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 AMTA200300892Stiffener · crackedWING FORWARD SPAR VERTICAL STIFFENER CRACKED. REPAIRED VERTICAL STIFFENER IAW EO L10-57AD-0606. (M)May 23, 2003 · N162AT · Lkheed 10113853SDR UIEA200300025Fitting · crackedDURING C-CHECK, FOUND RT KICK FITTING BOLT HOLES POSITION A, B AND K STILL SHOWING CRACK INDICATION AFTER 2ND OVERSIZE REAMING. PERMANENT REPAIR WITH DEVIATION TO REF 'A' SB PER REF 'B', 'C', AND 'D' BY OVERSIZING HOLE 'A', 'B'B AND 'K' THROUGH ALL COMPONENTSMay 20, 2003 · N809MC · Boeing 747228FSDR SWIA200312096Clip · damagedWING CLIP JUST IN FRONT OF NR 2 FUEL LEVEL STICK AT RT WING IS CRACKED. (DISCOVERED DURING C-CHECK.)REMOVED DAMAGED WING CLIP AS REQUIRED. INSTALLED NEW WING CLIP IN RH WING . NO LEAKS NOTED AT THIS TIME.May 19, 2003 · N296SW · Emb EMB120ERSDR 2003F00484Angle · brokenAT C-CHECK, FOUND BROKEN ANGLE BEHIND SLAT NR 3 STOP, LEADING EDGE LEFT WING. REPAIRED ANGLE IAW SRM 51-20-00. (M)May 15, 2003 · N951LF · Airbus A320233SDR ASOA03207Fitting · crackedDURING HANGAR MAINTENANCE IN BTR, THE RIGHT WING INBOARD SPOILER HINGE FITTING AT STATION WS 185.11 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE WILL REMOVE AND REPLACE THE RIGHT WING INBOARD SPOILER HINGE FITTING AT STATION WS 185.11 UPON ARRIVAL OF THMay 10, 2003 · N705EV · Cndair CL6002C10SDR DHL2003604579Intercostal · crackedLT WING T/E INTERCOSTAL WITH 2.000 CRACK IN IT AT STA. XRS.74.000. STOP DRILLED CRACK AND FABRICATED DOUBLER (2024-T3 0.040) IAW SRM 57-2-0 FIG.2. CLEANED, TREATED AND PRIMED AREA AND DOUBLER IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 51-1-21 PG.1.May 9, 2003 · N604AL · Doug DC873FSDR TN8A200300001Attach Angle · corrodedWHILE CHANGING A WING INSPECTION OF UNDER SURFACE OF WING ATTATCH REVEILED CORROSION REQUIREMENT REPLACEMENT OF ATTATCH ANGLE AND ASSOCIATED WING SKIN.May 5, 2003 · N31TN · Doug R4D8ZSDR DHL2003604559Attach Angle · crackedLT WING OUTBOARD STUB WING ATTACHING ANGLE CRACKED 1.000 AT XS 520.168. REMOVED CRACKED ATTACHING ANGLE ON LT WING OUTBOARD STUB WING AT XS 520.168 IAW SRM 51-1-21 PG 1. FABRICATED NEW ANGLE IAW SRM 57-2-0 PG 1. CLEANED, TREATED AND PRIMED NEW ANGLE AND AREMay 3, 2003 · N604AL · Doug DC873FSDR GTIA030365Support · crackedFTW - FOUND RIGHT WING LEADING EDGE STATION XFS 624 CRACKED AND BENT, SUPPORT. REMOVED SUPPORT. LOCATED AND DRILLED NEW SUPPORT. INSTALLED THE NEW SUPPORT. (M)May 3, 2003 · N800NK · Doug DC982SDR DHL2003801015Door · crackedLEFT WING OUTBOARD SLOT OUTBOARD DOOR CRACKED. REMOVED AND REPLACED OUTBOARD SLOT OUTBOARD DOOR AND TIGHTENED SRCEW OF