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 UPS204549Rib · crackedWHILE IN FOR SI CHECK, MAINTENANCE FOUND CRACKED RIB ON NR 5 SLAT 23 INCHES FROM O/B END (4TH RIB FROM O/B END, MARKED). REMOVED AND REPLACED 4TH RIB FROM O/B END OF NR 5 SLAT IAW SRM 51-30-2, 51-30-5.SDR UPS204532Slat · corrosionWHILE IN FOR C-CHECK, MAINTENANCE FOUND NR 5 K-FLAP ATTACH LUGS ARE CORRODED AT LUG MOUNT BOLTS OUT OF LIMITS. REMOVED AND REPLACED NR 5 K-FLAP PER MM 27-81-1 AND MM 27-81-00.SDR DL757953849Te Wedge · delaminatedDURING A SHOP INSPECTION, THE TRAILING EDGE WEDGE WAS FOUND TO BE DELAMINATED. A NEW WEDGE WAS INSTALLED PER SRM 57-42-02, ON NR 3 L/E SLAP PANEL.SDR DL72E960074Rib · crackedUPON ROUTINE INSPECTION, A CRACK WAS FOUND ON THE 5TH RIB FROM THE O/B END NR 4 L/E SLAT. REPAIRED AS PER 57-54-0, FIG 805.SDR DL72E960073Rib · crackedUPON ROUTINE INSPECTION, A CRACK WAS FOUND ON THE 17TH RIB FROM O/B END OF NR 4 L/E SLAT. REPAIRED AS PER MM 57-54-0, FIG 805.SDR DL767953822Te Wedge · dentedSLAT WAS SENT TO SHOP FOR REPLACEMENT OF T/E WEDGE DUE TO HAIL DAMAGE. WEDGE WAS INSTALLED ACCORDING TO THE CMM 57-43-55.SDR DL767953821Te Wedge · dentedSLAT WAS SENT TO SHOP FOR REPLACEMENT OF T/E WEDGE DUE TO HAIL DAMAGE. WEDGE WAS INSTALLED ACCORDING TO THE CMM 57-43-55.SDR DL72S953828Doubler · crackedFOUND DURING C-1 LETTER CHECK - DOUBLER UNDERNEATH I/B STOP PAD NR 7 SLAT IS CRACKED. REPAIRED PER MM 57-54-0 PAR 12.SDR DL72S953826Rib · crackedFOUND DURING C-1 LETTER CHECK - 1.25 INCH CRACK IN RIB ON NR 7 SLAT I/B OF I/B TRACK. REPAIRED PER MM 57-54-0.SDR 95FDEA01418Skin · gougedTHE NR 6 SLAT L/E HAS SMALL GOUGES APPROX 28 INCHES FROM O/B END. REMOVED DAMAGE, FABRICATED REPAIR AND INSTALLED ON NR 6 SLAT L/E APPROX 28 INCHES FROM O/B END IAW FEDEX SRM 57-50-1, 57-50-3, DWG 65-17302.SDR DL767953809Skin · dentedHAIL DAMAGE TO UPPER SURFACE OF NR 7 L/E SLAT. REPLACED WEDGE PER CMM 57-43-61.SDR EISA95334Hinge Fitting · corrodedUPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, THE LEFT WING NR 3 KRUGER FLAP INBOARD HINGE FITTING WAS FOUND WITH CORROSION. REMOVED AND REPLACED THE NR 3 KRUGER FLAP INBOARD HINGE FITTING IAW B727 MM 27-81-0. (M)SDR DL767953824Te Wedge · dentedTHE WEDGE OF THE SLAT WAS DENTED DUE TO HAIL DAMAGE. THE WEDGE WAS REPLACED PER THE CMM 57-43-61. THE WEDGE REPLACEMENT IS THE TERMINATING ACTION FOR A.D. 93-14-19.SDR DL72S954010Rib · crackedATL - HMV, RIB CRACKED NR 7 LE SLAT NR 10 RIB CRACKED ON TOP FLANGE. ROUTED OUT DAMAGE AND FABRICATED DOUBLER PER MM 57-54-0 PG 819. FABRICATED FILLER, INSTALLED DOUBLER AND FILLER PER M/M 57-54-0 PG 819.SDR DL72S953800Angle · crackedFOUND ON A2 LETTER CHECK, NUMBER 7 SLAT COVE SKIN ANGLE CRACKED .25 INCH IN UNDER ANTI-ICE DUCT. REPAIRED PER MM 57-54-0.SDR DL72S953799Angle · crackedFOUND ON A2 LETTER CHECK, NR 1 SLAT COVE SKIN ANGLE CRACKED AT THE OUTBOARD STOP PAD. REPAIRED PER MM 57-54-0.SDR