N749US

Service difficulty reports · 238

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 = 'N749US' 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 USAA2014041000007Light · inoperativeREPORTED THE FWD WALL MOUNTED EMERGENCY EXIT LOCATION LIGHT RED INOPERATIVE. RELAMPED FWD WALL MOUNTED EMERGENCY EXIT LOCATION LIGHT RED IAW AMM SUBTASK 33-51-18-420-052.Apr 9, 2014 · N749US · Airbus A319112 · Emergency LightingSDR USAA2014033100004Nut Plate · failedFLIGHT ATTENDANT REPORTED A STRONG HIGH PITCHED SOUND AROUND ROW 2. FLIGHT DIVERTED TO PHL & LANDED WITHOUT INCIDENT. FOUND A BAD DOME NUTPLATE AT FIRST OFFICER'S AOA. R & R BAD DOME NUTPLATE & ACCOMPLISHED ACFT PRESSURIZATION TEST. NO LEAKS NOTED, ACFT OKMar 29, 2014 · N749US · Airbus A319112 · Stall Warning SystemSDR USAA2014013000005Cover · missingCOVER MISSING AT EMERGENCY LIGHT, ACFT LT, OVERWING EXIT. REPLACED COVER, ACFT OK FOR CONTINUED SERVICE.Jan 29, 2014 · N749US · Airbus A319112 · Emergency LightingSDR USAA2013102400007Rectifier · faultyCREW REPORTED A TR 2 FAULT -STRONG ELECTRICAL ODOR. MAINTENANCE R & R TR 2 IAW AMM 24-32-51-400-001. ALSO, R & R CONTACTOR 14 PU IAW AMM 24-42-55-000-001 AND 7XX RELAY. SYS TESTED OK.Oct 23, 2013 · N749US · Airbus A319112 · DC Rectifier/ConverterSDR USAA2013072900040Priority Valve · leakingAFTER DEPARTURE, CREW REPORTED YELLOW HYD QTY WENT TO ZERO. FOLLOWED QRH PROCEDURES AND CONTINUED TO DESTINATION. DECLARED AN EMERGENCY. LANDED WITHOUT INCIDENT AND TAXIED TO THE GATE. MAINTENANCE R & R YELLOW HYD SYS PRIORITY VALVE IAW AMM 29-13-33-000-0Jul 26, 2013 · N749US · Airbus A319112 · Hydraulic System, MainSDR USAA2013051500019Bearing · lack of lubeCREW REPORTED THE FORWARD ENTRY DOOR NEEDS ADJUSTMENT - VERY HARD TO CLOSE. MAINTENANCE LUBRICATED HINGE ARM SUPPORT FITTING BEARINGS PER AMM 12-22-52-640-016A. OPS CHECK NORMAL. OK FOR SERVICE.May 14, 2013 · N749US · Airbus A319112 · Passenger/Crew DoorsSDR USAA2012102900015Damper · discharged2S CHECK - DURING MAYOR CHECK ESCAPE SLIDE WAS DEPLOYED ACCIDENTLY AT L1 DOOR 831. REPLACED L1 DOOR 831 DAMPER CYLINDER IAW A319 AMM 52-11-14-400-001-B.Oct 26, 2012 · N749US · Airbus A319112 · Passenger/Crew DoorsSDR USAA2012102900014Slide · unwanted deploy2S CHECK - DURING MAYOR CHECK ESCAPE SLIDE WAS DEPLOYED ACCIDENTLY AT L1 DOOR 831. REPLACED L1 DOOR 831 ESCAPE SLIDE & OPS TESTED IAW A319 AMM 25-62-44-400-006-A.Oct 26, 2012 · N749US · Airbus A319112 · Escape SlideSDR USAA2012102900013Angle · cracked2S CHECK - CRACK INDICATION WAS FOUND IN THE EMERGENCY EXIT HATCH DOOR 834 SEGMENT BETWEEN FR40 TO FR41 & BETWEEN BEAM 1 & BEAM 3. REPLACED SEGMENT ANGLE FRAME AT EMERGENCY EXIT HATCH DOOR 834 IAW EO 5210Y228.Oct 25, 2012 · N749US · Airbus A319112 · Emergency ExitsSDR USAA2012102900012Angle · cracked2S CHECK - CRACK INDICATION WAS FOUND IN THE EMERGENCY EXIT HATCH DOOR 844 SEGMENT BETWEEN FR40 TO FR41 & BETWEEN BEAM 1 & BEAM 3. REPLACED SEGMENT ANGLE