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 UPS00434339Strap · corrodedINSPECTION TYPE:C, RT WING BULGING ON UPPER L/E RABBET STRAP AT WS 1415. CORROSION REMOVED, AREA EVALUATED AND FOUND WITHIN LIMITS PER SRM 51-10-01.Nov 3, 2000 · N675UP · Boeing 747123SDR UPS00434281Strap · corrodedINSPECTION TYPE:C LH WING. BULGE ON UPPER L/E RABBET STRAP AT WS 1374 LIGHT CORROSION REMOVED IAW SRM 51-10-01. EVALUATED AND FOUND WITHIN LIMITS. IAW 57-30-01. AREA FLAP PEENED IAW BAC 5730. AREA REPROTECT ED IAW SRM 51-10-02. RIVETS INSTALLED IAW SRM 51Nov 2, 2000 · N675UP · Boeing 747123SDR UPS00434279Strap · corrodedINSPECTION TYPE:C LH WING . BULGE ON UPPER L/E RABBET STRAP AT WS 893 LIGHT CORROSION REMOVED IAW SRM 51-10-01. EVALUATED AND FOUND WITHIN LIMITS IAW 57-30-01. AREA FLAP PEENED IAW BAC 5730. AREA REPROTECTE D IAW 51-10-02. RIVETS INSTALLED IAW SRM 51-30-0Nov 2, 2000 · N675UP · Boeing 747123SDR UPS00434277Strap · corrodedINSPECTION TYPE:C LH WING . BULGING ON UPPER L/E RABBET STRAP AT WS 550. LIGHT CORROSION REMOVED IAW SRM 51-10-01. EVALUATED AND FOUND WITHIN LIMITS IAW SRM 57-30-01. AREA FLAP PEENED IAW BAC 5730. AREA REPROT ECTED IAW 51-10-02. RIVETS INSTALLED IAW SRM Nov 2, 2000 · N675UP · Boeing 747123SDR AWXA0000845Angle · crackedC-CHECK, ATTACH ANGLE CRACKED AT APPROX 683 RT WING OUTBOARD OF AILERON TRAILING EDGE. REMOVED AND REPLACED CRACKED ATTACH ANGLE IAW 737 SRM 51-30-2, FABBED REPLACEMENT PART IAW DWG 65-63461 AND 737 SRM 51-20-1.Nov 2, 2000 · N189AW · Boeing 737277SDR CA001122006Bushing · worn(CAN) DURING ROUTINE INSPECTION THE RT TOP LIFT STRUT BUSHING WAS FOUND TO BE WORN. THIS CONDITION APPEARS TO BE A WEAK PART IN DESIGN AS WE ARE CONSTANTLY REPAIRING THE TOP END OF THE LIFT STRUTS. : THE ALUMINIUM LIFT STRUT ENDS ARE FIELD REPAIRABLE.Nov 1, 2000 · Dhav DHC2*SDR L1GA200000318Flange · crackedFLANGE CRACKED 1.75 INCHES (UNDER ACCESS PNL TO AFT BOOST PUMP, 1305A).Oct 29, 2000 · N17533 · Doug DC932SDR DHL200080747CFitting · crackedAT C CK; WING CENTER SECTION AREA UNDER CABIN FLOOR FITTING CRACKED 2 INCHES AT STA 834.00 L-22 LT. REMOVED CRACKED FITTING IAW SRM 51-1-20D, PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B PG 1-2. INSTALLED NEW FITTING IAW SRM 51-1-20D, PG 9. REF:Oct 28, 2000 · N807DH · Doug DC873SDR UPS00234505Pin · corrodedINSPECTION TYPE:C, EVIDENCE OF CORROSION AT RIGHT WING FRONT SPAR BOTTLE PIN HEAD. REPLACED RIGHT WING FRONT SPAR BOTTLE PIN IN ACCORDANCE WITH MM 57-41-01.Oct 27, 2000 · N935UP · Boeing 7271A7CSDR DHL200080762CFitting · crackedAT C-CK; WING CENTER SECTION AREA UNDER CABIN FLOOR BELOW TRACK NR 6 FITTING .5 INCH AT STA 680.00 BL45R. REMOVED CRACKED FITTING IAW SRM 51-1-20D, CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B, PG 1-2, INSTALLED FITTING IAW SRM 51-1-20D. REF: N/R 1613.Oct 26, 2000 · N807DH · Doug DC873SDR DHL200080761CFitting · crackedAT C-CK; WING CENTER SECTION AREA UNDER CABIN FLOOR BELOW TRACK NR 2 FITTING CRACKED 1.5 INCH AT STA 680.000 BL 45L. REMOVED CRACKED FITTING IAW SRM 51-1-20D, CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B, PG 1-2, FABRICATED AND