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 DL72W951479Rib · crackedNR 5 SLAT RIB CRACKED, OB RIB OF OB TRACK ATTACH POINT IS CRACKED AT SCREW HOLE 2 INCHES UP FROM LOWER SKIN. REPAIRED PER SRM 57-50-3 FIG 9.SDR DL72W951478Rib · crackedRIB CRACKED NR 5 SLAT, FWD TOP CORNER OF RIB MARKED 119IB RIB AT ACT IS CRACKED. REPAIRED PER MM 57-54-0 PG 815 TO 815A. FOUND AT HMV.SDR DL72W951475Angle · crackedNR 8 SLAT ANGLE CRACKED, ANGLE IS CRACKED UNDER IB UPSTOP FITTING NR 8 SLAT. REPAIRED PER MM 57-54-0 FIG 812. FOUND AT HMV, INSPECTION.SDR DL72W951474Rib · crackedNR 3 SLAT RIB CRACKED IB RIB AT ACT ATTACH POINT IS CRACKED AFT LOWER CORNER. REPAIRED PER MM 57-54-00 PG 806-807.SDR UPS202767Rib · crackedDURING 'C' CHECK, MAINTENANCE FOUND NR 5 SLAT RIB CRACKED. FABRICATED AND INSTALLED REPAIR PER SRM 57-50-3.SDR UPS202766Attach Points · corrodedDURING 'C' CHECK, MAINTENANCE FOUND NR 6 K-FLAP ATTACH POINTS CORRODED ON K-FLAP SIDE. REPLACED FLAP PER MM 27-81-01.SDR DL72S951446Angle · crackedFOUND ON CV2 NR 8 SLAT ANGLE CRACKED UNDER TELESCOPING TAI DUCT. REPAIRED PER MM 57-54-0 PAR 5A.SDR DL72K951356Slat · crackedCRACK BELOW ANTI-ICE TUBE NR 2 SLAT OPN 5535 AD. FOUND AT B-1 LETTER CHECK. REPAIRED PER MM 57-54-0 FIG 805A.SDR SWAA95270Skin · crackedDURING SCHEDULED D-CHECK, FOUND NUMBER 3 SLAT SKIN CRACKED AT T/E. REPAIRED PER BOEING DRAWING BAC 65C30133.SDR DL72W951358Downstop · crackedFOUND AT HMV, NR 2 SLAT DOWNSTOP HAS CRACK WHERE DOWNSTOP CONTACTS. ADJACENT TO DOWNSTOP ON SLAT CORNER, AT UPSTOP. REPAIRED PER MM 57-54-0 PG 820 AND 821, REF NR CARD NR 1672.SDR DL72W951336Rib · crackedA .5 INCH CRACK AT NR 6 SLAT O/B ACT ROD END SUPPORT RIB. FOUND DURING E-1 LTR CK. REPAIRED PER MM 57-54-0 PG 803.SDR DL72S951333Skin · dentedLOWER LEADING EDGE SKIN DENTED 26 INCHES FROM INBORD END. REPAIED LEADING EDGE AS PER THE 727 SRM 57-50-3. FLUSH REPAIR FIGURE ONE. DURING SHOP INSPECTION OF SLAT PANEL.SDR UPS202759Flap · corrosionWHILE IN 'C' CHECK MAINTENANCE FOUND NR 3 K-FLAP O/B HINGE O/B LUG UPPER AND LOWER BOLT HOLES HAVE PITTING AROUND O/B SIDE. REPLACED K-FLAP PER MM 27-81-00.SDR UPS202758Flap · corrosionWHILE IN 'C' CHECK MAINTENANCE FOUND NR 6 K-FLAP O/B HINGE LUG ATTACH POINT HAS CORROSION UNDER TOP BOLT O/B SIDE. REPLACED K-FLAP PER SRM 57-51-1 AND MM 27-81-01.SDR UPS202725Rib · crackedWHILE IN 'D' CHECK, MAINTENANCE FOUND CRACK ON NR 3 SLAT RIB, LWR AFT CORNER WHERE RIB AND LWR CHORD ATTACH. INSTALLED REPAIR PER SRM 51-30-2, 57-50-3.SDR UPS202723Flap · corrodedWHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON NR 3 K-FLAP, O/B BULLNOSE, UPPER HINGE LUG ATTACH FRAME, UPPER SURFACE ON BOTH NUTS. REPLACED K-FLAP PER SRM 57-50-01, OHM 57-51-21, MM 27-81-01.SDR DL72S951312Rib · crackedTHE NR 4 L/E SLAT RIB CRACKED .5 INCHES O/B SIDE. FOUND DURING A-2 LTR CHECK. REPAIRED PER MM 57-54-0 PG 803.SDR DL72S951310Skin · crackedFOUND DURING E-2 LETTER CHECK, BOLT SHEARED AND UPPER SKIN WEDGE CRACKD 1 INCH NR 6 SLAT I/B GUIDE HOOK. REPAIRED PER SRM 57-50-3 FIG 10.SDR DL757951576Skin · delaminatedDURING INSPECTION, LEFT WING SLAT PANEL WAS FOUND WITH SKIN DELAMINATED AT THE INBOARD EDGE UNDER DOUBLER. REPAIRED PER SRM 51-70-10.SDR DL72E951287Slat · crackedNUMBER 5 SLAT CRACKED AT NOSE RIBS WHERE ACT ROD END ATTACHES. FOUND DURING E-2 LETTER CHECK TPAMM 3/27/95. FOUND PREVIOUS DOUBLERS CRACKED. REPLACED SLAT ASSEMBLY.SDR 95ZZZX1829Channel · crackedSTRESS CRACKS AT RT AFT LOWER RADIUS AND CRACKED AT LT LOWER RADIUS. SUSPECT IMPROPER OR LACK OF SHIMMING C/T CHANNEL TO TRACK ATTACH POINT.SDR 95ZZZX1828Channel · crackedCRACKED IN BEND RADIUS. SUSPECTED IMPROPER OR LACK OF SHIMMING C/T CHANNEL TO TRACK ATTACH POINT.SDR 95ZZZX1827Upstop · corrodedPITTING CORROSION AT CONTACT POINT. SUSPECT PROTECTIVE COATING MISSING.SDR 95ZZZX1826Spring · damagedSPRING (56) IS COMPRESSED INSIDE STOP (57). GUIDE (55) RELEASED FROM SPRING (56) AND WAS CRUSHED INSIDE LOCK PISTON (47). GUIDE (55) IS TIGHTLY INSTALLED INSIDE SPRING (56). SUSPECT THAT GUIDE (55) WAS NOT TIGHT INSIDE SPRING (56), CAME LOOSE AND CAUSED COLSDR 95ZZZX1825Fence · crackedDURING TEAR-DOWN INSPECTION, AERODYNAMIC FENCE WAS REMOVED FOR CLEANING AND INSPECTION OF SLAT SKIN. DYE PENETRANT INSPECTION PERFORMED WHICH REVEALED TWO CRACKS AT SLAT STA 86.75, .5 INCH LONG, STA 91.75, .4 INCH LONG UPPER SKIN SURFACE. SUSPECT TOO SMALL OSDR 95ZZZX1824Fence · crackedDURING TEAR-DOWN INSPECTION, AERODYNAMIC FENCE WAS REMOVED FOR CLEANING AND INSPECTION. DYE PENETRANT INSPECTION REVEALED TWO CRACK INDICATIONS AT STA 82.5-30.0 C/T LOWER SKIN NR 1 HOLE .2 INCH AND .25 INCH LONG OUT FROM HOLES. AT STA 86.5, UPPER SURFACE