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 07FDEA01281Cap · crackedRT WING L/E FOUND ONE CRACK 1" LONG ON FIXED CAP STA XORS 827. REPAIRED IAW SRM 57-10-00 FIG 49 VOL 1.SDR 07FDEA01255Structure · corrodedRT WING SEVERE CORROSION ON UPPER BEAVER TAIL. REPAIR CORROSION IAW FEDEX EA 8-5710-103714.SDR 07FDEA01251Skin · crackedCORROSION ON RT WING BOTTOM SKIN IN AREA OF RIB 4-5 AROUND SEVERAL FASTENERS. CRACKS WERE FOUND IN TWO HOLES. REPAIR PERFORMED BY REMOVING CORROSION AND REMOVING CRACKS AT HOLE NR 666 AND NR 1466 BY OVERSIZING IAW EA 6-5720-101321 AND RAS/BAE/1002865/2006 ISSDR 07FDEA01207Support · crackedRT WING INBD TE LOWER SURFACE FWD INNER SUPPORT CLIP IS CRACKED AT ATTACH TO REAR SPAR FLANGE OFF PANEL 10" O/B OF O/B END OF MLG BEAM REMOVED DAMAGED CLIP, VERIFIED REPAIR MATERIAL AS 2024-T3-.040 REF DWG NR 65-21656, AND FABRICATED REPLACEMENT CLIP REF DWGSDR DHL2007806506Angle · crackedFOUND RT OUTBD FLAP T/E ANGLE CRACKED (STA XF 125.000 - 169.000). REMOVED CRACKED ANGLE IAW SRM 51-1-21. FABRICATED NEW ANGLE (AL2024 "0" 0.050") IAW SRM 57-7-1 FIG 3. PERFORMED HEAT TREATMENT FROM 2024 "0" TO 2024T4 IAW SRM 51-1-1 PG 1-13-17. CLEANED, TRESDR SWIA200718169Shroud · crackedRIGHT L/E OUTBOARD SECTION SHROUD CRACKED, DISCOVERED AT C-CHECK. INSTALLED NEW SHROUD PER CRJ200 SRM REF 57-41-29 AND CRJ200 SRM REF 51-25-00 PG 1.SDR SWIA200718166Clamp · crackedLEFT WING PICCOLO TUBE CLAMPS CRACKED INSIDE ACCESS PANELS 530FZ, 530GZ, 530JZ, 530AZ AND 530BZ, DISCOVERED AT C-CHECK. REPLACED CLAMPS INSIDE ACCESS PANELS 530FZ AND 530GZ WITH P/N 601R80004-7, PANEL 530JZ WITH P/N 601R8004-9, AND PANELS 530AZ AND 530BZ WITHSDR 07FDEA01161Shroud · corrodedFOUND CORROSION FINDING ON RT WING OUTER SHROUD BOX RIB 25-29 REPAIR PERFORMED BY BLEND OUT IAW EA 6-5720-106375 AND RAS/BAE/1004284/2007 ISS. A.SDR 07FDEA01159Fairing · crackedCRACKED SHIM PLATE AT INNER SIDE AFT AREA OF LT NR 3 FLAP TRACK FIXED FAIRING. REPAIR PERFORMED BY WET LAY-UP PER SRM 57-20-35 AND INSERT INSTALLATION, APPROVED BY EA 6-5720-106421 AND RAS/FOK/016/2007 ISS. ASDR 07FDEA01138Angle · corrodedCORROSION AND CRACK FINDINGS DURING SEALING ANGLE INSTALLATION- EO 6-5710-7-5002- SB A300-57-6033 REV 1- SBA300-57-6027 REV 6- AD 98-18-02 AND AD 2006-07-07 REPAIR PERFORMED BY REAM UP IAW EA 6-5720-106433 AND RAS/BAE/1004205/2007 ISS. A.SDR 07FDEA01136Angle · corrodedCORROSION AND CRACK FINDINGS IN HOLES DURING SEALING ANGLES INSTALLATION-EO 6-5710-7-5002-SB A300-57-6033 REV 01-SB A300-57-6-27 REV 6- AD98-18-02 AND AD 2006-07-07. REPAIR PERFORMED BY REAM UP AND SEALING ANGLE REPLACEMENT IAW EA 6-5720-106433 