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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR SWAA061608Skin · delaminatedDURING SCHEDULED SPV CHECK, FOUND RIGHT WING NR 5 SLAT T/E WEDGE DELAMINATED. REPAIRED NR 5 SLAT T/E WEDGE PER SRM.SDR USAA060680Skin · corrodedINBOARD LOWER EDGE (NR 5 SLAT) SLAT NR 5 SN-1501 AL CORROSION. REMOVED, BONDED, REPAIRED DAMAGE PER SRM 51-70-06, DEFECT SIZE: 0.75"L X 0.5"W X .082"D.SDR USAA060681Skin · chafedRIGHT WING LEADING EDGE OF I/B FLAP, 71 INCHES FROM I/B END CHAFED. REPAIRED PER SRM 57-53-01, 51-21-10, DEFECT SIZE: 5"L X 1"W X .004"D.SDR CALA0600158Bracket · crackedINSPECTION FOUND A .5 INCH CRACK IN RT WING NR 9 SLAT L/E CAVITY STOP PAD SUPPORT BRACKET AT OSS 607. THE STOP PAD SUPPORT BRACKET WAS REPAIRED IAW ECRA 5740-02109.SDR CALA0600157Rib · crackedINSPECTION FOUND A 2 INCH CRACK IN THE RIGHT WING NR 9 SLAT CAVITY SUPPORT RIB AT I/B FLANGE, OSS 607. THE SUPPORT RIB WAS REPAIRED IAW ECRA 5740-02109.SDR 06FDEA1745Repair · misinstalledFOUND PREVIOUSLY REPAIR INSTALLED ON NR 7 LEADING EDGE SLAT IS NOT COMPLIED WITH FAA APPROVED DATA. REMOVED EXISTING REPAIR AND REINSTALLED REPAIR DOUBLER IAW SRM 57-50-3, FIG 1. REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.SDR AWXA200600956Skin · delaminatedNR 5865365 - DURING C11 CHECK DISCOVERED RT WING, NR 9 SLAT WEDGE, OB UPPER SKIN IS DELAMINATED AT WING STATION 698R TO WING STATION 705R. MAINTENANCE REPAIRED DELAMINATED AREA ON THE RT WING, NR 9 SLAT WEDGE, OB UPPER SKIN IAW SRM 51-70-10-2R REPAIR 4 FIG 20SDR AWXA200600863Skin · crackedMCN - DURING C19 CHECK DISCOVERED 4 CRACKS, .25 INCHES, ON THE BOTTOM OF THE NR 2 SLAT SKIN AT SLAT STATION 226L TO 231L. MAINTENANCE CUT OUT DAMAGED AREA IAW BOEING 737-300 SRM 57-43-01-2R6. FABRICATED FILLER AND SPLICE PLATE IAW BOEING 737-300 SRM 57-43-01SDR IXXA06RNG046SSkin · corrodedDURING ROUTINE C CHECK FOUND CORROSION OUT OF LIMITS ON INBOARD EXTENDED LEADING EDGE UPPER SKIN, STATION XFS 13.750 - 20.000 RIGHT. PERMANENT REPAIR WAS PERFORMED IAW EWO ATI 57-084.SDR USAA060654Skin · crackedFOUND SLAT ASSEMBLY CRACKED, NR 1 LEADING EDGE SLAT, LOWER SURFACE. CUT OUT DAMAGE AND FABRICATED FILLER AND SPLICE PLATE IAW SRM 57-43-01, DEFECT SIZE: 1".SDR QXEA200601237Skin · gougedPDX - C3 THE AFT SIDES OF THE LEFT HAND OUT BOARD SLAT IS GOUGED ON THE INBOARD AND OUTBOARD SIDES OF THE INBOARD TRACK. REPAIRED IAW SRM 51-12-00 AND SRM 57-42-01.SDR 06FDEA1666Doubler · crackedLT WING FIXED LEADING EDGE STA XOS 698 TO STA XOS 703 BEADED DOUBLER FOUND CRACKED. REPAIR CARRIED OUT IAW FEDEX EA 1-5730-97748.SDR