JASC 5754

Service difficulty reports · 17,344

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 UPS06146452Rib · crackedLEFT WING KRUEGER FLAP BOX AREA CURVED DOUBLER HAS APPROX 2" CRACK. REMOVED AND REPLACED DOUBLER PER SRM 51-40-00.Mar 2, 2006 · N129UP · Airbus A300F4622RSDR SWAA060706Skin · delaminatedDURING SCHEDULED 1/2D CHECK, FOUND RT WING NR 5 L/E SLAT UPPER WEDGE DELAMINATED AT OUTBOARD END. REPAIRED SLAT PER SRM.Mar 2, 2006 · N514SW · Boeing 7375H4SDR 06FDEA0874Skin · crackedLEFT HAND WING, NR 3 SLAT TELESCOPIC ANTI-ICE LEADING EDGE SPRING DOOR CUTOUT AREA UPPER CORNER CRACKED. COMPLIED WITH FEDEX EA 1-5740-94607. REPAIR CLASSIFIED AS MINOR PER FEDEX GMM 6-2-100.Feb 28, 2006 · N585FE · Doug MD11SDR SWAA060663Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND RIGHT WING NR 5 L/E SLAT DELAMINATED. REPAIRED SLAT PER SRM.Feb 28, 2006 · N670SW · Boeing 7373G7SDR MWEA060020Doubler · chafedLT WING FLAP FIXED VANE CHAFED AT OB END LEADING EDGE. FABRICATED AND INSTALLED DOUBLER.Feb 27, 2006 · N803ME · Doug DC981SDR 06FDEA0850Doubler · crackedLEFT HAND WING STATION XOS 640 (ACCESS FROM PANEL 519CB) LEADING EDGE SKIN INTERIOR BEADED DOUBLER FOUND CRACKED AS MARKED. REPAIRED AS PER FEDEX EA 1-5730-90774. CLASSIFIED AS MINOR REPAIR PER GMM 6-2-100.Feb 27, 2006 · N602FE · Doug MD11SDR 06FDEA0849Doubler · crackedLEFT HAND WING STATION XOS 645 (AFT OF NR 4 SLAT) LEADING EDGE SKIN INTERIOR BEADED DOUBLER FOUND CRACKED AS MARKED. REPAIR CARRIED OUT AS PER FEDEX EA 1-5730-90774. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Feb 27, 2006 · N602FE · Doug MD11SDR 06FDEA0848Doubler · crackedLEFT HAND WING XOS 660 LEADING EDGE INTERIOR SKIN BEADED DOUBLER FOUND CRACKED AT TWO PLACES AS MARKED. REPAIR CARRIED OUT AS PER FEDEX EA 1-5730-90774.Feb 27, 2006 · N602FE · Doug MD11SDR 06FDEA0847Doubler · crackedRIGHT HAND WING LEADING EDGE AT XORS 572 BEADED DOUBLER FOUND CRACKED AS MARKED.Feb 26, 2006 · N602FE · Doug MD11SDR USAA060363Skin · crackedSLAT ST 3.25 CRACKED. MAJOR REPAIR IAW SRM 57-41-02. DEFECT SIZE: .5 INCH.Feb 24, 2006 · N778AU · Boeing 7374B7SDR QXEA200600629Skin · corrodedPDX - C4 CHECK, LOWER FLANGE ON LEFT INBOARD WING LEDING EDGE 511AL HAS FRETTING DAMAGE AT INBOARD 9" ON WING FACE. REPAIRED IAW SRM 51-20-16 AND RD 8-57-811.Feb 22, 2006 · N349PH · Dhav DHC8202SDR SWAA060615Skin · crackedDURING SCHEDULED C2 CHECK, FOUND LT WING NR 2 L/E SLAT INBOARD LOWER