FRAME AT EMERGENCY EXIT HATCH DOOR 844 IAW EO 5210Y228.Oct 25, 2012 · N749US · Airbus A319112 · Emergency ExitsSDR USAA2012101600004Slide · low pressure2S CHECK - LOW PRESSURE IN RESERVOIR OF ESCAPE SLIDE AT DOOR 832 (L2). REPLACED ESCAPE SLIDE AT DOOR 832 (L2) IAW JOB CARD 26C83252008.Oct 15, 2012 · N749US · Airbus A319112 · Escape SlideSDR USAA2012101600003Slide · unserviceable2S CHECK - OVER PRESSURE IN RESERVOIR OF ESCAPE SLIDE ON DOOR 842 (R2). REPLACED ESCAPE SLIDE PACK ASSEMBLY ON DOOR 842 (R2) IAW JOB CARD 26C84252006.Oct 15, 2012 · N749US · Airbus A319112 · Escape SlideSDR USAA2012102500009Strut · corroded2S CHECK - CORROSION ON LEFT WING INTERCONNECTING STRUT BETWEEN WS 4067 TO WS 4862 & BETWEEN RIB 8 TO RIB 9. REPLACED LEFT WING INTERCONNECTING STRUT IAW A319 AMM 27-51-44-400-01-A.Oct 4, 2012 · N749US · Airbus A319112 · Trailing Edge FlapsSDR USAA2012102500008Strut · corroded2S CHECK - CORROSION ON RIGHT WING INTERCONNECTING STRUT BETWEEN WS 4067 TO WS 4862 & BETWEEN RIB 8 TO RIB 9. REPLACED RIGHT WING INTERCONNECTING STRUT IAW A319 AMM 27-51-44-400-01-A.Oct 4, 2012 · N749US · Airbus A319112 · Trailing Edge FlapsSDR USAA2012102200020Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK AT FR24+16 INCHES, S23R, -Y765. REPAIRED SEAT TRACK AT FR24+16 INCHES, S23R, -Y765 IAW A319 SRM 53-21-15 FIG 204 PAGES 239/240.Oct 3, 2012 · N749US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012102200019Splice · damaged2S CHECK - ELONGATED HOLE ON SEAT TRACK SPLICE AT FR24, S23R, -Y765. REPLACED SEAT TRACK SPLICE AT FR24, S23R, -Y765 IAW A319 SRM 51-72-11.Oct 3, 2012 · N749US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012101800013Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 251GF BETWEEN FR51 TO FR54 & BETWEEN Y765 TO Y254. REPLACED FLOOR PANEL 251GF IAW A319 SRM SUPPLEMENTAL INFORMATION 53-02-00-201 & IRM 9701 REV G SRM 53-12-00-201 FIG 209.Oct 1, 2012 · N749US · Airbus A319112 · Fuselage Floor PanelSDR USAA2012102200018Sill · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON CENTER SHAPE SILL BETWEEN FR66 TO FR68, S23L. REPLACED CENTER SHAPE SILL BETWEEN FR66 TO FR68, S23L IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53480505.Sep 30, 2012 · N749US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012101800012Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 212EF BETWEEN FR6 TO FR12 & BETWEEN -Y765 TO -Y254. REPLACED FLOOR PANEL 212EF IAW A319 SRM SUPPLEMENTAL INFORMATION 53-02-00-201, IRM 9701 REV G & SRM 53-12-00-201 FIG 206.Sep 30, 2012 · N749US · Airbus A319112 · Fuselage Floor PanelSDR USAA2012101800011Fitting · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON THE CENTER FITTING OF THE LEFT FORWARD DOOR THRESHOLD AREA BETWEEN FR16 TO FR20, S23R, -Y1732. REPLACED LEFT FORWARD DOOR THRESHOLD CENTER FITTING IAW A319 SRM 51-72-11.Sep 30, 2012 · N749US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012101800010Fitting · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON THE CENTER FITTING OF THE RIGHT FORWARD DOOR THRESHOLD AREA BETWEEN FR16 TO FR20, S23R, -Y1732. REPLACED RIGHT FORWARD DOOR THRESHOLD CENTER FITTING IAW A319 SRM 51-72-11.Sep 30, 2012 · N749US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012101500023Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 211EF BETWEEN FR6 TO FR9 & BETWEEN Y254 TO Y765. REPLACED FLOOR PANEL 211EF IAW A319 SRM SUPPLEMENTAL INFORMATION 53-02-00-201 & 53-12-00.Sep 30, 2012 · N749US · Airbus A319112 · Fuselage Floor PanelSDR USAA2012101500022Coupling · elongated2S CHECK - ELONGATED HOLE ON SEAT RAIL COUPLING AT FR64, -Y1292. REPLACED SEAT RAIL COUPLING AT FR64, -Y1292 IAW A319 SRM 51-72-11.Sep 30, 2012 · N749US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012101500021Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT RAIL BETWEEN FR47/51 TO FR64, -Y1292. REPLACED SEAT RAIL BETWEEN FR47/51 TO FR64, -Y1292 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53476977 & D53472831.Sep 30, 2012 · N749US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012101500024Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR36 TO FR42, -Y1292. REPLACED SEAT TRACK BETWEEN FR36 TO FR42, -Y1292 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53370500.Sep 29, 2012 · N749US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012103000009Angle · cracked2S CHECK - CRACK INDICATION WAS FOUND IN THE EMERGENCY EXIT HATCH DOOR 844 SEGMENT BETWEEN FR40 TO FR41 & BETWEEN BEAM 1 & BEAM 3. REPLACED SEGMENT ANGLE FRAME AT EMERGENCY EXIT HATCH DOOR 844 IAW EO 5210Y228.Sep 28, 2012 · N749US · Airbus A319112 · Emergency ExitsSDR USAA2012103000008Angle · cracked2S CHECK - CRACK INDICATION WAS FOUND IN THE EMERGENCY EXIT HATCH DOOR 834 SEGMENT BETWEEN FR40 TO FR41 & BETWEEN BEAM 1 & BEAM 3. REPLACED SEGMENT ANGLE FRAME AT EMERGENCY EXIT HATCH DOOR 834 IAW EO 5210Y228.Sep 28, 2012 · N749US · Airbus A319112 · Emergency ExitsSDR USAA2012102900005Flap · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON RIGHT OUTBOARD FLAP UPPER INTERNAL AREA OUTBOARD SIDE BETWEEN WS 10204 TO WS 10729 AT RIB 15. REPLACED RIGHT OUTBOARD FLAP IAW A319 AMM 27-54-62-400-001-A.Sep 28, 2012 · N749US · Airbus A319112 · Trailing Edge FlapsSDR USAA2012102500007Skin Panel · 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 503282.Sep 28, 2012 · N749US · Airbus A319112 · Fuselage Main, Plate/SkinSDR USAA2012101500026Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK AT FR29+12 INCHES, -Y1292. REPLACED SEAT TRACK AT FR29+12 INCHES, -Y1292 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53110920.Sep 28, 2012 · N749US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012101500025Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR24 TO FR35, -Y1292. REPLACED SEAT TRACK BETWEEN FR24 TO FR35, -Y1292 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53110920.Sep 