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 UPS06847086Stiffener · crackedINSPECTION TYPE:C3 BROKEN STIFFENING ANGLE INSIDE LEFT CTR L/E, AT INBOARD END OF SLOT DOOR COVE, STA XW 408. REMOVED BROKEN STIFFENER AT STA XW 408 IAW SRM 51-3-0, FABRICATED AND INSTALLED STIFFENER AT STA XW 408 LEFT CTR L/E IAW DWG 3770673 AND SRM 51-01-20May 20, 2006 · N715UP · Doug DC871FSDR UPS06146941Support · crackedINSPECTION TYPE:1C LT WING ABOVE NR 4 FLAP TRACK; WEB CRACKED. REMOVED AND REPLACED SKIN SUPPORT PER A300 SRM 51-40-00 AND 51-40-21.May 17, 2006 · N154UP · Airbus A300F4622RSDR HALA0600385Structure · corrodedRT WING TOP 5 AREAS OF MODERATE CORROSION JUST AFT OF NR 4 SLAT (MARKED). REMOVED CORROSION AT 5 AREAS PER SRM 51-10-04. BLENDED AREAS OK PER HALM105 NR 475086.May 17, 2006 · N475HA · Boeing 717200SDR HALA0600417Clip · crackedLEFT WING RIB ATTACHMENT CLIP IS CRACKED AT LE UPPER SPAR LES 571. REMOVED CLIP TRIMMED, LOCATED, DRILLED, ALODINED, PRIMED AND INSTALLED NEW CLIP L/W LES 571, UPPER SPAR USING BAC1503-100386 EXTRUSION 7675T6 LOT NR 681279 ALL WORK DONE IAW SRM 51-40-02-00-0 May 16, 2006 · N584HA · Boeing 767300SDR HALA0600413Web · damagedRT WING T/E VERTICAL WEB 9" O/B OF NR 7 SPOILER I/B HINGE IS DAMAGED AT CUT OUT. REPAIRED THE CUTOUT OF THE R/W T/E VERTICAL WEB 9" O/B OF NR 7 SPOILER I/B HINGE IAW SRM 57-51-02-27-1, 51-70-13, 51-10-02-06.May 15, 2006 · N584HA · Boeing 767300SDR 06FDEA1919Fitting · corrodedRT WING - OUTBOARD FLAP, INBOARD HINGE FITTING, INBOARD AFT BORE HOLE FOUND CORRODED. RIGHT WING OUTBOARD FLAP ASSEMBLY REMOVED AND REPLACED AS PER MM 27-50- 30-4 AND FLAP ADJUSTMENT CARRIED OUT AS PER MM 27-50-00-830-805. FLAP SYSTEM RANGE OF MOVEMEMay 15, 2006 · N599FE · Doug MD11SDR 06FDEA1918Fitting · corrodedRIGHT WING, OUTBOARD FLAP, INBOARD HINGE FITTING OUTBOARD MID BORE HOLE FOUND CORRODED. REMOVED AND REPLACED AS PER MM 27-50- 30-4 AND FLAP ADJUSTMENT CARRIED OUT AS PER MM 27-50-00-830-805. FLAP SYSTEM RANGE OF MOVEMENT TEST CARRIED OUT AS PER MM 27-5May 15, 2006 · N599FE · Doug MD11SDR 06FDEA1917Fitting · corrodedFOUND RIGHT WING, OUTBOARD FLAP, INBOARD HINGE FITTING INBOARD MID BORE HOLE FOUND CORRODED. REMOVED AND REPLACED AS PER MM 27-50- 30-4 AND FLAP ADJUSTMENT CARRIED OUT AS PER MM 27-50-00-830-805. FLAP SYSTEM RANGE OF MOVEMENT TEST CARRIED OUT AS PER MMMay 15, 2006 · N599FE · Doug MD11SDR QXEA200602244Strip · corrodedYYC: LT WING, L/E 513BL, UPPER AND LOWER ATTACHMENT STRIP IS CORRODED. MAINTENANCE REPAIRED IAW Q400 SRM TASK 51-14-00-350-803, SRM 51-42-05-330-801 AND SRM TASK 51-25-10-370-801.May 11, 2006 · N424QX · Bombdr DHC8402SDR DHL2006873503Structure · crackedRIGHT WING OUTBOARD L/E OUTER SECTION FORMER 0.250 INCH CRACK STA XFS 822.500. PERFORMED STOP HOLE AND FABRICATED 2EA ANGLE DOUBLER (AL7075T6 0.025") IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLED ANGLEMay 11, 2006 · N873SJ · Doug DC873FSDR QXEA200602245Strip · corrodedYYC: LT WING, L/E 513DL, UPPER AND LOWER ATTACHMENT STRIPS ARE CORRODED. MAINTENANCE REPAIRED IAW Q400 SRM 51-42-05-330-801, SRM 51-21-00-850-801 AND SRM 51-25-10-370-801.May 10, 2006 · N424QX · Bombdr DHC8402SDR QXEA200601321Attach Bracket · corrodedYYC - C4 LEFT HAND WING FRONT SPAR ATTACH BRACKET AT YW 58.0 IS CORRODED, BRACKET IS BLEED AIR DUCT ATTACHMENT SUPPORT. REPAIRED IAW EA 2-57-366, SRM 51-40-11.May 10, 2006 · N355PH · Dhav DHC8202SDR DHL2006873502Structure · crackedLEFT WING CTR L/E LWR FORMER 1 INCH CRACK STA XFS 341.500. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-1-20D. PERFORMED STOP HOLE AND FABRICATED ANGLE DOUBLERS (2EA) OF AL7075T6 0.032" IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLERMay 10, 2006 · N873SJ · Doug DC873FSDR DHL2006873501Angle · crackedRIGHT WING CTR L/E LWR REINFORCING ANGLE CRACK STA XFS 341.500. PERFORMED STOP HOLE IAW SRM 57-2-0 PG 9-10. FABRICATED 2EA ANGLE DOUBLERS (AL7075T6 0.040") IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLERS IAW SRM 51-1-8B. INSTALLMay 10, 2006 · N873SJ · Doug DC873FSDR UPS06447014Web · crackedINSPECTION TYPE:C RIGHT WING - L/E D-FAIRING SUPPORT WEB FOUND CRACK AT R2 PDU I/B AREA. CRACK LENGTH 3.5 INCHES. RIGHT WING L/E D-FAIRING SUPPORT WEB REPAIRED AT ILES943 TO ILES955.5 AREA APPROX AS PER SRM 57-20-03 FIG 7.May 9, 2006 · N521UP · Boeing 747200SDR DHL2006873500Support Angle · crackedLEFT WING CTR L/E INTERIOR UPPER SUPPORT ANGLE 1 INCH CRACK STA XOLDI 6.225. REMOVED CRACKED ANGLE IAW SRM 51-1-21. FABRICATED NEW ANGLE (AL7075T6 0.063") IAW SRM 57-2-0 PG 1. CLEANED, TREATED AND PRIMED AREA AND NEW ANGLE IAW SRM 51-1-8B. INSTALLED NEW ANMay 9, 2006 · N873SJ · Doug DC873FSDR UPS06446997Plate · crackedINSPECTION TYPE:C LEFT WING SURGE TANK WS 1516 UPPER STR 10 VENT CHANNEL ATTACH PLATE CRACK. CRACK LENGTH .375 INCH. LEFT WING SURGE TANK WS 1516 UPPER STR 10 VENT CHANNEL ATTACH PLATE REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 & 51-30-02.May 8, 2006 · N521UP · Boeing 747200SDR QXEA200601312Structure · corrodedYYC - C4 RIGHT HAND WING UPPER ACCESS 622AT, COUNTERSINK HOLES HAVE FRETTING CORROSION. REPAIRED IAW RD8-57-1715.May 6, 2006 · N355PH · Dhav DHC8202SDR UPS06446977Fitting · crackedINSPECTION TYPE:C LT WING NR 2 L/E PDU FWD SUPPORT ATT NOSE BEAM UPPER CHORD FOUND CRACK AS MARK, NR 7 VC FLAP I/B. CRACK LENGTH .625 AND 2.5 INCH. LT WING NR 2 L/E PDU FWD SUPPORT ATT NOSE BEAM UPPER CHORD AT BETWEEN AILES 949 - 962 AREA REPAIRED AS PER SRMMay 5, 2006 · N521UP · Boeing 747200SDR ABXA060248Intercostal · corrodedLEFT INTERCOSTAL WAS CORRODED JUST OUTBOARD OF LEFT MAIN LANDING GEAR. REMOVED AND REPLACED LEFT INTERCOSTAL IAW B767 SRM.May 2, 2006 · N784AX · Boeing 767281SDR QXEA200601502Fitting · damagedYYC C3 LEFT HAND WING, UPPER LEADING EDGE REBATES FROM STATION YW191 TO STATION YW535 HAVE CUT MARKS FROM BOX CUTTERS. REPAIRED IAW RD 8/4-57-646 , ISSUE 1 AND HORIZON AIR EA 6-57-469.May 2, 2006 · N425QX · Bombdr DHC8402SDR QXEA200601501Fitting · damagedYYC C3 RIGHT HAND WING, UPPER LEADING EDGE REBATES FROM STATION UYW310 TO STATION YW425, HAVE CUT MARKS FROM BOX CUTTERS. REPAIRED IAW Q400 RD 8/4-57-645, ISSUE 1.May 2, 2006 · N425QX · Bombdr DHC8402SDR USAA060645Stiffener · crackedFOUND VERTICAL STIFFENER CRACKED, STA 663 LBL 6.15. INSTALLED REPAIR PARTS ON VERTICAL STIFFENER IAW TR 57-10-03B, DEFECT SIZE: .5".May 1, 2006 · N334US · Boeing 737301SDR QXEA200601243Panel · chafedPDX - C3 PANEL 684 AB HAS CHAFING. REPAIRED IAW SRM 57-52-01 AND SRM 51-12-00.Apr 30, 2006 · N604QX · Cndair CL6002C10SDR QXEA200601226Bracket · crackedPDX - C3 "L" BRACKET LOCATED IN FAIRING ATTACHED TO THE TELESCOPING DE-ICE DUCT ON RIGHT HAND WING IS CRACKED. REPAIRED IAW SRM 51-12-06-001-001-1-01.Apr 30, 2006 · N604QX · Cndair CL6002C10SDR QXEA200601306Structure · gougedYYC - C4 LEFT HAND, TOP REBATE AT STATION YW 260.0 IS GOUGED. REPAIRED IAW RD8-57-1675 AND SRM 51-20-36.Apr 26, 2006 · N355PH · Dhav DHC8202SDR QXEA200601500Fitting · damagedYYC C3 RIGHT WING, CENTER FUSELAGE SECTION 621, ALL REBATES FOR PANELS IN SECTION 621 HAVE CUT MARKS FROM BOX CUTTERS. REPAIRED IAW Q400 SRM 51-14-00-350-803, 51-25-10-320-801 AND RD 8/4-53-451, ISSUE 1.Apr 19, 2006 · N425QX · Bombdr DHC8402SDR QXEA200601498Fitting · chafedYYC C3 RIGHT HAND WING, CENTER FUSELAGE SECTION 621, FORWARD REBATE FOR PANEL NR 261HT HAS CHAFFING DAMAGE. REPAIRED IAW Q400 SRM 51-14-00-350-803 AND SRM 51-25-10-370-801.Apr 13, 2006 · N425QX · Bombdr DHC8402SDR 2006UALA00682Stiffener · crackedFOUND STIFFENERS AT RBL 6.15 CRACKED ON THE WING REAR SPAR CENTER SECTION APPROX 17 INCHES UP FROM LOWER END OF LT & RT STIFFENER. STIFFENERS AT LBL & RBL REPLACED PER SB 737-57A1269. THIS IS TERMINATING ACTION FOR AD 2005-20-01.Apr 13, 2006 · N370UA · Boeing 737322SDR QXEA200601092Bracket · crackedPDX - C4 RIGHT INBOARD WING OUTBOARD UPPER NUT PLATE L BRACKET CRACKED AT NACELLE. REPAIRED IAW DASH8 200 SRM 51-40-00.Apr 12, 2006 · N356PH · Dhav DHC8202SDR QXEA200601523Fitting · scratchedYYC