JASC 5720

Service difficulty reports · 13,638

Reports filed under 5720 · Wing Miscellaneous Structure, 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 = '5720'
  ORDER BY difficulty_date DESC"

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SDR 05FDEA03525Intercostal · crackedRT WING INT L/E CRACK LONG 1,5" ON INTERCOSTAL AT STA XORS 980. REPAIRED CRACK INSTALLED 2 ANGLE PER SRM 57-00-01 FIG 3 SHT 2 VOL 1 AND SRM 51-35-01 PAGE 1-13 AND 51-33-01 PAG 34-47. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F160838-N00838 PER SRM 57-00-Oct 27, 2005 · N302FE · Doug DC1030SDR SWIA200516155Angle · crackedLEFT WHEEL WELL BAT ANGLE CRACKED, ITEM FOUND AT C-CHECK INSPECTION. INSTALLED ANGLE DOUBLER PER REO 601R-57-51-046 STEP 5-8 REV B.Oct 22, 2005 · N595SW · Cndair CL6002B19SDR 2005FA0001631Support Bracket · crackedWING T/E SKIN SUPPT BRACKET CRACKED IN BEND RADIUS. LOCATION OF CRACKED PART IS IB SIDE OF RT FLAP TRACK RIB AT STA 39. PART HAS .2500 INCH CRACK FROM L/E OF TAB AFT, ANOTHER CRACK IN SAME BEND RADIUS .7500 INCH FROM T/E OF TAB FWD. BEND RADIUS CRACK IS UNDOct 14, 2005 · N54844 · Cessna 172PSDR IXXA05SMN240SPan · crackedDURING ROUTINE C CHECK INSPECTION, RT INNER WING OUTBD L/E ZEE PAN CRACK 2” AT STA XS 250.089. REMOVED CRACKED SPLICE PAN IAW DC8 SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8B. INSTALLED NEW SPLICE PAN IAW DC8 SRM 51-1-21, DC8 SRM 51-1-2Oct 13, 2005 · N829BX · Doug DC871FSDR EIA2005229Support Bracket · crackedLHW NR 2 FLAP TRACK CANOE FAIRING AFT SUPPORT FRAME CRACKED. REPAIRED DEFECTIVE CRACKED FRAME PER SRM 51-40-04, FIG 2.Oct 7, 2005 · N486EV · Boeing 747212BSDR AWXA200501324Angle · crackedMCN - DURING C18 CHECK DISCOVERED ANGLE CRACKED AT LOWER LEFT WING, INSIDE TOP LT PYLON PANEL NR 57720L, AT FSS 237. MAINTENANCE REMOVED DAMAGED ZEE ANGLE IAW BOEING 737-300 SRM 51-40-02-0R. FORMED NEW ZEE ANGLE IAW BOEING DWG 65C26701 SHEET 1 REV D. INSTALOct 6, 2005 · N315AW · Boeing 7373S3SDR CA051004009Angle · cracked(CAN) LT AND RT ANGLES FOUND CRACKED WHEN DOING SB 215-454R3 PART B.Sep 30, 2005 · Cndair CL2151A10SDR QXEA200501325Bracket · loosePDX: LT TRAILING WING BOX BRACKET IS LOOSE YW 60. MAINTENANCE REMOVED 2 CHERRY MAX RIVETS IAW Q400 SRM 51-42-45-330-801, PAR 1-6A AND C. DRILLED HOLES TO AN ALTERNATE FASTENER SIZE REF RD 8/4-57-257. HFEC AROUND HOLES IAW 1-84-7A, PT-6, 51-00-02. NO CRACKSSep 28, 2005 · N401QX · Bombdr DHC8402SDR IXXA05RNG069SPlate · temporaryDURING INSPECTION CHECK, FOUND AN INTERIM REPAIR ON INBOARD FLAP UPPER FWD PLATING BETWEEN STA XW91-80, RT. EXISTING DOUBLER WAS REMOVED AND A NEW REINFORCEMENT DOUBLER WAS INSTALLED IAW EO ATI-091105 AND EWO ATI 57-047.Sep 24, 2005 · N721CX · Doug DC872SDR P5CA0501401Support