DL767953825Te Wedge · dentedHAIL DAMAGE OCCURRED TO UPPER SURFACE OF T/E WEDGE. REPLACED WEDGE IN C/W C.M.M.57-43-41.SDR DL767953823Skin · dentedHAIL DAMAGE TO UPPER SURFACE OF NR 4 L/E SLAT. THE TRAILING EDGE WEDGE WAS REPLACED PER CMM 57-43-55. THE PART NUMBER OF THE NEW WEDGE IS 114T4114-17. THIS IS THE TERMINATING ACTION FOR A.D. 93-14-19.SDR DL72S954009Angle · crackedATL - HMV, ANGLE CRACKED NR 2 K-FLAP ACT MOUNT, INBD LOWER ANGLE IS CRACKED. REMOVED ANGLE, STOP DRILLED CRACK, DRILLED REPAIR DOUBLER PER MM 57-20-21 PG 811 AND INSTALLED REPAIR DOUBLER PER MM 57-20-21.SDR UPS204481Rib · crackedWHILE IN FOR SI CHECK, MAINTENANCE FOUND A CRACK IN THE RIB OF THE NR 6 SLAT ATTACH ROD END ATTACH POINT. MAINTENANCE REMOVED THE CRACKED RIB AND REPLACED WITH A NEW RIB IAW SRM 51-30-2, 51-30-8 AND 51-30-5.SDR EISA95370Ribs · mismanufacturedDURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND NR 3 LEADING EDGE SLAT HAS THREE RIBS WITH LOWER SURFACE FLANGES PREVIOUSLY TRIMMED BEYOND .100 INCH LIMIT. FABRICATED THREE REPAIR ANGLES IAW B727 SRM CH 57-50-3 PO NR 60733 7075-0 X .040 HEAT SDR DL72S953778Rib · crackedDURING HMV, FOUND NR 8 SLAT, RIB NR 13 WAS CRACKED IN RADIUS. REPAIRED PER M/M 57-54-0 FIG 805.SDR MWEA95315Skin · punctureDURING INSPECTION, THE RT NR 1 SLAT RECEIVED A 2 INCH DIAMETER PUNCTURE HOLE, WHEN INADVERTENTLY STRIKING WORK STAND. MAINTENANCE INSTALLED 30 DAY TEMPORARY PATCH REPAIR IAW DOUGLAS APPROVAL AND SRM 57-09 FIG 10A. RETURNED A/C TO SERVICE.SDR DL72S953777Rib · crackedDURING HMV, FOUND NR 4 SLAT HAS CRACK AT ACTUATOR ATTACH O/B RIB. REPAIRED PER MM 57-54-0 FIG 804.SDR DL72S953776Rib · crackedDURING HMV, FOUND NR 3 SLAT HAS CRACK IN LOWER SURFACE OF NR 3 RIB FROM I/B END. REPAIRED PER MM 57-54-0 FIG 805.SDR DL72S953748Angle · crackedFOUND DURING HMV - NR 6 SLAT, CRACKED ANGLE BETWEEN DE-ICE TUBE AND FARTHEST ROLLER TRACK. REPAIRED PER M/M 57-54-0, FIG 812.SDR DL72S953730Actuator Mount · crackedFOUND AT HMV, NR 4 SLAT MAIN ACTUATOR MOUNT CRACKED AT PREVIOUSLY REPAIRED AREA. REPAIRED PER M/M 57-54-0, FIG 804A.SDR DL72S953729Rib · crackedFOUND ON HMV RIB WEB AT TAI, TUBE CRACKED AT NR 6 SLAT INBOARD WEB. REPAIRED RIB PER M/M 57-54-0, FIG 805.SDR EISA95362Skin · damagedDURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND NR 3 SLAT HAS EXCESSIVE MATERIAL REMOVED FROM UPPER SKIN IN AREA OF INBOARD SLAT HOOK FORWARD MOUNTING SCREW. FABRICATED REPAIR WITH 2024T3 X.090 TRAV NR 1A-720 PO NR 605687 APPROX 4.5 INCHES BSDR DL73S953736Skin · dentedDURING SHOP INSPECTION, NR 4 LEADING EDGE SLAT WAS FOUND WITH DENT TO LEADING EDGE SKIN AT 10 FROM THE OUTBOARD END, REPAIRED PER SRM 57-50-3, FIG 1.SDR USAA951053Skin · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND THREE .375 INCH CRACKS AT NR 1 SLAT BS 299.32 ON BOTTOM SKIN. CUT OUT SECTION OF SKIN AND INSTALLED DOUBLER, REPAIRED PER EA 39909. (M)SDR DL72S953711Rib · crackedDURING SHOP INSPECTION, FOUND NR 2 L/E SLAT WITH RIB NR 20 CRACKED. REPAIRED PER MM 57-54-0 FIG 14.SDR EISA95359Skin · damagedDURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, HEADS GROUND OFF HI-LOCS AND EXCESSIVE MATERIAL WAS REMOVED FROM NR 3 SLAT SKIN. REMOVED FASTENERS AND CLOSED OUT PANELS TO F.O.M. REPAIR. FABRICATED REPAIR 5 INCHES BY 6.5 INCHES FROM 2024T3-.080 SDR DL72W953704Angle · crackedFOUND ON B2 LETTER CHECK, CRACK IN NR 2 SLAT TAI DUCT CUTOUT. REPAIRED PER MM 57-54-0.SDR DL72S953695Bracket · crackedDURING HMV, FOUND NR 6 KRUEGER FLAP ACTUATOR BRACKET IS CRACKED AT I/B LOWER FWD CORNER. REPAIRED PER M/M 57-20-21.SDR DL72S953693Rib · crackedDURING SHOP INSPECTION, FOUND RIB NR 9 AND NR 14 CRACKED. REPAIRED PER MM 57-54-0 FIG 814, NR 2 L/E SLAT.SDR EISA95377Angle · corrosionDURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, CORROSION BEYOND LIMITS NR 2 SLAT ATTACH ANGLE IAW 51-10-6 100 PERCENT METAL REMOVAL WAS FOUND. FABRICATED NEW ATTACH ANGLE, ALODINED AND PRIMED AND INSTALLED NEW BRACKET IAW B727 SRM 51-10-1, 51-10-2SDR DL72S953690Angle · crackedDURING SHOP INSPECTION, NR 1 L/E SLAT LOWER COVE SKIN SUPPORT ANGLE WAS FOUND CRACKED. REPAIRED PER MM 57-54-0 FIG 812.SDR DL72S953674Angle · crackedFOUND ON A2 LETTER CHECK, NUMBER 2 SLAT COVE SKIN ATTACH ANGLE IS CRACKED AT INBD STOP PAD. REPAIRED PER MM 57-54-0.SDR DL72S953673Angle · crackedFOUND ON A2 LETTER CHECK, NR 2 L/E SLAT COVE SKIN ATTACH ANGLE IS CRACKED AT OUTBD STOP PAD. REPAIRED PER MM 57-54-0.SDR DL72S953670Angle · crackedCRACK AT L ANGLE UNDER TAI DUCT. REPAIRED PER M/M 57-54-9 FIG 805A. FOUND AT SHOP INSPECTION FOR NR 6 L/E SLAT PANEL.SDR DL72S953772Rib · crackedDURING HMV, NR 8 SLAT, RIB NR 6 FOUND CRACKED IN RADIUS. REPAIRED PER M/M 57-54-0.SDR DL72S953771Rib · crackedDURING HMV, FOUND NR 3 SLAT, RIB NR 6 CRACKED IN RADIUS. REPAIRED PER M/M 57-54-0 FIG 805.SDR DL72S953770Rib · crackedDURING HMV, FOUND NR 3 SLAT, RIB NR 7 CRACKED IN RADIUS. REPAIRED PER M/M 57-54-0 FIG 805.SDR DL72S953769Rib · crackedDURING HMV, FOUND NR 3 SLAT, RIB NR 9 CRACKED IN RADIUS. REPAIRED PER M/M 57-54-0 FIG 805.SDR DL72S953768Rib · crackedDURING HMV, FOUND NR 4 SLAT RIB CRACKED O/B RIB OF O/B TRACK. REPAIRED PER MM 57-54-0.SDR DL72S953745Rib · crackedFOUND DURING HMV - NR 8 SLAT NR 13 RIB IS CRACKED IN RADIUS. FABRICATED REPAIR PER M/M 57-54-0, FIG 805.SDR DL72S953744Angle · crackedFOUND DURING HMV, NR 6 SLAT, CRACKED ANGLE BETWEEN DE-ICE TUBE AND FARTHEST ROLLER TRACK. REPAIRED CRACK PER M/M 57-54-0, FIG 812.SDR DL72S953733Web · crackedDURING HMV, FOUND NR 6 SLAT I/B WEB AT DE-ICE TUBE CRACKED. REPAIRED ANGLE PER M/M 57-54-0 FIG 805.SDR DL72S953684Panel · damagedDURING SHOP INSPECTION, FOUND LEADING EDGE SLAT DAMAGED ON OUTBOARD END. REPAI RED DAMAGE PER THE 727 SRM 57-50-3 FIG 1, FOR NR 2 L/E SLAT PANEL.
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