C3 STATION YW389.019 TO YW425.019 FUEL TANK LID ATTACH REBATE HAS MINOR SCRATCHES AND LIGHT CORROSION AROUND FOUR SCREW HOLES. REPAIRED IAW DHC-8 Q400 SRM 57-20-30-320-802 AND 51-21-10-380-801.Apr 11, 2006 · N425QX · Bombdr DHC8402SDR QXEA200601499Fitting · damagedYYC C3 RIGHT WING, FURL TANK LID REBATES FROM STATION YW191 TO STATION YW425, HAVE CUT MARKS FROM BOX CUTTERS. REPAIRED IAW Q400 SRM 57-20-30-320-802, 57-20-30-992-8202 AND SRM TASK 51-21-10-380-801.Apr 11, 2006 · N425QX · Bombdr DHC8402SDR UPS06146720Intercostal · crackedLT WING T/E NR 4 SPOILER LOCATION INTERCOSTAL CRACKED IN FLAPWELL. REMOVED AND REPLACED INTERCOSTAL PER A300 SRM 51-40-00 AND 51-40-21.Apr 6, 2006 · N133UP · Airbus A300F4622RSDR USAA060574Strap · corrodedSTRAP AT STA 1015 RBL 6 CORRODED. REMOVED DAMAGE AND INSTALLED FABRICATED PART IAW BWG 65-46812, DEFECT SIZE: 1 X 4 INCH.Apr 5, 2006 · N505AU · Boeing 7373B7SDR USAA060541Angle · crackedRT WING 135.5 RIB LOWER CHORD ANGLE AT AFT END IN VERTICAL LEG CRACKED. REMOVED DAMAGE, FABRICATED AND INSTALLED NEW REPAIR PARTS IAW EA 97533, DEFECT SIZE: .50 INCH.Apr 3, 2006 · N777AU · Boeing 7374B7SDR IXXA06RNG020SSupport Bracket · corrodedDURING ROUTINE C CHECK, FOUND CORROSION AND ONE SCRATCH ON MAIN LANDING GEAR RETRACT BRACKET LEFT HAND. CORRODED AREA WAS REPAIRED IAW EWO ATI 57-073 AND AMM 57-40-1 PAGE 801. FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR.Apr 2, 2006 · N823BX · Doug DC871FSDR DU4R2006336Clamp · corrodedCORROSION NOTED ON RT WING FUEL PANEL 641AB CLAMP RING. REMOVED AND REPLACED RT WING FUEL PANEL 641AB CLAMP RING P/N 69-35343-5 IAW B757 MM 28-11-01.Mar 30, 2006 · N675DL · Boeing 757232SDR DU4R2006335Clamp · corrodedCORROSION NOTED ON RT WING FUEL PANEL 641DB CLAMP RING. REMOVED AND REPLACED RT WING FUEL PANEL 641DB CLAMP RING P/N 69-35343-5 IAW B757 MM 28-11-01.Mar 30, 2006 · N675DL · Boeing 757232SDR DU4R2006333Clamp · corrodedCORROSION NOTED ON RT WING FUEL 641EB CLAMP RING. REMOVED AND REPLACED FUEL PANEL 641EB CLAMP RING P/N 69-35343-5 IAW B757 SRM 28-11-01.Mar 30, 2006 · N675DL · Boeing 757232SDR DU4R2006331Clamp · corrodedCORROSION NOTED ON RT WING FUEL 641FB CLAMP RING. REMOVED AND REPLACED FUEL PANEL 641FB CLAMP RING IAW B757 SRM 28-11-01.Mar 30, 2006 · N675DL · Boeing 757232SDR DU4R2006329Clamp · corrodedCORROSION NOTED ON RT WING FUEL PANEL CLAMP RING 641GB. REMOVED AND REPLACED FUEL PANEL 641GB CLAMP RING IAW B757 SRM 28-11-01.Mar 30, 2006 · N675DL · Boeing 757232SDR DU4R2006327Clamp · corrodedCORROSION NOTED ON RT WING FUEL PANEL 641HB CLAMP UP RING. REMOVED AND REPLACED FUEL PANEL 641HB CLAMP RING P/N 69-35343-5 IAW B757 SRM 28-11-01.Mar 