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 SWAA000893Skin · crackedDURING SCHEDULED BC1 CHECK, FOUND BOTH LT AND RT WING O/B KRUEGER FLAPS HAVE .25 INCH CRACKS ON INNER SKIN ACROSS T/E OF VERTICAL STIFFENER RIB. REMOVED AND REPLACED BOTH KRUEGER FLAPS PER MM.May 12, 2000 · N701GS · Boeing 7377H4SDR DL72S000939Bracket · crackedFOUND ON F2 LETTER CK, INBOARD ATTACH BRACKET CRACKED NR 8 SLAT ACTUATOR. REPAIR PER MM 57-20-21.May 11, 2000 · N420DA · Boeing 727232SDR 0001929880Skin · crackedFLAP LEADING EDGE JUST AFT OF NR 2 FLAP HINGE IS CRACKED. REPAIRED PER EA 98-172453. L/P 1437664May 10, 2000 · N675MC · Doug DC951SDR TWAA0007703Skin · dentedDURING OP 16 MAINT CHECK ON LT WING, FOUND DENTS IN LEADING EDGE OF NUMBER 3 LEADING EDGE SLAT, DENT LOCATED 13 INCHES I/B FROM O/B END OF SLAT WAS 1 INCH WIDE BY 1 INCH LONG AND 0.050 INCH DEEP, DENT LOCATED 18 INCHES I/B FROM O/B END OF SLAT WAS .75 INCH LONMay 9, 2000 · N921L · Doug DC932SDR RRXA001755Skin · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK ON THE UPPER SIDE OF THE RT WING LE SKIN 2 INCHES FWD OF THE WING SPAR AT XFS 615, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8.May 8, 2000 · N2674U · Doug DC873FSDR RRXA001754Skin · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK ON THE UPPER SIDE 2 INCHES FWD OF THE WING SPAR ON THE RT WING LE SKIN AT XFS 603.75, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8.May 8, 2000 · N2674U · Doug DC873FSDR RRXA001753Skin · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK 2 INCHES FWD OF THE WING SPAR ON THE RT WING LE SKIN ON UPPER SIDE AT XFS 615, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8.May 8, 2000 · N2674U · Doug DC873FSDR RRXA001752Skin · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK TO THE SKIN ON UPPER SIDE 2 INCHES FWD OF THE WING SPAR AT THE RT WING LEADING EDGE AT XFS 603.75, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8.May 8, 2000 · N2674U · Doug DC873FSDR UPS00832655Angle · crackedINSPECTION TYPE:C123, LEFT WING L/E RIB ANGLE IS CRACKED AT XS 467.323. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 5770170 AND SRM 51-1-20D.May 8, 2000 · N802UP · Doug DC873FSDR UPS00832654Doubler · crackedINSPECTION TYPE:C123, LEFT WING L/E INTERNAL DOUBLER IS CRACKED AT XFS 572.5. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5769600 AND SRM 51-1-20D, 51-1-21, 51-1-21A.May 8, 2000 · N802UP · Doug DC873FSDR UPS00832653Angle · crackedINSPECTION TYPE:C123, LEFT WING L/E VERTICAL ANGLE IS CRACKED AT XS 256. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 9753294 AND SRM 51-1-20D.May 8, 2000 · N802UP · Doug DC873FSDR DL72K000919Stiffener · crackedFOUND ON B1 LETTER CK, L/E SPAR STIFFENERS CRACKED L/E SPAR I/B AND O/B OF NR 7 SLAT ACTUATOR. REPAIRED PER MM 57-20-21.May 8, 2000 · N526DA · Boeing 727232SDR MALA000315Rib · crackedRIB 3 & 4 CRACKED ON ENDS LEADING EDGE PNL 511 BL. REMOVED DAMAGE, FABRICATED REPAIR DOUBLERS IAW SRM 57-10-30. LOCATED AND DRILLED ROW HOLES IAW 57-10-30. NDT PER FFUNDT006, NO CRACKS NOTED. INSTALLED DOUBLERS ON LEADING EDGE IAW SRM 57-10-30.May 7, 2000 · N407XJ · Saab 340BSDR RRXA002240Skin · crackedDURING A MAINTENANCE VISIT FOUND CRACKS AT RIVETS ON THE LT WING O/B SLOT LEADING EDGE VANE AT STA XS 472 AND XS 478, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED RIVETS IAW DC-May 6, 2000 · N995CF · Doug DC862SDR RRXA002238Skin · damagedDURING A MAINTENANCE VISIT FOUND SCREWS PULLING THROUGH SKIN ON THE LT WING O/B SLOT L/E VANE AT STA XFS 428 34 TO 48 INCHES FWD OF SPAR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INMay 6, 2000 · N995CF · Doug DC862SDR AALA20005710Structure · wornTUL - FOUND RIGHT KRUEGER FLAP BLOCKER DOOR WORN 2 INCHES BY .080 DEEP IN FLANGE. REPAIRED FLAP BLOCKER DOOR PER ESO 30595 DATED 5/5/2000. (M)May 6, 2000 · N18066 · Airbus A300B4605RSDR CALA0000635Access Panel · crackedINSPECTION FOUND A 1 INCH CRACK IN NR 1 RIGHT SLAT LOWER CUTOUT DOOR. THE CUTOUT DOOR WAS REMOVED AND REPLACED.May 6, 2000 · N71828 · Doug DC982SDR UPS00832636Skin · crackedINSPECTION TYPE:C123, RIGHT WING L/E SKIN IS CRACKED AT XFS 710. REPAIRED IAW SRM 57-2-1 FIG 2H.May 5, 2000 · N802UP · Doug DC873FSDR DL72L000884Skin · wornUPPER SURFACE IS WORN ON NR 5 SLAT. BURNISHED WEAR AREA, MADE STAINLESS DOUBLER. INSTALLED DOUBLER PER MM 727 57-54-0 FIG 81.May 4, 2000 · N509DA · Boeing 727232SDR CALA0000612Skin · gougedLEFT NUMBER 5 FLAP LEADING EDGE IS GOUGED. REMOVED AND REPLACED RUB STRIP PER EC/RA 5750-01579 AND SRM 51-30-2.May 3, 2000 · N72830 · Doug DC982SDR UPS00232786Rib · crackedINSPECTION TYPE:C, CRACK FOUND AT NR 3 RIB AT INNER SKIN CONNECTING NR 7 SLAT. REPAIR CARRIED OUT IAW SRM 57-50-3, FIGURE 9.May 1, 2000 · N944UP · Boeing 72722CSDR QXEA0001187Skin · chafedYYC- SPAN WISE CHAFE DAMAGE ON UPPER SURFACE OF LEFT HAND INBOARD FLAP LEADING EDGE. REPAIRED IAW HORIZON AIR EA 9-57-501, DHC-8 SRM 51-2036 AND SRM 51-20-51.May 1, 2000 · N829PH · Dhav DHC8102SDR DL72K000868Stiffener · crackedA 2 INCH CRACK IN NR 3 SLAT O/B TRACK O/B SPAR STIFFENER. REPLACED STIFFENER PER M/M 57-20-21.May 1, 2000 · N524DA · Boeing 727232SDR RAAA00B1003Rib · crackedDURING SCHEDULED C2 CHECK, FOUND NR 3 SLAT ACTUATOR BUSHING/BOLT WORN. UPON FURTHER INVESTIGATIION FOUND RIB CRACKED. REPLACED BOLT AND BUSHING WITH NEW RIB IAW M/M 27-81-11 & 27-81-32, SRM 51-20-4, 51-10-1 & 51-30-2.Apr 30, 2000 · N831RV · Boeing 72722CSDR RRXA002239Skin · damagedDURING A MAINTENANCE VISIT FOUND ATTACH SCREWS PULLING THROUGH SKIN AT LT WING O/B SLOT L/E VANE AT STA XFS 508.000 34 INCHES TO 48 INCHES FWD OF SPAR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABApr 27, 2000 · N995CF · Doug DC862SDR GAIA00258Rib · crackedDURING HEAVY C-CHECK AT TIMCO/OSC THE FOLLOWING DISCREPANCY WAS FOUND, NR 5 SLAT 3RD RIB FROM INBOARD END RIB CRACKED. REPAIRED RIB PER IAW SRM 57-50-3. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Apr 27, 2000 · N6831 · Boeing 727223SDR DL72S000806Stiffener · crackedA 1 INCH CRACK IN SPAR STIFFENER I/B SIDE OF NR 6 SLAT I/B TRACK. REPLACED STIFFENER PER M/M 57-20-21. TPA D-1 LETTER CHECK.Apr 25, 2000 · N401DA · Boeing 727232SDR DL72K000980Skin · damagedDURING SHOP VISIT, THE LEADING EDGE SKIN WAS FOUND WORN AT THE I/B END OF THE MIDFLAP. THE SKIN WAS REPAIRED BY REMOVING THE DAMAGE AND INSTALLING A DOUBLER AND FLUSH FILLER PER MM 57-52-0, FIG 803.Apr 24, 2000 · N529DA · Boeing 727232SDR DL72K000979Skin · damagedDURING SHOP VISIT, THE LEADING EDGE SKIN WAS FOUND WORN AT THE I/B END. THE SKIN WAS REPAIRED BY REMOVING THE DAMAGE AND INSTALLING A DOUBLER AND FLUSH FILLER PER MM 57-52-0, FIG 803.Apr 24, 2000 · N529DA · Boeing 727232SDR 00FDEA00284Cap · crackedNR 5 LEADING EDGE SLAT I/B END CRACKED. REMOVED AND REPLACED I/B END CAP ON NR 5 SLAT IAW SRM 51-30-2.Apr 24, 2000 · N222FE · Boeing 727233SDR TWAA0006434Skin · debondedDURING CHECK-C MAINT, THE LT WING NUMBER 6 LEADING EDGE SLAT TOP SIDE AT MID SPAN HAD THE HOT BOND LIFTED AND HAD BEEN SEALED WITH SPEED TAPE PER SRM 57-43-02. APPLIED HOT BOND REPAIR ON NUMBER 6 SLAT APPROX 3 .75 BY 4.75 INCH DOUBLER PER SRM 57-43-20 AND 51-Apr 24, 2000 · N602TW · Boeing 767231SDR RRXA002500Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE LEADING EDGE LT WING AT XFS 566, 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 AND EO NR 00Apr 21, 2000 · N995CF · Doug DC862SDR DL757000771Skin · puncturedAFTER ACCOMPLISHMENT OF S/B 757-57A0043, THE I/B LEADING EDGE SLAT, TRAILING EDGE WEDGE, UPPER SKIN WAS DAMAGED. DAMAGE LOCATED 1 AFT OF THE FWD EDGE OF THE TRAILING EDGE WEDGE UPPER SKIN AND 46 I/B FROM THE O/B EDGE. REPAIR PER ER/A 387545-14.Apr 21, 2000 · N675DL · Boeing 757232SDR DL757000770Skin · puncturedAFTER ACCOMPLISHMENT OF BCAG S/B 757-57A0043, THE I/B LEADING EDGE SLAT, TRAILING EDGE WEDGE UPPER SKIN WAS DAMAGED. DAMAGE WAS LOCATED 2 INCHES FWD OF THE AFT EDGE OF THE TRAILING EDGE WEDGE UPPER SKIN AND 61 O/B FROM I/B EDGE. REPAIR PER ER/A 387546-14.Apr 21, 2000 · N649DL · Boeing 757232SDR UPS00832606Skin · crackedINSPECTION TYPE:C2, LEFT WING L/E LOWER SKIN IS CRACKED AT FASTENER HOLES BETWEEN XFS 640 - 649. REPAIRED IAW EO DC8-5720-4087-B.Apr 20, 2000 · N700UP · Doug DC871FSDR UPS00832565Rib · crackedINSPECTION TYPE:C-2, RIGHT WING L/E UPPER RIB CRACKED STA XS 250.089. STOP DRILLED CRACKED IAW SRM 57-2-0 FIG 2. FAB AND INSTALLED ANGLE DOUBLERS IAW SRM 51-1-20D & 51-3-0.Apr 20, 2000 · N700UP · Doug DC871FSDR UPS00832557Skin · crackedINSPECTION TYPE:C-2, LEFT WING CENTER L/E LWR SKIN CRACKED STA XW 257. STOP DRILLED CRACK IAW ADDUM DC8-5720-4087-B. FAB AND INSTALLED DOUBLER IAW DC8-5720-4087-B.Apr 20, 2000 · N700UP · Doug DC871FSDR UPS00832546Doubler · corrodedINSPECTION TYPE:C2, RIGHT WING L/E BETWEEN STA 772.500 TO XFS 760.00. THE INTERNAL DOUBLER HAS HEAVY CORROSION. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 3641257.Apr 20, 2000 · N700UP · Doug DC871FSDR UPS00832545Skin · crackedINSPECTION TYPE:C2, RIGHT WING L/E (NR 3 STUB WING) AT STA XS207.500. THE L/E SKIN IS CRACKED AT FRONT SPAR. REPAIRED AREA IAW DC8-5720-7767-A.Apr 20, 2000 · N700UP · Doug DC871FSDR UPS00832536Rib · crackedINSPECTION TYPE:C2, RIGHT WING L/E EXTERIOR SKIN IS CRACKED AT STA XFS288.00 ON THE L/E. REPAIRED AREA IAW SRM 57-2-1 FIG 2H.Apr 20, 2000 · N700UP · Doug DC871FSDR UPS00832534Rib · crackedINSPECTION TYPE:C2, RIGHT WING L/E AT STA XFS.792.250. THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.Apr 20, 2000 · N700UP · Doug DC871FSDR UPS00832532Rib · crackedINSPECTION TYPE:C2, LEFT WING L/E UPPER RIB IS CRACKED AT STA XS.00. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.Apr 20, 2000 · N700UP · Doug DC871FSDR UPS00832531Skin · corrodedINSPECTION TYPE:C2, RIGHT WING L/E SKIN HAS INTERNAL CORROSION AT STA XFS710.00. REPAIRED AREA IAW 8110-3 APPROVED DH SK 700-025.Apr 20, 2000 · N700UP · Doug DC871FSDR UPS00832421Rib · crackedINSPECTION TYPE:C2, LEFT WING L/E UPPER RIB IS CRACKED AT XFS 646. REPAIRED IAW SRM 57-2-0 FIG 2.Apr 20, 2000 · N700UP · Doug DC871FSDR UPS00832420Rib · crackedINSPECTION TYPE:C2, RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 283.25. REPAIRED IAW SRM 57-2-0 FIG 2.Apr 20, 2000 · N700UP · Doug DC871FSDR UPS00832417Rib · crackedINSPECTION TYPE:C2, LEFT WING L/E UPPER RIB IS CRACKED AT XFS 660. REPAIRED IAW SRM 57-2-0 FIG 2.Apr 20, 2000 · N700UP · Doug DC871FSDR RIVA0000011Rib · crackedNR 5 SLAT LEADING EDGE RIBS (2 EACH) CRACKED AT SLAT STATION 61 AND 63. REPAIRED IAW BOEING SRM 57-50-3, FIGURE 9. FABRICATED AND INSTALLED DOUBLERS (2 EACH) FROM .032 CRES A1S1,321 ANNEALED CONDITION. DOUBLER AT SLAT STATION 63 INSTALLED WITH SHIM AND RADIApr 19, 2000 · N362PA · Boeing 7272J0SDR RRXA002276Skin · damagedDURING A MAINTENANCE VISIT FOUND SCREWS PULLING THROUGH THE SKIN I/B SLOT LEADING EDGE VANE AT STA XS 250.000, 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 SRApr 19, 2000 · N995CF · Doug DC862SDR UPS00832535Rib · crackedINSPECTION TYPE:C2, LT WING CENTER L/E UPPER RIB IS CRACKED AT STA XFS 410.250. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.Apr 19, 2000 · N700UP · Doug DC871FSDR UPS00832419Rib · crackedINSPECTION TYPE:C2, LEFT WING L/E UPPER RIB IS CRACKED AT XFS 610. REPAIRED IAW SRM 57-2-0 FIG 2.Apr 19, 2000 · N700UP · Doug DC871F
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