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 DL72K960488Rib · crackedFOUND ON MV1 CHECK, REFERENCE EO 04-05512-12 OPN 0304, WHILE BORESCOPING SLAT TRACK BOLT HOLES, FOUND .75 INCH CRACK IN L/E RIB NR 4 SLAT AT I/B TRACK I/B RIB. REPAIR: REPAIRED PER M/M 57-54-00, FIG 813A.SDR DL72S960446Angle · crackedFOUND DURING E-1 LETTER CHECK, NR 7 SLAT ANGLE CRACKED AT ANTI-ICE DUCT CUTOUT. REPAIRED PER MM 57-54-0.SDR DL72S960445Angle · crackedFOUND DURING E-1 LETTER CHECK, .1875 INCH CRACK IN COVE ANGLE NR 1 SLAT BELOW TAI DUCT. REPAIRED PER MM 57-54-0 PG 5A.SDR EISA96016Skin · crackedNR SLAT LOWER SKIN CRACKED OUTBOARD END. CUT OUT CRACKED AREA. FABRICATED FILLER AND DOUBLER PER SRM 51-50-03. INSTALLED FILLER AND DOUBLER PER SRM 51-40-02. (M)SDR DL72S960616Skin · damagedDURING INSPECTION, NR 8 L/E SLAT WAS FOUND WITH DAMAGE TO OUTBOARD CORNER OF SKIN, APPROX 10 INCHES. REPAIRED PER SRM 57-50-3, FIG 5.SDR DL72S960442Rib · crackedDURING INSPECTION, NR 3 L/E SLAT WAS FOUND WITH CRACKED RIB JUST O/B OF THE ACTUATOR ATTACH FITTING. REPAIRED PER MM 57-54-0.SDR DL72S960441Rib · crackedDURING INSPECTION, NR 3 L/E SLAT WAS FOUND WITH CRACKED RIB AT THE ANTI-ICE T-DUCT. REPAIRED PER MM 57-54-0.SDR CAL960191Rollers/Tracks · lack of lubeFLT NR 1708 - EWR - WHEN FLAPS WERE SELECTED BEYOND 5 DEGREES CREW RECEIVED T/E FLAP ASYMMETRY. THE SAFETY WIRES WERE BROKEN ON GPWS AND ALTERNATE FLAP MASTER SWITCH. THE LEFT INDICATOR WENT TO 10 DEGREES AND THE RIGHT STAYED AT 5 DEGREES. THE AIRCRAFT WAS SDR UPS205603Bonding Jumper · corrosionWHILE IN FOR C-CHECK, MAINTENANCE REPORTED NR 5 K-FLAP I/B UPPER LUG CORRODED AT BONDING JUMPER. REMOVED AND REPLACED NR 5 K-FLAP NRC 432723.SDR DL72S960429Angle · crackedNR 3 L/E SLAT COVE SKIN ANGLE CRACKED UNDER TAI DUCT. REPAIRED PER MM 57-54-0 PAR 5A.SDR DL72S960428Angle · crackedNR 2 L/E SLAT COVE SKIN ANGLE IS CRACKED UNDER TAI DUCT. REPAIRED PER MM 57-54-0 PAR 5A.SDR 96FDEA00326Bracket · crackedLEFT O/B SLAT DRIVE OUTER BRACKET CRACKED .187 LONG IN FILLET RADIUS OF FWD FLANGE.SDR DL72S960398Rib · crackedA .5 INCH CRACK PAST PREVIOUS STOP DRILL, LOWER O/B SIDE OF NR 4 SLAT NOSE RIB AT ACTUATOR ATTACH. A .375 INCH CRACK UPPER O/B SIDE OF NR 4 L/E SLAT NOSE RIB AT ACTUATOR ATTACH. REPAIRED PER MM 57-54-0.SDR DL72K960443Rib · crackedUPON ROUTINE INSPECTION, THE I/B ACTUATOR RIB WAS FOUND TO BE DAMAGED. REPAIR WAS ACCOMPLISHED PER THE 727 M/M 57-54-0 FIG 804, FOR NR 8 L/E SLAT.SDR UPS205582Attach Lug · corrodedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED LT WING NR 1 K-FLAP BULLNOSE I/B ROD ATTACH LUG IS CORRODED. REMOVED AND REPLACED NR 1 K-FLAP BULLNOSE IAW UPS OHM 57-51-01.SDR DL72S960552Rib · crackedDURING INSPECTION, NR 4 L/E SLAT INTERNAL SUPPORT RIB NR 5 AND NR 17 WERE FOUND CRACKED. REPAIRED PER MM 57-54-0.SDR DL72S960551Skin · crackedDURING INSPECTION, NR 4 L/E SLAT UPPER SKIN WAS FOUND CRACKED SEVERAL PLACES