JASC 5754

Service difficulty reports · 17,348

Reports filed under 5754 · Leading Edge Devices, 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 = '5754'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR RRXA001796Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACKED UPPER RIB ON THE LT CENTER L/E AT STA XFS 297.500, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK, FABRICATED AND INSTALLED DOUBLER IAW DC-8 SRM 57-2-0Mar 22, 2000 · N961R · Doug DC873FSDR DL72K000641Skin · wornAT HMV THE SKIN ON 4 L/E SLAT WAS WORN ON UPPER AND LWR SURFACES I/B TRACK. AREA BURNISHED REPAIR DOUBLER MANUF INSTALLED DOUBLER PER MM 57-54-0 FIG 813.Mar 22, 2000 · N410DA · Boeing 727232SDR DL72K000640Rib · crackedAT HMV A RIB WAS FOUND CRACKED ON 4 L/E SLAT I/B END. REPAIRED PER 57-54-0 FIG 814.Mar 22, 2000 · N410DA · Boeing 727232SDR DL72K000639Rib · crackedAT HMV 4 L/E SLAT RIB WAS FOUND CRACKED ON O/B END. REPLACED PER MM 57-54-0 FIG 814. DYE CHECKED, FOUND NO CRACKS.Mar 22, 2000 · N410DA · Boeing 727232SDR CALA0000328Skin · crackedINSPECTION FOUND SEVERAL .25 INCH CRACKS IN NR 6 L/E SLAT LOWER SIDE OF SKIN AT HYDRAULIC ACTUATOR AREA. THE SLAT WAS REPAIRED IAW ECRA 5750-02586 AND BOEING DRAWING NR 65C30133.Mar 22, 2000 · N14336 · Boeing 7373T0SDR RRXA001936Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK EXTENDING BEYOND STOP DRILL AT LT WING CENTER L/E LWR RIB AT STA XFS 304.000 PANEL 523, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED RMar 21, 2000 · N961R · Doug DC873FSDR RRXA001935Rib · misrepairedDURING A MAINTENANCE VISIT FOUND AN IMPROPER REPAIR LT WING CENTER L/E LWR RIB AT STA XFS 310.250, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 51-1-21 ANDMar 21, 2000 · N961R · Doug DC873FSDR RRXA001933Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE LEFT WING LWR L/E LWR RIB DOUBLER AT STA XFS 297.500, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 57-2-0 AMar 21, 2000 · N961R · Doug DC873FSDR RRXA001801Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK EXTENDING BEYOND STOP DRILL LT WING CENTER LEADING EDGE LOWER RIB AT STA XFS 304.000 PANEL 523, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACKMar 21, 2000 · N961R · Doug DC873FSDR RRXA001800Rib · misrepairedDURING A MAINTENANCE VISIT FOUND AN IMPROPER REPAIR TO THE LT WING CENTER LEADING EDGE LOWER RIB AT XFS 310.250, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SMar 21, 2000 · N961R · Doug DC873FSDR RRXA001798Rib Doubler · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE DOUBLER REPAIR ON THE LT WING LOWER LEADING EDGE LOWER RIB AT STA XFS 297.500, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK, FABRICATMar 21, 2000 · N961R · Doug DC873FSDR RRXA001783Baffle · crackedDURING A MAINTENANCE VISIT, FOUND CRACKED DE-ICE HOLES INSIDE ACCESS PANEL 522A AT THE LT WING CENTER LE AT STA XFS 322.750 AND 316.500, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK, APPLMar 21, 2000 · N961R · Doug DC873FSDR RRXA001925Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE RIB AT THE LT LEADING EDGE LWR RIB AT STA XFS 360, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-0.Mar 20, 2000 · N961R · Doug DC873FSDR RRXA001909Web · crackedDURING A MAINTENANCE VISIT FOUND A CRACK IN UPPER WEB LEFT WING O/B LEADING EDGE I/B SECTION AT STA 610.000 ACCESS PANEL 519L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUMar 20, 2000 · N961R · Doug DC873FSDR RRXA001790Rib · crackedDURING A MAINTENANCE VISIT FOUND A PREVIOUS REPAIR ON RIB CRACKED AT LT LE LWR. RIB AT STA XFS 360, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. INSTALLED REPAIR DOUBLER IAW DC-8 SRM 57-2-0.Mar 20, 2000 · N961R · Doug DC873FSDR DL72S000797Skin · crackedNR 5 SLAT LOWER SKIN WORN O/B OF O/B ALIGNMENT SPADE. CUT INNER SKIN MADE NEW SKIN DOUBLERS. REPAIRED PER MM 57-54-0 FIG 801.Mar 20, 2000 · N519DA · Boeing 727232SDR RRXA000990Structure · damagedDURING A MAINTENANCE VISIT, FOUND ELONGATED SCREW HOLES LT WING IB LE LWR. SURFACE AT STA XFS 107 TO 113, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. SCREW HOLES ARE WITHIN ALLOWABLE CRITERION IAW E.OMar 17, 2000 · N994CF · Doug DC862SDR RRXA000877Skin · crackedDURING A MAINTENANCE VISIT FOUND AN ENLARGED AND ELONGATED SCREW HOLE ON THE LT WING O/B SLOT LE I/B END AT STA XS 520, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8.Mar 17, 2000 · N994CF · Doug DC862SDR RRXA000876Skin · crackedDURING A MAINTENANCE VISIT FOUND A CRACK EMANATING FROM A SCREW HOLE LT WING CENTER LE AT O/B SLOT LE AT STA XS 520, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8.Mar 17, 2000 · N994CF · Doug DC862SDR P2EA00089Skin · crackedYXD - DURING C-CHECK, FOUND LEFT WING LE SKIN NR 3 SLAT ARM CUTOUT AT WSS 42 WBL 227 AND WSS 90 WBL 279 WITH CRACKS, LENGTH .600 INCH AND .450 INCH. REPAIRED LEFT WING LEADING EDGE SKIN AT NR 3 SLAT ARM CUTOUT WSS 42 WBL 227 AND WSS 90 WBL 279 PER BOEING SRM Mar 16, 2000 · N121NJ · Boeing 7372Q8SDR DL72W000647Bracket · crackedFOUND AT MV2 CHECK, NR 7 SLAT ACTUATOR O/B MOUNT BRACKET CRACKED AT LWR END. REPAIR PER M/M 57-42-0.Mar 16, 2000 · N293WA · Boeing 727247SDR DHL200072410CAngle · crackedAT C-CHECK FOUND NR 6 L/E SLAT I/B TRACK ROLLER SUPPORT WEBS I/B AND O/B VERTICAL ATTCH ANGLES CRACKED AT LOWER SPAR. REMOVED NR 6 L/E SLAT TO AFILIATE SHEET METAL REPAIR IAW B727 M/M 27-81-11. REMOVED HYD LINES IAW M/M 27-81-0. REMOVED NR 6 SLAT ROLLER ANDMar 16, 2000 · N724DH · Boeing 727228SDR SWAA000509Skin · crackedDURING SCHEDULED C2 CHECK, FOUND NR 3 L/E SLAT LOWER SKIN CRACKED 2.5 INCHES LONG NEAR OUTBOARD END. REPAIRED SLAT PER RA # 1-A57-0555.Mar 15, 2000 · N81SW · Boeing 7372H4SDR RRXA001745Skin · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK TO THE RT WING LEADING EDGE SKIN AT THE INBD PRESSURE FUELING RECEPTICAL AT XRS 261, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW Mar 10, 2000 · N2674U · Doug DC873FSDR RRXA001746Skin · crackedDURING A MAINTENANCE VISIT, FOUND A 5 INCH CRACK ON THE LWR SURFACE OF THE RT WING LE SKIN APPROX. 