NR SDR 95ZZZX1823Fence · crackedDURING TEAR-DOWN INSPECTION, A CRACK WAS DETECTED IN THE EXTERIOR SKIN C/T AERODYNAMIC FENCE ATTACHMENT POINTS (3 PLACES) AT SLAT STA 86.5, STA 88.0, AND STA 91.75. DYE PENETRANT INSPECTION CONFIRMED CRACKS ALL APPROXIMATELY 1.25 INCH LONG IN LENGTH, IN UPPERSDR 95ZZZX1822Fence · crackedDURING TEAR-DOWN INSPECTION FOR CLEANING AND INSPECTION OF SLAT EXTERIOR SKIN C/T AERODYNAMIC FENCH ATTACH HOLES, DYE PENETRANT INSPECTION REVEALED CRACK INDICATION, STA 82.5 .35 INCH LONG NR 1 HOLE UPPER SURFACE. SUSPECT TOO SMALL OF AREA WASHER, PN 66-20913SDR 95ZZZX1821Fence · crackedDURING TEAR-DOWN INSPECTION, A CRACK WAS DETECTED IN THE EXTERIOR SKIN C/T AERODYNAMIC FENCE ATTACHMENT POINT AT SLAT UPPER SURFACE NR 2 HOLE FROM L/E AT STA 86.5. DYE PENETRANT INSPECTION CONFIRMED CRACK, WAS .80 INCH LONG. SUSPECT TOO SMALL OF AREA WASHER,SDR DL72W951301Doubler · misinstalledAT HMV, FOUND DOUBLERS INSTALLED BACKWARDS ON UPPER T/E SKIN OF NR 4 SLAT, NOT AERODYNAMICALLY SMOOTH. INSTALLED DOUBLERS PER SRM 57-50-3 PG 27.SDR DL72S951259Doubler · crackedDURING SHOP INSPECTION, DOUBLER ON RIB NR 11 AND 12 WERE FOUND CRACKED INSIDE SLAT PANEL. REPAIRED PER MM 57-54-00.SDR DL72L951257Slat · crackedA .375 INCH CRACK EMANATING FROM I/B STOP PAD NR 7 SLAT. FOUND DURING C-1 LETTER CHECK, TPAMM 3-24-95. REPAIRED PER MM 57-54-0 PG 816.SDR DL72S951357Skin · crackedDURING THE INITIAL INSPECTION, THE NR 5 LEADING EDGE SLAT, THE AFT HOLE ON THE OUTER SKIN WHERE THE FENCE IS MOUNTED WAS FOUND TO HAVE A .5 INCH LONG CRACK BESIDE IT. THE SKIN WAS REPAIRED PER MM 57-54-0 FIG 813.SDR DL72S951322Angle · crackedDURING INITIAL INSPECTION, OF THE NR 5 LEADING EDGE SLAT, THE LOWER AFT ANGLE AT THE O/B END WAS FOUND TO HAVE A CRACK. THE CRACK WAS REPAIRED PER MM 57-54-0 FIG 805A.SDR DL72S951221Bullnose · crackedCRACK AT I/B BULLNOSE HINGE ATTACH POINT, NR 4 KRUGER FLAP. REPAIRED PER SRM 57-50-3 PG 32.SDR DL72K951306Skin · dentedDURING A SHOP INSPECTION, A DENT IN THE LEADING EDGE WAS FOUND TO BE BEYOND ALLOWABLE DAMAGE LIMITS. A REPAIR WAS INSTALLED PER SRM 57-50-3. RT WING NR 6 L/E SLAT.SDR DL72K951305Rib · crackedDURING A SHOP INSPECTION, TWO RIBS WERE FOUND TO BE CRACKED. ITEM NR 1 RIB NR 16 RIB CRACKED, A REPAIR WAS INSTALLED PER SRM 57-50-3. ITEM NR 2 RIB NR 17 CRACKED. A REPAIR WAS