INSTALLED FITTING IAW SRM 5Oct 26, 2000 · N807DH · Doug DC873SDR DHL200080749CFitting · crackedAT C-CK; CENTER WING SECTION AREA UNDER CABIN FLOOR-FITTING BELOW TRACK NR 3 CRACKED 1 INCH AT STA 739.000 BL24L. REMOVED CRACKED FITTING IAW SRM 51-1-20D, PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B PG 1-2. INSTALLED NEW FITTING IAW SRM 51-1-20Oct 26, 2000 · N807DH · Doug DC873SDR QXEA0002951Angle · chafedPDX- RIGHT HAND MAIN LANDING GEAR WHEEL WELL ANGLE CHAFED, AFT SIDE OF STRUT BAY CUTOUT. REPAIRED IAW HORIZON AIR EA 4-57-500, AND FOKKER SRM 53-31-01.Oct 25, 2000 · N483US · Fokker F28MK4000SDR MWEA001108Stiffener · corrodedSECOND VERTICAL STIFFENER INBOARD OF RIGHT TRUNNION CORRODED. REMOVED AND REPLACED STIFFENER. DURING REPAIR, SPAR WEB WAS DAMAGED, DOUBLE DRILLED. REPAIRED SPAR PER TELEX MWX-ORD-00-00402.Oct 24, 2000 · N807ME · Doug DC981SDR DL72L011138Angle · crackedDURING SHOP VISIT THE LOWER AFT CHORD ANGLE WAS FOUND CRACKED AT I/B AFT FLAP DRIVE ROD CUTOUT.Oct 20, 2000 · N508DA · Boeing 727232SDR RRXA003247Stringer Clip · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE CLIP AT THE LT CENTER WING THRU ACCESS HOLE 516 THRU MID SPAR ACCESS HOLE 560E AT STA XCW +46 BETWEEN STRINGER 72 - 73, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 18, 2000 · N500MH · Doug DC871FSDR RRXA003246Stringer Clip · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE CLIP AT THE LT CENTER WING THRU ACCESS HOLE 516 THRU MID SPAR ACCESS HOLE 560E AT STA XCW +46 BETWEEN STRINGER 73 - 74, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 18, 2000 · N500MH · Doug DC871FSDR RRXA003245Stringer Clip · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE RT LWR CLIP LT CENTER WING THRU ACCESS HOLE 516 THRU MID SPAR ACCESS HOLE 560E AT STA XCW +23 & SCW +46 BETWEEN STR 73 - 74, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 18, 2000 · N500MH · Doug DC871FSDR P5CA0000338Bolt · brokenNR 2 SEQUENCE CARRIAGE ASSY HOOK BOLT FOUND SHEARED DURING INSPECTION. BOTH HOOK BOLTS REPLACED PER MM 27-51-30.Oct 17, 2000 · N806FT · Boeing 747249FSDR P5CA0000337Hook · looseABNORMALITY FOUND ON RT WING NR 7 POSITION SEQUENCE CARRIAGE HOOK ASSY FOUND LOOSE. REPLACE WITH NEW TOGGLE SEQUENCE ASSY P/N 65B17198-10, INSTALLED PER MM 27-51-30.Oct 17, 2000 · N806FT · Boeing 747249FSDR DL72E002144Stiffener · crackedFOUND DURING MV4 CORROSION VISIT NRC 22, L/E SPAR STIFFENER CRACK APPROX 1 INCH AT NR 7 SLAT INBOARD TRACK INBOARD ANGLE. REPLACED ANGLE PER M/M 57-20-21.Oct 17, 2000 · N283WA · Boeing 727247SDR DHL200080751CAngle · crackedAT C CK; LT WING T/E REINFORCING L ANGLE CRACKED 3 INCHES AT STA 409.000. REMOVED ANGLE IAW SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B PG 1-2. FABRICATED AND INSTALLED ANGLE IAW SRM 51-1-21 PG 1. REF: N/R 1582.Oct 14, 2000 · N807DH · Doug DC873SDR DHL200080750CFitting · crackedAT C CK; WING CENTER SECTION AREA UNDER CABIN FLOOR BELOW TRACK NR 5 FITTING CRACKED .5 INCH AT STA 680.000 BL24R. REMOVED CRACKED FITTING IAW SRM 51-1-20D, PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B, PG 1-2, INSTALLED NEW FITTING IAW SRM 51-1-2Oct 