JASC 5730
Service difficulty reports · 27,262
Reports filed under 5730 · Wing, Plate/Skin, 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 = '5730' 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 = '5730' 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 SWAA2022020912697Plate · crackedRIGHT WING; ABOVE #6 FLAP TRACK; WIGGLE PLATE IS CRACKED AT INBOARD FASTENER. (MARKED) / REMOVED AND REPLACED WIGGLE PLATE ABOVE #6 FLAP TRACK PER SRM 51-40-02SDR SWAA2022020969378Panel · elongatedRIGHT WING LEADING EDGE PANEL 621LB HAS AN ELONGATED HOLE (MARKED) N / REPAIRED AND APPLIED DECORATIVE FINISH TO RIGHTR WING LEADING EDGE PANEL 621LB OF ELONGATED HOLE IAW B737 SRM 51-70-04-2R-9 REV 63 AND B737SDR SWAA2022020986751Panel · crackedLH WING LOWER SURF PANEL 661CB; COMPOSITE MATERIAL UNDER COUNTERSINKS CRACKED; AND PULLED THROUGH. / EVALUATED; CLEANED; PREPPED AND REPAIRED DAMAGED FASTENER HOLES ON L/H WING PANEL 661CB IAW B737 SRM 51-70-04-2R-9; PAR 4 (A-0) REV 63SDR SWAA2022020986752Panel · crackedLH WING LOWER SURF PANEL 661AB; COMPOSITE MATERIAL UNDER COUNTERSINKS CRACKED; AND PULLED THROUGH. / EVALUATED; CLEANED; PREPPED AND REPAIRED DAMAGED FASTENER HOLES ON L/H WING PANEL 661AB IAW B737 SRM 51-70-04-2R-9; PAR 4 (A-0) REV 63SDR SWAA2022020937000Bracket · crackedPANEL 551FB; CENTER FWD. BRACKET CRACK; MARKED. / REMOVED & REPLACED CENTER FWD BRACKET ON PANEL 551FB IAW SRM 51-40-02-OG-O STEP 4SDR SWAA2018021919770Fairing · crackedRIGHT WING AFT FLAP TRACK FAIRING 642BB, INTERIOR SURFACE CRACKED AT THE OTBD LOWER CORNER. REPAIRED THE FAIRING IAW SRM.SDR IPXA2018021726606Skin · chafedINSPECTION TYPE: 4C, LT WING L/E LOWER SKIN PANEL CHAFED JUST INBD OF THE NR 3 SLAT AT NR 1 PYLON. REMOVED THE SKIN PANEL, FABRICATED REPLACEMENT SKIN PANEL AND INSTALLED IAW DWG ARB2363 AND SRM 51-35-01 & 51-33-01.SDR AALA20180313005Skin · corrodedAIRCRAFT WAS IN BASE MAINTENANCE. LEFT OVERWING FILL PORT FAILS BONDING RESISTANCE CHECK. UPON REMOVAL OF THE LEFT OVERWING FILL-PORT FITTING CORROSION WAS DISCOVERED ON THE UPPER AND LOWER SURFACES OF THE FILL-PORT LANDING ON THE WING SKIN. REPAIRED SKIN PER SDR AALA20180313004Skin · corrodedCORROSION ON THE UPPER AND LOWER SURFACES OF THE RIGHT OVERWING FUEL PORT SKIN FITTING. REPAIRED THE SKIN IAW AMM 28-11-04 AND EA 277597.SDR REXA2018013100089Skin · damagedEXTERIOR SURFACE OF CTR WING HAS BARE METAL WITH MINOR FRETTING AT LBL 45 FROM CONTACT WITH WING AERODYNAMIC FAIRING 193AB. REPAIRED THE SKIN IAW SRM 57-21-31, 54-42-21, 51-24-11, REO 601R-57-21-2724, AND REO 601R-57-21-880. IAW AMM 28-11-00-790-802.SDR JGVR20180131002Skin · corrodedBLENDED 10 AREAS OF CORROSION ON THE LT UPPER WING SKIN, PERFORMED EDDY CURRENT CRACK AND ULTRASONIC THICKNESS INSPECTION, PREPPED AND TREATED AREAS IAW SRM 51-10-03, AND MM 51-10-00.SDR JGVR20180131001Skin · corrodedCORROSION ON THE RT UPPER WING SKIN, BLENDED AND PERFORMED AN EDDY CURRENT AND ULTRASONIC THICKNESS INSPECTIONS, PREPPED AND TREATED AREAS IAW SRM 51-10-03, 51-70-08, AND MM 51-10-00.SDR IPXA2018022026724Panel · crackedRIGHT WING ROOT PANEL 613AB LAND IS CRACKED. REPAIRED IAW SRM 53-15-63, REPAIR A.SDR FDEA201801280269Skin · crackedONE CRACK FOUND APPROXIMATELY. .2 INCHES IN LENGTH IN THE RT FIXED LEADING EDGE SKIN ADJACENT TO CUTOUT CORNER NR 11 AT FUEL ACCESS DOOR. REPAIRED IAW SRM 57-40-01-2R REPAIR 18 FIG 201. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201801280268Doubler · crackedLEFT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 553, FOUND CRACKED. REPAIRED THE DOUBLER IAW SRM 57-40-02-2R, REPAIR 15, FIG 203. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201801280267Doubler · crackedLEFT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 749, FOUND CRACKED. REPAIRED THE DOUBLER IAW SRM 57-40-02-2R, REPAIR 15, FIG 203. THE REPAIRSWAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201801280266Doubler · crackedRIGHT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 731, FOUND CRACKED. REPAIRED THE DOUBLER IAW SRM 57-40-02-2R, REPAIR 15, FIG 203. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201801280265Former · crackedRIGHT WING FIXED LEADING EDGE FORMER AT XOS 734, FOUND CRACKED. THE FORMER WAS REMOVED IAW SRM 51-31-01-0G. A NEW FORMER WAS FABRICATED IAW DWG ARB2923, REV D, AND INSTALLED IAW SRM 51-31-01-0G. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201801280264Doubler · crackedLEFT WING FIXED LEADING EDGE RIB DOUBLER AT XOS 789 FOUND CRACKED. THE DOUBLER WAS REMOVED IAW SRM 51-31-01- 0G. A NEW DOUBLER WAS FABRICATED IAW DWG ARB3954, REV K AND INSTALLED IAW SRM 51-31-01-0G. THE REPAIR WAS CLASSIFID AS MAJOR IAW GMM 6-2-100.SDR FDEA201801280263Skin · crackedLEFT WING, DROOPED LEADING EDGE UPPER SKIN AT XDLE 325, FOUND CRACKED. REPAIRED THE SKIN IAW SRM 57-40-01-2R, REPAIR 5, FIG 201. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201801280262Former · crackedRIGHT WING, FIXED LEADING EDGE FORMER AT XOS 584 FOUND CRACKED. THE FORMER WAS REMOVED IAW SRM 51-31-01-0G. A NEW FORMER WAS FABRICATED IAW DWG ARB 2931, REV H, AND INSTALLED IAW SRM 51-31-01-0G. THE REPAIR WAS CLASSIFIED MAJOR IAW GMM 6-2-100.SDR SWIA201844229Skin · corrodedWING PLANK HOLE IS CORRODED. REPAIRED WING PLANK IAW REO.SDR FDEA201801260231Doubler · crackedLEFT WING LEADING EDGE BEADED DOUBLER AT XOS 642 FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201801260230Doubler · crackedLEFT WING LEADING EDGE BEADED DOUBLER AT XOS 630, FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201801260229Doubler · crackedLEFT WING LEADING EDGE BEADED DOUBLER AT XOS 627 FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201801260228Doubler · crackedLEFT WING LEADING EDGE BEADED DOUBLER AT XOS 617, FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201801260241Doubler · crackedRT WING LEADING EDGE CAVITY BEADED DOUBLER AT STA XOS 640 FOUND CRACKED. REPAIR CARRIED OUT AT RT WING LEADING EDGE CAVITY BEADED DOUBLER AT XOS 640 PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201801260236Doubler · crackedLT WING FIXED LEADING EDGE LOWER SURFACE PANEL CUTOUT AT STA XOS 993 FOUND CRACKED. REPAIR CARRIED OUT AT LT WING FIXED LEADING EDGE LOWER SURFACE PANEL CUTOUT AT STA XOS 993 AS PER SRM 57-40-03-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-10SDR CALA2018012600310Skin · crackedA CRACK WS FOUND ON LOWER LT WING SKIN AT WS 990.2. REPAIRED THE SKIN IAW EA 5720-02611, REV B.SDR CALA2018012600309Skin · crackedA CRACK WAS FOUND ON THE LOWER RT WING SKIN WS 990.2. REPAIRED CRACK ON LOWER SKIN WS 990.2 FASTENER HOLE 1 ON RIGHT WING IAW EA 5720-02611 REV B.SDR SCNA20180124011Dome Nut · crackedON WALK AROUND FOUND RIGHT FUEL TANK PANEL 632DB LEAKING. FOUND DOME NUT TO BE CRACKED ON FUEL PANEL 632DB. R&R RT WING FUEL PANEL 632DB. LEAK CHECK GOOD.SDR FDEA201801230177Doubler · crackedLEFT WING LEADING EDGE BEADED DOUBLER AT XOS 760 