Beam · crackedLEFT WING TRAILING EDGE SUPPORT BEAM UPPER CHORD CRACKED (APPROX 2 INCHES) AT WS 528.20, WBL 235.20.Sep 22, 2005 · N921FT · Boeing 747283BSDR SWIA200516263Angle · crackedRT BATT ANGLE CRACKED, ITEM FOUND AT C CHECK INSPECTION. INSTALLED ANGLE DOUBLER PER REO 601R-57-51-046 REV 'B STEPS 5-10 OF RT BAT ANGLE.Sep 17, 2005 · N405SW · Cndair CL6002B19SDR IXXA05RNG107SFairing · crackedDURING INSPECTION CHECK, FOUND A CRACK ON LT ELEVATOR LOWER SURFACE, STA XE 149.000. FAIRING WAS FABRICATED AND REPLACED IAW DOUGLAS DRAWING 5655694 VIEW C-C, AND RIVETS WERE INSTALLED IAW DC8 SRM 51-1-21 PAGE 1-7.Sep 16, 2005 · N721CX · Doug DC872SDR 2005FA0001328Strip · unserviceableWHILE INSPECTING FOR STORM DAMAGE, DURING THE INSPECTION OF THE AILERON CABLES, FOUND A FLAT SPOT ON THE LT AILERON CROSSOVER CABLE AT THE AILERON CABLE ABRASION STRIP ATTACHED TO A RIB ASSEMBLY LOCATED AT WING STATION 71.19. FURTHER INVESTIGATION FOUND THE CSep 14, 2005 · N2134M · Cessna 172SSDR 2005FA0001327Strip · unserviceableDURING 100 HOUR INSPECTION, WHILE INSPECTING THE AILERON CABLES, FOUND A FLAT SPOT ON THE LT AILERON CROSSOVER CABLE AT THE AILERON CABLE ABRASION STRIP ATTACHED TO A RIB ASSEMBLY LOCATED AT WING STATION 71.19. FURTHER INVESTIGATION FOUND THE CABLE BEGINNINGSep 14, 2005 · N141CW · Cessna 172SSDR IXXA05RNG102SPlate · crackedDURING INSPECTION CHECK, FOUND A CRACK ON CENTER L/E SLOT DOOR PLATING AROUND STA XFS 510.222-LT. DAMAGE WAS REPAIRED IAW EO ATI-092705 AND EWO ATI 57-052.Sep 8, 2005 · N721CX · Doug DC872SDR UPS05845416Stiffener · crackedINSPECTION TYPE: C3, RIGHT WING L/E, OUTBOARD STUB WING L/E STIFFENER CRACKED 1 INCH LONG AT XW 463.000 NR 4 PYLON UPPER. REMOVED CRACKED STIFFENER, FABRICATED AND INSTALLED REPLACEMENT STIFFENER IAW 51-3-0, 51-1-21A, AND DWG 5769891.Sep 4, 2005 · N874UP · Doug DC873FSDR 1050812038Structure · corrodedLT COLLECTOR TANK CORROSION AND SURFACE CORROSION AROUND DRAINS. MORE INFORMATION WILL BE AVAILABLE AT A LATER DATE.Aug 24, 2005 · N143YV · Beech 1900DSDR UPS05245467Stiffener · crackedINSPECTION TYPE:C-CRACK IN VERTICAL STIFFENER LT WING FRONT SPAR AT STA 557. STIFFENER REPLACED IAW SRM 51-30-2 AND DRW NR 65-16200.Aug 23, 2005 · N922UP · Boeing 72731CSDR USAA051038Structure · crackedINTERNAL FUEL TANK AT BOTTOM SKIN AT WBL 13550 CRACKED. FABRICATED NEW T-SECTION & INSTALLED REPAIR T-SECTION IAW EA 96796, DEFECT SIZE: 2.250 INCH.Aug 23, 2005 · N449US · Boeing 7374B7SDR ASAA0540423Web · misdrilledCENTER FUEL CELL, AFT CELL, DRILL START DAMAGE ON UPPER CHORD AND SPANWISE BEAM WEB. REPAIRED DRILL START ON UPPER CHORD AND SPANWISE BEAM. (K)Aug 22, 2005 · N771AS · Boeing 7374Q8SDR 05FDEA02461Channel · crackedRIGHT WING LOWER T/E PANEL SUPPORT BRACKET CRACKED AT WS 519. REMOVED AND REPLACED CHANNEL IAW SRM 51-30-2.Aug 13, 2005 · N479FE · Boeing 727200SDR 05FDEA02393Panel · corrodedCENTRAL WING BOX FOUND SEVERAL CORROSION ON PANEL AT STA 1219 X=104. PERFORMED REPAIR IAW E.A. 1-5720-88880 PT.1.Aug 11, 2005 · N624FE · Doug MD11SDR IXXA05SMN164SVane · damagedDURING C-CHECK INSPECT, LT WING, VANE SLOT L/E HAS INTERIM REPAIR, XOLDI 6.225. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05368 DATED 08-19-05, DWG SEMAN ED-4054 DATED 08-15-05 AND EO SEMAN NR 20051136 DATED 08-19-05. REMOVED NON STANDARD REPAIR IAW DC8 Aug 10, 2005 · N603AL · Doug DC873FSDR 05FDEA02335Angle · damagedLEFT WING FWD INT L/E XOS 667 EXISTING REPAIR ANGLE ON INTERNAL STIFFENER. REPAIR IS IN COMPLIANCE WITH SRM 51-00-01 FIG 100 VOL 1.Aug 9, 2005 · N564FE · Doug DC1010SDR 05FDEA02294Channel · crackedRIGHT WING TRAILING EDGE AT AFT SPAR AREA 3 EA CLOSE OUT PANEL SUPPORTS ARE CRACKED LOCATED UNDER NR 12 & 13 SPOILER PANELS. REMOVED AND REPLACED 3 EACH CHANNEL SUPPORTS IAW SRM 51-30-2.Aug 6, 2005 · N107FE · Boeing 727100SDR 05FDEA02272Web · crackedLEFT WING L/E CRACK LONG 2 INCHES ON INTERNAL WEB AT STA XORS 525. REPAIR IAW SRM 57-10-00 FIG 25 VOL I.Aug 5, 2005 · N624FE · Doug MD11SDR 05FDEA02271Structure · crackedLEFT WING L/E CRACK ON CHORD FIXED PANEL AT STA XORS 450. REPAIR IAW SRM 57-10-00 FIG 18.Aug 5, 2005 · N624FE · Doug MD11SDR 05FDEA02270Splice · crackedRIGHT WING L/E CRACK .5 INCH LONG ON INTERNAL HORIZONTAL SPLICE AT STA XORS 552. REPAIR IAW SRM 51-00-01 VOL I FIG 100.Aug 5, 2005 · N624FE · Doug MD11SDR UPS05445127Web · crackedINSPECTION TYPE:C LEFT WING UPPER WING L/E CAVITY NOSE L/E WEB CRACK AT WS 670-680 ABOVE NR 2 PYLON AREA, (CRACK LENGTH 1.25"). WEB FABRICATED & INSTALLED AS PER SRM 57-20-03 FIG 7.Jul 24, 2005 · N683UP · Boeing 747121SDR UPS05445066Web · corrodedRHW I/B MID FLAP T/E WEB UPR AREA SEVERAL AREA CORROSION REVEAL BETWEEN NR 3 AND NR 4 ARM, COUNT FROM O/B. CORROSION BLEND OUT 0.039" BY 0.5" BY 2" EXCEED SRM 57-50-01 FIG 3 LIMITS, WEB REPAIRED AS PER SRM 51-40-02 FIG 1.Jul 24, 2005 · N683UP · Boeing 747121SDR IXXA05RNG041SPlate · corrodedDURING A ROUTINE C CHECK INSPECTION, FOUND CORROSION AT WING OUTER INBD EXTENDED LE PLATING A STA XFS XW 560 TO SPAR RT. CORROSION ON RT WING L/E LOWER SKIN WAS REMOVED AND REPAIR WAS ACCOMPLISHED IAW EWO ATI-57-033 AND SRM 57-2-1 FIGURE 2H.Jul 23, 2005 · N71CX · Doug DC862FSDR USAA050898Vertical Support · crackedCLT - C6 - VERTICAL STIFFNER, .5 INCH CRACK, WS 537 VERTICAL STIFFNER FWD NR 2 ARERON HINGE, RT WING. DRILLED NEW ANGLE AND INSTALLED IAW SRM. (K)Jul 20, 2005 · N419US · Boeing 737401SDR DHL2005802523Fitting · crackedMAIN TANK INTERIOR LWR SECTION INBD AFT FITTING CRACK STA XRS 74.689 