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 SWI2023F00330Unknown · corrodedRH WING BATT RIB WS48.30 HAS CORROSION (C-CHECK RO 9/13/2023) REMOVED CORROSION AT RH WING BATT RIB WS48.30 REF CRJ200 SRM 51-21-06. FOUND TO BE OUT OF LIMITS. COMPLIED WITH REO 601R-57-21-3778 REV-- DATED 2023-07-21. SEE CONTINUATION CARD FOR DETAILS. SDR SWI2023F00328Unknown · corrodedRH WING ANGLE ATTACHED TO BATT RIB AT WS53.60 HAS CORROSION (C-CHECK RO 9/13/2023) RH WING ANGLE ATTACHED TO BATT RIB AT WS53.60 CORRODED OUT OF LIMITS. REMOVED AND INSTALLED NEW ANGLE ATTACHED TO BATT RIB AT WS53.60 REF CRJ200 SRM 51-42-21 AND DWG # 60SDR SWI2023F00326Unknown · crackedLH WING BATT RIB AT WS53.60 IS CRACKED (C-CHECK RO 9/13/2023) REMOVED AND REPLACED WITH NEW LH WING BATT RIB AT WS53.60 REF CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-21 AND DWG NO 601R10203 REV -G. LEAK CHECK GOOD SEE CONTINUATION CARD FOR DETAILS. COMPLIEDSDR SWI2023F00324Unknown · crackedRH WING THE CAP THAT ATTACHES TO BATT RIB AT WS48.30 IS CRACKED (C-CHECK RO 9/13/2023) REMOVED AND REPLACED WITH NEW BATT RIB AT RH WING CAP WS48.30 REF CRJ200 SRM 51-42-21 AND DWG 601R10204 REV -J. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY. SEE CSDR SWAA2023081576004Plate · shearedL/W T/E ORSS 261 LOWER CORRAGATED PLATE FASTENERS SHEARED OFF.<[01] REMOVED WIGGLE PLATE ASSY SHEARED OFF; LEFT WING ORSS 261 AND INSTALLED NEW WIGGLE PLATE ASSY PART #115A2781-13 SAME LOCATION ABOVE IAW AIPC 57-50-00-30; SRM 51-40-02-0G-0 & UPDATED PART REQUISDR IXXA2023070703Rib · mislocatedDOUBLE DRILLED HOLES FOR A NUTPLATE INSTALLATION WERE FOUND ON THE R/H WING TRAILING EDGE RIB AT WSTA 507.85SDR SWAA2023080475374Bracket · damagedELONGATED HOLE ON SUPPORT BRACKET LOCATED INBOARD LEADING EDGE AT INTERNAL CAVITY ACCESS PANEL 611AT RT WING 2023-422560<[01] REPLACED SUPPORT BRACKET LOCATED INBOARD LEADING EDGE AT INTERNAL CAVITY ACCESS PANEL 611AT RT WING IAW. B373-700 SRM 51-40-02-0G-0 ANSDR SWAA2023080474849Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED ON ORSS 261 AT LT WING 2023-422505<[01] REPLACED CORRUGATED PLATE TRAILING EDGE AND FASTENERS LOCATED ON ORSS 261 AT LT WING IAW B737-700 SEM 51-40-02 AND DWG 115A2001 REV:-. SEE INDIVIDUAL SIGN OFF BELOW.;[02] CORRSDR SWAA2023080474851Angle · damagedELONGATED HOLE ANGLE TRAILING EDGE LOCATED ON ORSS255 AT LT WING 2023-422507 IAW DWG NAME OF PART IS CLIP ASSY DWG114A5300 REV :A<[01] REPLACED ANGLE TRAILING EDGE LOCATED ON ORSS255 AT LT WING IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 115A5300; SSDR SWAA2023080474858Support Bracket · crackedCRACK SUPPORT BRACKET TRAILING EDGE LOCATED ORSS 280 RT WING 2023-422516<[01] REPLACED SUPPORT BRACKET TRAILING EDGE LOCATED ORSS 280 RT WING IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 115A3700 REV.