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 QXEA200501613Skin · damagedYYC - DURING C3 CHECK, RIGHT WING UPPER SKIN T/EDGE HAS BROKEN AND LOOSE FASTENERS. REPLACED BROKEN AND LOOSE RIVETS IAW CRJ-700 SRM 51-42-06-001-001-AO1.Oct 31, 2005 · N603QX · Cndair CL6002C10SDR IXXA05RNG094SSkin · corrodedDURING INSPECTION CHECK WAS FOUND A CORROSION ON UPPER SKIN AT OB EXTENDED LEADING EDGE AROUND STA. XFS 791.250 TO 816.000 - LT. DAMAGED AREA WAS CLEANED AND REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-2-1 FIGURE 38 AND EWO ATI-57-059.Oct 31, 2005 · N721CX · Doug DC872SDR I5HA0258010Access Panel · crackedDURING A RECENT SCHEDULED INSPECTION, A FUEL LEAK WAS DISCOVERED ON THE LOWER RT WING NEAR THE IB FUEL TANK ACCESS PANEL. A CRACK LOCATED AT WS 8. A NEW ACCESS PANEL DOUBLER WAS INSTALLED IAW DWG. THE AIRCRAFT WAS RETURNED TO SERVICE. (K)Oct 30, 2005 · N581P · Cvac 580SDR 05FDEA03590Panel · crackedRT WING BOTTOM PNL 675 DB CUT-OUT HAS CRACK.Oct 30, 2005 · N720FD · Airbus A300B4622RSDR IXXA05RNG099SSkin · corrodedDURING INSPECTION CHECK WAS FOUND A CORROSION ON CENTER EXTENDED LEADING EDGE LOWER SKIN AROUND STA XFS 710.50-RT. DAMAGED AREA WAS BLENDED OUT AND A REINFORCEMENT DOUBLER WAS FABRICATED AND INSTALLED IAW EO ATI-092905 AND EWO ATI-57-063. FAA FORM 8110-3 WAS Oct 28, 2005 · N721CX · Doug DC872SDR IXXA05RNG090SSkin · corrodedDURING INSPECTION CHECK CORROSION WAS FOUND ON INNER EXTENDED LEADING EDGE OUTER UPPER SKIN AROUND STA XFS 207.500 - RT. DAMAGED AREA WAS BLENDED OUT AND REINFORCEMENT DOUBLER WAS FABRICATED AND INSTALLED IAW EO ATI-092305 AND EWO ATI-57-055. FAA FORM 8110-3 Oct 28, 2005 · N721CX · Doug DC872SDR IXXA05RNG089SSkin · corrodedDURING INSPECTION CHECK, CORROSION WAS FOUND ON CENTER EXTENDED LEADING EDGE OUTER LOWER SKIN AROUND STA XFS 304.00 - RT. DAMAGED AREA WAS REMOVED AND A REINFORCEMENT DOUBLER WAS FABRICATED AND INSTALLED IAW EO ATI-092205 AND EWO ATI-57-054. FAA FORM 8110-3 Oct 28, 2005 · N721CX · Doug DC872SDR IXXA05RNG091SSkin · corrodedDURING INSPECTION CHECK, FOUND CORROSION ON UPPER SKIN AT OUTBOARD EXTENDED LEADING EDGE AROUND STA XFS 591.250 - 603.750 - RT. CORROSION WAS REMOVED IAW SRM DC8 51-1-8 PAGE 20 AND THICKNESS WAS FOUND OUT OF LIMITS IAW DC8 SRM 57-2-0 PAGE 16 AND ASTME 79701. Oct 28, 2005 · N721CX · Doug DC872SDR IXXA05RNG088SSkin · corrodedDURING INSPECTION CHECK, FOUND CORROSION ON CENTER EXTENDED LEADING EDGE OUTER LOWER SKIN AROUND STA XOLDI 6.225 - RT. CORROSION WAS REMOVED IAW DC8 SRM 51-1-8 PAGE 20 AND THICKNESS WAS FOUND OUT OF LIMITS IAW SRM 57-2-0 PAGE 16 (MAX: 0.063 IN, MIN: 0.035 IN)Oct 28, 2005 · N721CX · Doug DC872SDR 05FDEA03578Skin · crackedLT WING L/E WING TIP FOUND 1 EA CRACK .50 INCH LONG ON EXISTING REPAIR ON LOWER SKIN AT STA XW99. TRIMED OUT CRACKED PORTION SKIN REPAIR IAW SRM 57-00-01 FIG 4 