AND RAS/BAE/10SDR QXEA200700582Panel · corrodedC3 OKC - BUTE DOOR PANEL 691KB HAS LIGHT SURFACE CORROSION IN FASTENER HOLES. REPAIRED IAW SRM 51-21-06, 51-25-16.SDR SWAA071572Bar · corrodedDURING SCHEDULED SERVICE CHECK, FOUND RIGHT WING STABILIZER BAR CORRODED. REMOVED AND REPLACED RIGHT WING STABILIZER BAR PER MM.SDR K11A2008120272206Stiffener · corrodedVERTICAL STIFFENER CORRODED WS 198.SDR K11A2008112672210Stiffener · corrodedREAR SPAR VERTICAL STIFFNER HAS AREA OF A COOROSION.SDR K11A2008112672209Stiffener · corrodedREAR SPAR VERTICAL STIFFNER HAS AREA OF CORROSION.SDR 07FDEA01026Web · crackedR/M/G WEB CRACKED AT NR 8 SPOILER MOUNT AFT OF GEAR. REMOVED AND REPLACED WEB IAW SRM 51-40-2, AND SRM 51-30-2. REMOVED AND REPLACED EXTERNAL DOUBLER IAW SRM 51-20-1, FIG 7, AND SRM 51-30-2.SDR TRAX200700401Angle · crackedUPPER ATTACH ANGLE BETWEEN LT WING INBOARD AND MIDDLE LE`S ARE CRACKED. REMOVED DAMAGED ANGLE ON LT WING LE AND DUPLICATED USING 0.040, 2024-T3 PER CRJ SRM 51-24-21 AND 51-40-11. OK TO ALODINE, PRIME, AND INSTALL. ALODINED AND PRIMED ANGLE IAW CRJ SRM 51-25-0SDR 07FDEA00993Angle · crackedCRACK FINDINGS IN ANGLE (HOLE 11, 13, 42, 45, 160, 180, 191, ALL LT SIDE) DURING ACCOMPLISHMENT OF EO 6-5710-7-3305, SB A300-57-6050 REV.03, AD 2005-23-08 REPAIR WAS PERFORMED BY REAM OUT, OVERSIZING AND COLD WORKING IAW EA 6-5710-106435 AND RAS/049856/032/SDR 07FDEA00948Stiffener · damagedRT WING, SHROUD BOX F/S SPAR, DAMAGE BY MAIN BARREL PIN. REPAIR WAS RENEWED BY REPLACEMENT OF VERTICAL STIFFENER.SDR PG9A114594Pitch Control · damagedA BROKEN TT BAR LAMINATE DAMAGED THE SPIDER BEYOND LIMITS. INSTALLED SERVICEABLE SPIDER ASSY.SDR 2007UALA00783Web · crackedRIGHT WING LEADING EDGE CAVITY, WEB CRACKED AT LES 588. DAMAGE TO WING FIXED LEADING EDGE NOSE BEAM WEB. AFFECTED SRM REPAIR PROCEDURE. VERIFIED CRACK CONTAINED BY STOP DRILLS PER HFEC NDT 51-00-19, PRT 6. FABRICATED REPAIR PARTS AND INSTALLED PER SRM 57-SDR QXEA200701329Bracket · crackedC4 PDX - RIGHT WING LEADING EDGE BRACKET IS CRACKED AT YW 138.00. REPAIRED IAW SRM 51-40-11 AND 51-40-00.SDR CA070314006Structure · cracked(CAN) RT FORWARD WING WALK ASSEMBLY, P/N 62061-002. RT ROOT WAS CRACKED. (TC NR 20070314006)SDR UIEA200700123Angle · crackedVERTICAL "L" EXTRUSION ANGLE CRACKED AT RIGHT WING UPPER SURFACE, BELOW GAP PANEL 611CT FOR NR 3 PYLON AT INBOARD SIDE, FORWARD CORNER, WING STATION 670.25. REMOVED AND REPLACED "L" ANGLE EXTRUSION P/N 221738-3-1 AS PER 747-200 SRM 51-30-02 AND SRM 51-10-02. SDR 07FDEA00597Stringer · damagedFOUND LT AND RT WING STRINGER NR 8 FUEL COMPENSATOR FASTENER HOLES OF THE ARB0903 