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 UPS08854129Skin · misrepairedINSPECTION TYPE:SV LT WING OUTBOARD L/E HAS A REPAIR DOUBLER INSTALLED THAT DOES NOT MEET SRM SURVEY SEQ 729-W3-10 XFS 701. REPAIRED IAW DC8 SRM 57-2-1 FIG 2H SHT 1 REV 78.Nov 10, 2008 · N729UP · Doug DC871FSDR CALA0801052Skin · crackedRIGHT WING NUMBER 4 SLAT LEADING EDGE SKIN AT ACTUATOR CUTOUT APPEARS TO BE CRACKED. REMOVED ACTUATOR DOOR SEAL ASSEMBLY IAW B737 SRM 57-41-01, STOP DRILLED CRACK IAW B737 SRM 57-41-01. MATERIAL ID 301 1/2 HARD, .040", IC 0649022 IAW B737 SRM 57-41-01, FABRINov 10, 2008 · N16648 · Boeing 737524SDR UPS08854063Skin · misrepairedINSPECTION TYPE:SV RT WING L/E SKIN DOUBLER DOES NOT MEET SRM LIMITS XFS 623. REPAIR IAW UPS EO DC8 5720 31344 A.Nov 6, 2008 · N700UP · Doug DC871FSDR COMA0860460Skin · corrodedLT WING 540BB FUEL PANEL CUTOUT HAS FRETTING CORROSION. REPAIRED LT WING FUEL ACCESS PANEL CUTOUT 540BB AT WS 54.897 AS PER CRJ REO 601R-57-21-030 REV. G FIG 6 DETAIL III.Nov 6, 2008 · N783CA · Cndair CL6002B19SDR COMA0860459Skin · corrodedRT WING 640BB FUEL PANEL CUTOUT HAS FRETTING CORROSION. REPAIRED RT WING FUEL ACCESS PANEL CUTOUT 640BB AT WS 54.897 AS PER CRJ REO 601R-57-21-030 REV. G FIG 6 DETAIL III.Nov 6, 2008 · N783CA · Cndair CL6002B19SDR UPS08853925Skin · damagedINSPECTION TYPE:SV LT WING LEADING EDGE AT STA 700 DOES NOT HAVE REPAIR DOUBLER INSTALLED AS PER APPENDIX H (3)(4) OF EO DC8 5100 30418. INSTALLED DOUBLER AS IAW 57-02-01 FIG 38Nov 6, 2008 · N700UP · Doug DC871FSDR 08FDEA04724Skin · crackedLH WING L/E FOUND CRACK ON SKIN L/E.Nov 5, 2008 · N319FE · Doug DC1030FSDR 08FDEA04714Skin · chafedRT WING O/B MAIN FLAP O/B L/E CORNER HAS 4 INCH CHAFF MARK (FROM LOWER WING PANEL). DEFECT REPAIRED IAW EA F-5750-120571. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.Nov 5, 2008 · N919FD · Boeing 75723ASDR 08FDEA04695Panel · chafedLEFT WING INBD L/E PANEL 516 HB IS CHAFED. BLENDED AREA IAW SRM 57-00-01 VOL I, CHECKED LIMITS, FOUND TO BE OUT OF LIMITS, ORIG THICKNESS .090 BLEND LIMITS 20 PERCENT OR .072 WAS .067 IAW SRM 51-31- 01 VOL II FIG 1. FABRICATED DOUBLER IAW SRM 57-00-01 VOL INov 4, 2008 · N390FE · Doug MD1010FSDR DHLA2008745677Skin · corrodedWING CENTER SECTION, AS ACCESSED THROUGH CABIN, UPPER SKIN CORRODED AT BS 823, BL 0 TO RBL 25. REPAIRED WING CENTER SECTION SKIN DAMAGE AND SPANWISE BEAM BETWEEN RBL 6.5 TO RBL 25 PER EO COO-2-57-284-08 DATED 10/16/08. REFERENCE FAA FORM 8110-3 DATED 10/29/2Nov 3, 2008 · N745DH · Boeing 727224SDR IXXA08SMN219SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING INBOARD CENTER LEADING EDGE LOWER SKIN CRACKED AT STATION XS 520.