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 DHL2000801105Rib · crackedAT C CK; LT WING LEADING EDGE RIB CRACKED 1/2 INCH. STA. XFS. 725.000. PERFORMED STOP DRILL IAW SRM 57-2-0, PAGE 12, CLEANED,TREATED AND PRIMED AREA IAW SRM 51-1-8B, PAGE 1-2, FABRICATED AND INSTALLED DOUBLER IAW SRM 57-2-0, PAGE 12. REF: N/R 0443.SDR DHL2000801104Rib · crackedAT C CK; LT WING LEADING EDGE RIB CRACKED 1/4 INCH, STA. XFS. 730.000. PERFORMED STOP DRILL IAW SRM 57-2-0 PAGE 12, CLEANED,TREATED AND PRIMED AREA IAW SRM 51-1-8B,PAGE 1-2, FABRICATED AND INSTALLED DOUBLER IAW SRM 57-2-0, PAGE 12. REF: N/R 0442.SDR DHL200080137CRib · crackedAT C CK; LT WING LEADING EDGE (2EA) RIBS CRACKED 1/4 INCH STA. XFS. 750.000. PERFORMED STOP DRILL IAW SRM 57-2-0 PAGE 12, FABRICATED AND INSTALLED DOUBLER IAW SRM 57-2-0 PAGE 12. REF: N/R 0440.SDR DHL200080136CRib · crackedAT C CK; LT WING LEADING EDGE RIB CRACKED 1/2 INCH STA. XFS. 755.000. PERFORMED STOP DRILL IAW SRM 57-2-0 PAGE 12, FABRICATED AND INSTALLED DOUBLER IAW SRM 57-2-0, PAGE 12. REF: N/R 0439.SDR DHL200080135CRib · crackedAT C CK; LT WING LEADING EDGE RIB CRACKED 3/4 INCH STA. XFS. 780.000. PERFORMED STOP DRILL IAW SRM 57-2-0 PAGE 12, FABRICATED AND INSTALLED DOUBLER IAW SRM 57-2-0., PAGE 12. REF: N/R 0438.SDR DHL200080134CRib · crackedAT C CK; LT WING LEADING EDGE RIB CRACKED 1/2 INCH STA. XFS. 785.000. PERFORMED STOP DRILL IAW SRM 57-2-0 PAGE 12, FABRICATED AND INSTALLED DOUBLER IAW SRM 57-2-0 PAGE 12. REF: N/R 0437.SDR DHL200080133CRib · crackedAT C CK; LT WING LEADING EDGE RIB CRACKED 1/4 INCH STA. XFS. 730.000. PERFORMED STOP DRILL IAW SRM 57-2-0 PAGE 12, FABRICATED AND INSTALLED DOUBLER IAW SRM 57-2-0, PAGE 12. REF: N/R 0442.SDR DHL200080132CRib · crackedAT C CK; LT WING LEADING EDGE RIB CRACKED .5 INCH STA XFS 725.000. PERFORMED STOP DRILL IAW SRM 57-2-0 PAGE12, FABRICATED AND INSTALLED DOUBLER IAW SRM 57-2-0 PAGE 12. REF: N/R 0443.SDR 20001128AP003Hinge · wornDURING SCHEDULED MAINTENANCE, FOUND LEFT WING INNER TRAIL FLAP OUTBOARD HINGE ARM WORN. REPAIRED LEFT WING INNER FORE FLAP TO TRAIL FLAP OUTBOARD HINGE ARM IAW BOMBARDIER (DEHAV) RD7-57-030. (M)SDR DHL200080173CRib · crackedAT C CK; LT WING LEADING EDGE RIB CRACKED 3/4 INCH, STA. XFS. 740.00. PERFORMED STOP DRILL IAW SRM 57-2-5, FIG 1, CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B, PAGE 1-2, FABRICATED AND INSTALLED DOUBLER IAW SRM 57-2-5, FIG 1. REF: N/R 0441.SDR TWAA0009702Angle · crackedDURING OP 15 MAINT CHECK, ON THE RT WING, NUMBER 8 L/E SLAT WAS CRACKED ON THE L/E. SPAR SUPPORT ANGLE, O/B END. REPLACED LOWER CORD ANGLE 114T07-71, PER BOEING DRAWING 114T4105.SDR TWAA0009616Skin · wornDURING OP 15 MAINT CHECK ON THE RT WING THE NUMBER 12 LEADING EDGE SLAT HAD WORN SPOT ON I/B TRAILING EDGE 43 INCHES FROM THE O/B END. REPAIRED PER SRM 51-70-10, PAGE 37, FIG 9. REPAIRED WITH ONE FLUSH DOUBLER.SDR UPS00433315Rivet · looseINSPECTION TYPE:C, LOOSE RIVETS IN TORQUE TUBE DRIVES AT VARIOUS LOCATIONS I/B END NR 15 KRUEGER FLAP, I/B AND O/B OF NR 1 L/E PDU, I/B AND O/B OF NR 3 PDU RT, OUTPUT OF L/E NR 4 PDU, I/B AND O/B OF NR 3 LT PDU, TORQUE TUBE