VOL 2 FAB PART IAW DETAIL PART TRAVELER N00550/F160550.Oct 28, 2005 · N302FE · Doug DC1030SDR 05FDEA03574Skin · crackedRT WING OUTBD FLAP CRACK LONG 1 INCH ON UPPER SKIN AT STA XOF787. CUTE DAMAGED AREA AND REPAIRED PER SRM 57-10-00 VOL 1 FIG 85 FAB PART IAW DETAIL PART TRAVELER F160347/N00347 PER SRM57-10-00 VOL 1 SHT 4.Oct 28, 2005 · N302FE · Doug DC1030SDR 05FDEA03571Skin · crackedRT WING L/E CRACK ON CHORD FIXED PANEL AT STA XORS 498. FAB AND INSTALLED REPAIR DOUBLER PER SRM 57-10-00 FIG 49 AND SRM 51-35-01 PAG 1-13. FAB PART IAW DETAIL PART TRAVELER F160742/N00742 PER SRM 57-10-00 FIG 49.Oct 28, 2005 · N302FE · Doug DC1030SDR 05FDEA03568Skin · crackedLT WING L/E NR 517 CT FOUND 1 CRACK 3'' LONG ON SKIN. REPAIRED PANEL IAW SRM 57-10-00 FIG 10-A VOL 1 AND SRM 51-35-01 PAGE 1-13 VOL 2.Oct 28, 2005 · N302FE · Doug DC1030SDR IXXA05RNG114SSkin · corrodedDURING INSPECTION CHECK WAS FOUND A CORROSION ON RT WING CENTER LE UPPER EXTERIOR SURFACE, STA XW 408.343. SKIN WAS REPLACED IAW MFG DRAWING 5769857, RIVETS WERE INSTALLED IAW SRM 51-1-21 PAGE 1-7 AND PROTECTIVE TREATMENT WAS APPLIED IAW SRM 51-1-8 PAGE 13-16Oct 27, 2005 · N721CX · Doug DC872SDR 05FDEA03539Skin · crackedRT WING EXT L/E, CRACK LONG 0,5'' ON EXT SKIN AT STA XORS 804. REPAIRED CRACK PER SRM 57-00-01 FIG 4 SHT 2 VOL 1 AND SRM 51-33-01 PAGE 34-47 FABRICATED PART IAW DETAIL PART TRAVELER F161055/N01055 PER SRM 57-00-01 FIG 4 SHT 2 VOL 1.Oct 27, 2005 · N302FE · Doug DC1030SDR 05FDEA03532Doubler · crackedRT WING INT L/E, CRACK LONG 0,5" ON INTERNAL DOUBLER AT STA XORS 540. REPAIRED BEADED DOUBLER PER SRM 57-10-00 FIG 71 VOL 1 AND SRM 51-35-01 PAGE 1-13 AND SRM 51-33-01 PAGE 34-47. FABRICATED PART IAW DETAIL PART TRAVELER F160799/N00799 PER SRM 57-10-00 FIG 7Oct 27, 2005 · N302FE · Doug DC1030FSDR 05FDEA03531Panel · crackedRT WING INT L/E, CRACK ON CHORD FIXED PANEL AT STA XORS 803. REPAIRED STRINGER DOUBLER PER SRM 57-10-00-00 FIG 49 VOL 1 AND SRM 51-33-01 PAGE 34-47. FABRICATED PART IAW DETAIL PART TRAVELER F161054/N01054 PER SRM 57-10-00 FIG 49 VOL 1.Oct 27, 2005 · N302FE · Doug DC1030FSDR 05FDEA03529Doubler · crackedRT WING INT L/E, 3EA CRACKS ON DOUBLER AT STA XORS 685.REPAIRED BEADED DOUBLER PER SRM 57-10-00 FIG 71 VOL 1 AND SRM 51-35-01 PAGE 1-13 AND 51-33-01 PAGE 34-47. FABRICATED PART IAW DETAIL PART TRAVELER F160836/N00836 PER SRM 57-10-00 FIG 71 VOL 1.Oct 27, 2005 · N302FE · Doug DC1030FSDR 05FDEA03527Doubler · crackedLT WING L/E INT STRUCTURE FOUND 1 EA CRACK 0,5" ON UPPER DOUBLER AT STA XORS 683. REPAIRED BEADED DOUBLER PER SRM 57-10-00 FIG 71 VOL 1 AND SRM 51-35-01 PAGE 1-13 AND 51-33-01 PAGE 34-47. FABRICATED PARTS IAW DETAIL PART TRAVELER F160726/N00726 PER SRM 57-10Oct 27, 2005 · N302FE · Doug DC1030FSDR 05FDEA03526Skin · crackedRT WIND INT L/E, CRACK LONG 1, 5" ON RIB AT STA XOS 450. REPAIRED CRACK PER SRM 57-20-00 FIG 1 SHT 3 VOL 1 AND SRM 51-35-01 PAGE 1-13 AND 51-33-01 PAGE 34-47. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F160840/N00840 PER SRM 57- 20-00 FIG 1 SHT VOL 1.Oct 27, 2005 · N302FE · Doug DC1030FSDR 05FDEA03524Doubler · crackedLT WING L/E INT STRUCTURE FOUND 1 CRACK 5" LONG ON UPPER DOUBLER AT STA XORS 660. REPAIRED BEADED DOUBLER PER SRM 57-10-00 FIG 71 VOL1 AND SRM 51-35-01 PAGE 1-13 AND SRM 51-33-01 PAGE 34-47. FABRICATED PARTS IAW DETAIL PART TRAVELER F160729/N00729 PER SRM 5Oct 27, 2005 · N302FE · Doug DC1030FSDR 05FDEA03522Panel · crackedFOUND RT WING L/E, CRACK ON CHORD FIXED PANEL AT STA XORS 442. INSTALLED REPAIR DOUBLER PER SRM 57-10-00 FIG 49 AND SRM 51-33-01 PAGE 34-47. FABRICATED PARTS IAW DETAIL PART TRAVELER F160798/N00798 PER SRM 57-10-00 FIG 49.Oct 27, 2005 · N302FE · Doug DC1030FSDR 05FDEA03498Skin · corrodedIN THE LT WING REAR SPAR AT STA XORS 338 FOUND CORROSION EXFOLIATION ON UPPER SKIN PANEL SUPPORT. REPAIRED IAW SRM 57-00-01 FIG 3 SHEET 2 VOL 1.Oct 26, 2005 · N556FE · Doug DC1010SDR 05FDEA03497Skin · corrodedIN THE LT WING REAR SPAR AT STA XORS 308 FOUND EXFOLIATION CORROSION IN THE UPPER SKIN PANEL SUPPORT. REMOVED CORROSION IAW SRM 51-21-01 PAR 34 FOUND OUT OF LIMITS. REPAIRED IAW SRM 57-00-01 FIG 3 SHEET 2.Oct 26, 2005 · N556FE · Doug DC1010SDR 2005FA0001509Skin · crackedFORWARD WING WALK DOUBLER CRACKED. DOUBLER SHOULD BE HEAVIER GAUGE METAL. (K)Oct 25, 2005 · N35705 · Piper PA28161SDR ERA2005F00003Plate · crackedFOUND WHILE AIRCRAFT UNDERGOING C1-CHECK, AWC 19419. FOUND CRACK IN RT IB LADDER PLATE BETWEEN STRINGER 4 AND 6 AT WING STA YW137. REPAIRED IAW RD. (K)Oct 24, 2005 · N881EA · Dhav DHC8103SDR 05FDEA03478Skin · crackedRT WING DROOP L/E UPPER SKIN FOUND WITH CRACK. RT WING DROOP L/E UPPER SKIN CRACK CARRIED OUT REPAIR AS PER SRM 57- 10-00 FIG.26 VOL.I. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Oct 21, 2005 · N574FE · Doug MD11SDR P5CA0501407Skin · corrodedCORROSION ON RT UPPER SKIN AFT OF REAR SPAR WS 560 TO 575. REMOVED CORROSION & REPAIRED IAW BOEING REPAIR PROCEDURE 1-129539127-5 AND 8100-9.Oct 19, 2005 · N921FT · Boeing 747283BSDR QXEA200501385Access Panel · damagedPDX - THE LEFT WING LADDER PLATE FOR ACCESS PANEL 522AT HAS A CHIP IN THE EDGE OF THE SIXTH SCREW HOLE IN THE AFT ROW, COUNTING FROM THE INBOARD AFT EDGE. REPAIRED IAW RD 8-57-1471 AND HORIZON AIR EA 2-57-333.Oct 18, 2005 · N345PH · Dhav DHC8202SDR LR7A05164Panel · crackedDURING C-6 CHECK PER SB 382-57-85, FOUND CRACKS IN NR 3 CENTER WING LOWER SURFACE PANEL, FS 597, LBL 60. REPAIRED IAW LOCKHEED REPAIR TASK 39 UNDER GLD 1720 (SK382-57-296) PER LAC MEA382-57-05-086, NR 0459.Oct 17, 2005 · N403LC · Lkheed 382GSDR LR7A05162Skin Panel · corrodedDURING C-6 CHECK PER HC5711, FOUND LEFT HAND CENTER WING LOWER PLANK CORROSION CWS171-213. REPAIRED