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. PERFORMED STOP HOLE. PERFORMED NDT INSPECTION. NO CRACK AND NO CORROSION FOUND. FABRICAOct 28, 2008 · N71CX · Doug DC862FSDR UPS08853864Skin · misrepairedINSPECTION TYPE:SV SURVEY SEQUENCE 715-W4-28 STA XFS 310.750 RT WING LEADING EDGE DOUBLER IS STAINLESS STEEL AND IS NOT IN COMPLIANCE WITH SRM APP G. REPAIRED PER EO DC8 5720-31062A.Oct 28, 2008 · N715UP · Doug DC871FSDR UPS08854166Skin · damagedINSPECTION TYPE:SV REPAIR SEQUENCE 803-W3-06 AT LT STUB WING SKIN XFS 249.5 - 258.9 EO DC8-5100-30418-C APPX H STEP 4 IS MARKED NO AND STEP 6&7 ARE MARKED NOT VISIBLE. REMOVED REPAIR, FABRICATED AND INSTALLED REPAIR DOUBLER IAW UPS EO DC8-5730-31485-A AND FVCOct 27, 2008 · N803UP · Doug DC873FSDR UPS08854142Skin · damagedINSPECTION TYPE:SV REPAIR SEQUENCE 803-W3-19 LT STUB WING PLATING XFS 516.5 EO DC8 -5100-30418-C APPX H STEP 6 & 7 ARE MARKED NOT VISIBLE. REMOVED REPAIR DOUBLER, FABRICATED AND INSTALLED REPLACEMENT REPAIR DOUBLER IAW DC-8 SRM 57-02-01A FIG 1 SHEET 1 AND 57-Oct 27, 2008 · N803UP · Doug DC873FSDR UPS08M53758Fairing · damagedINSPECTION TYPE:N/A LT WINGLET UPPER T/E FAIRING DAMAGED. REPAIRED IAW EO MD11-5730-90798-B.Oct 27, 2008 · N259UP · Doug MD11FSDR 08FDEA04578Panel · chafedLEFT WING ANTI-ICE TELESCOPIC ACCESS PANEL FOUND CHAFED. REMOVED AND REPLACED IAW AMM 30-11-01-4. ADJUSTMENT CARRIED OUT IAW AMM 30-11-01-4, FOUND SATISFACTORY.Oct 27, 2008 · N578FE · Doug MD11FSDR UPS08M53724Skin · damagedINSPECTION TYPE:1C RT WING SLAT TRACK 312 CUTOUT LWR O/B CORNER CRACKED. HFEC AREA NO CRACK FOUND, HOWEVER FOUND DAMAGED. CUT OUT DAMAGE IAW SRM VOL 1 57-10-00. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM VOL 1 57-10-00 PG 58.Oct 25, 2008 · N260UP · Doug MD11FSDR UPS08M53723Skin · damagedINSPECTION TYPE:1C LEFT WING FIXED LEADING EDGE HAS SKIN DAMAGE. REF D-370970 AND EO MD11-5730-2877-B EXTENDED EXISTING TRIMOUT PER SAA EA 011-5730-01-A1540. HFEC NO CRACKS NOTED, PER NDTSPM 06-10-01.001. FABRICATED AND INSTALLED WEB RIB P/N AR B2875-5SAAU Oct 25, 2008 · N260UP · Doug MD11FSDR IXXA08SMN202SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING UPPER SKIN CRACKED AT STATION XRS 74.869 STRINGER 9. