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 USAA050092Plate · fatiguedPIT - Q6 - MAIN LANDING GEAR FG; INSTALLATION OF REAR SPAR FATIGUE PLATE; INSTALLATION OF REAR SPAR FATIGUE PLATE; LT REAR SPAR UPPER CHORD BETWEEN WBL 150 AND 126. FABRICATED DOUBLER AND INSTALLED IAW EA 79629. (K)Jan 3, 2005 · N517AU · Boeing 7373B7SDR ASA044408Angle · crackedPAE - LT WING T/E LWR ANGLE CRACK ON UPPER T/E PANEL. REMOVED, FABRICATED AND REPLACED ANGLE. (K)Dec 31, 2004 · N765AS · Boeing 7374Q8SDR DHL2004809512Fairing · crackedRIGHT WING T/E FAIRING CRACKED 2.000 (STA XW -5.000 TO 5.000) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 12-22-04, DWG X32-R01, REV IR DATED 12-20-04, DWG 5651221. REMOVED CRACKED FAIRING IAW SRM 51-1-21 PG 1. FABRICATED NEW FAIRING (AL2Dec 30, 2004 · N809DH · Doug DC873FSDR 04FDEA03492Rub Strip · corrodedLEFT HAND WING - NR 2 TANK NR 531 AT CUTOUT RUB STRIP FOUND CORRODED. REMOVED DAMAGED RUB-STRIP AS PER SRM 51-31-01 VOL II AND INSTALLED NEW RUB-STRIP AS PER SRM 51-42-04 VOL II AND SRM 51-35-01 VOL II AT LT WING NR 2 TANK 531AT CUT-OUT.Dec 28, 2004 · N577FE · Doug MD11SDR 04FDEA03491Channel · damagedLEFT HAND WING NR 2 TANK NR 531 AT CUTOUT GANG CHANNEL FOUND DAMAGED. REMOVED DAMAGED GANG CHANNEL AS PER SRM 51-31-01 VOL II. FABRICATED BUSHING AS PER SRM 51-73-00 VOL II AND INSTALLED AS PER SRM 51-73-00 VOL II. INSTALLED NEW GANG CHANNEL AS PER SRM 51Dec 28, 2004 · N577FE · Doug MD11SDR QXEA200500087Pan · crackedPDX - THE RIGHT STUB WING PRESSURE PAN HAS A CRACK IN IT. REO 670-53-61-060.Dec 25, 2004 · N613QX · Cndair CL6002C10SDR DHL2004809501Intercostal · crackedLT WING CTR L/E INTERCOSTAL CRACKED 1.000, XFS 410.250 (UPPER PART). REMOVED CRACKED INTERCOSTAL IAW SRM 51-1-21 PG 1. FABRICATED NEW INTERCOSTAL (AL2024-T3 0.063) IAW SRM 57-2-0 PG 1. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW INTERCOSTAL Dec 22, 2004 · N809DH · Doug DC873FSDR QXEA200500077Flange · corrodedPDX - PITTING ON THE UPPER SURFACE OF THE LOWER INBOARD FLANGE. COMPLETED BLENDING OF PITTING IN ACCORDANCE WITH EA2-57-151A.Dec 21, 2004 · N357PH · Dhav DHC8202SDR 2004FA0000932Angle · corrodedLEFT WING NACELLE, ANGLE JUST AFT OF FIREWALL EXHIBITED SEVERE CORROSION. CORROSION WAS TRANSFERED TO UPPER WING SKIN AND FUEL CELL.Dec 13, 2004 · N717LR · Cessna 421CSDR 04FDEA03370Structure · brokenDURING AIRPLANE'S CONVERSION FROM P-F/ACF, FOUND ON RT WING LWR SIDE XORS 309, B/T REAR SPAR AND HINGE FLAP, 5 EA TL WITH HEAD BROKEN AND 1 EA WITH HIGH SUSPECT CORROSION BELOW SKIN. REMOVE EAS TL WITH HEAD BROKEN PER SRM 51-34-01 PAG 1-7. PERFORM ULTRASONICDec 6, 2004 · N559FE · Doug DC1010SDR 04FDEA03313Support Bracket · corrodedRT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4. ORIGINAL DIAMATER = 1.094, FINAL DIAMETER = 1.149, AND FABRICATED BUSHING