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 SWAA084973Skin · delaminatedDURING SCHEDULED 22Y CHECK, FOUND LT WING NR 2 L/E SLAT INBOARD END DELAMINATED. REMOVED AND REPLACED SLAT PER MM.SDR ASAA0843604Skin · chafedRT WING L NR 4 LEADING EDGE SLAT I/B TRAILING EDGE WEDGE HEAVY CHAFE AT I/B END. REMOVED DAMAGED AREA, FABRICATED SKIN AND DOUBLER BONDED IAW B737 400 SRM 51 70 10 REPAIR 4.SDR USAA920081645Wedge · delaminatedCLT Q1 MAJOR REPAIR NR 03C40257009/011 & 03C40257009/015 - NR 5 SLAT LOWER WEDGE DELAMINATED AT INBD AND OTBD END. REPAIRED NR 5 SLAT LOWER WEDGE AT INBD AND OTBD END IAW B737 SRM 51-70-10.SDR 08FDEA03727Skin · crackedNR 1 SLAT TRAILING EDGE IS GOUGED AND CRACKED AT I/B HOOK WS 716 TRIMMED OUT DAMAGED AREA DIM 1/2 PER 1/2 IAW SRM 57-50-3 FIG 10. FABRICATED REPAIR DOUBLER MAT USED 7075T6 0.125, DIM 4 INCH PER 3 1/2 INCH IAW SRM 57-50-3 FIG 10. TREATED AND PRIMED IAW SRM 5SDR ASAA0843437Skin · dentedNR 6 SPOILER IS DENTED ON UPPER SURFACE FROM SEAL SCREWS ON LOWER SURFACE. REPAIRED NR 6 SPOILER IAW B737 400 SRM 51-70-10 REPAIR 4 PG 201.SDR 08FDEA03652Skin · crackedLT WING - LEADING EDGE AT SLAT NR 3, NR 8 TRACK AREA, 01 EA EDGE CRACK. REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 21 VOLUME I. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100.SDR 08FDEA03629Skin · crackedRIGHT NR 1 SLAT LOWER SURFACE SKIN IS CRACKED AT A FASTENER HOLE, TRAILING EDGE APPROX 1 INCH FROM THE INBD END. REMOVED RIGHT WING NR 1 SLAT IAW AMM 27-80-01-4. OPENED SKIN FOR ACCESS. REMOVED THE CRACKED SECTION. FABRICATED A REPAIR, INSTALLED REPAIR ASDR UPS08M53273Slat Track · crackedINSPECTION TYPE:1C RIGHT WING SLAT TRACK 16 CRACKED. REMOVED, REPLACED, AND INSTALLED FITTING IAW MD-11 SRM 51-33-01, 51-31-01.SDR UDSS920081591Skin · delaminatedCLT Q6 MAJOR REPAIR NR 03C40257009/001 AREA OF DELAMINATION ON RT WING NR 6 SLAT TRAILING EDGE WEDGE LOWER SURFACE. REPLACED RT WING NR 6 SLAT IAW US AIRWAYS TASK CARD 03C40227004.SDR 2008UALA05490Wedge · damagedLT NR 3 SLAT WEDGE HAS DAMAGE. REMOVED NR 3 SLAT, R&R R425 60 TO SHOP AND RE-INSTALLED. INSPECTED INSTALLATION, FOUND OKAY.
SDR 08FDEA03572Vane · damagedKRUEGER FLAP VANE WAS DAMAGED DURING FUNCTION CHECKS. REPAIR PERFORMED BY REPLACEMENT OF KRUEGER FLAP VANE ASSY IAW AMM 27-87-12/401.SDR 08FDEA03571Skin · damagedKRUEGER FLAP WAS DAMAGED DURING FUNCTION CHECKS REPAIR PERFORMED BY REPLACEMENT OF KRUEGER FLAP ASSY IAW AMM 27-87-11/401.SDR C8GA20080054Mount · crackedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE NR 7 SLAT ACTUATOR OB MOUNTING BRACKET HAD A 1" CRACK. REMOVED CRACKED SUPPORT. FABRICATED NEW DOUBLER AND NEW STIFFNER. INSTALLED NEW SUPPORT PARTS IAW SB 727-57-0130. NO OTHER DEFECTS WERSDR C8GA20080053Mount · crackedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE NR 7 SLAT ACTUATOR IB MOUNTING BRACKET HAD A 1" CRACK. REMOVED CRACKED SUPPORT. FABRICATED NEW DOUBLER FROM 301 1/2 HD .100" (7.5 X 3) AND NEW STIFFNER FROM BAC 1503-100145 (9" X 4"). INSTASDR DL757081219Skin · gougedSMALL GOUGE ON T/E OF SLAT NR 3. BONDED SKIN FILLER AND INTERNAL DOUBLER AND CORE PLUG IAW SRM 51-70-10.SDR ASAA0843461Skin · delaminatedNR 2 SLAT T/E LOWER SURFACE IS DELAMINATED AT OUTBOARD CORNER. REMOVED DAMAGED AREA, FABBED FILLER AND DOUBLER, INSTALLED REPAIR IAW B737 400 SRM 51-70-10 FIG 4.SDR ASAA0843454Skin · chafedNR 3 SLAT LOWER SURFACE T/E INBOARD END IS CHAFED. REMOVED DAMAGED AREA, FABBED FILLER AND DOUBLER. BONDED REPAIR IAW B737 400 SRM 51-70-10.SDR ASAA0843452Skin · delaminatedNR 4 SLAT INBOARD T/E IS DELAMINATED ON THE TOP INBOARD END. PREPPED DAMAGED AREA, FABBED CORE PLUG AND DOUBLER, INSTALLED REPAIR IAW B737 400 SRM 51-70-10 REPAIR 4.SDR UPS08M53298Skin · dentedINSPECTION TYPE:C RT WING NR 2 SLAT LEADING EDGE DENT. DENT SKIN REMOVED PER SRM 57-10-00 FIG 37 VIR 40 & CUT OUT PROTECTED PER SRM 51-21-01 VII R40. HFEC INSP C/OUT PER NDTSPM R.13 06-10-01.001 FOUND NO CRACK ON TRIMMED OUT AREA. REP FILLER & DOUBLER FABRISDR USAA920081568Skin · delaminatedCLT - Q6 - MAJOR REPAIR - NR 03C40257009/003 - DELAMINATION ON NR 5 SLAT LOWER SURFACE OUT BOARD TRAILING EDGE. REPLACED NR 5 SLAT.SDR 08FDEA03517Skin · crackedLEFT WING - NR 6 LEADING EDGE SLAT OUTBOARD TRACK CUTOUT CORNER FOUND SUSPECTED CRACK. LEFT WING NR 6 LEADING EDGE SLAT OUTBOARD TRACK CUTOUT OUTBOARD CRACKED CORNER TRIMMED OFF AND REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 21 VOLUME I. REPAIR CLASSIFIEDSDR ASAA0843426Skin · chafedLEFT WING NR 3 SLAT LOWER T/E WEDGE CHAFED ON I/B SIDE. PREPARED DAMAGED AREA, FABRICATED REPAIR DOUBLER AND BONDED IAW B737 400 SRM 51-70-10 REPAIR 2.SDR USAA920081586Skin · crackedCLT MAJOR REPAIR C4 CHECK NR 5030564 AND 03C0057002/022, LT WING NR 1 SLAT SKIN CRACKED AT INBOARD AUXILIARY TRACK R&R THE LT WING NR 1 SLAT IAW 737 AMM 27-81-21.SDR ASAA0843433Skin · chafedINBOARD TRAILING EDGE OF NR 4 SLAT CHAFED. REMOVED DAMAGED SKIN, FABRICATED REPAIR PARTS AND INSTALLED IAW B737 400 SRM 51-70-10.SDR 08FDEA03476Pan · crackedLT