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 07FDEA04040Reinforcement · chafedFOUND CHAFING DAMAGE TO REINFORCING PLATE ADJACENT TO THRUST AND SIDE LOAD FITTING RIB 9 REPAIR PERFORMED BY BLEND OUT TO SMOOTH CONTOUR AND NDT FOR CRACK FREE IAW EA 6-5720-81076 AND RAS/BAE/1125/2004 ISS A.SDR 07FDEA03873Support Beam · inoperativeLT WING SPOILER SUPPORT BEAM LOWER CHORD ANGLE I/B OF NR 4 FLAP TRACK HAS INCORRECT REPAIR INSTALLED REF SR-27-57-038. REMOVED AND REINSTALLED LOWER WING T/E PANELS, REMOVED EXISTING DOUBLER. REMOVED AND REINSTALLED NR 4 SPOILER ACTUATOR MOUNT, FLAP TORQUSDR 07FDEA03664Bracket · crackedUPPER TRAILING EDGE PANEL BRACKET IS CRACKED ABOVE ACTUATOR REMOVED AND REINSTALLED UPPER WING ROOT PANEL AT TRAILING EDGE. REMOVED AND REINSTALLED NR 8 SPOILER MOUNT. REMOVED AND REPLACED TRAILING EDGE PANEL BRACKET REPLACED STIFFENERS ON PANEL BRACKET, SDR 07FDEA03673Fitting · wornAT RT SPIGOT FITTING FWD OUTBOARD SIDE FOUND WEAR MARKS REPAIR PERFORMED BY BLEND OUT TO SMOOTH CONTOUR IAW EA 6-5720-79605 AND RAS/BAE/0818/2004 ISS A.SDR TRAX200701339Angle · crackedRIGHT WING BOX AREA, ANGLE CRACKED AT FR 25 (FABRICATION REQ'D).SDR AWXA200701073Stiffener · crackedPHX - MAJOR REPAIR - NR 4118486, CRACKED CENTER WING REAR SPAR VERTICAL STIFFENER, BS 540, RBL 6, WL 158. REPAIRED CENTER WING REAR SPAR VERTICAL STIFFENER, BS 540, RBL 6, WL 158 IAW AWA ER 03-5712-06054-BA1.SDR TRAX200701359Frame · crackedAT JCT FR 25 & WING RIB 4, WING BOX FRAME FOUND CRACKED AROUND RIVET.SDR TRAX200701358Angle · crackedLEFT WING BOX FAIRING, ANGLE AT RIB 4 FR 25 CRACKED.SDR TRAX200701332Angle · crackedWING BOX AREA ANGLE CRACKED AT FR 25 LEFT SIDE.SDR ASAA0752015Support Bracket · crackedRIGHT WING UPPER FIXED TRAILING EDGE PANEL RIG AFT ANGLE SUPPORT BRACKET CRACKED. REPLACED TRAILING EDGE PANEL WITH NEW PART.SDR ASAA0752012Support · crackedLEFT WING UPPER TRAILING EDGE PANEL (WS 278.5) RT AFT ANGLE SUPPORT CRACKED. REPLACED WITH FABRICATED PART.SDR 07FDEA03270Plate · damagedDAMAGED CORNER SECTION AT LT PYLON AFT MOUNT FITTING REPAIR PERFORMED BY BLEND OUT TO SMOOTH PROFILE AND NDT INSPECTION FOR CRACK FREE IAW EA 6-5720-99222 AND RAS/BAE/1002436/2006 ISSUE A.SDR UPS07M50888Structure · crackedINSPECTION TYPE:C LEFT WING LOWER SURFACE L/E ACCESS PANEL CUTOUT STRUCTURE AT STA XORS 51 0 APPROX FOUND CRACK AS MARKED. LEFT WING LOWER SURFACE L/E APPROX XORS 510 DOUBLER REMOVED. NEW DOUBLER FABRICATED USING MAT'L 7075-T6-0.090" PER DOUGLAS DWG ARB2933.SDR 07FDEA03168Panel · delaminatedDELAMINATION FOUND ALONG THE EDGE LANDING OF L/E PANEL A572-46071, BETWEEN TRACK 7-8 ON RT WING. REPAIR PERFORMED BY REMOVING THE DAMAGED LAYERS AND PERFORMING A HOT BOND REPAIR AND RESTORING THE ALUMINIUM LAYER ON THE INTERNAL SURFACE IAW EA 6-5741-103258 SDR 07FDEA03146Intercostal · crackedLT WING L/E CRACK ON INTERNAL INTERCOSTAL. REPAIRED INTERCOSTAL IAW SRM 57-00-01 VOL I FIG 10.SDR 07FDEA03145Intercostal · crackedLT WING L/E INTERNAL CRACK LONG 0.50" ON INTERCOSTAL. 