N741UW

Service difficulty reports · 267

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. 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 n_number = 'N741UW' AND registry_match = 'registration'
  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.

SDR USAA2012061900002Door · out of adjust2S CHECK - OUT OF ADJUSTMENT DIM B (J1) BETWEEN FINGER AND STRIKER LEVER AT DOOR 832. PERFORMED ADJUSTMENT OF DIM B (J1) BETWEEN FINGER AND STRIKER LEVER AT DOOR 832 IAW A319 AMM 52-13-14-820-002-A PROCEDURE 1 THRU 4 ITEM A STEP 1.Jun 18, 2012 · N741UW · Airbus A319112 · Passenger/Crew DoorsSDR USAA2012061800011Door · out of adjust2S CHECK - DOOR 842 OUT OF ADJUSTMENT DIM B (J1) BETWEEN FINGER AND STRIKER LEVER. PERFORMED ADJUSTMENT OF DOOR 842 DIM B (J1) BETWEEN FINGER AND STRIKER LEVER IAW A319 AMM 52-13-14-820-002-A.Jun 16, 2012 · N741UW · Airbus A319112 · Passenger/Crew DoorsSDR USAA2012061800010Door · out of adjust2S CHECK - DOOR 842 OUT OF ADJUSTMENT DIM A (J2) BETWEEN FINGER AND STRIKER LEVER. PERFORMED ADJUSTMENT OF DOOR 842 DIM "A" (J2) BETWEEN FINGER AND STRIKER LEVER IAW A319N AMM 52-13-14-820-002-A.Jun 16, 2012 · N741UW · Airbus A319112 · Passenger/Crew DoorsSDR USAA2012062700012Slide · misinstalled2S CHECK - RIGHT OFF WING SLIDE ENCLOSURE DOOR ISN'T FLUSH WITH OUTER SURFACE OF THE SLIDE ENCLOSURE. REPACKED RIGHT OFF WING SLIDE IAW CMM 25-60-58 REV 18 AND FOLDING PROCEDURE P-11907 REV R.Jun 8, 2012 · N741UW · Airbus A319112 · Escape SlideSDR USAA2012062500030Skin · worn2S CHECK - WEAR ON LEFT WING LOWER SURFACE AT SLAT TRACK 2 OF SLAT 1 AT WFX 1244. REPAIRED LEFT WING 1 SLAT ON LOWER SURFACE AT SLAT TRACK 2 AT AT WFX 1244 IAW EA 501979.Jun 8, 2012 · N741UW · Airbus A319112 · Leading Edge DevicesSDR USAA2012061400024Slide · misinstalled2S CHECK - LEFT OFF WING SLIDE ENCLOSURE DOOR ISN'T FLUSH WITH OUTER SURFACE OF THE SLIDE ENCLOSURE. REPACKED LEFT OFF WING SLIDE IAW CMM 25-60-58 REV 18 AND FOLDING PROCEDURE P-11907 REV R.Jun 5, 2012 · N741UW · Airbus A319112 · Escape SlideSDR USAA2012062500032Access Door · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON RIGHT WING LOWER FUEL ACCESS DOOR 640NB BETWEEN WS 970 & WS 1020 & BETWEEN RIB 18 & RIB 19. REPLACED RIGHT WING LOWER FUEL ACCESS DOOR 640NB IAW JOB CARD 26C60057091.Jun 3, 2012 · N741UW · Airbus A319112 · Wing, Plate/SkinSDR USAA2012062500031Hinge Fitting · damaged2S CHECK - ELONGATED HOLE ON NR 1 ENGINE PYLON OUTBOARD FAN COWL AT NR 1 HINGE AT PYLON NACELLE STA 409. REPLACED NR 1 ENGINE PYLON OUTBOARD FAN COWL AT NR 1 HINGE IAW A319 SRM 51-42-11.Jun 3, 2012 · N741UW · Airbus A319112 · Nacelle/Pylon Miscellaneous StructureSDR USAA2012062000003Fuel Door · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON RIGHT WING LOWER FUEL DOOR PANEL 640NB BETWEEN WS 9704 TO WS 10204 & BETWEEN RIB 18 TO RIB 19. REPLACED RIGHT WING LOWER FUEL DOOR PANEL 640NB IAW A319 SRM 57-27-11 & JOB CARD 26C60057091.Jun 3, 2012 · N741UW · Airbus A319112 · Wing, Plate/SkinSDR USAA2012061900008Strut · corroded2S CHECK - CORROSION ON INTERNAL AREA OF INTERCONNECTING STRUT ON RIGHT FLAP BETWEEN WS 4067 TO WS 4862, RIB 9. REPLACED INTERCONNECTING STRUT ON RIGHT FLAP IAW A319 AMM 27-51-44-400-001 & JOB CARD 26C67057001.Jun 3, 2012 · N741UW · Airbus A319112 · Trailing Edge FlapsSDR USAA2012062200010Flap · corroded2S CHECK - CORROSION ON OUTBOARD FLAP BETWEEN WS 670 TO WS 732 AT FLAP RIB 6. REPLACED OUTBOARD FLAP IAW A319 AMM 27-54-62-400-001-A & EA 104060.Jun 2, 2012 · N741UW · Airbus A319112 · Trailing Edge FlapsSDR USAA2012062500034Frame · corroded2S CHECK - CORROSION ON