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 CA000511013Screw · misinstalled(CAN) DURING A PHASE 1 INSPECTION, INCORRECT LENGTH SCREWS WERE FOUND INSTALLED AT WING ACCESS PANELS FOR THE AILERON BELLCRANK. THE SCREWS WERE RUBBING ON THE BELLCRANK AND THE SUBMITTER STATED THAT THE ENDS OF THE SCREWS WERE FOUND WORN OFF.Mar 5, 2000 · Cessna 208BSDR QXEA0000784Flap Track · corrodedYYC- RIGHT HAND FLAP TRACK OUTBOARD LOWER TRACK HAS PITTING. REPAIRED IAW DHC-8 SRM 8-57-11.Mar 4, 2000 · N351PH · Dhav DHC8202SDR QXEA0000708Channel · damagedPDX- RIGHT HAND WING INTERNAL RIB LOWER U-CHANNEL AT WS 7600 HAS TOOL MARKS INSIDE CHANNEL BETWEEN BOTTOM SKIN STRINGERS 2.17 AND 2.15. REPAIRED IAW FOKKER SRM 57-01-01 PAGE 4.Mar 4, 2000 · N478US · Fokker F28MK4000SDR QXEA0000707Channel · damagedPDX- RIGHT HAND WING INTERNAL RIB LOWER O CHANNEL AT WS 7600 HAS TOOL MARKS INSIDE CHANNEL BETWEEN BOTTOM SKIN AT STRINGERS 2.8 AND 2.7. REPAIRED IAW FOKKER SRM 57-01-01 PAGE 4.Mar 4, 2000 · N478US · Fokker F28MK4000SDR DHL200072474CAngle · crackedAT C CHECK, FOUND RT WING LE RIB ATTACH ANGLE CRACKED AT SLAT STA 0. REMOVED AND REPLACED RT WING RIB ATTACH ANGLE PER SRM 51-40-3 AND 51-30-2.Mar 3, 2000 · N724DH · Boeing 727228SDR QXEA0000709Stringer Clip · damagedPDX- RIGHT HAND WING TOP SKIN STRINGERS 2.34 AND 2.36 FORWARD TIE CLIPS TO RIB 8780 HAVE UNTREATED CHAFE DAMAGE ON FORWARD EDGE. REPAIRED IAW FOKKER SRM 57-01-01 PAGE 3.Mar 3, 2000 · N478US · Fokker F28MK4000SDR RRXA000681Stiffener · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE R/H WING ROOT AT ACCESS DOOR WEB STIFFNER BELOW CONTROL TRAP FITTING AT STA XW-0 AND LONGERON 54R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICMar 2, 2000 · N831AL · Doug DC873FSDR DHL200072482CAngle · brokenAT C CHECK, FOUND LT WING TE PANEL AT WS 491 TO 519 HAS A BROKEN ATTACH ANGLE ON INBD SIDE BELOW NR 3 SPOILER. REMOVED AND REPLACED ANGLE PER SRM 51-30-2. TREATED AND PRIMED PER SRM 51-10-2.Mar 2, 2000 · N724DH · Boeing 727228SDR DHL200072437CAngle · crackedFOUND AT C CHECK, LT WING TE PANEL BELOW NR 2 SPOILER HAS CRACKED ATTACH ANGLES ON I/B SIDE. REMOVED AND REPLACED WITH NEW ANGLE AT LT WING TE PANEL BELOW NR 2 SPOILER.Mar 2, 2000 · N724DH · Boeing 727228SDR UPS00832064Access Door · crackedINSPECTION TYPE: C1, RT INBOARD SLOT, UPPER DOOR IS CRACKED. REMOVED AND REPLACED DOOR I.A.W. MM 27-80-00,OP''S CHECH WAS GOOD.Mar 2, 2000 · N748UP · Doug DC871FSDR UPS00832044Doubler · corrodedINSPECTION TYPE: C1, RT WING LE AT STA. XFS810.0, THE INTERNAL DOUBLER HAS HEAVY CORROSION. REMOVED, FABRICATED AND REPLACED DOUBLER I.A.W. DWG3641257,Mar 2, 2000 · N748UP · Doug DC871FSDR QXEA0000626Web · corrodedPDX - RIGHT WING FUEL ACCESS 74D HAS NUMEROUS SCREW HOLES WITH FRETTING CORROSION AROUND THEM. REPAIRED IAW FOKKER SRM 57-01-01, PAGE 65, PARAGRAPH B.Mar 2, 2000 · N478US · Fokker F28MK4000SDR 20000414AP002Flange · corrodedDURING MAINTENANCE AT MIA, WHILE COMPLYING WITH SB DC10-57A143, INTERGRANULAR CORROSION WAS FOUND ON THE FORWARD HORIZONTAL FLANGE (UPPER/INTERIOR SIDE) OF ARC1713-2 RIGHT OUTBOARD FLAP LOWER REAR SPAR CAP AT STATIONS