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 DL767981469Wedge · delaminatedDELAMINATION WAS FOUND ON THE NR 1 SLAT T/E WEDGE. DELAM AREA IS APPROX 4 IN DIAMETER. REPAIRED PER ERA 365245-14AD.SDR P2EA98129Slat · dentedSJO - LEFT WING NR 1 SLAT LEADING EDGE DENTED AT SS 373. REPAIRED NR 1 SLAT SKIN SECTION BETWEEN SS 373 AND SS 382 PER SRM 57-50-3 FIG 1. (M)SDR UPS98227223Skin · crackedINSPECTION TYPE:C SUSPECT CRACK ON NR 5 KREUGER FLAP OUTER SURFACE AT BULLNOSE MID HINGE CUTOUT. KREUGER FLAP REPLACED IAW MM 27-81-01.SDR DHL9872124DHeat Shield · crackedAT D-CHECK, NR 5 L/E FLAP HEAT SHIELD AT 4TH BAY FROM I/B SIDE IS CRACKED. REPLACED HEAT SHIELD PER SRM 51-30-2, 11 X 8. N/R 2466.SDR DHL9872123DHeat Shield · damagedAT D-CHECK, RT WING FIXED L/E INTERIOR HEAT SHIELD IS DAMAGED ABOVE THE NR 5 L/E FWD FLAP ACTUATOR FITTING. CUT OUT DAMAGED AREA, INSTALLED DOUBLER REPAIR PER SRM 57-30-4, 4 X 5'. N/R 2472.SDR DHL9872122DHeat Shield · crackedAT D-CHECK, 35 L/E FLAP HEAT SHIELD AT THE 3 RD BAY FROM I/B SIDE IS CRACKED AND LOOSE AT LOWER ATTACH RIVETS. REMOVED AND REPLACED PER SRM 51-30-2, 11 X 8. N/R 2467.SDR DHL9872164DSkin · crackedAT D-CHECK, NR 6 LE SLAT ABOVE ANTI-ICE DUCT ANGLE CRACKED I/B END. STOP DRILL, HFEC, FABRICATED DOUBLER PER SRM 57-50-3, 7 X 6. N/R 2423.SDR UPS98227227Angle · crackedINSPECTION TYPE:C, SUSPECT CRACK IN NR 1 KREUGER FLAP ACTUATOR MOUNT SUPPORT STRUCTURE. REPLACED PART WITH NEW FABRICATED ANGLE IAW SRM 51-10-1, PAGE 4.SDR CALA9801195Bracket · crackedINSPECTION FOUND A .75 INCH CRACK IN NR 5 LEADING EDGE FLAP INBOARD MOUNT BRACKET. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-40-3, AND 51-10-2.SDR DL76L981370Wedge · delaminatedTHE UPPER SKIN ON THE TRAILING EDGE WEDGE OF THE NR 3 SLAT WAS FOUND WITH A DELAMINATED AREA. DAMAGE WAS APPROX 1.5 BY 1.5. REPAIRED PER ERA 365144-14AD.SDR F3LA98110Skin · crackedDURING C-CHECK INSPECTION, REPORTED CRACK IN NR 2 SLAT OUTBOARD LOWER TRAILING EDGE SKIN NEAR UPSTOP. MAINTENANCE REMOVED DAMAGED AREA. FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-40-02, DRAWING 65C30133. (M)SDR TWAA9810804Splice · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND ON RT WING A CRACK IN WING L.E. ON SPLICE DOUBLER. LOCATED OTBD END OF NR 1 SLAT. INSTALLED SPLICE PER SRM 51-01, PG 1 ITEM C. ACFT TT: 77,210 HOURS. ACFT TC: 84,221. (X)SDR AALA981280Flap · corrodedTUL - KRUGER FLAP HAS CORROSION THROUGHOUT INTERNAL STRUCTURE. REPLACED KRUGER FLAP PER A-300MM 27-87-11-4. (M)SDR TWAA9810809Skin · delaminatedLAX - DURING CHECK-C, MAINTENANCE FOUND ON LT WING NR 5 L.E. SLAT INBD SIDE WITHSKIN DELAMINATION ON AFT SIDE. INSTALLED 2 INCH BY 3 INCH IN HOT BONDED FLUSH DOUBLER PER SRM 57-43-02 AND SRM 51-70-10. (X)SDR TWAA9810207Skin · delaminatedLAX - DURING CHECK-C, MAINTENANCE FOUND ON LT WING THE NR 5 LE SLAT INBD SIDE WITH DELAMINATION ON AFT SIDE. INSTALLED 2 INCH BY 3 INCH HOT BONDED FLUSH DOUBLER PER SRM'S 57-43-02 AND 51-70-10. TOTAL TIME: 63,613 HOURS. TOTAL CYCLES: 14,886. (X)SDR TWAA9801803Doubler · delaminatedLAX - DURING CHECK-C, MAINTENANCE ON LT WING DOUBLER REMOVED ON FWD SIDE, INBD END OF NR 5 L.E. SLAT, AND FOUND DELAMINATION ON AFT SIDE. INSTALLED 8 INCH BY 7 INCH HOT BONDED DOUBLER PER SRM 567-43-02 AND SRM 51-70-10. ACFT TT: 63,613 HOURS. ACFT TC: 14,SDR GAIA9868Flap · corrodedDURING ROUTINE C-CHECK INSPECTION. CORROSION WAS FOUND ALONG THE NR 1 KRUGER FLAP BULLNOSE WHERE THE JUMPER CABLE IS ATTACHED. THE CORROSION WAS REMOVED BY BLENDING OUT. THE JUMPER ATTACH HOLE WAS RELOCATED IN THE MAIN FLAP BODY FORWARD 1.0 INCH WHILE MAINTSDR DL76S981317Skin · delaminatedTHE NR 9, 11 AND 12 SLATS WERE FOUND WITH AREAS OF DELAMINATION ON THE TRAILING EDGE WEDGES. THE DAMAGED AREAS WERE TRIMMED OUT AND REPAIRED PER THE B767 SRM, 57-43-02. THE REPAIRS WERE DOCUMENTED PER ER/A 365088-14AD. (S/N 000222).SDR SWAA981200Seal · wornDURING SCHEDULED C2 CHECK, FOUND O/B K-FLAP TEFLON RUBSTRIP AND SEAL WORN. REMOVED AND REPLACED PER BOEING SRM.SDR SWAA981199Seal · wornDURING SCHEDULED C2 CHECK, FOUND K-FLAP BULB SEAL WORN. REMOVED AND REPLACED PER BOEING SRM.SDR TWAA9810102Skin · delaminatedLAX - DURING CHECK-C, MAINTENANCE FOUND APPROXIMATELY A 5 INCH BY 5 INCH DELAMINATION ON UPPER LEADING EDGE AFT OF NR 6 LE SLAT, APPROXIMATELY 5 FEET OTBD OF INBD END OF SLAT, LT WING. ROUTED OUT DELAMINATION. REMOVED 1 INCH SKIN AROUND AREA AND INSTALLED HESDR CALA9801137Panel · corrodedINSPECTION FOUND RT WING NR 3 FLAP LEADING EDGE PANEL CRACKED AND CORRODED AT XFLS 283. THE CORROSION WAS REMOVED AND THE AREA WAS REPAIRED IAW SRM 51-30-2 AND 51-70-2.SDR CALA9801136Panel · delaminatedINSPECTION FOUND LT FLAP LEADING EDGE PANEL NR 3 DELAMINATED AT XFL 267. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-70-2.SDR DL76S981272Skin · delaminatedUPPER SKINS ON THE TRAILING EDGE WEDGES OF THE NR 9, 10, AND 12 SLATS WERE FOUND WITH DELAMINATED AREAS. REPAIRED PER ERA 365048-14AD.SDR UPS98227022Slat · damagedINSPECTION TYPE:C, NR 5 SLAT I/B ACTUATOR RIB DAMAGED. REPAIR CARRIED IAW SRM 51-40-2.SDR CALA9801085Rib · crackedINSPECTION FOUND FLAP RIB LEADING EDGE OF LT WING AT XRS 270 CRACKED AND CORRODED. THE FLAP RIB WAS REMOVED IAW SRM 51-30-2. A NEW RIB WAS FABRICATED AND INSTALLED IAW SRM 51-10-4 AND 51-10-3.SDR 98UAL900283Arm · crackedRIGHT INBOARD NR 8 LEADING EDGE SLAT CENTER PAIR OUTBOARD ARM (114W2804-8) CRACKED AT UPPER FLANGE NEAR AFT END ROLLERS. REPLACED ARM (114W2804-8).SDR CALA9801033Rib · crackedINSPECTION FOUND A 1 CRACK IN INBOARD END RIB OF NR 2 SLAT. THE RIB WAS REMOVED AND A NEW RIB WAS INSTALLED IAW SRM 51-31-01.SDR CALA9801032Rib · crackedINSPECTION FOUND A 1 CRACK IN OUTBOARD RIB OF NR 1 SLAT. THE RIB WAS REMOVED AND A NEW RIB WAS INSTALLED IAW SRM 51-37-01 AND 51-35-02.SDR DHL9870932CBracket · crackedAT C CHECK, NR 8 INBD FLAP TRACK FAIRING ATTACH BRACKET CRACKED. REMOVED AND REPLACED PER SRM 51-30-2, N/R 2229.SDR CALA9801023Skin · crackedINSPECTION FOUND A 2 CRACK IN RT WING LOWER SURFACE ON LEADING EDGE SLAT CUTOUT FOR SLAT TRACK. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 57-10-00, 51-31-01, AND 54-11-00, FIGURE 1C.SDR DL767981281Skin · delaminatedDELAMINATION WAS FOUND ON SEVERAL T/E WEDGES OF THE L/E SLATS (NR 1, 2, 4 AND 5). REPAIRED PER ERA 365004-14AD.SDR DL72W981232Bracket · crackedA 1.75 INCH CRACK O/B AFT MOUNT BRACKET NR 1 SLAT ACT. ALSO INBD BRACKET CRACKED 2 INCHES. REPAIRED PER MM 57-21-21.SDR DHL9870920CBracket · crackedAT C CHECK, NR 6 LEADING EDGE FLAP ACTUATOR MOUNT IS CRACKED BOTH SIDES OF ACTUATOR. REMOVED AND REPLACED BRACKET PER SRM 57-20-1, 10 BY 10, N/R 2161.SDR DL72S981200Bracket · crackedA .5 INCH CRACK NR 2 L/E FLAP ACT ATTACH BRACKET, LOWER FWD END. FOUND ON D1 LTR CHECK. INSTALLED DOUBLER PER M/M 57-20-21.SDR DL76G981221Skin · delaminatedTHE NR 6 LEADING EDGE SLAT TRAILING EDGE WEDGE WAS FOUND WITH THE UPPER SKIN DELAMINATED ALONG THE O/B EDGE 1 FWD OF THE TRAILING EDGE OF THE PANEL. THE DAMAGED AREA MEASURED 2 X 2 AND WAS REPAIRED USING SRM COMPOSITE REPAIR PER ER/A 364972-14AD.SDR DL76G981220Skin · delaminatedTHE NR 4 LEADING EDGE SLAT TRAILING EDGE WEDGE WAS FOUND WITH THE UPPER SKIN DELAMINATED AT A LOCATION 6 INCHES FROM THE O/B END. THE DAMAGE MEASURES APPROX 4 X 4 AND WAS REPAIRED USING AN SRM COMPOSITE REPAIR PER ER/A 364971-14AD.SDR DL76G981219Skin · delaminatedTHE NR 11 LEADING EDGE SLAT TRAILING EDGE WEDGE WAS FOUND TO HAVE THE UPPER SKIN DELAMINATED ALONG THE O/B EDGE. THE DAMAGE MEASURES 3 X 3. THE DAMAGE WAS REPAIRED USING AN SRM COMPOSITE REPAIR AUTHORIZED BY ER/A 364970-14AD.SDR