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 CALA0200115Skin · crackedINSPECTION FOUND A 4" CRACK IN #4 L/E SLAT PANEL AT O/B ACTUATOR. REPAIRED IAW SRM 57-43-01.SDR COOSDR02003Skin · crackedRIGHT WING, OUTBOARD FORE FLAP PN 6521631144, SN BN78 LOWER SKIN CRACKED.SDR COOSDR02004Skin · delaminatedLEFT WING, OUTBOARD FOR FLAP PN 6521631261, SN PN 418, LOWER AND UPPER SKIN DELAMINATED.SDR AALA20020263Skin · dentedAFW - FOUND DENT AT NR 6 SLAT TOP TRAILING EDGE JUST INBOARD OF OUTBOARD SLAT TRACK. CORRECTED PER MRB 777-030. (M)SDR TSAA0257052Hinge Fitting · damagedREMOVED DAMAGED KRUEGER FLAP PER MM 57-56-42 DUE TO ELONGATED HINGE FITTING HOLES. REMOVED AND REPLACED KRUEGER FLAP WITH A LOWER PART NR IAW ECO 3273. AIRCRAFT RETURNED TO SERVICE. (M)SDR UPS02237822Rib · crackedINSPECTION TYPE:C LT WING, NR 3 SLAT, CRACK IN O/B RIB AT O/B TRACK, FWD TRACK ATTACH AREA. CRACK STOP DRILLED IAW SRM 51-10-1, REPAIR CARRIED OUT IAW SRM 57-50-3.SDR 02FDEA00140Slat · crackedNR 1 SLAT RT WING CRACKED AT LIGHTNING HOLE AT I/B END AT XFS 145. REMOVED AND REPLACED DOUBLER PER SRM 57-00-01 VOL 1 FIG 4.SDR DL72S020216Spar · crackedFOUND ON A2 LETTER CHECK, NR 7 SLAT FWD SPAR AND RIB CRACKED AT ACTUATOR ROD END. REPAIRED PER MM 57-54-000-8.SDR SWAA020332Slat · debondedDURING SCHEDULED D-CHECK, FOUND NR 3 L/E SLAT DISBONDED ON UPPER SURFACE AT THE T/E WEDGE ON INBOARD END AND OUTBOARD END. REPAIRED NR 3 L/E SLAT PER SRM.SDR SWAA020331Slat · debondedDURING SCHEDULED D-CHECK, FOUND NR 2 L/E SLAT DISBONDED ON UPPER SURFACE OUTBOARD END OF T/E WEDGE. REMOVED AND REPLACED NR 2 L/E SLAT PER MM.SDR USAA020093Skin · crackedPIT - FOUND NR 1 SLAT LOWER LEADING EDGE SKIN CRACKED 3.250 INCHES WIDE BY 17 INCH LONG DOUBLER, STA WBL 557-540 LOWER 4E SKIN AT RIVET LINE. DOUBLER PREVIOUSLY INSTALLED PER SRM 57-43-01 FIG 206. (M)SDR USAA020094Skin · crackedPIT - FOUND NR 2 SLAT LOWER LEADING EDGE SKIN CRACKED 4 INCHES WIDE BY 28 INCHES LONG, STATION WBL 453 SLAT ACT ROD END. DOUBLER PREVIOUSLY INSTALLED PER SRM 57-43-01 FIG 206. (M)SDR USAA020095Skin · crackedPIT - FOUND NR 4 SLAT LOWER LEADING EDGE SKIN CRACKED 4 INCHES WIDE BY 54.5 INCH LONG DOUBLER, BETWEEN STATION WBL 254-304 LOWER L/E RIVET LINE. DOUBLER PREVIOUSLY INSTALLED PER SRM 57-43-01 FIG 206. (M)SDR USAA020096Skin · crackedPIT - FOUND NR 5 SLAT LOWER LEADING EDGE SKIN CRACKED 4 INCHES WIDE BY 30.5 INCH LONG DOUBLER, NR 5 SLAT LOWER RIVET LINE STATION WBL 355-453. DOUBLER PREVIOUSLY INSTALLED PER SRM 57-43-01 FIG 206. (M)SDR USAA020097Skin · crackedPIT - FOUND NR 6 SLAT LOWER LEADING EDGE SKIN CRACKED 4 INCHES WIDE BY 17.5 INCH LONG DOUBLER, STATION WBL 531 NR 6 SLAT LOWER 4E SKIN AT RIVET LINE. DOUBLER PREVIOUSLY INSTALLED PER SRM 57-43-01 FIG 206. (M)SDR MWEA020066Horn · corrodedRIGHT SLAT HORN HAS SPOTS OF CORROSION BY FASTENERS (INBOARD). FABRICATED AND INSTALLED DOUBLER.SDR MWEA020065Horn · corrodedLEFT INBOARD SLAT HORN HAS CORROSION AROUND SEVERAL FASTENER HOLES THAT ATTACH THE INBOARD GAP SEAL. FABRICATED AND INSTALLED DOUBLER AND FILLER.SDR MWEA020064Horn · corrodedLEFT