10-10-07 REPAIRED INTERCOSTAL IAW SRM 57-00-01 VOL I FIG 10.SDR USAA070658Angle · crackedON RIGHT WING, LOWER -T- CRACKED AT WBL 135.5. REMOVED & REPLACED WING LOWER ANGLE PER EA 98794, DEFECT SIZE: .75 INCH.SDR CA070910005Washer · damaged(CAN) WHILE DOING CF-1981-25R6 LOWER FWD WING ATTACH FITTINGS YOU MUST REPLACE THE LOWER FWD. WING BOLT WASHER ASSY UPON RE-INSTALL OF BOLTS. NEW WASHER KITS WERE INSTALLED, BUT WERE UNABLE TO TORQUE IAW THE MFG SIRM., THE TORQUE WAS TOO GREAT TO GET THE REQUISDR P5CA0701531Support Bracket · crackedDURING WALK AROUND INSPECTION IN THE LEFT WING FUELING SERVICE PANEL BRACKET SUPPORT CRACK. PERFORMED PART 1 PER XEO 57-082107 AND INTERIM REPAIR APPROVED.SDR 07FDEA02997Angle · corrodedDAMAGED REINFORCING ANGLE IN KRUEGER FLAP AREA RT WING. REPAIR PERFORMED BY REPLACEMENT OF REINFORCEMENT ANGLE IAW SRM 57-41-11.SDR UPS07850708Structure · corrodedINSPECTION TYPE:C2 LEFT WING FLAPWELL FUEL DUMP CHUTE FWD AREAS CORRODED. REPAIRED LEFT WING FLAPWELL FUEL DUMP CHUTE FWD AREAS IAW SRM 51-01-08- 0, 57-02-00 FIG 007, DWG 5649654, AND SRM 51-01-21.SDR TRAX200701184Intercostal · crackedLEFT WING BOX FR 28 INTERCOSTAL CRACKED. LEFT WING BOX FR28 INTERCOSTAL REPLACED IAW SRM 57-25-01. REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IN ACCORDANCE WITH SP 663 FAR 43 APPENDIX A. REPAIR ACCOMPLISHED IN ACCORDANCE SRM 57-25-01. SUPPLEMENTAL - SDR CLSDR 07FDEA02885Channel · crackedLT WING AR T/E REAR SPAR AREA APPROX RS STA491. LOWER FIXED PANEL UPPER INBD CHORD MOUNT BRACKET HAS A CRACK BELOW SPOILER PNL NR 3. REMOVED AND REPLACED BRACKET IAW SRM 51-30-2.SDR 07FDEA02871Bushing · misalignedACCOMPLISHED DVI OF THE LT WING OUT BOARD DRAG FITTING AND FOUND THE INBOARD SIDE BUSHING MIGRATED .060 INCH. REMOVED BUSHINGS IAW SOPM 20-50-03. HFEC INSPECTED FITTING IAW NTM 51-00-16, PT.6. NO DEFECTS NOTED. HONED, CHAMFERED AND FLAP PENNED LUG BORES IASDR TSAA0757045Web · crackedWHILE PERFORMING INSPECTIONS TO COMPLY WITH AD 93-08-04 A CRACK APPROXIMATELY 3 INCHES LONG WAS DISCOVERED AT BS 663.5 RBBL 40 WL 20. REPAIRED IN ACCORDANCE WITH ALOHA ECO 3667. FORM 8100-9 APPROVING REPAIR HAS BEEN RECEIVED. FINAL REPAIR SIZE APPROX 6 X 9SDR TRAX200701153Angle · crackedCRACK FOUND AT FR 27 STR 4L BEHIND WING FITTING ON FORMED PART. EC PERFORMED IAW NTM CRACK CONFIRMED TO RIVET AND DOES NOT EXTEND BEYOND. CRACK CONFIRMED IN RADIUS FROM AFT EDGE RUNNING FWD. CRACK ON LEFT WING PRESSURE DECK SPLICE ANGLE INSPECTED AND FOUND SDR 07FDEA02823Support · crackedLT WING AT T/E REAR SPAR AREA APROX RS STA 383 UPPER FIXED PANEL LOWER C CHANNEL BRACKET MOUNT