LT WING IAW SRM 51-3-1 PG 2A. FOR OPS CHECK SEE N/R 0075.May 3, 2003 · N801DH · Doug DC873FSDR DHL2003604535Splice Plate · brokenLT OUTER WING OTBD L/E FORMER SPLICE PLATE BROKEN AT XFS 710.000. REMOVED SPLICE PLATE IAW SRM 51-1-21 PG 1. FABRICATE NEW SPLICE PLATE IAW SRM 57-1-0 PG 2, SRM 57-3-0 FIG 20. CLEANED, TREATED AND PRIMED AREA AND NEW SPLICE PLATE IAW SRM 51-1-8B. INSTALLEDMay 2, 2003 · N604AL · Doug DC873FSDR 03FDEA00572Bracket · crackedLEFT WING TIP UPPER SUPPORT BRACKET FOR NAVIGATION LIGHT LENS HAS 1.5 INCH CRACK IN RADIUS OF BRACKET. FABRICATED AND INSTALLED BRACKET IAW BOEING 727 SRM 51-20-1 AND 51-30-2.Apr 22, 2003 · N218FE · Boeing 727200SDR 03FDEA00511Intercostal · bentINTERCOSTAL BENT ON LEFT WING LOWER SURFACE AT ATTACH POINT FOR WING ACCESS PANEL 12 INCHES INBOARD OF MAIN LANDING GEAR FORWARD TRUNNION.Apr 18, 2003 · N218FE · Boeing 727200SDR 03FDEA00498Cover · gougedLEFT WING INBOARD FORE FLAP UPPER SURFACE GOUGED UNDER NR 2 GROUND SPOILER. REMOVED AND REPLACED COVER PLATE IAW BOEING 727-200 SRM 51-30-02.Apr 17, 2003 · N218FE · Boeing 727200SDR UPS03840482Angle · crackedINSPECTION TYPE: C1, RT WING CENTER LE. SUPPORT ANGLE AT XS 520 IS CRACKED. REMOVED,FABRICATED AND REPLACED ANGLE IAW DWG. 9753297,AND SRM. 51-1-20DApr 16, 2003 · N808UP · Doug DC873FSDR 03FDEA00463Stiffener · gougedLEFT WING NR 3 FLAP TRACK MOVEABLE FAIRING I/B FORWARD INTERNAL STIFFENER GOUGED. *S/D* REMOVED AND REPLACED RIB STIFFENER IAW BOEING 727-200 SRM 57-20-03.Apr 16, 2003 · N218FE · Boeing 727200SDR SWIA200311870Stringer Clip · missingSTRINGER CLIP AT WS 106.4 LOWER WING PLANK, FORWARD INTEGRAL STRINGER MISSING. FOUND DURING C-CHECK INSPECTION.Apr 16, 2003 · N588SW · Cndair CL6002B19SDR AWXA200300432Angle · crackedMCN - MAJOR REPAIR - DURING C-17 CHECK A .1875 INCH CRACK WAS FOUND ON THE RT WING INBOARD TRAILING EDGE UPPER FIXED PANEL LOWER SUPPORT ANGLE WBL 72.25. MAINTENANCE REMOVED CRACKED LOWER SUPPORT ANGLE AT WBL 72.25; FABRICATED A NEW REPLACEMENT ANGLE; INSTALLApr 13, 2003 · N168AW · Boeing 73733ASDR UPS03840615Stiffener · crackedINSPECTION TYPE: C1, RIGHT WHEEL WELL AT STA. XW 5 AFT T-CAP STRUT FOR TE. IS CRACKED REMOVED,FABRICATED AND REPLACED STIFFENER I.A.W. 9887427,AND SRM. 51-1-20DApr 12, 2003 · N808UP · Doug DC873FSDR ASAA0380311Support Bracket · crackedOAK - FOUND DURING 15K CHECK, RIGHT FUEL TANK FUEL LINE SUPPORT BRACKET IS CRACKED ON OUTBOARD SIDE. REPLACED SUPPORT BRACKET PER SRM 51-30-1 AND 10-4. (M)Apr 11, 2003 · N947AS · Doug DC983SDR TSAA0357064Flange · corrodedREMOVED CORROSION DAMAGE BY SMOOTHLY BLENDING REWORK AREA. PERFORMED HFEC