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.
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 UPS96221030Web · crackedINSPECTION TYPE-C, THE NR 1 SLAT ACTUATOR I/B ATTACH WEB CRACKED. REMOVED WEB DAMAGE AND FABRICATED REPLACEMENT WEB PER SB 727-57-0130, INSTALLED REPLACEMENT WEB PER SB 727-57-0130 AND SRM 51-30-2.SDR 96UAL900639Flap · corner missingOUTBOARD CORNER OF NR 16 KRUEGER PLAP WAS FOUND MISSING. DETAILED INVESTIGATION OF THE REMAINING FLAP STRUCTURE FOUND NO DELAMINATION OR CRACKS. INSTALLED DOUBLER REPAIR.SDR 9618682715Casting · crackedDURING H-CHECK, FOUND A CRACK IN THE NR 2 LEADING EDGE FLAP BULLNOSE HINGE CASTING, OUTBOARD SIDE AT THE RADIUS. REPLACED FLAP (P/N 65-16226-7A) PER MM 27-81-01.SDR DL72S971363Skin · crackedSKIN CRACKED AT FAIRING NUMBER 5 SLAT.SDR TAOA089604Skin · crackedFOUND NR 4 LEADING EDGE SLAT, P/N 651622171, HAS 2.5 INCH TO 3 INCH CRACK ON LOWER TRAILING EDGE AT OUTBOARD EDGE OF SKIN. (M)SDR DL757961895Te Wedge · delaminatedT/E WEDGE HAD SEVERAL DELAMINATED AREAS. REPLACED DAMAGED WEDGE PER SRM 57-43-02, FIGURE 2.SDR P5CA9601229Arm · corrodedL/E FLAP 7 INCHES INBOARD ARM SURFACE CORROSION. CORROSION REMOVED FROM SURFACE PER SRM 51-10-01.SDR P5CA9601228Beam · crackedLEFT INBOARD KREUGER L/E FLAP PDU AFTER MOUNT BEAM INBOARD EDGE CRACKED. FAB NEW ANGLE PER SRM 57-12-01 AND INSTALLED PER SRM 51-30-02.SDR EISA96141Shield · crackedLEFT WING, NR 3 LEADING EDGE FLAP ANTI-ICE SHIELD CRACKED IN SEVERAL PLACES AROUND RIVETS. REPLACED BAFFLES PER SRM 51-30-02. (M)SDR EISA96130Bracket · crackedRIGHT WING NR 5 SLAT INBOARD TRACK, INBOARD SIDE, BRACKET CRACKED. FABRICATED AND INSTALLED NEW BRACKET PER SRM 51-10-01. (M)SDR EISA96129Rib · crackedRIGHT WING NR 5 SLAT, TWO CRACKED RIBS AT ACTUATOR ATTACH BOLT. FABRICATED DOUBLER PER SRM 51-40-00 AND INSTALLED PER SRM 53-40-0. (M)SDR DL76S961847Te Wedge · delaminatedTHE NRS 10, 11, 12 LEADING EDGE SLATS' TRAILING EDGE WEDGES WERE FOUND TO HAVE AREAS OF DELAMINATION. THE AREAS MEASURE 4 INCHES BY 6 INCHES, 2 INCHES BY 3 INCHES, AND 10 INCHES BY 6 INCHES, RESPECTIVELY. REPAIRED IN ACCORDANCE WITH B767-300 SRM, 57-43-02, FSDR W8PA960107Skin · delaminatedNR 5 SLAT UPPER SKIN AT OUTBOARD END HAS DELAMINATED SKIN. REMOVED DAMAGE ON UPPER SKIN TIE OUTBOARD. RECOVERED AND FABRICATED DOUBLERS. INSTALLED DOUBLERS AND ADHESIVE CORE. BAGGED