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"

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SDR HNAA0700128Doubler · corrodedLEFT AUX BOOST PUMP (FUEL) WING DOUBLER FOUND CORRODED INSIDE AND OUTSIDE FUEL TANK. LEFT AUX BOOST PUMP (FUEL) WING DOUBLER INSIDE AND OUTSIDE OF FUEL TANK CORROSION REMOVED IAW RD8-57-3679 (MATERIAL REMAINING .415") S/B 8-57-28 PREVIOUSLY COMPLIED WITH. HFJun 28, 2007 · N912HA · Dhav DHC8102SDR FDKA200706314Strip · corrodedANTI STATIC STRIPS ON PANELS 5731 AND 5732 ARE CORRODED OUT OF LIMITS. REMOVED AND REPLACED DAMAGED STRIPS.Jun 27, 2007 · N826MJ · Emb EMB145LRSDR FDKA200706313Strip · corrodedANTI STATIC STRIPS ON PANELS 6731 AND 6732 ARE CORRODED OUT OF LIMITS. REMOVED AND REPLACED DAMAGED STRIPS.Jun 27, 2007 · N826MJ · Emb EMB145LRSDR 07FDEA02293Panel · crackedLT WING OB TE FLAP WELL LWR FIXED PANEL CORRUGATED SUPPORT PLATE IS CRACKED RSS 516-523. REPLACED CORRUGATED SPLICE IAW SRM 51-30-02.Jun 27, 2007 · N286FE · Boeing 727233SDR UPS07850080Channel · crackedINSPECTION TYPE:C3 R/WING CENTER L/E OUTBD T CHANNEL IS CRACKED. STOP DRILLED CRACKED T CHANNEL AT R/WING STA X 501 IAW SRM 57-02-00 FIG 2. FABRICATED AND INSTALLED REPAIR ANGLE ON T CHANNEL IAW SRM 57-02-00 FIG 002.Jun 22, 2007 · N705UP · Doug DC871FSDR 07FDEA02230Stiffener · crackedLT WING FIXED LEADING EDGE CAVITY AT XOS = 665, STIFFENER FOUND WITH CRACK. [07-09-07] COMPLIED WITH FEDEX E.A. 1-5710-111130. CLASSIFIED AS MINOR REPAIR AS PER FEDEX GMM 6-2-100.Jun 20, 2007 · N575FE · Doug MD11FSDR 07FDEA02220Stiffener · crackedLEFT WING FIXED LEADING EDGE CAVITY, AT XOS = 570, STIFFENER FOUND CRACKED. [07-06-07] REPAIRED AS PER FEDEX EA 1-5710-111129, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Jun 20, 2007 · N575FE · Doug MD11FSDR ASMF200706004Vortex Gen · damagedDURING TRANSIT CHECK, THE AIRCRAFT WAS HIT BY A GROUND HANDLING TRUCK IN THE LOWER SECTION OF RIGHT WING, DAMAGING IN THE VORTILON AND IN THE FORWARD INBOARD FLAP HINGE FAIRING. MAINTENANCE PERSONNEL REPLACED VORTILION IAW MM 57-20-04 AND THE FORWARD INBOARD FJun 17, 2007 · N169PL · Doug MD88SDR UPS07850159Fitting · crackedINSPECTION TYPE:C3 STRINGER END FITTING TO FRONT SPAR CRACKED BETWEEN XRS 463 TO XRS 450 NR 1 ALT TANK REMOVED STRINGER END FITTING FROM FWD SPAR BETWEEN XRS 463 TO XRS 450 IAW SRM 51-01-20D, FABRICATED AND INSTALLED STRINGER END FITTING AT WING STA XRS 46Jun 14, 2007 · N810UP · Doug DC873FSDR UPS07850064Angle · crackedINSPECTION TYPE:C3 R/WING CENTER LEADING EDGE SLOT INBD SIDE "L" ANGLE CRACKED. STOP DRILLED CRACK ON "L" ANGLE AT R/WING CENTER L/E SLOT DOOR IAW SRM 