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 05FDEA02369Access Panel · damagedLEFT WING ACCESS PANEL PRESSURE REFUEL AREA AT XOS 611 EXISTING EXTERNAL REPAIR DOUBLER ON SKIN. REPAIR IAW SRM 57-10-00 FIG 68 VOL 1.Aug 9, 2005 · N564FE · Doug MD1010FSDR 05FDEA02368Access Panel · damagedLEFT WING ACCESS PANEL SLAT DRIVE MECHANISM LOWER EXTERNAL L/E XOS 487 EXISTING EXTERNAL REPAIR DOUBLER ON SKIN. REPAIR PER SRM 57-10-00 FIG 68 VOL 1.Aug 9, 2005 · N564FE · Doug MD1010FSDR 05FDEA02351Skin · damagedLT WING SLAT 2 XORS 231 EXISTING FLUSH REPAIR DOUBLER ON LWR SKIN. REPAIR PER SRM 57-10-00 FIG 29 VOL 1.Aug 9, 2005 · N564FE · Doug MD1010FSDR 05FDEA02350Skin · damagedLEFT WING DROOP L/E FLUSH REPAIR SKIN ON EXTERNAL SKIN. REPLACED OLD REPAIR PER SRM 57-00-01 FIG 4 VOL 1 SHEET 2.Aug 9, 2005 · N564FE · Doug MD1010FSDR 05FDEA02348Skin · damagedLEFT WING XOS UPPER EXT L/E SIDE, EXISTING REPAIR DOUBLER ON SKIN. REMOVED SLAT TRACK DOOR AND REMOVED AND REPLACED AND REINSTALLED TRACK SLAT DOOR IAW MM 57-21-01-2, SRM 51-35-02 VOL 2 AND SRM 57-10-00 FIG 68 VOL 1.Aug 9, 2005 · N564FE · Doug MD1010FSDR 05FDEA02339Skin · damagedRIGHT WING XORS 506 L/E TRACK NR 8 EXISTING 1EA EXT REPAIR DOUBLER ON SKIN. REPLACED REPAIR PER SRM 57-10-00 FIG 68 SHT 1-3 VOL 1.Aug 9, 2005 · N564FE · Doug MD1010FSDR UPS05845394Doubler · crackedINSPECTION TYPE: C3, LT WING L/E LOWER INTERNAL DOUBLER IS CRACKED AT DRAIN HOLE XFS 597.500. REMOVED, FABRICATED, AND INSTALLED INTERNAL DOUBLER IAW DC-8 SRM 57-3- 0, 51-1-20D, AND 51-1-21.Aug 8, 2005 · N801UP · Doug DC873FSDR 05FDEA02303Skin Panel · chafedRIGHT WING - DROOP L/E SKIN PANEL OUTBOARD EDGE FOUND CHAFED MARK. FOUND WITHIN LIMITS AS PER SRM 57-00-01. TRIMMED AND FIGURE 1A VOLUME I. MATERIAL REMOVED 0.375 FROM EDGE. NDT INSPECTED AND VERIFIED CRACK FREE CONDITION. OPERATION CHECKED AND FOUND 'SAT'Aug 7, 2005 · N601FE · Doug MD11SDR 05FDEA02274Access Panel · crackedACCESS PANEL ON RIGHT WING FOUND CRACK 1 INCH LONG ON L/E AT STA XORS 455. REPAIRED DOUBLER IAW SRM 57-10-00 FIG 18 VOL I.Aug 5, 2005 · N624FE · Doug MD11SDR 05FDEA02269Doubler · crackedRIGHT WING L/E NR 7 CRACKS ON INTERNAL DOUBLER AT STA XORS 552. REPAIR IAW SRM 57-10-00 FIG 25 VOL I.Aug 5, 2005 · N624FE · Doug MD11SDR ABXA050182Panel · debondedLT WING OB UPPER TRAILING EDGE PANEL HAD SKIN DAMAGE AT STA. XRS 516. SKIN DEBONDED AND ROLLED BACK FROM THE LEADING EDGE PANEL. DAMAGED AREA MEASURED 6 INCHES LONG BY 18 INCHES WIDE. DEFERRED: NR 45199. TEMP REPAIRED IAW REA D957-52280. CLEARED: DI NR 45199.Aug 3, 2005 · N933AX · Doug DC933FSDR UPS05544998Panel · delaminatedJUST AFT OF RIGHT WING JACK PAD LWR SURFACE PANEL HAS DELAM. PANEL HAS A 3X4 AREA OF DELAM