INSPECTION TO VERIFY CRACK AND CORROSION FREE. FLAT PEENED REWORKED SURFACE. FABRICATED A FILLER FROM 2024-T3 SIZED TO FIT BLENDOUT AREA AND RESTORE TO ORIGINAL CONTOUR. APPLIED ALODApr 10, 2003 · N827AL · Boeing 737209SDR TSAA0357062Leg Assy · corrodedCUTOUT THE DAMAGED FROM THE VERTICAL LEG. BLENDED OUT REMAINING AREA OF THE CHORD MAINTAINING A GREATER THAN .050 INCH THICKNESS. PERFORMED 10X VISUAL AND HFEC INSPECTION TO VERIFY CRACK AND CORROSION FREE. FLAP PEENED REWORKED SURFACES. FABRICATED REPAIR Apr 10, 2003 · N827AL · Boeing 737209SDR TSAA0357063Leg Assy · corrodedREMOVED CORROSION DAMAGE BY BLENDING TO A 20 TO 1 RATION. PERFORMED 10X VISUAL AND HFEC INSPECTON TO VERIFY CRACK AND CORROSION FREE. FABRICATED A TAPERED SHIM FROM 2024-T3. FLAT PEENED SURFACE. APPLIED ALODINE AND TWO COATS OF BMS 10-11, TYPE I PRIMER TO BApr 10, 2003 · N827AL · Boeing 737209SDR 2003UALA00368Seal · deterioratedSMOKE APPEARING FROM RIGHT WING. SMOKE WAS ACTUALLY ONE END OF A RUBBER SEAL THAT HAD BECOME DISLODGED AND WAS FLUTTERING AT 500 MPH. DISLODGED PART OF THE SEAL END WAS CUT AND SURFACE REPAIRED.Apr 9, 2003 · N771UA · Boeing 777222SDR ASAA02402FFStructure · chafedDURING C-CHECK, FOUND RIGHT WING INBOARD EXHAUST FATE UPPER SURFACE CHAFED AT OUTBOARD FORWARD EDGE. REPAIRED IAW SRM. (M)Apr 7, 2003 · N775AS · Boeing 7374Q8SDR UPS03840479Fitting · crackedINSPECTION TYPE: C3, NR 1 ALT AFT BOOST PUMP MOUNT FITTING IS CRACKED. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D RECEIVED NEW FITTING P/ N 3645611U PO SP094626. LOCATED, DRILLED, AND DEBURRED IAW DC8 SRM 5 1-1-24. INSTALLED IAW DC8 SRM 51-1-20D.Apr 7, 2003 · N819UP · Doug DC873FSDR ASAA02402SSSupport Bracket · wornDURING C-CHECK, FOUND RT WING TRAILING EDGE LOWER SURFACE PANEL SUPPORT BRACKET WORN AT NR 5 SPOILER OUTBOARD ACTUATOR. REPAIRED IAW SRM. (M)Mar 31, 2003 · N775AS · Boeing 7374Q8SDR MWEA030149Nut Plate · corrodedCORROSION AROUND NUT PLATE AT STATION 1015 INSIDE RIGHT FLAP TRACK STRUCTURE SUPPORT/FAIRING SUPPORT. DRILLED UP AND INSTALLED SUPPORT.Mar 28, 2003 · N803ME · Doug DC981SDR DHL2003741526Angle · crackedDURING C-CHECK, RT WING, LWR I/B LEADING EDGE, INSIDE ACCESS PANEL CAVITY 6401 UPPER O/B, L/E WEB TO L/E SKIN ATTACH ANGLE HAS 2 INCH CRACK. REMOVED FASTENERS RT LOWER I/B, L/E INSIDE ACCESS PANEL UPPER O/B L/E WEB TO L/E SKIN ANGLE IAW B-727 SRM 51-30-2. CUMar 24, 2003 · N741DH · Boeing 727200SDR DHL2003741534Stiffener · crackedDURING C-CHECK DISCREPANCY AS FOLLOWS, LT WING FRONT SPAR VERTICAL STIFFENER HAS TWO CRACKS AT LOWER TWO RIVETS AT LEADING EDGE STA 90. REMOVED FASTENER AT LT