INBOARD SLAT HORN HAS SPOT OF CORROSION BY A FASTENER. FABRICATED AND INSTALLED DOUBLER.SDR CA020215007Arm · dislodged(CAN) MAINTENANCE FOUND NR 2 SLAT FOUND PROTRUDING 4 INCHES ON ONE SIDE ON WALKAROUND CHECK. SLAT MECHANISM FOUND OFF GUIDE TRACK. FLIGHT PERMIT (SPECIFIC PURPOSE, FERRY FLIGHT) ISSUED AND AIRCRAFT FLOWN TO BASE FOR REPAIRS. NR 2 LEADING EDGE SLAT DETENT ARM SDR CALA0200033Skin · crackedINSPECTION FOUND A 1/2" CRACK IN R/H WING #4 SLAT SKIN LOWER AREA, BELOW ACTUATOR ATTACHMENT TO SLAT. THE CRACKED AREA WAS CUTOUT. REPAIR FILLER AND A SPLICE PLATE WERE INSTALLED IAW SRM 57-43-01, FIGURE 206.SDR G60A061Skin · damagedFATIGUE DAMAGE TO THE INNER SKIN OF THE NR 1 SLAT ON THE LEFT WING. MISSING MATERIAL HOLE SIZE IS APPROXIMATELY 8 INCHES BY 11 INCHES WITH ONE AREA EXCEEDING THIS DIMENSION BY AN ADDITIONAL 2.5 INCHES BY 4 INCHES. THERE ARE 4 OBVIOUS FATIGUE CRACKS IN THE ARSDR SWAA020072Slat · delaminatedDURING SCHEDULED C4 CHECK, FOUND NR 1 L/E SLAT DELAMINATED APPROX 2 INCH SQUARE ON TOP OTBD T/E. REPAIRED L/E SLAT PER SRM.SDR ASAA0210009Skin · wornPAE - DURING SCHEDULED C-CHECK, FOUND SKIN PANEL AT WING STATION 447-474 ON NR 5 SLAT WORN. REPAIRED PER EA. (M)SDR TSAA0257032Structure · crackedREPAIRED CRACK AT NR 5 SLAT STATION 195.53. REPAIR CONSISTS OF BLENDING OUT THE DAMAGED AREA, MAINTAINING A BLEND OUT LENGTH OF .075 INCH MAXIMUM AND USING A MINIMUM RADIUS OF .050 INCH. REMOVED ALL BURRS AND SHARP EDGES IAW SRM 57-20-1 PAGE 1 FIGURE 1. AIRSDR TSAA0257033Structure · crackedREPAIRED CRACK AT NR 4 SLAT STATION 35.84. REPAIR CONSISTS OF BLENDING OUT THE DAMAGED AREA, MAINTAINING A BLEND OUT LENGTH OF .075 INCH MAXIMUM AND USING A MINIMUM RADIUS OF .50 INCH. REMOVED ALL BURRS AND SHARP EDGES IAW SRM 57-20-1 PAGE 2 DETAIL II. AIRCSDR TSAA0257039Structure · crackedREPAIRED CRACK AT NR 4 SLAT STATION 35.84. REPAIR CONSISTS OF BLENDING OUT THE DAMAGED AREA, MAINTAINING A BLEND OUT LENGTH OF .075 INCH MAXIMUM AND USING A MINIMUM RADIUS OF .50 INCH. REMOVED ALL BURRS AND SHARP EDGES IAW SRM 57-20-1 PAGE 1 FIGURE 1. AIRCRSDR TSAA0257031Slat · crackedREPAIRED CRACK AT NR 6 SLAT STATION 370.56. BLENDED OUT THE DAMAGED AREA IAW SRM 57-20-1, FIG 1, PAGE 1. AIRCRAFT RETURNED TO SERVICE. (M)SDR IXXA0200006SWing · crackedDURING ROUTINE C-CHECK INSPECTION A CRACK WAS DETECTED ON THE RIGHT WING CENTER LEADING EDGE FORWARD SIDE AT STATION WS485. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IN ACCORDANCE WITH DOUGLAS STRUCTURAL REPAIR MANUAL AND ENGINEERING ORDER EDSDR 2002F00116Wedge · damagedFOUND RIGHT WING OUTBOARD FORWARD FLAP TRAILING EDGE WEDGE COMPOSITE HAS DELAMINATION AND APPROXIMATELY 75 PERCENT OF THE SECTION OF WEDGE IS MISSING. (M)SDR SWAA020009Slat · crackedDURING SCHEDULED C4 CHECK, FOUND NR 5 L/E SLAT WEDGE LOWER SKIN CRACKED AT OUTBOARD END. REMOVED AND REPLACED NR 5 L/E SLAT PERMM.SDR SWAA013440Slat · crackedDURING SCHEDULED C3 CHECK, FOUND NR 4 L/E SLAT CRACKED (2 EA) ON LOWER T/E RIVET ROW ADJACENT TO OTBD AUX TRACK. REPAIRED SLAT PER SRM.SDR 01FDEA01110Rib · crackedN 241 #7 SLAT