DOUBLER, EXISTING REPAIRS. FOR SUSPECT CRACK STRIP PAINT AREA WITH CHEMICAL METHOD FOR PERFORMED PENETRANT INSP STRIPPED PAINT IAW SRM 51-21-01 PAGE 26 VOL 2. PERFORMED INSP IASDR QXEA200700327Bracket · crackedC4 PDX - FOUND UPPER LEFT LEADING EDGE BRACKET AT YW 137.0 IS CRACKED. REPAIRED IAW SRM 51-40-00 AND 51-40-11.SDR EIA2007042Structure · corrodedRIGHT WING LEADING EDGE LOWER CHORD FORWARD FACE CORRODED AT OLES 1520, 1440 AND 1374 AND LOWER CHORD TO SKIN INTERFACE AT OLES 1405. REMOVED CORROSION, NDT AREAS, FABBED AND INSTALLED REPAIR PER B747 SRM 57-30-01 PAGES 21-22.SDR A6WA200740071Structure · damagedFOUND NR 15 HOLE AT WS 148 LHS IS ELONGATED TO .230 INCH. (M) MAINTENANCE REPAIRED BY CLEANING UP HOLE AND INSTALLING FREEZE PLUG IAW EO 601R57-10925A. (K)SDR UPS07849243Web · crackedINSPECTION TYPE:C3 NR 2 MAIN TANK THRU PNL 506C WEB IS CRACKED FWD OF CTR/SPAR XRS -6. STOP DRILLED CRACK AT NR 2 MAIN TANK WEB AT STA XRS -6 IAW SRM 57-02-00 FIG 002. FABRICATED AND INSTALLED REPAIR DOUBLER AT NR 2 MAIN TANK WEB AT STA XRS -6 IAW SRM 57-02-SDR 07FDEA00494Structure · damagedDAMAGED HOLES FOUND DURING ACCOMPLISHMENT OF EO 6-5710-7-3305. HOLES H/I ON LT AND L/K ON RT. REPAIR WAS PERFORMED IAW RAS 033237/026/2004 ISSUE: A AND EA 6-5710-106351.SDR 07FDEA00493Structure · damagedDAMAGED HOLES FOUND DURING ACCOMPLISHMENT OF EO 6-5710-7-3305, HOLES L/U/I/K ON LT AND K ON RT. REPAIR WAS PERFORMED IAW. RAS 033237/026/2004 ISSUE: A AND EA 6-5710-106351.SDR 07FDEA00491Repair · unknownFOUND OLD REPAIR BY INSTALLATION OVERSIZE FASTENERS, HOLE 2 LT, 187 RT AND 165 RT. REPAIR VERIFICATION OF OVERSIZED FASTENERS IAW RAS 033237/017/2004 ISSUE: A AND EA 6-5710-106363.SDR UPS07849210Doubler · crackedINSPECTION TYPE:C3 LEFT WING CENTER L/E UPPER INNER DOUBLER CRACKED AT STA XOLDI 6.2246. REMOVED CRACKED DOUBLER AT LEFT WING CENTER L/E STA XOLDI 6.2246 IAW SRM 51-1-21. FABRICATED AND INSTALLED REPLACEMENT DOUBLER AT LEFT WING CENTER UPPER L/E STA XOLDI 6.SDR P5CA0701510Support Tube · damagedLT WING FIXED L/E PANEL DAMAGED AT REFUEL ACCESS PANEL DOOR. REPLACED FIXED L/E SUPPORT RODS FORWARD OF REFUEL PANEL DOOR. ACCOMPLISHED TIME LIMITED, INTERIM REPAIR TO SKIN AND RIB IAW MA A4 57-41-01:01.SDR 200700114Stiffener · crackedWHILE PERFORMING CASA COM LETTER 212-224 AND CASA SB 212-57-57-30, A CRACK WAS NOTED FROM THE 4TH RIVET TO THE 5TH RIVET FROM THE BOTTOM, ON THE VERTICAL STIFFINER LOCATED ON THE LT WING AT STA 4700, AFT SPAR WEB. THREE STIFFINERS NEXT TO THE ORIGINAL ARE CRASDR DHL2007802511Splice · crackedRT WING CTR LE UPPER INTERNAL SPLICE 2" CRACK STA XOLD 6.2246. REMOVED CRACKED