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 SWAA970837Seals · jammedAFTER TAKEOFF, EXPERIENCED L/E FLAP AND NR 4 SLAT YELLOW TRANSIT LIGHTS REMAINING ILLUMINATED. AIRCRAFT RETURNED TO PHX AND MADE AN UNEVENTFUL LANDING. REMOVED JAMMED AUX TRACK SLAT SEALS. INSTALLED NEW PER BOEING M/M.SDR UPS97224365Skin · corrodedINSPECTION TYPE-C, NR 4 K-FLAP O/B BONDING JUMPER HOLE HAS CORROSION AROUND OLD BONDING JUMPER LOCATION. CORROSION REWORK OUT OF LIMITS IAW UPS EO B727-5740-3980 (SRM ADDENDOM) REPAIRED NR 4 K-FLAP AT OLD BONDING JUMPER LOCATION IAW SRM 57-50-3.SDR UPS97224366Rib · crackedINSPECTION TYPE-C, NR 5 K-FLAP I/B LOWER BONDING JUMPER ON K-FLAP HAS CRACK EMANATING FROM HOLE. CUT OUT DAMAGE FABRICATED AND INSTALLED REPAIR PARTS ON NR 5 K-FLAP I/B RIB AT BONDING JUMPER PER SRM 57-50-3.SDR UPS97224480Ribs · crackedINSPECTION TYPE-C, NR 1 L/E SLAT ROD END CRACKED. ROD END AND RIBS REPLACED PER OHM 20-50-03 AND MM 27-81-32.SDR DL72S971702Angle · crackedFOUND DURING B-1 LETTER CHECK, .25 IN CRACK NR 8 SLAT COVE SKIN ATTACH ANGLE BELOW O/B STOP PAD. REPAIRED PER M/M 57-54-0.SDR DL72S971700Stiffener · crackedFOUND DURING B-1 LETTER CHECK, INBD VERTICAL STIFFENER CRACKED NR 6 SLAT O/B TRACK BOX. REPAIRED PER M/M 57-20-21.SDR 97FDEA00627Rib · crackedLT WING NR 2 SLAT INBOARD RIB FLANGE CRACKED. REPAIRED CRACKED FLANGE AS PER EA 8-5740-34907.SDR 97FDEA00587Rib · crackedLT WING NR 2 SLAT INBOARD RIB FLANGE CRACKED. REPAIRED CRACKED FLANGE AS PER EA 8-5740-34907.SDR DHL9772711CBracket · crackedAT C-CHECK, NR 6 SLAT I/B UP STOP HAS BOTH LT AND RT SUPPORT BRACKETS CRACKED. REMOVED AND REPLACED SUPPORT BRACKETS AND STOPS PER SRM 51-10-1. ADJUSTED STOPS, BRACKETS 3 BY 5.SDR DHL9772703CSkin · crackedAT C-CHECK, NR 7 SLAT UPPER SKIN AT L/E IS DENTED AND TWO CRACKS RADIATING FROM RIVET HOLES. PERFORMED HFEC, ONE CRACK ONLY. STOP DRILLED CRACK, HFEC, INSTALLED REPAIR PER SRM 57-50-3, 4 BY 4.SDR DHL9772702CSkin · damagedAT C-CHECK, NR 5 SLAT PREVIOUS REPAIR ON LOWER SKIN IS NOT WITHIN SRM LIMITS. INSTALLED REPAIR PER SRM 57-50-3, 4 BY 6.SDR CALA9701374Skin · puncturedINSPECTION FOUND A .25 INCH DIAMETER HOLE IN SKIN AT UPPER LEADING EDGE OF NR 7 SLAT. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 57-50-3.SDR P5CA9701437Panel · damagedON PREFLIGHT, FOUND DAMAGE TO NR 16 LEADING EDGE FLAP OUTER PANEL. REPLACED OUTER PANEL PER BOEING M/M 27-81-01 OPERATIONAL AND RIG CHECK GOOD.SDR HALA9700163Fitting · crackedSBA - IN C-CHECK, RIGHT NR 5 SLAT OUTBOARD END FITTING HAS 3 CRACKS AT SEAL ATTACH HOLES. REMOVED AND REPLACED FITTING PER SRM 51-30-8 AND 51-30-2. (M)SDR DL72S971948Rib · crackedRIB CRACKED INBD END NR 5 L/E SLAT. REPAIRED PER M/M 57-54-0 FIG 814.SDR DL72S971695Rib · crackedTWO RIBS CRACKED IN NR 6 L/E SLAT. REPAIRED PER M/M 57-54-0 PG 807.SDR DL757971592Wedge · delaminatedTRAILING EDGE WEDGE DELAMINATED. REPLACED WEDGE PER SRM 57-43-02.SDR GTIA9700364Fixed Vanes · out of adjustDTW - FLT 640 - AS FLAPS ARE PROGRESSIVELY EXTENDED, MORE