AT NR 5 VCF, TORQUE TUBE AT NR 4 VCFSDR USAA000821Fitting · gougedPIT - FOUND ACT SPAR INBOARD FITTING GOUGED BY NR 4 SLAT, .5 INCH SEMI CIRCLE BY .002 INCH DEEP, FRONT SPAR ATTACH FITTING, INBOARD LUG FITTING. (M)SDR DHL200080115CAngle · crackedAT C CK; LT WING LE HOUSING ANGLE CRACKED 4 INCH AT XFS. 10.5. REMOVED CRACKED ANGLE, FABRICATED AND INSTALLED NEW ANGLE IAW SRM 57-2-0, FIG 2 AND 51-3-0, PAGE 1. REF: N/R 1450.SDR DHL200080114CPlate · crackedAT C CK; LT WING LE PLATE CRACKED 3/4 INCH AT XFS 11.500. REMOVED CRACKED PLATE, FABRICATED AND INSTALLED NEW PLATE IAW SRM 57-2-1, PARA. 7, AND 51-1-21 PAGE 1. REF: N/R 1449.SDR DL72W001098Stiffener · crackedTPA LTR CHK C-1 06/05/00, I/B SPAR STIFFENER CRACKED AT NR 6 SLAT I/B TRACK. REPLACED PER MM 57-20-21SDR SWAA001019Skin · crackedDURING SCHEDULED C4 CHECK, FOUND NR 1 L/E SLAT LOWER SKIN CRACKED NEAR AFT RIVET ROW OF MID O/B AUX TRACK. REPAIRED SLAT PER SWA RA NR 1-A57-001.SDR CALA0000818Skin · crackedINSPECTION FOUND A 1 INCH CRACK IN LT WING NR 2 SLAT LOWER SKIN AT ACTUATOR AREA. A DOUBLER REPAIR WAS INSTALLED IAW ECRA 5750-02586.SDR P2EA00202Skin · delaminatedYYC - DURING C-CHECK, RIGHT OUTBOARD FOREFLAP, REPAIR DELAMINATED ON UPPER SURFACE 87 INCHES OUTBOARD OF INBOARD END. REPAIRED FOREFLAP IAW SRM 51-40-6, PAGE 8 PARAGRAPH 11. (M)SDR UPS00233235Hinge Fitting · corrodedINSPECTION TYPE: C, NR 6 KRUGER FLAP FIXED CENTER LE HINGE FITTING CORRODED AT LE ATTACH POINT. REPLACED FIXED CENTER LE FITTINGSDR SWAA001001Skin · crackedDURING SCHEDULED A1 CHECK, FOUND NR 1 KRUEGER FLAP CRACKED AT CENTER SECTION. REMOVED AND REPLACED FLAP PER MM.SDR RRXA002667Skin · damagedDURING A MAINTENANCE VISIT FOUND TOO LONG OF SCREWS AND SCREWS PULLING THROUGH SKIN ON THE LEFT I/B SLOT L/E AT STA XS 250 46.5 INCHES FROM FRONT SPAR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE. FABRICATED AND INSTALLED REPAIR IAW EO 00-107 WITSDR CALA0000771Skin · gougedINSPECTION FOUND SKIN OF RT WING O/B LEADING EDGE (AFT OF NR 5 SLAT O/B END) GOUGED AND CHAFED. A REPAIR WAS INSTALLED IAW SRM 51-10-3 AND 51-30-5.SDR UPS00232745Rib · crackedINSPECTION TYPE:C, CRACK FOUND AT I/B RIB NR 5 SLAT. CRACK STOP DRILLED IAW 51-10-01, REPAIR CARRIED OUT IAW SRM 57-50-0 3 FIG 9.SDR SWAA000951Skin · delaminatedDURING SCHEDULED SERVICE CHECK, FOUND NR 1, 2, 3 L/E SLATS DELAMINATED. REMOVED AND REPLACED L/E SLATS PER MM.SDR DHL2000801106Rib · crackedLT WING LEADING EDGE RIB CRACKED 3/4 INCH, STA XFS 603. STOP DRILLED CRACK PER SRM 57-2-0 FIG 2. FABRICATED DOUBLER WITH ALCLADE 2024-T3 0.050 PER SRM 57-2-0.CLEANED TREATED AND PRIMED PER SRM 51-1-8B PAGE 1&2.INSTALLED DOUBLER ON INBD AREA PER SRM 57-2-0SDR AWXA0000328Skin · crackedC-CHECK, CRACKS IN LOWER SKIN OF THE LEADING EDGE OF NR 2 AND NR 3 SLATS. REMOVED DAMAGED AREA IAW ER NR 3-57-55-17E, FABRICATED FILLERS FROM MAT SHT 77075 T6 X .063 QQA 250, 2 DOUBLERS FROM 2024T3 QQA 250/5, INSTALLED FILLER AND DOUBLER IAW 737 SRM 51-40-02SDR UPS00832770Angle · crackedINSPECTION TYPE:C123, RIGHT WING L/E VERTICAL ANGLE IS CRACKED AT XS 520. REMOVED, FABRICATED, AND REPLACED ANGLE IAW DWG 9753297 AND