JASC 5730

Service difficulty reports · 27,269

Reports filed under 5730 · Wing, Plate/Skin, newest first.

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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 07FDEA03871Panel · delaminatedPREVIOUS REPAIR FOUND LOCATED ON RT WING LOWER SURFACE T/E, STA 1787/1835, RIB 29-30. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUS REPAIR EVALUATED AND FOUND DEBONDED. RT WING Aug 27, 2007 · N419FE · Airbus A310222SDR COEA0761821Skin · corrodedFOUND DURING HEAVY CHECK. MAJOR REPAIR: LEVEL 2 CORROSION AND FRETTING DAMAGE ON LT WING, UPPER WING PLANK. DAMAGE IS LOCATED AT ACCESS DOOR 522CT HOUSING AT DOOR CUTOUT. BLENDED OUT DAMAGE AND REWORKED DOOR STIFFENER IAW SRAS DO/TS 4811/07..4338 AND NOTE DAug 24, 2007 · N821FX · Aerosp ATR72202SDR COEA0748821Skin · corrodedFOUND DURING HEAVY CHECK. CORROSION ON RT WING LOWER EXTERNAL SKIN PANEL AT FUEL PUMP CUT OUT HOLE, BETWEEN RIBS 4 AND 5. BLENDED CORROSION IAW SRAS DO/ TS-806/04, 2754, NOTE DO/TS-4893/ 07. WO 72241, NR 500002. (K)Aug 24, 2007 · N821FX · Aerosp ATR72202SDR 07FDEA04318Skin · corrodedRT WING FRONT SPAR WITH CORROSION BETWEEN STA 482/RIB 8 AND STA 935/RIB 15. RT WING UPPER SKIN REPAIRED IAW FEDEX EA 6-5710-113179.Aug 24, 2007 · N419FE · Airbus A310222SDR UIEA200700324Skin · delaminatedLT WING UPPER SURFACE TRAILING EDGE FIXED PANEL AT STATION 1224 HAS AN AREA OF 2.0 INCH LONG BY 15.0 INCH WIDE AREA OF DELAMINATION. PERMANENT REPAIR OF AREA WAS ACCOMPLISHED AS PER B747-200 SRM 51-40-09 FIG 2, SHEETS 4 & 5.Aug 24, 2007 · N809MC · Boeing 747228FSDR 07FDEA03097Skin Panel · wornELONGATED HYDRAULIC FITTING HOLES IN LOWER SKIN PANEL RT. REPAIR PERFORMED BY OVERSIZING AND BUSHING OF AFFECTED HOLES IAW EA 6-5720-101266 AND RAS/BAE/1003250/2006 ISS "A".Aug 24, 2007 · N811FD · Airbus A310324SDR 07FDEA03096Skin · wornELONGATED HYDRAULIC FITTING HOLES IN LOWER SKIN PANEL LT. REPAIR PERFORMED BY OVERSIZING AND BUSHING OF AFFECTED HOLES IAW EA 6-5720-101266 AND RAS/BAE/1003250/2006 ISS "A".Aug 24, 2007 · N811FD · Airbus A310324SDR 07FDEA03086Skin · corrodedLT WING OUTBOARD FLAP CORROSION UNDER UPPER SKIN. 10-11-07 REPAIRED AREA IAW SRM 57-10-00 VOL I FIG 85.Aug 24, 2007 · N369FE · Doug DC1010FSDR 07FDEA03084Skin · deformedRT WING T/E LOWER SKIN OF ISLAND DEFORMATION. REPAIRED AREA IAW SRM 57-00-01 VOL 1 SHT 2 FIG 4.Aug 24, 2007 · N68052 · Doug DC1010FSDR SWIA200718634Access Panel · crackedLOWER FORWARD STRINGER IN LEFT WING ACCESS PANEL INBOARD OF NACELLE IS CRACKED. FOUND AT C-CHECK, REPAIRED LEFT WING STRINGER IAW SRM 57-20-103 PG 203.Aug 23, 2007 · N582SW · Emb EMB120ERSDR WRLA2007088Skin · crackedDURING 3C+12A CHECK, EGAT MECHANIC FOUND CRACK ON RIGHT HAND WING FIXED LEADING EDGE NOSE SKIN AT STA XOS=906. 