INSTALLED PER 57-50-3. RT WING NR 6 L/E SLAT.SDR DL72K951304Rib · crackedDURING SHOP INSPECTION, A RIB WAS FOUND TO BE CRACKED IN RT WING NR 6 L/E SLAT. REPAIRED PER MM 57-54-00.SDR DL72K951284Rib · crackedDURING SHOP INSPECTION, ITEM NR 1 AND NR 2 CRACKS WERE FOUND IN RIBS OF NR 6 SLAT. REPAIRS WERE INSTALLED PER MM 57-54-0.SDR 95ZZZW661Slot Door · puncturedDURING C-CHECK, FOUND LEFT INBOARD SLOT DOOR UPON SURFACE PUNCUTURED. REPAIRED PER DSRM 57-02-01 FIG 2A. TOTAL CYCLES 25,289.SDR UPS202691Chord · crackedWHILE IN "C" CHECK, MAINTENANCE FOUND NR 3 SLAT CHORD CRACKED AT TAI DUCT CUTOUT. MAINTENANCE REPAIRED IAW SRM 51-40-4.SDR UPS202689Rib · crackedWHILE IN "D" CHECK, MAINTENANCE FOUND NR 6 SLAT HAS CRACKED RIB AT SS 225 AT AFT CORNER WHERE LOWER CHORD ATTACHES TO RIB. MAINTENANCE REPAIRED IAW SRM 57-50-3 AND 51-30-2.SDR UPS202688Rib · crackedWHILE IN "D" CHECK, MAINTENANCE FOUND NR 4 SLAT HAS CRACKED RIB AT SS 112 LOWER AFT CORNER. MAINTENANCE REPAIRED IAW SRM 57-50-3.SDR UPS202687Slat · crackedWHILE IN "D" CHECK, MAINTENANCE FOUND NR 6 SLAT INBOARD END CRACKED. MAINTENANCE REPAIRED IAW SRM 51-30-2 AND 57-50-3.SDR DL72S951584Anti-Ice Duct · crackedWHILE IN SHOP 380, THE NR 4 KRUEGER FLAP ANTI-ICE DUCT TORQUE TUBE WAS FOUND WITH TWO CRACKS EXTENDING FROM AN EXISTING CUT OUT LOCATED 22.5 INCH FROM THE I/B EDGE OF THE FLAP. REPAIRED PER DL ERA 270445-14.SDR UPS202676Skin · crackedWHILE IN 'C' CHECK, MAINTENANCE FOUND CRACK ON LEADING EDGE SKIN OF NR 6 SLAT 20 INCHES DOWN AND 50 INCHES OUTBOARD OF INBOARD END AT A FASTENER. MX REMOVED DAMAGE AND REPAIRED PER SRM 57-50-1, 57-50-3 AND INSTALLED PER SRM 51-30-2.SDR DL72S951315Skin · crackedLOWER SKIN TO RIB ATTACH ANGLE CRACKED BETWEEN RIBS NR 7 AND NR 8. REPAIRED PER SRM 57-54-0. DURING SHOP INSPECTION, OF NR 7 L/E SLAT.SDR DL72S951314Rib · crackedA CRACK IN RIB NR 13. REPAIRED PER MM 57-54-0 PG 819.SDR DL72S951179Stiffener · crackedFOUND DURING A-1 LETTER CHECK - .50 INCH CRACK AT NR 6 SLAT STIFFENER AT COVE PANEL BELOW ANTI-ICE T-DUCT. REPAIRED PER M/M 57-54-0 PG 807A.SDR DL72S951303Rib · crackedA CRACK IN NR 10 RIB LOWER AFT CORNER. REPAIRED PER MM 57-54-0. ALSO, A CRACK IN NR 11 RIB LOWER FWD CORNER. REPAIRED PER MM 57-54-0. DAMAGE FOUND AT SHOP INSPECTION, OF NR 7 SLAT.
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