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 A6WA200740135Skin · corrodedRT WING PLANK ACCESS HOLE AT 640 AB HAS MINOR PITTING IN CRITICAL AND NON-CRITICAL AREA. (K) [SUP 06-05-07] MAINTENANCE CLEANED EDGE OF FUEL TANK ACCESS DOOR SKIN CUTOUT. BLENDED CORROSION IN DETAIL AREA I AND IV TO DEPTH OF .002 IAW STEPS 1-4 OF BOMBARDIMar 17, 2007 · N415AW · Cndair CL6002B19SDR ASMF200703006Seal · leakingDURING TRANSIT CHECK, A FUEL LEAK WAS DETECTED IN AN UPPER PANEL OF THE LT WING. MAINTENANCE PERSONNEL RELOCATED THE SEAL AND APPLIED SEALANT IAW SRM 51-20-04 AND 51-22-2A, LEAK WAS CORRECTED. AS A PRECAUTIONARY ACTION, DURING OVERNIGHT CHECK THE SEAL WAS REPMar 17, 2007 · N803ML · Doug DC987SDR 07FDEA00943Skin · crackedLEFT WING, LEADING EDGE NR 5 SLAT NR 12 TRACK CUT OUT FOUND CRACK. LEFT WING, LEADING EDGE NR 5 SLAT NR 12 TRACK CUT OUT REPAIRED AS PER SRM 57-10-00 FIG 21 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.Mar 16, 2007 · N597FE · Doug MD11FSDR 07FDEA00942Skin · crackedRIGHT WING, LEADING EDGE NR 4 SLAT NR 10 TRACK CUT OUT FOUND CRACK. RIGHT WING, LEADING EDGE NR 4 SLAT NR 10 TRACK CUT OUT REPAIRED AS PER SRM 57-10-00 FIG 21 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.Mar 16, 2007 · N597FE · Doug MD11FSDR 07FDEA00941Skin · crackedRIGHT WING, LEADING EDGE NR 7 SLAT NR 14 TRACK CUT OUT FOUND CRACK. RIGHT WING, LEADING EDGE NR 7 SLAT NR 14 TRACK CUT OUT. REPAIRED AS PER SRM 57-10-00 FIG 21 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.Mar 16, 2007 · N597FE · Doug MD11FSDR 07FDEA00940Skin · crackedRIGHT WING, LEADING EDGE NR 7 SLAT NR 15 TRACK CUT OUT FOUND CRACK. RIGHT WING, LEADING EDGE NR 7 SLAT NR 15 TRACK CUT OUT. REPAIRED AS PER SRM 57-10-00 FIG 21 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.Mar 16, 2007 · N597FE · Doug MD11FSDR 07FDEA00962Skin · delaminatedCORROSION AND DELAMINATION ON T/E BOTTOM SURFACE LT WING. REPAIR WAS PERFORMED BY INSTALLING A NEW WEDGE SECTION AND A REPAIR PLATE IAW EA 6-5750-103433 AND RAS/BAE/1003821/2006 ISSUE "A".Mar 16, 2007 · N813FD · Airbus A310324SDR 07FDEA00947Skin · crackedRT WING BOTTOM SKIN PANEL NR 2, AFT OF REAR SPAR INBOARD OF RIB 11 CRACKED. REPAIR WAS PERFORMED IAW REPAIR DRAWING R572-49152-001 AND SB A310-57-2066 (DOUBLER INSTALLED).Mar 16, 2007 · N816FD · Airbus A310304SDR 07FDEA00919Skin · corrodedOLD CORROSION REPAIRS ON TOP WING SKIN LT BETWEEN RIB 8 AND RIB 19, P12-15. OLD BLEND REPAIRS ARE WITHIN LIMITS GIVEN FROM AI EA 6-5720-103417 AND RAS/BAE/1003706/2006 ARE VALID FOR THIS SUBJECT.Mar 16, 2007 · N813FD · Airbus A310324SDR 07FDEA00917Skin · corrodedRIGHT WING UPPER SKIN HAS SEVERAL AREAS OF SURFACE CORROSION XW118- XORS 264 (32 AREAS MARKED). REMOVED CORRODED AREAS NR 1 THRU NR 32 IAW DC10 SRM 57-10-00 FIG 59 VOL I AREAS NR 1 THRU NR 