09-26-07 PERFORM NDT/ET FOR REWORK AREA REF JC 0032337. REPAIR CRACK AREA PER MD-11 SRM 57-10-00 FIG.41 VOL.1 REV.40.Aug 23, 2007 · N275WA · Doug MD11FSDR 07FDEA03076Skin Panel · corrodedCORROSION AROUND OVERWING REFUELING PORT RT OUTER WING BETWEEN RIB 27-28, STRG 12-13. REPAIR PERFORMED BY BLEND OUT CORROSION, NDT INSPECTION FOR CRACK FREE IAW EA 6-5720-103253 AND RAS/BAE/1003233/2006 ISS "A".Aug 23, 2007 · N811FD · Airbus A310324SDR FDEA200708223046Skin · crackedLT WING L/E CRACK ON EXTERNAL LOWER SKIN. REPAIRED SKIN IAW SRM 57-10-00 FIG 68 VOL I.Aug 22, 2007 · N369FE · Doug MD1010FSDR FDEA200708223034Skin · crackedL/E RT WING CRACK ON EXTERNAL SKIN L/E. REPAIRED SKIN IAW SRM 57-10-00 FIG 68 SHT 2 VOL I.Aug 22, 2007 · N369FE · Doug MD1010FSDR COEA0734821Panel · corrodedFOUND DURING HEAVY CHECK. MAJOR REPAIR. CORROSION ON RT WING UPPER FIXED PANEL COMMON TO THE AILERON CENTER HINGE FITTING. REPLACED PANEL WITH NEW FABRICATED PANEL. WO 72245, NR 602006. (K)Aug 22, 2007 · N821FX · Aerosp ATR72202SDR 07FDEA03047Skin · crackedLT WING LWR SURFACE FOUND CRACK ON SKIN. REPAIRED SKIN IAW SRM 57-10-00 FIG 68 SHT 2 VOL I.Aug 22, 2007 · N369FE · Doug DC1010FSDR 07FDEA03046Skin · crackedLT WING L/E CRACK ON EXTERNAL LOWER SKIN.Aug 22, 2007 · N369FE · Doug DC1010FSDR 07FDEA03034Skin · crackedL/E RT WING CRACK ON EXTERNAL SKIN L/E .Aug 22, 2007 · N369FE · Doug DC1010SDR 07FDEA03030Skin · unknownLT WING TIP EXTERNAL DOUBLER ON SKIN. ACCOMPLISHED EA NR 8-5760-112423.Aug 22, 2007 · N68052 · Doug DC1010FSDR 07FDEA03029Skin · unknownRT WING TIP EXTERNAL DOUBLER ON SKIN. ACCOMPLISHED EA NR 8-5760-112423.Aug 22, 2007 · N68052 · Doug DC1010FSDR 07FDEA03027Skin · damagedWING BOTTOM SKIN PANEL NR 1 LT, INCOMPLETE RECORDS OF EMBODIMENT OF DRW: R572-40179 AT FWD EDGE JUST OUTBOARD OF PYLON. IN ADDITION FOUND NUMEROUS DEVIATIONS (AT HOLE 7 & 9) AND CRACK IN HOLE 23 REPAIR PERFORMED BY RE-EMBODIMENT OF DRW: R572-40179 WITH CRACK Aug 22, 2007 · N726FD · Airbus A300B4622RSDR 2007UALA03374Skin Panel · damagedLEFT WING IS DAMAGED. REMOVED UNDERWING SKIN PANEL FOR REPLACEMENT.Aug 21, 2007 · N548UA · Boeing 757222SDR 07FDEA03008Skin · crackedRT WING LOWER SKIN CRACKED AT T/E ACCESS PANEL 675FB CUTOUT. FORWARD O/B CORNER AREA TOTAL CRACKED LENGTH 1.25 APPROX REF A300-600 SRM 51-10-00. COMPLIED WITH EA 6-5730-110509 REF SB'S A300-600 57-6064 AND 57-6029 DWG R57340199, SMALL