JASC 5730

Service difficulty reports · 27,269

Reports filed under 5730 · Wing, Plate/Skin, 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 = '5730'
  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 IXXA0500085SDoubler · damagedDURING A ROUTINE C CHECK INSPECTION, FOUND RT WING OUTBOARD L/E INTERIM REPAIR AT STA XFS 710.000. ACCOMPLISHED MAJOR REPAIR BY REMOVING EXISTING REPAIR AND THE DAMAGED AREA. PERFORMED NDT INSPECTION. FABRICATED EXTERNAL DOULBER AND FILLER IN ACCORDANCE WITHNov 11, 2004 · N602AL · Doug DC873FSDR USAA040971Doubler · crackedPIT - Q4 - DOUBLER, .25 INCH LONG CRACKS (2 EA), RT WING FUEL PANEL REBATE PANEL NR 8817R. INSTALLED EXT DOUBLER .125 THICK IAW EA 79453.Nov 11, 2004 · N352US · Boeing 737301SDR 04FDEA03088Skin · damagedLT WING UPPER SURFACE STA XOS=772, ON PREVIOUS METAL FILLER REPAIR FOUND EXISTING BLENDOUT EXCEEDED SRM 57-10-00, VOLUME 1, FIGURE 32 SHEET. NR 2 LIMITS. BLENDOUT DIMENSION: LENGTH=1.5 INCH, WIDTH= 1.25 INCH, DEPTH=0.0052 INCH; ORIGINAL THICKNESS= 0.312 INov 11, 2004 · N618FE · Doug MD11FSDR IXXA0500110SSkin Panel · corrodedDURING A ROUTINE C CHECK INSPECTION, FOUND RT INNER WING EXTENDED LEADING EDGE SLANT PANEL UPPER CAP CORROSION DAMAGE BETWEEN STA XFS 63.500 AND XFS 107.500. MAJOR REPAIR ACCOMPLISHED BLEND OUT ON CORRODED AREA REMAINING OUT OF LIMITS IAW DC8 SRM 57-2-1 FIG 3Nov 10, 2004 · N602AL · Doug DC873FSDR USAA040967Skin · corrodedPIT - Q6 - WING SKIN CUT OUT, 1.2500 INCH X .2500 INCH AT 4 LOCATIONS, CORROSION; NO LEVEL OR TASK, RT WING BOOST PUMP CUT OUT. REMOVED CORROSION AND INSTALLED REPAIR IAW SRM.Nov 9, 2004 · N516AU · Boeing 7373B7SDR SPAA0400073Skin · corrodedCORROSION DAMAGE WAS FOUND ON THE LT UPPER WING SKIN P/N 65C17191-1 AT THE REAR SPAR AT APPROXIMATELY WS 442.0. THE CORROSION WAS REMOVED AND TRIMMED AND A REPAIR SCHEME WAS PROVIDED BY BOEING ENGINEERING. THE CORROSION AREA WAS REPAIRED PER BOEING INSTRUCTIONNov 9, 2004 · N712S · Boeing 7372Y5SDR QXEA200400746Skin · crackedPDX - RIGHT HAND WING UPPER SURFACE TRAILING EDGE APPEARS CRACKED, RIGHT HAND INBOARD END OF INBOARD MULTIFUNCTION SPOILER. REPAIRED IAW CRJ 700 MM 29-10-00-870-801-A01, SRM 51-42-06 AND SRM 51-41-21.Nov 8, 2004 · N604QX · Cndair CL6002C10SDR 04FDEA03024Skin · delaminatedLT WING OUTBOARD TE PANEL (BOTTOM SKIN - FOUND 6 LOCATIONS WITH DELAMINATION. AREAS OF DELAMINATION ARE AS FOLLOW (INBD TO OUBD): 1: 36.5 X 12, 2: 14 X 14, 3: 4 X 3, 4: 2.5 X 2.5, 5: 2 X 0.5, 6: 1.5 X 0.5 ......NOTED 2EA EXISTING REPAIRS ON UPPER SKINNov 7, 2004 · N456FE · Airbus A310SDR EIA2004141Skin · corrodedBS 1180 LBL 95-100 CENTER TANK UPPER SKIN HAS CORROSION. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PER ECRA 470-57-270-2.Nov 5, 2004 · N470EV · Boeing 747273CSDR DHL2004873516Skin · crackedLEFT OUTBOARD SLOT DOOR SKIN CRACKED 0.500, STA XS 478.897 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1, SRM 57-3-3 FIG 21. REMOVED LEFT OUTBOARD SLOT DOOR SKIN IAW SRM 51-1-21 PG 1. FABRICATED NEW SKIN (AL2024-T6 0.050) IAW SRM 57-3-3 FIG 21.Nov 3, 2004 · N873SJ · Doug DC873FSDR UPS04843524Skin · corrodedRT WING UPPER SKIN CORRODED AROUND HILOCK AT XRS554, ABOVE S54. NDT VERIFIED MATERIAL THICKNESS AT CORROSION REMOVAL SITE RANGED FROM .090-0.125. CUT OUT CORROSION SITE REF SRM 57-2-1 FIG28. FABRICATED DOUBLER AND FILLER FROM SHT7075T6-.190, MACHINED FILLERNov 3, 2004 · N798UP · Doug DC871FSDR 04FDEA03010Panel · debondedRIGHT WING PANEL NR 661 EB IS DISBONDED AT FINGER DOUBLER AT MIDDLE FASTENER HOLE. REPAIRED BY FABRICATING AND BONDING NEW INNER AND OUTER SKIN, DOUBLER AND CORE IAW DAC DWG ARC0633 AND FEDEX EA 8-5710-81508. REMOVED AND REINSTALLED HINGED PANEL 661 EB SEAL Nov 2, 2004 · N367FE · Doug DC1010SDR ASAA0480547Skin · chafedC-CHECK- LT WING L/E SURFACE HAS 7 CHAFED AREAS 5 INCHES FROM L/E AND I/B OF NR 5 L/E SLAT TRACK. REMOVED DAMAGED AREAS, THEN HFEC TREATED, PRIMED AND TOPCOATED THOSE AREAS IAW EA.Oct 30, 2004 · N969AS · Doug DC983SDR UPS04443501Skin · crackedINSPECTION TYPE:C, RT WING - CRACK FOUND ON RT WING UPPER SKIN AT BS 1241 UPPER SPLICE PLATE AREA AT HOLE NR 11 BY APPROX 0.040 INCH LONG RUNNING FWD. HOLE CRACKS REMOVED AND BUSHING FABRICATED AND INSTALLED AS PER SOPM 20-50-03 AND WORK PROCESS CARD UW653051Oct 30, 2004 · N521UP · Boeing 747200SDR CALA0400690Skin · crackedINSPECTION FOUND AN 8 INCH CRACK IN RT WING LEADING EDGE SKIN AT OSS 421-471. REPAIR WAS ACCOMPLISHED IAW EA 5731-01010, REV D.Oct 29, 2004 · N67134 · Boeing 757224SDR CALA0400689Skin · crackedINSPECTION FOUND A 6.5 INCH CRACK IN LT WING LEADING EDGE SKIN AT OSS 421 T0 471. REPAIRED IAW EA 5731-01010, REV D.Oct 29, 2004 · N19136 · Boeing 757224SDR AMTA200401328Skin · chafedRT WING LWR SKIN, 2 INCHES AFT OF FUEL ACCESS PANEL 641DB, SKIN CHAFED. REWORKED LOWER SKIN AT FUEL ACCESS PANEL 641DB, SKIN CHAFED WAS REPAIRED IAW SRM 57-20-01 AND ER 04-3910.Oct 27, 2004 · N522AT · Boeing 75723NSDR CA041025003Skin · corroded(CAN) DURING A ROUTINE HEAVY MAINTENANCE INSPECTION WIDESPREAD LEVEL ONE CORROSION WASFOUND ON THE UPPER WING SKIN AT THE MATIN SURFACES OF THE FORWARD AND REAR SPARS. INITIALLY LEVEL ONE CORROSION WAS FOUND JUST AHEAD OF THE REAR SPAR AND JUST AFT OF THE FORWOct 25, 2004 · Dhav DHC8102SDR DHL2004755511Skin · dentedDURING A C-CHECK, DENT RIGHT WING L/E WS 650. CUT OUT DAMAGED AREA SIZE 2 X 1 INCH ON RT WING L/E WS 650 IAW B727 SRM 51-10-1. FABRICATED REPAIR DOUBLER FROM 2024-T3 .063 SIZE 6 X 6 INCH PO 90024 IAW B727 SRM 57-30-4 FIG 1. TREATED, PRIMED PART AND AREA IAWOct 21, 2004 · N755DH · Boeing 727225SDR A6WA200460049Skin · damagedCHAFE DAMAGE TO THE LT WING UPPER SKIN MAX DEPTH OF DAMAGE IS .028 INCH. MAINTENANCE REQUESTED REPAIR FROM AVMAX FAX 608-2049001.Oct 21, 2004 · N608AW · Bac 146200ASDR ASOA04810Skin Panel · crackedDURING A C-CHECK, THE RT WING PLANK AT APPROXIMATELY WS 148 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE RT WING PLANK AT APPROXIMATELY WS 148 IAW EO600-57-0134A.Oct 21, 2004 · N824AS · Cndair CL6002B19SDR P5CA0401256Skin · corrodedRT WING UPPER SKIN HAS CORROSION AT WING STATION 697 MID SPAR. BLENDED OUT CORROSION, WITHIN LIMITS IAW SRM 57-30-01 AND 57-30-03.Oct 19, 2004 · N858FT · Boeing 747123SDR P5CA0401257Skin · delaminatedRT WING FIXED L/E UPPER SKIN B/W WING STATION 570 AND 600 LWR SURFACE DELAMINATED. REMOVED PANEL REPAIRED AND REINSTALLED IAW SRM 51-30-02.Oct 19, 2004 · N858FT · Boeing 747123SDR 2004F00416Skin · crackedDURING MAINTENANCE WORK ON THE LT CENTER WING LOCKER BAY COMPARTMENT FUEL TANK, MAINTENANCE FOUND A WING SKIN CRACK OF 3.0 INCH AT APPROX WING STATION 60.00 AND FUSELAGE STATION 54.00. THE CRACK RUNS NEAR THE LT LANDING GEAR UP AND DOWN MECHANISM SUPPORT STRUCOct 18, 2004 · N134JR · Cessna 310RSDR P5CA0401262Skin · delaminatedLEFT WING STATION 382 UPPER SURFACE ON TOP PANEL BY STRUT DELAMINATED & CRACKED. REMOVE PANEL & REBONDED, REINSTALLED PER SRM 51-10-09.Oct 17, 2004 · N858FT · Boeing 747123SDR 417011Access Panel · debondedWING FUEL PANELS HAVE A FOAM FILLER BLOCK AND SEALANT TO PREVENT WATER FROM BEING TRAPPED AT PANELS. THE SEALANT HAD TORN FREE AND THE FOAM BLOCK WAS FLOATING LOOSE IN THE TANK FROM ONE PANEL AND WAS LOOSE FROM A SECOND PANEL BUT WAS NOT FREE IN THE TANK YET.Oct 15, 2004 · N767TP · Piper PA46500TPSDR 04FDEA02933Skin Panel · crackedRT WING LEADING EDGE SKIN PANEL W/ STA XORS = 799 FOUND WITH APPROXIMATELY 13 INCH CRACKED. RIGHT WING LEADING EDGE SKIN PANEL W/ STA XORS = 799 CRACKED . REPAIR CARRIED OUT AS PER FEDEX EA 1-5710-79779, TITLE: WINGS, BASIC WING STRUCTURE, RIGHT LEADING EDGOct 14, 2004 · N595FE · Doug MD11FSDR IXXA060015SSkin · crackedDURING ROUTINE C CHECK, FOUND RIGHT WING UPPER SKIN CRACKED AT STATION XFS 132.250. REMOVED FASTENERS AS NEEDED TO PERFORMED REPAIR. REMOVED DAMAGE. FABRICATED DOUBLER AND FILLER, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED DOUBLER, FILLER AND NEWOct 11, 2004 · N825BX · Doug DC871FSDR IXXA060013SSkin · crackedDURING ROUTINE C CHECK, FOUND RIGHT HAND WING SKIN CRACKED AT STATION 143.000. REMOVED FUEL DUCTS. REMOVED FASTENERS AS NEEDED. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED NEW REPAIR PARTS AND FASTENERS WETOct 11, 2004 · N825BX · Doug DC871FSDR IXXA0500066SPlate · damagedDURING A ROUTINE C CHECK INSPECTION, FOUND LT WING EXTENDED LEADING EDGE OUTBOARD VANE PLATING INTERIM REPAIR STA XOLDO 67.000. REPAIR ACCOMPLISHED REMOVAL OF FASTENERS AND EXISTING INTERIM REPAIR. REMOVED THE DAMAGED SKIN AREA AND PERFORMED NDT INSPECTION. Oct 11, 2004 · N606AL · Doug DC873FSDR IXXA0500065SPlate · damagedDURING A ROUTINE C CHECK INSPECTION, FOUND LT OUTER WING OUTBOARD EXTENDED LEADING EDGE PLATING WITH INTERIM REPAIR AT STA XFS 710.000. REPAIR ACCOMPLISHED REMOVAL OF ALL FASTENERS WITHIN THE REPAIR AREA AND THE EXISTION INTERIM REPAIR. REMOVED THE DAMAGED SOct 11, 2004 · N606AL · Doug DC873FSDR IXXA0500049SSkin · damagedDURING A ROUTINE C CHECK INSPECTION, RT WING INBOARD VANE SLOT HAS INTERIM REPAIR AT STA XILD 7095.00. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED SECTION. PERFORMED NDT INSPECTION. FABRICATED EXTERNAL REPAIR DOUBLER, FILLER, AND INTERNAL DOUBLER. CLEANED, TREATOct 11, 2004 · N606AL · Doug DC873FSDR UPS04543334Panel · bird strikeBIRD STRIKE LEFT WING LWR INBOARD SURFACE PANEL. DAMAGE MEASURED MORE THAN 8 INCHES DIAMETER DELAMINATION 511FB. REMOVED PANEL 511FB FOR REPAIR TD0559172. REINSTALLED SAME PANEL WITH SERVICEABLE REPAIR FROM SIA. OK FOR SERVICE.Oct 11, 2004 · N437UP · Boeing 75724APFSDR P5CA0401245Panel · crackedRIGHT WING I/B FIXED T/E LWR PNL, I/B EXTENDED CHORD HAS CRACK 2 INCHES LONG AT WS 440. REMOVE CHORD INSTALLED NEW CHORD AS PER SRM 51-30-02.Oct 11, 2004 · N858FT · Boeing 747123SDR 04FDEA02901Skin · corrodedLEFT WING SKIN LOWER SURFACE IS CORRODED, STATION XORS 799 APPROX 19 INCHES AFT OF FORWARD SPAR CAP. SKIN HAS SMALL AMOUNTS OF PITTING. REMOVED CORROSION AND FOUND TO BE WITHIN LIMITS IAW EA 8-5710-81493. ORIGINAL MATERIAL THICKNESS IS .096 INCH, REMOVED .0Oct 11, 2004 · N392FE · Doug MD1010FSDR IXXA060020SSkin · crackedDURING ROUTINE C CHECK FOUND LEFT HAND WING UPPER SKIN CRACKED AT STATION XRS 22.7 AT CENTER SPAR. REMOVED ALL FASTENERS COMMON TO REPAIR AREA. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW REPAIR PARTOct 10, 2004 · N825BX · Doug DC871FSDR COMA0460567Skin · crackedCRACK FOUND ON RIGHT WING PLANK. PERFORMED CRJ REO 601R-57-21-130.Oct 7, 2004 · N912CA · Cndair CL6002B19SDR COMA0460563Skin · crackedCRACK FOUND ON RIGHT WING PLANK. PERFORMED CRJ REO 601R-57-21-130.Oct 7, 2004 · N912CA · Cndair CL6002B19SDR IXXA060023SSkin · corrodedDURING ROUTINE C CHECK, FOUND THE LT WING UPPER SURFACE CORRODED AT STATION XFS304. REMOVED LEFT WING CENTER SECTION LEADING EDGE TO FACILITATE REPAIR. REMOVED DAMAGE. FABRICATED FILLER AND DOUBLER. LOCATED, DRILLED, REMOVED, TREATED, PRIMED, AND INSTALLEDOct 6, 2004 · N825BX · Doug DC871FSDR IXXA060022SSkin · corrodedDURING ROUTINE C-CHECK FOUND LT WING UPPER SURFACE CORRODED BEOND LIMITS AT STATION XRS111.000 AT FORWARD SPAR. REMOVED FASTENERS AS NEEDED. REMOVED DAMAGE. FABRICATED REPAIR DOUBLER, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW REPAIR DOUBLEROct 6, 2004 · N825BX · Doug DC871FSDR UPS04243382Skin · crackedINSPECTION TYPE: C, SUSPECT CRACK AT FWD UPPER CORNER OF LEFT WING ICE LIGHT CUTOUT. HFEC CARRIED OUT ON ABOVE AREA IAW B727 NDTM 51-00-00 PT 6 FIG 4, CRACKS CONFIRMED, ENDS MARKED. DOUBLER AND FILLER INSTALLED IAW SRM 53-30-03. WEIGHT OF REPAIR 2.37 LBS.Oct 5, 2004 · N954UP · Boeing 727185CSDR IXXA060188SFillet · delaminatedDURING ROUTINE C CHECK, FOUND LEFT WING FILLET PANEL (NUMBER 1612) DELAMINATED. REPLACED PANEL PER ALL APPLICABLE DATA.Oct 4, 2004 · N41CX · Doug DC862FSDR IXXA0500214SCloseout Panel · corrodedDURING ROUTINE C-CHECK FOUND AFT WING FILLET PANEL NUMBER 161X SKIN DISBONDED AND CORRODED. FABRICATED NEW PANEL, LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED NEW FILLET PANEL IAW COOPESA EO COO-8-53-431-04.Oct 4, 2004 · N825BX · Doug DC871FSDR ASAA0480531Access Panel · leakingOKC - C-CHECK, EVIDENCE OF FUEL LEAK FROM RT WING LOWER DOORS, NR 5 AND NR 7, FROM IB ENSURED HOLE CLEAN AND ROUND, TOUCH COUNTER SUNK, NDT FOR CRACKS. INSTALLED AD RIVET AND SHAVED BOTH SIDES OF REPAIR IAW EA 5710-01109 AND EA 10575.Oct 2, 2004 · N973AS · Doug DC983SDR ASAA0480530Access Panel · leakingOKC - C-CHECK, EVIDENCE OF FUEL LEAK FROM RT WING LOWER DOORS NR 5 AND NR 7 FROM IB. REMOVED PANEL, ORDERED AND INSTALLED NEW PANEL IAW MM 28-00-00.Oct 2, 2004 · N973AS · Doug DC983SDR P5CA0401231Skin · delaminatedRT WING L/E UPPER SKIN BETWEEN WING STATIONS 445-476 LOWER SURFACE IS DELAMINATED. REMOVED PANEL & SENT TO COMPOSITE SHOP, REPAIRED & REINSTALLED PER SRM 51-40-09.Oct 1, 2004 · N858FT · Boeing 747123SDR 04FDEA02859Panel · delaminatedPANEL 66CT HAS SEVERAL AREAS OF DELAMINATION. REPAIRED BY REMOVING DAMAGE, FABRICATING AND BONDING NEW SKIN, CORE AND DOUBLERS IAW DAC DWG ARC0627 AND EA 8-5710-77619, REFERENCE NON-ROUTINE N00129.Oct 1, 2004 · N68058 · Doug DC1010FSDR DHL2004801550Skin · damagedITEM REF. NR. 2127: RT CTR L/E HAS INTERIM REPAIR AT XFS 304.000 (LWR. PART). PERFORMED MAJOR REPAIR IAW DWG W51-R10, FAA FORM 8110-3 DATED 09-28-2004. REMOVED INTERIM REPAIR IAW DC8 SRM 51-1-21 PG.1, SRM 51-1-20D PG.21, DC8 SRM 51-3-0 PG.1, DWG W51-R10. PERFOSep 30, 2004 · N801DH · Doug DC873FSDR UPS04443323Skin · crackedINSPECTION TYPE:C, RT BS 1241 WL 178 WING REAR SPAR UPPER SPLICE FITTING AREA FOUND HOLE NR 7 CRACKED AT WING UPPER SKIN. HOLE CRACK REWORKED AND OVERSIZED AS PER EO 5740-17032-B.Sep 30, 2004 · N681UP · Boeing 747121SDR UPS04443320Skin · crackedINSPECTION TYPE:C, RIGHT BS 1241 WL 178 WING REAR SPAR UPPER SPLICE FITTING AREA FOUND HOLE NR 11 CRACKED AT WING UPPER SKIN. CRACKED HOLE REWORKED AND OVERSIZED AS PER EO B747-5740-17032.Sep 30, 2004 · N681UP · Boeing 747121
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