SPLICE IAW SRM 51-1-21, SRM 51-3-0, SRM 51-1-20D. FABRICATED SPLICE (AL7075T6 0.080") IAW BOEING MSG NR 1-275396206-21 DATED JAN 23,2007. CLEANED, TREATED AND PRIMED AREA AND SPLSDR USAA070065Angle · crackedLEFT WING STA 135.50 AFT INBOARD TOP CHORD ANGLE HAS CRACK. INSTALLED REPAIR PLATES, DOUBLERS & FILLER PER EA 98385, DEFECT SIZE: 1 INCH.SDR USAA070067Attach Angle · crackedATTACH ANGLE AT LT WING STA 114 INBOARD SIDE UPPER AFT END IN FUEL TANK HAS CRACK. REMOVED DAMAGE, FABRICATED ANGLE DOUBLERS & INSTALLED PER EA 98389, DEFECT SIZE: 0.1 INCH.SDR K11A2008112672205Attach Angle · crackedFWD SPAR VERTICAL ATTACH ANGLE HAS EVIDENCE OF A CRACK.SDR K11A2008112672204Attach Angle · crackedFWD SPAR VERTICAL ATTACH ANGLE HAS EVIDENCE OF A CRACK.SDR K11A2008112672203Attach Angle · crackedFORWARD SPAR VERTICAL ATTACH ANGLE HAS EVIDENCE OF A CRACK.SDR CALA0700038Stiffener · crackedINSPECTION FOUND A CRACK IN THE WING CENTER SECTION REAR SPAR VERTICAL STIFFENER AT RBL 6.15. THE STIFFENER WAS REPAIRED IAW ECRA 5714-01019.SDR A6WA200740048Intercostal · crackedFOUND LEFT SIDE FS 621 TO FS 625.30 INTERCOSTAL AT STRINGER 14L IS CRACKED NEAR RADIUS APPROX 1.1 INCH LONG. (M)SDR IXXA07SMN042SVane · elongatedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING OUTBOARD SLOT VANE HOLES ELONGATED AT STATION XS520.168. REMOVED EXISTING INTERNAL DOUBLER. REMOVED OUT DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND AFTER DAMAGE REMOVED. FABRICATSDR 2007UALA00135Structure · misdrilledFWD INBOARD HOLE OF UPPER WING WAS MISDRILLED. MAJOR REPAIR: INSTALLED FREEZE PLUG REPAIR TO DAMAGED HOLE.SDR TRAX200700105Angle · crackedRT WING MIDDLE LEADING EDGE, I/B ATTACH ANGLE CRACK.SDR TRAX200700062Web · corrodedCORROSION FOUND ON THE LOWER WEB OF LE 612. REFER TO EXELTECH WORK PACKAGE YUL000164 NRTC 600-28 FOR ALL WORK ACCOMPLISHED. CORROSION REMOVED AS PER SRM 51-21-42 ON THE LOWER WEB OF L/E 612 AND FOUND WITHIN LIMIT AS PER SRM 51 10 10 REPAIR DETERMINED NOT TOSDR UPS07848840Stiffener · crackedINSPECTION TYPE:C2 RADIOGRAPHIC INSP DETECTED A CRACK ON THE LT WING AT STA XRS437.00 VERTICAL STIFFENER IN THE LEADING EDGE. REMOVED REPAIR FROM VERTICAL STIFFENER IAW SRM 51-1-21. FABRICATED AND INSTALLED REPAIR DOUBLER, AND REPAIR ANGLE AT LT WING STA XRSSDR UPS07849052Intercostal · crackedINSPECTION TYPE:C3 - FOUND IB UPPER RIB OF OB SLOT DOOR STRUCTURE HAS 4" CRACK,CENTER LEADING EDGE LW ABOVE PNEUMATIC DUCT. REMOVED, STOP DRILLED CRACK, FABRICATED AND INSTALLED 1 INTERCOSTAL, AND 1 REPAIR ANGLE IAW SRM 51-1-20D, 57-03-01-0, 51-03-02.
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