- SEE INDIVIDUAL SIGN OFFS BELOW;[02] REPLACED SUPSDR SWAA2023080474857Plate · crackedCRACK PLATE ASSY TRAILING EDGE LOCATED ORSS 290 TO ORSS 299 RT WING 2023-422518<[01] REPLACED PLATE ASSY TRAILING EDGE LOCATED ORSS 290 TO ORSS 299 RT WING IAW B737-700 SRM 51-40-02 AND DWG 115A3700 REV:-. LENGTH OF CRACK:0.807?. TOOL USED CALIPER P/N: 500-752SDR SWAA2023080474856Plate · crackedCRACK PLATE ASSY TRAILING EDGE LOCATED ORSS 270 TO ORSS 275 RT WING 2023-422520<[01] REPLACED PLATE ASSY TRAILING EDGE LOCATED ORSS 270 TO ORSS 275 RT WING AND FASTENERS IAW B737-700 SRM 51-10-02 Ï¿½TEM 9; SRM 51-40-02 AND DWG 115A2001 REV-. SEE INDIVIDUAL SIGSDR SWAA2023080474854Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED ORSS 273 FWD POSITION DEFLECTION CONTROL RIB RT WING 2023-422530PART INSTALLEDP/N: 115A2953-2 PO# 2022 196669<[01] REPLACED ANGLE TRAILING EDGE LOCATED ORSS 273 FWD POSITION DEFLECTION CONTROL RIB RT WING IAW B737-700 SRM 51-4SDR SWAA2023080474853Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED ORSS 273 AFT POSITION DEFLECTION CONTROL RIB RT WING 2023-422532<[01] REPLACED ANGLE TRAILING EDGE LOCATED ORSS 273 AFT POSITION DEFLECTION CONTROL RIB RT WING IAW SRM B737-700 51-40-02 SRM 51-10-02 PARAGRAPH 9;[02] STEP 1 CORSDR SWAA2023080474852Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED IRSS140 AT LT WING 2023-422526 IAW DGW NAME PART IS CLIP ASSY 115A2000 REV-<[01] REPLACED ANGLE TRAILING EDGE LOCATED IRSS140 AT LT WING; MEASURE CRACK IS L=0.817? TOOL USED CALIPER P/N: 500-193-30; S/N: 0039393; DUE DATE: 02-SDR SWAA2023081681722Bracket · crackedLEFT WING FRONT SPAR STATION IFFS 150 ANTI ICE DUCT SUPPORT BRACKET IS CRACKED VIEW WITH LEADING EDGE FLAP EXTENDED<[01] REMOVED AND REPLACED SUPPORT BRACKET AT L/W FRONT SPAR STATION IFFS 150 REF B-737-800 SRM 51-40-02-0G-0; SRM 51-40-04-0G-0 TOOL USED ; TORQSDR UIEA2023070600719Unknown · unknownCRACK - WEB AND STIFFENER, LH WING INBD FIXED T/E BEAM OUTBD END WBL 429.47(<P>1) PERFORM EI T2023A57M-1568 REV 0. 2) ACCOMPLISHED IAW EI T2023A57M-1568 REV 1. 3) JOB COMPLETED AND CONDITION CHECK NORMAL. PN 65B10865-3</P>)SDR 2024FA0000021Stiffener · crackedFOUND RIGHT WING LOWER, INBOARD, FORWARD SKIN, AFT STIFFENER CRACKED. REPLACED
STIFFENERSDR FDEA202306301224Web · crackedLH WING T/E CAVITY TOP SKIN PNL SUPPORT WEB CRACK AT SPOILER#5 HINGE ARM REPLACED THE CRACK SUPPORT WEB WITH NEW PART I.A.W A300-600F SRM 51-72-10-001, PAGE2SDR SWAA2023080473478Angle · crackedCRACK ANGLE TRAILING EDGE ORSS 267 DEFLECTION CONTROL RIB LT WING 2023-422362<[01] REPLACED ANGLE TRAILING EDGE ORSS 267 DEFLECTION CONTROL RIB LT WING I.A.W B737-700 SRM 51-10-02 Ï¿½TEM 9 AND SRM 