SLAT NR 1 FOLDING NOSE INNER PAN WITH CRACK FINDING REPAIR PERFORMED BY INSTALLING SB A300-6067 WITH INNER PAN REPLACEMENT, APPROVED BY EA 6-5742-120064.SDR 08FDEA03475Structure · damagedSLAT NR 2 LT WAS DAMAGED AT RIB 12-14 REPAIR PERFORMED IAW SRM 57-43-11 PARA 4A.SDR UIEA200800282Panel · crackedRT WING UPPER LEADING EDGE PANEL HAS A 20.0 INCH COMPOSITE CRACK AT ILES 522.56 AND IS 26 INCHES FROM FORWARD END OF PANEL. PERMANENT REPAIR ACCOMPLISHED AS PER 747-200 SRM 51-40-09 FIG 18, SHEETS 2 AND 5, PREPEG LAYUP 250 DEGREES F CURE PER SRM 51-40-12. RESDR SWAA084522Slat · crackedDURING SCHEDULED 10Y CHECK, FOUND RT WING NR 8 L/E SLAT CRACKED AT OUTBOARD END. REMOVED AND REPLACED SLAT PER MM.SDR C8GA20080051Mount · crackedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THE THE NR 2 KFLAP ACTUATOR UPPER MOUNT WAS CRACKED AT THE UPPER INBOARD CORNER. REMOVED DAMAGED MOUNT AND FABRICATED NEW. INSTALLED NEW MOUNT IAW SRM 57-20-02. NO OTHER DEFECTS WERE NOTED. AIRCRAFTSDR SWAA084565Slat · delaminatedDURING SCHEDULED HC2 CHECK, FOUND RT WING NR 5 L/E SLAT DELAMINATED AT OUTBOARD T/E END. REPAIRED SLAT PER SRM.SDR 08FDEA03384Skin · chafedFOUND CHAFING MARKS ON SLAT NR 1 RT LOWER SKIN. REPAIR PERFORMED BY BLEND OUT THE DAMAGE IAW RAS/FOK/153/2008 ISS A, APPROVED BY EA 6-5742-120090.SDR UPS08M53170Skin · dentedINSPECTION TYPE:C LT WING NR 6 SLAT EXTERIOR SURFACE FOUND QTY 04EA DENTED AREA AT 20 TO 27 INCHES FROM B/B END AND 26 INCHES FROM T/E. DENTED AREAS MEASURED DEPTH: 0.039 INCH AND FOUND EXCEED LIMIT AS PER SRM 57-10-00 FIG 16 VOL I REV 40. DENTED AREA TRIMMESDR UPS08M53140Skin · dentedINSPECTION TYPE:C LT WING NR 6 SLAT EXTERIOR SURFACE FOUND DENTED AT 40.5 INCHES FROM I/B END AND 30.5 FROM T/E. LT WING NR 6 SLAT EXTERIOR SURFACE DENTED AREA MEASURED DEPTH 0.037 INCH AND FOUND EXCEED LIMIT AS PER SRM 57-10-00 FIG 16 VOL I REV 40. DENT ARESDR UPS08M53139Strap · crackedINSPECTION TYPE:C RT WING L/E LOWER ACCESS AT 13 INCHES O/B OF SLAT NR 12 FOUND STRAP SUSPECT CRACK. HFEC CARRIED OUT IAW DAC NDT SPM REV 13 PART 06-10-01.001 AND CRACK CO CONFIRM APPROX 4.75 INCHES LONG. DAMAGE STRAP AND ATTACH FORMER REMOVED, STRAP FABRICASDR SWAA084393Skin · crackedDURING SCHEDULED 24Y CHECK, FOUND RT WING NR 4 L/E SLAT CRACKED AT INBOARD END. REPAIRED SLAT PER SRM.SDR UPS08553084Bracket · chafedINSPECTION TYPE:C3 NR 1 SLAT O/B AUX TRACK CLOSURE PANEL ATTACH BRACKET I/B AFT EDGE IS CHAFED. REMOVED CHAFED BRACKET. FABRICATED REPLACEMENT BRACKET. INSTALLED REPLACEMENT