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN, AND FILLER PLUG. PERFORMED NDT INSPECTION. NO CRACK AND NO COct 24, 2008 · N71CX · Doug DC862FSDR UPS08M53856Skin · crackedINSPECTION TYPE:3C RT WING TELESCOPING DUCT CUTOUT UPPER CORNERS CRACKED. REMOVED DAMAGE, FABRICATED, AND INSTALLED REPAIR DOUBLER IAW MD-11 SRM 57-10-00 FIG 43, 51-33-01 ITEM 16, 51-35-01 ITEM 7.Oct 24, 2008 · N278UP · Doug MD11FSDR UPS08853842Fastener · improper partINSPECTION TYPE:SVN/ SEQ 715-W4-100 RIGHT WING STA XRS 366.300 UPPER LEADING EDGE DOUBLER HAS BLIND FASTENERS NOT CALLED OUT IN SRM. REPLACED FASTENERS AS IAW 57-02-01 FIG 38.Oct 24, 2008 · N715UP · Doug DC871FSDR COMA0860437Skin · damagedFUEL DRAIN FWD OF ACCESS PANELS 640AB AFT DRAIN ATTACH HOLE IS DAMAGED. REAMED AND INSTALLED FREEZE PLUG AT FUEL DRAIN AFT ATTACH HOLE PER COMAIR EA NR 10-5721-02382.Oct 24, 2008 · N781CA · Cndair CL6002B19SDR COMA0860436Skin · damagedFUEL DRAIN FWD OF ACCESS PANELS 610AB FWD AND AFT DRAIN ATTACH HOLES ARE DAMAGED. REAMED AND INSTALLED FREEZE PLUGS AT FUEL DRAIN FWD AND AFT ATTACH HOLES PER COMAIR EA NR 10-5721-02382.Oct 24, 2008 · N781CA · Cndair CL6002B19SDR COMA0860435Skin · damagedFUEL DRAIN FWD OF ACCESS PANELS 640AB AFT DRAIN ATTACH HOLE IS DAMAGED. REAMED AND INSTALLED FREEZE PLUG AT FUEL DRAIN AFT ATTACH HOLE PER COMAIR EA NR 10-5721-02382.Oct 24, 2008 · N781CA · Cndair CL6002B19SDR COMA0860434Skin · damagedFUEL DRAIN INSIDE FUEL ACCESS PANELS 510AB FWD AND AFT DRAIN ATTACH HOLES ARE DAMAGED. REAMED AND INSTALLED SERVICEABLE FREEZE PLUGS AT FUEL DRAIN FWD AND AFT ATTACH HOLES PER COMAIR EA 10-5721-02382.Oct 24, 2008 · N781CA · Cndair CL6002B19SDR 08FDEA04510Skin · cracked04 FASTENER HOLES FOUND CRACK INDICATION DURING OPEN HOLE HFEC INSPECTION AT RIGHT WING LOWER SKIN ACCESS DOOR CUT OUT BETWEEN STA XORS = 690 AND STA XORS = 700. RIGHT WING LOWER SKIN ACCESS DOOR CUT OUT BETWEEN STA XORS = 690 AND STA XORS = 700, 04 FASTEOct 23, 2008 · N578FE · Doug MD11FSDR 08FDEA04509Skin · cracked08 FASTENER HOLES FOUND CRACK INDICATION DURING OPEN HOLE HFEC INSPECTION AT LEFT WING LOWER SKIN ACCESS DOOR CUT OUT BETWEEN STA XORS = 690 AND STA XORS = 700. LEFT WING LOWER SKIN ACCESS DOOR CUT OUT BETWEEN STA XORS = 690 AND STA XORS = 700, 08 EACH FASTOct 23, 2008 · N578FE · Doug MD11FSDR ASAA0843744Skin · dentedRIGHT WING INBOARD LEADING EDGE DENTED. REMOVED DAMAGED AREA. INSTALLED DOUBLER AND FILLER PER SRM 57 41 01.Oct 23, 2008 · N792AS · Boeing 737490SDR UPS08854134Skin · damagedINSPECTION TYPE:SV REPAIR SEQUENCE 803-W3-11 LT WING O/B LEADING EDGE SKIN PLATING XFS 534.1 EO DC8-5100-30418-C APPX H IS MARKED NOT VISIBLE ON STEP 6&7. REMOVED REPAIR DOUBLER, CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW DC-8 SRM Oct 22, 2008 · N803UP · Doug DC873FSDR IXXA08SMN190SSkin · corrodedDURING ROUTINE C-CHECK INSPECTION, FOUND LT WING INBOARD OUTER L/E UPPER EXTERNAL SKIN CORRODED AT STATION XFS 560.