ASAA0640527Skin · chafedLT WING NR 3 SLAT IB LWR T/E IS CHAFED. REPAIRED SLAT IAW SRM 51 70 10 PARA 1 REPAIR 4 PG 201.SDR QXEA200601575Skin · corrodedYYC - C3 LEADING EDGE 511AL HAS CORROSION IN ATTACHMENT SCREW COUNTERSINK HOLES. REPAIRED IAW DHC-8-400 SRM 51-21-00-350-801 AND 51-25-10-370-801.SDR USAA060619Skin · wornFOUND LEFT WING OUTBD MID FLAP INBD END L/E BOTTOM AREA WORN. FABRICATED NEW REPAIR IAW SRM 57-53-01, DEFECT SIZE: 2.5" BY .2".SDR USAA060618Skin · wornFOUND INBOARD LOWER L/E OF O/B MIDFLAP WORN. REMOVED OLD DOUBLER AND FABRICATED NEW DOUBLER IAW SRM 57-53-01, DEFECT SIZE: .4".SDR MWEA060043Skin · crackedLEFT WING LEADING EDGE SKIN AT STATION XFS215 HAS A SIX INCH CRACK LOWER SIDE IN OPEN BAY. FABRICATED AND INSTALLED DOUBLER.SDR UPS06246883Rib · crackedINSPECTION TYPE:C LT 2 SLAT SUPPORT RIB CRACKED 2ND FROM LEADING EDGE O/B END, NUT PLATE DE-RIVETED IAW SRM 51-30-02. CRACK FOUND ON BOTH ENDS OF NUT PLATE AND RIB END CRACKED. REPAIR DOUBLER FABRICATED IAW SRM 51-40-3. NUT PLATE RIVETED IAW SRM 51-40-02. SDR UPS06246879Rib · crackedINSPECTION TYPE:C LT NR 2 SLAT SUPPORT RIB CRACKED 2ND FROM LEADING EDGE O/B END NUT PLATE DE-RIVETED IAW SRM 51-30-02. CRACKS FOUND ON NUT PLATE, END BROKEN ON RIB. FABRICATED REPAIR DOUBLER IAW SRM 51-40-03. NUT PLATE RIVETED PER SRM 51-30-02. RIB REPAIRSDR UPS06246874Angle · crackedINSPECTION TYPE:C LEFT NR 4, 2 RIBS CRACKED I/B AND O/B OF SLAT ACTUATOR FWD ATTACH POINT. DISCONNECTED ACTUATOR ROD END IAW MM 27-81-32 AND FOUND RIB ANGLES BROKEN. REMOVED FASTENERS IAW SRM 51-30-02. FABRICATED REPAIR DOUBLERS IAW SRM 51-40-03. REPAIR DOSDR 06FDEA1571Skin · dentedACCOMPLISHED EA 6-5750-92415A NR 3 SLAT DENT REPAIR OF LEADING EDGE SKIN RIBS 9 AND 8.SDR DL764060298Skin · damagedFOUND ON ARRIVAL LEFT WING LWR LEADING EDGE PANEL DAMAGED. FOUND 3.5 INCH TEAR TO OUTER SKIN OF PANEL 521TB ON LEFT WING, MADE TEMPORARY REPAIR PER ERA 455217-14. PERMANENT REPAIR WITHIN 100 FLIGHT HOURS.SDR USAA060608Wedge · damagedFOUND SLAT NR 2 LT INBOARD TRAILING EDGE WEDGE. REPAIRED AND REPLACED TRAILING EDGE WEDGE PER EA 96238 & SRM 57-40-00 FIG 200, DEFECT SIZE: 12" BY 3".SDR 06FDEA1551Structure · crackedFOUND CRACKED-DROOPED LEADING EDGE IN LT WING. SKIN REPLACED AS PER DRAWING ACA3822 AND SRM 51-35-01 VOL2 (MAJOR REPAIR).SDR ASAA0640464Skin · debondedFOUND LT WING SLAT O/B EDGE LWR SKIN DISBONDED. ACCOMPLISHED HOT BOND REPAIR PER SRM 51 70 10.SDR CA060413010Skin · corroded(CAN) EXFOLIATED CORROSION AT 2 ADJACENT LOCATIONS (TC NR 20060413010)SDR SWAA061259Skin · crackedDURING SCHEDULED C3 CHECK, FOUND