N770UW

Service difficulty reports · 288

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 = 'N770UW' 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 USAA2012112600022Floor Panel · corrodedC11 CHECK - FLOOR PANEL CORRODED AT FR 67 & Y 1732. REMOVED AND REPLACED PANEL IAW JOB CARD 26C26053014.Nov 9, 2012 · N770UW · Airbus A319112 · Fuselage Floor PanelSDR USAA2012112600055Floor Panel · delaminatedC11 CHECK - DELAMINATION ON FLOOR PANEL 261DF BETWEEN FR66 TO FR67, Y=0. REPLACED FLOOR PANEL 261DF IAW MCGILL CORP IRM 9701 REV G.Nov 9, 2012 · N770UW · Airbus A319112 · Fuselage Floor PanelSDR USAA2012112600054Floor Panel · delaminatedC11 CHECK - DELAMINATION ON FLOOR PANEL 222EF BETWEEN FR16 TO FR20 & BETWEEN -Y1292 TO -Y765. REPLACED FLOOR PANEL 222EF IAW JOB CARD 26C22053001.Nov 9, 2012 · N770UW · Airbus A319112 · Fuselage Floor PanelSDR USAA2012112600053Floor Panel · delaminatedC11 CHECK - DELAMINATION ON FLOOR PANEL 261AG BETWEEN FR64 TO FR66 & BETWEEN -Y254 TO Y254. REPLACED FLOOR PANEL 261AG IAW JOB CARD 26C26053001.Nov 9, 2012 · N770UW · Airbus A319112 · Fuselage Floor PanelSDR USAA2012112600052Floor Panel · delaminatedC11 CHECK - DELAMINATION ON FLOOR PANEL 221EF BETWEEN FR16 TO FR20 & BETWEEN Y1292 TO Y765. REPLACED FLOOR PANEL 221EF IAW JOB CARD 26C22053001.Nov 9, 2012 · N770UW · Airbus A319112 · Fuselage Floor PanelSDR USAA2012112600042Seat Track · corrodedC11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SEAT TRACK ASSEMBLY AT FR16, Y503.2. REPLACED SEAT TRACK ASSEMBLY AT FR16, Y503.2 IAW A319 SRM 51-42-11 PARA 7, FIGS 12-20.Nov 9, 2012 · N770UW · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012112600039Seat Track · corrodedC11 CHECK - LEVEL 2 FILIFORM CORROSION ON SEAT TRACK ASSEMBLY AT FR20, Y1292. REPLACED SEAT TRACK ASSEMBLY AT FR20, Y1292 IAW A319 SRM 51-42-11 FIG 12, 53-11-13 FIG 104.Nov 9, 2012 · N770UW · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012112600032Floor Panel · delaminatedC11 CHECK - FLOOR PANEL DELAMINATED AT FR 21 AND Y -765. REMOVED AND REPLACED PANEL IAW JOB CARD 26C22053014.Nov 9, 2012 · N770UW · Airbus A319112 · Fuselage Floor PanelSDR USAA2012112600031Floor Panel · delaminatedC11 CHECK - FLOOR PANEL DELAMINATED BETWEEN FR 14 AND FR 20 FROM Y 765 TO Y 1292. REMOVED AND REPLACED PANEL IAW MC GILL IRM 9701.Nov 9, 2012 · N770UW · Airbus A319112 · Fuselage Floor PanelSDR USAA2012112600028Floor Panel · delaminatedC11 CHECK - FLOOR PANEL DELAMINATED BETWEEN FR 64 AND FR 66 FROM Y -254 TO Y 254. REMOVED AND REPLACED PANEL IAW JOB CARD 26C26053014.Nov 9, 2012 · N770UW · Airbus A319112 · Fuselage Floor PanelSDR USAA2012112600027Floor Panel · delaminatedC11 FLOOR PANEL DELAMINATED BETWEEN FR 20 & FR 24 FROM Y 265 TO Y 765. REMOVED AND REPLACED PANEL IAW T/C 26C22053014, MC GILL IRM 9701.Nov 9, 2012 · N770UW · Airbus A319112 · Fuselage Floor PanelSDR USAA2012112600024Floor Panel · delaminatedC11 CHECK - FLOOR PANEL DELAMINATED BETWEEN FR 16 & FR 21 FROM Y -254 TO Y 254. REMOVED AND REPLACED PANEL IAW T/C 26C22053014 AND MC GILL IRM 9701.Nov 9, 2012 · N770UW · Airbus A319112 · Fuselage Floor PanelSDR USAA2012112600023Floor Panel · delaminatedC11 CHECK - FLOOR PANEL DELAMINATED BETWEEN FR 20 & FR 21 FROM Y 1292 