51-40-02 AND DWG 115A2930 SHEET 7 REV. - DUE TO NOT FOUND ALLOWSDR REXA2022072700548Angle · corrodedANGLE UNDER PANEL 542AZ IS CORRODED ANGLE UNDER PANEL 542AZ IS CORRODED UPON FURTHER INVESTIGATION, DISCREPANCY IS ACTUALLY FOR CORRODED ANGLE UNDER PANEL 642AZ. ANGLE IS IDENTIFIED AS MLG PROTECTIVE COVER ANGLE P/N CC670-10338-2. ANGLE IS SEVERELY CORRODED ASDR SWAA2023072472683Fitting · crackedRT WING RIB CONTROL PANEL LOWER FWD SUPPORT SEALIS CRACKED.<[01] REMOVED AND REPLACED RT. WING T/E FITTING PER SRM 51-40-02-0G-0;[02] VERIFIED STEP#1SDR SWAA2023071771938Angle · crackedRH DEFLECTION RIB INBOARD SHELF PANEL SUPPORT ANGLE CRACKED.<[01] REMOVED AND REPLACED SUPPORT ANGLE PER SRM 51-40-02.SDR FDEA202306271123Former · crackedR/W L/E FORMER CRACKED STA OSS 499 0000237172 : LAFFOND, MARK P - 27-JUN-2023 19:21 REMOVED AND INSTALLED NEW FORMER A R/H L/E OSS 499. REF SR 67-57-002 REV F. (MPN: B67-57-002-12)SDR FDEA202306271122Former · crackedR/W L/E FORMER CRACKED STA OSS 437 CORRECTION, STA OSS 565 INSTEAD OF STA OSS 437 0000358872 : FERGUSON, STEVE M - 27-JUN-2023 19:18 REMOVED AND INSTALLED NEW FORMER ON RIGHT WING FIXED LEADING EDGE AT OSS 565 REF SR67-57-002 REV F (MPN: B67-57-002-06)SDR FDEA202306271121Former · crackedR/W L/E FORMER CRACKED STA OSS 441 0000245521 : EDWARDS, WILLIAM B - 27-JUN-2023 19:14 REMOVED AND REPLACED PANEL 621ANB FOR FORMER ACCESS REF B767 AMM 57-41-57-4. REMOVED AND REPLACED R/W L/E FORMER AT STA 441, REF FEDEX DRAWING SR67-57-002, SHEET 3. (MPN:SDR SWAA2023072871754Angle · crackedCRACK SLAT 8 ANGLE LOC INBOARD AUXILIARY TRACK AT RT WING 2023-405034<[01] REPLACED ANGLE LOCATED ON SLAT 8 ON I/B AUXILIARY TRACK AT RT WING. IAW B737-700 SRM 51-40-02 AND CMM 57-43-01.;[02] REPLACED ANGLE LOCATED ON SLAT 8 ON I/B AUXILIARY TRACK AT RT WING. SDR SWAA2023062671226Bracket · crackedRIGHT WING UPPER PANEL SUPPORT FWD ATTACH POINT BRACKET IS CRACKED. (Z BRACKET)<[01] REMOVED AND REPLACED RIGHT WING UPPER PANEL SUPPORT FWD ATTACH POINT BRACKET PER SRM 51-40-02.SDR FDEA202306241091Bracket · crackedRH WING OUTBD LEADING EDGE, FUELING STATION DOOR HOLD-OPEN BRACKET AT INBD EDGE OF DOOR IS CRACKED REMOVED AND REPLACED BRACKET IAW BAC DWG 114T2450, SHEET 1, REVISION JSDR FDEA202306241090Panel · dentedRH WING LOWER O/B ACCESS PANEL 643BB IS DENTED ON LOWER SURFACE REPAIRED RH WING LOWER O/B ACCESS PANEL 643BB REMOVING DAMAGE ON LWR SURFACE, CLEANING, POTTING HOLE REPAIR, LAYING UP REPAIR DOUBLER AND CURED IAW B767 SRM 57- 20-01-2R FIG. 201 REP 7 AND SRM SDR SWAA2023072870653Angle · crackedCRACK WING TO BODY FAIRING ANGLE LOCATED BS500D AT LEVEL STR19RH AT LOWER FUSELAGE 2023-404889<[01] REPLACED BODY FAIRING ANGLE LOCATED ON BS500D AT LEVEL STR 19RH AT LOWER FUSELAGE I.A.W