INSTALLED AS PER FEDEX EA 1-5750-779Dec 1, 2004 · N577FE · Doug MD11SDR 04FDEA03311Support Bracket · corrodedRT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT INBOARD HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4. ORIGINAL THICKNESS=0.505, REMAINING THICKNESS=0.495, MATERIAL REMOVED=0.010 AND REPAIRED AS PER FEDEXDec 1, 2004 · N577FE · Doug MD11SDR 04FDEA03310Support Bracket · corrodedRT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT OUTBOARD HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4. ORIGINAL THICKNESS=0.510, REMAINING THICKNESS=0.506, MATERIAL REMOVED=0.004 AND REPAIRED AS PEDec 1, 2004 · N577FE · Doug MD11SDR CA041209006Strap · corroded(CAN) DURING REPLACEMENT OF LOWER SPAR CAP, WE WERE ADVISED THAT AN NEW AD IS PENDING AND WILL BE ISSUED IN JANUARY 2005 TO ADDRESS A CORROSION PROBLEM WITH THE PART NUMBERS. THE STRAPS WERE REMOVED AND EXTENSIVE CORROSION WAS FOUND UNDER THE STEEL STRAPS ON TNov 24, 2004 · Gulstm 690ASDR MALA040833Intercostal · chafedDURING C-CHECK INSPECTION IN YYC, INTERCOSTAL UNDER RT AILERON QUADRANT CHAFED. MAINTENANCE REPAIRED INTERCOSTAL IAW EO NR A53206. REFER TO 409 NR 224428 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURNED TO SERVICE 11/23/04.Nov 23, 2004 · N502XJ · Bac AVRO146RJ85ASDR UPS04843541Gusset · crackedCRACKED GUSSET IN LT WING CENTER L/E NEAR XW371. REMOVED CRACKED GUSSET REF SRM 51-1-21. FAB REPLACEMENT FROM SHT 7075T6-.063 REF DWG5769589 AND SRM 51-1-8. INSTALLED GUSSET REF SRM 51-1-21.Nov 19, 2004 · N744UP · Doug DC871FSDR 04FDEA03098Skin · wornDURING AIRPLANE'S CONVERSION FROM P-F/ACF, FOUND ON LT WING FIX TE LWR SKIN WORN STA XORS 270 . REPLACE SKIN PER SRM 513501 PAGE 1-12.Nov 12, 2004 · N559FE · Doug DC1010SDR USAA040875Flange · crackedFUEL PLATE FLANGE, (2 EA) .189 INCH IN LENGTH, CRACK (2) FUEL PANEL NR 881, 17R, 6 O`CLOCK AND 12 O`CLOCK POSITIONS. STOP DRILLED CRACKS, TRIMMED SKIN PANEL, INSTALLED FILLER AND DOUBLER IAW EA 79453.Nov 11, 2004 · N352US · Boeing 737301SDR 2004FA0000910Screw · brokenWHILE REMOVING THE JURY STRUTS BEFORE REMOVING THE WINGS FOR RECOVER, WHEN THE BOLT HOLDING THE JURY STRUT TO THE ADJUSTING SCREW AT THE FRONT SPAR WAS REMOVED THE ADJUSTING SCREW WAS IN TWO PIECES. THE EAR THAT IS WELDED TO THE SCREW BROKE JUST ABOVE THE WELNov 7, 2004 · N5031M · Tcraft BC12DSDR ASOA04930Housing · corrodedDURING C-CHECK INSPECTION, CORROSION BEYOND LIMITS WAS FOUND ON THE FLANGE HOUSING AT 522CT. MAINTENANCE REPAIRED THE CORRODED FLANGE HOUSING ON THE RT WING IAW SRM 57-14-12.Nov 2, 2004 · N630AS · Aerosp ATR72212SDR MALA040792Intercostal · damagedDURING C-CHECK IN YYC, MAINTENANCE FOUND INTERCOSTAL ABOVE LEFT AILERON CABLE COMPENSATOR DAMAGED. MAINTENANCE REPAIRED IAW EO A53206. AIRCRAFT RETURNED TO SERVICE 11/08/04.Oct 28, 2004 · N521XJ · Bac