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.

SDR 06FDEA1197Doubler · crackedLT WING AT STA XOS 632 LEADING EDGE CAVITY BEADED DOUBLER FOUND CRACKED. CRACK ON LEFT WING STA XOS 632 LEADING EDGE CAVITY BEADED DOUBLER REPAIRED AS PER FEDEX EA NR1-5730-95801, TITLE: WINGS, LEADING EDGE BEADED DOUBLER PERMANENT REPAIR. THIS REPAIR IS Mar 22, 2006 · N588FE · Doug MD11SDR UPS06146513Support · crackedSTIFFENER O/B OF STA 1132/RIB NR 16 FOUND TO BE CRACKED APPROX 1" LOWER FWD CORNER RADIUS (RT WING). REMOVED AND REPLACED STIFFENER PER A300 SRM 51-40-00.Mar 15, 2006 · N131UP · Airbus A300F4622RSDR UPS06146512Stiffener · crackedO/B OF RIB NR 9, RT WING, STIFFENER HAS A CRACK FROM LOWER RADIUS TO FWD RADIUS OF ATTACHING POINT, LOWER WING AREA I/B OF TRACK NR 3. REMOVED AND REPLACED RIB O/B OF RIB NR 9 RT PER A300 SRM 51-40-00 AND 51-40-21.Mar 15, 2006 · N131UP · Airbus A300F4622RSDR UPS06146509Support · crackedFOUND LT WING AFT OF REAR SPAR INBD SIDE OF RIB 16, WEB CRACKED. REMOVED AND REPLACED SKIN SUPPORT PER A300 SRM 51-20-00 AND 51-24-00.Mar 15, 2006 · N131UP · Airbus A300F4622RSDR UPS06146508Web · crackedFOUND LT WING BETWEEN RIB 9 AND RIB 10 AFT SECTION OF WEB CRACKED (AFT OF REAR SPAR). REMOVED AND REPLACED WEB STIFFENER PER A300 SRM 51-40-00.Mar 15, 2006 · N131UP · Airbus A300F4622RSDR UPS06146507Stiffener · crackedSTIFFENER AT STA 1132/ RIB 16 (ON THE RT WING) FOUND TO BE CRACKED APPROX 1" FROM FWD LOWER RADIUS AREA. REMOVED AND REPLACED STIFFENER PER A300 SRM 51-40-00 AND 51-24-00.Mar 15, 2006 · N131UP · Airbus A300F4622RSDR UIEA200600028Tee Fitting · corrodedRT WING TRAILING EDGE - LOWER T-CHORD HAS CORROSION AT REAR SPAR CAVITY WS 725. REPLACED LOWER T-CHORD IAW SRM 51-30-02.Mar 13, 2006 · N512MC · Boeing 747230BSDR DHL2006750505Stiffener · crackedFOUND LEFT WING REAR SPAR VERTICAL STIFFENER AT WS 546 INB OF NR 2 SPOILER FITTING SUPPORT IS CRACKED FROM BOTTOM END. REMOVED AND REPLACED L WING REAR SPAR VERT STIFFENER AT WS 546 I/B OF NR 2 SPOILER FITTING SUPPORT IAW B727 SRM 51-30-2, LEAK CHECK GOOD IAWMar 12, 2006 · N750DH · Boeing 7272M7SDR 2006UALA00470Stiffener · gougedLT WING STIFFENER GOUGED BEYOND LIMITS AT WS 825 REAR SPAR. THE LEFT WING STIFFENER, P/N 112T1237-1, WAS FOUND GOUGED BEYOND LIMITS AT WS 825 REAR SPAR. NO DAMAGE WAS REPORTED ON THE ADJACENT STRUCTURES. THEREFORE, THE GOUGED WAS LIKELY CAUSED BY FOD. REPLMar 12, 2006 · N641UA · Boeing 767322SDR CA060316004Fitting · gougedDURING WING REMOVAL FOR PAINT, LT LOWER WING STRUT FITTING WAS FOUND TO HAVE A GOUGE OF APPROXIMATELY 1/8" FROM STRUT FAIRING SCREW.Mar 6, 2006 · Cessna T207ASDR