BRACKET PER OHM20-50-01, DWG 114N4146, M/M 51-21-10-7.SDR UPS08M53092Slat Track · crackedINSPECTION TYPE:C RT WING NR 11 SLAT TRACK I/B ENCLOSURE FOUND SKIN DOUBLER CRACKED. CRACKED SKIN DOUBLER AT RT WING NR 11 SLAT TRACK I/B ENCLOSURE TRIMMED OUT AS PER SRM 57-10-00 V1 R40 FIG 27. HFEC INSPECTION CARRIED OUT PER DAC NDTSPM REV 13 PART 06.10.01SDR SWAA084297Slat · crackedDURING SCHEDULED SPV CHECK, FOUND RT WING NR 6 L/E SLAT CRACKED AT OUTBOARD END. REPAIRED SLAT PER SRM.SDR FDEA200807303165Skin · crackedDURING INSPECTION RT WING SLAT NR 2 FOUND CRACK ON INNER SKIN. REPAIRED SKIN IAW SRM 57-10-00 FIG 31 VOL I.SDR 08FDEA03165Skin · crackedDURING INSPECTION RT WING SLAT NR 2 FOUND CRACK ON INNER SKIN.SDR WRLA2008063Structure · crackedDURING C CHECK INSPECTION CRACK-FOUND RT WING LE INBD SLAT NR 1 AFT SIDE HAD CRACK 11.5 INCHES LONG AT XIS 247. REMOVED THE RT INBD NR 1 SLAT ASSY COMPLETED PER AMM 27-80-20-000-801 REV 62. REPAIRED THE DAMAGED AREA IAW MD-11 SRM VOL ONE 57-10-00 REV. 40. ISDR SWAA084230Slat · delaminatedDURING SCHEDULED HC2 CHECK, FOUND RT WING NR 5 L/E SLAT DELAMINATED AT INBOARD END. REMOVED AND REPLACED SLAT PER MM.SDR SWAA084229Slat · delaminatedDURING SCHEDULED HC2 CHECK, FOUND RT WING NR 4 L/E SLAT DELAMINATED AT INBOARD END. REMOVED AND REPLACED SLAT PER MM.SDR USAA920081426Skin · debondedCLT - IRAN - MAJOR REPAIR - NR 10 SLAT HAS DISBONDING AT INBOARD AFT CORNER OF THE UPPER SKIN. REPAIRED NR 10 SLAT AT INBOARD AFT CORNER OF THE UPPER SKIN IAW US AIRWAYS EA NR100580. (S)SDR CALA0800750Skin · delaminatedNR 5 SLAT TRAILING EDGE WARPED AT OUTBOARD END AT PREVIOUS REPAIR. REPAIRED AT OUTBOARD END AT PREVIOUS REPAIR AND UPPER SURFACE REFINISHED PER SRM 51-70-10 AND CAL 5100500128 REV Q.SDR SWAA084125Skin · crackedDURING SCHEDULED BRDG CHECK, FOUND RH WING NR 6 L/E SLAT CRACKED AT OUTBOARD END. REPAIRED SLAT PER SRM.SDR FDEA200807233027Skin · wornRT WING L/E SLAT NR 6 FOUND DEEP WEAR INTERNAL SIDE. REPAIRED AREA IAW SRM 57-10-00 FIG 30 SHT 1 VOL I.SDR CA080801004Access Panel · missing(CAN) ON ARRIVAL, LEADING EDGE SLAT TRACK ACCESS PANEL 512HB FOUND MISSING. ADJACENT PANEL 512JB ALSO FOUND DAMAGED. LOST IN FLIGHT. PANEL 512HB REPLACED AND PANEL 512JB REPAIRED IAW SRM.SDR 08FDEA03027Skin · wornRT WING L/E SLAT NR 6 FOUND DEEP WEAR INTERNAL SIDE.SDR SWAA084032Skin · delaminatedDURING SCHEDULED BRDG CHECK, FOUND LT WING NR 1 L/E SLAT INBOARD END DELAMINATED. REPAIRED SLAT PER SRM.
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