TO Y 1732. REMOVED AND REPLACED PANEL IAW TASK CARD 26C22053014.Nov 9, 2012 · N770UW · Airbus A319112 · Fuselage Floor PanelSDR USAA2012112600019Floor Panel · delaminatedC11 CHECK - FLOOR PANEL AT FR 22 AND Y 0 IS DELAMINATED. REMOVED AND REPLACED PANEL IAW JOB CARD 26C22053014.Nov 9, 2012 · N770UW · Airbus A319112 · Fuselage Floor PanelSDR USAA2012112600018Floor Panel · delaminatedC11 CHECK - FLOOR PANEL AT FR 22 AND BL 0 DELAMINATED. REMOVED AND REPLACED PANEL IAW JOB CARD 26C22053014.Nov 9, 2012 · N770UW · Airbus A319112 · Fuselage Floor PanelSDR USAA2012111900022Floor Panel · delaminatedC11 CHECK - DELAMINATION ON FLOOR PANEL 261BG AT FR66, -Y1732. REPLACED FLOOR PANEL 261BG IAW JOB CARD 26C26053014.Nov 9, 2012 · N770UW · Airbus A319112 · Fuselage Floor PanelSDR USAA2012111900021Floor Panel · delaminatedC11 CHECK - DELAMINATION ON FLOOR PANEL 262EF BETWEEN FR66 TO FR68, -Y1732. REPLACED FLOOR PANEL 262EF IAW JOB CARD 26C26053014.Nov 9, 2012 · N770UW · Airbus A319112 · Fuselage Floor PanelSDR USAA2012111900020Floor Panel · delaminatedC11 CHECK - DELAMINATION ON FLOOR PANEL 261EF BETWEEN FR66 TO FR68, Y1732. REPLACED FLOOR PANEL 261EF IAW JOB CARD 26C26053014.Nov 9, 2012 · N770UW · Airbus A319112 · Fuselage Floor PanelSDR USAA2012092400027Lens · missingLENS MISSING ON L2 DOOR EXIT SIGN, AFT OF DOOR. REPLACED MISSING LENS ON L2 DOOR PER AMM 33-51-13-401.Sep 21, 2012 · N770UW · Airbus A319112 · Emergency LightingSDR USAA2012020200012Cylinder · low pressureR1 DOOR PRESSURE ACCUMULATOR LOW. SERVICED R1 DOOR ACCUMULATOR TO REQUIRED LIMITS (1800 PSI).Jan 31, 2012 · N770UW · Airbus A319112 · Service DoorsSDR USAA2010122793246Sleeve · damagedFLT 819 CLT-GCM - ODOR - STRONG CHEMICAL ACID ODOR REPORTED PRIOR TO LANDING FROM FIRST CLASS THROUGH ROW 19. FLIGHT ATTENDANT REPORTED IT WAS VERY DIFFICULT TO BREATHE. MAINTENANCE FOUND DAMAGED DUCT SLEEVE IN RT PACK BAY. REPLACED SLEEVE.Dec 26, 2010 · N770UW · Airbus A320214 · Air Distribution SystemSDR USAA2010122793243Ballast · faultyFLT 1521 CLT-DEN - BURNING SMELL - STRONG ODOR PERMEATED ENTIRE AIRCRAFT FROM TIME GEAR WAS LOWERED UNTIL CLEARED THE RUNWAY. COCKPIT CREW NOTICED ODOR WHICH WAS LATER REPORTED BY FORWARD AND AFT FLIGHT ATTENDANTS. ODOR EVENTUALLY DISSIPATED FOUR MINUTES AFTDec 23, 2010 · N770UW · Airbus A320214 · Passenger Compartment LightingSDR USAA2010111592603Bottle · low pressureFLT 787 - CLT-ATL - EMERGENCY EGRESS SYSTEM - DOOR ASSIST BOTTLE FOR R1 DOOR LOW. SERVICED DOOR ASSIST BOTTLE PER AMM 52-10-0-001.Nov 14, 2010 · N770UW · Airbus A320214 · Service DoorsSDR USAA2009112093181Pin · crackedDCA - C6 - MAJOR REPAIR - NOSE LANDING GEAR TORQUE LINK APEX PIN HAS A CRACK INDICATION. REPLACED NOSE LANDING GEAR TORQUE LINK APEX PIN IAW JOB CARD 26C71032003.Nov 17, 2009 · N770UW · Airbus A319112 · Nose/Tail Landing Gear Strut/AxleSDR USAA2009083192298Lens · missingFLT 1471 - PVD-CLT - EMERGENCY LIGHTS - SEAT 3C NEEDS EMERGENCY LIGHT LENS. REPLACED EMERGENCY LIGHT LENS AT SEAT 3C.Aug 30, 2009 · N770UW · Airbus A320214 · Emergency LightingSDR USAA2009051891198Lens · missingLOGPAGE:8419131 - FLT 976 - SMF-PHL - EMERGENCY LIGHTS - EXIT ROW 10C MISSING EMERGENCY LIGHT LENS. REPLACED MISSING EMERGENCY LIGHT LENS