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 MWEA00283Pad · damagedTEMPORARY REPAIR INSTALLED ON RIGHT HAND JACK PAD, INSTALLED PERMANENT REPAIR. MAINTENANCE FABRICATED AND INSTALLED DOUBLER.Apr 4, 2000 · N401ME · Doug DC932SDR MWEA00299Stringer Clip · crackedRIGHT WING STRINGER 11, STATION XRS 111.5 OUTBOARD CLIP IS CRACKED. FABRICATED AND INSTALLED NEW CLIP.Apr 4, 2000 · N900ME · Doug DC915SDR UPS00832398Doubler · crackedINSPECTION TYPE:C123 RIGHT WING L/E LOWER INTERNAL DOUBLER IS CRACKED AT XFS 597.5. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5769600 AND SRM 51-1-21, 51-1-20D.Apr 3, 2000 · N709UP · Doug DC871FSDR UPS00832221Doubler · crackedINSPECTION TYPE: C1, LT WING LE, LOWER DOUBLER CRACKED OUTBOARD OF XOLDI 6.225. REMOVED, FABRICATED, AND REPLACED DOUBLER I.A.W. DWG. 5769891, AND SRM. 51-1-20DApr 3, 2000 · N709UP · Doug DC871FSDR UPS00832220Doubler · crackedINSPECTION TYPE: C1, RT WING LE, LOWER INTERNAL DOUBLER IS CRACKED AT XFS 201.250 REMOVED, FABRICATED, AND REPLACED DOUBLER I.A.W. DWG. 5718325, AND SRM. 51-1-20D,51-1-21Apr 3, 2000 · N709UP · Doug DC871FSDR RAAA00E9008Dome Nut · corrodedLEAKING DOME NUT, WING TO NACELLE FILLET, NR 3 PLANK UPPER SURFACE. REMOVED DOME NUT, INSPECTION FOR CORROSION FOUND BEYOND LIMITS. REMOVED CORROSION IAW LAC SRM 57-2-1. INSTALLED REPAIR IAW LAC DRAWING 841880. ALODINED AND PRIMED IAW SRM 51-2-14.Apr 3, 2000 · N1968R · Lkheed 188CSDR UPS00832216Doubler · crackedINSPECTION TYPE: C1, LT WING LE INTERNAL DOUBLER IS CRACKED AT XW 485 REMOVED, FABRICATED, AND REPLACED DOUBLER I.A.W. DWG. 5769600,AND SRM. 51-1-20D,51-1-21Apr 2, 2000 · N709UP · Doug DC871FSDR DHL200080427CAngle · crackedCENTER WING (MAIN CARGO) CENTRAL TANK UPPER SKIN ANGLE CRACKED AT 857 BL-22 RT. INSTALLED ANGLE IAW SRM 51-2-0 AND 51-1-21.Mar 31, 2000 · N804DH · Doug DC873FSDR DHL2000804126Angle · brokenRT WING 4 EACH INTERIOR PNUEMATIC TUBING SUPPORT ANGLE BROKEN 2 INCHES AT UPPER PART BETWEEN XW 398.00 AND XW 408.00 ACCESS DOOR. REMOVED BROKEN SUPPORT ANGLE PER SRM 51-1-21. FABRICATED NEW ANGLE PER SRM 57-2-0. CLEANED, TREATED AND PRIMED AREA PER SRM 51-Mar 30, 2000 · N804DH · Doug DC873FSDR RRXA001835Fitting · elongatedDURING A MAINTENANCE VISIT FOUND A CRACK INDICATION TO THE STRINGER END FITTING AT THE LT WING LWR WING AT STA 64, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. OVERSIZED FASTENER HOLES AND INSTALLED SMar 28, 2000 · N961R · Doug DC873FSDR AALA2000262Stiffener · corrodedTUL - FOUND 3 GROUND LUGS CORRODED, 3RD STIFFENER INBOARD OF TANK 2 FUEL DUMP VALVE. BLENDED AREA TO REMOVE CORROSION. INSTALLED