AVRO146RJ85ASDR USAA040858Bracket · crackedBRACKET, 1 INCH CRACK, LT WING SPAR (AFT) STA 218, MFG NEW BRACKET IAW J020-37-20.Oct 19, 2004 · N352US · Boeing 737301SDR IXXA060056SStrap · crackedDURING ROUTINE C CHECK, FOUND LEFT WIND CENTER LEADING EDGE RIB SUPPORT STRAP CRACKED AT STATION XFS 347.750. REMOVE DAMAGED STRAP. FABRICATED NEW STRAP, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED NEW STRAP AND FASTENERS AT LEFT WING CENTER LEADINOct 16, 2004 · N825BX · Doug DC871FSDR IXXA060057SStrap · crackedDURING ROUTINE C CHECK, FOUND LEFT WIND CENTER LEADING EDGE RIB SUPPORT STRAP CRACKED AT STATION XFS 366.500. REMOVE DAMAGED STRAP. FABRICATED NEW STRAP, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED NEW STRAP AND FASTENERS AT LEFT WING CENTER LEADINOct 16, 2004 · N825BX · Doug DC871FSDR MALA040801Rib · crackedDURING 6Y/4Y INSPECTION IN LAN, MAINTENANCE FOUND PANEL 612AR 4 CRACKED RIBS. MAINTENANCE REPAIRED IAW SRM 57-10-30-2. AIRCRAFT RETURNED TO SERVICE 10/12/04.Oct 11, 2004 · N449XJ · Saab 340BSDR 04FDEA02906Support · corrodedBORE CORRODED RIGHT WING INBOARD FLAP OUTBOARD HINGE LOWER SWIVEL BEARING. REMOVED CORROSION IAW DACCMM 57-44-07. ORIGINAL BORE 2.530 INCH FINAL 2.543 INCH MATERIAL LOSS .013 INCH. FABBED BUSHING IAW DACCMM 57-44-07 AND EA8-5750-81474. PERFORMED MPI IAW DPOct 11, 2004 · N392FE · Doug MD1010FSDR 04FDEA02905Support · corrodedRIGHT WING INBOARD FLAP OUTBOARD HINGE LOCATION NR 1 INBOARD AND OUTBOARD LUG HAS CORROSION. REMOVED CORROSION IAW DACCMM 57-44-07. FOUND TO BE STRUCTURALLY ACCEPTABLE IAW EA8-8750-81474. ALODINED AND PRIMED LUG FACES IAW DC10 SRM 51-21-01 VOLUME II. BEGINOct 11, 2004 · N392FE · Doug MD1010FSDR UPS04843450Intercostal · crackedINSPECTION TYPE: C3, RT WING CENTER L/E INTERCOSTAL IS CRACKED AT XFS 387.750. STOP DRILLED CRACK AT STA XFS 387.750 IAW SRM 57-02-00-0 FIG 002. FABRICATED & INSTALLED REPAIR ANGLES IAW SRM 57-02-00-0 FIG 2 & DC-8 SRM 51-1-20D.Oct 10, 2004 · N755UP · Doug DC871FSDR UPS04843451Channel · crackedINSPECTION TYPE: C3, LT WING LEADING CENTER SECTION LOWER SUPPORT U-CHANNEL HAS A CRACK AT AFT 2 FASTENERS 2 INCHES LONG STA XFS 510. STOPPED DRILLED CRACK IAW SRM 57-02-00-0. FABRICATED AND INSTALLED REPAIR ANGLE IAW DWG 5770375 AND DC-8 SRM 51-1-21 & 51-1Oct 9, 2004 · N755UP · Doug DC871FSDR IXXA060054SSupport Fitting · crackedDURING ROUTINE C CHECK, FOUND LEFT WING FLAP CANOE FITTING UPPER SUPPORT CRACKED AT STATION XRS 235. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED FITTING. FABRICATED NEW SUPPORT, LOCATED, DRILLED, TRIMMED, TEREATED, PRIMED, INSTALLED NEW SUPPORT AND FASTWENEROct 4, 2004 · N825BX · Doug DC871FSDR GTIA040833Channel · corrodedLT WING L/E STA XRS 240 AFT L/E FLANGE ACCESS PANEL ATTACHED HAS CORROSION AT GANG CHANNEL. REMOVED CORRODED GANG CHANNEL, INSTALLED NEW GANG CHANNEL IAW SRM 51-30-2.Sep 29, 2004 · N823NK · Doug DC982SDR UPS04443315Fitting · crackedINSPECTION TYPE:C, RIGHT BS 1241 WL 180 UPPER WING SPLICE PLATE FITTING NR 5 FASTENER HOLE CRACK REVEALED RUNNING AFT HOLE CRACK EXCEED EO LIMIT. REF NRC 6676 FOR REPLACEMENT OF SPLICE PLATE.Sep 29, 2004 · N681UP · Boeing 747121SDR 371PA0080Angle · corrodedCORROSION IN ANGLE FOR LEFT WHEEL WELL TO WING CLOSEOUT PANEL. REPLACED ANGLE PER BAC DWG 65-45687.Sep 27, 2004 · N371PA · Boeing 737306SDR EIA2004122Structure · corrodedBULGING CORROSION LEFT WING JUST AFT NR 12 K-FLAP, LOWER LEADING EDGE AT FIXED COMPOSITE FAIRING. SUSPECT INT METAL STRAP CORROSION. REMOVED CORROSION PER SRM 51-10-01, REWORK AREA 3 IN LONG BY .5 IN WIDE, BY 0.04 IN DEEP IS OUT OF SRM 57-20-01, FIG 1 LIMIT.Sep 22, 2004 · N477EV · Boeing 747SR46SDR EIA2004109Splice · crackedLEFT WING UPPER SIDE OF BODY SPLICE, LT WING AT REAR SPAR OPEN HOLE NR 4 FOUND CRACK. HOLE CONCENTRICALLY REAMED 1.375 IN DIAMETER IN SPLICE FITTING ONLY. OPEN HOLE HFEC INSP PERFORMED. FREEZE PLUG FAB'D AND INSTALLED COMMON TO SPLICE FITTING ONLY PER SRM 5Sep 20, 2004 · N477EV · Boeing 747SR46SDR UIEA200400159Support · crackedDURING OVERNIGHT, EXTERNAL IMPACT BY A FOREIGN OBJECT CAUSED BY A TORNADO. AN INSPECTION OF THE AIRCRAFT WAS CARRIED OUT AND IT WAS OBSERVED THAT AT BS 1034 RBL 104, THE UNDERWING FAIRING SUPPORT LOWER CHORD WAS CRACKED AT THE OUTBOARD FLANGE. THE LONGITUDINSep 20, 2004 · N505MC · Boeing 7472D3BSDR SWAA042705Angle · crackedDURING SCHEDULED 5Y CHECK, FOUND LT WING SUPPORT ANGLE AT REAR SPAR PANEL BETWEEN SPOILER NR 5 AND SPOILER NR 6, CRACKED. REMOVED AND REPLACED ANGLE PER SRM.Sep 16, 2004 · N751SW · Boeing 7377H4SDR UPS04843137Doubler · crackedINSPECTION TYPE:C3, UPON REMOVAL OF STUB WING NR 4 FOUND AT TRAILING EDGE OF STUB WING INTERNAL DOUBLER CRACKED AT STA XW406 RIGHT WING. REPAIRED NR 4 STUB WING INTERNAL DOUBLER IAW DC-8 SRM 57-2-0 FIG 2.Sep 14, 2004 · N772UP · Doug DC871FSDR GAIA04124Support · crackedDURING C-CHECK INSPECTION FOUND RT WING FRONT SPAR WS 726, NR 8 SLAT ACTUATOR OB PLATE TRUNNION SUPPORT CRACKED. REF FASI NR 86620, REMOVED AND REPLACED NR 8 SLAT SUPPORT PLATES IAW SB 57-0130, REV 3.Sep 10, 2004 · N180AX · Boeing 727222SDR GAIA04119Support Angle · crackedDURING C-CHECK INSPECTION FOUND PANEL SUPPORT ANGLE CRACK, RT WING L/E STA 130. REF FASI NR REMOVED, FABRICATED AND REINSTALLED PANEL SUPPORT ANGLE IAW SRM 57-20-2, FIG 1.Sep 10, 2004 · N180AX · Boeing 727222SDR GAIA04118Angle · crackedDURING C-CHECK INSPECTION FOUND RT WING L/E FWD STA 130 OB CHORD ANGLE CRACK. REF FASI NR 86591, STOP DRILLED CRACK AREA AND INSTALL ANGLE REPAIR IAW SRM 57-20-2, FIG 1.Sep 10, 2004 · N180AX · Boeing 727222SDR DHL2004780504Bracket · crackedDURING A "C" CHECK AT FLIGHTSTAR AIRCRAFT SERVICES