OUT OF LIMITS PER 57-51-01-1A. SECOND, REMOVED PANEL TO S/M SHOP. THIRD, REMOVED DAMAGE, INSTALLED NEW CORE, INSTALLED PLIES & STARTED CURE SRM 51-70-05-06. REMOVED Jul 30, 2005 · N421UP · Boeing 75724APFSDR UPS05845001Skin · damagedLT UPPER WING PANEL AT T/E IN FRONT OF NR 4 SPOILER HAS SKIN ROLLED UP APPROX 18 - 24 INCHES ALONG AFT EDGE W/APPROX 30 RIVETS PULLED. ROLLED APPX 1.5 - 2 INCHES FWD AT DEEPEST SPOT. REMOVED DAMAGED MATERIAL, INSTALLED REPAIR DOUBLER & ANGLE & SEAL PER EO DC8Jul 29, 2005 · N894UP · Doug DC873FSDR USAA050902Panel · crackedCLT - C1 - PANEL, 2 INCH CRACK, TOP OF LT WING PANEL JUST OB OF GROUND SPOILER. REMOVED DAMAGE AND INSTALLED REPAIR SPLICE AND DOUBLER IAW SRM. (K)Jul 27, 2005 · N404US · Boeing 737401SDR UPS05845151Skin · crackedR/W UPPER SURFACE 6" AFT OF FRONT SPAR AT FUEL PROBE NR 12 HAS A 1" CRACK AT FASTENER HOLE. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 57- 2-1 FIG 10.Jul 26, 2005 · N809UP · Doug DC873FSDR GTIA050237Vane · gougedFOUND LEFT WING, FIXED FLAP VANE, 4TH FROM INBOARD, L/E IS GOUGED. FIXED T-CAP VANE, FOUND OUT OF LIMITS. FABRICATED DOUBLERS AND REPAIRED LEFT FIXED VANE. (M)Jul 24, 2005 · N831NK · Doug DC983SDR 05FDEA02055Skin · corrodedRIGHT HAND WING UPPER SURFACE TRAILING EDGE FORWARD OF NR 2 SPOILER 4 EACH SKIN BULGE FOUND AS MARKED. CORROSION REMOVED AND FOUND WITHIN LIMIT REFER TO SNRM N1237 FOR WORK DETAILS AND 03 EA AREA CORROSION REMOVED AND FOUND EXCEED LIMIT REFER TO SNRM N123Jul 24, 2005 · N579FE · Doug MD11SDR 05FDEA02050Skin · corrodedRIGHT HAND WING UPPER SURFACE TRAILING EDGE FORWARD OF OUTBOARD AILERON SEVERAL SKIN BULGE FOUND AS MARKED. CORROSION REMOVED AND FOUND WITHIN LIMIT - REFER TO SNRM N1244, N1245, N1246 AND N1247 FOR WORK DETAILS AND 03 EA AREA CORROSION REMOVED AND FOUND EXCEJul 24, 2005 · N579FE · Doug MD11SDR 05FDEA02049Skin · corrodedLT WING UPPER SURFACE FORWARD OF FUEL TANK PANEL 533AT 1 EACH SKIN BULGE FOUND AS MARKED. CORROSION ON LTW UPPER SURFACE FWD OF FUEL TANK PANEL 533AT REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL THICKNESS: 0.749"; THK. REMOVED: 0.033"; THK. REMAINED: 0.716Jul 24, 2005 · N579FE · Doug MD11SDR UPS05445131Skin · corrodedINSPECTION TYPE:C, LEFT WING UPPER WING SKIN L/E RABBIT AREA 2 PLACES BULGED UP AT WS 1470-1515 AFT OF NR 1 VC FLAP AREA. CORROSION THROUGH WHOLE THICKNESS AREA 7.3" X 4.3". LEFT WING UPPER WING SKIN REPAIRED AS PER HX RS R57-25-35357 & UPS ENGINEERING FILE Jul 23, 2005 · N683UP · Boeing 747121SDR KPVA200511Skin · damagedLT WING TIP IS TORN ALMOST ALL THE WAY OFF. REPAIRED LT WING TIP IAW RD8-57-3143. REMOVED AND REPLACED LT AILERON IAW DHC MM 27-12-11 PG 201-204. RIGGED AILERON CONTROL