DHL2006760512Web · crackedLEFT WING AT WBL 603.5 THRU ACCESS PANEL 8112 THE WEB IS CRACKED. CUT OUT DAMAGE 1 X 2 INCH IAW B727SRM 51-40-2 FIG 1. HFEC CUT OUT NO CRACKS NOTED IAW NDT MAN PART 6 51-00 FIG 23. REMOVED WEB IAW B727 SRM 51-30-2. FABBED DOUBLER FROM 2024 T3 .040 PO 90030Mar 4, 2006 · N760AT · Boeing 7272B7SDR ABXA060166Support Bracket · corrodedRIGHT WING ROOT TOP FAIRING SUPPORT BRACKET WAS WORN AND WITH CORROSION AT REAR SPAR, TOP SURFACE. REPLACED FAIRING SUPPORT BRACKET IAW DC8 SRM 51-1-2 AT RIGHT WING ROOT TOP FAIRING.Mar 2, 2006 · N828AX · Doug DC863FSDR UPS06146426Intercostal · crackedFOUND LT WING T/E TOP BETWEEN 4 AND 5 SPOILERS OTBD 1 EA INTERCOSTAL CRACKED IN RADIUS. REMOVED AND REPLACED INTERCOSTAL PER SRM 51-40-00 & 51-41-00.Mar 2, 2006 · N130UP · Airbus A300F4622RSDR 06FDEA0923Doubler · out of limitsREPAIR LT WING IB FLAP IB LWR FAIRING FWD END MARKED NR 51. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. N00719, EVALAUATED REPAIR IAW FAA DATA FOUND REPAIR WAS NOT IN COMPLIANCE. FAMar 2, 2006 · N68057 · Doug MD1010FSDR 06FDEA0921Doubler · incorrectR/W IB FLAP IB LOWER FAIRING FWD EDGE SIDE AFT OF FWD END MARKED NR 49. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCCOMPLISHED USING FAA APPROVED DATA. N00717, EVALUATED DOUBLER FAA APPROVED DATA, FOUND DOUBLER WAS NOT IMar 2, 2006 · N68057 · Doug MD1010FSDR QXEA200600699Structure · corrodedYYC C4, RIGHT HAND WING FUEL BAY REBATE AT 624CT, INBOARD END HAS AREA OF CORROSION. REPAIRED IAW RD 8-57-984, PAGE 3, NOTE 8.Mar 1, 2006 · N350PH · Dhav DHC8202SDR UPS06146399Angle · crackedINSPECTION TYPE:5 YR LT WING KRUEGER BOX AREA CURVED DOUBLER ON 2ND RIB FROM FUSELAGE HAS A CRACK. REMOVED & REPLACED DOUBLER PER SRM 51-40-00.Feb 22, 2006 · N130UP · Airbus A300F4622RSDR 06FDEA0797Support Angle · crackedRIGHT WING OUTBOARD FLAP OUTBOARD HINGE FAIRING 636BR SUPPORT ANGLE FOUND CRACKED. RT WING OUTBOARD FLAP OUTBOARD HINGE FAIRING 636BR SUPPORT ANGLE REMOVED AND REPLACED AS PER SRM 51-35-01 VOLUME II. NEW ANGLE FABRICATED AS PER DRAWING ARC0752 AND FEDEX EA 1Feb 21, 2006 · N615FE · Doug MD11SDR 2006FA0000208Cover · chafedCOVER IS CHAFING LWR FWD LT AND RT WING ATTACH POINT SPAR CAP AND WING SKIN. THE COVER HAS NO ANTI-CHAFE PROTECTION. RECOMMEND RUBBER EDGE SEAL OR FAY SEAL EDGE TO AVOID METAL TO METAL CONTACT WITH SPAR WING SKIN. (K)Feb 21, 2006 · N103CW · Beech 300BEECHSDR 2006FA0000206Cover · chafedCOVER IS CHAFING LOWER FWD LT AND RT WING ATTACH POINT, SPAR CAP AND WING SKIN. THE COVER HAS NO ANTI-CHAFE PROTECTION. RECOMMEND RUBBER EDGE SEAL OR FAY SEAL EDGE TO AVOID METAL TO METAL CONTACT WITH