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 SWAA091246Skin · delaminatedDURING SCHEDULED 14Y CHECK, FOUND LT WING NR 1 L/E SLAT DELAMINATED AT LOWER SKIN. REPAIRED SLAT PER SRM.SDR AALA2009022300234Skin · crackedNR 3 SLAT HAS CRACK IN THE BACK SKIN 1.25 INCH LONG AT THE INBD DRIVE TRACK. REPAIRED IAW AARD 57-43-04. INSTALLED DOUBLER.SDR DU4R20090331Wedge · corrodedDURING SCHEDULED INSP, FOUND L/E SLAT NR1 HAS HEAVY CORROSION IN L/E AND IN T/E WEDGE.SDR FDEA200902200600Skin · misrepairedRIGHT WING NR 4 SLAT INNER SURFACE FOUND 03 EACH EXISTING REPAIRED PATCH AT APPROXIMATELY XORS 538. RIGHT WING NR 4 SLAT INNER SURFACE 03 EACH EXISTING DOUBLERS EVALUATED AND FOUND NOT IN ACCORDANCE WITH SRM REPAIR. EXISTING DOUBLERS 03 EACH REMOVED AND RESDR USAA2009031790620Slat · warpedSAL - C17 - MAJOR REPAIR - NR 2 SLAT WARPED AT OUTBOARD END. REPLACED NR 2 SLAT IAW AMM 27-81-21-4.SDR SWAA091153Slat · delaminatedDURING SCHEDULED 24Y CHECK, FOUND LT WING NR 3 SLAT O/B EDGE DELAMINATED. REPAIRED SLAT PER MM.SDR FDEA200902170558Skin · damagedLEFT WING LEADING EDGE SKIN AT NR 3 SLAT FOUND WITH CUT MARK. REPAIR CARRIED AT LT WING LEADING EDGE SKIN AT NR 3 SLAT TRACK AS PER SRM 57-10-00 FIG 24 VOL I. REPAIR CLASSIFIED AS PER GMM 6-2-100.SDR ASAA0944885Skin · dentedNR 3 SLAT LWR SURFACE DENTED 18 INCHES FROM I/B END. REMOVED DAMAGED AREA, FABRICATED, TREATED AND BONDED SKIN AND DOUBLER REPAIR IAW B737 400 SRM 51 70 10.SDR ASAA0944838Skin · dentedNR 3 SLAT LOWER SURFACE DENTED 18 INCHES FROM I/B END. REMOVED DAMAGED AREA, FABRICATED, TREATED AND BONDED SKIN AND DOUBLER REPAIR IAW B737 400 SRM 51 70 10.SDR IPXA09M54895Angle · misrepairedINSPECTION TYPE:4C REPAIR SURVEY SEQ W4-004, RT WING NR 2 SLAT, SUPPORT ANGLE HAS AN EXISTING REPAIR, BASE STRUCTURE IS .050 INCH, PER SRM 57-00-01 FIG 3 REQUIRES STACKED ANGLE (2) NOT ON MRCSSR. REMOVED EXISTING REPAIR ANGLE, FABRICATED AND INSTALLED 2 EA ANSDR SWAA091144Slat · crackedDURING SCHEDULED 10Y CHECK, FOUND RT WING NR 8 L/E SLAT CRACKED. REMOVED AND REPLACED SLAT PER MM.SDR IPXA09855979Skin · dentedINSPECTION TYPE:SV SS NR 852-S4-08, LT SIDE, FLUSH REPAIR, STA ZR 170.656 HAS A DENT, GOUGED, TOOLING DAMAGE, AND FASTENERS DISTANCE LESS THAN 4D. REPAIRED PER TIMCO REO-G12807 REV IR, AND UPS EO NR DC8-5520-33390-A.SDR IPXA09M54867Skin · misrepairedINSPECTION TYPE:4C REPAIR SURVEY SEQ W3-003, LT WING, DROOPED L/E, SKIN HAS AN EXTERNAL DOUBLER, .072 INCH THICK, WITH A CRACK AND .25 INCH STOP DRILL UNDERNEATH. NO SPECIFIC REPAIR IN SRM AND NOT IAW 57-00-0 FIG 8, CALLS FOR SAME GAUGE DOUBLER AND CUTOUT/TRISDR AALA20090708TUL19Slat · damagedNR 9 SLAT HAS INTERIM REPAIR. REPAIRED IAW SRM 57-43-01-2R2 FLUSH DOUBLER.SDR AALA20090708TUL18Slat · crackedNR 9 SLAT CRACKED AT AFT SIDE AT OUTBOARD TRACK. REPAIRED IAW AARD 57-43-00-4 EXTERNAL DOUBLER.SDR AALA2009022300231Slat Track · crackedNR 9 SLAT HAS AN APPARENT CRACK ON THE BACK SIDE AT OTBD TRACK. REPAIRED IAW SRM 57-43-00-4. INSTALLED