IAW DRAWING R05-025-05 PER LAC MEA382-57-05-077, NR 0416.Oct 17, 2005 · N403LC · Lkheed 382GSDR DHLA102005AASkin · crackedLEFT WING SKIN CRACKED AT STRINGER 64 LT. APPROX XRS 450 AT FASTENER HOLE FOUND WHILE ACCOMPLISHING S/B 57-100 INSPECTIONOct 17, 2005 · N801DH · Doug DC873FSDR CA060328003Skin · corrodedON DE-ICER BOOT REPLACEMENT DUE TO WEAR AND CONDITION FOUND LT WING AND LT HORIZONTAL STAB LEADING EDGE SKINS CORRODED. THERE WERE HOLES THROUGH THE METAL. SKINS WERE BEYOND REPAIR AND HAD TO BE REPLACED. RT SIDE WAS FOUND OK.Oct 15, 2005 · Piper PA31SDR IXXA05SMN261SDoubler · corrodedDURING ROUTINE C CHECK INSPECTION, LT OUTER WING, OTBD L/E ACCESS DOOR INTERNAL DOUBLER CORRODED, XFS 847.500. REMOVED CORROSION IAW DC8 SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW DC8 SRM 57-2-0 PG 16. REMOVED CORRODED INTERNAL DOUBLER IAW DC8 SRM 51-1-21Oct 13, 2005 · N829BX · Doug DC871FSDR IXXA05SMN241SDoubler · crackedDURING ROUTINE C CHECK INSPECTION, RT INNER WING CTR L/E INTERNAL DOUBLER CRACK 3 AT STA XFS 250.000. REMOVED CRACKED INTERNAL DOUBLER IAW DC8 SRM 51-1-21. FABRICATED NEW INTERNAL DOUBLER (AL7075T6 0.063”) IAW DC8 SRM 57-3-1 FIG 3. CLEANED, TREATED, PRIMED Oct 13, 2005 · N829BX · Doug DC871FSDR IXXA05SMN238SDoubler · crackedDURING ROUTINE C-CHECK INSPECTION, LEFT WING CTR L/E LWR INTERNAL DOUBLER CRACK 2 AT STA XFS 342.500. REMOVED CRACKED INTERNAL DOUBLER IAW DC8 SRM 51-1-21, DC8 SRM 51-1-20D. FABRICATED NEW INTERNAL DOUBLER (AL7075T6 0.090”) IAW DC8 SRM 57-3-1 FIG 4. CLEANEDOct 13, 2005 · N829BX · Doug DC871FSDR IXXA05SMN237SDoubler · crackedDURING C CHECK INSPECTION, LT WING CTR L/E LWR PART INTERNAL DOUBLER CRACKED 7, XFS 341.500. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05463 DATED 10-11-05, SEMAN DWG # ED-4083 DATED 10-10-05, EO SEMAN # 20051312 DATED 10-11-05. REMOVED EXISTING REPAIR DOct 13, 2005 · N829BX · Doug DC871FSDR IXXA05SMN232SDoubler · improperDURING ROUTINE C-CHECK INSPECTION, LEFT INBOARD FLAP L/E UPPER SKIN HAS NON STANDARD REPAIR, XW 105.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 SRM 57-7-1, EO SEMAN 20051209. REMOVED DAMAGED PANEL PLATING IAW DC8 SRM 57-1-0 PG 1, DC8 SRM 51-1-21. FABOct 13, 2005 · N829BX · Doug DC871FSDR IXXA05SMN231SSkin · improperDURING C CHECK INSPECT, LT INBD FLAP L/E UPPER SKIN HAS NON STANDARD REPAIR, XW 91.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 # 05446 DATED 10-05-05, SEMAN DWG # ED 4065 DATED 09-27-05, EO SEMAN # 20051208 DATED 10-05-05. REMOVED NON STANDARD REPAIR IAWOct 13, 2005 · N829BX · Doug DC871FSDR IXXA05SMN230SSkin · dentedDURING C CHECK INSPECT, LT INBD FLAP UPPER SKIN DENTED, XW 77.