REPAIR PLATE.Aug 21, 2007 · N653FE · Airbus A300F4605RSDR A6WA200740469Skin · corrodedLT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT AT WS 12.245 (510AB, HOLE NR 2) HAS FRETTING DAMAGE AROUND ENTIRE CIRCUMFERENCE OF HOLE, IN CRITICAL AREA, APPROX .30 INCH WIDE BY .006 INCH DEEP. MAINTENANCE REPAIRED DAMAGED AREA IAW REO 601R-57-21-030 REV FAug 20, 2007 · N467AW · Cndair CL6002B19SDR A6WA200740471Skin · damagedRIGHT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT AT WS 54.897 9640BB, HOLE NR 1) HAS FRETTING DAMAGE AT INBOARD AND OUTBOARD ENDS OF CUTOUT IN NON-CRITICAL AREA. INBOARD AREA MEASURES APPROX 6 INCH LENGTH BY .30 INCH WIDE BY .005 INCH DEEP. OUTBOARD AREA Aug 20, 2007 · N467AW · Cndair CL6002B19SDR A6WA200740470Skin · corrodedLEFT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT AT WS 54.897 (540BB, HOLE NR 1) HAS FRETTING DAMAGE AT INBOARD AND OUTBOARD ENDS. INBOARD END MEASURES APPROX 9.5 INCH BY .30 INCH BY .004 INCH DEEP. OUTBOARD END MEASURES APPROX 4.5 INCH BY .30 INCH BY .004Aug 20, 2007 · N467AW · Cndair CL6002B19SDR 07FDEA02994Skin · crackedLEFT WING BOTTOM SKIN PANEL NR 2, SKIN CRACKED I/B OF RIB 11, AFT OF REAR SPAR, WRI 57-10 9572, W/C T 6-5710-91017. STOP DRILLED CRACK, AND PERFORMED HFEC INSPECTION IAW A310 NTM 51-10-08 PT6, TO CONFIRM NO CRACK PAST STOP DRILLED AREA. INSTALLED SKIN DOUBLEAug 20, 2007 · N405FE · Airbus A310203SDR 07FDEA02991Skin Panel · chafedCHAFING MARKS WERE FOUND ON RT LOWER SURFACE BOTTOM SKIN REINFORCING PLATE AT RIB 7 FRONT SPAR INBOARD. REPAIR PERFORMED BY BLENDING OUT IAW EA 6-5720-106522, APPROVED BY RAS/BAE/1005107/2007 ISSUE "A".Aug 20, 2007 · N749FD · Airbus A300B4622RSDR 07FDEA02990Skin Panel · chafedCHAFING MARKS WERE FOUND ON LT LOWER SURFACE BOTTOM SKIN REINFORCING PLATE AT RIB 7 FRONT SPAR INBOARD. REPAIR PERFORMED BY BLENDING OUT IAW EA 6-5720-106522, APPROVED BY RAS/BAE/1005107/2007 ISSUE "A".Aug 20, 2007 · N749FD · Airbus A300B4622RSDR 07FDEA02973Skin · crackedCRACK INDICATIONS REVEALED IN FASTENER HOLES TOWARDS EDGE OF ACCESS CUTOUT IN LHW LOWER SKIN ACCESS DOOR, BETWEEN STA XORS=683.400 TO STA XORS=713.600. 09-04-07 COMPLIED WITH FEDEX E.A. 1-5710-115154, CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100.Aug 19, 2007 · N582FE · Doug MD11FSDR 07FDEA02972Skin · crackedCRACK INDICATIONS REVEALED IN FASTENER HOLES TOWARDS EDGE OF ACCESS CUTOUT IN RT WING LOWER SKIN ACCESS DOOR, BETWEEN STA XORS=683.400 TO STA XORS=713.600. 