XOF 549.672 - 557.489 AND XOF 722.235 - 72Mar 2, 2000 · N142WE · Doug DC1040SDR TWAA0006106Structure · crackedDURING OP 16 MAINT CHECK, THE SUPPORT STRUCTURE IN SIDE OF RT WING FLAP OTBD IDLE HINGE WAS CRACKED AT INBD AND OTBD SIDE. INSTALLED INBD AND OTBD RIBS PER DRAWING 5910134, SHEET 2 ZONE 18. ---CLOSED---Mar 1, 2000 · N989Z · Doug DC931SDR TWAA0003812Bracket · crackedDURING OP 16 MAINT CHECK, ON LT WING THE INBD BUTE DOOR ATTACH BRACKET AND REPAIR DOUBLER WERE CRACKED AT AFT END, APPROX 21 INCHES INBD OF INBD FLAP HINGE CASTING. FABRICATED NEW DOUBLER 0.032 SS 301 HALF HARD AND INSTALLED PER SRM 57-01 PAGE 8.Mar 1, 2000 · N925L · Doug DC932SDR QXEA0000750Strap · chafedPDX- WING TO FUSELAGE JOINT STRAP IS CHAFED UNDER PANEL 92J. REPAIRED IAW FOKKER SRM 51-10-04, PARAGRAPH 4B (1), PAGE 9 AND PARAGRAPH 3C (1-4) PAGE 8.Feb 29, 2000 · N478US · Fokker F28MK4000SDR QXEA0000749Strap · chafedPDX- WING TO FUSELAGE JOINT STRAP IS CHAFED UNDER PANEL 91J. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4B STEP 2 AND PARAGRAPH 3C STEPS 1 THRU 4 AND HORIZON AIR EA 4-53-376.Feb 29, 2000 · N478US · Fokker F28MK4000SDR RRXA003785Angle · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO ANGLE RT WW CEILING FWD RT SIDE AT STA 883 AND 47 INCHES RIGHT OF CENTER LINE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8Feb 28, 2000 · N792FT · Doug DC873FSDR RRXA000671Angle · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK TO THE RIGHT WING L/E UPPER RIB AT XFS 297.500, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED FASTENER, FABRICATED ANGLE AND INSTALLED IAW DC-8 SRM 51-1-20D,Feb 26, 2000 · N831AL · Doug DC873FSDR UPS00432185Web · corrodedINSPECTION TYPE:C 44. RT WING L/E CORROSION ON FRONT SPAR WEB AT SEVERAL LOCATIONS BETWEEN OLES 1200 AND OLES 1300 RT. PLEASE INVESTIGATE / RECTIFY. REPAIRED IAW QUERY NOTE N522UP/9/2000 AND APPROVED 8110-3.Feb 24, 2000 · N522UP · Boeing 747212BSDR UPS00832038Fitting · crackedINSPECTION TYPE:C123 RIGHT WING L/E FITTING CRACKED AT XS 250.089. REMOVED AND REPLACED FITTING IAW DWG 5754705, AND SRM 51-1-20D, 51-1-21.Feb 24, 2000 · N706UP · Doug DC871FSDR DHL200080377CAngle · crackedAT C-CHECK, NR 4 MAIN TANK LWR AFT ANGLE CRACKED 1 INCH APPROX XRS 255 (INTERIOR). REMOVED FITTING IAW SRM 51-1-21A PG 4, FABRICATED AND INSTALLED FITTING IAW SRM 51-1-21 PG 6 & 51-1-20D PG 9 & 10. N/R 1350Feb 24, 2000 · N803DH · Doug DC873FSDR RRXA002396Bracket · damagedDURING A MAINTENANCE VISIT FOUND ELONGATED HOLES ON THE ATTACH ANGLE BRACKET ON THE RT LEADING EDGE CENTER SECTION O/B SLOT DOOR PANEL AT STA XFS 520, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRFeb 23, 2000 · N995CF · Doug DC862SDR UPS00831892Doubler · crackedINSPECTION TYPE:C123, RIGHT WING L/E INTERNAL DOUBLER IS CRACKED AT XW 485. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW DWG 5769600, AND SRM 51-1-21, 51-1-21A.Feb 23, 2000 · N706UP · Doug DC871FSDR 20000328SH002Support Bracket · crackedBRAND NEW TANK SUPPORTS HAVE BEEN FOUND TO BE CRACKED ALONG THE BEND RADIUS WHERE THE ALUMINUM HAS BEEN COLD-FORMED, CLOSE TO THE TANK STRAP CLEVIS PEN HOLES. THIS PROBLEM HAS ALSO BEEN FOUND ON PARTS WITH TIME IN SERVICE, AND THE CRACKS PROGRESS WITH USE. (Feb 22, 2000 · Dhav DHC2*SDR QXEA0000548Bracket · damagedPDX - RIGHT NR 2 LIFT DUMPER CENTER ATTACH POINT AT HINGE BRACKET HAS DEEP NICKS. REPAIRED IAW HORIZON AIR EA 4-57-368.Feb 21, 2000 · N488US · Fokker F28MK4000SDR RRXA000658Clip · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK AT THE RIGHT WING L/E RIB CLIP AT STA XOLDI 6.225, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED IAW SRM 51-1-20D AND DAC DWG NR 5769589.Feb 19, 2000 · N831AL · Doug DC873FSDR 00FDEA00089Web · corrodedNR 693 CORROSION (C57-571-01-01) ON L/W FRONT SPAR WEB AT FUEL CELL PANEL CUT OUT 7340, FWD AND AFT WEB SURFACE WS 182. REMOVED AND REPLACED CORROSION PER FEDEX SRM 57-10-1, AND IAW FEDEX EA 7-5710-47901, FUEL LEAK CK IAW FEDEX MM 28-11-000-8 DTEP 7C.Feb 18, 2000 · N151FE · Boeing 72722SDR RRXA000657Clip · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK TO THE LT WING L/E INTERCOSTAL ATTACH CLIP AT STA XOLDI 6.225, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED IAW DC-8 SRM 51-1-21 AND DAC DWG 357Feb 16, 2000 · N831AL · Doug DC873FSDR DHL2000803132Channel · crackedAT C-CHECK, LEFT WING ACCESS PANEL 505C DOME NUT CHANNEL CRACKED (2) PLACES. REMOVED CRACKED CHANNEL AND FASTENERS IAW SRM 51-1-21A PAGE 4. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8 PAGE 11 & 12. FABRICATED PLATE IAW DC-8 MM 57-33-07 PAGE 201 AND 202 Feb 14, 2000 · N803DH · Doug DC873FSDR TWAA0002904Bracket · brokenDURING CHECK-C MAINT, THE LT WING NUMBER 4 LE SLAT, OTBD STRUCTURAL UP STOP MOUNT BRACKET WAS BROKEN/CRACKED BOTH SIDES. MANUFACTURED NEW BRACKET FROM 7075-T6 PER BOEING PRINT PL-65-17220. PRIMED, PAINTED, AND INSTALLED PER SRM 51-30-2.Feb 14, 2000 · N64339 · Boeing 727231SDR ASAA0080122Splice · crackedPHX - DURING 15K CHECK, THE LEFT WING LEADING EDGE SPLICE AT XRS 164 WAS FOUND CRACKED. REPLACED SPLICE PER SRM 51-30-2. (M)Feb 10, 2000 · N979AS · Doug DC983SDR RRXA000858Shim · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE LT. WING I/B NR 1 PYLON WING SPAR LWR CHORD SHIM PLATE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED SHIM FROM 7075-T6 AND INSTALLED IAW E.O. #99-236 WFeb 10, 2000 · N994CF · Doug DC862SDR RRXA000857Shim · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE RT. WING I/B NR 4 PYLON WING SPAR LWR CHORD SHIM PLATE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED SHIM FROM 7075-T6 AND INSTALLED IAW DCFeb 10, 2000 · N994CF · Doug DC862SDR UPS00231943Pin · corrodedINSPECTION TYPE:C&SI, LEFT WING REAR SPAR TO BODY BOTTLE PIN HAS PITTING CORROSION ON FLANGE THAT SITS AGAINST SPAR TO BODY FITTING. BOTTLE PIN REPLACED IAW MM 57-41-01.Feb 10, 2000 · N908UP · Boeing 72727CSDR TSAA200057060Splice Plate · crackedCENTER FUEL TANK SPLICE PLATE FOUND CRACKED. REPAIRED IAW ECO 1854. AIRCRAFT RETURNED TO SERVICE. (M)Feb 9, 2000 · N802AL · Boeing 7372S5CSDR UPS00831689Pan · crackedINSPECTION TYPE:C123 RIGHT WING L/E SLOT PAN AT STA XS 520.158 IS CRACKED. REMOVED AND REPLACED SLOT PAN IAW DWG 5769857, AND SRM 51-1-20D.Feb 9, 2000 · N707UP · Doug DC871FSDR