B737-700 SRM 51-10-02 Ï¿½TEM 9; SRM 51-40-02 AND DWG 116A3110 SHEET 8 RESDR FDEA202306231081Bracket · crackedR/W, I/B LEADING EDGE, LES 283, TORQUE TUBE SUPPORT BRACKET IS CRACKED REMOVED CRACKED TORQUE TUBE BRACKET ON RIGHT WING I/B LEADING EDGE LES 283 IAW FEDEX B767 SRM 51-40-02-0G AND REPLACED WITH NEW TORQUE TUBE BRACKET PN 256T2425-5, P.O 1060626.1 PER BOEISDR SWAA2023072870642Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED DEFLECTION CONTROL RIB ORSS270 AT RT WING 2023-404841<[01] REPLACED ANGLE TRAILING EDGE LOCATED DEFLECTION CONTROL RIB ORSS270 AT RT WING I.A.W B737-700 SRM 51-40-02 AND SRM 51-10-02; SEE INDIVIDUAL SIGN-OFF BELOW;[02] REPLACESDR SWAA2023072773275Panel · crackedCRACK ACCESS PANEL 632NB FUEL TANK ON FUEL PUMP FLOAT AT RT WING 2023-394805<[01] REPLACED ACCESS PANEL 632NB FUEL TANK ON FUEL PUMP FLOAT AT RT WING IAW B737-700 SRM 51-40-02-0G-0;[02] REPLACED FLOAT FUEL TANK AT RT WING ACCES PANEL 632NB P/N:4066-0074-1 S/N:SDR SWAA2023072774642Shim · brokenLH FUEL WING ACCESS AT RIB 6 UPPER SHIM IS BROKEN.<[01] REMOVED AND REPLACED LH FUEL WING ACCESS AT RIB 6 UPPER SHIM AS PER B 737-700 SRM 51-40-02-0G-0. TOOL USED B/C: 169684 CAL. DATE 10/22 ; DUE DATE: 10/23.;[02] (AMENDING STEP 1) REMOVED AND REPLACED LH FUESDR SWAA2023072774644Shim · brokenLH WING FUEL TANK ACCESS AT RIB 12 HAS TWO UPPER SHIMS MIGRATED OUT AND BROKEN.<[01] REMOVED AND REPLACED LEFT WING FUEL TANK ACCESS RIB #12 UPPER SHIM AS PER B 737-700 SRM 51-40-02-0G-0.;[02] (CORRECTING STEP #1) REMOVED AND REPLACED LEFT WING FUEL TANK ACCESSDR SWAA2023072774645Shim · brokenLEFT WING FUEL TANK ACCESS AT RIB 19 UPPER SHIM IS BROKEN.<[01] REMOVED AND REPLACED LEFT WING FUEL TANK ACCESS RIB #19 UPPER SHIM AS PER B 737-700 SRM 51-40-02-0G-0.;[02] (CORRECTING STEP #1) REMOVED AND REPLACED LEFT WING FUEL TANK ACCESS RIB #19 UPPER SHIM SDR SWAA2023072774643Shim · brokenLEFT WING FUEL TANK ACCESS AT RIB 18 UPPER SHIM IS BROKEN.<[01] REMOVED AND REPLACED LEFT WING FUEL TANK ACCESS RIB #18 UPPER SHIM AS PER B 737-700 SRM 51-40-02-0G-0.;[02] (CORRECTING STEP #1) REMOVED AND REPLACED LEFT WING FUEL TANK ACCESS RIB #18 UPPER SHIM SDR SWAA2023072775478Shim · out of positionLH FUEL WING ACCESS AT RIB 10 UPPER SHIMI IS MIGRATED OUT.<[01] (AMENDING STEP 1) REMOVED AND REPLACED LH FUEL WING ACCESS AT RIB 10 UPPER SHIM AS PER B 737-700 SRM 51-40-02-0G-0; SRM 51-40-04-0G-0 AND DWG#112A5060. TOOL USED B/C: 169684 CAL. DATE 10/25/22 ; DSDR SWAA2023072570424Nut Plate · crackedCRACK INTERNAL CAVITY LEADING EDGE NUTPLATE RAIL AT LEVEL OFSS 308 AT LT WING 2023-394781<[01] REPLACED NUTPLATE RAIL AT LEVEL OFSS 308 AT LEADING EDGE LT WING IAW B737-700 SRM 51-40-02 AND DWG: 112A4402 REV:B SHEET:8;[02] REPLACED NUTPLATE RAIL AT LEVEL