L-ANGLE 13 INCHES LONG, INSIDE OF FORWARD FLANGE ON Z-ANGLE STIFFENER PER AARD 51-40-00-1. (M)Mar 28, 2000 · N878AA · Boeing 727223SDR TWAA0005501Tie Clip · crackedDURING CHECK-C MAINT ON THE RT WING, THE TIE CLIP FROM RIB TO FRONT SPAR WAS CRACKED AT UPPER T/E 26 INCHES O/B OF NR 11 L/E TRACK. CONFIRMED BY NDT. REPLACED RIB PER SPM 6-70-01 PAGE 3, AND INSTALLATION DRAWING 9919329.Mar 28, 2000 · N9306T · Doug DC983SDR 20000630AP001Flange · corrodedDURING C-CHECK, FOUND CORROSION ON RIGHT WING REAR SPAR UPPER CAP AT STATION XORS 562.390, UNDER THE INBOARD FLAP HINGE OF THE OUTBOARD FLAP. CORROSION WAS REMOVED AND A MAJOR REPAIR WAS MADE IAW BOEING MESSAGE DAR-FCO-00-00001E, AND A FAA FORM 8110-3 WAS ISSMar 25, 2000 · N140WE · Doug DC1040FSDR QXEA0001092Stringer Clip · crackedPDX - LT CENTER WING LOWER SKIN, OUTBOARD Z STRINGER CLIPS, ARE CRACKED IN SIX LOCATIONS SEEN AT FAIRING PANEL 91L OPENING. Z STRINGERS ARE 2.23, 2.22, 2.21, 2.20, 2.19 AND 2.14. REMOVED AND REPLACED CLIPS IAW FOKKER SRM 51-31-01 AND SRM 51-30-02.Mar 25, 2000 · N494US · Fokker F28MK4000SDR QXEA0001100Channel · corrodedPDX - CORROSION IN BOTTOM U CHANNEL OF RIB 2230, RT COLLECTOR TANK, BETWEEN STRINGER 15 AND 16 FROM FORWARD SPAR. REPAIRED IAW HORIZON AIR EA 4-57-396.Mar 23, 2000 · N487US · Fokker F28MK4000SDR AT0000150Strap · corrodedDURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND CORROSION ON NUTPLATE STRAP UPPER SPAR CAP WS 445 - 430. AFTER REMOVAL OF CORROSION FOUND MATERIAL OUT OF LIMITS. CORRECTIVE ACTION: FABRICATED AND INSTALLED NEW STRAP IAW DC9 SRM 51-30-02, 51Mar 21, 2000 · N810AT · Doug DC932SDR UPS00232142Support Bracket · crackedINSPECTION TYPE: C, LT WING, FIXED TE SUPPORT BRACKET CRACKED, AREA BELOW 37 SPOILER I/B HINGE. REPLACED BRACKET IAW SRM 51-30-02Mar 20, 2000 · N934UP · Boeing 72721CSDR QXEA0001101Channel · corrodedPDX - CORROSION IN BOTTOM U CHANNEL OF RIB 2230, RT COLLECTOR TANK, BETWEEN STRINGER 5 AND 6, FROM FORWARD SPAR. REPAIRED IAW FOKKER SRM 57-01-01, PAGE 5, PARAGRAPH B3A.Mar 19, 2000 · N487US · Fokker F28MK4000SDR P2EA00087Frame · crackedYXD - DURING C-CHECK, FOUND A CRACK ON RIGHT INBOARD LEADING EDGE UPPER CHORD AT WBL 219.67, LENGTH .4OO INCH, WIDTH .016 INCH. REPAIRED CRACK AT WBL 219.67 RIGHT INBOARD UPPER CHORD BY REPLACEMENT PER SRM 51-10-1 ADN 52-20-2 WORK ACCOMPLISHED ON NON-ROUTINE Mar 18, 2000 · N121NJ · Boeing 7372Q8SDR DHL200072408CAngle · crackedAT C-CHECK, FOUND RT/W O/B UPPER T/E PANEL O/B SUPPORT ANGLE CRACKED JUST I/B OF O/B AILERON. REMOVED AND REPLACED ANGLE IAW 727 SRM 51-30-2. ALODINED AND PRIMED AREA IAW 727 SRM 