IN JACKSONVILLE FLORIDA, THE FOLLOWING DISCREPANIES WERE NOTED; LT WING L/E CAVITY WS 301 HAS NR 1 KRUGER FLAP ACT OB LOWER MOUNT BRACKET CORNER CRACKED. REMOVED BRACKET, FABRICATED NEW ONE (BRACKET) FROM 707Sep 9, 2004 · N780DH · Boeing 727223SDR DHL2004801532Clip · brokenRT WING NR 4 ALT TANK CLIP BROKEN REF 505B ACCESS DOOR. REMOVED BROKEN CLIP IAW SRM 51-1-20D PG 21. FABRICATED NEW CLIP (AL2024-T3 0.050) IAW SRM 57-2-0 PG 1. CLEANED, TREATED AND APPLIED FUEL TANK COATING MATERIAL IAW SRM 51-1-12 PG 7 TO 12. INSTALLED NEWSep 8, 2004 · N801DH · Doug DC873FSDR DHL2004801506Angle · crackedITEM REF. NR. 1391: RT CTR L/E (L) ANGLE CRACKED 0.750 AT XFS 526.000. REMOVED CRACKED L ANGLE IAW SRM 51-3-0 PG. 1-2. FABRICATED NEW L ANGLE (AL 2024-T3 0.040) IAW SRM 57-2-0 PG.1. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED L ANGLE WITH NEW FASTSep 1, 2004 · N801DH · Doug DC873FSDR IXXA0500004SDoubler · crackedDURING ROUTINE C-CHECK INSPECTION PERFORMED MAJOR REPAIR IAW DC8 SRM 57-2-1 FIG 36 PG 133-134. REMOVED FASTENERS IAW DC8 SRM 51-1-21 PG 1, PERFORMED STOP HOLE ON CRACK END IAW DC8 SRM 57-2-1 PAGES 133, 134 FIG 36. FABRICATED EXTERNAL DOUBLER (AL 707576 0-160Aug 22, 2004 · N606AL · Doug DC873FSDR USAA040423Support Angle · crackedPIT - FOUND SUPPORT ANGLE CRACKED 1.125 INCH LONG, LEFT WING UPPER TRAILING EDGE PANEL SUPPORT ANGLE AT REAR SPAR STAITON 243. REPLACED SUPPORT ANGLE PER BOEING DWG 69-39228, SRM 51-10-00. (M)Aug 4, 2004 · N376US · Boeing 7373B7SDR DHL2004804534Clip · crackedITEM REF. NR. 2091: NR 1 ALT. TANK LWR SECTION INTERIOR CLIP CRACKED (STA. XRS 456.562 - 460.000, S-62L TO S-63L). REMOVED CRACKED CLIP IAW DC8 SRM 51-1-20D PG. 21. FABRICATED NEW CLIP (AL 7075-T651) IAW EA NR 5720-037, DWG 3864001. HEAT TREATED IAW DACO CP 7Jul 31, 2004 · N804DH · Doug DC873FSDR UPS04M43169Support Fitting · crackedINSPECTION TYPE: C, RIGHT WING LEADING EDGE SLAT TRACK NR 16 ROLLER SUPPORT FITTING CRACKED. RIGHT WING NR 16 SLAT TRACK REMOVED PER MM 27-80-32 R.50. RIGHT WING LEADING EDGE NR 16 TRACK FITTING REMOVED PER SRM 51-33-01, 51-35-01 V2.R35. NEW NR 16 ROLLER SUJul 16, 2004 · N277UP · Doug MD11FSDR 04FDEA02091Support · corrodedCOMPLY WITH EA 8-5740-80572 WINGS RT SUPPORT ASSY ACTUATOR AND HOLD DOWN NR 1 SPOILER CORROSION REPAIR. COMPLIED WITH EA 8-5740-80572 WINGS RT SUPPORT ASSY ACTUATOR AND HOLD DOWN NR 1 SPOILER CORROSION REPAIR AT MAE.Jul 16, 2004 · N359FE · Doug MD1010FSDR DHL2004804519Angle · crackedLEFT WING INBOARD SLOT SUPPORT ANGLE CRACKED 1.000, XILD 7095.000. REMOVED CRACKED SUPPORT ANGLE IAW SRM 51-1-21 PG 1. FABRICATED NEW ANGLE (AL 7075-0 0.063) IAWJ SRM 57-2-0 PG 1. PERFORMED HEAT TREATMENT TO NEW ANGLE IAW SRM 51-1-1 PG 1, 13, 17. PERFORMEDJul 13, 2004 · N804DH · Doug DC873F
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