16 INCHES FWD OF THE WING FRONT SPAR AT XRS 255, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED ANMar 8, 2000 · N2674U · Doug DC873FSDR DL72S000795Rib · crackedNR 3 SLAT RIB NR 6 CRACKED. INSTALLED DOUBLER PER MM 57-54-00 PG 818.Mar 7, 2000 · N419DA · Boeing 727232SDR DHL200072465CStop · crackedAT C CHECK, FOUND RT WING NR 6 SLAT I/B STOP BLOCK CRACKED. REMOVED AND REPLACED STOP BLOCK PER SRM51-30-2.Mar 7, 2000 · N724DH · Boeing 727228SDR DHL200072431CAngle · crackedAT C CHK FOUND NR 6 LE SLAT O/B TRACK ROLLER SUPPORT WEB O/B VERTICAL ATTACH ANGLE IS CRACKED BETWEEN FASTNERS AT LOWER SPAR CHORD. CLEANED AREA NR 6 LE SLAT O/B TRACK ROLLER SUPPORT WEB O/B VERTICAL ATTCH ANGLE BETWEEN FASTNERS AT LOWER SPAR CHORD PER SRM 51Mar 6, 2000 · N724DH · Boeing 727228SDR TWAA0003810Skin · delaminatedDURING CHECK-C MAINT, THE RT WING NUMBER 7 LE SLAT HAD A REPAIR 3.5 INCH BY 2.75 INCH THAT WAS DELAMINATED ON INBD SIDE. INSTALLED A 3.5 INCH BY 2.75 INCH HOT BOND REPAIR PER SRM 51-70-10.Mar 6, 2000 · N603TW · Boeing 767231SDR TWAA0003809Skin · delaminatedDURING CHECK-C MAINT, THE RT WING NR 7 LE SLAT HAD A REPAIR 2 FT 9 IN BY 4.75 INCH THAT WAS DELAMINATED AT THE OBTD TE. INSTALLED A 3 FT BY 4.75 INCH HOT BOND REPAIR PER SRM 51-70-10.Mar 4, 2000 · N603TW · Boeing 767231SDR DHL200072430CAngle · crackedAT C CHECK FOUND NR 7 LE I/B SLAT TRACK ROLLER SUPPORT WEBS I/B & O/B ATTACH ANGLES ARE CRACKED AT LOWER SPAR CHORD. REMOVED I/B & O/B VERTICAL ANGLES ON & NR 7 LE PER SRM 51-30-2. FABRICATED NEW ANGLES PER SRM 57-10-1 FIG 1. ALODINED AND PRIMED AREA & PARTSMar 3, 2000 · N724DH · Boeing 727228SDR UPS00831925Skin · crackedINSPECTION TYPE:C1, LEFT CENTER L/E UPPER SKIN IS CRACKED AT XFS 304. REPAIRED IAW SRM 57-2-1 FIG 38.Mar 3, 2000 · N748UP · Doug DC871FSDR UPS00831917Rib · crackedINSPECTION TYPE:C1, RIGHT WING L/E RIB IS CRACKED AT XFS 341.500. REPAIRED IAW SRM 57-2-0 FIG 2.Mar 3, 2000 · N748UP · Doug DC871FSDR UPS00831906Rib · crackedINSPECTION TYPE:C1, RIGHT WING L/E LOWER RIB IS CRACKED AT XFS. 653.750. REPAIRED IAW SRM 57-2-0 FIG 2.Mar 2, 2000 · N748UP · Doug DC871FSDR COMA0060229Skin · dentedTHE LEFT WING LEADING EDGE WAS DENTED AT STATION 183 AND PREVIOUSLY REPAIRED USING AERODYNAMIC FILLER. PERFORMED A PERMANENT REPAIR TO LEFT WING 183 IAW WVAC EO 601R-57-1033.Mar 2, 2000 · N926CA · Cndair CL6002B19SDR RRXA002275Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACKED LWR RIB ON THE LEFT WING O/B LEADING EDGE I/B SEGMENT AT STA 603.750, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC-8 Mar 1, 2000 · N995CF · Doug DC862SDR RRXA000566Skin · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO RIGHT WING LEADING EDGE AT STA XW 259.5, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED IAW DC-8 SRM 57-2-1 FIG 2H. (CORROSION DAMAGEFeb 28, 2000 · N831AL · Doug DC873FSDR RRXA000552Structure · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO LT WING LEADING EDGE STUB AT STA 520 TO XW 856, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED IAW DC-8 SRM 57-1-21 DAC