RT WING NR 6 L/E SLAT LOWER T/E SKIN CRACKED AT AFT RIVET ROW. REPAIRED SLAT PER SRM.SDR SWAA061258Skin · crackedDURING SCHEDULED C3 CHECK, FOUND RT WING NR 4 L/E SLAT LOWER T/E SKIN CRACKED AT AFT RIVET ROW. REPAIRED SLAT PER SRM.SDR ASAA0640449Skin · damagedNR 1 SLAT DAMAGED IN 2 PLACES ON UPPER SIDE. REMOVED DAMAGED AREAS FABRICATED AND INSTALLED REPAIR PIECES IAW SRM 51 70 10.SDR 06FDEA1399Support · crackedCRACKED ANGLE SUPPORT AT RIGHT WING NR 2 L/E SLAT OUTBOARD. REMOVED AS PER SRM 51-31-01 VOL.II. NEW ANGLE FABRICATED AS PER DWG ARB 1647 AND INSTALLED AS PER SRM 51-35-01 AND 51-35-02 VOL.II. CLASSIFIED AS MAJOR REPAIR AS PER GMM 6-2-100.SDR DU4R2006367Skin · dentedS/O 304001, N/R 23584 - RT WING NR 5 SLAT TOPSIDE L/E DENTED. CUT OUT DENT THAT WAS OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR SKIN DOUBLER 5.5 INCH X 5.5 INCH FROM 2024-T3 .016 AND 2 EA. SKIN REPAIR DOUBLERS 4.1 INCH X 4.1 INCH AND 1.6 INCH X 1.6 INCH 2SDR ASAA0640413Structure · delaminatedNR 2 SLAT DELAMINATED AT OB TE. REMOVED DAMAGED AREA FABRICATED AND INSTALLED REPAIR PIECES PER SRM 51 70 10.SDR USAA060579Skin · crackedOUTBOARD END LWR SKIN NR 4 SLAT SKIN CRACKED. REMOVED DAMAGE, INSTALLED FILLER AND DOUBLER, DEFECT SIZE: .500 INCH.SDR USAA060582Wedge · debondedUPPER SURFACE T/E WEDGE OUTBOARD END DISBOND. PREVIOUSLY INSTALLED DOUBLER IAW SRM 51-70-10 AND TYP 57-42-02, DEFECT SIZE: 1.5 X 2 INCH.SDR USAA060583Structure · damagedINBOARD T/E UPPER SURFACE OF NR 5 SLAT COMPOSITE. REPAIRED PER T/R 57-42-02/04, DEFECT SIZE: 5 X 7 INCH.SDR DHL2006801527Angle · crackedRT WING CTR L/E ZEE PAN ANGLE 1.500" CRACK STA XW 454.000. REMOVED CRACKED ZEE PAN IAW SRM 51-1-20D, SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW ZEE PAN IAW SRM 51-1-20D, SRM 51-1-21, SRM 51-3-1. REFER TO JC EA57400003-001-SDR 06FDEA1325Skin · crackedLT WING FIXED L/E TELESCOPING DUCT CUTOUT FOUND CRACKED. CRACK AT LT WING FIXED L/E TELESCOPING DUCT CUTOUT REPAIRED AS PER FEDEX EA NR 1-5730-95669, TITLE: "WINGS - STRUCTURE. LEFT LEADING EDGE SKIN CRACKS AT ANTI-ICE TELESCOPING DUCT CUTOUT". REPAIR CLASSSDR DHL2006801525Skin · scratchedLT WING L/E INBD UPPER SURFACE 0.75" SCRATCH AT STA XCW 69.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 04-03-06, DWG NR AB07-53-120 REV IR DATED 03-21-06. REMOVED FASTENERS IAW SRM 51-1-21. BLENDED OUT DAMAGED AREA. FOUND OUT OF LIMITS IAW SRM 57SDR ABXA060195Skin · crackedRIGHT WING LEADING EDGE PANEL ASSEMBLY INNER (WAFFLED) SKIN HAD 3 EACH CRACKS AT XFS 410 - 423. REPAIRED CRACKS IAW REA D857-53581, REV IR.SDR DHL2006764512Attach Bracket · crackedLT WING INSIDE NR 4 SLAT LE ACTUATOR ATTACHED POINT IB AND OB RIB CRACKED. REMOVED RIBS AT LT WING NR 4 SLAT IB AND OB ACTUATOR ATTACHED POINT AND 1 CHANNEL IAW B727 SRM 51-30-5. TREATED AND PRIMED HOLES AND AREA IAW B727 SRM 51-10-2. INSTALED RIBS P/N 65-1SDR IXXA06RNG039SVane · corrodedDURING ROUTINE C CHECK, FOUND ELONGATED HOLES AND CORROSION ON EXTENDED LEADING EDGE OUTBOARD VANE BETWEEN STATIONS XILD 0.7095 XILD 40.00 RIGHT. CORRODED AREA WAS REMOVED, DAMAGED SECTION HOLES WERE CUT OUT AND PERMANENT REPAIR WAS PERFORMED IAW EWO ATI 57-0SDR IXXA06RNG019SVane · elongatedDURING ROUTINE C CHECK, FOUND ELONGATED HOLES ON EXTENDED LEADING EDGE OUTBOARD VANE, STATION XOLDI 6.224 RIGHT HAND. DAMAGED WAS REMOVED, REPAIR DOUBLER AND FILLERS WERE FABRICATED AND INSTALLED IAW EWO ATI 57-072. FAA FORM 8110-3 WAS ISSUED APPROVING THIS SDR IXXA06RNG005SSkin · crackedDURING ROUTINE C CHECK FOUND A CRACK ON CENTER EXTENDED LEADING EDGE AROUND LOWER SKIN STATION XOLDI 6.225 - RIGHT HAND. RIGHT HAND WING CENTER LEADING EDGE WAS REMOVED IAW DC8 AMM 57-20-02 PAGE 203, REPAIRED OUTER SKIN IAW EWO ATI 57-069 AND INSTALLED RT WINSDR UIEA200600068Skin · crackedNR 16 KRUEGER FLAT DEFECTS, P/N 65B39200-10, S/N 000296. STIFFENER CRACKS AT RTS EDGE. ALL "P" SEAL AND MOLDING SEAL WORN. MICA STRIPE CRACK. 1 LOCATION DELAMINATED AS MARKED. EXTERNAL PAINT WORK DETERIORATED. REPAIRED CARRIED OUT AS PER SWJC, MSG 63/02/SDR UIEA200600067Structure · crackedNR 15 KRUEGER FLAP DEFECTS, P/N 65B39250-2, S/N 000292, ALL "P" SEAL AND MOLDING SEAL WORN. OUTBD ARM PIVOT BEARING MIGRATED. STIFFENER CRACK AT EX-REPAIR AREA. BULL NOSE CRACK AT MID SECTION. REPAIR CARRIED OUT AS PER SWSC MSO 66/02/06, CS/020/03/06, TPAFSDR USAA060553Skin · debondedSLAT LOWER SIDE INBOARD EDGE DISBOND. REMOVED DAMAGE AND INSTALLED REPAIR PARTS IAW SRM 51-70-10, DEFECT SIZE: 2 X 3 INCH.SDR USAA060549Skin · debondedSLAT LOWER SIDE INBOARD EDGE DISBOND. REMOVED DAMAGE AND INSTALLED REPAIR PARTS IAW SRM 51-70-10, DEFECT SIZE: 2 X 3 INCHES.SDR USAA060542Wedge · delaminatedT/E WEDGE OUTBOARD END DELAMINATED. INSTALLED REPAIR IAW EA 97548, DEFECT SIZE: 11.0" X 6.5".SDR QXEA200601048Skin · corrodedYYC - C4 RIGHT INBOARD LEADING EDGE 611AR LOWER ATTACHMENT REBATE INBOARD HAS FRETTING CORROSION. REPAIRED IAW RD 8-57-811, DHC-8-200 SRM 51-40-11, PAGES 1-4 AND DHC-8 AMM 20-34-11.SDR USAA060529Skin · damagedOSS 607.25 - OSS 646.35 NR 9 SLAT DAMAGED. CUT OUT DAMAGED AREA & REPAIR IAW WITH SRM 52-70-10, DEFECT SIZE: .250"L X .250"W X .020"D.
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