51-03-02. FABRICATED AND INSTALLED REPAIR ANGLE DOUBLER IAW SRM 57-02-00 FIG 002.Jun 13, 2007 · N810UP · Doug DC873FSDR DHL2007740527Angle · crackedWHILE AT C CHECK, LWR END OF VERTICLE SUPPORT ANGLE CRACKED ON L/W FIXED IN STA 110. CUT-OUT DAMAGED AREA APPROX DIM 2.3" BY 1" IAW B272 SRM 51-10-1 FIG 1 AND 51-40-3 FIG 1. FAB ANGLE REPAIR APPROX DIM 9" BY 3" FROM 7075-0 .063 PO NR 9004779 IAW B727 SRM 51-Jun 10, 2007 · N740DH · Boeing 7272Q9SDR DHL2007783527Web · crackedLEFT WING TIP, VERTICAL WEB SHOWS MULTIPLE CRACKS BY FWD NAV LIGHT, WBL 640. CUT OUT DAMAGED AREA OF LEFT WING TIP, VERTICAL WEB AT NAV LIGHT AREA IAW B727 SRM 51-40-3, DIM 7.875 BY 3. FABRICATED AND INSTALLED REPAIR DOUBLER IAW B727 SRM 51-40-3, MATERIAL IDJun 5, 2007 · N783DH · Boeing 727227SDR USAA070425Flange · crackedCRACK AT WBL 135.5 AT LEFT WING, LOWER CHORD FLANGE HAS CRACK. INSTALLED DOUBLER PER EA 98655, DEFECT SIZE: 2 INCHES.Jun 5, 2007 · N420US · Boeing 737401SDR DHL2007803519Channel · crackedRT WING LWR FAIRING ZEE CHANNEL CRACKED 1" STA XW -3.125. REMOVED CRACKED ZEE CHANNEL IAW SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW CHANNEL IAW SRM 51-1-21. REFER TO JC EC-00360-00 (WO 1028) FOR ZEE FABRICATION.Jun 3, 2007 · N803DH · Doug DC873SDR DHL2007803520Channel · crackedLT WING LWR FAIRING ZEE CHANNEL CRACKED 0.750" STA XW -3.125. REMOVED ZEE CHANNEL IAW SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW CHANNEL IAW SRM 51-1-21. REFER TO JC EC-00361-001 (WO 1028) FOR ZEE FABRICATION.Jun 3, 2007 · N803DH · Doug DC873SDR UPS07M50155Web · crackedINSPECTION TYPE:C RIGHT WINGTIP LOWER WINGLET LOWER STRUCTURAL BORE FOUND CRACK. WEB CRACK END STOP HOLE DRILLED PER EN 1350-07. CRACK BOLT HOLE REAMED PER EN 1350-07. REP BUSHING FAB & INSTALLED PER EN 1350-07. FPI CARRIED OUT AS PER DPS 4.707 REV AW ON FMay 29, 2007 · N288UP · Doug MD11FSDR UPS07450026Channel · crackedINSPECTION TYPE:C LT WING NR 4 L/E PDU AFT SUPPORT CHANNEL FOUND CRACKED AT MOUNT BOLT AREA. (CRACK LENGTH .375 INCH). LT WING NR 4 L/E PDU AFT SUPPORT CHANNEL REPAIRED AS PER SRM 51-40-03 FIG 2.May 29, 2007 · N520UP · Boeing 747212BSDR TRAX200700742Intercostal · crackedRIGHT I/B SLAT CLOSING PLATE AND INTERCOSTAL CRACKED. LOCATED NEW SERVICEABLE INTERCOASTAL AND INSTALLED WITH SOLID FASTENERS TO SERVICEABLE CLOSING PLATE IAW CRJ 700 SRM 51-42-06. TRIMMED SERVICEABLE CLOSING PLATE TO FIT. OKAY TO PAINT. PRIME AND PAINTED, May 29, 2007 · N716EV · Cndair CL6002C10SDR 2007UALA01707Fitting · damagedINBOARD SIDE LOAD FITTING, INBOARD FWD HOLE DAMAGED RIGHT WING. MAJOR REPAIR ACCOMPLISHED: REAMED HOLE OVERSIZED. COLD