WING FRONT SPAR VERTICAL STIFFENER CUT OUT DAMAGE AREA DIM APPROX 2.375 BY 2.4375 INCH IAW B-727 SRMMar 23, 2003 · N741DH · Boeing 727200SDR QXEA0300368Bracket · crackedLEFT HAND WING FORM BRACKET CRACKED (NACELLE TO WING UPPER SHROUD SUPPORT). REPAIRED IAW HORIZON AIR EA 6-54-214.Mar 14, 2003 · N406QX · Bombdr DHC8401SDR 03FDEA00318Stringer Clip · crackedRIGHT WING NR 3 FUEL TANK HAS A CRACKED UPPER BUTTERFLY CLIP AT STA XORS 402. THIS WAS FOUND DURING A ROUTINE INSPECTION.Mar 14, 2003 · N68052 · Doug DC1010SDR LR7A03013Stiffener · crackedDURING SCHEDULED C4 INSPECTION PER JOB CARD HC5711 FOUND LT WING FLAP WELL BULKHEAD WEB BRACE/ STIFFENER CRACKED AT OWS 241. REPLACED STIFFENER IAW SRM SMP 583 51-60 AND 51-70. NR 2033.Mar 13, 2003 · N403LC · Lkheed 382GSDR ASAA0340124Channel · crackedPAE - DURING C-CHECK, FOUND LEFT WING UPPER INBOARD TRAILING EDGE PANEL SUPPORT CHANNEL CRACKED WBL 87. REPAIRED IAW EA. (M)Mar 10, 2003 · N705AS · Boeing 737490SDR ASAA0340123Web · gougedDURING C-CHECK, FOUND GOUGE IN WEB AT RIGHT AIR CONDITIONING BAY 1 INCH BELOW THE AFT RT HEAT EXCHANGER OUTBOARD FLANGE INBOARD SIDE OF WEB. REPAIRED IAW SRM.Mar 10, 2003 · N705AS · Boeing 737490SDR 2003F00430Angle · crackedAT C-CHECK, FOUND STRUCTURE CRACKED, NOSE WHEEL WELL AT BS 294.5, LBL 12 RT, WL 177. STOP DRILLED CRACKS. FABRICATED FORMED ANGLE REPAIRS AND STRAPS. TREATED, PRIMED AND INSTALLED ANGLES AND STRAPS IN NOSE WHEEL WELL RIGHT SUPPORT AT STATION 294.5. (M)Mar 10, 2003 · N7640U · Boeing 727222SDR 2003F00446Bracket · crackedAT C-CHECK, FOUND CRACK AT LT WING LOWER TRAILING EDGE PANEL SUPPORT BRACKET, OUTBOARD OF NR 2 SPOILER ACTUATOR. REMOVED AND REPLACED BRACKET ON LEFT WING LOWER TRAILING EDGE PANEL SUPPORT BRACKET AT NR 2 SPOILER, OUTBOARD OF ACTUATOR. (M)Mar 8, 2003 · N7640U · Boeing 727222SDR UPS03240297Rib · crackedINSPECTION TYPE:C&SI ON REMOVAL OF WING TIP, INNER RIB FOUND TO BE CRACKED RIB REPLACED IAW SRM 51-20-1 FIG 7 & DRAWING 65-72719 SHEET 6Mar 8, 2003 · N949UP · Boeing 72725CSDR ASAA0310119Angle · crackedOKC - DURING D-CHECK, FOUND RIGHT WING LEADING EDGE ANGLE AT WING STATION 567 CRACKED. REMOVED AND REPLACED ANGLE PER SRM. (M)Mar 7, 2003 · N745AS · Boeing 737298CSDR 2003F00426Web · crackedAT C-CHECK, FOUND RT MLG WW FORWARD BULKHEAD INBOARD WEB CRACKED, STATION 870. STOP DRILLED CRACK AT INBOARD SIDE OF STATION 870, RIGHT WHEEL WELL. HFEC VERIFIED STOP DRILL. FABRICATED REPAIR DOUBLER FOR AFT SIDE OF STATION 870 BULKHEAD WEB AND REPAIR DOUBLMar 5, 2003 · N7640U · Boeing 727222SDR ASAA0340105Angle · crackedDURING C-CHECK, FOUND CRACKED INBOARD UPPER RIGHT