OFSS SDR FDEA202306211070Panel · crackedLEFT WING FIXED LEADING EDGE SKIN UPPER SURFACE CRACKED IN TWO EACH AREAS AT INBD END OF #3 SLAT. REPAIRED L/H WING FIXED LEADING EDGE SKIN UPPER SURFACE IS CRACKED IN 2 EACH LOACTIONS AT INBD END OF #3 SLAT IAW FED EX B757 SRM 57-41-01-0I, 57-41-01-2R REPSDR SWAA2023062164013Angle · crackedCRACK ANGLE TRAILING EDGE LOC. ORSS 273 AT LT WING 2023-330513. REPLACED ANGLE TRAILING EDGE LOC. ORSS 273 AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 115A2930 REV -.;[02] REPLACED ANGLE TRAILING EDGE LOC. ORSS 273 AT LT WING IAW B737-700 SRM 51-10-02SDR R61A2023070700383Support · corroded******MAJOR******PERFORM SB57-73G1P2 RIGHT OUTBOARD MAIN WING SPAR 1 INSPECTION AND REWORK. PERFORMED JC# 170EO-57-20-0050MA_1 ********MAJOR******SDR R61A2023070700382Support · corrodedCORROSION FOUND ON UPPER FLANGE CROSSBEAM @ FWD FUSE FR14 RBL30-35.REPLACED UPPER SUPPORT PN 170-13939-001 IAW SRM 53-00-10 #3 FIG 203SDR SWAA2023071960699Angle · crackedRT WING TE TRANSVERSE WEB; OB ATTACH ANGLE CRACKED; AT THE DEFLECTION CONTROL RIB.<[01] VERIFIED APPLICABILITY FOR ALLOWABLE DAMAGE LIMITS RT WING TE TRANSVERSE WEB;ATTACH ANGLE IAW SRM 51-10-02;[02] NO ALLOWABLE DAMAGE LIMITS RT WING TE TRANSVERSE WEB ;OB ATTSDR SWAA2023071760180Angle · crackedLEFT WING TRAILING EDGE FIX DEFLECTOR PANEL LOWER CENTER BRACKET O/B END CRACKED<[01] REMOVED DAMAGED ANGLE BRACKET & INSTALLED NEW ANGLE BRACKET AT L/W T/E FIX DEFLECTOR PANEL LOWER AREA; AS PER SRM 51-40-02 & DWG. 115A2156.;[02] VERIFIED STEP # 1SDR SWAA2023070360681Angle · crackedCRACK ANGLE WING TO BODY FAIRING AT LEVEL BS 500D AND STR 19L AT LOWER FUSELAGE 2023-360395<[01] REPLACED ANGLE WING TO BODY FAIRING AT LEVEL BS 500D AND STR 19L AT LOWER FUSELAGE IAW B737-700 SRM-51-40-02 AND DWG-116A3110 REV: B SEE INDIVIDUAL SIGN-OFF BELOW;SDR SCNA20240310104Support Angle · crackedDEFECT WO 74296 NR00098: CRACK ON SUPPORT ANGLE LOCATED AT LEVEL ORSS 277 TRAILING EDGE AT LT W ING - - RESOLUTION: REPLACED ANGLE LOCATED AT LEVEL ORSS 277 TRAILING EGGE AT LT WING B737-800 SRM 51-40-02 AND DWG 115A6200 SHEET 9 REV: ASDR SCNA20240310103Support Angle · crackedDEFECT WO 74296 NR00097: CRACK ON SUPPORT ANGLE LOCATED AT LEVEL ORSS 268 TRAILING EDGE AT LT WING. - - RESOLUTION: REPLACED SUPPORT ANGLE LOCATED AT LEVEL ORSS 268 TRAILING EDGE AT LT WING IAW B737-800 SRM51-40-02 DWG 115A2930 SHEET 7 REVSDR FDEA202306171050Beam · crackedTHIS SDR IS A CORRECTION TO SDR 23-1014 (AS IT CALLED OUT P5 INSTEAD OF P6 OF EO E.O. H- 5720-E0353920 REV A) A DETAILED INSPECTION OF THE 113T1913-24 SUPPORT BEAM AT THE WS 1054 UPPER CHORD ATTACHMENT SHOWED A CRACK INDICATION. REF IN STEP 5.E COMPLIED W
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