WORKED HOLE & FINAL REAMED FOR OVERSIZED FASTENER INSTALLATION.May 28, 2007 · N514UA · Boeing 757222SDR DLM88070621Vane · dentedDENT ON MID GUIDE VANE OF RIGHT OUTBD FLAP. MID GUIDE VANE WAS REPAIRED IAW SRM 57-03D PARA 8 FIG 9A ON N/R T0056900.May 27, 2007 · N946DL · Doug MD88SDR UPS07M50229Structure · crackedINSPECTION TYPE:C RIGHT FIXED L/E STRUCTURE FOUND CRACKS ON UPPER DOOR CUTOUT AREA NR 3 SLAT TELESCOPIC DUCT VICINITY. DAMAGE AREA TRIM OFF PER ADV EN1356-07. HFEC INSP CARRIED OUT PER DAC NDTSPM R13 06-10-01.001 FOUND NO CRACK EVIDENT. REPAIR PARTS FAB, HOMay 25, 2007 · N260UP · Doug MD11FSDR TRAX200700715Angle · crackedRT WING MIDDLE LEADING EDGE, I/B ATTACH ANGLE IS CRACKED. REMOVED RT WING MIDDLE LEADING EDGE I/B CRACKED ATTACH ANGLE. INSTALLED NEW SERVICEABLE ATTACH ANGLE, P/N 600-12025-8, RT WING MIDDLE LEADING EDGE I/B, IAW SRM 51-40-11. W/C 1102.May 23, 2007 · N976EV · Cndair CL6002B19SDR 07FDEA01930Deflector · crackedPNL RACK RT WING TO BODY RT WING TO BODY PLN UPPER SURFACE HAS A CRACKED BRACKET. PAINTED AND INSTALLED NEW PARTS, REF SRM 51-30-023 PG 1.May 22, 2007 · N210FE · Boeing 7272S2FSDR 07FDEA01929Support Angle · crackedLT WING T/E ANGLE SUPPORT FOR JACKSCREW MOST OUTBD FAIRING IS CRACKED FROM FASTENER HOLE (INBD ANGLE). REPLACED WITH NEW DOUBLER REF 51-30-5 AND SRM 51-30-2.May 22, 2007 · N210FE · Boeing 7272S2FSDR TRAX200700702Bracket · crackedLEFT WING I/B LEADING EDGE O/B BRACKET CRACKED.May 21, 2007 · N836AS · Cndair CL6002B19SDR 07FDEA01852Support Angle · crackedRT WING OB TE LWR SURFACE PANEL SUPPORT ANGLE CRACKED, 4" FWD OF TE, BELOW OB HINGE OF NR 12 SPOILER REPLACED PANEL SUPPORT ANGLE REF SRM 51-30-02 PAGE 19.May 19, 2007 · N210FE · Boeing 7272S2FSDR QXEA200700854Support · wornC4 OKC - LEFT WING, OUTBOARD FLAP, VANE SUPPORTS ARE WORN TO THE POINT OF RAISED METAL. REPAIRED IAW SRM57-53-02, 51-12-00.May 10, 2007 · N606QX · Cndair CL6002C10SDR C1HA200795001Angle · crackedRIGHT WING L/E STA 130.7 INTERNAL ANGLE AT FRONT SPAR LWR CRACKED. FABRICATED AND INSTALLED REPAIR PART IAW B727 M/M 57-20-21 PG 801 AND SEALED AS REQUIRED IAW B727 M/M 51-30-11.May 4, 2007 · N295AS · Boeing 727290SDR C1HA200795005Plenum · corrodedA/C RAM AIR PLENUM HAS SURFACE CORROSION ON NR 2 TANK LWR SKIN ABOVE LT PRIMARY HEAT EXCHANGER. BLENDED OUT CORROSION DAMAGE, MAT LOSS .050, ORIGINAL THK .225. FLUORESCENT DYE PENETRANT AREA, NO DEFECTS NOTED. TREATED AND PRIMED AREA IAW B727 SRM 51-10-2. May 4, 2007 · N295AS · Boeing 727290SDR K11A2008112672207Attach Angle · crackedFWD SPAR VERTICAL ATTACH ANGLE HAS EVIDENCE OF A CRACKMay 2, 2007 · N722CK · Boeing 