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. Oct 21, 2008 · N71CX · Doug DC862FSDR IXXA08SMN189SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND LT WING LOWER CENTER OUTER LEADING EDGE SKIN CORRODED AT STATION XFS 280.250.REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NOOct 21, 2008 · N71CX · Doug DC862FSDR IXXA08SMN188SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING OUTBOARD OUTER LEADING EDGE UPPER EXTERNAL SKIN CORRODED AT STATION XW 762.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK AOct 21, 2008 · N71CX · Doug DC862FSDR UPS08853773Skin · misrepairedINSPECTION TYPE:SV SURVEY SEQUENCE 702-W4-15, RT LEADING EDGE ACCESS PNL DOUBLER LOCATION 477.750 NOT IN COMPLIANCE WITH SRM (NO SRM REPAIR). VERIFIED DOUBLER MEETS SRM 57-02-00 FIG 2A & TR 57-84.Oct 21, 2008 · N702UP · Doug DC871FSDR 08FDEA04454Skin · corrodedSUB-SURFACE CORROSION FOUND ON THE RT WING SKIN UPPER PANEL COMPLIDE WITH EA NR 6-5710-125470.Oct 21, 2008 · N725FD · Airbus A300B4622RSDR UPS08854128Skin · misrepairedINSPECTION TYPE:SV REPAIR SEQUENCE 803-W4-02 RT WING STA XFS 265 - XFS 527 REPAIR DOUBLER THINNER THAN BASE STRUCTURE. REMOVED REPAIR DOUBLER, CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW DC-8 SRM 57-02-01 FIG 38 SHEET 1.Oct 20, 2008 · N803UP · Doug DC873FSDR COEA0808917Panel · corrodedFOUND AT COE MAJOR REPAIR AND LEVEL 2 CORROSION. CORROSION ON CENTER WING UPPER SKIN, ON THE CUTOUT FLANGE FOR PANEL 622CT.Oct 20, 2008 · N917FX · Aerosp ATR42300SDR UPS08853831Skin · damagedINSPECTION TYPE:SV LT WING CENTER L/E UPPER AFT EDGE HAS A STEEL REPAIR DOUBLER INSTALLED AT STA XFS 396-404. INSTALLED CONICAL WASHER REPAIR DOUBLER AND FILLER 4 EA IAW DC8 SRM 57-2-1 REV 78.Oct 20, 2008 · N715UP · Doug DC871FSDR UPS08853830Skin · damagedINSPECTION TYPE:SV LT WING CENTER L/E UPPER AFT EDGE HAS A STEEL REPAIR DOUBLER INSTALLED AT STA XFS 297-299. INSTALL CONICAL WASHERS, REPAIR DOUBLER FILLER 4EA IAW DC8 SRM 57-2-1 REV 78.Oct 20, 2008 · N715UP · Doug DC871FSDR 08FDEA04446Skin · chafedLEFT WING, OUTBD LOWER L/E NOSE PANELS ARE CHAFED ON THE INBD EDGE FROM 34 INCHES OUTBD. FOUND OUT OF LIMITS. REMOVED PANEL IAW SRM 51-35-01 & SRM 51-33-01. FABRICATED A NEW PANEL IAW TPS 1003. LOCATED & DRILLED HOLES IAW DWG ARC 1109-37. ALODINED & PRIOct 20, 2008 · N390FE · Doug MD1010FSDR HNAA2009012500027Skin · corrodedCORROSION FOUND ON LOWER SKIN OF THE RT WING BETWEEN STA 130.0 TO 145 AT REAR ON RT WING AT REAR SPAR, LOWER FLAP SHROUD. P/N 85730018-011 R&R IAW STRUCTURAL REPAIR MANUAL 51-40-00.Oct 17, 2008 · N327EN · Dhav DHC8311SDR UPS08M53693Skin · crackedINSPECTION TYPE:1C