WING TRAILING EDGE PANEL INBOARD SUPPORT ANGLE AFT END. REPAIRED IAW SRM. (M)Mar 1, 2003 · N773AS · Boeing 7374Q8SDR F3LA200300099Channel · corrodedDURING EXIT CHECK, INSPECTION REPORTED LT. WING CHANNEL CRACKED AT WBL 73.00. FABRICATED AND INSTALLED REPLACEMENT ANGLE PER SRM 51-10-2, PARA 6, AND SRM 51-40-2.Feb 28, 2003 · N318FL · Boeing 7373Q8SDR ASAA0310026Angle · chafedPAE - DURING C-CHECK, FOUND LEFT WING TRAILING EDGE SIDE SUPPORT ANGLE AT WING STATION 337L, WATERLINE 180 CHAFED. REMOVED AND REPLACED SUPPORT PER SRM. (M)Feb 22, 2003 · N744AS · Boeing 737210CSDR UPS03240305Panel · delaminatedINSPECTION TYPE:C&SI DELAM ON R/H WING TE PANEL UPPER FWD OF NO 10 SPOILER PANEL REPAIRED IAW SRM 51-40-5Feb 17, 2003 · N936UP · Boeing 727108CSDR CA030214006Skin · cracked(CAN) THE DOUBLERS ON THE BOTTOM OF THE WING WALK SKINS JUST OUTBOARD OF THE INBOARD STAMPED STIFFENERS WERE SEVERELY CRACKED. THE AFT SKIN CRACK WAS 42CM IN LENGTH. THE FORWARD SKIN HAD 3 CRACKS 5CM IN LENGTH. THIS AREA IS NOT NORMALLY ACCESSIBLE BUT THIS AIRFeb 14, 2003 · Piper PA28140SDR DHL2003804898Angle · crackedRT WING- CTR L/E TO STUB WING JOINT ANGLE CRACKED 0.500. REMOVED CRACKED JOINT ANGLE IAW SRM 51-1-21 PG 1. FABRICATED JOINT ANGLE (7075-0-0.080) IAW SRM 57-2-0 PG 2. PERFORMED HEAT TREATMENT IAW SRM 51-1-4 PG 1-3, DPS 1-05.3, SRM 51-1-1 PG 1, 17. CLEANED, Feb 11, 2003 · N804DH · Doug DC873FSDR DHL2003804880Angle · crackedLT STUB WING CTR L/E ATTACH ANGLE AT STA XS 515.750 WITH 2.000 INCH CRACK. REMOVED DAMAGED ANGLE IAW SRM 51-3-0 PAGE 1. FABRICATED ANGLE (7075-T6 AL 0.080) IAW SRM 57-2-0 FIG 2. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW ANGLE IAW SRM 51-3-Feb 10, 2003 · N804DH · Doug DC873FSDR DHL2003804891Vane · damagedRT OUTBOARD SLOT VANE AT STA XOLDI6.224 HOLES ELONGATED (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW EODHL-030105,ED-3210. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. TRIMMED OUT THE DAMAGED SKIN SEGMENT IAW EODHL-030105, ED-3210. FABRICATED AN EXTERNAL REPAIR DFeb 8, 2003 · N804DH · Doug DC873FSDR MWEA030059Fillet · crackedCREW REPORTED LEFT SIDE WING AREA VIBRATION WITH FLAPS UP AND GEAR RETRACTED. FOUND FILLET CRACKS AND RIGHT ACM DUCT SUPPORT BRACKET BOLTS BROKE. REPAIRED FILLET PER SRM 53-01 AND WELDED REPAIR DUCT MOUNT FLANGES.Feb 8, 2003 · N401ME · Doug DC932SDR UPS03840230Stringer Clip · crackedINSPECTION TYPE: C1, RIGHT WING STRINGER CLIP IS CRACKED AT STRINGER 73 AT XRS 50. REMOVED, FABRICATED, AND REPLACED CLIP IAW SAA SK 811-162.Feb 8, 2003 · N811UP · Doug DC873F
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