT BRACKET CRACKED. (Z BRACKET)<[01] REMOVED AND REPLACED RT WING UPPER INBD FWD UPPER PANEL SUPPORT BRACKET (Z BRACKET) PER SRM 51-40-02.SDR JR2R20231028495Angle · crackedLH WING TRAILING EDGE WING SPAR 2 LOWER STUB ANGLE CRACKEDSDR SCNA20240311143Support · crackedINITIAL INSPECTION: CRAK ON WEB SUPPORT AT FIXED PANEL REAR SPAR STA.WS 280 APROX. AT RH WING. WEB SUPPORT AT FIXED PANEL REAR SPAR STA.WS 280 APROX. AT RH WING WAS REPLACED PER B737-800 SRM 51-40-02-0G-0SDR SWAA2024010315557Nut Plate · corrodedCORROSION RAIL NUT INTERNAL CAVITY LEADING EDGE OFSS 292 AT RT WING 2023-652286<[01] REPLACED RAIL NUT INTERNAL CAVITY LEADING EDGE OFSS 292 AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG: 112A4402 SHEET 8 REV.B;[02] REPLACED RAIL NUT INTERNSDR SWAA2023121315269Plate · elongatedRIGHT WING TRAILING EDGE STRUCTURE - DEFLECTION CONTROL RIB TO SUPPORT PANEL ATTACH SERRATED PLATES HOLES ELONGATED AND GOUGED WITH PLAY.<[01] TRIMMED OUT DAMAGED AREA; FABRICATED OUTBOARD DOUBLER AND FILLER; INSTALLED OUTBOARD DOUBLER; FILLER WITH I/B AND O/BSDR AALA202311066598Bracket · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND WING LEADING EDGE OUTBOARD FIXED LOWER ACCESS PANEL BRACKET AT SS 308. REPLACED BRACKET PER SRM 51-40-02SDR AALA202311068091Bracket · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT HAND WING LEADING EDGE OUTBOARD FIXED LOWER ACCESS PANEL BRACKET AT SS 308. REPLACED BRACKET PER SRM 51-40-02SDR CALA2023102503182Angle · crackedL/H WING RIB 15 L/E WEB SUPPORT ANGLE CRACKED. PER HAECO LCQ NR 9294242/38242 REMOVED AND REPLACED WEB SUPPORT ANGLE ON LH WING RIB 15 L/E IAW A319 SRM 51-42-11SDR SWAA2023110813099Unknown · crackedPANEL #551FB HAS A CLIP CRACKED<[01] REMOVED AND INSTALLED NEW CLIP PER SRM 51-40-02-0G-0;[02] CORRECT STEP 1 REMOVED AND INSTALLED NEW CLIP AT PANEL #551FB PER SRM 51-40-02-0G-0;[03] VERIFIED STEP 2; CLIP REPLACEDSDR AALA202310230784Bracket · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON BRACKET AT LEFT WING STA 308. REPLACED BRACKET PER SRM 51-40-02.SDR 2026FA0000387Stiffener · shearedFLAP TRACK STIFFENERS THAT KEEP THE FLAP TRACKS STRAIGHT AND TRUE WERE FOUND TO BE SHEARED OFF AND/OR CRACKED.SDR SWAA2023113018756Panel · corrodedFUELING PANEL HAS LIGHT CORROSION AROUND INDICATOR HOLES.<[01] R&R FUELING PANEL AND OPS CHECK GOOD PER AMM 28-41-61.SDR SWAA2023112212414Fitting · crackedRIGHT WING REAR SPAR FIXED T/E LOWER ATTACHED WIGGLE FITTING CRACKE AND SHEARED RIVETS @ ORSS 261 O/B OF FLAP TRACK NO- 6 MKD DOT<[01] REMOVED RIGHT WING REAR SPAR FIXED T/E LOWER ATTACHED WIGGLE FITTING AS PER SRM 51-40-02-0G-0.