09-04-07 COMPLIED WITH FEDEX EA 1-5710-115155, CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100.Aug 19, 2007 · N582FE · Doug MD11FSDR DLM88071103Skin · crackedCRACK ON LEFT WING FIXED LEADING EDGE AT STA. XFS=238. REPAIRED PER ERA 380953-14MA ON N/R T0064417 AT HMV IN GDL.Aug 17, 2007 · N952DL · Doug MD88SDR DL764071092Skin · delaminatedLEFT WING OB END OF RAKED WING LOWER SKIN HAS EDGE DELAMINATION. REPAIRED LOWER SKIN DELAMINATION BY APPLYING GRAPHITE LAYUP REPAIRS IAW DELTA ERA 463393. REPAIR COMPLIED WITH BYTIMCO DURING HMV-1 IN GSO.Aug 17, 2007 · N830MH · Boeing 767432ERSDR DL764071091Skin · delaminatedLT WING OB END OF RAKED WING UPPER SKIN HAS DELAMINATION. REPAIRED UPPER SKIN DLAMINATION BY APPLYING GRAPHITE LAYUP REPAIRS IAW DELTA ERA 463393-14. COMPLIED WITH REPAIR ON TIMCO NR OPERATION 26942 DURING HMV-1 IN GSO.Aug 17, 2007 · N830MH · Boeing 767432ERSDR 07FDEA02931Skin · corrodedRT WING LOWER SKIN RIB 20-21 AROUND MAGNETIC LEVEL INDICATOR CORROSION ON LOWER SKIN REPAIR PERFORMED BY BLEND OUT THE COROSION IAW SRM 51-74-10, APPROVED BY EA 6-57820-112490 AND RAS/BAE/1005335/2007 ISS A.Aug 16, 2007 · N732FD · Airbus A300B4605RSDR 07FDEA02930Skin · corrodedLT WING LOWER SKIN RIB 20-21 AROUND MAGNETIC LEVEL INDICATOR CORROSION ON WING SKIN REPAIR PERFORMED BY BLEND OUT THE CORROSION IAW SRM 51-74-10, APPROVED BY EA 6-5720-112490 AND RAS/BAE/100535/2007 ISS A.Aug 16, 2007 · N732FD · Airbus A300B4605RSDR DLM90071086Skin · chafedL WING L/E SKIN CHAFED 2 EA PLACES AT NR 5 SLAT TRACK. REPAIRED LT WING L/E IAW MD-90 SRM 57-20-01 FIG 11 VOL 1.Aug 15, 2007 · N907DA · Doug MD9030SDR 07FDEA02836Skin · delaminatedFOUND OLD REPAIR ON LT AILERON , LOWER SKIN TRAILING EDGE WITH SIGN OF DELAMINATION. REPAIR RENEWED IAW SRM 517712 PB 201, PARA 4.Aug 13, 2007 · N749FD · Airbus A300B4622RSDR A6WA200740457Skin · corrodedTHE LEFT WING LOWER PLANK ACCESS HOLE FOR PANEL 510AB AT WS 12.245 HAS PITTING APPROX .007 INCH DEEP. 10-04-07 MAINTENANCE C/W REPAIR OF LT WING LOWER PLANK ACCESS HOLE PANEL 510AB IAW REO 601R-57-20-030 REV F. (M)Aug 12, 2007 · N464AW · Cndair CL6002B19SDR A6WA200740456Skin · corrodedTHE LEFT WING LOWER PLANK ACCESS HOLE FOR PANEL 540BB AT WS 54.897 HAS PITTING APPROX .005 INCH DEEP AT THE INBOUND AND OUTBOARD RADIUS. 10-04-07 MAINTENANCE REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV F. (M)Aug 12, 2007 · N464AW · Cndair CL6002B19SDR A6WA200740458Skin · corrodedTHE RT WING LOWER PLANK ACCESS HOLE FOR PANEL 640BB HAS PITTING APPROX .005 INCH DEEP AT THE INBOARD AND OUTBOARD RADIUS. 