S-61. PERFORMED MAJOR RELPAIR IAW SRM 57-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. CLEANED AND APPLIED TOP COATING MATERIAL TO AREA IAW SRM 51-1-12 PG 7. Jul 17, 2005 · N802DH · Doug DC873SDR DHL2005802536Fitting · crackedNR 2 MAIN TANK INTERIOR OUTBD FWD FITTING CRACKED STA XRS 74.869 S-61 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG.1. REMOVED CRACKED FITTING IAW SRM 51-1-21 PG.1, SRM 51-1-20D PG. 21. CLEANED AND APPLIED TOP COATING MATERIAL TO AREA IAW SRM 51-1-Jul 15, 2005 · N802DH · Doug DC873SDR DHL2005802530Fitting · crackedNR 2 MAIN TANK INTERIOR LWR SECTION OUTBD AFT FITTING CRACKED STA XRS 74.869 S-61 (MAJOR REPAIR). CORR.: PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG.1. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG. 21. CLEANED AND APPLIED TOP COATING MATERIAL TO AREA IAW SRM 51-1-Jul 15, 2005 · N802DH · Doug DC873SDR DHL2005802527Fitting · crackedNR 2 MAIN TANK INTERIOR LOWER SECTION INBD FWD FITTING CRACK, STA XRS 74.869 S-61 (MAJOR REPAIR). CORR.: PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG.1. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG. 21. CLEANED AND APPLIED TOP COATING MATERIAL TO AREA IAW SRM 51-1-Jul 15, 2005 · N802DH · Doug DC873SDR IXXA05SMN158SVane · improperDURING ROUTINE C CHECK INSPECTION, RT WING. OB VANE SLOT HAS INTERIM REPAIR XOLDO 67.000. PERFORMED MAJOR REPAIR, REMOVED EXISTING REPAIR DOUBLER IAW SRM 51-1-21 PAGE 1. REMOVED THE DAMAGED AREA IAW DWG NR ED 4022, PERFORMED NDT INSPECTION. IAW NDT SPM PART 06Jul 6, 2005 · N822BX · Doug DC871FSDR IXXA05SMN146SAngle · deformedDURING ROUTINE C CHECK INSPECTION, LT WING INTERIOR ANGLE DEFORMED, STA XFS -17.500 TO XFS -11.000. PERFORMED MAJOR REPAIR, EO MFG NR 2005948 DATE 06-24-05. REMOVED FASTENERS IAW SRM. REMOVED DAMAGED AREA IAW DWG NR ED 4016, PERFORMED NDT INSPECTION. IAW NDT.Jun 30, 2005 · N822BX · Doug DC871FSDR IXXA05SMN142SVane · misrepairedDURING ROUTINE C CHECK INSPECTION, LT WING SLOT VANE NON STANDARD REPAIR, STA XOLDI 6.235. REMOVED EXISTING REPAIR DOUBLER IAW SRM 51-1-21 PAGE 1. REMOVED DAMAGED AREA IAW SEMAN DWG ED 4003, PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION FOUND. FABRICATED Jun 30, 2005 · N822BX · Doug DC871FSDR IXXA05SMN108SWing · corrodedDURING C CHECK INSPECT, LT WING NR 2 STUB WING UPPER PART CORRODED, XFS 212.000. PERFORMED MAJOR REPAIR IAW DC-8 SRM 57-2-1 FIG 38. TR NR 57-85, EO SEMAN NR 2005848 DATE 06-18-05. REMOVED FASTENERS IAW DC-8 SRM 51-1-21 PG 1, DC-8 SRM 51-1-20D PG 21. REMOVED Jun 27, 2005 · N822BX · Doug DC871FSDR IXXA05SMN107SSkin · improperDURING ROUTINE C CHECK INSPECTION, LH INBD FLAP UPPER PART SKIN NON STANDARD REPAIR, XW 132.000. PERFORMED MAJOR REPAIR IAW DC-8 SRM 57-1-0 PAGE 1, DC-8 SRM 57-7-1 FIG. 1, EO SEMAN NR 2005851 DATE 06-18-05. REMOVED PLATING WITH IMPROPER REPAIR IAW DC-8 SRM 51Jun 27, 2005 · N822BX · Doug DC871FSDR IXXA05SMN102SVane · elongatedDURING ROUTINE C-CHECK INSPECTION, LT WING.