SUPPORT HAS A CRACK AT FWD SECTION ABOVE NR 3 TRANS ASSY. REMOVED AND REPLACED C CHANNEL SUPPORT IAW SRM 51-30-2. C CHANNEL SUPPORT, FABRICATED ON TRAVELER NR T7SDR DL76S071049Stiffener · crackedDURING HMV AT HAECO, THE WING CENTER SECTION FRONT SPAR LBL 10.94 STIFFENER WAS FOUND CRACKED.SDR TRAX200701167Attach Bracket · crackedRIGHT WING I/B LEADING EDGE O/B ATTACH BRACKET CRACKED. REMOVED RIGHT WING I/B LEADING EDGE O/B ATTACH BRACKET. OK TO INSTALL SERVICEABLE RT WING I/B LEADING EDGE O/B ATTACH BRACKET P/N 600-12025-8. INSTALLED SERVICEABLE RT WING I/B LEADING EDGE O/B ATTACH SDR UPS07M50812Stiffener · crackedINSPECTION TYPE:C RIGHT WING L/E COMPARTMENT AT STA XORS 714 APPROX FOUND UPPER STIFFENER CRACKED AS MARKED. CRACKED STIFFENER REMOVED. NEW STIFFENER FABRICATED USING MAT'L 707 5-0-0.071" AS PER DOUGLAS DWG ARB3954. STIFFENER HEAT TREATED PER DPS 7.00-1 & HSDR UPS07M50741Stiffener · crackedINSPECTION TYPE:C RIGHT WING L/E COMPARTMENT AT STA XORS 568 APPROX FOUND UPPER STIFFENER CRACKED AS MARKED. CRACKED STIFFENER & ATTACH PARTS REMOVED. NEW STIFFENER FABBED USING MAT'L 7075-0-0.071" PER DOUGLAS DWG ARB3954. STIFFENER HEAT TREATED PER DPS 7.0SDR TRAX200701134Angle · crackedLEFT WING BOX FR 28 FAIRING FRAME ANGLE CRACKED. REPAIRED AS PER ANA/YUL07/192/375-004 REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IAW SP663 AND FAR 43 APPENDIX A.SDR WRLA2007080Structure · crackedDURING 1C+12A CHECK, EGAT MAINT FOUND CRACK ON LT WING ANTI-ICING TELESCOPING DUCT DOOR CUTOUT AT STA XOS=464 & XOS=470. CRACK REPAIRED PER MD-11 SRM VOL 1 57-10-00 FIG 43 REV 39 & EI 2006P20A-124 REV 00. (REPAIR DOUBLER)SDR 07FDEA02662Support Bracket · crackedRT WING O/B FLAP, I/B HINGE, O/B ATTACH BRACE CRACKED AT REAR SPAR. REMOVED AND REPLACED CRACKED SUPPORT ARB0029-506. REF SRM 57-00-01.SDR 07FDEA02618Splice · crackedLEFT WING LEADING EDGE OVER WING PANEL 3342, FORWARD SPLICE ANGLE HAS LOOSE/WORKING RIVETS AND IS CRACKED IN HALF. REPLACED FASTENERS AND FAB SPLICE ANGLE REF 51-30-2, GMM 7-0-1001, DWG 65-22555.SDR 07FDEA02613Fairing · crackedRT WING OB TE NR 8 JACKSCREW FAIRING, CRACK COMING OUT OF FASTENER HOLE AT FWD END. REMOVED DAMAGE AREA REF SRM 57-20-4 FIG 1 PG 5. FAB`D REPAIR PARTS REF SRM 51-30- 05 AND 57-20-4 FIG, 1 PG 5. INSTALLED REPAIR PARTS REF SRM 51-30-02 PG 1 AND REF SRM 57-20-SDR 07FDEA02611Bracket · crackedRT WING FWD NAV LIGHT BRACKET CRACKED. REPLACED RT WING FWD NAV LIGHT BRACKET, REF SRM 51-30-02 P.13.SDR TRAX200701029Plate · crackedLEFT TELESCOPE DUCT CLOSING PLATE CRACKED (LT OR RT WING SLAT CLOSING PLATES). 