7272H3SDR 07FDEA01684Bracket · crackedRT WING'S LOWER TRAILING EDGE PANELS OUTBD STRUT MOUNT BRACKET IS CRACKED BY NR 7 TRANSMISSION REMOVED AND REPLACED RT WING LOWER EDGE PANEL MOUNT BRACKET SRM 51-30-2 PG 1.May 2, 2007 · N210FE · Boeing 7272S2FSDR USAA070335Stiffener · crackedLBL 6 AT STA 663.75 AT CENTER WING SPAR, FWD WALL OF MLG WHEELWELL ABOVE A. INSTALLED DOUBLER PER TR 57-10-03 REV B. DEFECT SIZE: 1"May 1, 2007 · N503UW · Boeing 737301SDR 07FDEA01668Stiffener · crackedLEFT WING LEADING EDGE CAVITY STIFFENER FOUND WITH APPROX 0.25 INCH CRACK AT XOS 667. [SUP 05-15-07] REPAIRED AS PER FEDEX EA 1-5720-109874, WINGS - LEADING EDGE STRINGER - CRACK REPAIR. REPAIR CLASSIFIED AS MINOR PER GMMM 6-2-100.Apr 30, 2007 · N574FE · Doug MD11FSDR 07FDEA01659Angle · crackedRIGHT WING, LEADING EDGE CAVITY AT ABOUT XOS 659 STRIP ANGLE FOUND WITH APPROX 0.5 INCH CRACKED. [SUP 05-14-2007] FIXED LEADING EDGE STRINGER, CRACK REPAIR. CLASSIFIED AS MINOR REPAIR AS PER FEDEX GMM 6-2-100.Apr 28, 2007 · N574FE · Doug MD11SDR 07FDEA01658Angle · crackedRIGHT WING, LEADING EDGE CAVITY AT ABOUT XOS 774 STRIP ANGLE FOUND WITH APPROX 0.3124 INCH CRACKED. [SUP 05-14-07] RT FIXED LEADING EDGE STRINGER, CRACK REPAIR. REPAIR CLASSIFIED AS MINOR PER FEDEX GMM 6-2-100.Apr 28, 2007 · N574FE · Doug MD11SDR UPS07M50139Doubler · crackedINSPECTION TYPE:C LEFT LEADING EDGE LWR COMPT 519CB (PRESSURE REFUEL) FOUND STIFFENER DOUBLER SUSPECTED CRACK AS MARKED. HFEC INSP CUTOUT FOUND CRACK APPROX .25 INCH. LEFT WING LEADING EDGE LWR COMPT 519CB (PRESS REFUEL) RIBS REMOVED. CRACK AREA TRIMMED OUTApr 24, 2007 · N288UP · Doug MD11FSDR UPS07M50117Stiffener · crackedINSPECTION TYPE:C LT LE LWR COMPT ACCESS NR 519DB FOUND STIFFENER DOUBLER SUSPECTED CRACK AS MARKED, JUST O/B OF REFUEL PNL NR 519CB. HFEC INSP C/OUT FOUND CRACK APPROX 1/4". LT LE LWR COMPT ACCESS NR 51 9DB CLAMPS REMOVED. DAMAGED AREA AT LT LE LWR COMPT NApr 24, 2007 · N288UP · Doug MD11SDR TRAX200700590Structure · crackedRANRC 356. POSSIBLE CRACK FOUND AT AFT FASTENER HOLE FOR LT DRAIN NEXT TO BOOST PUMP IN CANISTER. [07-23-07] REPAIRED IAW ALL SRM AND EO`S.Apr 24, 2007 · N974EV · Cndair CL6002B19SDR IXXA07SMN155SFitting · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING INBOARD SLOT VANE FITTING WITH CORROSION AT STATION XILD 0.7095. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED FITTING. FABRICATED NEW FITTING. CLEANED, TREATED AND PRIMED AREA AND FITTING. APApr 21, 2007 · N828BX · Doug DC871FSDR DHL2007806591Angle · crackedRT INBD FLAP LWR "T" ANGLE CRACKED 1 1/2" STA XW 91.000. REMOVED CRACKED "T" ANGLE IAW SRM 51-1-21. FABRICATED NEW "T' ANGLE (EXTRUSION S2701008) IAW SRM 57-7-1 PG 4. CLEANED, TREATED AND PRIMED AREA AND "T" ANGLE IAW SRM 51-1-8B. INSTALLED "T" ANGLE IAW SApr 20, 2007 · N806DH · Doug DC873FSDR 2007UALA01155Vent · damagedLT WING HAS INTERNAL DAMAGE AT VENT SCOOP AREA (WING TIP). [SUP 05-16-07] REMOVED DAMAGED PARTS AND REPLACED IAW FRR UAL-744-0263. A/C OK FOR SERVICE. SUSPECT VENT DAMAGED BY GROUND SERVICE EQUIPMENT.Apr 16, 2007 · N173UA · Boeing 747422SDR EIA2007088Support Beam · corrodedRT WING INBOARD LEADING EDGE SUPPORT BEAM FOUND WITH EXFOLIATION CORROSION. REMOVED SUPPORT BEAM HFEC INSPECTION CARRIED OUT ON CUT OUT AREA. NIL CRACKS NOTED. REPAIR CARRIED OUT PER N482EV-07-0004/SRM 51-40-04.Apr 13, 2007 · N482EV · Boeing 747212BSDR UPS07849684Channel · crackedINSPECTION TYPE:C1 T-CHANNEL CRACKED UPPER SURFACE AT XRS 204 BETWEEN STRINGERS 60 AND 59. STOPPED DRILLED CRACK AT XRS 204 BETWEEN STRINGERS 59 & 60 IN NR 4 MAIN TANK IAW SRM 57-02-00 FIG 2. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-02-00-0, AND SRApr 12, 2007 · N819UP · Doug DC873FSDR 07FDEA01454Fairing · crackedCRACK FOUND AT INNER SKIN OF NR 4 LT FLAP MOVABLE FAIRING. REPAIR PERFORMED BY BONDING IAW SRM 57-20-35 AND EA 6-5720-99236 AND RAS/FOK/126/2006 ISSUE (A).Apr 12, 2007 · N810FD · Airbus A310SDR DHL2007806540Angle · crackedNR 1 STUB WING FORMER ANGLE CRACKED STA XS 527.000. REMOVED CRACKED ANGLE IAW SRM 51-1-21. FABRICATED NEW ANGLE (7075"0" 0.080") IAW DOUGLAS DWG NR 9753297. HEAT TREATED ANGLE FROM 7075"0" TO 7075T6 IAW SRM 51-1-1 PG 1-13-17. CLEANED, TREATED AND PRIMED ARApr 10, 2007 · N806DH · Doug DC873FSDR 07FDEA01388Stiffener · corrodedCORROSION ON RT WING HINGE ARM FITTING AND TOP SKIN PANEL. REPAIR PERFORMED BY BLEND OUT IAW EA 6-5722-103262 AND RAS/BAE/1003079/2006 ISSUE "A" (ALTERNATE MATERIAL DAN 26H30 IN PLACE OF 7150-T651 FOR STIFFENER A572-42583-203) AND RAS/BAE/1003026/2006 ISSUEApr 10, 2007 · N814FD · Airbus A310324SDR K11A2008112672208Stiffener · corrodedVERTICAL STIFFNER HAS AREA OF CORROSION.Apr 9, 2007 · N722CK · Boeing 7272H3SDR DU4R2007098Plate · corrodedFOUND RT WING TANK PLATE 641JB CORRODED. REPAIRED BY REMOVING AND REPLACING WITH P/N 10-60031-83 IAW DELTA JOB CARD OPN 3612.Apr 8, 2007 · N604DL · Boeing 757232SDR QXEA200700603Angle · crackedC5 PDX - LEFT WING FORWARD SPAR Z-ANGLE AT YW 58.2 IS CRACKED. REPAIRED IAW SRM 51-40-11.Apr 5, 2007 · N346PH · Dhav DHC8202SDR FDKA200704166Doubler · corrodedDOUBLER ON PANEL 6732 IS CORRODED. REMOVED AND REPLACED DOUBLER.Apr 4, 2007 · N848MJ · Emb EMB145LR
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