21 AND NR 23, NR 25, THRU NR 32 FOUND TO BE WITHIN LIMITS IAW DC10 SRMar 15, 2007 · N40061 · Doug DC1010SDR 07FDEA00915Skin · dentedRIGHT WING L/EDGE FWD OF PRESSURE "REFUEL" PANEL AT XORS 510 TO XORS 538 DENTED 2 AREAS. REMOVED, REPLACED, FABBED AND INSTALLED DOUBLER IAW DC10 SRM 57-00-01 FIG 4 SHEET 2 VOL I, ALODINED AND PRIMED IAW DC10 SRM 51-21-01 VOL II.Mar 15, 2007 · N40061 · Doug DC1010SDR 07FDEA00914Skin · dentedRIGHT WING L/EDGE FWD OF PRESSURE "REFUEL" PANEL AT XORS 510 TO XORS 538 DENTED 2 AREAS. REMOVED, REPLACED, FABBED AND INSTALLED DOUBLER IAW DC10 SRM 57-00-01 FIG 4 SHEET 2 VOL I . ALODINED AND PRIMED IAW DC10 SRM 51-21-01 VOL II.Mar 15, 2007 · N40061 · Doug DC1010SDR 07FDEA00911Skin · corrodedRIGHT WING LOWER SURFACE HAS CORROSION AT NR 6 FLAP TRACK MID ATTACH POINT. ACCOMPLISHED REPAIR OF ATTACH POINT, REF EA 7-5730-107001, WRI 57309127.Mar 15, 2007 · N463FE · Boeing 727225SDR 07FDEA00895Skin · corrodedFOUND DAMAGED HOLES ON LT WING TOP SKIN, REAR SPAR, RIB 4-5. REPAIR WAS PERFORMED BY REAMING UP HOLE 248 IAW EA 6-5720-103430 AND RAS/BAE/1003766/2006 ISSUE "A".Mar 15, 2007 · N813FD · Airbus A310324SDR 07FDEA00893Skin · damagedOVERSIZED HOLES FOUND DURING ACCOMPLISHMENT OF SB A310-53-2072 ON WING CENTER SECTION UPPER SURFACE STIFFENER 9 AND 10. REPAIR CONSISTS OF INSTALLING OF BOTH HOLES EN 6115-V5X IN TRANSITION FIT IAW EA 6-5315-103426 AND RAS 048117/009/2006 ISSUE "A".Mar 15, 2007 · N813FD · Airbus A310324SDR 07FDEA00876Skin · crackedLT WING LOWER SKIN SURFACE HAS A CRACK OF APPROX 1 INCH LONG AT AFT END OF RIB 11, 4 INCHES AFT OF REAR SPAR, FWD INBD END OF CUTOUT FOR ACCESS PANEL 581AB. CRACK RUNS THROUGH 1 FASTENER HOLE. ACCOMPLISHED RIB 11 PERMANENT REPAIR IAW FED EX EA 6-5710-107675 Mar 15, 2007 · N412FE · Airbus A310203SDR 07FDEA00869Skin · corrodedFOUND TWO DAMAGED HOLES (HOLE NR 4 RIB 17 AND HOLE NR 4 RIB 3-4) ON RT WING TOP SKIN AND CORROSION ON WING TOP SKIN. REPAIR WAS PERFORMED IAW EA 6-5720-106356 AND RAS/BAE/1003742/2006 ISSUE "A".Mar 15, 2007 · N813FD · Airbus A310324SDR 07FDEA00867Skin · corrodedFOUND CORROSION ON LT WING TOP SKIN. REPAIR WAS PERFORMED BY BLEND OUT IAW EA 6-5720-106356 AND RAS/BAE/1003742/2006 ISSUE "A".Mar 15, 2007 · N813FD · Airbus A310324SDR 07FDEA00864Skin · corrodedBOTTOM SKIN REWORK CAUSED BY CORROSION AT RIB 8, P19, RT OUTER WING REPAIR WAS PERFORMED IAW EA 6-5721-106402 AND RAS/BAE/1004132/2007 ISS A (BLEND OUT CORROSION, FASTENER REPLACEMENT.Mar 15, 2007 · N748FD · Airbus A300B4622RSDR 07FDEA00860Skin · chafedCHAFING MARKS TO LEADING EDGE 'D' NOSE SKIN, BOTH WINGS. LT WING BETWEEN TRACK 5 AND TRACK 6, LT WING BETWEEN TRACK 9 AND TRACK 10, RT WING BETWEEN TRACK 5 AND TRACK 6 AND RT WING AREA OF TRACK 1. REPAIR WAS PERFORMED IAW EA 6-5741-103419 AND RAS/BAE/1003686Mar 15, 