10-18-07 INSTALLED NEW ANT-ICE TELESCOPIC DUCT CLOSING PLATE IAW CRJ 700 AMM 57-40-01. OPS CK GOOD.SDR UPS07M50438Cable Guard · chafedINSPECTION TYPE:C LEFT WING - L/E PANEL NR 527AB U-BRACKET GUARD FOUND CHAFING AS MARKED. LEFT WING - L/E PANEL NR 527AB U-BRACKET GUARD CHAFE MARK REMOVED. ORG THK 0.0 63" MATL REMAIN 0.040" MATL REMOVED 0.023". FOUND EXCEED LIMIT SRM 51-00-01F IGAVIR38. SDR UPS07M50349Structure · crackedINSPECTION TYPE:C RIGHT WING - WING T/E INBOARD ISLANDS UPPER SURFACE FOUND CRACK ON FWD SIDE APPROX AT XORS 444 AS MARKED. HFEC INSP C/O DAC NDTSPM R13P6 06-10-01.001 & 05 EA CRACKS END CON- FIRMED. FASTENERS AT AFFECTED AREA REMOVED FOR ACCESS SRM 51-31-01SDR 07FDEA02495Stop Fitting · crackedLEFT WING OUTBOARD FLAP SECONDARY UP STOP FITTING FOUND CRACKED. [08-02-07] REMOVED CRACKED FITTING AND INSTALLED NEW FITTING AT LT WING OUTBOARD FLAP AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR UPS07M50439Cable Guard · chafedINSPECTION TYPE:C RIGHT WING - L/E PANEL NR 627AB CABLE GUARD U-CHANNEL FOUND CHAFED AS MARKED. RIGHT WING - L/E PANEL NR 627AB CABLE GUARD U-CHANNEL CHAFE MARK REMOVED. ORG THK 0.063" MATL REMAIN 0.033" MATL REMOVED 0.030". FOUND EXCEED LIMIT SRM 57-00-01 SDR 07FDEA02477Stiffener · crackedDURING PERFORM OF OAN J/C 0600B620-2JR, FOUND NR 2 CRACKS 0.50" LONG ON STIFFENERS OF L/E ACCESS PANEL 617CT. REPAIRED STIFFENERS IAW SRM 57-10-00 VOL 1 FIG 10.SDR 07FDEA02402Channel · crackedLT WING OB TE FLAP WELL LWR FIXED PNL SPPT CHANNEL IS CRACKED AT STRUT ATTACH POINT RSS 501 IB SIDE (MKD). REMOVED AND REPLACED CHANNEL ON LT WING OB TE FLAP P/N 65-21658 USE P/O 1013862, FX 0993 IAW B 727 SRM 51-30-2.SDR DLM88070883Angle · corrodedEXFOLIATION CORROSION ON LT TRAPAZOIDAL PANEL UPPER ANGLE. ANGLE WAS REPLACED PER DWG 5930515 ON N/R TOO60106 HMV-3.SDR UPS07450317Stiffener · corrodedINSPECTION TYPE:C RT W/G W/W STIFFENER APPEAR CORRODED AT STA1241 RBL 63. RT W/G W/W AT BS 1241 RBL63 VERTICAL STIFFENER REPLACED AND INSTALLED AS PER SRM 51-10-10 PG 9 AN 51-30-02.SDR 07FDEA02374Seal Depressor · crackedLT WING TE PNL 8155 SEAL DEPRESSOR IS FRETTED, CRACKED ALONG INBD EDGE. REPLACED SEAL DEPRESSOR IAW SRM 51-30-2.SDR 07FDEA02373Skate Angle · crackedRT WING AT NR 6 FLAP TRACK FWD FAIRING, I/B SKATE ANGLE IS CRACKED. REMOVED DAMAGE, FABRICATED NEW 2 REPAIR ANGLE AND INSTALLED 2 REF. REPAIR ANGLES, REF SRM 51-40-3 PG 1-6.SDR UPS07M50348Structure · crackedINSPECTION TYPE:C RIGHT WING - WING T/E INBOARD ISLANDS UPPER SURFACE FOUND CRACK ON FWD SIDE APPROX AT XORS 455 AS MARKED. HFEC INSP C/O DAC NDTSPM REV13 06-10-01.001 & FOUND CRACK OF .375 INCH. FASTENERS AT AFFECTED AREA REMOVED FOR ACCESS SRM 51-31-01VII SDR 07FDEA02346Channel · crackedLEFT WING FIXED TRAILING PANEL SUPPORT BRACKETS, ARE CRACKED AT SUPPORT ROD. SUPPORT ROD ATTACHS TO, TWO PANELS LOCATED JUST INBD OF THE NR 2 SPOILER. REMOVED, LOCATED, DRILLED AND INSTALLED Z BRACKET LT WING T/E PANEL SUPPORT BRACKET INBD OF NR 2 SPOILER PE
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