T/E SKIN CRACKED. REPAIRED SLAT PER SRM.Feb 22, 2006 · N336SW · Boeing 7373H4SDR 2006UALA00580Wedge · delaminatedTHE NR 2, 3 AND 13 LEADING EDGE SLATS HAVE LOCALIZED DELAMINATION ON THE LOWER SKIN OF THE TRAILING EDGE WEDGE. DELAMINATION REPAIRED TEMPORARILY WITH STRUCTURAL ADHESIVE INJECTION UNTIL PERMANENT REPAIR CAN BE ACCOMPLISHED AT THE NEXT HMV. AN NDT INSPECTIONFeb 21, 2006 · N791UA · Boeing 777222SDR 06FDEA0801Door · crackedRT WING, NR 3 SLAT TELESCOPIC ANTI-ICE LEADING EDGE SPRING DOOR CUTOUT AREA UPPER CORNER WITH APPROXIMATELY ONE (1) INCH CRACKED. COMPLIED WITH FEDEX EA 1-5740-94606.Feb 21, 2006 · N585FE · Doug MD11SDR USAA060318Skin · crackedFOUND CRACK OB END, LOWER SKIN NR 4 SLAT. REMOVED DAMAGE, INSTALLED FILLER AND DOUBLER IAW SRM 57-43-02, DEFECT SIZE: .5000".Feb 21, 2006 · N778AU · Boeing 7374B7SDR USAA060317Structure · debondedFOUND DISBOND INBOARD END. REMOVED DAMAGE, INSTALLED NEW CORE, DEFECT SIZE: 6.5" BY 9.0".Feb 21, 2006 · N778AU · Boeing 7374B7SDR 06FDEA0780Rib · chafedNR 2 SLAT I/B END RIB HAS CHAFING DAMAGE. *S/D* REPAIRED I/B RIB IAW SRM 51-30-2.Feb 20, 2006 · N488FE · Boeing 727200SDR DHL2006760520Skin · crackedFOUND NR 4 SLAT INBD HOOK CUTOUT IS CRACKED AT TOP OUTBD CORNER WING STA 390, NDT CONFIRMED). CUT OUT EXISTING FILLER STRIP TO ALLOW REPAIR FAB PLATE FROM P/N 301 1/2 HARD .025 PO #9002473 DIM 7" BY 5 1/4" FILLER FROM P/N 301 1/2 HARD .032 PO NR 9002473 DIM 7Feb 18, 2006 · N760AT · Boeing 7272B7SDR DHL2006760519Skin · crackedFOUND NR 3 SLAT OUTBD HOOK CUT OUT IS CRACKED AT TOP OUTBD CORNER WING STA 525. (NOT CONFIRMED). STOP DRILLED CRACK IAW B727 SRM 57-30-4 ACCOMPLISHED HFEC AROUND STOP HOLE NO CRACKS NOTED IAW NDT MAN PART 6 51-00-00 FIG 23. FABBED DOUBLER FROM .020 CRES 301 Feb 18, 2006 · N760AT · Boeing 7272B7SDR SWAA060562Skin · delaminatedLT WING NR 3 L/E SLAT UPPER SKIN, OUTBD AFT EDGE DELAMINATED. REMOVED AND REPLACED SLAT PER MM.Feb 16, 2006 · N343SW · Boeing 7373H4SDR SWAA060555Skin · delaminatedLT WING NR 3 L/E SLAT UPPER SKIN, OUTBOARD AFT EDGE DELAMINATED. REMOVED AND REPLACED SLAT PER MM.Feb 16, 2006 · N343SW · Boeing 7373H4SDR USAA060273Skin · crackedLOWER SURFACE OF NR 6 SLAT, INBOARD END AT STOP PADS. REMOVED AFFECTED RIVETS, CUT OUT DAMAGE FABRICATED REPAIR PANEL AND INSTALLED IAW SRM 57-43-01 R-6. DEFECT SIZE: .250 INCHFeb 16, 2006 · N527AU · Boeing 7373B7SDR USAA060252Skin · crackedCRACKS FROM RIVET HOLES AT 