SPAR AND WING SKIN. (K)Feb 21, 2006 · N79TE · Beech 300BEECHSDR 06FDEA0770Structure · crackedLEFT HAND WING LEADING EDGE ANTI-ICE TELESCOPIC DUCT CUTOUT AT XORS372 FOUND CRACKED, AS MARKED. REPAIRED AS PER FEDEX EA 1-5730-90764. THIS REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.Feb 20, 2006 · N602FE · Doug MD11SDR DHL2006760518Support Angle · crackedLEFT WING, NR 4 SPOILER ACTUATOR INBOARD SUPPORT ANGLE AT WS 460 APPROX HAS CRACK. INSPECTED NR 4 SPOILER I/B SUPPORT ANGLE USING HFEC AS GIVEN IN B727 NDTM, PART 6 SUB, 51-00-00 FIG 23, CRACK IS CONFIRMED. REMOVED EXISTING ANGLE IAW B727 SRM 51-30-2, PROCURFeb 18, 2006 · N760AT · Boeing 7272B7SDR 06FDEA0708Bracket · crackedLEFT HAND WING, LEADING EDGE RIB BRACKET LOWER AREA, STA XORS 538, OUTBOARD SIDE OF REFUEL ACCESS 519CB CUTOUT AREA FOUND CRACKED ARB1187-15. REMOVED AND REPLACED AS PER SRM 51-31- 01 VOLUME II. NEW FORMER FABRICATED AS PER DWG ARB2917. REPAIR CLASSIFIEDFeb 17, 2006 · N585FE · Doug MD11SDR DHL2006804548Doubler · crackedRT WING NR3 MAIN TANK 506C ACCESS DOOR INTERNAL DOUBLER FLANGE CRACKED 0.250 INCH STA 12.000 S-13 S-14 (MAJOR REPAIR). REMOVED FASTENERS IAW SRM 51-1-20D. CUT OUT DAMAGED SECTION IAW DWG AA66-57-R08. PERFORMED NDT INSP USING DYE PENETRANT METHOD IAW NDT SPM PAFeb 16, 2006 · N804DH · Doug DC873FSDR DHL2006804544Fitting · crackedNR 1 ALT TANK 505B ACCESS DOOR FITTING CRACKED 1" XRS 428.000 - XRS 463.000 S-38. PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 57-1-0 PG 1, SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTINGFeb 15, 2006 · N804DH · Doug DC873FSDR A6WA200640078Structure · corrodedRT WING FUEL PANEL 640BB ACCESS HOLE HAS CORROSION ON LIP, NON-CRITICAL AREA .002 INCH DEEP. MAINTENANCE BLENDED DAMAGED AREA AS REQUIRED IAW REO. (K)Feb 9, 2006 · N435AW · Cndair CL6002B19SDR A6WA200640077Structure · corrodedRT WING FUEL PANEL 640BB ACCESS HOLE HAS CORROSION, NON-CRITICAL AREA .002D X 2.0 INCH L. MAINTENANCE BLENDED AREA IAW REO. (K)Feb 9, 2006 · N435AW · Cndair CL6002B19SDR A6WA200640076Structure · corrodedLT WING FUEL PANEL 510AB, ACCESS HOLE HAS MINOR CORROSION ON LIP, NON-CRITICAL AREA .003D X 2.5L. MAINTENANCE BLENDED MINOR CORROSION IAW REO. (K)Feb 9, 2006 · N435AW · Cndair CL6002B19SDR A6WA200640075Angle · corrodedLT WING FUEL ANGLE 540BB HAS MINOR CORROSION ON LIP, NON CRITICAL AREA .002D X 2.0L. MAINTENANCE BLENDED MINOR CORROSION IWA REO. (K)Feb 9, 2006 · N435AW · Cndair CL6002B19SDR A6WA200640081Panel · corrodedRT WING FUEL PANEL 6500B ACCESS HOLE CORROSION, NON-CRITICAL AREA .002D X 2.75 INCHES L. MAINTENANCE BLENDED OUT CORROSION IAW REO. (K)Feb 