51-10-2. INSTALLED PANELS PER M/M 51-30-2.Mar 18, 2000 · N724DH · Boeing 727228SDR DL72W000576Angle · crackedFOUND DURING MV2 CORROSION VISIT, LOWER COVE SKIN ATTACH ANGLE CRACKED ON NR 8 SLAT AT O/B STOP PAD. REPAIRED PER M/M 57-54-0 FIG 812. NR 8 L/E SLAT (S/N BN 390).Mar 16, 2000 · N293WA · Boeing 727247SDR DHL200072403CStructure · crackedAT C-CHECK, FOUND LEFT WING T/E CORRUGATED STRIP CRACKED AT STA 520. REMOVED CRACKED CORRUGATED STRIP LEFT WING T/E COVE PANEL AT WS 521.53 WS 498.08 AS PER BOING 727 SRM 51-30-2. FWD I/B CORNER DELAMINATED LEFT WING T/E COVE PANEL BETWEEN WS 521.53 AND WS 4Mar 16, 2000 · N724DH · Boeing 727228SDR RRXA002156Angle · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE ANGLE ON THE AFT END OF THE CENTER WING BOX LOWER SKIN EXTERIOR AT FS 855 AND XCW 68 RT., DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLMar 13, 2000 · N2674U · Doug DC873FSDR UPS00432184Channel · corrodedINSPECTION TYPE: C, RT WING LEADING EDGE. CORROSION ON SUPPORT CHANNEL FOR LE LOWER. FALSE WORK PANEL I/B OF NR 4 ENGINE.Mar 13, 2000 · N522UP · Boeing 747212BSDR UPS00432160Channel · corrodedINSPECTION TYPE: C, LT WING LEADING EDGE. CORRODED ON SUPPORT CHANNEL FOR LE LOWER. FALSEWORK PANEL INBOARD OF NR 1 ENGINE. CHANNEL REPAIRED I.A.W QUERY NOTE 36/2000.Mar 13, 2000 · N522UP · Boeing 747212BSDR DL72L000500Flap Track · corrodedDURING OVERHAUL ON THE I/B FLAP, I/B TRACK ASSY, CORROSION WAS FOUND AT THE MLG AND SPOILER BEAM ATTACH PAD AREAS AND WEAR AT THE FWD ATTACH LUGS AND SPACER BAR HOLES. REPAIRED PER ER/A 387258-14AD AND BF GOODRICH ENGINEERING REPAIR NR 23-0575.Mar 13, 2000 · N506DA · Boeing 727232SDR DL72L000498Flap Track · corrodedDURING OVERHAUL OF THE I/B FLAP I/B TRACK ASSY, TYPICAL CORROSION WAS FOUND AT THE MLG AND SPOILER BEAM ATTACH PAD AREAS. IN ADDITION, TYPICAL WEAR WAS FOUND AT THE FWD ATTACH LUGS, AND THE MLG DOOR HINGE FITTING ATTACH HOLES, THE SPACER BAR ATTACH HOLES, ANDMar 13, 2000 · N506DA · Boeing 727232SDR USAA000364Support Bracket · crackedPIT - FOUND CRACK OUTBOARD PANEL SUPPORT UPPER AFT LEG AT STATION XW.99016. CUT DAMAGED LEG OF BRACE AND SPLICED IN NEW SECTION PER EO 5788MM381. (M)Mar 13, 2000 · N800US · Doug DC981SDR DHL200072429CFitting · crackedAT C CHECK, FOUND RT WING TE FITTING CRACKED AT WS 578. REMOVED RT WING TE FITTING AT WS 578. ALODINE AND PRIMED AREA. INSTALLED NEW FITTING ON RT WING TE AT WS 578, PER SRM 51-10-1 PART 4. LEAK CHECK PER MM 28-10-01.Mar 10, 2000 · N724DH · Boeing 727228SDR RRXA000708Fitting · crackedDURING A MAINTENANCE VISIT FOUND A CRACK ON THE LT WING L/E INTERNALLY 28 1/2 