FOR A 250 DEGREE COOK. REMOVED BAG CLEANED AND SANDED AREA IAW SRM 51-70-SDR MWEA96356Rib · crackedDURING D-CHECK, RT WING NR 4 SLAT OUTBD DRIVE FITTING RIB ASSY WAS FOUND CRACKED BETWEEN 2 FASTENERS ON LOWER FLANGE. REPLACED RIB SET IAW SRM 57-02 PAGE 1, 2.SDR MWEA96350Fitting · oversize holeDURING D-CHECK, RT NR 2 SLAT CENTER FITTING FOUND WITH ENLARGED HOLE DIAMETER FOR THE ECCENTRIC ATTACH BOLT. REPAIRED OVERSIZED HOLE IAW DAC TELEX SVC-MSP-0451/PPS DATED 11 JUNE 96.SDR MWEA96349Fittings · corrodedDURING D-CHECK, NR 4 SLAT INBD FITTING FOUND WITH TWO PREVIOUSLY CORRODED SPOT FACES WHICH ARE PRESENTLY RECORRODED. REPAIRED FITTINGS IAW DAC TELEX SVC-MSP-0365/PDG DATED 17 MAY 96.SDR MWEA96348Ribs · crackedDURING D-CHECK, LT WING HAD TWO LEADING EDGE RIBS FOUND CRACKED AT NR 1 SLAT INBD AREA. REPLACED RIBS IAW SRM 57-01, PG 1, 2.SDR DL72W970183Rib · crackedDURING INITIAL INSPECTION, RIB NR 4 AND RIB NR 5 WERE FOUND CRACKED. THEY WERE REPAIRED PER SRM 57-50-3.SDR USAA960544Skin · crackedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND THREE .5 INCH CRACKS NR 1 SLAT LOWER SKIN SLAT STATION 299.10. CUT OUT CRACKED SKIN, INSTALLED FILLER AND DOUBLER. (M)SDR 96FDEA01284Bonding Jumper · corrosionNR 0261 003. CORROSION AROUND NR 2 K-FLAP OUTBOARD LOWER BONDING JUMPER UPPER ATTACH POINT. REPAIRED NR 2 K-FLAP OUTBOARD LOWER BONDING JUMPER UPPER ATTACH POINT IAW SRM 57-50-03. MOVED ATTACH POINT IAW SRM 27-57-010C.SDR UPS96220724Rib · crackedINSPECTION TYPE SI, NR 4 SLAT 5TH RIB FROM I/B END IS CRACKED AT NUTPLATE. REPAIRED NR 4 SLAT 5TH RIB FROM I/B END SRM 57-50-3.SDR UPS96220738K-Flap · crackedINSPECTION TYPE-C, NR 1 K-FLAP 6 INCHES O/B OF I/B HINGE, WEB L/E INSIDE HAS A 3 INCH CRACK. REMOVED, FABRICATED REPLACEMENT PART AND INSTALLED IAW 57-10-2 AND 51-30-2.SDR 96FDEA01277Skin · delaminatedDISCREPANCY: (NR 0026)(O01) LEFT WING INBOARD AFT FLAP IS DELAMINATING ALONG 0113 EDGE UPPER AND LOWER SURFACES. CORRECTIVE ACTION: ****S/D****** COMING.SDR UPS96220736Inner Web · crackedINSPECTION TYPE-C, NR 3 SLAT INNER WEB AT ACTUATOR CRACKED ON BOTH SIDES. STOP DRILLED CRACKS PER SRM 51-10-1, FABRICATED AND INSTALLED WEB REPAIR PER SRM 51-40-3 AND 57-50-1.SDR DL72L961705Rib · crackedRIB CRACKED AT RADIUS. REPAIRED RIB PER M/M 57-54-00.SDR DL72L961704Rib · crackedRIB CRACKED AT RADIUS. REPAIRED RIB PER M/M 57-54-00 