4 LOCATIONS ON LOWER TRAILING EDGE OF NR 4 SLAT. SRM 57-43-01-2R6, DEFECT SIZE: .25.Feb 15, 2006 · N257AU · Boeing 737201SDR UPS06M46717Angle · crackedRT NR 2 SLAT O/B END RIB ATTACH ANGLE FOUND CRACKED AS MARKED. RHW NR 2 SLAT REMOVED. INNER SKIN OPENED FOR ACCESS. CRACKED ANGLE REMOVED NEW ATTACHMENT ANGLE FAB USING MAT'L 7075-0-0.050" PER DWG ARB1647. ANGLE HEAT TREATED. HOLES PICK-UP ON NEW ANGLE. Feb 14, 2006 · N283UP · Doug MD11FSDR 06FDEA0676Skin · crackedLEFT HAND WING FIXED LEADING EDGE TELESCOPIC DUCT CUTOUT FOUND CRACKED. LEFT HAND WING FIXED LEADING EDGE TELESCOPIC DUCT CUTOUT CRACKED AREA REPAIRED AS PER FEDEX EA 1-5730-90744, REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.Feb 14, 2006 · N615FE · Doug MD11SDR VNAA0602007Flap · bird strikeDURING THE SERVICE CHECK, MAINTENANCE FOUND EVIDENCE OF BIRD STRIKE DAMAGE TO THE LEFT INBOARD FLAP. MAINTENANCE COMPLIED WITH A TEMPORARY REPAIR IAW BOMBARDIER REO 601R-57-52-517. THE AIRCRAFT WAS RELEASED FOR SERVICE.Feb 13, 2006 · N202PS · Cndair CL6002B19SDR SWAA060537Skin · crackedDURING SCHEDULED 1/2D CHECK, FOUND LEFT WING NR 2 L/E SLAT LOWER T/E SKIN CRACKED AT OUTBOARD END. REPAIRED SLAT PER SRM.Feb 12, 2006 · N672SW · Boeing 7373Q8SDR UPS06M46716Angle · crackedINSPECTION TYPE:C LT WING NR 2 SLAT O/B RIB ATTACHMENT ANGLE FOUND CRACKED 1 INCH LONG AS MARKED. LHW NR 2 SLAT REMOVED. INNER SKIN OPENED. CRACKED ANGLE NR 2 SLAT REMOVED. NEW ATTACHMENT ANGLE FAB, MAT'L 7075-0-0.050" AS PER DWG ARB1647 ANGLE HEAT TREATEDFeb 11, 2006 · N283UP · Doug MD11FSDR 06FDEA0616Doubler · crackedRIGHT HAND FIXED LEADING EDGE INTERNAL BEADED DOUBLER FOUND CRACKED AT XORS 663. REPAIR CARRIED OUT AT RIGHT HAND FIXED LEADING EDGE BEADED DOUBLER AT XORS 663 CRACKED AREA AS PER FEDEX EA 1-5730-90749.Feb 9, 2006 · N615FE · Doug MD11SDR 06FDEA0615Doubler · crackedRIGHT HAND FIXED LEADING EDGE INTERNAL BEADED DOUBLER FOUND CRACKED AT XORS 658. REPAIR CARRIED OUT AT RIGHT HAND FIXED LEADING EDGE INTERNAL BEADED DOUBLER AT XORS 658 CRACKED AREA AS PER FEDEX EA -5730-90749.Feb 9, 2006 · N615FE · Doug MD11SDR 06FDEA0614Doubler · crackedFOUND RIGHT FIXED LEADING EDGE INTERNAL BEADED DOUBLER FOUND CRACKED AT XORS 590. REPAIR CARRIED OUT AT RIGHT HAND FIXED LEADING EDGE INTERNAL BEADED DOUBLER AT XORS 590 CRACKED AREA AS PER FEDEX EA 1-5730-90751.Feb 9, 2006 · N615FE · Doug MD11SDR 06FDEA0613Doubler · crackedRIGHT FIXED LEADING EDGE INTERNAL