JASC 5720
Service difficulty reports · 13,638
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 ASAA0240118Angle · crackedPAE - DURING C-CHECK, FOUND NR 3 IFOT FAIRING HAS A CRACKED ANGLE OUTBOARD OF SIDE UPPER EDGED JUST INBOARD OF NR 3 SPOILER. REMOVED AND REPLACED ANGLE IAW SRM. (M)SDR GAIA02130STStiffener · crackedDURING A LTC INSPECTION, IN WAS DISCOVERED THAT THE LEFT WING LEADING EDGE AT WS 62.4 HAS A BOTTOM STIFFENER CRACKED. ACCOMPLISHED REPAIR IAW BOEING 727 SRM 57-10-2, FIGURE 3 AND 51-40-4, FIGURE 1. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR MWEA020568Splice · damagedFASTENER HOLES DAMAGED IN CENTER TANK ON STRINGER 17 AFT SPLICE PLATE APPROXIMATELY 1 INCH LEFT OF STATION 0 BULKHEAD. SPOTFACED HOLE TO REMOVE DAMAGE, FABRICATED AND INSTALLED FASTENERS IN STRAP.SDR SWIA200211290Bracket · crackedLOWER BRACKET AT RIB 16 APPEARS TO BE CRACKED ALONG OUTBOARD, AFT AREA OF BRACKET. RIGHT FUEL CELL. FOUND ON C-CHECK INSPECTION. REMOVED CRACKED CLIP AND FABRICATED NEW CLIP AND INSTALLED NEW SKIN CLIP IAW EMB SRM 51-40-02.SDR SWIA200211289Bracket · crackedSMALL LOWER BRACKET AT RIB 15 IN RIGHT FUEL CELL IS CRACKED. CRACK IS ON INBOARD SIDE OF FRAME. FOUND ON C-CHECK INSPECTION. REMOVED AND REPLACED CRACKED SKIN CLIP IAW EMB SRM 51-40-02.SDR CALA0200465Angle · crackedINSPECTION FOUND A 3" CRACK IN L/H WING LOWER/AFT O/B SUPPORT ANGLE. THE SUPPORT ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-2.SDR QXEA0201489Stiffener · chafedPDX- ACCESS PLATE 524AT HAS CHAFFED STIFFENER WHERE IT CONTACTED NR 1 WIGGINS FITTING. REPAIRED IAW HORIZON AIR EA 2-57-194.SDR MWEA020562Fitting · corrodedRIGHT WING XCW 58 LOWER WING TEE REQUIRES REPAIR OR REPLACEMENT DUE TO CORROSION REMOVAL. REMOVED WING TEE, RECEIVED NEW WING TEE, LOCATED AND DRILLED AND INSTALLED WING TEE.SDR MWEA020550Clip · crackedCENTER TANK FORWARD SPAR ACCESS WEB 8 EACH INSULATION ATTACH CLIPS REQUIRE REMOVAL TO FACILITATE OTHER MAINTENANCE. REMOVED AND INSPECTED CLIPS, FABRICATED AND INSTALLED CLIPS.SDR QXEA021482Bracket · crackedPDX- LT WING FRONT SPAR "Z" BRACKET IS CRACKED AT TOP END AT STATION YW58.20. REPAIRED IAW DHC-8 SRM 51-40-11.SDR UPS02839486Stringer Clip · crackedINSPECTION TYPE:C1 RIGHT WING STA XRS 289 LOWER STRINGER CLIP IS CRACKED AT STRINGER 61. REMOVED, FABRICATED, AND INSTALLED CLIP IAW DWG 4614391, SAA SK 708-435, UPS ENGINEERING FILE NUMBER DC8-57-20058, AND SRM 51-1-20D.SDR AWXA200200930Stiffener · crackedMCN - MAJOR REPAIR - DURING C-17 CHECK A 1.75 INCH CRACK WAS FOUND ON THE RT WING INTERNAL STRAP AT THE INBOARD SIDE AFT END OF NR 6 FLAP TRACK FAIRING, WS 259 RT. MAINTENANCE REMOVED DOUBLER AND DAMAGED STIFFENER, FABRICATED A NEW