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"

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SDR CALA0300464Skin · crackedINSPECTION FOUND A 1 INCH CRACK IN RT WING LEADING EDGE SKIN AT NR 4 SLAT ACTUATOR. A REPAIR DOUBLER WAS INSTALLED IAW SRM 57-41-01.Aug 11, 2003 · N70330 · Boeing 7373T0SDR 2003FA0000824Skin · corrodedWHILE COMPLYING WITH AD NR 2002-26-02 ON THE WING CENTER SECTION OF THIS ERCOUPE WE FOUND SEVERAL SPOTS THAT WERE WELL BEYOND LIGHT CORROSION AND HAD PROGRESSED INTO THE EXFOLIATION STAGE. WE ENDED UP REMOVING THE BOTTOM SKIN ON THE RIGHT WALKWAY TO REPLACE 2 Aug 11, 2003 · N6620W · Univar A2ALONSDR DHL2003805593Skin · corrodedRIGHT OUTER WING INBD L/E UPPER SKIN SURFACE CORRODED STA XFS 568.000 - 633.750 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 44. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-Aug 8, 2003 · N805DH · Doug DC873FSDR DHL2003805573Skin · corrodedLEFT WING CTR L/E CORRODED FROM STA XFS 297.500 - XFS 310.250 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 44. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 5Aug 7, 2003 · N805DH · Doug DC873FSDR 03FDEA01363Skin · corrodedRIGHT WING UPPER SURFACE AT OUTBOARD OF OUTBOARD AILERON FOUND WITH MINOR CORROSION. RT WING UPPER SURFACE AT OUTBD OF OUTBD AILERON MINOR CORROSION REMOVED AS PER FEDEX EA 1-5710-71785 - WINGS - WING STRUCTURE - RT UPPER SURFACE CORROSION.Aug 7, 2003 · N596FE · Doug MD11SDR DHL2003805565Plate · damagedELONGATED HOLES IN UPPER PLATING OF LEFT WING CTR L/E STA XS 520.168. PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1, SRM 57-3-3 PG 12. REMOVED UPPER PLATING WITH ELONGATED HOLES IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1, SRM 51-1-20D PG 21. FABRICATED NEW PLATING Aug 6, 2003 · N805DH · Doug DC873FSDR 2003F00532Skin · lightning strikeDURING A POST FLIGHT INSPECTION, FOUND EVIDENCE OF AN APPARENT LIGHTNING STRIKE ON THE TRAILING EDGE OF RIGHT WING TIP, BELOW THE WINGLET. AS PER REO 601-57-20-036, ALUMINUM TAPE APPLIED TO DAMAGED AREA. AIRCRAFT TO BE REPOSITION FROM PBI TO AGS FOR FURTHER Aug 5, 2003 · N601VH · Cndair CL6002B16SDR CALA0300448Panel · delaminatedINSPECTION FOUND LT WING L/E PANEL DELAMINATED ON UPPER SURFACE AT FSS 410. THE AREA WAS REPAIRED IAW EA 5731-01010, REV D, OP 4.Aug 5, 2003 · N12116 · Boeing 757224SDR DHL2003805589Skin · corrodedLEFT OUTER WING INBD L/E CORRODED BETWEEN STA XFS 572.250 - XFS.603.750. PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 44. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 PG 11-12. TRIMMED Aug 4, 2003 · N805DH · Doug DC873FSDR 03FDEA01205Ring · corrodedR/H WING FUEL TANK ACCESS PANEL CHAFE RING HAS PITTED CORR. REMOVED AND REPLACED CHAFE RING AND GANG CHANNEL IAW SRM 51-42-04 AND SRM 51-31-01 AT MAE ON N/R N00926Aug 3, 2003 · N311FE · Doug DC1030FSDR DHL2003805568Skin Panel · delaminatedLEFT WING T/E LWR PANEL EXTERNAL SKIN DELAMINATED (STA XW.5.000 - 90.000). REMOVED AND REPLACED PANEL ASSY ON LEFT WING T/E LWR PART STA XW 5.000 - 90.000 IAW SRM 51-3-0 PG 1.Aug 2, 2003 · N805DH · Doug DC873FSDR CALA0300429Panel · delaminatedINSPECTION FOUND LT WING O/B TRAILING EDGE PANEL DELAMINATED. A NEW PANEL WAS INSTALLED IAW SRM 51-40-02.Jul 31, 2003 · N17316 · Boeing 7373T0SDR CALA0300428Skin · gougedINSPECTION FOUND A GOUGE IN LT WING FIXED L/E UPPER SKIN PANEL AT O/B END OF NR 2 SLAT. THE SKIN WAS REPAIRED IAW SRM 51-70-16 AND ECRA 5721-01048.Jul 31, 2003 · N16642 · Boeing 737524SDR DHL2003805567Skin · corrodedLEFT WING CTR L/E CORRODED BETWEEN STA XFS 422.750 AND XOLDI-6.225 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 38. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 PG 11-12.Jul 30, 2003 · N805DH · Doug DC873FSDR DHL2003805592Skin · corrodedRIGHT WING CTR L/E UPPER SKIN CORRODED AT XFS 423.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 38. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 PG 11-12. TRIMMED OUTJul 29, 2003 · N805DH · Doug DC873FSDR MWEA030294Skin · corrodedRIGHT WING APPEARS TO BE BURNT OR CORRODED NEAR NR 3 STATIC WICK ON LOWER WING SURFACE. FABRICATED AND INSTALLED NEW SKIN AND DOUBLER.Jul 28, 2003 · N809ME · Doug DC982SDR COMA0360335Skin · crackedFOUND LOWER LEFT WING PLANK CRACKED AT WS 148.019 DURING EO 57-014. PERFORMED TEMPORARY REPAIR AND DEFERRED PER REO 601R-57-21-138Jul 27, 2003 · N936CA · Cndair CL6002B19SDR COMA0360334Skin · crackedFOUND LOWER RIGHT WING PLANK CRACKED AT WS 148.019 DURING EO 57-014. PERFORMED TEMPORARY REPAIR AND DEFERRED PER REO 601R-57-21-138Jul 27, 2003 · N936CA · Cndair CL6002B19SDR EIA2003096Doubler · crackedCRACK ON DOUBLER OF 1241 WEB APPROX LBL 80 ABOVE LOWER CHORD. REMOVED AND REPLACED DOUBLER PER B747 SRM 57-30-2 AND ECRA 485-53-151-2.Jul 24, 2003 · N485EV · Boeing 747212BSDR 03FDEA01161Skin · bulgedRT WING PANEL AT STA XORS 1042 REAR SPAR SKIN BULGE. RT WING PANEL AT STA XORS 1042 REAR SPAR SKIN BULGE REPAIRED AS PER FEDEX EA 1-5720-69399 - WINGS - OUTER WING - RH REAR SPAR/TRAILING EDGE CORROSION REWORK.Jul 22, 2003 · N605FE · Doug MD11SDR UPS03841029Skin · corrodedINSPECTION TYPE: C2, RT WING UPPER SKIN HAS INTERGRANULAR CORROSION BETWEEN XFS 195 TO XFS 220.190. CUT OUT DAMAGE, FABRICATED AND INSTALLED DOUBLER AND FILLER IAW EO DC8-5720-7767-A AND SRM 57-3-3 FIG 3.Jul 22, 2003 · N874UP · Doug DC873FSDR UPS03841026Doubler · corrodedINSPECTION TYPE:C2 RIGHT WING LOWER SKIN DOUBLER AT XW 408 IS CORRODED BEYOND LIMITS BETWEEN CENTER AND REAR SPAR. REMOVED, FABRICATED AND INSTALLED DOUBLER IAW DWG 3887776 AND SRM 51-1-20D.Jul 22, 2003 · N874UP · Doug DC873FSDR AUS20030761Access Panel · leaking(AUS) FUEL LEAKING FROM WING AND