2007 · N813FD · Airbus A310324SDR 07FDEA00857Skin · corrodedFOUND LT WING L/E FOUND CORROSION WITH EXF ON SKIN FIXED PANEL AT STA XOS 910-930. REPAIRED SACRIFICIAL DOUBLER IAW SRM 57-10-00 FIG 19D SHT 1 VOL 1. TOUCHED UP IAW SRM 51-21-01 VOL 2 PAG 21-25 AND SRM 51-21-02 VOL 2. FABRICATED PARTS IAW DETAIL PARTS TRAVEMar 15, 2007 · N304FE · Doug DC1030FSDR 07FDEA00852Skin · corrodedLT WING TIP, CORROSION UNDER ONE STATIC DISCHARGER AND CRACK ON NAVIGATION LIGHT BRACKET. REPAIR WAS PERFORMED IAW EA 6-5730-106400 AND RAS/FOK/004/2007 ISSUE "A".Mar 15, 2007 · N748FD · Airbus A300B4622RSDR 07FDEA00851Skin · damagedELONGATED HOLES IN LT BOTTOM WING SKIN AT PYLON SUPPORT BRACKET. REPAIR WAS PERFORMED IAW EA 6-5720-106422, DRAWING R572-49184 AND RAS/BAE/1004144/2007 ISSUE "A".Mar 15, 2007 · N816FD · Airbus A310304SDR 07FDEA00835Skin · corrodedFOUND CORROSION ON RT WING TOP SKIN AT TRAILING EDGE AREA OUTER SHROUD BOX. REPAIR PERFORMED IAW EA 6-5720-103382.Mar 14, 2007 · N813FD · Airbus A310324SDR 07FDEA00811Skin · corrodedOLD REPAIR ON LT WING ON TOP SKIN, REAR SPAR, BETWEEN RIB 4-5. VISUAL INSPECTION FOR FURTHER CORROSION AND CORRECT TAPERLOCK INSTALLATION IAW AMM570000/601/PARA 2, SRM514021/001/PARA 9 AND RAS/BAE/0439/98 ISSUE "B". (FURTHER DR422).Mar 14, 2007 · N813FD · Airbus A310324SDR HSRA3132007Skin · crackedFOUND CRACKS IN THE WING SKIN ON THE LT WING UPPER CENTER SECTION WHERE IT IS RIVETED TO THE ATTACH FITTING. THE FORWARD OB FAIRING NEXT TO THE NACELLE MUST BE LIFTED TO SEE THE CRACKS. LIKELY CAUSED BY LANDING CYCLES AND FATIGUE. SUBMITTER ADVISES THAT MFGMar 13, 2007 · N90EJ · Beech C90SDR UPS07849551Skin · damagedINSPECTION TYPE:C3 DEEP CREASED DENT 3 INCHES LONG ON LEADING EDGE O/B RIGHT WING. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-02-01-00 FIG 002H.Mar 12, 2007 · N811UP · Doug DC873FSDR A6WA200740123Skin · corrodedRT WING PLANK ACCESS HOLE NR6 HAS MINOR PITTING IN CRITICAL AND NOT CRITICAL AREAS. MAINTENANCE REPAIRED RT WING PLANK ACCESS HOLE NR6 UNDER FUEL ACCESS PANEL 640 DB IAW REO 601R-57-21-030 REV D AND AWAC E06/021-457. (K)Mar 10, 2007 · N453AW · Cndair CL6002B19SDR QXEA200700433Panel · gougedC4 PDX - GOUGE UNDER PANEL 521AT. REPAIRED IAW SRM 51-20-11, 51-20-36.Mar 10, 2007 · N367PH · Dhav DHC8202SDR UIEA200700137Skin Panel · crackedRT WING UPPER TRAILING EDGE COMPOSITE PANEL HAS A 2.0 INCH CRACK, INBOARD OF INBOARD AILERON AT WBL 445.00, 10.0 INCHES FROM AFT EDGE. PERMANENT REPAIR WAS ACCOMPLISHED AS PER 747-200 SRM 51-40-09, FIG 2, TABLE 1 AND 747-200 SRM 51-40-12. ALSO, REFERENCE ATLMar 10, 2007 · N517MC · Boeing 747243BSDR UIEA200700136Skin Panel · delaminatedLT WING UPPER TRAILING EDGE SKIN PANEL HAS A 6.0 INCH BY 6.0 INCH AREA OF DELAMINATION AND FASTENERS ARE PULLING THRU THE SKIN, AT WBL 239.00 INBOARD