SRM 51-1-20D.SDR SWAA000938Skin · crackedDURING SCHEDULED C1 CHECK, FOUND NR 5 AND NR 6 L/E SLAT LOWER SKINS CRACKED AROUND IDLER TRACK CUTOUTS. REPAIRED SLATS PER SWA RA 1-A57-0691.SDR UPS00832788Rib · gougedINSPECTION TYPE:C123, LEFT WING L/E RIB XS 510 IS GOUGED BEYOND LIMITS. REPAIRED RIB IAW SRM 57-2-0 FIG 2.SDR UPS00832779Rib · crackedINSPECTION TYPE:C123, RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 379. REPAIRED RIB IAW SRM 57-2-0 FIG 2.SDR UPS00832778Rib · crackedINSPECTION TYPE:C123, RIGHT WING L/E RIB IS CRACKED AT XS497.491. REPAIRED RIB IAW SRM 57-2-0 FIG 2.SDR UPS00832776Rib · crackedINSPECTION TYPE:C123, LEFT WING L/E UPPER RIB IS CRACKED AT XFS 647.5. REPAIRED RIB IAW SRM 57-2-0 FIG 2.SDR UPS00832775Angle · 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.SDR UPS00232787Rib · crackedINSPECTION TYPE:C, CRACKS FOUND AT BOTH RIBS I/B TRACK TO NR 7 SLAT CONN. REPAIR CARRIED OUT IAW SRM 57-50-03, FIGURE 9.SDR DL72S001022Angle · crackedNR 4 SLAT ANGLE CRACKED AT I/B STOP PAD. INSTALLED REPAIR PER M/M 57-54-0 PG 816.SDR UPS00832773Rib · crackedINSPECTION TYPE:C123, RIGHT WING L/E UPPER RIB IS CRACKED AT XOLDI 6.225. REPAIRED RIB IAW SRM 57-2-0 FIG 2.SDR DHL200070719CPanel · crackedNR 6 L/E SLAT ANTI-ICE TELOSCOPIC DUCT FAIRING PANEL CRACKED. REMOVED AND REPLACED ANTI ICE DUCT PANEL ON NR 6 L/E SLAT PER SRM 51-30-2. ALODINED AND PRIMED PER SRM 51-10-2.SDR RAAA00B2024Frame · crackedDURING SCHEDULED B2 CHECK, NR 5 SLAT L/E FRAME CRACKED. STOP DRILLED CRACK, FABRICATED REPAIR IAW SRM 51-40-3. INSTALLED FASTENERS IAW SRM 51-30-2.SDR CALA0000697Skin · crackedINSPECTION FOUND A .5 INCH CRACK AT RIVET HOLES OF NR 3 SLAT PANEL ON I/B SIDE OF PANEL. FILLER AND DOUBLER WERE INSTALLED IAW BOEING DRAWING 65C30133.SDR DHL200070721CSlat Track · crackedTHE NR 2 SLAT O/B TRACK TO SLAT ATTACH CLIP IS CRACKED ON THE I/B RADIUS. REPLACED ATTACH CLIP AT NR 2 SLAT O/B TRACK TO SLAT PER SRM 51-30-2.SDR SWAA000910Skin · crackedDURING SCHEDULED 1/4D CHECK, FOUND NR 1 AND NR 4 L/E SLATS LOWER SKIN CRACKED AROUND ACTUATOR CUTOUT. REPAIRED SKIN PER BOEING DRAWING AND TI-657-012.SDR DL72S000968Skin · crackedNR 3 KRUEGER FLAP CRACKED AT O/B LIP HINGE CUTOUT. TPA D-2 LTR CHK. INSTALLED DOUBLER PER M/M 57-53-0, NR 2A.SDR TWAA0007709Skin · delaminatedDURING CHECK-C MAINT, NUMBER 1 SLAT WAS DELAMINATED. REMOVED DELAMINATION, SKIN AND MOISTURE. INSTALLED FILLER AND 7 INCH BY 14 INCH DOUBLER METAL TO METAL HOT BOND PER SRM 51-70-10 AND SEALED EDGE.SDR AWXA0000316Skin · crackedC-CHECK, NR 1 SLAT HAS 2.5 INCH LONG CRACK AT AFT ROW OF RIVETS 62 INCHES O/B OF I/B EDGE. REPAIRED DAMAGE IAW 737 SRM 51-40-02, MATERIAL USED SHEET 2024 T3 X .063 QQA 250/5.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.SDR DL72S000939Bracket · crackedFOUND ON F2 LETTER CK, INBOARD ATTACH BRACKET CRACKED NR 8 SLAT ACTUATOR. REPAIR PER MM 57-20-21.SDR 0001929880Skin · crackedFLAP LEADING EDGE JUST AFT OF NR 2 FLAP HINGE IS CRACKED. REPAIRED PER EA 98-172453. L/P 1437664SDR 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 LON
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