BEADED DOUBLER FOUND CRACKED AT XORS 563. REPAIR CARRIED OUT AT RIGHT HAND FIXED LEADING EDGE INTERNAL BEADED DOUBLER AT XORS 563 CRACKED AREA AS PER FEDEX EA 1-5730-90751.Feb 9, 2006 · N615FE · Doug MD11SDR 06FDEA0612Doubler · crackedRT FIXED LEADING EDGE INTERNAL BEADED DOUBLER FOUND CRACKED AT XORS 538. REPAIR CARRIED OUT AT RIGHT HAND FIXED LEADING EDGE BEADED DOUBLER AT XORS 538 CRACKED AREA AS PER FEDEX EA 1-5730-90750.Feb 9, 2006 · N615FE · Doug MD11SDR 06FDEA0611Doubler · crackedLEFT HAND FIXED LEADING EDGE INTERNAL BEADED DOUBLER FOUND CRACKED AT XORS 522. CRACKED AREA REPAIRED AS PER FEDEX EA 1-5730-90748, REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.Feb 9, 2006 · N615FE · Doug MD11SDR 06FDEA0610Doubler · crackedLEFT HAND FIXED LEADING EDGE INTERNAL BEADED DOUBLER FOUND CRACKED AT XORS 600. REPAIR CARRIED OUT AT LEFT HAND FIXED LEADING EDGE INTERNAL BEADED DOUBLER AT XORS 600 CRACKED AREA AS PER FEDEX EA 1-5730-90747.Feb 9, 2006 · N615FE · Doug MD11SDR AALA20060131Skin · crackedAFW - NR 2 SLAT NOSE SKIN CRACKED AND GOUGED IN LOWER SLAT SKIN. AREA IS 2 INCHES BY 1.5 INCHES AND 3/64 INCH DEEP. REPAIRED NUMBER TWO SLAT IN SHOP ON E58 NUMBER 6177178 AND REPAIRED DAMAGED AREA PER MRB 777175. SYSTEM GROUND CHECKED NORMAL OPERATION.Feb 8, 2006 · N789AN · Boeing 777223SDR DHL2006753524Skin · dentedFOUND NR 019920; NR 8 SLAT OUTER SKIN SHOW DENT WS 700 APPROX. CUT OUT DAMAGED AREA IAW B727 SRM 57-050-3 FIG 1. FABBED FILLER 1 040 2024 T3 PO #9003055 SPLICES 4.1X2.1 2 EACH 2024 T3 .080 PO #9002727 4.1 X 2.8 2EA 040 2024 T3 PO #9003055 1.7X2.8 1EA .040 20Feb 8, 2006 · N753DH · Boeing 727223SDR TSAA0653010Skin · crackedFOUND 3 CRACKS AROUND CENTER UPSTOP OF NR 2 SLAT; WING LEADING EDGE. BETWEEN LEFT WS 453 AND WS 479. L/E SKIN FABRICATED, TRIMMED, CLEANED, ALODINED, PRIMED, AND SEALED IAW SRM 57-30-04. REPAIR SIZE APPROX 14" BY 25".Feb 8, 2006 · N808AL · Boeing 7372T4SDR SWAA060498Wedge · delaminatedDURING SCHEDULED C2 CHECK, FOUND LT WING NR 2 L/E SLAT T/E WEDGE DELAMINATED. REMOVED AND REPLACED SLAT PER MM.Feb 8, 2006 · N600WN · Boeing 7373H4SDR SWAA060493Wedge · delaminatedDURING SCHEDULED C4 CHECK, FOUND LT WING NR 2 L/E SLAT OUTBOARD T/E WEDGE DELAMINATED. REMOVED AND REPLACED SLAT PER MM.Feb 8, 2006 · N356SW · Boeing 7373H4SDR SWAA060492Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND RIGHT WING NR 5 L/E SLAT OUTBOARD UPPER T/E SKIN DELAMINATED. REPAIRED