SYSTEM IAW DHC-8 MM 27-12-00 PG 201-213. NO DEFECTS NOTED. REMOVED AND REPLACED LT WINJul 23, 2005 · N806WP · Dhav DHC8103SDR UPS05445088Skin · corrodedINSPECTION TYPE:C RIGHT WING UPPER SURFACE RABBIT AREA FOUND BULGED BETWEEN WS 1375 AND WS 1395 (AFT NR 24 VC FLAP). CORROSION BLEND OUT 0.127" X 1.625" X 6" EXCEED SRM 57-30-01 FIG 1 LIMITS. RIGHT WING UPPER SURFACE RABBIT AREA REPAIRED AFTER CORROSION BLENJul 22, 2005 · N683UP · Boeing 747121SDR ASOA05619Panel · crackedDURING A C-CHECK, THE LOWER WING PLANK AT WS 148.019 LT SIDE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LOWER WING PLANK AT WS 148.019 LT SIDE IAW EO. (K)Jul 22, 2005 · N833AS · Cndair CL6002B19SDR DL76L050389Panel · missingLEFT WING PANEL (NR 521EB) COMPLETELY MISSING FROM WING WHEN AIRCRAFT ARRIVED IN LGW. REPLACED SAME.Jul 21, 2005 · N189DN · Boeing 767332SDR IXXA05RNG045SSkin · corrodedSKIN CORROSION DAMAGE FOUND ON RIGHT OUTER WING AT UPPER PLATING AROUND WING STATION XRS 727.00 AND STRINGER 3RH DURING A ROUTINE C CHECK INSPECTION. CORRODED AREA WAS BLENDED OUT, DOUBLER WAS FABRICATED AND INSTALLED IAW EWO ATI 57-035 AND EO ATI-071605. FAJul 20, 2005 · N71CX · Doug DC862FSDR IXXA05RNG039SSkin · corrodedDURING A ROUTINE C CHECK INSPECTION FOUND SKIN CORROSION DAMAGE ON THE RT OUTER WING AT INBD EXTENDED L/E AROUND STA XFS 603.750REMOVED CORROSION DAMAGE, FABRICATED REPAIR DOUBLER AND INSTALLED IAW EWO ATI 57-031 & EO ATI-071405. FAA FORM 8110-3 WAS ISSUED APPJul 20, 2005 · N71CX · Doug DC862FSDR SIM2005F00010Skin · damagedLT AILERON AND WING WERE DAMAGED BY A CATERING TRUCK. MAINTENANCE REPLACED LT WING SPAR SEGMENT AND WING SKIN. REPLACED LT AILERON IAW EO. AIRCRAFT WAS RETURNED TO SERVICE. (K)Jul 20, 2005 · N925AE · Emb EMB145LRSDR SIM2005F00009Skin · damagedLT AILERON AND WING WERE DAMAGED BY A CATERING TRUCK. MAINTENANCE REPLACED LT WING SPAR SEGMENT AND WING SKIN. REPLACED LT AILERON IAW EO. AIRCRAFT WAS RETURNED TO SERVICE. (K)Jul 20, 2005 · N925AE · Emb EMB145LRSDR IXXA05RNG042SSkin · corrodedDURING A ROUTINE C CHECK INSPECTION, FOUND CORROSION OVER EXISTING REPAIR ON WING ON INNER OUTBOARD EXTENDED L/E SLAT STA XFS 207-XILD42. CORROSION ON RT WING LEADING EDGE UPPER SKIN WAS REMOVED AND REPAIR "DOUBLER' WAS INSTALLED IAW EWO ATI 57-034 AND SRM 57Jul 19, 2005 · N71CX · Doug DC862FSDR IXXA05RNG038SSkin · corrodedDURING A "C" CHECK INSPECTION, FOUND SKIN CORROSION DAMAGE ON THE RIGHT OUTER WING AT THE INBOARD EXTENDED L/E STA XFS 653.750. RT WING L/E UPPER SKIN WAS REPAIRED IAW EWO ATI 57-030 AND EO ATI-071305. FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR.Jul 19, 2005 · N71CX · Doug DC862FSDR IXXA05RNG037SSkin Panel · corrodedDURING INSPECTION