OUTBD RIB CRACKED. R&R RIB PER SRM 57-50-3.SDR 01FDEA01109Rib · crackedNR 3 SLAT INBD RIB CRACKED. R&R RIB PER SRM 57-50-3.SDR GTIA012319Rib · crackedFTW - FOUND RIGHT WING NR 4 SLAT 8TH INNER RIB FROM OUTBOARD END OF SLAT IS CRACKED. REMOVED RIB. FABRICATED NEW RIB. INSTALLED NEW RIB IAW DC9 SRM 51-30-2. (M)SDR CALA0101034Skin · crackedINSPECTION FOUND A 1/4" CRACK IN R/H WING #6 SLAT PANEL SKIN. REPAIRED IAW SRM 57-43-01.SDR 01FDEA01081Rib · crackedRIB CRACKED ON NR 6 L/E SLAT WS 520 AT WBL 415. REPAIRED RIB IAW FEDEX SRM 57-50-3.SDR 01FDEA01080Rib · crackedRIB CRACKED ON NR 6 L/E SLAT WS 491 AT WBL 398. REPAIRED RIB IAW FEDEX SRM 57-50-03.SDR 01FDEA01079Rib · crackedRIB CRACKED ON NR 7 L/E SLAT WS 601 AT WBL 492. REPAIRED RIB IAW FEDEX SRM 57-50-3.SDR DL764011953Bolt · missingON LANDING GEAR ROLL WITH FLAPS AT 30 DEGREES, LEADING EDGE SLAT ASYMMETRY EICAS MESSAGE ILLUMINATED. FOUND NR 4 SLAT OUTBOARD AUXILIARY TRACK BOLT MISSING. ALSO MISSING ARE BEARING, WASHER ASSY (TARGET), NUT AND COTTER PIN. FOUND NR 4 LEADING EDGE PROX TARSDR 2002F00174Slat · delaminatedFOUND LEFT WING NUMBER TWO SLAT IS DELAMINATED IN SEVERAL AREAS. (M)SDR SWAA013315Slat · damagedON WALKAROUND, FOUND DAMAGE TO TOP SIDE OF NR 5 L/E SLAT AND SKIN UNDER NR 5 SLAT PEELED BACK. REMOVED AND REPLACED L/E SLAT AND REPAIRED L/E SKIN PER SRM.SDR SWAA013263Angle · crackedDURING SCHEDULED A1 CHECK, FOUND NR 3 L/E SLAT T-ANGLE CRACKED AT ACTUATOR ATTACH AREA. REMOVED AND REPLACED SLAT ASSY.SDR GTIA012182Angle · chafedNR 4 SLAT RIGHT CHORD ANGLE CHAFFED MORE THAN 50 PERCENT THICKNESS OF MATERIAL. REMOVED CHAFFED ANGLE. FABRICATED NEW CHORD ANGLE. INSTALLED NEW CHORD ANGLE IAW DC9 SRM 51-30-2. (M)SDR GTIA012176Angle · chafedFTW - FOUND NR 3 RIGHT SLAT OUTBOARD LOWER CHORD ANGLE CHAFFED MORE THAN 50 PERCENT OF MATERIAL THICKNESS. FORMED NEW CHORD ANGLE. INSTALLED FASTENERS IAW DC9 SRM 51-30-2. (M)SDR F3LA200100130Rivet · looseDURING C-7 CHECK, INSPECTION REPORTED RT WING NR 6 L/E SLAT HAD PULLED AND WORKING RIVETS ON INSIDE L/E OTBD OF ACTUATOR AND INBD OF OTBD MAIN TRACK. REPLACED FASTENERS PER SRM 51-30-02.SDR F3LA200100127Rivet · looseDURING C-7 CHECK, INSPECTION REPORTED RT WING NR 5 SLAT HAD WORKING RIVETS ON LOWER T/E SKIN AROUND ACTUATOR AND INBD OF TRACKS. REPLACED RIVETS PER SRM 51-30-02.SDR F3LA200100128Rivet · looseDURING C-7 CHECK, INSPECTION REPORTED RT WING NR 4 SLAT LOWER INNER SKIN RIVETS LOOSE FROM INSIDE STRUCTURE BETWEEN ACTUATOR AND OTBD OF TRACKS. REPLACED LOOSE FASTENERS PER SRM 51-30-2.SDR F3LA200100129Rivet · looseDURING C-7 CHECK, INSPECTION REPORTED RT WING NR 6 SLAT HAD PULLED AND WORKING RIVETS ON LOWER SKIN T/E AROUND ACTUATOR. REPLACED FASTENERS PER SRM 51-30-02.SDR F3LA200100131Rivet · looseDURING C-7 CHECK, INSPECTION REPORTED RT WING NR 5 SLAT HAD WORKING RIVETS ON INNER SKIN NEXT TO ACTUATOR CUTOUT. REPLACED FASTENERS PER SRM 51-30-2.SDR SWAA013171Slat · delaminatedDURING SCHEDULED C2 CHECK, FOUND NR 4 L/E SLAT TRAILING WEDGE DELAMINATED AT INBD END. REMOVED AND REPLACED NR 4 L/E SLAT PER MM.
Back to JASC 5754