PG 813.SDR DHL9671535DRib · crackedAT D-CHECK, NR 2 SLAT, SECOND RIB FROM THE OUTBOARD END, FOUND CRACKED . CUT OUT DAMAGED AREA AND INSTALLED DOUBLER REPAIR, PER SRM 57-30-3, 5 INCHES BY 3 INCHES.SDR EISA96115Angle · crackedLEFT WING NR 1 SLAT OUTBOARD TRACK ATTACH FORWARD ANGLE BRACKET CRACKED. INSTALLED NEW ANGLE BRACKET PER SRM 51-10-1. TT: 66,991:57 HOURS. TC: 45,084. (X)SDR EISA96114Angle · crackedLEFT WING, NR 1 SLAT, INBOARD TRACK ATTACH FORWARD ANGLE BRACKET CRACKED. FABRICATED AND INSTALLED REPAIR PER SRM 51-40-03. TT: 66,991:57 HOURS. TC: 45,084. (X)SDR DL72S961736Rib · crackedRIB CRACKED NR 3 L/E SLAT, O/B OF ACTUATOR ATTACH BRACKET O/B RIB. FABRICATED REPAIR PER MM 57-54-0 PG 804.SDR DL72S961734Bracket · crackedFOUND CRACK ON I/B ACTUATOR BRACKET FOR THE NR 2 L/E K-FLAP. REPAIRED PER M/M 57-20-21 FIG 807 AND INSTALLED PER M/M 57-20-21 PG 811.SDR DL72S961696Skin · gougedDEEP GOUGE IN LWR SKIN BY LINE UP SPADE. REPAIRED PER SRM 57-50-3.SDR UPS96220636Angle · crackedINSPECTION TYPE-C, LT WING NR 2 SLAT, RIB TO RIB ATTACH ANGLE HAS 5 INCH CRACK AT O/B HOOK. REMOVED ANGLE, FAB'D REPLACE ANGLE AND INSTALLED IAW SRM 57-50-2, 51-30-2.SDR DL757961722Te Wedge · delaminatedTHE TRAILING EDGE WEDGE ON THE NR 7 SLAT WAS FOUND WITH DELAMINATION 20 INCHES FROM THE INBOARD END OF THE SLAT. THE DAMAGE MEASURED 2 INCHES ACROSS AND EXTENDED .25 INCH FWD OF THE AFT END OF THE PART. THIS DAMAGE WAS REPAIRED PER B757 SRM 51-70-10 AS SPECISDR DL72K961733Angle · crackedA .25 INCH CRACK EXTENDING FROM NR 2 SLAT O/B TRACK UPSTOP PAD IN COVE SKIN ATTACH ANGLE. INSTALLED DOUBLER PER M/M 57-54-0 PG 816.SDR DL72K961714Cove Skin Angle · crackedFOUND .25 INCH CRACK EXTENDING FROM NR 2 SLAT O/B TRACK UP STOP PAD, IN COVE SKIN ATTACH ANGLE. REPAIRED PER M/M 57-54-0 PG 816.SDR 96FDEA01217Bonding Jumper · corrodedDISCREPANCY: NR 0551 (015) CORROSION (C57-562-01) NR 2 K-FLAP TO BULLNOSE INBOARD BONDING JUMPER UPPER ATTACH POINT. CORRECTIVE ACTION: CORRODED AREA FOUND TO BE OUT OF LIMITS PER FEDEX DWG R 27-57-010. REPAIRED NR 2 K-FLAP TO BULLNOSE INBOARD BONDING JUMPSDR 96FDEA01226Bonding Jumper · corrodedNR 0552, 018, CORROSION (C57-562-01) NR 3 K-FLAP TO BULLNOSE O/B BONDING JUMPER, UPPER LOWER ATTACH POINTS. *S/D* REPLACED NR 3 K-FLAP BULLNOSE, REPAIRED K-FLAP RIB AT O/B BONDING JUMPER UPPER ATTACH POINT IAW MM 27-81-1, SRM 