FUSELAGE FRAME AT FR68, S23L. REPAIRED FUSELAGE FRAME AT FR68, S23L IAW EA 500730.Jun 1, 2012 · N741UW · Airbus A319112 · Fuselage Main, FrameSDR USAA2012061900004Floor Panel · delaminated2S CHECK - DELAMINATION ON SEAT FLOOR PANEL 212EF BETWEEN FR6 TO FR12 & BETWEEN -Y765 TO -Y254. REPLACED SEAT FLOOR PANEL 212EF IAW A319 SRM 53-12-00 DIAGRAM 102 & IRM 9701 REV G.Jun 1, 2012 · N741UW · Airbus A319112 · Fuselage Floor PanelSDR USAA2012061500016Hinge Pin · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON RIGHT WING AILERON HINGE PIN BETWEEN WS 1406 TO WS 1446, RIB 26 TO RIB 27. REPLACED RIGHT WING AILERON HINGE PIN BETWEEN WS 1406 TO WS 1446, RIB 26 TO RIB 27 IAW A319 AMM 27-14-41-400-001-A- AND JOB CARD 26C60027005.Jun 1, 2012 · N741UW · Airbus A319112 · AileronsSDR USAA2012061500015Hinge Pin · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON RIGHT WING AILERON HINGE PIN BETWEEN WS 1406 TO WS 1446, RIB 26 TO RIB 27. REPLACED RIGHT WING AILERON HINGE PIN BETWEEN WS 1406 TO WS 1446, RIB 26 TO RIB 27 IAW A319 AMM 27-14-41-400-001-A AND JOB CARD 26C60027005.Jun 1, 2012 · N741UW · Airbus A319112 · AileronsSDR USAA2012062200002Hinge Pin · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON LEFT WING NR 2 SPOILER HINGE PINS (2 EA) BETWEEN WS 613 TO WS 670 & BETWEEN RIB 11 TO RIB 12. REPLACED LEFT WING NR 2 SPOILER HINGE PINS (2 EA) IAW A319 AMM 27-64-42 & JOB CARD 26C58327003.May 31, 2012 · N741UW · Airbus A319112 · SpoilersSDR USAA2012062000002Hinge Pin · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON NR 1 SPOILER HINGE PINS 2 EA ON LEFT WING BETWEEN WS 306 TO WS 376 & BETWEEN RIB 6 TO RIB 7. REPLACED NR 1 SPOILER HINGE PINS 2 EA IAW A319 AMM 27-64-41 & JOB CARD 26C58227003.May 31, 2012 · N741UW · Airbus A319112 · SpoilersSDR USAA2012061900007Web · cracked2S CHECK - CRACK ON WEB BETWEEN FR8 TO FR11, -Y765. REPLACED WEB BETWEEN FR8 TO FR11, -Y765 IAW A319 SRM 51-72-11 & DRAWING D53110285.May 31, 2012 · N741UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012061900006Tee Fitting · cracked2S CHECK - CRACK ON TEE FITTING AT FR8, -Y765. REPLACED TEE FITTING AT FR8, -Y765 IAW A319 SRM 51-72-11 & DRAWING D53113009.May 31, 2012 · N741UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012061800019Hinge Pin · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON RIGHT WING NR 2 SPOILER CENTER HINGE PINS (2 EA) BETWEEN WS 5512 TO WS 7316 & BETWEEN RIB 10 & RIB 13. REPLACED RIGHT WING NR 2 SPOILER CENTER HINGE PINS IAW A319 SRM 51-42-11.May 31, 2012 · N741UW · Airbus A319112 · SpoilersSDR USAA2012061800017Hinge Pin · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON RIGHT WING NR 1 SPOILER CENTER HINGE PINS (2 EA) BETWEEN WS 2580 TO WS 4067 & BETWEEN RIB 5 & RIB 8. REPLACED RIGHT WING NR 1 SPOILER CENTER HINGE PINS IAW A319 SRM 51-42-11.May 31, 2012 · N741UW · Airbus A319112 · SpoilersSDR USAA2012061800016Hinge Pin · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON RIGHT WING NR 4 SPOILER CENTER HINGE PIN BETWEEN WS 8744 TO WS 20204 & BETWEEN RIB 16 & RIB 19. REPLACED RIGHT WING 4 SPOILER CENTER HINGE PIN IAW A319 SRM 51-42-11.May 31, 2012 · N741UW · Airbus A319112 · SpoilersSDR USAA2012062500036Skin Panel · corroded2S CHECK - CORROSION ON FUSELAGE SKIN PANEL BETWEEN FR63 & FR64 & BETWEEN S41R & S42R. REPAIRED FUSELAGE SKIN PANEL BETWEEN FR63 & FR64 & BETWEEN S41R & S42R IAW EA 500475.May 30, 2012 · N741UW · Airbus A319112 · Fuselage Main, Plate/SkinSDR USAA2012062200008Skin · corroded2S CHECK - CORROSION ON FUSELAGE SKIN BETWEEN FR63 TO FR64 & BETWEEN S41L TO S42L. REPAIRED FUSELAGE SKIN