DL76G981218Skin · delaminatedTHE NR 2 LEADING EDGE SLAT TRAILING EDGE WEDGE WAS FOUND TO HAVE THE UPPER SKIN DELAMINATED ALONG THE I/B EDGE 4 FWD OF THE TRAILING EDGE. THE DELAMINATED AREA MEASURES 4 X 4. THE DAMAGE WAS REPAIRED USING AN SRM COMPOSITE REPAIR AUTHORIZED BY ER/A 364969-1SDR DL76G981217Skin · delaminatedTHE NR 5 LEADING EDGE SLAT TRAILING EDGE WEDGE WAS FOUND WITH THE UPPER SKIN DELAMINATED ALONG THTE I/B EDGE 3 FWD OF THE TRAILING EDGE OF THE PANEL. THE DAMAGED AREA MEASURES APPROX 5 (FWD/AFT) X 12. THE DAMAGE WAS REPAIRED WITH AN SRM COMPOSITE REPAIR PER SDR DL76L981182Wedge · delaminatedWING, LEADING EDGE SLAT NR 1 TE WEDGE. REPAIR FOR DISBONDING SKIN. THE TRAILING EDGE WEDGE ON THE NR 1 SLAT WAS FOUND WITH A 6 AREA OF DELAMINATION ON THE UPPER AND LOWER SKINS. THE DAMAGED AREA WAS TRIMMED OUT AND REPAIRED PER B767 SRM 57-43-02, FIGURE 201SDR DL72S981175Skin · crackedFOUND AT B2 LETTER CHECK, 2 CRACKS .75 INCH AND 2 INCH AT NR 4 L/E FLAP O/B HINGE CUTOUT. REPAIRED PER ERA 364950-14 AND M/M 57-53-0.SDR UPS98226846Hinge · corrodedINSPECTION TYPE:C, NR 4 K-FLAP OUTBRD HINGE LUG CORRODED AROUND UPPER AND LOWER FASTENER HOLES. REPLACED COMPLETE K-FLAP ASSY PER MM 27-81-01.SDR SWAA981041Skin · crackedDURING SCHEDULED BC 1 CHECK, FOUND CRACKED NR 2 L/E SLAT LOWER SKIN AT INBOARD AUX TRACK. REPAIRED PER BOEING TYPICAL REPAIR T1-A57-015 AND BOEING DRAWING 65C30133 SHEET 3.SDR SWAA981040Skin · crackedDURING SCHEDULED BC 1 CHECK, FOUND CRACKED NR 1 L/E SLAT LOWER SKIN AT INBOARD AUX TRACK. REPAIRED PER BOEING SRM AND TYPICAL REPAIR T1-A57-015.SDR CALA9800915Skin · crackedINSPECTION FOUND THREE .25 CRACKS COMING FROM RIVETS IN NR 1 SLAT LOWER SKIN BETWEEN OUTBOARD MAIN TRACK AND OUTBOARD AUX TRACK. A REPAIR WAS INSTALLED IAW BOEING DRAWING NR 65C30133.SDR SWAA980966Skin · crackedDURING SCHEDULED D CHECK, FOUND CRACKED NR 4 SLAT ON LOWER SKIN, O/B OF PUSHROD SITTING. REPAIRED PER TRAMCO EO NR 98-0440.SDR DHL9870636CRib · crackedAT C-CHECK, NR 5 SLAT I/B CLOSURE RIB IS CRACKED. REPLACED RIB PER SRM 51-30-2. N/R 2137.SDR UPS98226831Skin · crackedINSPECTION TYPE:C, CRACK GROWING PAST STOP DRILL HOLE IN NR 4 SLAT, I/B TRACK, O/B SIDE OF SKIN SUPPORT ANGLE. STOP DRILLED END OF CRACK, NDT VERIFIED CONTAINMENT, RE-INSTALLED EXISTING REPAIR IAW SRM 57-50-3.SDR DL767981097Wedge · delaminatedNR 5 LEADING EDGE SLAT T/E WEDGE WAS FOUND WITH DELAMINATION ON THE UPPER SURFACE MEASURING 3 X 5. REPAIR PER ERA 364831-14AD.
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