DOUBLER.SDR AALA2009022300232Skin · corrodedNR 9 SLAT HAS BLENDED AREA WITH FILLER MATERIAL OVER BLIND FASTENER. REPAIRED IAW SRM 57-43-01-2R2. INSTALLED DOUBLER.SDR IPXA09554854Skin · debondedINSPECTION TYPE:C4 VERIFY STRUCTURAL SOUNDNESS OF PREVIOUS REPAIR ON NR 3 SLAT T/E WEDGE UPPER SURFACE AT OSS 519.55-528.55 EVALUATION REQUIRED PER EO B757-5100-30760 (438-W3-04). REMOVED DISBONDED REPAIR AND REPAIRED PER ATS ER09-1688 DATED 26FEB09 UPS EO B7SDR USAA2009021890372Panel · crackedMCN - C12 - MAJOR REPAIR - NR 9 SLAT COVE PANEL CRACKED INBOARD SIDE OF INBOARD MAIN TRACK. REPLACED NR 9 SLAT COVE PANEL IAW BOEING DRAWING 114N4076.SDR SWAA091096Slat · peelingDURING SCHEDULED MV1 CHECK, FOUND LT WING NR 2 SLAT PEELING AT O/B CORNER. REPAIRED SLAT PER SRM.SDR AALA20090708TUL17Slat · damagedNR 2 SLAT HAS INTERIM REPAIR. REPAIRED IAW SRM 5743-01.SDR AALA20090708TUL16Slat Track · crackedNR 2 SLAT CRACKED AT INBOARD DRIVE TRACK. REPAIRED IAW AARD 57-43-00-4. (INSTALLED EXTERNAL DOUBLER).SDR AALA20090708TUL13Slat · damagedNR 3 SLAT HAS INTERIM REPAIR. REPAIRED IAW SRM 57-43-01. (INSTALLED FLUSH DOUBLER)SDR AALA20090302TUL04Fitting · crackedLEFT NR 5 SLAT, SECOND FROM OUTBOARD SLAT RIB FITTING IS CRACKED AT NR 14 SLAT TRACK ATTACH. REMOVED AND REPLACED ATTACH FITTING PER ESO 80117.SDR AALA20090302TUL02Fitting · crackedLEFT NR 5 SLAT OUTBOARD RIB FITTING CRACKED AT NR 15 SLAT TRACK ATTACH POINT. REMOVED AND REPLACED OUTBOARD ATTACH FITTING PER ESO 80117.SDR AALA2009022300236Skin · corrodedNR 3 SLAT HAS LOCAL BLEND AND BLIND FASTENER AT LOCATION 43 INCHES FROM INBD END AT THE AFT LWR END NOSE SKIN. REPAIRED IAW SRM 57-43-01. INSTALLED DOUBLER.SDR AALA2009022300237Skin · corrodedNR 3 SLAT HAS LOCAL BLEND AND BLIND FASTENER 61 INCH FROM INBD END - FWD OF THE AFT END OF UPPER SKIN. REPAIRED IAW SRM 57-43-01. INSTALLED DOUBLER.SDR AALA2009022300239Skin · crackedNR 3 SLAT CRACKED AT BACK SKIN 1.25 INCH LONG AT THE INBD DRIVE TRACK AREA.SDR AALA2009022300238Skin · corrodedNR 3 SLAT HAS LOCAL BLEND AND BLIND FASTENER AT LOCATION 31 INCH INBD OF THE OTBD EDGE - 105 INCH FWD OF THE AFT END. REPAIRED IAW SRM 57-43-01. INSTALLED DOUBLER.SDR AALA2009022300240Skin · damagedNR 2 SLAT HAS LOCAL BLEND AREA WITH BLIND FASTENER INSTALLED AT THE LOCATION 30 INCH OTBD OF INBD END AND 17 INCHES FWD OF AFT END ON LEADING EDGE NOSE SKIN.SDR AALA2009022300241Skin · crackedNR 2 SLAT BACK SKIN CRACKED THROUGH FASTENER HOLE AT INBD DRIVE TRACK AREA.SDR AALA2009022300242Skin · crackedNR 2 SLAT BACK SKIN CRACKED THROUGH FASTENER HOLE AT INBD DRIVE TRACK AREA.SDR ASAA0944544Wedge · dentedNR 3 SLAT LOWER SURFACE T/E WEDGE IS DENTED. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR SKIN AND DOUBLER IAW B737 400 SRM 51 70 10 REP 4.SDR UPS09654805Slat · delaminatedINSPECTION TYPE:C LT WING NR 3 SLAT UPPER SURFACE DELAMINATION. METAL HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-10 REPAIR 2 FIG 203 REV 43. DOUBLER MATERIAL 2024T3-0016IN AND ADHESIVE FILM AF163-2K0010IN. REPAIR DOUBLER SIZE 4.125 X 5 INCHES.SDR AALA20090708TUL25Skin · corrodedNR 8 SLAT TOP SKIN CORRODED. REPAIRED IAW AARD 57-43-01.SDR AALA2009022300235Skin · corrodedNR 8 SLAT HAS TWO CORROSION BLISTERS IN TOP SKIN ON 33 INCH FROM THE INBD END. REPAIRED IAW AARD 57-43-0. INSTALLED DOUBLER.SDR ASAA0944893Wedge · chafedNR 3 SLAT T/E WEDGE WORN THIN I/B AFT LOWER CORNER. REMOVED DAMAGED AREA, FABRICATED, TREATED, PRIMED AND BONDED NEW SKIN AND DOUBLER IAW B737 400 SRM 51 70 10.SDR DL757090430Panel · damagedNR 10 SLAT ASSY INBD END COVE PANEL HAS CHAF FWD AREA. INSTALLED REPL PANEL AT NR 10 SLAT IAW SRM 51-40-02, APPLIES TOPCOAT IAW AMM 51-21-00-377.SDR UPS09654780Panel · misrepairedINSPECTION TYPE:C LT WING NR 6 SLAT LOWER CLOSURE PANEL THE EXISTING REPAIR PATCH NON- STANDARD REPAIR. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-17 PARA 4H FIG 19 REV 43.SDR UPS09654779Panel · misrepairedINSPECTION TYPE:C RT WING NR 7 SLAT LOWER CLOSURE PANEL THE EXISTING REPAIR PATCH NON- STANDARD REPAIR. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-17 PARA 4H FIG 19 REV 43.SDR USAA2009022390417Skin · crackedMCN - C24 - MAJOR REPAIR - CRACK ON NR 6 SLAT LOWER SKIN STA 255. REPAIRED NR 6 SLAT LOWER SKIN STA 255 IAW B737 SRM 57-43-01.SDR AALA20090302TUL08Fitting · crackedNR 14 SLAT TRACK TRACK FITTING CRACKED. REMOVED AND REPLACED SECOND FROM OUTBOARD RIB AT NR 14 SLAT TRACK ATTACH POINT PER ESO 80117.SDR AALA20090302TUL07Rib · crackedRIB CRACKED ON LEFT WING SLAT AT OUTBOARD RIB, NR 15 SLAT TRACK ATTACH. REMOVED AND REPLACED OUTBOARD ATTACH RIB PER ESO 80117 AND SRM 27-80-1.SDR AALA20090302TUL06Rib · crackedNR 5 SLAT OUTBOARD RIB CRACKED AT NR 15 SLAT TRACK ATTACH POINT. REPLACED OUTBOARD RIB AT NR 15 SLAT TRACK ATTACH POINT PER ESO 80117.SDR SWAA091011Slat · crackedDURING SCHEDULED 14Y CHECK, FOUND RT WING NR 5 L/E SLAT O/B ARM CRACKED. REMOVED AND REPLACED SLAT PER SRM.SDR SWAA091010Slat · delaminatedDURING SCHEDULED 14Y CHECK, FOUND LT WING NR 3 L/E SLAT I/B UPPER CORNER DELAMINATED. REPAIRED SLAT PER SRM.SDR SWAA091009Slat · delaminatedDURING SCHEDULED 14Y CHECK, FOUND LT WING NR 2 L/E SLAT I/B UPPER CORNER DELAMINATED. REPAIRED SLAT PER SRM.SDR IPXA09554912Wedge · dentedINSPECTION TYPE:C3 NR 7 SLAT HAS A DENT ON THE UPPER SURFACE OF THE T/E WEDGE, 18 INCHES O/ O/B OF I/B END AND 3 INCHES FWD OF T/E. NR 7 SLAT REPAIRED PER SRM 51-70-10-2R2.SDR IPXA09554911Skin · dentedINSPECTION TYPE:C3 NR 7 SLAT HAS A DENT WITH A GOUGE IN IT ON THE UPPER SURFACE T/E WEDGE, 18.5 INCHES I/B OF O/B END AND 6" INCHES FWD OF T/E. NR 7 SLAT WAS REPAIRED PER SRM 51-70-10-2R3SDR C8GA20090048Rib · crackedWHILE IN HEAVY MAINTENANCE IT WAS NOTED THAT THE NR 7 SLAT OTBD HOOK HAS 2 CRACKED RIBS ON THE SIDES OF THE ACTUATOR FWD MOUNT AT THE LOWER AFT RADIUS. REMOVED BOTH RIBS, STOP DRILLED CRACK IN OTBD RIB, PERFORMED HFEC, NO CRACKS NOTED. FABRICATED DOUBLER FOR
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