DOUBLER AND STIFFENER, AND SDR 2002FA0001090Bracket · misinstalledDURING AN ANNUAL INSPECTION, FOUND WING ROOT FAIRING BRACKET AGAINST LOWER PART OF FORWARD SPAR (LEFT WING). THE BRACKET APPEARS TO HAVE BEEN INSTALLED TOO CLOSE TO THE SPAR AT MANUFACTURE, CAUSING LOCAL MINOR DAMAGE. REPAIRED LOCAL DAMAGE. INSPECTED ENTIRESDR UPS02839329Angle · crackedINSPECTION TYPE:C1 LEFT WING L/E VERTICAL ATTACH ANGLE IS CRACKED AT LOWER END AT XS 250. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 9753293, AND SRM 51-1-20D, 51-3-0.SDR UPS02839411Fitting · crackedINSPECTION TYPE:C1 LT WING NR 2 MAIN XRS 74.000 STRINGER END FITTING CRACKED AFT FITTING. REMOVED AND REPLACED END FITTING IAW DC8 SRM 51-1-20D AND 51-1-23SDR UPS02839451Fitting · crackedINSPECTION TYPE:C1 S-51 STRINGER END FITTING CRACKED FWD SIDE AT XRS 74.000 2 MAIN. REMOVED AND REPLACED END FITTING IAW DC8 SRM 51-1-20D AND 51-1-23.SDR UPS02839447Fitting · crackedINSPECTION TYPE:C1 S-51 STRINGER END FITTING CRACKED AFT SIDE AT XRS74.000 NR 3 ALT. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D AND 51-1-23.SDR QXEA0201329Angle · crackedPDX - LEFT HAND WING FRONT SPAR CONNECTION ANGLE FROM NACELLE TO WING SPAR HAS A CRACK IN CONNECTION ANGLE AT TOP AFT RIVET. REPAIRED IAW DHC-8 SRM 51-40-00 AND SRM 51-40-11.SDR QXEA0201247Angle · scratchedPDX - LEFT HAND WING TOP EDGE NUT PLATE ANGLE FOR LEADING EDGE PANELS 512AL AND 512DL HAS SCRATCH DAMAGE TO FORWARD SPAR TOP EDGE. REPAIRED IAW RD 8-57-1675.SDR AUS20020935Plate · corroded(AUS) WING SPLICE PLATE CONTAINED EXFOLIATION CORROSION ON THE RH AFT EDGE. FOUND DURING INSPECTION IAW AD/PA31/122 AMDT1.SDR ARWA20020910Support Fitting · crackedDURING C-CHECK, RT WING L/E INTERIOR STA XW 239.743 INBOARD PYLON FRONT SPAR SUPPORT FITTING (FOOT STOOL) WITH CRACK. REMOVED AND REPLACED FOOT STOOL FITTING IAW BOEING MESSAGE INSTRUCTIONS ARW-MIA-02-00020H DATED 08/21/02, S/B DC8-57-84, DC8-A57-84 AND DC8-SDR QXEA0201265Support Bracket · crackedPDX - CRACKED SUPPORT BRACKET UPPER FOR LEADING EDGE AT STATION 139.000, LEFT HAND WING. REPAIRED IAW DHC-8 SRM 51-20-11.SDR QXEA0201264Support Bracket · crackedPDX - CRACKED SUPPORT BRACKET BOTTOM FORWARD SPAR FOR LEADING EDGE AT YW139.000. REPAIRED IAW DHC-8 SRM 51-40-00 AND SRM 51-40-11.SDR QXEA0201263Support Bracket · crackedPDX - CRACKED THE SUPPORT BRACKET AT TOP FORWARD SPAR FOR LEADING EDGE. REPAIRED IAW DHC-8 SRM 51-40-00.SDR UPS02839095Angle · corrodedINSPECTION TYPE:PFLT RIGHT W/W CORROSION FLAP WELL AREA. REPLACED ANGLE.SDR MWEA020482Clip · crackedREMOVED LEFT FUEL TANK SHEAR CLIP AT 69 BULKHEAD BETWEEN STRINGER 12 & 13. DRILLED UP CLIP AND INSTALLED FASTENERS.SDR TSAA0251189Stiffener · crackedLT WING FRONT SPAR STIFFENER CRACK AT FSS 473.31 AND FSS 475.55. REMOVED, FABRICATED AND INSTALLED STIFFENERS. NEW STIFFENERS FABRICATED FROM 7178-T6511 EXTRUSION AND NEW SHIMS FABRICATED FROM 2024-T3, APPLIED ALODINE AND BMS 10-11 TYPE 1 PRIMER AND BMS 10-1SDR QXEA0201218Support Bracket · crackedPDX - BLEED AIR SUPPORT Z-BRACKET CRACKED AT RIGHT HAND WING FRONT SPAR, STATION YW53.200. REPAIRED IAW DHC-8 SRM 51-40-11 AND HORIZON AIR EA 2-57-178.SDR MWEA020488Fitting · crackedLEFT WING TEE OUTBOARD LOWER LEG HAS PITTING/EXFOLIATION CORROSION ON UPPER SURFACE BETWEEN STRINGER 13 AND 14, ALSO EXTENDING UNDER STRINGER 14 AND 13. ALSO FOUND CRACK ON OUTBOARD LEG. BLENDED OUT CRACK AND REMOVED CORROSION AROUND AND UNDER STRINGER.SDR AZ5Y745MPanel · looseDURING REMOVAL OF A DRY BAY PANEL FOR TROUBLESHOOTING OF A FUEL LEAK, ONE OF THE ATTACHMENT BOLTS FELL OUT. IT LOOKED AS IF IT HAD BEEN SAWN OFF. THE DRY BAY PANEL IS NUMBER 4 AS PER 28-11-00 PG 653 (PANEL 532BL AS PER 28-11-07 PG 603). ALSO A TOTAL OF 4 ATSDR UPS02839123Fitting · crackedINSPECTION TYPE:C1 RT WING STR 51 I/B SIDE STA 74 IS CRACKED. REMOVED FITTING IAW DC8 SRM 51-1-20D, LOCATED DRILLED AND DEBURRED NEW FITTING IAW DC8 SRM 51-1-24, INSTALLED FITTING IAW DC8 SRM 51-1-20D, TORQUED BOLT IAW DC8 SRM 51-1-23.SDR DHL2002721511Fitting · crackedDURING C-CHECK, RT WING STRINGER LUG CRACKED AT RIB ATTACH WS 656. CRACK IN LUG TERMINATES AT FASTENER HOLE ON RT VENT BOX STRINGER AT RIB ATTACH WS 656 VERIFIED BY 10 X MAGNIFYING GLASS. DRILLED UP REPAIR PARTS AND INSTALLED.SDR UPS02439225Stiffener · corrodedINSPECTION TYPE:C, RIGHT WLG BS 1241 BULKHEAD STIFFENER FOUND CORROSION AT WL 150 RBL 4-10. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT EXCEEDS SRM 57-10-01 FIG 1 LIMITS FOR REPAIR REFER TO HX RS R57-12-34875.SDR QXEA0201183Support · chafedPDX-CHAFING ON BRIDGE SUPPORT ASSEMBLY. SUPPORTING WING TO FUSELAGE FAIRING AT STATION YW57.000. REPAIRED IAW DHC8 SRM 51-20-11, PAGE 5.SDR QXEA0201182Intercostal · chafedPDX-CHAFING ON INTERCOSTAL OF WING TO FUSELAGE FAIRING AT STATION YW57.000. REPAIRED IAW DHC8 SRM 51-20-11, PAGE 5.SDR SWIA200211105Structure · leakingLEFT OUTBOARD FLAP ACTUATOR REMOVED DUE TO FUEL CONTAMINATION ON FLAP FROM FUEL LEAK. REPAIRED LEAK IN FUEL CELL & INSTALLED ACTUATOR IAW 28-10-00 & 27-50-00.SDR QXEA0201134Bracket · crackedPDX- UPPER END OF Z-BRACKET IS CRACKED AT FORWARD RIGHT HAND WING SPAR AT STATION Y58.20. REPAIRED IAW HORIZON AIR EA 2-57-171 AND DHC-8 SRM 51-40-11.SDR QXEA0201133Bracket · crackedPDX- Z-BRACKET IS CRACKED AT FORWARD SPAR STATION YW58.200 ON LEFT HAND WING. REPAIRED IAW HORIZON AIR EA 2-57-170 AND DHC-8 SRM 51-40-11.SDR QXEA0201132Mount