LT WING FIXED L/E TELESCOPIC DUCT CUTOUT FOUND CRACKED AS MARKED. CUT OUT CRACK, FABRICATED, AND INSTALLED DOUBLER IAW MD-11 SRM VOL 1 57-10-00 PG 133.Oct 17, 2008 · N288UP · Doug MD11FSDR 08FDEA04396Panel · chafedRIGHT WING INBD LOWER T/E PANEL 641 KB IS CHAFED. REPAIRED RT WING INBD LOWER T/E PANEL 641 KB BY FABRICATING A DOUBLER & BONDING IT TO THE PANEL. SEALING & RESTORING THE FINISH IAW 51-71-00.Oct 17, 2008 · N390FE · Doug MD1010FSDR 08FDEA04394Panel · chafedLEFT WING INBD LOWER T/E PANEL 541 FB IS CHAFED. REPAIRED CHAFED AREAS BY BLENDING AND FOUND OUT IF LIMITS. FABRICATED REPAIR DOUBLER & BONDED IAW SRM 51-71-00, 51-21-01 & 51-31-01. ALODINED, PRIMED & SEALED IAW SRM 51-21-01. RE-INSTALLED HINGE REMOVED TOOct 17, 2008 · N390FE · Doug MD1010FSDR 08FDEA04393Panel · chafedLEFT WING INBD LOWER T/E PANEL 541 KB IS CHAFED. REPAIRED PANEL BY BONDING A DOUBLER IAW SRM 51-71-00. REMOVED & RE-INSTALLED PANEL IAW SRM 51-31-01.Oct 17, 2008 · N390FE · Doug MD1010FSDR 08FDEA04379Skin · crackedCRACK FOUND ON 7 EACH FASTENER HOLES ON RIGHT WING AT LOWER WING SKIN OUTER ACCESS DOOR CUTOUT AT PANEL NR 636AB. 7 CRACKED FASTENER HOLES ON RT WING LOWER WING SKIN REPAIRED AS PER E.A. 1-5710-125558, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Oct 16, 2008 · N607FE · Doug MD11FSDR 08FDEA04378Skin · damagedCHIPPED EDGE FOUND ON 1 FASTENER HOLE ON LEFT WING AT LOWER WING SKIN OUTER ACCESS DOOR CUTOUT AT PANEL NR 536AB. REPAIR CARRIED OUT AT LEFT HAND WING AT LOWER WING SKIN. 01 EACH HOLE AT OUTER ACCESS DOOR CUTOUT AT PANEL NR 536AB AS PER E.A. 1-5710-125559, Oct 16, 2008 · N607FE · Doug MD11FSDR 08FDEA04377Skin · crackedCRACK FOUND ON 3 FASTENER HOLES ON LEFT WING AT LOWER WING SKIN OUTER ACCESS DOOR CUTOUT AT PANEL NR 536AB. 3 CRACKED FASTENER HOLES ON LEFT HAND WING AT LOWER WING SKIN REPAIRED AS PER EA 1-5710-125557, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Oct 16, 2008 · N607FE · Doug MD11FSDR COMA0860425Skin · crackedDURING HMV4 LT WING PLANK INSPECTION NDT FOUND CRACK INDICATION AT FUEL DRAIN MOUNT HOLES WS 12 AND WS 60. DAMAGE REMOVED BY OVERSIZING HOLES AND INSTALLING FREEZE PLUGS PER EA 10-5721-02374.Oct 15, 2008 · N436CA · Cndair CL6002B19SDR 08FDEA04368Panel · crackedRIGHT WING LOWER T/E PANEL 641 GB IS CRACKED. FABRICATED PANEL IAW DWG ARC 0389. ALODINED & PRIMED IAW SRM 51-21-01. PAINTED PANEL IAW SRM 51-21-02. PART MARKED PANEL AMM 7-0-1000.Oct 15, 2008 · N390FE · Doug MD1010FSDR 08FDEA04352Skin · crackedLT WING L/E CRACK ON EXT LOWER SKIN.Oct 15, 2008 · N319FE · Doug DC1030F
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