QXEA0000593Web · crackedPDX - CEILING STRUCTURE ABOVE LEFT-HAND MAIN LANDING GEAR FITTING AFT LUG AFT ANGLE IS CRACKED AT A BLIND RIVET. REPAIRED IAW HORIZON AIR EA 4-57-354.Feb 6, 2000 · N488US · Fokker F28MK4000SDR QXEA0000592Web · crackedPDX - CEILING STRUCTURE ABOVE LEFT-HAND MAIN LANDING GEAR FITTING AFT LUG HAS THREE CRACKS. REPAIRED IAW HORIZON AIR EA 4-57-354.Feb 6, 2000 · N488US · Fokker F28MK4000SDR UPS00831721Fitting · crackedINSPECTION TYPE:C123, STA 440 STRINGER 64 SPLICE WAS CRACKED AFT OF FWD SPAR. REMOVED, FABRICATED AND REPLACED SPLICE FITTING IAW DWG 3644046 AND SRM 51-1-20D.Feb 4, 2000 · N707UP · Doug DC871FSDR UPS00431755Fitting · crackedINSPECTION TYPE:C 44, RT WING NR 3 MAIN FUEL TANK WS 586 REAR SPAR FITTING WAS CRACKED IN UPPER RADIUS. REPAIRED IAW EO B747-5720-10909 REF QUERY NOTE 12/2000, EFN 747-53-1095 AND ATTACHED 8110-3 NOTE, THIS IS A TIME LIMITED REPAIR, PERMANENT REPAIR WITHIN 18Feb 4, 2000 · N674UP · Boeing 747123SDR AWXA0000061Angle · crackedC-CHECK, PANEL SUPPORT ANGLE CRACKED PAST STOP DRILL, ON LT WING UPPER SURFACE UNDER PANEL 6301 UPPER FWD PYLON PANEL. REMOVED DAMAGED ANGLE IAW 737 SRM 51-30-2, FABRICATED NEW REPAIR ANGLE FRM (2024-0 .063 R700214) IAW 737 SRM 51-20-1, H/T TO 2024-T4 ALODINEFeb 4, 2000 · N185AW · Boeing 737277SDR CA000209019Structure · missing(CAN) THE CHAFE STRIP LOCATED AT THE TRAILING EDGE OF THE WING WAS FOUND TO BE MISSING. THE SUBMITTER STATES THAT HE HAS LOST FOUR SIMILAR STRIPS IN THE PREVIOUS FOUR DAYS.Feb 3, 2000 · Pilats PC1245SDR RRXA000952Fitting · brokenDURING A MAINTENANCE VISIT FOUND A BROKEN FASTENER AT THE RT. WING NR 3 STUB WING THROUGH STUB WING FRAME FITTING, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. REMOVED AND INSTALLED FITTING, PLUFeb 3, 2000 · N994CF · Doug DC862SDR USAA000157Slat Track · crackedPIT - LEFT FIXED LEADING EDGE OUTBOARD OF NR 7 SLAT TRACK HAS A .6 INCH CRACK. REMOVED TEMP REPAIR AND INSTALLED DOUBLERS PER EA 52344A. (M)Feb 2, 2000 · N813US · Doug DC981SDR QXEA0000547Fitting · chafedPDX - LEFT WING STATION 8200 FLAP FITTING HAS CHAFE DAMAGE. REPAIRED IAW HORIZON AIR EA 4-57-355.Feb 2, 2000 · N488US · Fokker F28MK4000SDR DHL200080380CBracket · crackedAT C-CHECK, RT WING L/E LWR PART NR 555L ACCESS DOOR SLOT ADJUSTMENT FRAME CRACKED 1 INCH. STOP DRILLED CRACK, FABRICATED REPAIR DOUBLER AND INSTALLED IAW EO NR DHL020301. N/R 1889Feb 2, 2000 · N803DH · Doug DC873FSDR 20000405SH005Bolt · crackedDURING INSPECTION OF WING SPARS IAW AD 89-25-10 AND BEECH SIRM MANUAL, THE LEFT LOWER FORWARD WING BOLT WAS FOUND CRACKED USING DYE PENETRANT. (X)Feb 1, 2000 · N16NM · Beech E90SDR UPS00831724Doubler · crackedINSPECTION TYPE:C123, LEFT WING L/E INTERNAL DOUBLER CRACKED AT XFS 297.5. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5641252 AND SRM 51-1-21.Jan 26, 2000 · N707UP · Doug DC871FSDR UPS00831719Doubler · crackedINSPECTION TYPE:C123, RIGHT WING L/E INTERNAL DOUBLER CRACKED AT XW485. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5769600 AND SRM 51-1-20D, 51-1-21.Jan 26, 2000 · N707UP · Doug DC871F
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