OF NR 6 SPOILER AND 62.0 INCHES FROM AFT EDGE. PERMANENT REPAIR WAS ACCOMPLISHED AS PER 747-200 SRM 51-40-09,Mar 10, 2007 · N517MC · Boeing 747243BSDR QXEA200701330Skin · damagedC4 PDX - AT LEFT WING STATION YW 222.4 THERE IS AN AREA OF SMALL NICKS. REPAIRED IAW RD8-57-2996 AND SRM 51-20-11.Mar 9, 2007 · N367PH · Dhav DHC8202SDR A6WA200740128Skin · corrodedRIGHT WING INBOARD FUEL PANEL 640BB FOUND CORROSION AROUND WING PLANK APPROX .005 INCH DEEP IN NON-CRITICAL AREA. MAINTENANCE REPAIRED CORROSION BY BLENDING IAW BOMBARDIER REO 601R-57-21-030 REV F. (M)Mar 9, 2007 · N413AW · Cndair CL6002B19SDR A6WA200740127Skin · corrodedLEFT WING OUTBOARD FUEL PANEL 550BB FOUND CORROSION AROUND WING PLANK APPROX .005 INCH DEEP IN NON-CRITICAL AREA. MAINTENANCE REPAIRED CORROSION BY BLENDING IAW BOMBARDIER REO 601R-57-030 REV F. (M)Mar 9, 2007 · N413AW · Cndair CL6002B19SDR A6WA200740126Skin · corrodedRIGHT WING OUTBOARD FUEL PANEL 650B FOUND CORROSION AROUND WING PLANK APPROX .005 INCH DEEP IN NON-CRITICAL AREA. MAINTENANCE REPAIRED CORROSION BY BLENDING IAW BOMBARDIER REO 601R-57-030 REV F. (M)Mar 9, 2007 · N413AW · Cndair CL6002B19SDR WRLA2007041Skin · crackedDURING C-04 CHECK FOUND CRACK LT WING FIXED LEADING EDGE ACCESS DOOR CUTOUT BOTH UPPER SIDE XOS:464 TO XOS:470, NR 3 SLAT. PERFORM REPAIR PER MD-11 SRM 57-10-00 FIG 42 VOL 1 REV 38 TR 57-8Mar 9, 2007 · N271WA · Doug MD11SDR 07FDEA00701Panel · crackedRT WING, WING LWR SKIN SURFACE NEXT TO TOP INB OF PNL 681AB FOUND CRACKED REPAIRED PER FEDEX ENG AUTH 6-5710-106686. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR".Mar 8, 2007 · N409FE · Airbus A310203SDR 07FDEA00679Skin · corrodedFOUND CORROSION AROUND TWO FASTENERS BETWEEN RIB 7-8 AT STRINGER 19 ON RT WING BOTTOM SKIN. REPAIR WAS PERFORMED IAW EA 6-5721-106402, APPROVED BY RAS/BAE/1004132/2007.Mar 7, 2007 · N748FD · Airbus A300B4622RSDR 070059Skin · crackedDURING A ROUTINE MAINTENANCE INSPECTION MAINTENANCE REPORTED AN APPARENT CRACK IN AN UPPER WING SURFACE PANEL AT APPROXIMATELY WING STATION 48.00. FURTHER INSPECTION REVEALED A CRACK OF APPROXIMATELY 13-INCHES LENGTH IN THE COMPOSITE PANEL AT WING STATION 47.Mar 6, 2007 · N883GA · Doug DC983SDR CA070307008Skin Panel · corroded(CAN) SEVERAL CORRODED RIVET HEADS FOUND ON THE LOWER SURFACE OF WING. THE AREA OF CONCENTRATION IS THE GAS PATHS FROM THE EXHAUST STACKS. REPAIRS TO CORRODED RIVETS WAS INITIATED AND REVEALED CORROSION UNDER THE RIVET HEADS EXISTED TO A DEPTH OF 0.011. REPAIRMar 5, 2007 · Dhav DHC6300SDR CA070307007Skin · corroded(CAN) SEVERAL CORRODED RIVET HEADS FOUND ON THE LOWER SURFACE OF WING. THE AREA OF CONCENTRATION IS THE GAS PATHS FROM THE EXHAUST STACKS. REPAIRS CARRIED OUT IAW REO6-57-30-V019 (YW 85-91.25) AND REO6-57-30-V020 (YW 122-135). (TC NR 20070307007)Mar 