12, 2000 · N807DH · Doug DC873SDR GAIA00662Angle · crackedDISCREPANCY: DURING ROUTINE MAINTENANCE AT DFW, IT WAS DISCOVERED THAT THE RIGHT HAND WING BS 601. THE LOWER RIB ATTACH ANGLE HAS A TWO INCH CRACK. CORRECTIVE ACTION: STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER PER B727 SRM 57-10-5 AND S/B 727-57-0127. THOct 11, 2000 · N6838 · Boeing 727223SDR GAIA00661Angle · crackedDISCREPANCY: DURING ROUTINE MAINTENANCE AT DFW, IT WAS DISCOVERED THAT THE LEFT HAND WING BS410, THE LOWER RIB ATTACH ANGLE HAS A TWO INCH CRACK. CORRECTIVE ACTION: STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER PER B727 SRM 57-10-5 AND S/B 727-57-0127. THE Oct 11, 2000 · N6838 · Boeing 727223SDR UPS00434231Fitting · crackedINSPECTION TYPE:C, CENTER WING FRONT SPAR. LOWER CHORD CORRODED AT RBL 85, BS 1000. REPAIRS ACCOMPLISHED PER Q/NOTES 57/00 AND 57/00 SHEAR TIE P/N 69B14 267-6 AND FITTING P/N 69B14592-6 REPLACED.Oct 10, 2000 · N675UP · Boeing 747123SDR UPS00434234Web · crackedINSPECTION TYPE:C, RIGHT WING L/E CRACK ON L/E RIB BOLT HOLE AT OLES 1206.05. REPAIR CARRIED OUT IAW QUERY NOTE 61/2000.Oct 9, 2000 · N675UP · Boeing 747123SDR RRXA003179Web · crackedDURING A MAINTENANCE VISIT FOUND A CRACK IN WEB WHERE WEDGE ATTACH POINT IS ON THE RIGHT I/B FLAP AT STA XW 75, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 3, 2000 · N957R · Doug DC863FSDR SWAA001924Stiffener · crackedDURING SCHEDULED D-CHECK, FOUND CRACKED VERT STIFFENERS ON LT WING L/E FRONT SPAR, STA 386 & 388.3. REMOVED AND REPLACED VERT STIFFENERS PER SRM.Oct 3, 2000 · Boeing 7372H4SDR SWAA001910Stiffener · crackedTWO STIFFENERS FOUND CRACKED AT FWD BULKHEAD BS 663, MLG W/W. REMOVED AND REPLACED STIFFENERS PER SRM.Oct 1, 2000 · N338SW · Boeing 7373H4SDR RRXA003201Fitting · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE AFT REAR SPAR ATTACH T FITTING AT STA XRS 446, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Sep 29, 2000 · N500MH · Doug DC871FSDR RRXA003199Clip · crackedDURING A MAINTENANCE VISIT FOUND A CRACKED CLIP ON THE RT CENTER WING THRU ACCESS 516 AND I/B AT STA XCW -23 BETWEEN STRINGERS 53 & 54, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Sep 29, 2000 · N500MH · Doug DC871FSDR QXEA0002803Angle · crackedYXX- LEFT HAND WING YW139 ANGLE BETWEEN FORWARD SPAR AND NACELLE HAS EVIDENCE OF CRACKING AT TOP OF ANGLE. REPAIRED IAW DHC-8 SRM 51-20-00, PAGE 4 AND SRM 51-40-11, PAGE 1-6.Sep 29, 2000 · N368PH · Dhav DHC8202SDR RRXA003209Angle · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE AND A CRACK TO THE ATTACH ANGLE REAR SPAR UPPER CENTER WING IN CABIN Z-21 AT STA 857 +25 TO -45 LWR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Sep 28, 2000 · N500MH · Doug DC871FSDR USAA001574Web · crackedCLT - FOUND WEB CRACKED TWO PLACES .25 INCH EACH, 2 INCHES AND 3 INCHES AFT OF BS 706 AT BL 0. INSTALLED FILLER, DOUBLER AND TRIPLER PER TR 57-10-05. (M)Sep 27, 2000 · N261AU · Boeing 737201SDR RRXA003843Skin · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO DE-ICER VENT HOLES AT STA. XFS204-310, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-4,Sep 26, 2000 · N500MH · Doug DC871FSDR QXEA0002773Fastener · misinstalledPDX- STEMS PROTRUDING FROM THREE BLIND RIVETS AT RIGHT HAND STATION 8200 UPPER RIB FROM PANEL 74E. REPAIRED IAW HORIZON AIR EA 4-57-474.Sep 23, 2000 · N499US · Fokker F28MK4000SDR ABXA000462Angle · crackedLEFT WING LOWER AUX SPAR FITTING CRACKED. REPLACED ANGLE IAW DC9 SRM.Sep 19, 2000 · N931AX · Doug DC933FSDR 20001106SH013Carriage · chafedDURING C-CHECK, FOUND RIGHT FLAP TRACK CARRIAGE CHAFING DAMAGE. (X)Sep 18, 2000 · N944F · Doug DC933FSDR AU001064Stiffener · cracked(AUS) WING CENTRE SECTION VERTICAL STIFFENERS CRACKED IN HOLES. FOUND DURING INSPECTION IAW SB A320-57-1017.Sep 15, 2000 · Airbus A320211SDR RRXA003029Former · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE R/H WING L/E TOP I/B-T/E FORMER AT STA XFS 822.500, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLSep 14, 2000 · N500MH · Doug DC871FSDR RRXA003028Former · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE R/H WING L/E BOTTOM I/B-T/E FORMER AT STA XFS 791.250, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTSep 14, 2000 · N500MH · Doug DC871FSDR RRXA003027Former · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE R/H WING L/E TOP I/B-T/E FORMER AT STA XFS 728.750, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLSep 14, 2000 · N500MH · Doug DC871FSDR RRXA003021Former · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE L/H WING L/E TOP I/B-T/E FORMER AT STA XFS 562, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED ISep 14, 2000 · N500MH · Doug DC871FSDR RRXA003020Former · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE L/H L/E O/B-I/B SECTION TOP T/E FORMER AT STA XFS 578.750, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND Sep 14, 2000 · N500MH · Doug DC871FSDR RRXA003019Former · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE L/H L/E O/B-I/B SECTION TOP T/E FORMER AT STA XFS 597.500, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND ISep 14, 2000 · N500MH · Doug DC871FSDR CALA0001408Fairing · crackedINSPECTION FOUND A 1 INCH CRACK IN RT WING FLAP HINGE FAIRING NR 3 AFT. THE CRACK WAS STOP DRILLED AND A DOUBLER REPAIR WAS INSTALLED IAW SRM 57-01, FIGURE 3, SHEET 2, 51-10-4, AND 51-10-3.Sep 11, 2000 · N15841 · Doug DC982SDR UPS00833965Angle · crackedINSPECTION TYPE:C123, RT INBOARD PRESSURE PANEL LWR ATTACH ANGLE IS CRACKED, STA 857.0 ABOVE CTR WING TANK UPPER SKIN RWW. CLEANED SEALANT FROM AREA, FABED REPAIR ANGLE AND STRAPS IAW DC8 SRM 53-2-5. ALODINED AND PRIMED IAW 51-1-8, INSTALLED REPAIR PARTS IAWSep 9, 2000 · N798UP · Doug DC871FSDR ABXA000455Angle · crackedINTERNAL DOUBLER CRACKED AT LEFT WING STATION 267 LEADING EDGE. REPLACED ANGLE IAW DC9 SRM 51-30-25, 51-10-4, 51-10-3, 51-30-2, AND DWG 9919326.Sep 8, 2000 · N931AX · Doug DC933FSDR CALA0001406Channel · corrodedINSPECTION FOUND DOME NUT GANG CHANNEL AND OUTER SHIM OF LT WING LOWER FUEL TANK OPENING (PANEL 1371C) CORRODED. THE RUB STRIP AND GANG CHANNEL WERE REMOVED AND REPLACED IAW SRM 51-22-2 AND ECRA 5100-02063.Sep 8, 2000 · N35832 · Doug DC982
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