FOUND CRACKED. THE DOUBLER REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201801230176Doubler · crackedLEFT WING LEADING EDGE BEADED DOUBLER AT XOS 764, FOUND CRACKED. THE DOUBLER REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201801230178Doubler · crackedLT WING LEADING EDGE BEADED DOUBLER AT STA XOS 612 FOUND CRACKED. REPAIR CARRIED OUT AT LT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 612 AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201801230175Doubler · crackedLT WING LEADING EDGE BEADED DOUBLER AT STA XOS 755 FOUND CRACKED. LT WING LEADING EDGE AT STA XOS 755 CRACKED BEADED DOUBLER REPAIRED AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR CALA2018012200298Skin · crackedLEFT WING LE SLAT 1 COVE SKIN HAS CRACKED FWD OF OTBD MAIN TRACK. REPAIRED THE SKIN IAW SRM 57-43-10, FIG 201, REPAIR 4.SDR YENA201801210896Skin · cracked(1/2018) BASIC 6 CHECK AT SAL, REPORTED 2 CRACKS ON THE LT WING LOWER SKIN (P/N 190-33065-009, REF /3/) AT THE AFT EDGE BETWEEN RIBS 9-10, AS SHOWN IN THE REF /1/ EA. THE DAMAGE WAS EVALUATED AGAINST THE SRM AND FOUND TO BE OUT OF LIMITS OF THE REF /4/ SRM. THSDR AALA201802069009Access Panel · damagedELONGATED HOLES FOUND ON THE ACCESS PANEL 640 PB, RIGHT WING, BETWEEN WS 10204 & 10729, BETWEEN RIBS 19 & 20. REPLACED THE ACCESS PANEL IAW AMM 57-27-11.SDR IPXA2018012425839Skin · crackedINSPECTION TYPE: 1C, CRACK ON THE RIGHT WING TRAILING EDGE TOP SPOILER SKIN. REPAIRED IAW SRM 57-51-12, REPAIR G.SDR SWIA201844265Skin · dentedDENT FOUND ON THE LT WING LEADING EDGE WS 200, JUST OUTBOARD FROM OVERWING FUEL CAP. REWORKED THE DAMAGE IAW SRM AND REO.SDR UIEA2018012900130Skin · crackedCRACK ON THE RT WING LOWER IN SPAR SKIN NEAR RWS 655. REPAIR DAMAGED AREA IAW EI T2017A57M-3075, REV 5, AND EI T2017 A57M-3132, REV 1.SDR YENA201801160020Skin · crackedDURING HEAVY MAINTENANCE, THE LEFT WING CRACKED ON THE LOWER SKIN, THE SKIN WAS REPAIRED IAW ETD2018-190-001572, SRM 57-10-01, REP 54, REV 36 AND E18-014-01.SDR DALA2018011800319Panel · crackedLEFT WING T/E FIXED PANEL OTBD FOUND CRACKED. REPLACED THE PANEL.SDR SWAA2022020843362Plate · crackedLH WING AT #3 FLAP TRACK WIGGLE PLATE FOR PANEL 551 EB CRACKED. / L/H WING #3 FLAPTRACK WIGGLE PLATE FOR PNL 551EB CRACKED DRILLED & REMOVED CRACKED WIGGLE PLATE I/A/W SRM 51-40-02-0G-0. LOCATED AND DRILLED NEW L/H WING WIGGLE PLATE IAW SRM 51-40-05-0G-0 ALSO SDR 2018F00075Skin · corrodedLEFT UPPER WING SKINS CORRODED. REPAIRED IAW S-680-0081/14RD, MAJOR REPAIR.SDR 2018FA0000033Skin · corrodedLEFT WING LOWER SKIN CORRODED. REPAIRED IAW DOCUMENT DQ10493M1.SDR 2018FA0000032Skin · corrodedRIGHT WING LOWER SKIN CORRODED. REPAIRED IAW ENGINEERING LETTER DQ10472M1.SDR 2018FA0000030Structure · damagedLEFT WING LEADING EDGE CUFF OVERSIZED ATTACH HOLES. REPAIRED IAW ENGINEERING LETTER DQ10582M1.SDR SWAA2022020813691Retainer · crackedRT WING UPPER AFT T/E PANEL AT #2 PYLON HORIZ. SEAL RETAINER IS CRACKED. / REMOVED CRACKED HORIZ. SEAL RETAINER FROM RT WING UPPER AFT T/E PANEL AT #2 PYLON. INSTALLED NEW SEAL RETAINER IAW SOPM 20-50-01; SRM 51-40-02-0G-0 STEP 4. FASTENER CALLOUTS PER IPC 57-SDR SWAA2022020813672Retainer · crackedLT WING UPPER AFT T/E PANEL AT #1 PYLON VERT SEAL RETAINER IS CRACKED. / REMOVED & REPLACED LT WING UPPER AFT T/E PANEL AT #1 PYLON VERT. SEAL RETAINER IAW SRM 51-40-02-0G-0 PARA 4 & IPC 57-50-00-25 & SRM 51-40-03-0G-0 TAB. 11. 55920U 15JAN18
Back to JASC 5730