CHECK CORROSION WAS FOUND ON PANEL AT WING OUTER INBOARD EXTENDED LEADING EDGE PLATING STA XFS 710.0, RT. CORROSION ON RT WING LEADING EDGE UPPER SKIN WAS REMOVED AND REPAIR "DOUBLER" WAS INSTALLED IAW EWO ATI 57-029 AND EO ATI-071505. FAA Jul 19, 2005 · N71CX · Doug DC862FSDR IXXA05RNG036SSkin · corrodedDURING INSPECTION CHECK, SKIN CORROSION DAMAGE WAS FOUND ON THE LEFT INNER WING AT OUTBOARD EXTENDED LEADING EDGE SLOT AROUND L/E STATION XFS 207.00. REMOVED CORROSION AND ACCOMPLISHED REPAIR "DOUBLER" IAW EWO ATI 57-028 AND EO ATI-071205. FAA FORM 8110-3 WAJul 18, 2005 · N71CX · Doug DC862FSDR IXXA05RNG046SSkin · misdrilledDURING A ROUTINE C CHECK INSPECTION FOUND A MISS DRILL HOLE ON PLATING STA XRS 795 LONGERON 3-RHD. REPAIR WAS MADE AND DOUBLER WAS INSTALLED IAW EWO ATI 57-036 & EO ATI-071705.FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR.Jul 17, 2005 · N71CX · Doug DC862FSDR A6WA200540249Access Panel · damagedRT LOWER WING PLANK AT WS 45, FUEL ACCESS PANEL 640BB CUT OUT, RAS FRETTING DAMAGE 2 INCH LONG X .175 INCH WIDE. (K)Jul 16, 2005 · N420AW · Cndair CL6002B19SDR DHL2005802516Panel · delaminatedLT WING T/E UPPER PANEL DELAMINATED (STA XW 5.000 - 47.000). REMOVED AND REPLACED LT WING TE UPPER PANEL (STA XW 5.000-47.000) IAW SRM 51-3-0 PG. 1. TORQUED IAW3 SRM 51-3-1.Jul 15, 2005 · N802DH · Doug DC873SDR 05FDEA01952Skin · crackedLT WING FIXED TE UPPER SKIN CRACKED/CUT LOC 5 IN FROM INBD END 2.5 IN FROM AFT END.Jul 14, 2005 · N671FE · Airbus A300F4605RSDR 05FDEA01957Skin · crackedLEFT WING, FORWARD FIXED LEADING EDGE INNER SKIN FOUND CRACKED, ADJACENT TO REFUELING PANEL AT STA 530. FABRICATED REPAIR DOUBLER AS PER SRM 57-10-00 FIG. 25 VOL.I AND INSTALLED REPAIR DOUBLER AT LT WING FORWARD FIXED LEADING EDGE INNER SKIN, ADJACENT TO REFUJul 14, 2005 · N589FE · Doug MD11SDR 05FDEA01956Skin · crackedLT WING FORWARD FIXED LEADING EDGE INNER SKIN FOUND CRACKED, ADJACENT TO REFUELING PANEL AT STA 522. FABRICATED REPAIR DOUBLER AS PER SRM 57-10-00 FIGURE 25 VOLUME I AND INSTALLED REPAIR DOUBLER AT LEFT HAND WING FORWARD LEADING EDGE INNER SKIN, ADJACENT TO RJul 14, 2005 · N589FE · Doug MD11SDR 05FDEA01955Skin · crackedLEFT WING, FORWARD FIXED LEADING EDGE INNER SKIN FOUND CRACKED, ADJACENT TO REFUELING PANEL AT STA 512. FABRICATED REPAIR DOUBLER AS PER SRM 57-10-00 FIG. 25 VOL.I AND INSTALLED REPAIR DOUBLER AT LH WING FORWARD FIXED LEADING EDGE INNER SKIN, ADJACENT TO Jul 14, 2005 · N589FE · Doug MD11SDR 05FDEA01954Skin · crackedLEFT WING, FORWARD FIXED LEADING EDGE INNER SKIN FOUND CRACKED, ADJACENT TO NR 4 SLAT STA 540. FABRICATED REPAIR DOUBLER AS PER SRM 57-10-00 FIG. 25 VOL.I AND INSTALLED REPAIR DOUBLER AT LH WING