5, 2007 · Dhav DHC6300SDR CA070307006Skin · corroded(CAN) SEVERAL CORRODED RIVET HEADS FOUND ON THE LOWER SURFACE OF WING. THE AREA OF CONCENTRATION IS THE GAS PATHS FROM THE EXHAUST STACKS. REPAIRS CARRIED OUT IAW REO6-57-30-V017 (YW 85-91.25) AND REO6-57-30-V018 (YW 127-146). (TC NR 20070307006)Mar 5, 2007 · Dhav DHC6300SDR CA070307004Skin Panel · debonded(CAN) DEBONDING OF UPPER WING SKIN, IB OF NACELLE. DEBONDING DETECTED DURING ULTRA SONIC INSPECTION IAW SB 6/543. REPAIR CARRIED OUT IAW REO6-57-30-V012 REV A. (TC NR 20070307004)Mar 5, 2007 · Dhav DHC6300SDR CA070307003Skin Panel · debonded(CAN) DEBONDING OF UPPER WING SKIN, OB OF NACELLE. DEBONDING DETECTED DURING ULTRA SONIC INSPECTION IAW SB 6/543. REPAIR CARRIED OUT IAW REO6-57-30-V013 REV A. (TC NR 20070307003)Mar 5, 2007 · Dhav DHC6300SDR UIEA200700128Doubler · separatedNR 3 PYLON FWD FIXED FAIRING LT EXTERIOR SURFACE AFT CORNER SKIN DOUBLER SEPARATED. FAIRING REPLACED BUT NUMEROUS FASTENERS HOLES FOUND MISALIGNED. TIME LIMIT REPAIRED ACCOMPLISHED AS PER BOEING MESSAGE NR 1-292185930-1 THRU -14, DWG 65B90813-52 AND FAA FORMMar 2, 2007 · N505MC · Boeing 7472D3BSDR UIEA200700119Panel · crackedRIGHT WING, UPPER TRAILING EDGE PANEL, OUTBOARD OF NR 8 SPOILER HAS A 7.0 INCH LONG BY 1.5 INCH WIDE CRACK. PERMANENT REPAIR WAS ACCOMPLISHED AS PER 747-200 SRM 51-40-09, FIG 2, TABLE 1 AND SRM 51-40-12. ALSO, REFERENCE ATLAS AIR XEO NR 57-030107.Mar 2, 2007 · N540MC · Boeing 747243BSDR 2007FA0000191Skin · corrodedRT WING LEADING EDGE(S) HAD SEVERE CORROSION WHERE THE TKS PANELS ATTACH. AFTER COMPLETE DISASSEMBLY IT WAS DETERMINED TO BE BEYOND ECONOMICAL REPAIR. RT WING LEADING EDGE HAD BEEN INSPECTED AT MFG 2.5 YEAR PRIOR TO THIS DISCOVERY. (K)Feb 27, 2007 · N224EA · Braero HS125700ASDR 07FDEA00603Skin · corrodedRT WING LOWER SURFACE AT STA XW 486 ON SKIN TANK BOX FOUND SEVERE CORROSION WITH EXFOLIATION. FASTENERS REMOVED AND REINSTALLED IAW SRM 51-33-01. CORROSION REMOVED IAW SRM 57-10-00 FIG 59 VOL 1 O/B FLAP I/B HINGE SUPPORT REMOVED AND REINSTALLED IAW SRM 51-33Feb 27, 2007 · N554FE · Doug DC1010SDR 07FDEA00599Doubler · corrodedRT WING LOWER SURFACE AT XORS 264 ON BEAVER TAIL DOUBLER AROUND NR 15 HEAD FASTENERS FOUND LIGHT CORROSION WITH EXFOLIATION. TAPER LOCKS REMOVED IAW SRM 51-34-01 PAGE 1-7 VOL 2. CORROSION REMOVED IAW SRM 57-10-00 FIG 69 VOL 1, AREA OUT OF LIMITS TRIMMED OUT Feb 27, 2007 · N554FE · Doug DC1010SDR 07FDEA00575Skin · crackedRT WING L/E EXT FOUND 1 CRACK 1.50" LONG ON SKIN AT STA XORS 506. REMOVED REFUELING DOOR IAW MM 20-50-02-2 AND DWG ARB1067. REMOVED PLATE SP10240168 IAW SRM 51-31-01 VOL 2 PAR 6. REMOVED EXISTING DOUBLER AND INSTALLED A NEW ONE IAW SRM 57-10-00 VOL 1 FIG 68Feb 26, 2007 · N373FE · Doug DC1010
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