UNDER THE WING FENCE. REPAIRED SKIN PER MM 57-54-0.SDR DL72S960389Rib · crackedDURING INSPECTION, NR 4 L/E SLAT WAS FOUND WITH FOUR CRACKED/DAMAGED LEADING EDGE SUPPORT RIBS. REPAIRED PER MM 57-54-0.SDR DL72S960385Skin · crackedDURING INSPECTION, NR 4 L/E SLAT OUTER SKIN WAS FOUND CRACKED AT FENCE ATTACH MOUNT HOLE. REPAIRED SKIN PER MM 57-54-0 FIG 813.SDR USAA960265Skin · crackedPIT - PILOT REPORTED AFTER WALK AROUND THAT THERE WAS A 1 INCH CRACK IN THE LEFT WING LEADING EDGE NR 1 SLAT SKIN AT STATION XF-126 ABOVE TELESCOPING ANTI-ICE DUCT. REMOVED CRACK AND INSTALLED FILLER AND DOUBLER REPAIR PER SRM 57-02 FIG 6. AIRCRAFT RETURNED SDR DL757960365Te Wedge · delaminatedDURING INSPECTION, LEFT WING NR 2 SLAT T/E WEDGE WAS FOUND DELAMINATED. REPLACED WEDGE PER SRM 57-43-02 FIG 202.SDR CAL960315Skin · corrodedKUL - INSPECTION FOUND INNER SKIN OF NR 1 SLAT CORRODED AROUND TRACK FITTING NR 1 AND NR 2. THE SLAT SKIN WAS REPAIRED IAW SRM 57-10-00, FIGURE 31. (M)SDR UPS205561Upper Lug · corrodedWHILE IN FOR C-CHECK MAINTENANCE REPORTED, NR 5 K-FLAP O/B UPPER LUG CORRODED AT BONDING POINT. REMOVED AND REPLACED NR 5 K-FLAP IAW UPS MM 27-81-01.SDR 96FDEA00267Hinge · corrodedFIXED L/E FITTING PER NR 1 K-FLAP CENTER LUG IS CORRODED. REPAIRED CENTER HINGE FITTING WITH NEW.SDR DL757960449Skin · delaminatedDURING SHOP INSPECTION FOR NR 2 L/E SLAT, FOUND T/E WEDGE DELAMINATED. REPAIRED PER SRM 57-43-02.SDR DL72W960349Angle · crackedFOUND DURING F-1 LETTER CHECK, .375 INCH CRACK NR 2 L/E SLAT COVE SKIN ATTACH ANGLE BELOW TAI DUCT. REPAIRED PER MM 57-54-0.SDR DL72W960347Rib · crackedFOUND DURING F-1 LETTER CHECK, 2 INCH CRACK NR 8 L/E SLAT NOSE RIB AT I/B SIDE OF ACTUATOR ATTACH FITTING. REPAIRED PER M/M 57-54-00 PAR 9.SDR DL72K960345Skin · crackedDURING SHOP VISIT, INNER TAI SKIN CRACKED BETWEEN RIBS NR 11 AND NR 12 AT AFT RIVET TAIL. REPAIRED PER MM 57-54-0 FIG 803A, FOR NR 2 L/E SLAT.SDR UPS205542Bullnose · corrodedWHILE IN FOR C-CHECK MAINTENANCE REPORTED, L/W NR 2 K-FLAP BULLNOSE IS CORRODED AT O/B HINGE LOWER ATTACH POINT. REMOVED AND REPLACED BULLNOSE IAW MM 27-81-01 AND SRM 57-50-1.SDR DL72K960338Skin · crackedDURING SHOP INSPECTION, NR 8 L/E SLAT WAS FOUND WITH CRACKED TAI SKIN. REPAIRED SKIN PER MM 57-54-0 FIG 803.SDR DL72K960337Rib · crackedDURING SHOP INSPECTION, NR 8 L/E SLAT WAS FOUND WITH CRACKED RIB. REPAIRED PER MM 57-54-0.SDR DL757961605Skin · puncturedA .25 INCH HOLE WAS FOUND ON THE LOWER SKIN AND PARTIALLY INTO THE CORE ON THE NR 4 LEADING EDGE SLAT. THE HOLE IS LOCATED 3 FT OUTBOARD OF THE INBOARD EDGE OF THE SLAT. THE TRAILING EDGE WEDGE IS AN ALUMINUM/HONEYCOMB PANEL WITH THE ALUMINUM SKIN MADE FROM SDR DL757960761Te Wedge · delaminatedNR 3 SLAT T/E WEDGE DELAMINATED. REPLACED T/E WEDGE PER SRM 57-43-02.SDR DL72L960331Angle · crackedFOUND DURING B-1 LETTER CHECK - .50 INCH CRACK NR 2 L/E SLAT COVE SKIN ATTATCH ANGLE BELOW I/B UPSTOP PAD. REPAIRED