Bracket · crackedPDX- BOTTOM MOUNT BRACKET IS CRACKED AT STATION YW139.000 ON FORWARD SPAR OF LEFT HAND WING. REPAIRED IAW DHC-8 SRM 51-40-00.SDR QXEA0201131Mount Bracket · crackedPDX- TOP MOUNT BRACKET CRACKED AT STATION YW139.00 OF FORWARD SPAR LEFT HAND WING. REPAIRED IAW DHC-8 SRM 51-40-00.SDR 0203229867Rib · crackedDuring Mck in ATL, a crack was found in the left wing leading edge rib at station x 134.921. The crack emanates from the fastener hole and extends inbrd to the edge of the part. Repaired per EA 98-190577.SDR UPS02839034Stiffener · crackedINSPECTION TYPE:C2 LEFT WING T/E INBOARD VERTICAL STIFFENER AT FLAP HINGE 98 IS CRACKED AT BOTTOM. REMOVED, FABRICATED, AND INSTALLED STIFFENER IAW DWG 3643320, AND SRM 51-3-0.SDR QXEA0200995Support · chafedPDX - RT WING TOP TRAILING EDGE SUPPORT STRUCTURE HAS CHAFE DAMAGE FROM CONTACTING FLAP WHILE IN UP POSITION, AT YW174. REPAIRED IAW DHC-8 SRM 51-40-11 AND RD 8-57-1549, PAGE 3, STEPS 1, 3, AND 4.SDR QXEA0200973Support · chafedPDX- LEFT HAND WING TOP TRAILING EDGE SUPPORT STRUCTURE HAS CHAFE DAMAGE FROM CONTACTING OUTBOARD FLAP WHILE IN THE UP POSITION. REPAIRED IAW DHC-8 RD 8-57-1549.SDR MWEA020445Stiffener · corrodedRIGHT WING LIGHT CORROSION ON UPPER SURFACE OF HORIZONTAL STIFFENER ON INBOARD SIDE OF XRS 91 RIB ABOVE STRINGERS 17 TO 19. REMOVED AND INSTALLED STIFFENER AND FLAPPER VALVE.SDR CUX2002F00002Stiffener · crackedRIGHT WING UPPER FORWARD STIFFENER (PN 50-120068-7) WAS DISCOVERED CRACKED DURING A ROUTINE PHASE 1 INSPECTION. THE CRACK BEGAN AT THE INBOARD EDGE, EMANATING OUTWARD THROUGH THE FIRST 2 RIVET HOLES FOR A TOTAL LENGTH OF 1.55 INCHES. THE DAMAGED PART WAS REMSDR CUX2002F00000Fitting · scratchedLEFT WING LOWER FORWARD INBOARD WING BOLT ATTACH FITTING (PN 50-120073-7) WAS DISCOVERED TO HAVE 3 SMALL SCRATCHES DURING A REPETITIVE INSPECTION OF AD. THE SCRATCHES WERE LOCATED ON THE ATTACH BOLT WASHER SEARING FACE RADIUS IN AN AXIAL DIRECTION AND WERE APSDR DHL2002806504Flange · brokenDURING C-CHECK, FOUND LT FWD AUX TANK UPPER CAP FLANGE 2 BROKEN AT STA XFS 20.000. FABRICATED DOUBLER PER SRM 57-2-0 FIG 2. INSTALLED DOUBLER PER SRM 57-2-0 FIG 2.SDR ABXA020098Fitting · corrodedRIGHT WING STATION 219, FLAP LINK SUPPORT (CANOE) WAS CORRODED AND PITTED UNDER AFT TRACK PLATES. REMOVED CORROSION FROM FLAP LINK SUPPORT FITTING AND FABRICATED REPAIR FILLERS IAW DC-8 SERVICE BULLETIN 27-164. REMOVED CORROSION FROM LEFT AND RIGHT SIDE SUPPSDR 02FDEA00482Structure · damagedNR 2 RT PYLON AFT FAIRING UPPER SIDE HYDRAULIC LINES HOLE ELONGATED ON THE FAIRING SIDE. REMOVED AND REPLACED HYD LINE HOLES PER EA 6-5710-64292.
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