BETWEEN FR63 TO FR64 & BETWEEN S41L TO S42L IAW EA 500746.May 30, 2012 · N741UW · Airbus A319112 · Fuselage Main, Plate/SkinSDR USAA2012062500026Slat · missing2S CHECK - MISSING MATERIAL ON LEFT WING LOWER EDGE AT SLAT TRACK 6 OF SLAT NR 2 AT WFX 7080.35. REPAIRED LEFT WING 2 SLAT AT LOWER EDGE AT SLAT TRACK 6 AT AT WFX 7080.35 IAW EA 500747.May 29, 2012 · N741UW · Airbus A319112 · Leading Edge DevicesSDR USAA2012062000006Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR47/51 TO FR64, -Y765. REPLACE SEAT TRACK BETWEEN FR47/51 TO FR64, -Y765 IAW A319 SRM 51-72-11.May 29, 2012 · N741UW · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012062000005Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR41 TO FR47+51 INCHES, -Y1292. REPLACED SEAT TRACK BETWEEN FR41 TO FR47+51 INCHES, -Y1292 IAW A319 SRM 51-72-11.May 29, 2012 · N741UW · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012061900003Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT RAIL BETWEEN FR47/51 TO FR64 TO Y765. REPLACED SEAT RAIL BETWEEN FR47/51 TO FR64 TO Y765 IAW A319 SRM 51-72-11 & DRAWING D53476977.May 29, 2012 · N741UW · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012061800023Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR47/51 TO FR61+12 INCHES, Y1292. REPLACED SEAT TRACK BETWEEN FR47/51 TO FR61+12 INCHES, Y1292 IAW A319 SRM 51-72-11.May 29, 2012 · N741UW · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012061800022Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR47/51 TO FR35, -Y1292. REPLACED SEAT TRACK BETWEEN FR47/51 TO FR35, -Y1292 IAW A319 SRM 51-72-11.May 29, 2012 · N741UW · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012061800026Coupling · elongated2S CHECK - ELONGATED HOLE ON SEAT TRACK COUPLING AT FR64, Y1292. REPLACED SEAT TRACK AT FR64, Y1292 IAW A319 SRM 51-72-11.May 29, 2012 · N741UW · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012061800025Coupling · corroded2S CHECK - CORROSION ON SEAT TRACK COUPLING AT FR61 PLUS 12 INCHES, Y1292. REPAIRED SEAT TRACK BETWEEN FR61 TO FR64, Y1292 IAW A319 SRM 53-11-15 FIGURE 202.May 29, 2012 · N741UW · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012061800024Coupling · corroded2S CHECK - CORROSION ON SEAT TRACK COUPLING BETWEEN FR61TO FR64, -Y1292. REPLACED SEAT TRACK BETWEEN FR61 TO FR64, -Y1292 IAW A319 SRM 53-41-15, FIGURE 202, PAGE 215 AND 216.May 29, 2012 · N741UW · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012061500009Fitting · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON CENTER FITTING BETWEEN FR16 + 5 INCHES TO FR19 + 5 INCHES, S23R. REPLACED CENTER FITTING BETWEEN FR16 + 5 INCHES TO FR19 + 5 INCHES, S23R IAW A319 SRM 51-72-11 AND DRAWING D53112109.May 29, 2012 · N741UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012061200018Fitting · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FITTING BETWEEN FR16 TO FR20, S23L. REPLACED FITTING BETWEEN FR16 TO FR20, S23L IAW A319 SRM 51-72-11 AND DRAWING D53112109.May 29, 2012 · N741UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012060600012Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 232XG BETWEEN FR28 TO FR35 & BETWEEN -Y765 TO -Y254. REPLACED FLOOR PANEL 232XG IAW A319 SRM 53-02-00 & IRM 9701 REV G.May 29, 2012 · N741UW · Airbus A319112 · Fuselage Floor PanelSDR USAA2012060400010Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 231FF BETWEEN FR20 TO FR24 & BETWEEN Y1292 TO Y765. REPLACED FLOOR PANEL 231FF IAW A319 SRM 53-12-00 & IRM 9701 REV G.May 29, 2012 · N741UW · Airbus A319112 · Fuselage Floor PanelSDR