PER M/M 57-54-0.SDR DL757960353Te Wedge · delaminatedDURING INSPECTION, NR 3 L/E SLAT T/E WEDGE WAS FOUND DELAMINATED. REPLACED WEDGE PER SRM 57-43-02.SDR DL72S960352Te Wedge · dentedNR 5 L/E SLAT T/E WEDGE UPPER SURFACE DENTED. REPLACED WEDGE PER SRM 57-43-02.SDR DL72W960306Angle · crackedSLAT ANGLE CRACKED UNDER NR 7 SLAT I/B STOP PAD AREA. FOUND DURING LETTER CHECK, NR 7 L/E SLAT. INSTALLED REPAIR PER MM 57-54-0.SDR 96FDEA00233Bonding Strap · corrosionCORROSION (097-562-01-2) NR 4 RT FLAP BULLNOSE OB BONDING JUMPER UPPER ATTACH POINT AND TOOLING MARKS BS 950A, STR 7 RT AFT SIDE OF FRAME. *S/D* REMOVED CORROSION PER FEDEX SRM 57-50-3 AND 27-57-010.SDR AALA960283Track · wornAFW - NR 1 AND NR 12 SLAT TRACKS FOUND WORN BEYOND MM LIMITS. NR 1 WORN TO .011 INCH AND NR 12 WORN TO .014 INCH. BLENDED WORN AREAS. EDDY CURRENT CHECKED. NO CRACKS FOUND. ROTO-PEENED, PRIMED, AND LUBED. APPROVED BY ENGINEERING PER MRB 767-1147. TRACKSSDR AALA960282Track · wornAFW - FOUND NR 11 SLAT TRACKS WORN BEYOND MM LIMITS. INBOARD TRACK WORN TO .011 INCH. OUTBOARD TRACK WORN TO .013 INCH. BLENDED WORN AREAS. EDDY CURRENT CHECKED. NO CRACKS FOUND. ROTO-PEENED, PRIMED, AND COATED WITH AEROSHELL 7. APPROVED BY ENGINEERING SDR UPS96805684Skin · corrodedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED RT I/B SLAT UPPER SURFACE PITTED AND MODERATE CORROSION. REPLACED SLAT PANEL PER SRM 51-3-0.SDR DL72W960270Angle · crackedFOUND ON C-2 LETTER CHECK, COVE SKIN SUPPORT ANGLE CRACKED .0625 INCH BELOW NR 7 SLAT ANTI-ICE DUCT. REPAIRED PER MM 57-54-0.SDR DL72S960266Slat · damagedON CREW WALK-AROUND, NR 2 LEADING EDGE SLAT DAMAGE. ANTI-ICE TELESCOPING DUCT DAMAGED SLAT AND WING. REPLACED SLAT, FERRIED TO ATL FOR FURTHER MAINTENANCE.SDR DL72S960264Panel · wornHMV, LEADING EDGE O/B END WORN, NR 4 TRAILING EDGE FLAP. REPLACED WORN SEAL ON TRAILING EDGE PANEL, CUT OUT DAMAGE AND REPAIRED PER M/M 57-52-0 FIG 803.SDR 96FDEA00162Hinge Fitting · corrodedFIXED L/E FITTING FOR NR 1 K-FLAP CENTER LUG IS CORRODED. REPLACED CENTER HINGE FITTING WITH NEW.SDR DL72S960249Angle · crackedFOUND DURING C-1 LETTER CHECK, .5 INCH CRACK NR 7 L/E SLAT LWR COVE SKIN ATTACH ANGLE BELOW I/B TRACK. REPAIRED PER M/M 57-54-0.SDR DL72S960248Bracket · crackedFOUND DURING C-1 LETTER CHECK, .375 INCH CRACK NR 2 L/E FLAP ACTUATOR ATTACH BRACKET AT I/B LWR END. REPAIRED PER M/M 57-20-21 PAR 12.SDR DL72S960247Bracket · crackedFOUND DURING C-1 LETTER CHECK, .5 INCH CRACK NR 1 L/E FLAP ACTUATOR ATTACH BRACKET I/B LWR SIDE. REPAIRED PER M/M 57-20-21 PAR 12.SDR DL72K960245Rib · crackedUPON INSPECTION FOR NR 1 LEADING EDGE SLAT, RIB NR 15 WAS FOUND CRACKED. REPAIRED PER MM 57-54-0.SDR 96FDEA00157Rib · corrodedCORROSION ON NR 6 K-FLAP MOST OUTBOARD RIB WHERE LANDING LIGHT CONDUIT ATTACHES TO RIB UPPER BOLT HOLE. REMOVED CORROSION, REPAIRED PER EWO NR 96-2025.
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