30, 2006 · N675DL · Boeing 757232SDR DL733060250Stiffener · crackedDURING ACCOMPLISHMENT OF 05-086589-12AD, THE WING CENTER SECTION REAR SPAR STIFFENER AT LBL 6.15 WAS FOUND CRACKED. REPLACED REAR SPAR STIFFENER.Mar 29, 2006 · N306WA · Boeing 737347SDR AWXA200600647Shim · migratedGYR - DURING C12 CHECK DISCOVERED NR 2 ENGINE PYLON DIAGONAL BRACE ATTACH FITTING VERTICAL SHIMS MIGRATED LT 0.200 INCHES AND R/H 0.030 INCHES. MAINTENANCE REMOVED AND REPLACED LEFT AND RIGHT DIAGONAL BRACE ATTACH FITTING SHIMS PER AWA ER 19-5453-06060-BA1.Mar 29, 2006 · N910AW · Boeing 7572G7SDR DHL2006764505Stiffener · crackedLWR END OF VERTICAL STIFFENER CRACKED ON RT WING FIXED LE WSTA125. STOP DRILLED CRACK PER B727 SRM 51-10-1, HFEC STOP DRLL IAW B727 NDT MAN PT 6 51-00-00 FIG 23. FAB`D DOUBLER FROM 7075T6 .063 PO# 9002454 DIM. 25" BY 7" IAW B727 SRM 51-40-3 FIG 1 AND 57-20-2Mar 27, 2006 · N764AT · Boeing 727264SDR 06FDEA1240Doubler · crackedLT WING, AT STA XOS 762 LEADING EDGE CAVITY BEADED DOUBLER FOUND CRACKED. LEFT WING AT STA XOS 762 LEADING EDGE CAVITY CRACKED BEADED DOUBLER. REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 25 VOLUME I. THIS REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100.Mar 27, 2006 · N588FE · Doug MD11SDR 06FDEA1239Doubler · crackedLT WING, AT STA XOS 697 LEADING EDGE CAVITY BEADED DOUBLER FOUND CRACKED. LEFT WING AT STA XOS 697 LEADING EDGE CAVITY CRACKED BEADED DOUBLER. REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 25 VOLUME I. THIS REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100.Mar 27, 2006 · N588FE · Doug MD11SDR 06FDEA1238Doubler · crackedLT WING, AT STA XOS 670 LEADING EDGE CAVITY BEADED DOUBLER FOUND CRACKED. LEFT WING AT STA XOS 670 LEADING EDGE CAVITY CRACKED BEADED DOUBLER REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 25 VOLUME I. THIS REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100.Mar 27, 2006 · N588FE · Doug MD11SDR 06FDEA1237Doubler · crackedLT WING, AT STA XOS 647 LEADING EDGE CAVITY BEADED DOUBLER FOUND CRACKED. LEFT WING AT STA XOS 647 LEADING EDGE CAVITY CRACKED BEADED DOUBLER REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 25 VOLUME I. THIS REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100.Mar 27, 2006 · N588FE · Doug MD11SDR 06FDEA1198Doubler · crackedLT WING, AT STA XOS 624 LEADING EDGE CAVITY BEADED DOUBLER FOUND CRACKED. CRACK ON LEFT WING STA XOS 624 LEADING EDGE CAVITY BEADED DOUBLER REPAIRED AS PER FEDEX EA NR 1-5730-95801, TITLE: WINGS, LEADING EDGE BEADED DOUBLER, PERMANENT REPAIR. THIS REPAIR IS Mar 22, 2006 · N588FE · Doug MD11
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