SLAT PER SRM.Feb 8, 2006 · N356SW · Boeing 7373H4SDR DHL2006754517Support Fitting · crackedFOUND NR 4 SLAT ACTUATOR ROD END SUPPORT PLATE CRACKED, O/B. REMOVED BRACKET, FABBED AND INSTALLED NEW, MAT USED 7075-T6 .071, PO 596275 DIM 12" X 4" IAW B727 SRM 57-50-2 FIG 2 AND 51-30-2.Feb 7, 2006 · N753DH · Boeing 727223SDR QXEA200600500Panel · chafedYYC - C3 RIGHT INBOARD WING LEADING EDGE PANEL 622AR HAS CHAFED MARKS FROM SLAT AT NS50.88, 108. REPAIRED IAW CRJ700/900 SRM 57-41-01-101-001-A01.Feb 7, 2006 · N607QX · Cndair CL6002C10SDR 06FDEA0574Repair · unknownFOUND PREVIOUS REPAIR INSTALLED ON NR 8 LEADING EDGE SLAT UPPER SURFACE WAS DETERMINED TO BE ACCOMPLISHED IAW SRM 57-50-3 FIG 10. BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL THICKNESS AND TYPE, FASTENER SPACING AND NUMBFeb 7, 2006 · N487FE · Boeing 727200SDR MALA060050Skin · ground damageRIGHT WING OUTBOARD LEADING EDGE PART NUMBER 601R12310-2S SUSTAINED DAMAGE BY CONTACT WITH A GROUND SUPPORT VEHICLE. THE DAMAGE STARTS AT THE OUTBOARD END OF THE OUTBOARD SECTION OF WING LEADING EDGE. THE DAMAGE THEN EXTENDS INBOARD OVER 7 INCHES OF THE LEADFeb 5, 2006 · N602XJ · Cndair CL6002B19SDR ASAA0640128Skin · delaminatedNUMBER 2 SLAT DELAMINATED I/B SIDE 3 INCHES FROM EDGE. REMOVED DAMAGE, FABRICATED AND INSTALLED FILLER AND DOUBLER PER SRM 51-70-10 REPAIR 4.Feb 5, 2006 · N769AS · Boeing 7374Q8SDR ASAA0640121Skin · delaminatedNR 2 SLAT DELAMINATED AT O/B CORNER. REMOVED DAMAGE, FABRICATED FILLER AND DOUBLER AND INSTALLED REPAIR PIECES IAW SRM 51-70-10.Feb 5, 2006 · N769AS · Boeing 7374Q8SDR ASAA0640120Wedge · delaminatedNR 1 SLAT T/E WEDGE HAS 2 EACH AREAS OF DELAMINATION. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PIECES IAW SRM 51-70-10 REPAIR 4.Feb 5, 2006 · N769AS · Boeing 7374Q8SDR ABXA060097Skin · corrodedCORROSION AROUND FASTENERS ON RIGHT WING, LEADING EDGE, UPPER SURFACE AT XFS 356.00. CORROSION OUT OF LIMITS. FABRICATED REPAIR DOUBLERS AND FILLERS IAW DC8 SRM 57-2-1. INSTALLED REPAIR IAW ABX SSRM K08002.Feb 2, 2006 · N842AX · Doug DC861SDR AWXA200600244Hinge · crackedCREW REPORTED THAT THE LT LEADING EDGE FLAP AT THE ENGINE PYLON WAS CRACKED AND OFF THE HINGE. MAINTENANCE REMOVED BOTH KRUEGER FLAP DOORS AND PLACED ON CDL. PARTS HAVE BEEN ORDERED. DOOR ASSEMBLY AND DRIVE LEVER ASSEMBLY WERE REPLACED.Feb 2, 2006 · N175AW · Boeing 73733A
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