RUNNING OVER UPPER SURFACE OF INBOARD FLAPS. INVESTIGATION FOUND THE FUEL LEAKING FROM THE FUEL TANK PANEL ACCESS DOOR AT LOWER WING SKIN CUTOUT NR 7404R LOCATED BETWEEN WBL 157 AND WBL 183.4. THE FUEL TANK CUTOUT HAD BEEN RECEJul 20, 2003 · Boeing 737376SDR GAIA03048SPSkin · debondedDURING C-CHECK, FOUND RT WING LOWER TRAILING EDGE PANEL 8605 HAS DISBONDED SPOT OUTER SKIN. CUT OUT 3 INCHES BY 48 INCHES, FABRICATED FILLER 3 INCHES BY 48 INCHES, LOWER DOUBLER 3 INCHES BY 48 INCHES 2024 T-3 .016 UPPER DOUBLER 4.5 BY 50 INCHES 2024 T-3 .020,Jul 19, 2003 · N281KH · Boeing 7272J0SDR SWIA200312288Skin · crackedRT LWR WING PLANK WS 148 CRACKED. DISCOVERED DURING C-CHECK, REPAIRED DAMAGED AREA IAW CRJ REO 601R-57-21-130 REV 'D'.Jul 19, 2003 · N590SW · Cndair CL6002B19SDR SWIA200312287Skin · crackedLT LWR WING PLANK WS 148 CRACKED. DISCOVERED DURING C-CHECK, DAMAGED AREA REPAIRED IAW CRJ REO 601R-57-21-130 REV 'D' & 601R-57-21-131 REV 'NC'.Jul 19, 2003 · N590SW · Cndair CL6002B19SDR ABXA030311Skin · corrodedMAIN CARGO COMPARTMENT CORROSION ON CENTER WING UPPER SKIN AND DOUBLER FROM FS 760 - 855, LEFT BUTTLINE 3 - 23. REMOVED CORROSION, FABRICATED REPAIR DOUBLER AND BUSHINGS, ALODINED, PRIMED, INSTALLED AND LEAK CHECKED IAW REA D857-47555MR AND REA D857-47547MR, Jul 19, 2003 · N819AX · Doug DC863FSDR 2003FA0001044Skin · corrodedDURING A C-CHECK INSPECTION, CORROSION WAS FOUND ON LOWER SURFACE OF CENTER WING, CENTER SECTION, WHICH FORMS THE UPPER WALL OF THE RAM AIR DUCT USED FOR COOLING OF THE AIR CONDITION SYSTEM ABOVE LEFT PLENUM CHAMBER ASS AT LBL 20 AND STIFFENER 5. DURING CORROJul 15, 2003 · N521DB · Boeing 727243SDR DHL2003873602Skin · damagedRT WING EXTENDED L/E I/B VANE HOLES ELONGATED AT STA XS.247 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW EODHL-0306029, ED-3468. REMOVED FASTENERS, TRIMMED OUT THE ELONGATED HOLES SKIN AREA, PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 6-10-01-001. CLEANED, Jul 10, 2003 · N873SJ · Doug DC873FSDR 03FDEA01102Skin · corrodedRT WING UPPER SURFACE FOUND CORROSION AT BETWEEN XORS799.4 AND XORS826.5 FWD OF FIXED PANEL. RT WING UPPER SURFACE CORROSION AT BETWEEN XORS799.4 AND XORS826.5 FWD OF FIXED PANEL REPAIR CARRIED AS PER FEDEX EA 1-5720-69365 WINGS OUTER WING / RT OUTER AFT SKINJul 9, 2003 · N618FE · Doug MD11SDR DHL2003873601Skin · corrodedRT OUTER WING INBD EXTENDED L/E OUTER PLATING SHOWS CORROSION & ELONGATED HOLES AROUND STA XFS 710 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS, REMOVED CORROSION, FOUND OUT OF LIMITS. TRIMMED OUT THE CORRODED SKIN AREA. PERFORMED NDT INSPECTIJul 9, 2003 · N873SJ · Doug DC873FSDR SWAA031517Skin · crackedDURING SCHEDULED C2 CHECK, FOUND LT WING SKIN CRACKED AT INBD FIXED L/E JUST OUTBD OF KRUGER FLAP. REPAIRED SKIN PER SWA EA.Jul 9, 2003 · N342SW · Boeing 7373H4SDR