AND MORE AILERON TRIM IS REQUIRED TO BE SELECTED TO MAINTAIN NEUTRAL TRIM. AT 40 PERCENT OF FLAPS, 5 UNITS OF RIGHT WING DOWN TRIM IS REQUIRED. FLAP POSITION ACCORDING TO THE GAUGE APPEARS TO BE THE SSDR IH971355012Slat · dentedLEFT AND RIGHT WING NR 1 SLAT LEADING EDGE DENTED IN SEVERAL PLACES. DAMAGE WAS REPORTED TO BOTH THE LEFT AND RIGHT WING NR 1 LEADING EDGE SLATS. AMOUNT AND SPACING OF THE DENTS EXCEEDED THE DC-9 SRM 57-03 FIGURE 14A ALLOWABLE LIMITS. THE DAMAGE WAS REMOVEDSDR DL76S971560Skin · delaminatedTHE NR 6 SLAT TRAILING EDGE WEDGE UPPER SURFACE WAS FOUND DELAMINATED. THE DELAMINATION IS LOCATED 10 FROM THE AFT EDGE EDGE, 82 FROM THE INBOARD END AND IS APPROX 3 IN DIAMETER. THE DELAMINATED AREA WAS REPAIRED PER B767 SRM, CHAPT 51-70-10, FIGURE 9.SDR DL757971596Wedge · delaminatedNUMBER 1, 6, 7 AND 9 SLAT WEDGE DELAMINATED. REPLACED ALL FOUR SLATS.SDR DL767971526Skin · delaminatedTWO AREAS OF DELAMINATION WERE FOUND ON THE UPPER SKIN OF THE NR 11 SLAT T/E WEDGE. ONE AREA OF DELAMINATION WAS FOUND ON THE UPPER SKIN OF THE NR 12 SLAT T/E WEDGE. NO CORE DAMAGE OCCURRED ON ANY OF THE DAMAGE. THE DAMAGE WAS REPAIRED PER B767-200 SRM 57-4SDR SWAA970636Slat · delaminatedFOUND NR 5 L/E SLAT DELAMINATED. REPLACED NR 5 L/E SLAT PER BOEING M/M.SDR AALA971305Angle · crackedTUL - NR 5 LEADING EDGE INBOARD ATTACH ANGLE CRACKED LOWER LEG. INSTALLED NEW ACTUATOR MOUNT INBOARD NR 5 SLAT. TST: 43,979 HOURS. CYCLES, 23,050. (X)SDR P5CA9701295Bull Nose · missingON POST FLIGHT, FOUND NR 6 LEADING EDGE FLAP BULL NOSE MISSING. AIRCRAFT DISPATCHED PER CDL 27-81-3. BULL NOSE TO BE REPLACED.SDR MWEA97653Skin · crackedDURING B-CHK, RT WING NR 4 SLAT CRACKED. MAINT REPAIRED IAW SRM 57-01 FIG 3 SHT 2.SDR MWEA97649Cover · crackedDURING C-CHK, FOUND CRACK BETWEEN 4 AND 5 OTBD RT WING SLAT TRACK COVER. MAINT REPAIRED IAW SRM 51-10-2A AND 57-01.SDR P5CA9701285Skin · dentedDENT ON RIGHT WING LEADING EDGE FLAP PANEL 16. REPAIRED PER BAC SRM 51-30-02.SDR MWEA97615Skin · dentedDURING D-CHECK, FOUND A DENT WITH HEAVY SCRATCHES ON THE LEADING EDGE RT NR 4 SLAT. MTC REPAIRED IAW SRM 57-09 FIG 10 PG 31 AND 51-30.SDR DL767971332Slat · delaminatedTHE NR 9 LEADING EDGE SLAT TRAILING EDGE WEDGE WAS FOUND TO HAVE A 4 INCH INBOARD/OUTBOARD X 2 FWD/AFT SECTION OF THE UPPER SKIN DELAMINATED. THE DAMAGE IS LOCATED INBOARD OF THE END OF THE SLAT WEDGE. THIS AREA WAS REPAIRED PER B767 SRM 57-43-02, FIGURE 201SDR DL72S971421Skin · wornNR 4 L/E SLAT INNER SKIN WORN AND GOUGED I/B OF ACTUATOR. REPAIRED PER B-727 M/M57-54-0, FIG 801.SDR DL76G971343Skin · delaminationTHE NR 2 LE SLAT TRAILING EDGE WEDGE WAS FOUND WITH UPPER SKIN DELAMINATION. THE SLAT HAS A DELAMINATION AREA OF 4 X 2 LOCATED ON THE I/B EDGE OF THE PART, APPROX 6 FORWARD OF THE AFT EDGE OF THE PART. THE DELAMINATION WAS REPAIRED PER B767-300 SRM 57-43-02,SDR DL72S971395Stop Pad · crackedDOUBLER CRACKED AT LWR COVER SKIN ANGLE AT NR 7 SLAT I/B STOP PAD. REPAIRED PER DELTA ER/A 362251-14.SDR DL72S971311Skin · crackedA .25 INCH VISIBLE CRACK AT NR 2 SLAT COVE SKIN ANGLE AT I/B UPSTOP PAD. REPAIRED PER MM 57-54-0.SDR DL76S971347Skin · delaminatedTHE NR 9 LE SLAT TRAILING EDGE WEDGE WAS FOUND TO HAVE A 3.5 DIAMETER SECTION OF THE UPPER SKIN DELAMINATED. THE DAMAGE IS LOCATED IN THE CENTER OF THE SLAT WEDGE FWD/ AFT AND INB'D/OUTB'D. THE DAMAGED SECTION WAS REPAIRED PER B767 SRM 57-43-02, FIGURE 201.SDR CALA9701091Skin · crackedINSPECTION FOUND A 1 INCH CRACK BETWEEN TWO RIVETS IN LT WING NR 1 SLAT SKIN NEAR ACTUATOR. A DOUBLER WAS INSTALLED IAW BOEING DRAWING NR 65C30133.SDR CALA9700988Skin · dentedINSPECTION FOUND NR 5 SLAT SKIN DENTED BETWEEN NR 9 AND 10 RIB FROM INBOARD END. THE SKIN WAS REPAIRED IAW SRM 57-50-3.SDR DL757971346Skin · dentedA SPARE NR 3 SLAT WAS DAMAGED UPON REMOVAL FROM A SHIPPING CRATE AND PRIOR TO INSTALLATION ON A/C 637. THE INB'D AFT CORNER OF THE TE WEDGE WAS DENTED. THE SLAT WAS REPAIRED PER B757 SRM 51-70-10.SDR MWEA97569Slat · dentedDURING D-CHECK, FOUND 2 DENTS ON RT NR 3 SLAT APPROX 1.5 FROM OUTBOARD END AND 1 AT MIDPOINT OF SLAT. MTC REPAIRED IAW SRM 57-09 FIGURE 10 PAGE 31.SDR MWEA97568Skin · dentedDURING D-CHECK, FOUND DENT ON LEFT NR 5 SLAT LEADING EDGE. MTC REPAIRED IAW SRM 57-03 FIG 14A.SDR AALA971125Angle · corrodedTUL - NR 5 SLAT ACTUATOR INBOARD AND OUTBOARD ATTACH ANGLES CORRODED. REMOVED AND REPLACED BOTH ANGLES. TST: 55,431 HOURS. CYCLES: 34,330. (X)SDR DL767971445Te Wedge · delaminatedTHE NR 5 SLAT TRAILING EDGE WEDGE UPPER SURFACE WAS FOUND DELAMINATED ON THE AFT INBOARD CORNER. THE DELAMINATION IS APPROX 3 BY 3.5. THIS AREA WAS REPAIRED PER B767-200 SRM 51-70-10, FIGURE 9.SDR DL757971192Wedge · delaminatedTHE NR 9 LEADING EDGE SLAT WEDGE WAS DELAMINATED. REPLACED SLAT.SDR SWAA970558Skin · crackedDURING SCHEDULED BC2 CHECK, FOUND LT WING NR 3 SLAT, LOWER T/E SKIN CRACKED. REPAIRED PER SWA RA 1-A57-0377.SDR MZZA97183Rib · crackedGUM - DURING QC INSPECTION OF AIRCRAFT, FOUND NR 4 LEADING EDGE SLAT ACTUATOR ROD END ATTACHMENT, INBOARD RIB FLANGE CRACKED APPROXIMATELY .5 INCH AT FWD FLANGE LOWR SECTION. MAINTENANCE REMOVED AND REPLACED NR 4 LEADING EDGE SLAT ASSY AS PER MM 27-81-32. ADSDR DL72S971244Skin · damagedLEADING EDGE SLAT DENTED 48 INBOARD OF OUTBOARD END. ALSO, 3, 4, 10 RIBS CRACKED. REPAIRED PER SRM 57-54-0.SDR DL72S971237Skin · crackedAT HMV, A CRACK WAS FOUND AT NR 3 SLAT AT RIB 4. THIS WAS REPAIRED PER MM 57-54-0 PG 801.SDR DL72S971167Rib · crackedFOUND ON A1 LETTER CK, .75 IN CRACK IN RADIUS OF NR 6 SLAT RIBS I/B AND O/B SIDES OF ACTUATOR AT COVE SKIN ATTACH. REPAIRED PER MM 57-54-0.SDR ABXA9701380Slat · corrodedWHILE COMPLYING WITH 'D' INSPECTION, FOUND THE NR 1 LEFT SLAT CORRODED AT CENTER ATTACH FITTING. REPLACED NR 1 LEFT SLAT IAW DC-9 MAINTENANCE MANUAL, CHAPTER 27-80-1.SDR MWEA97494Fittings · corrodedDURING D-CK, NR 1 SLAT INBD/CNTR/OUTBD ATTACH FITTING INSIDE HOLES CORRODED. MAINT REPAIRED IAW DAC TELEX MISC3906/PDG, SRM 57-09, 51-30-0.
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