FORWARD FIXED LEADING EDGE INNER SKIN ADJACENT TO NR 4 SLAT STJul 14, 2005 · N589FE · Doug MD11SDR 05FDEA01953Skin · crackedLEFTWING, FORWARD FIXED LEADING EDGE INNER SKIN FOUND CRACKED, ADJACENT TO NR 5 SLAT STA 590 TO STA 600. FABRICATED REPAIR DOUBLER AS PER SRM 57-10-00 FIG. 25 VOL.I AND INSTALLED REPAIR DOUBLER AT LH WING FORWARD FIXED LEADING EDGE INNER SKIN ADJACENT TJul 14, 2005 · N589FE · Doug MD11SDR 05FDEA01901Skin · crackedRT WING, LEADING EDGE SKIN AT STA XORS 797 FOUND WITH 17 IN CRACKED. REPAIR CARRIED OUT AS PER SRM 57-10-00 VOLUME I, FIGURE 37.Jul 13, 2005 · N598FE · Doug MD11SDR 05FDEA01899Access Panel · damagedACCESS PANEL 650GB HAS 1 ELONGATED HOLE, COMPLIED WITH EA6-5710-90863.Jul 12, 2005 · N411FE · Airbus A310SDR 05FDEA01898Access Panel · damagedACCESS PANEL 650 FB HAS 1 ELONGATED HOLE, COMPLIED WITH EA6-5710-90863.Jul 12, 2005 · N411FE · Airbus A310SDR DHL2005746524Skin · crackedC-CHECK CRACK ON R/W TRAILING EDGE UPPER SURFACE AT NR 12 SPOILER NR 2 HINGE CUTOUT. STOP DRILLED CRACK AT NR 12 SPOILER CUTOUT IAW B727 SRM 57-30-04 FIG 10, C/W HFEC IAW NDT M PT6, 51-00-00 FIG 23, CRACK IS CONTAINED. FABBED REPAIR PLATE FROM .071 7075T6 POJul 11, 2005 · N746DH · Boeing 727224SDR 05FDEA01869Panel · corrodedLT WING, UPPER WING, CORROSION FOUND ON FIXED PANEL AND MARKED ON REAR SPAR SECTION AT STA 948. REPAIRED AS PER FEDEX EA 1-5710-90068.Jul 9, 2005 · N589FE · Doug MD11SDR A6WA200540228Skin · corrodedMWC 59 WING PLANK, RT WING, UNDER FUEL ACCESS PANEL 650EB IS SEVERLY CORRODED AROUND ENTIRE CIRCUMFERENCE OF OPENING, .150 INCH WIDE X .005 INCH DEEP. BLENDED LOWER WING PLANK IAW MFG REO. (K)Jul 8, 2005 · N461AW · Cndair CL6002B19SDR IXXA05SMN157SSkin · crackedDURING ROUTINE C CHECK INSPECTION, LT WING. STUB WING UPPER SURFACE STA XS 250.000 XS 240.000 HAS TWO CRACKS OF .5 INCH. PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG. 38, TR NR 57-85, EO SEMAN NR 2005983 DATE 06-18-05. REMOVED FASTENERS IAW SRM 51-1-21 PAGE 1.Jul 6, 2005 · N822BX · Doug DC871FSDR IXXA05SMN156SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, RT WING IB L/E UPPER PART EXTERNAL SKIN CORRODED XS 250.089. PERFORMED MAJOR REPAIR IAW SRM, TR NR 57-85, EO SEMAN NR 2005984 DATE 06-18-05. REMOVED FASTENERS IAW SRM 51-1-21 PAGE 1, SRM. REMOVED CORROSION IAW SRM. FOUND Jul 6, 2005 · N822BX · Doug DC871FSDR PNSA050701Fairing · failedDEPARTED AKN EN ROUTE FOR DLG ON V453, JUST AFTER LEVELING OFF AT 4000 FEET THE AIRCRAFT STARTED SHAKING. CREW DECLARED AN EMERGENCY AND RETURNED TO AKN WITHOUT INCIDENT. MAINTENANCE FOUND LT WING FAIRING P/N 2620014-23 HAD FAILED.Jul 6, 2005 · N9481F · Cessna 208
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