USAA2012060400009Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 232MF BETWEEN FR24 TO FR28 & BETWEEN -Y1292 TO -Y765. REPLACED FLOOR PANEL 232MF IAW A319 SRM 53-02-00 & IRM 9701 REV G.May 29, 2012 · N741UW · Airbus A319112 · Fuselage Floor PanelSDR USAA2012062800004Splice · damaged2S CHECK - ELONGATED HOLE ON SPLICE AT FR24, S23R, -Y765. REPLACED SPLICE AT FR24, S23R, -Y765 IAW A319 SRM 51-72-11 AND AIRBUS DRAWING D53110920.May 28, 2012 · N741UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012062800003Angle · cracked2S CHECK - CRACK ON SEGMENT ANGLE OF LEFT AFT EMERGENCY EXIT DOOR (834) BETWEEN FR40 TO FR41, BEAM 1 TO BEAM 3. REPAIRED SEGMENT ANGLE OF LEFT AFT EMERGENCY EXIT DOOR (834) IAW EO 5210Y228.May 28, 2012 · N741UW · Airbus A319112 · Emergency ExitsSDR USAA2012062500033Sill · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON LOWER WEB SILL AT L2 ENTRY BETWEEN FR66 TO FR68, S23L. REPLACED LOWER WEB SILL AT L2 ENTRY BETWEEN FR66 TO FR68, S23L IAW A319 SRM 51-72-11 EA 500750.May 28, 2012 · N741UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012062200009Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR25 TO FR35, -Y1292. REPLACED SEAT TRACK BETWEEN FR25 TO FR35, -Y1292 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53233450.May 28, 2012 · N741UW · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012062200007Angle · cracked2S CHECK - CRACK IN EMERGENCY EXIT DOOR 844 FORWARD SEGMENT ANGLE BETWEEN FR40 TO FR41 & BETWEEN BEAM 1 TO BEAM 3. REPLACED EMERGENCY EXIT DOOR 844 FORWARD SEGMENT ANGLE IAW EO 5210Y228.May 28, 2012 · N741UW · Airbus A319112 · Emergency ExitsSDR USAA2012062100012Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK ASSEMBLY BETWEEN FR35 TO FR36, -Y1292. REPLACED SEAT TRACK ASSEMBLY BETWEEN FR35 TO FR36, -Y1292 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53374044.May 28, 2012 · N741UW · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012062000004Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR36 TO FR41, -Y1292. REPLACED SEAT TRACK BETWEEN FR36 TO FR41, -Y1292 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D57130300.May 28, 2012 · N741UW · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012061900005Fitting · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON CORNER FITTING AT FR68, S23L. REPLACED CORNER FITTING AT FR68, S23L IAW A319 SRM 51-72-11 & DRAWING D53480505.May 28, 2012 · N741UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012061800021Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR24 TO FR35, S23R, -Y765. REPLACED SEAT TRACK BETWEEN FR24 TO FR35, S23R, -Y765 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53233450.May 28, 2012 · N741UW · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012061400021Fitting · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SILL FITTING BETWEEN FR16 TO FR20, S23L. REPLACED CORNER FITTING BETWEEN FR16 TO FR20, S23L IAW A319 SRM 51-72-11, DRAWING D53112109.May 28, 2012 · N741UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012061400020Fitting · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON CORNER FITTING AT FR20, S23L. REPLACED CORNER FITTING AT FR20, S23L IAW A319 SRM 51-72-11 AND DRAWING D53112109.May 28, 2012 · N741UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012061400019Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR36 TO FR41, Y1292. REPLACED SEAT TRACK BETWEEN FR36 TO FR41, Y1292 IAW A319 SRM 51-72-11 AND DRAWING D57130300.May 28, 2012 · N741UW · Airbus A319112 · Fuselage, Seat/Cargo Attach Fittings
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