<BR>LOCATED AND DRILLED NEW LOWSDR 2023F00306Web · crackedLH WING FWD WEB P/NP/N 6910269-39. CRACKED. ACCOMPLISHED TEXTRON AVIATION ENGINEERING REPAIR OF THE LH WING FWD WEB CRACK SR-680A-ATA57-33170 DATED APRIL 25, 2022 AND 8100-9 DATED APRIL 25, 2022; STANDARD REPAIR - CRACK DAMAGE, CENTER WING FAIRINGS, LH AND RH SDR SWAA2023113011137Panel · corrodedCORROSION AT R/W FIXED L/E FRONT SPAR FUELING STATION QTY GAUGES SUPPRT PANEL MKD DOT<[01] REFUELING STATION QTY GAUGES SUPPORT PANEL WILL BE REPLACED ON CARD # TTG8Q00NZZCQ.;[02] FINAL INSPECTION; REFUELING STATION QTY GAUGES SUPPORT PANEL WILL BE REPLACED ONSDR SWAA2023113010782Angle · crackedCRACK TRAILING EDGE ON ANGLE LOCATED ORSS269 AT RT WING 2023-649833<[01] REMOVED AND REPLACED TRAILING EDGE ON ANGLE LOCATED ORSS269 AT RT WING I.A.W. B737-700 SRM 51-40-02 AND 51-10-02 ITEM 9. THE MEASURE OF CRACK IS= (1.125?) TOOL USED DIGITAL P/N:700-113-10SDR SWAA2023113010785Web · crackedCRACK TRAILING EDGE ON WEB LOCATED ORSS269 AT RT WING 2023-649832<[01] REPLACED WEB AND FASTENERS LOCATED ON TRAILING EDGE ORSS269 AT RT WING IAW B737-800 SRM 51-10-02-0G-0; SRM 51-40-02-0G-0; DWG 115A2512 SHEET 16 REV -.;[02] CORRECTED STEP 1<BR>REPLACED WEB SDR SWAA2023110810814Panel · corrodedRIGHT WING FUEL ACCESS PANEL 633AB HAS CORROSION.<[01] CORROSION OUT OF LIMITS; REPLACED RIGHT WING FUEL ACCESS PANEL 633AB PER AMM 28-11-11. PANEL INSTALLATION ON CLOSE UP TASK CARD # TTG8Q00N5WCL;[02] VERIFIED WORK PERFORMED.SDR SWAA2023110810815Panel · corrodedRIGHT WING FUEL ACCESS PANEL 632JB HAS CORROSION ON LANDING<[01] CORROSION OUT OF LIMITS; REPLACED RIGHT WING FUEL ACCESS PANEL 632JB PER AMM 28-11-11. PANEL INSTALLATION ON CLOSE UP TASK CARD # TTG8Q00N5WD2;[02] VERIFIED WORK PERFORMED.SDR SWAA2023110810816Panel · corrodedRIGHT WING FUEL ACCESS PANEL 632CB HAS CORROSION ON LANDINGS<[01] REMOVED AND REPLACED FUEL ACCESS PANEL 632CB PER M/M REF. 28-11-11.;[02] VERIFIED REMOVED AND REPLACED FUEL ACCESS PANEL 632CB PER M/M REF. 28-11-11.SDR VNAA20231014002Strap · corroded670-57-21-867_REV-A (PERM REPAIR-LOWER SKIN ASSY AND INSTL WINGBOX) REPAIR IAW REO-670-57-21-867 WITHIN 8000 FH OR NEXT "C" CHECK.SDR SWAA2023113010495Retainer · crackedL/W REAR SPAR FIXED T/ E DEFLECTION CONTROL RIB PANEL VERTICAL BULB SEAL RETAINER CRACKED MKD DOT<[01] REMOVED AND REPLACED SEAL RETAINER AT LT WING REAR SPAR FIXED T/E DEFLECTION CONTROL RIB VERTICAL PANEL PER REF B737 SRM 51-40-02-0G-0;[02] VERIFIED STEP 1SDR SWAA2023101610332Support Angle · crackedSUPPORT CLIP AT RIGHT WING INBOARD FIXED TRAILING EDGE/DEFLECTION CONTROL RIB CRACKED<[01] REMOVED AND REPLACED CLIP REF SRM 51-40-02.SDR SWAA2023110810139Plate · crackedLEFT WING WAFFLE PLATE (PANEL SUPPORT) INBOARD OF #3 FLAP TRACK IS CRACKED.<[01] REMOVED AND REPLACED LEFT WING WAFFLE PLATE (PANEL SUPPORT) INBOARD OF #3 FLAP TRACK PER SRM 51-40-02.;[02] CW
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