- VANE SLOT REPAIR HOLE ELONGATED, XW 454.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3, SEMAN DWG ED 3982, EO SEMAN 2005835. REMOVED FASTENERS IAW DC-8 SRM 51-1-21 PAGE 1, DC-8 SRM 51-1-20D PAGE 21. TRIMMED OUT Jun 27, 2005 · N822BX · Doug DC871FSDR IXXA05SMN101SWeb · crackedDURING ROUTINE C CHECK INSPECTION, LT WING T/E WEB UPPER PART CRACKED 1/2, XCW 69.000. PERFORMED MAJOR REPAIR IAW DC-8 SRM 57-2-6 FIG. 15, EO SEMAN NR 2005836 DATE 06-25-05. REMOVED FASTENERS IAW DC-8 SRM 51-1-20D PAGE 21. REMOVED DAMAGED AREA IAW DC-8 SRM 57-Jun 27, 2005 · N822BX · Doug DC871FSDR ASAA0510182Web · dentedDENT ON WEB ON LT WING RSS 497 APPROX 10 INCHES AFT OF REAR SPAR. REPAIRED IAW SRM. (K)Jun 14, 2005 · N742AS · Boeing 737290CSDR CA050722006Rudder Pedal · crackedPILOT REPORTED THAT RT PARK BRAKE DOES NOT HOLD WHEN SET. UPON MAINTENANCE INSPECTION IT WAS DISCOVERED THAT CAPTAINS OB RUDDER PEDAL INTERCOSTAL MOUNT AT STATION 110.00 WAS CRACKED. IT WAS REPAIRED AS PER CESSNA SRM SECTION 16-38 FIGURE 16-25.May 27, 2005 · Cessna 401ASDR UPS05844574Splice · crackedINSPECTION TYPE:C3 RIGHT WING CENTER L/E INTERNAL DOUBLER SPLICE CRACKED .5 INCH LONG AT XFS 42 9. REMOVED 2 EA CRACKED SPLICES, FABRICATED, AND INSTALLED 2 EA REPLACEMENT SPLICES IAW DC-8 SRM 51-1-20D, DWG 5769589-15 & -17.May 25, 2005 · N840UP · Doug DC873FSDR UPS05844570Doubler · crackedINSPECTION TYPE:C3, RIGHT CTR WING L/E LWR INNER DOUBLER AROUND DRAIN HOLE CRACKED .5 INCH LONG AT XFS 335. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT INNER DOUBLER IAW DC8 SRM 57-3-3 FIG 5 AND 51-1-21.May 25, 2005 · N840UP · Doug DC873FSDR UPS05844569Doubler · crackedINSPECTION TYPE:C3, CENTER WING L/E UPPER INNER DOUBLER CRACKED .5 INCH LONG AT XFS 422. REMOVED INNER DOUBLER, FABRICATED, AND INSTALLED REPLACEMENT DOUBLER IAW DC-8 SRM 51-1-21 AND DWG 5769891.May 25, 2005 · N840UP · Doug DC873FSDR DHL2005807536Fitting · crackedNR 3 MAIN TANK INTERNAL SKIN AFT FITTING CRACKED 3.000 AT STA 74.000 S-51 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG 21. CLEANED AND APPLIED COATING MATERIAL AREA IAW SRM 51-1-12. INSTALLED NEW FMay 16, 2005 · N807DH · Doug DC873FSDR DHL2005807533Fitting · crackedNR 2 MAIN TANK AFT FITTING CRACK 1.500, STA XRS 74.000 OUTBD SIDE, S-51. PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG 21. CLEANED AND APPLIED COATING MATERIAL AREA IAW SRM 51-1-12. INSTALLED NEW FITTING (PN 370484May 16, 2005 · N807DH · Doug DC873F
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