DWG 5754701. (CORROSION DAFeb 26, 2000 · N831AL · Doug DC873FSDR UPS00831913Rib · crackedINSPECTION TYPE:C123, RIGHT WING L/E UPPER RIB CRACKED AT XILD .7095. REPAIRED IAW SRM 57-2-0 FIG 2.Feb 26, 2000 · N706UP · Doug DC871FSDR RRXA000553Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO RIGHT WING LEADING EDGE LOWER SKIN AT STA XW760 TO XW761 AT ATTACH FASTENER HOLES, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. REPAIRED SKIN IAW DC-8 SRM 5Feb 25, 2000 · N831AL · Doug DC873FSDR RRXA000953Structure · chafedDURING A MAINTENANCE VISIT, FOUND CHAFFING BY THE ATTACH HOLES ON THE RT WING NR 4 STUB WING LE BOTTOM IB, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED ANGLE PLATES FROM AISI 301 QUARFeb 25, 2000 · N994CF · Doug DC862SDR RRXA000679Skin · wornDURING A MAINTENANCE VISIT, FOUND A SCREW HOLE WORN AT THE RIGHT WING L/E LWR SKIN AT XFS 663, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. REPAIRED SKIN IAW DC-8 SRM 57-2-0 FIG 2A.Feb 25, 2000 · N831AL · Doug DC873FSDR TWAA0003703Skin · delaminatedDURING CHECK-C MAINT THE RT WING NUMBER 7 LE SLAT, DURING A TAP CHECK, A 6 INCH ROUND PATCH INDICATED DELAMINATION IN CENTER OF PATCH, TOP SURFACE OF SLAT OTBD END. REMOVED DOUBLER AND FILLED WITH HYSOL 934. INSTALLED 6 IN ROUND PATCH, AND ACCOMP HOT BOND PEFeb 25, 2000 · N603TW · Boeing 767231SDR TWAA0003702Skin · delaminatedDURING CK-C ,FOUND NUMBER 7 LEADING EDGE SLAT HAD A 2 INCH SQUARE PATCH INDICATING DELAMINATION IN THE CENTER OF THE PATCH. TOP SURFACE OF THE SLAT 7 IN OUTBOARD. REMOVED THE DOUBLER AND FILLED WITH HYSOL 934 AND INSTALLED 6 IN ROUND HOT BOND PATCH PER THE SFeb 25, 2000 · N603TW · Boeing 767231SDR RRXA000668Skin · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK TO THE LEFT O/B LEADING EDGE UPPER SKIN AT XFS 697, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED, REPAIRED AND INSTALLED DOUBLER IAW DC-8 SRM 57-2-1 FIG 38, 5Feb 24, 2000 · N831AL · Doug DC873FSDR RRXA000665Frame · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK TO THE RIGHT WING L/E RIB AT STA XFS 760.0, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK, FABRICATED AND INSTALLED DOUBLER IAW DC-8 SRM 53-2-00 FIG 1BFeb 24, 2000 · N831AL · Doug DC873FSDR UPS00831922Rib · crackedINSPECTION TYPE:C123, RIGHT WING L/E LOWER RIB IS CRACKED AT XFS 660. REPAIRED IAW SRM 57-2-0 FIG 2.Feb 24, 2000 · N706UP · Doug DC871FSDR UPS00831920Angle · crackedINSPECTION TYPE:C123, RIGHT WING L/E ANGLE IS CRACKED AT INBOARD RIB NR 4 PYLON AT XS 520. REMOVED, FABRICATED, AND REPLACED ANGLE IAW DWG 9753297, AND SRM 51-1-20D.Feb 24, 2000 · N706UP · Doug DC871FSDR UPS00831912Rib · crackedINSPECTION TYPE:C123, RIGHT WING L/E UPPER RIBS CRACKED ST XFS 322.75,XFS 448.51, XFS454.976,XFS484.895. REPAIRED IAW SRM 57-2-0 FIG 2.Feb 24, 2000 · N706UP · Doug DC871FSDR CALA0000190Skin · crackedINSPECTION FOUND THE LEFT NR 1 SLAT I/B SKIN CRACKED. THE SLAT WAS REPLACED IAW MM 27-80-01.Feb 23, 2000 · N41068 · Doug DC1030
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