DHL2003873598Skin · corrodedRT OUTER WING TOP AFT PANEL PLATING CORRODED AROUND STA XRS 728.000 S-5 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS, REMOVED CORROSION, FOUND OUT OF LIMITS IAW SRM 57-2-0 PG.16. BLENDED OUT THE DAMAGED AREA, PERFORMED NDT INSPECTION AROUND REWJul 8, 2003 · N873SJ · Doug DC873FSDR DHL2003873576Skin · corrodedRT INNER WING CTR EXTENDED L/E OUTER PLATING CORRODED ON SEVERAL AREAS, AROUND XW.257.500 (MAJOR REPAIR). PERFORMED MAJOR REPAIR, REMOVED FASTENERS, REMOVED CORROSION, FOUND OUT OF LIMITS. TRIMMED OUT DAMAGED AREA IAW EODHL-030624, ED-3448. PERFORMED NDT INJul 6, 2003 · N873SJ · Doug DC873FSDR DHL2003873615Skin · corrodedLT OUTER STUB WING OUTER PLATING UPPER SURFACE SHOWS CORROSION BETWEEN STA XFS 526 AND XW.485 (MAJOR REPAIR). PERFORMED MAJOR REPAIR, REMOVED FASTENERS, TRIMMED OUT DAMAGED SKIN AREA IAW EODHL-030630, ED-3461. PERFORMED NDT INSPECTION IAW DC8 NDTSPM 6-10-01-Jul 5, 2003 · N873SJ · Doug DC873FSDR DHL2003873600Skin · corrodedRT OUTER WING INBD L/E LOWER PLATING SHOWS CORROSION AND 2EA CRACKS 0.44 EACH ONE (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 PG 11-12. TRIMMED OUT CORRODED AND CJul 5, 2003 · N873SJ · Doug DC873FSDR DHL2003873579Skin · crackedLT WING OTBD FLAP LOWER FWD PLATING SHOWS CRACK (1.000 ) AND DENT BETWEEN STA XF.322.000 AND XF.355.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW EODHL-030620, ED-3451. REMOVED FASTENERS. TRIMMED OUT AND REMOVED THE DAMAGED SKIN SEGMENT IAW EODHL-030620, EJul 4, 2003 · N873SJ · Doug DC873FSDR DHL2003873610Skin · corrodedLT WING FUEL TANK I/B EXTENDED L/E OUTER PLATING CORRODED BTW STA XFS 207 AND XFS189 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS, TRIMMED OUT THE DAMAGED SKIN SEGMENT. PERFORMED NDT INSPECITION. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8Jul 4, 2003 · N873SJ · Doug DC873FSDR DHL2003873594Plate · corrodedN/R 1450.: RT. OUT WING OB EXTEND L/E LWR PLATING SHOWS CORR BTWN STA. XFS.710.000, XFS.722.500. PERFORMED MJR REPAIR IAW EODHL, ED-3445. RMD FASTENERS IAW SRM. REMOVED CORR IAW SRM. FOUND OUT OF LIMITS IAW SRM. TRIMMED OUT DAMAGED AREA IAW EODHL, ED-3445. PJul 4, 2003 · N873SJ · Doug DC873FSDR DHL2003873569Skin · corrodedLT WING OB L/E PLATING CORRODED BETWEEN STA XFS.710.000 AND XW.761.000. REMOVED FASTENERS. REMOVED CORROSION. FOUND OUT OF LIMITS. TRIMMED OUT DAMAGED SKIN SEGMENT IAW. PERFORMED NDT INSPECTION IAW DC8 NDTSPM PART 6-10-01-001. CLEANED, TREATED AND PRIMEDJul 4, 2003 · N873SJ · Doug DC873FSDR DHL2003873608Skin · corrodedRT OUTER WING AFT TOP PANEL PLATING AROUND STA XRS.693.000, S-3 S-5R CORRODED (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS, REMOVED CORROSION FROM DAMAGED AREA. FOUND OUT OF LIMITS. BLENDED OUT DAMAGED AREA IAW EODHL-030622, ED-3469. PERFORMEJul 3, 2003 · N873SJ · Doug