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 SRM 57-2-5 FIG 1, EO SEMAN #20051207 DATED 09-21-05. REMOVED FASTENERS IAW DC8 SRM 51-1-21, DC8 SRM 51-1-21, DC8 SRM 51-3-0. REMOVED DAMAGED SECOct 13, 2005 · N829BX · Doug DC871FSDR P5CA0501405Skin · corrodedLEFT WING LOWER SKIN CORROSION ON OUTBOARD JACK PAD AREA AT FSS 1295. REPAIR CARRIED OUT IAW BOEING FAA FORM 8100-9. SUPPLEMENTARY JOB CARDS AFM 0147 AND AFM 1068 FOR DETAILS.Oct 13, 2005 · N920FT · Boeing 747249FSDR VTZA200500200Skin · crackedRIGHT WING PLANK AT WS 148.019 IS CRACKED.Oct 13, 2005 · N621BR · Cndair CL6002B19SDR DHL2005801014Plate · unknownNR 4 ALT TANK PLATE 505A REMOVED FOR ACCESS. FOUND CRACK FOUND ON VISUAL INSPECTION R/WING WND OF STRINGER 64 APPROX 1" LONG FRONT TO REAR O/B FASTENER AND BY HIGH FREQ EDDY CURRENT. ACP HIGH FREQ EDDY CURRENT INSP. OF LOWER WING SKIN LT SIDE OF LWR WING. OOct 12, 2005 · N801DH · Doug DC873FSDR 05FDEA03401Skin · chafedLEFT WING O/B UPPER SURFACE HAS 4 EA CHAFE MARKS. COMPLIED WITH EA 6-5750-93355 REF N00076.Oct 12, 2005 · N681FE · Airbus A300B4605RSDR 05FDEA03355Doubler · crackedSNRM N0605 : RIGHT HAND WING FIXED LEADING EDGE INTERNAL RIB DOUBLER FOUND CRACKED AT XORS 680. CORRECTIVE ACTION: SNRM N0605 : CRACKED INTERNAL RIB DOUBLER AT RIGHT HAND WING FIXED LEADING EDGE XORS 680 REMOVED AS PER SRM 51-31-01 VOLUME II. NEW Oct 11, 2005 · N610FE · Doug MD11SDR 05FDEA03350Doubler · crackedLEFT HAND WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER FOUND CRACKED AT XORS 653. FASTENERS ON CRACKED INTERNAL BEADED DOUBLER AT XORS 653 OF LEFT HAND WING FIXED LEADING EDGE REMOVED AS PER SRM 51-31-01 VOLUME II. REPAIR DOUBLER FABRICATED AS PER SRM Oct 11, 2005 · N610FE · Doug MD11SDR 05FDEA03348Doubler · crackedLEFT HAND WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER FOUND CRACKED AT XORS 663. FASTENERS ON CRACKED INTERNAL BEADED DOUBLER AT XORS 663 OF LEFT HAND WING FIXED LEADING EDGE REMOVED AS PER SRM 51-31-01 VOLUME II. REPAIR DOUBLER FABRICATED AS PER SOct 11, 2005 · N610FE · Doug MD11SDR 05FDEA03351Doubler · crackedLT WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER FOUND CRACKED AT XORS 628. FASTENERS AT LT WING FIXED LEADING EDGE CRACKED INTERNAL BEADED DOUBLER AT XORS 628 REMOVED AS PER SRM 51-31-01 VOLUME II. REPAIR DOUBLER FABRICATED AS PER SRM 57-10-00 FIGURE 25Oct 11, 2005 · N610FE · Doug MD11SDR 05FDEA03347Skin · crackedLEFT WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER FOUND CRACKED AT XORS 598. TRIMMED OUT AS PER FEDEX EA 1-5710-89996, FABRICATED AND INSTALLED AS PER FEDEX EA 1-5710-89996.Oct 11, 2005 · N610FE · Doug MD11SDR 05FDEA03344Doubler · crackedLEFT WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER FOUND CRACKED AT XORS 538. RIMMED OUT AS PER FEDEX EA 1-5710-89995. REPAIR DOUBLER AND ANGLE FABRICATED AND INSTALLED AS PER FEDEX EA 1-5710-89995 REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100.Oct 11, 2005 · N610FE · Doug MD11
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