10-04-07 MAINTENANCE REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV F. (M)Aug 12, 2007 · N464AW · Cndair CL6002B19SDR 07FDEA02824Panel · corrodedRT WING T/E LOWER HINGE PANEL 8506R INNER SURFACE HAS CORROSION AROUND EDGE REPAIRED IAW SRM 51-20-151-7.Aug 10, 2007 · N254FE · Boeing 727233SDR IXXA07SMN200SSkin · dentedDURING ROUTINE C CHECK INSPECTION, LT WING NON STANDARD REPAIR ON INBD SLOT VANE AT STA XS 247.000.Aug 9, 2007 · N606AL · Doug DC873FSDR UPS07M50906Skin · crackedINSPECTION TYPE:C RIGHT WING LOWER SURFACE FIXED L/E SKIN AT I/B FWD CORNER OF REFUELING PANEL FOUND CRACK AS MARKED. FASTENERS AT RIGHT WING REFUELING PANEL CRACKED AREA REMOVED. DAMAGED AREA TRIMMED OFF. HFEC INSP C/OUT ON TRIMMED OFF AREA FOUND NO CRACK.Aug 8, 2007 · N290UP · Doug MD11FSDR UPS07M50851Skin · crackedINSPECTION TYPE:C RIGHT WING LOWER SURFACE L/E ACCESS PANEL CUTOUT STRUCTURE AT STA XORS 51 0 APPROX FOUND CRACK AS MARKED. HFEC INSP C/OUT & CRACK FOUND AS MARKED. CRACKED DOUBLER REMOVED. RIGHT WING LOWER SURFACE APPROX XORS 510 DOUBLER FABBED USING MAT'LAug 8, 2007 · N290UP · Doug MD11FSDR UPS07M50696Doubler · crackedINSPECTION TYPE:C RIGHT WING L/E COMPARTMENT AT STA XORS 710 APPROX FOUND UPPER DOUBLER CRACKED AS MARKED. RIBS REMOVED FOR ACCESS. CRACKED AREA TRIMMED OFF. HFEC INSP C/OUT ON TRIMMED OFF AREA FOUND NO CRACK. REPAIR ANGLES FABRICATED, HEAT TREATED & HARDNAug 8, 2007 · N290UP · Doug MD11FSDR UPS07M50695Doubler · crackedINSPECTION TYPE:C RIGHT WING L/E COMPARTMENT AT STA XORS 538 APPROX FOUND UPPER DOUBLER CRACKED AS MARKED. FRAMES REMOVED FOR ACCESS. CRACKED AREA TRIMMED OFF. HFEC INSP C/O ON TRIMMED OFF FOUND NO CRACK. REPAIR ANGLES FABRICATED, HEAT TREATED & HARDNESS VAug 8, 2007 · N290UP · Doug MD11FSDR 07FDEA02803Panel · crackedRT WING REAR SPAR LWR CHORD WAVY PANEL HAS 2 EA CRACKS APPROX FROM RSS 542-RSS 563. REMOVED SEAL IAW SRM 51-30-2. FABRICATED NEW SPLICES ON TRAVELER T7/691015 2024 T3 .063. FABRICATED LWR CHORD PANEL OB SIDE ON TRAVELER T7/691016 2024 T3 .063. INSTALLED REAug 8, 2007 · N212FE · Boeing 7272S2FSDR UPS07M50926Skin · chafedINSPECTION TYPE:C LT WING LEADING EDGE SKIN CHAFED AT SLAT TRACK NR 2 AREA STICKER 5712. LT WING L/E SKIN CHAFED AT SLAT TRACK NR 2 AREA CHAFED MARK REMOVED FOUND W/N LIMIT & REPROTECTED. HFEC INSP C/OUT FOUND CRACK APPROX .75 INCH LONG WING L/E ACCESS PANELAug 7, 2007 · N290UP · Doug MD11FSDR DHL2007804520Panel · delaminatedRT WING T/E UPPER PANEL DELAMINATED (STA XA 566.000 - 613.000). REMOVED AND REPLACED DELAMINATED RT WING T/E UPPER PANEL (STA XA 566.000 - 613.000) IAW SRM 51-3-0, SRM 51-3-1 (TORQUE).Aug 7, 2007 · N804DH · Doug DC873F
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