DC873FSDR DHL2003873560Skin · corrodedRT OUTER WING OUTB L/E UPPER SKIN CORRODED AT STA XFS.90.000. PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG.38. REMOVED FASTENERS IAW SRM 51-1-21 PG 1 SRM 51-3-0 PG 1. REMOVED CORROSION FROM UPPER SURFACE OF RH WING OUTBD L/E SRM 51-1-8 PG 17-18. FOUND OUT OF LIMIJul 3, 2003 · N873SJ · Doug DC873FSDR QXEA200300812Skin Panel · chafedPDX - RIGHT WING INBOARD LEADING EDGE PANEL 622AR HAS CHAFE FROM CONTACT WITH SLAT LOWER EDGE, AT APPROXIMATELY WS108. REPAIRED IAW EA R-57-40.Jul 2, 2003 · N609QX · Cndair CL6002C10SDR DHL2003873597Skin · corrodedLT WING CTR L/E OUTER PLATING SHOWS CORROSION AROUND XW 257.500 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS & EXSITING DOUBLER. REMOVED CORROSION, FOUND OUT OF LIMITS. TRIMMED OUT THE DAMAGED SKIN SEGMENT. PERFORMED NDT INSPECTION IAW DC8 NDJul 1, 2003 · N873SJ · Doug DC873FSDR AUS20030661Skin · corroded(AUS) RT WING UPPER SKIN LOWER SURFACE AND STIFFENERS CONTAINED LEVEL 2 CORROSION IN THE AREA OF THE RT WING VENT TANK BETWEEN WS557 AND WS583. FOUND DURING INSPECTION IAW A-B73-5791-51.Jun 30, 2003 · Boeing 73733ASDR DHL2003873559Skin · corrodedRT WING CTR L/E PLATING CORRODED AT XFS 354.000 UPPER PART (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 44. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED CORRSION ON CTR L/E PLATING IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1Jun 28, 2003 · N873SJ · Doug DC873FSDR DHL2003873531Skin · corrodedRT OUTER WING IB L\E PLATING CORRODED, XFS.591.250 - XFS.685.000. PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 38. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED CORROSION FROM RT WING IB L\E PLATING IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 PGJun 28, 2003 · N873SJ · Doug DC873FSDR 03FDEA01065Skin Panel · corrodedMAIN DECK - BETWEEN BS 1215-1235, LEFT XCW 0-50, CENTER WING UPPER PANEL STRUCTURE FOUND CORROSION. REPAIR CARRIED OUT AS PER SRM 51-21-01 VOL 2 AND FEDEX EA 1-5720-69361 WINGS - CENTER WING/UPPER FWD AND UPPER CENTER WING SKIN PANEL - CORROSION REWORK.Jun 25, 2003 · N582FE · Doug MD11SDR 03FDEA01066Skin Panel · corrodedMAIN DECK - BETWEEN BS 1215-1235, LEFT XCW 75-115, CENTER WING UPPER PANEL STRUCTURE FOUND CORROSION. REPAIR CARRIED OUT AS PER SRM 51-21-01 VOL 2 AND FEDEX EA 1-5720-69361 WINGS - CENTER WING / UPPER FWD AND UPPER CENTER WING SKIN PANEL - CORROSION REWORK.Jun 25, 2003 · N582FE · Doug MD11SDR 03FDEA01067Skin Panel · corrodedMAIN DECK - BETWEEN BS 1215-1235, RIGHT XCW 0-50, CENTER WING UPPER PANEL STRUCTURE FOUND CORRODED. REPAIR CARRIED OUT AS PER SRM 51-21-01 VOL 2 AND FEDEX EA 1-5720-69361 WINGS - CENTER WING / UPPER FWD AND UPPER CENTER WING SKIN PANEL - CORROSION REWORK.Jun 25, 2003 · N582FE · Doug MD11
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