28, 2012 · N749US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012101100006Floor Panel · delaminatedS2 CHECK - DELAMINATION ON FLOOR PANEL 151ZG BETWEEN FR59 TO FR55 BETWEEN Y765 TO -Y765. REPLACED FLOOR PANEL 151ZG IAW A319 SRM 53-02-00-201 FIG 209 & IRM 9701 REV G.Sep 27, 2012 · N749US · Airbus A319112 · Fuselage Floor PanelSDR USAA2012101700002Sill · corroded2S CHECK - REPLACING R1 DOOR LOWER SILL DUE TO PREVIOUS REWORK FOR CORROSION AT FR19+7.5 INCHES, S23R. REPLACED R1 DOOR LOWER SILL BETWEEN FR16 TO FR20, S23R, -Y1732 IAW A319 SRM 51-72-11.Sep 23, 2012 · N749US · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012081000010Servo · malfunctionedRUDDER RANDOMLY AND BRIEFLY KICKS RIGHT YAWING THE AIRCRAFT NOTICEABLY. REMOVED AND REPLACED YAW DAMPER ACTUATOR SERVO NR 1. PERFORMED SATISFACTORY CAT 3 AUTOLAND TEST IAW AMM 27-97-00-710-001.Aug 4, 2012 · N749US · Airbus A319112 · Autopilot SystemSDR USAA2012090400023Resistor · defectiveFLIGHT CREW REPORTED UNCOMMANDED RUDDER MOVEMENTS ON CLIMB, AT LEAST SIX TIMES, ON BOTH AUTO PILOTS 1 AND 2, IN LEVEL FLIGHT AND TURNS. DECLARED AN EMERGENCY AND RETURNED TO BOS. REMOVED AND REPLACED BOTH LEFT AND RIGHT FLIGHT AUGMENTATION COMPUTERS AND BOTHJul 17, 2012 · N749US · Airbus A319112 · Rudder Control SystemSDR USAA2012090400022Resistor · defectiveFLIGHT CREW REPORTED UNCOMMANDED RUDDER MOVEMENTS ON CLIMB, AT LEAST SIX TIMES, ON BOTH AUTO PILOTS 1 AND 2, IN LEVEL FLIGHT AND TURNS. DECLARED AN EMERGENCY AND RETURNED TO BOS. REMOVED AND REPLACED BOTH LEFT AND RIGHT FLIGHT AUGMENTATION COMPUTERS AND BOTHJul 17, 2012 · N749US · Airbus A319112 · Rudder Control SystemSDR USAA2012090400021Resistor · defectiveFLIGHT CREW REPORTED UNCOMMANDED RUDDER MOVEMENTS ON CLIMB, AT LEAST SIX TIMES, ON BOTH AUTO PILOTS 1 AND 2, IN LEVEL FLIGHT AND TURNS. DECLARED AN EMERGENCY AND RETURNED TO BOS. REMOVED AND REPLACED BOTH LEFT AND RIGHT FLIGHT AUGMENTATION COMPUTERS AND BOTHJul 17, 2012 · N749US · Airbus A319112 · Rudder Control SystemSDR USAA2012090400020Crystal · defectiveFLIGHT CREW REPORTED UNCOMMANDED RUDDER MOVEMENTS ON CLIMB, AT LEAST SIX TIMES, ON BOTH AUTO PILOTS 1 AND 2, IN LEVEL FLIGHT AND TURNS. DECLARED AN EMERGENCY AND RETURNED TO BOS. REMOVED AND REPLACED BOTH LEFT AND RIGHT FLIGHT AUGMENTATION COMPUTERS AND BOTHJul 17, 2012 · N749US · Airbus A319112 · Rudder Control SystemSDR USAA2012071800008Module · defectiveFLIGHT CREW REPORTED UNCOMMANDED RUDDER MOVEMENTS ON CLIMB, AT LEAST SIX TIMES, ON BOTH AUTO PILOTS 1 AND 2, IN LEVEL FLIGHT AND TURNS. DECLARED AN EMERGENCY AND RETURNED TO BOS. REMOVED AND REPLACED BOTH LEFT AND RIGHT FLIGHT AUGMENTATION COMPUTERS AND BOTHJul 17, 2012 · N749US · Airbus A319112 · Rudder Control SystemSDR USAA2012052900028Power Supply · faultyAFT EMERGENCY POWER SUPPLY UNIT (ESPU) FAULTING. REMOVED AND REPLACED AFT EMERGENCY POWER SUPPLY UNIT (ESPU) PER AMM 33-51-38 PB0401. OPS CHECKED GOOD.May 26, 2012 · N749US · Airbus A319112 · Emergency LightingSDR USAA2012040300007Strut · wornC9 CHECK - LEFT WING FLAP INTERCONNECTING STRUT HAS INTERNAL DAMAGE. NORMAL INSERVICE WEAR. FAILED WEAR CHECK. REPLACED LEFT WING FLAP INTERCONNECTING STRUT IAW A319 AMM 27-51-44.Apr 2, 2012 · N749US · Airbus A319112 · Wing Miscellaneous StructureSDR USAA2012020600002Door · out of adjustC11 CHECK - OUT ADJUSTMENT DIM B BETWEEN FINGER AND STRIKER LEVER AT DOOR 842 (R2). ADJUSTED DIM B BETWEEN FINGER AND STRIKER LEVER AT DOOR 842 (R2) IAW A319 AMM 52-13-14-820-002 PARAGRAPH 4, STEP A, ITEM 1.Feb 5, 2012 · N749US · Airbus A319112 · Service DoorsSDR USAA2012020300001Door · out of adjustC11 CHECK - OUT OF ADJUSTMENT DIM B(J1) BETWEEN FINGER AND STRIKER LEVER AT DOOR 841(R1). PERFORMED ADJUSTMENT OF DIM B (J1) BETWEEN FINGER AND STRIKER LEVER AT DOOR 841(R1) IAW A319 AMM 52-11-14-820-002 PARAGRAPH 4, ITEM A, STEP 1.Feb 2, 2012 · N749US · Airbus A319112 · Passenger/Crew DoorsSDR USAA2012020100017Seat Track · corrodedC11 CHECK - CORROSION ON SEAT TRACK AT FR24, -Y1292. REPAIRED SEAT TRACK BETWEEN FR24 TO FR27+11 INCHES, -Y1292 IAW A319 SRM 53-21-15 FIG 204.Jan 27, 2012 · N749US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012020300021Floor Panel · delaminatedC11 CHECK - DELAMINATION ON FLOOR PANEL 262BG BETWEEN FR64 TO FR66 & BETWEEN -Y1732 TO -Y254. REPLACED FLOOR PANEL 262BG IAW A319 SRM 53-02-00, IRM 9701 REV G & AIRWAYS EA 133857.Jan 26, 2012 · N749US · Airbus A319112 · Fuselage Floor PanelSDR USAA2012020200008Floor Panel · delaminatedC11 CHECK - DELAMINATION ON FLOOR PANEL 261PF BETWEEN FR68 TO FR70 & BETWEEN -Y1292 TO Y1292. REPLACED FLOOR PANEL 261PF IAW A320 SRM 53-02-00 & IRM 9701 REV G.Jan 26, 2012 · N749US · Airbus A319112 · Fuselage Floor PanelSDR USAA2012020200001Floor Panel · delaminatedC11 CHECK - DELAMINATION ON FLOOR PANEL 221EF BETWEEN FR16 TO FR20 & BETWEEN Y1292 TO Y254. REPLACED FLOOR PANEL 221EF IAW A319 SRM 53-12-00 & IRM 9701 REV G.Jan 26, 2012 · N749US · Airbus A319112 · Fuselage Floor PanelSDR USAA2012020100008Seat Track · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR12 TO FR24, -Y765. REPLACED SEAT TRACK BETWEEN FR12 TO FR24, -Y765 IAW A319 SRM 51-72-11, AIRBUS DRAWING # D53112812 & D53110920.Jan 26, 2012 · N749US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012013100017Dummy Rail · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON RAIL DUMMY BETWEEN FR12 TO FR16, -Y81. REPLACED RAIL DUMMY BETWEEN FR12 TO FR16, -Y81 IAW A319 SRM 51-72-11, AIRBUS DRAWING D53112828 & D53110984.Jan 26, 2012 · N749US · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012013100016Floor Support · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT BETWEEN FR12 TO FR24, Y254. REPLACED FLOOR SUPPORT BETWEEN FR12 TO FR24, Y254 IAW A319 SRM 51-72-11.Jan 26, 2012 · N749US · Airbus A319112 · Fuselage Miscellaneous Structure
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