INCHES FWD OF WING SPAR UPPER CORD AT XILD .7095, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FITTING IAW DMar 9, 2000 · N831AL · Doug DC873FSDR RRXA000696Channel · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO RIB STIFFNER 16 IN. INBD OF LT MLG ACTUATOR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW STIFFNER.Mar 7, 2000 · N831AL · Doug DC873FSDR DHL200072478CDoubler · crackedAT C CHECK, FOUND LT WING TE CORROGATED DOUBLER AT REAR SPAR LOWER CHORD CRACKED AT STA 533. REPLACED CORROGATED DOUBLER TE AT REAR SPAR LOWER CHORD WS 533.Mar 7, 2000 · N724DH · Boeing 727228SDR DHL200072477CPlate · crackedAT C CHECK, FOUND LT WING CORROGATED PLATE CRACKED AT TE BELOW NR 3 SPOILER WS 540. REPLACED CORROGATED DOUBLER TE AT REAR SPAR LOWER CHORD WS 540 PER SRM 51-30-2.Mar 7, 2000 · N724DH · Boeing 727228SDR DHL200072413CAngle · brokenAT C-CHECK, FOUND LEFT WING T/E LOWER PANEL SUPPORT BROKEN AT WING STA 542. REMOVED AND REPLACED BROKEN ANGLE SUPPORT (P/N 65-21658-27) LEFT WING T/E PANEL AT WING STA 543.68 AS PER BOING 727 SRM 51-30-2. CHECKED ROD ADJUSTMENT FOR COVE PANEL AND FORE FLAP CMar 7, 2000 · N724DH · Boeing 727228SDR DHL200072412CSupport Bracket · crackedAT C-CHECK, FOUND LEFT WING T/E LOWER PANEL SUPPORT BRACKET CRACKED AT WING STATION 520. REMOVED AND REPLACED LEFT WING T/E LOWER COVE PANEL SUPPORT ANGLE (P/N 65-21658-30) AT WING STA 521.53 AS PER BOEING 727 SRM 51-30-2. CHECK ROD ADJUSTMENT FOR COVE PANELMar 7, 2000 · N724DH · Boeing 727228SDR DHL200072414CAngle · crackedAT C-CHECK, FOUND LEFT WING LOWER PANEL SUPPORT BRACKET CRACKED AT WING STA 566. REMOVED AND REPLACED LEFT WING T/E LOWER COVE PANEL SUPPORT ANGLE (P/N 65-21658-25) AT WING STA 567 AS PER BOING 727 SRM 51-30-2. CHECKED ROD ADJUSTMENT FOR COVE PANEL AND FORE Mar 7, 2000 · N724DH · Boeing 727228SDR DHL200072411CSupport Bracket · crackedAT C-CHECK, FOUND LEFT WING T/E LOWER PANEL SUPPORT BRACKETS CRACKED AT WING STA 500. REMOVED AND REPLACED LEFT WING T/E LOWER COVE PANEL SUPPORT ANGLES AT WING STA 498.08 PER BOEING SRM 51-30-2. CHECKED ROD ADJUSTMENT FOR COVE PANEL AND FORE FLAP CLEARANCE Mar 7, 2000 · N724DH · Boeing 727228SDR DHL200072424CDoubler · crackedAT C-CHECK, FOUND LEFT WING REAR SPAR LOWER CHORD, CORRUGATED DOUBLER CRACKED AT WING STATION 522. REMOVED AND REPLACED CORRUGATED DOUBLER AT LT WING REAR SPAR LOWER CHORD WS 522 AS PER 727 SRM 51-10-1.Mar 7, 2000 · N724DH · Boeing 727228SDR UPS00831992Doubler · crackedINSPECTION TYPE:C1, LEFT WING INTERNAL DOUBLER IS CRACKED AT STA XFS 297.5. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5769589 AND SRM 51-1-20D.Mar 7, 2000 · N748UP · Doug DC871FSDR 2000ZZZX570Fitting · looseRIGHT WING ATTACHMENT FITTING STA 136 UNDER AFT BAGGAGE COMPARTMENT FLOOR. PLATE, P/N 23662-00, AND FITTING, P/N 23663-00, RIVETS GONE.Mar 7, 2000 · N5457P · Piper PA24250SDR QXEA0000699Angle · crackedPDX- RIGHT HAND WING TO FUSELAGE ATTACH ANGLE CRACKED AT STATION 1700 Z STRINGER STATION 1825. REPAIRED IAW FOKKER SRM 51-31-01 AND FOKKER SRM 51-30-02.Mar 7, 2000 · N478US · Fokker F28MK4000SDR RRXA000692Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE RT WING L/E RIB AT UPPER END (AFT) AT STA XFS 753.75, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED, REPAIRED AND INSTALLEMar 6, 2000 · N831AL · Doug DC873FSDR DHL200072479CDoubler · crackedAT C CHECK, FOUND CORROGATED DOUBLER AT SPAR LOWER CHORD, CRACKED LT WS 544. REMOVED AND REPLACED CORROGATED DOUBLER AT REAR SPAR LOWER CHORD LT WS 544 PER SRM 51-10-1.Mar 6, 2000 · N724DH · Boeing 727228SDR DHL200072475CAngle · crackedAT C CHECK, FOUND SUPPORT ANGLE CRACKED AT RT WING FWD SPAR UPPER CHORD 2 INCHES I/B OF SLAT STA 0. REMOVED AND REPLACED SUPPORT ANGLE PER SRM 51-30-2.Mar 6, 2000 · N724DH · Boeing 727228SDR DHL200072472CChannel · crackedAT C CHECK, FOUND RT WING TE COVE PANEL SUPPORT CHANELS AT WS 521.53 ARE CRACKED AND BROKEN. REPLACED COVE PANEL SUPPORT CHANELS PER SRM 51-30-2.Mar 6, 2000 · N724DH · Boeing 727228SDR DHL200072471CAngle · wornAT C CHECK, FOUND RT WING TE COVE PANEL SUPPORT ROD AT WS 543.68 UPPER ATTACH ANGLE WORN, ROD IS LOOSE. REMOVED AND REPLACED ANGLES PER SRM 51-30-2.TREATED AND PRIMED AREA PER SRM 51-10-2.Mar 6, 2000 · N724DH · Boeing 727228SDR DHL200072470CChannel · crackedAT C CHECK, FOUND RT WING TE COVE PANEL I/B SUPPORT CHANEL AT WS 567 CRACKED. REMOVED AND REPLACED SUPPORT CHANEL PER SRM 51-30-2.Mar 6, 2000 · N724DH · Boeing 727228SDR DHL200072469CChannel · crackedAT C CHECK, FOUND RT WING TE COVE PANEL O/B SUPPORT CHANEL WS 447.90 CRACKED. REPLACED SUPPORT CHANEL PER SRM 51-10-1 PARA 4 & 51-30-2.Mar 6, 2000 · N724DH · Boeing 727228SDR DHL200072468CChannel · crackedAT C CHECK, FOUND RT WING TE COVE PANEL INBD SUPPORT CHANEL AT WS 469.93 CRACKED. REMOVED OLD SUPPORT CHANEL PER SRM 51-30-2. INSTALLED NEW CHANEL PER SRM 51-30-2.Mar 6, 2000 · N724DH · Boeing 727228SDR DHL200072466CAngle · crackedAT C CHECK, FOUND RT WING TE SMALL LOWER SUPPORT ANGLE ON THE FWD SIDE OF THE NR 8 SPOILER ACTUATER FITTING CRACKED. REMOVED AND REPLACED SUPPORT ANGLE PER SRM 51-30-2. TREATED AND PRIMED PER SRM 51-10-6.Mar 6, 2000 · N724DH · Boeing 727228
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