57-50-3.SDR 96FDEA01219Bonding Jumper · corrodedNR 0547, 007, CORROSION (C57-562-01) AT BOTH ATTACH POINTS ON THE O/B BONDING JUMPER ON THE NR 5 K-FLAP BULLNOSE. *S/D* REPAIRED UPPER ATTACH POINT PER FEDEX SRM 57-50-3 FIG 3, LOWER ATTACH POINT WITHIN LIMITS AFTER CORROSION REMOVAL PER FEDEX DWG R 27-57-01SDR P2EA96004Track Rib · wornDEN - FLT 48 - THE NR 6 SLAT WOULD NOT FULLY RETRACT AFTER TAKEOFF. (RETURN TO DEN, NO EMERGENCY DECLARED, LANDING UNEVENTFUL.) REMOVED AND REPLACED INBOARD AND CENTER AUXILIARY TRACK RIBS ON NR 6 SLAT. ADJUSTED IAW MM 27-81-21. OPS CHECK GOOD. (X)SDR 96FDEA01227Upper Lug · corrodedNR 0549, 019, CORROSION (C57-562-01) ON THE O/B UPPER LUG O/B HINGE NR 4 K-FLAP. *S/D* REMOVED AND REPLACED K-FLAP PER MM 27-81-1.SDR 96FDEA01222Skin · corrodedNR 0181, 008, NR 1 K-FLAP DATA PLATE AREA HAS CORROSION. *S/D* REMOVED CORROSION BY CUTTING OUT DAMAGED AREA AND INSTALLING FILLER AND REPAIR PLATES IAW SRM 29-57-010 AND 51-10-06.SDR UPS96220627Rib · crackedINSPECTION TYPE-C, LT WING, NR 4 SLAT L/E RIB IS CRACKED AT BOTTOM 8 INCHES I/B OF O/B END. REMOVED DAMAGED AREA PER SRM 57-50-3, FIG 9, FAB AND INSTALLED DOUBLER PER SRM 57-50-3 FIG 9.SDR 96FDEA01184Hinge Lugs · corrodedNR0088 AND 021, NR 2 K-FLAP CENTER HINGE LUGS UPPER AND LOWER FASTENERS HAVE CORROSION. *S/D* REMOVED K-FLAP AND REPLACED IAW FEDEX MM 27-81-1.SDR 96FDEA01172Flap · corrodedNR0078 AND 018, NR 4 K-FLAP O/B HINGE LUGS CORRODED UNDER FASTENERS. *S/D* REMOVED CORRODED NR 4 K-FLAP AND INSTALLED NEW NR 4 K-FLAP IAW FEDEX MM 27-81-1, FUNCTIONAL CHECK GOOD IAW FEDEX MM 27-81-11.SDR DL72S961528Rib · crackedFOUND A .5 INCH CRACK IN RADIUS OF NOSE RIB INBD SIDE OF INBD TRACK, NR 6 SLAT. REPAIRED PER MM 57-54-0.SDR DL72E961711Spar Web · damagedUPPER SPAR WEB FLANGE DAMAGED BY STOP DRILLING RIBS NR 11 AND NR 12. MANUFACTURED DOUBLER, REPAIRED PER SRM 57-50-3 FIG 4.SDR DL72E961710Rib · crackedLOWER FLANGE OF RIB NR 18 CRACKED IN RADIUS. STOP DRILLED CRACK AND REPAIRED PER SRM 57-54-0.SDR DL72E961709Rib · crackedLOWER AFT FLANGE CRACKED, UPPER FLANGE CRACKED AND STOP DRILLED BUT NO DOUBLER AND FWD FLANGE HAS TEMPORARY REPAIR. REPLACED RIB.SDR DL72E961708Rib · crackedLOWER AFT FLANGE DOUBLER CRACKED, UPPER FWD FLANGE CRACKED PAST STOP DRILL AND LOWER FWD FLANGE DOUBLER CRACKED. REPLACED RIB.
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