COVER ROW 10C.May 16, 2009 · N770UW · Airbus A320214 · Emergency LightingSDR USAA920081515Battery · dischargedFLT 1231 PHL-TPA - EMERGENCY EQUIPMENT - CENTER EMERGENCY LIGHT BATTERY LOW POWER. MAINTENANCE REMOVED AND REPLACED CENTER EMERGENCY LIGHT BATTERY. OPERATIONAL CHECK WAS GOOD. (S)Aug 13, 2008 · N770UW · Airbus A319112 · Emergency LightingSDR USAA061403Floorbeam · corrodedFLOORBEAM AT FRAME 17 Y50 CORRODED. DEFECTIVE PART REPLACED WITH IDENTICAL PART. CORR TASK JA-220-53500; LEVEL 1, DEFECT SIZE: 1 X 1 INCH.Dec 7, 2006 · N770UW · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA061402Floor Support · corrodedFLOOR SUPPORT SEGMENT FRAME 66-68 Y1162/-Y1292 CORRODED. DEFECTIVE PART REPLACED WITH IDENT PART. CORR TASK JA-260-53500; LEVEL 1, DEFECT SIZE: 1 X 1 INCH.Dec 7, 2006 · N770UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA061378Floorbeam · corrodedFLOORBEAM AT FRAME 16 Y50 HAS CORROSION. DEFECTIVE PART REPLACED WITH IDENTICAL PART. CORR TASK JA-220-53500, LEVEL 1, DEFECT SIZE: 1 X 1 INCH.Dec 1, 2006 · N770UW · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA061379Floorbeam · crackedY254 AT FRAME 20 CRACKED. DEFECTIVE PART REPLACED WITH IDENTICAL PART. REMOVED AND REPLACED FLOORBEAM PER SRM 51-72-11, DEFECT SIZE: .5 INCH LONG.Dec 1, 2006 · N770UW · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA061380Shear Web · corrodedBETWEEN FR 69 & 70 AT Y1162 CORROSION. REMOVED & REPLACED SHEAR WEB PER SRM 51-72-11; CORR TASK JA-260-53500, LEVEL 1, DEFECT SIZE: 1 INCH AT 5 MOUNT HOLES.Dec 1, 2006 · N770UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA061381Floorbeam · corrodedFLOORBEAM 500 + OF FR 16 HAS CORROSION. REMOVED & REPLACED FLOORBEAM PER SRM 51-72-11; CORR TASK JA-220-53500; LEVEL 1, DEFECT SIZE: 1 X 6 INCHES.Dec 1, 2006 · N770UW · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA061382Floorbeam · corrodedY254 AT FLOORBEAM 16 CORRODED. REMOVED AND REPLACED FLOORBEAM PER SRM 51-72-11; CORR TASK JA-220-53500, DEFECT SIZE: 2 INCH SQ.Dec 1, 2006 · N770UW · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA061383Frame · corrodedFRAME 66 LEFT SIDE AT NUT CLIP HOLE HAS CORROSION. REMOVED & REPLACED WITH IDENTICAL PART PER SRM 53-41-14, FIG 201, DEFECT SIZE: .5 X .5 X .040 INCH DEEP.Dec 1, 2006 · N770UW · Airbus A319112 · Fuselage Main, FrameSDR USAA061365Floor Support · corrodedFLOOR SUPPORT SEGMENT FRAME 66-68 - Y1162/-Y1292 HAS CORROSION. DEFECTIVE PART REPLACED WITH IDENTICAL PART; CORR TASK JA-60-53500, LEVEL 1, DEFECT SIZE: 1 X 1 INCH.Nov 29, 2006 · N770UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR SA05066Windshield · crackedAT FL 380, F/O WINDSHIELD STARTED CRACKING FROM SEVEN O'CLOCK POSITION TO TWO O'CLOCK POSITION. FLIGHT CREW COMPLIED WITH QRH PROCEDURES AND PULLED WINDOW HEAT CIRCUIT BREAKER. FLIGHT DIVERTED AND LANDED WITHOUT FURTHER INCIDENT. MX REMOVED AND REPLACED F/O Jun 6, 2005 · N770UW · Airbus A319112 · Flight Compartment WindowsSDR USAASA02030Power Supply · inoperativePHL - THE FORWARD AIRCRAFT EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE LEFT FORWARD EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKED OK. (M)Mar 24, 2002 · N770UW · Airbus A319112 · Emergency Lighting
Back to N770UW