9, 2006 · N435AW · Cndair CL6002B19SDR A6WA200640080Structure · corrodedRT WING FUEL 650VV ACCESS HOLE LIP HAS MINOR CORROSION, NON-CRITICAL AREA .002 D X 1.5 INCHES L. MAINTENANCE BLENDED MINOR CORROSION IAW REO. (K)Feb 9, 2006 · N435AW · Cndair CL6002B19SDR A6WA200640079Panel · corrodedRT WING FUEL PANEL 640 CB ACCESS HOLE LIP HAS CORROSION NON-CRITICAL AREA .002D X 1.0 INCH L. MAINTENANCE BLENDED OUT DAMAGED AREA AS REQUIRED IAW REO. (K)Feb 9, 2006 · N435AW · Cndair CL6002B19SDR 06FDEA0627Channel · brokenLT WING L/E AT PYLON INTERSECTION ZONE 517 STA XDLE 315 FOUND CHANNEL BROKEN 1"1/2 LONG AND NUTPLATE MISSING ON THE AFT SECTION REF SRM 57-21-01 PAGE 18 ITEM 2. REMOVED SKIN IAW SRM 51-31-01 PAG 36/41 VOL 2 AND INTERCOSTAL IAW SRM 51-35-01 PAGE 1/13 VOL 2. TFeb 9, 2006 · N68056 · Doug DC1010SDR CA060221002Channel · wrong partFOUND CHANNEL ASSEMBLY WAS MADE FROM APPROXIMATELY .125 STEEL. CHECKED WITH VIKING AND WAS INFORMED THAT CHANNEL IS .080 ALUMINUM. AIRCRAFT WAS RECENTLY IMPORTED FROM VENEZULA.Feb 8, 2006 · Dhav DHC2MKISDR DHL2006804530Angle · crackedRIGHT STUB WING ANGLE CRACKED 1 INCH XOLD 67.000. REMOVED CRACKED ANGLE IAW SRM 51-1-21. FABRICATED NEW ANGLE (AL7075"0" 0.080") IAW SRM 57-3-3 FIG 3. HEAT TREATED NEW ANGLE FROM 7075"0" TO 7075T6 IAW SRM 51-1-1 PG 1-13-17. CLEANED, TREATED AND PRIMED AREAFeb 6, 2006 · N804DH · Doug DC873FSDR QXEA200600437Plate · damagedPDX - LT WING FUEL PANEL LADDER PLATE AFT FLANGE HAS 2 TOOLING MARKS ABOVE RIB YW117.5. MAINTENANCE REPAIRED IAW NDTM PART 6, 51-00-02, RD 8/4-57-623 AND HORIZON EA 6-57-433.Feb 2, 2006 · N404QX · Bombdr DHC8402SDR USAA060155Angle · corrodedFOUND CORROSION RT FIXED WING T/E WHERE HYDRO LINES ATTACH. REMOVED SURFACE CORROSION, TREATED AND PAINTED IAW SRM 51-10-02, DEFECT SIZE: 3" BY 1".Jan 27, 2006 · N775AU · Boeing 7374B7SDR DHL2006804503Doubler · crackedRIGHT WING L/E UPPER PART ANGLE DOUBLER CRACKED XS 454.976. REMOVED CRACKED ANGLE DOUBLER IAW DC8 SRM 51-1-21. FABRICATED NEW ANGLE DOUBLER (AL 2024T3 0.063) IAW SRM 57-2-0 PG 1. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW ANGLE DOUBLER IAW Jan 16, 2006 · N804DH · Doug DC873FSDR A6WA200640049Structure · corrodedRT WING PLANK HOLE NR 14 HAS CORROSION AT IB SIDE 8 INCH L X .002 INCH-.003 INCH DEEP AND AT OB SIDE 5 INCH L X .001 INCH-.002 INCH D. NOT IN CRITICAL AREA. MAINTENANCE REPAIRED RT WING PLANK ACCESS HOLE AT WS 274.319 HOLE NR 14 IAW REO. (K)Jan 13, 2006 · N428AW · Cndair CL6002B19SDR 06FDEA00049Structure · crackedCRACK FOUND DURING HFEC INSPECTION AT LEFT WING TANK AT THE END OF STRINGER 14 (UPPER STRINGER) ARB7514-1.Jan 5, 2006 · N613FE · Doug MD11SDR QXEA200600040Angle · crackedPDX - Z ANGLE CRACKED AT RIGHT WING FRONT SPAR STATION UW560. REPLACED IAW HORIZON AIR EA 2-57-105.Dec 31, 2005 · N379PH · Dhav DHC8202SDR CALA0500463Stiffener · crackedA 2 INCH CRACK WAS FOUND TO THE WING CENTER SECTION REAR SPAR AT STA 540, RBL 6.15 VERTICAL STIFFENER DURING A WALKAROUND INSPECTION. AN INTERIM REPAIR WAS INSTALLED PER EA 5714-01002, REV C, OP 8 AND ECRA 5714-01011. A DIP WAS ISSUED TO REINSPECT THE STIFFEDec 22, 2005 · N14358 · Boeing 7373T0SDR AU510002147Support · corrodedLT WING REAR SUPPORT CORRODED. FOUND DURING INSPECTION IAW AD/PA32/27 AMDT2.Dec 12, 2005 · Piper PA32300SDR 05FDEA04149Latch · corrodedSNRM N0539: RT WING LEADING EDGE ACCESS PANEL 617CB INTERIOR FRONT, SPAR LOWER CAP, UPPER SURFACE FOUND CORROSION AT LATCH CONTACT AREA.** S/D COMING**Dec 5, 2005 · N578FE · Doug MD11SDR DHL2005803540Fitting · crackedITEM REF NR 039051: NR 4 ALT TANK S-64 END CRACKED 1 INCH STA XRS 445.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-2 FIG. 3D TR# 57-86. REMOVED FASTENERS IAW SRM 51-1-20D. FABRICATED REPAIR ANGLE (EXTRUSION AND 101342003 0.090") IAW SRM 57-2-2 FIG. Nov 28, 2005 · N803DH · Doug DC873SDR ERA2005F00006Plate · crackedFOUND WHILE AIRCRAFT UNDERGOING C1-CHECK IN THE RT LADDER PLATE AT (RT) YW137, FORWARD OF STRIGER 6. REPAIRED IAW RD. (K)Nov 19, 2005 · N882EA · Dhav DHC8103SDR DHL2005803506Angle · crackedITEM REF NR 033540: RT WING CTR L/E INTERCOSTAL JOINT ANGLE TO FORMER CRACKED XS 454.976. REMOVED CRACKED ANGLE IAW SRM 51-3-0. FABRICATED NEW ANGLE (AL7075T6 0.063") IAW SRM 57-2-0 PG. 1. CLEANED, TREATED AND PRIMED AREA AND ANGLE IAW SRM 51-1-8B. INSTALLED NNov 18, 2005 · N803DH · Doug DC873SDR SWAA053574Floor Support · crackedDURING SCHEDULED 1/4D CHECK, FOUND CENTER CABIN LONGITUDINAL FLOORBEAM CRACKED BETWEEN BS 663 TO BS 665.5, BL 0. REPAIRED FLOORBEAM PER SWA EA.Nov 13, 2005 · N336SW · Boeing 7373H4SDR 2005UALA01239Angle · crackedLEFT WING, LEFT PYLON, AFT BULKHEAD, LOWER OUTBOARD ANGLE CRACKED. *S/D* THE LEFT WING LEFT PYLON, AFT BULKHEAD LOWER OUTBOARD ANGLE WAS FOUND CRACKED ON A/C 6768 DURING A C-CHECK VISIT. CRACK IS DUE TO FATIGUE. CRACKED ANGLE WAS REPLACED AND INSTALLED PERNov 7, 2005 · N668UA · Boeing 767322SDR ASAA0540617Stiffener · damagedOKC - FOUND DURING ACCOMPLISHMENT OF EO 5710-01108, 1 FASTENER HOLE COMMON TO LBL 6.15 STIFFENER WAS OVERSIZED BEYOND ALLOWABLE DIAMETER TO REMOVED DAMAGE. REAMED HOLE TO .388/.391 DIAMETER, INSTALLED FASTENER IAW ASA EA 5710-01123. (M)Nov 2, 2005 · N794AS · Boeing 737490
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