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 AALA201604089001Lens · unsecureAIRCRAFT WAS NOT GNDED. EMER ESCAPE PATH LIGHT LENS COVER AT 4C FELL OFF. REPLACED LENS COVER.Apr 7, 2016 · N770UW · Airbus A319112 · Emergency LightingSDR AALA201510299008Beam · crackedRIGHT SIDE BOX BEAM, UPPER FLANGE BACK TWO HOLES CRACKED AT FRAME 43 & -Y1650. REPAIRED IAW EO 6315Y066.Oct 28, 2015 · N770UW · Airbus A319112 · Fuselage Main, StructureSDR AALA201510299007Beam · crackedLEFT SIDE BOX BEAM, UPPER FLANGE BACK TWO HOLES CRACKED AT FRAME 43 & +Y1650. REPAIRED IAW EO 6315Y066.Oct 28, 2015 · N770UW · Airbus A319112 · Fuselage Main, StructureSDR AALA201509289016Stiffener · crackedKEEL BEAM MOD, VERTICAL STIFFENER IN RT MAIN WW, BETWEEN FRAME 41 & 41, AT Z-140 IS CRACKED. REPAIRED ANGLE IAW EO EO5313Y037.Sep 26, 2015 · N770UW · Airbus A319112 · Fuselage Main, KeelSDR AALA201504229007Bottle · low pressureR1 DOOR ASSIST BOTTLE LOW PRESSURE. SERVICED R1 DOOR ASSIST BOTTLE.Apr 20, 2015 · N770UW · Airbus A319112 · Service DoorsSDR USAA2015010900007Computer · faultyUNCOMMANDED NOSE DOWN ON APPROACH LEVEL FLIGHT. THEN SE THRUST NON-RESPONSIVE. DISCONNECT AUTO PILOT 1 & AUTO THRUST, MANUALLY FLOWN, NO ECAMS & NORMAL LANDING. REPLACED NR 1 ELAC IAW AMM 27-93-34-000-001 400-001-A.Jan 8, 2015 · N770UW · Airbus A319112 · Flight Control SystemSDR USAA2014092900006Ptu · unserviceableDURING PUSHBACK & ENG START, CREW RECEIVED A SEC 2 & SEC 3 FAULT. ECAM PROCEDURES CLEARED THESE FAULTS, THEN A LOUD GRINDING NOISE & BURNING SMELL FILLED CABIN. THEN THEY RECEIVED A HYD G RES OVHT ECAM MSG. FOLLOWED ECAM PROCEDURE & FAULT CLEARED SHORTLY. Sep 27, 2014 · N770UW · Airbus A319112 · Hydraulic System, AuxiliarySDR USAA2014072500002Indicator · faultedRECEIVED AN INFLIGHT ECAM MESSAGE. HYD G LOW RESERVOIR SCHEMATIC SHOWS A BLANK BELOW NORMAL QTY. ECAM & QRH PROCEDURES APPLIED. GREEN SYS BELOW BOX. DECLARED AN EMERGENCY & DIVERTED. FLIGHT LANDED WITHOUT INCIDENT & WAS TOWED TO THE GATE. AFTER LANDING, Jul 22, 2014 · N770UW · Airbus A319112 · Hydraulic Indicating SystemSDR USAA2014061200011Bottle · low pressureTHE R1 DOOR ASSIST BOTTLE HAS LOW PRESS. SERVICED ASSIST BOTTLE AT R1 DOOR IAW 52-10-00.Jun 11, 2014 · N770UW · Airbus A319112 · Passenger/Crew DoorsSDR USAA2014012100011Cover · missing3C EMERGENCY EXIT LIGHT COVER NEEDS REPLACING. REPLACED MISSING LENS COVER AS REQUIRED.Jan 18, 2014 · N770UW · Airbus A319112 · Emergency LightingSDR USAA2013082200004Floor Panel · delaminatedDURING 2S CHECK, DELAMINATION FOUND ON FLOOR PANEL 151ZG BETWEEN FR 56 TO 58 & BETWEEN S38L - S38R. REPLACED FLOOR PANEL IAW SRM 53-02-00, FIG 209.Aug 18, 2013 · N770UW · Airbus A319112 · Fuselage Floor PanelSDR USAA2013082200003Floor Panel · delaminatedDURING 2S CHECK, DELAMINATION FOUND ON FLOOR PANEL 151VG BETWEEN FR53 TO FR56 & BETWEEN S38L TO S38R. REPLACED FLOOR PANEL IAW SRM 53-02-00, FIG 209.Aug 18, 2013 · N770UW · Airbus A319112 · Fuselage Floor PanelSDR USAA2013082200002Floor Panel · delaminatedDURING 2S CHECK, DELAMINATION FOUND ON FLOOR PANEL 161BF BETWEEN FR 59 - 63 & BETWEEN S35-38L. REPLACED FLOOR PANEL IAW SRM 53-02-00, FIG 209.Aug 18, 2013 · N770UW · Airbus A319112 · Fuselage Floor PanelSDR USAA2013080900019Floor Panel · delaminatedDURING 2S CHECK, FOUND DELAMINATION ON FLOOR PANEL 232MF BETWEEN FR 24 TO 28 & -Y765 TO -Y1292. REPLACED FLOOR PANEL IAW SRM 53-02-00, FIG 209.Aug 9, 2013 · N770UW · Airbus A319112 · Fuselage Floor PanelSDR USAA2013080900018Floor Panel · delaminatedDURING 2S CHECK, FOUND DELAMINATION ON FLOOR PANEL NR 232LF BETWEEN FR 24 TO 28 & -Y254 TO Y765. REPLACED FLOOR PANEL IAW SRM 53-02-00, FIG 209.Aug 9, 2013 · N770UW · Airbus A319112 · Fuselage Floor PanelSDR USAA2013080700030Seat Track · corrodedDURING 2S CHECK, CORROSION WAS FOUND ON SEAT TRACK BETWEEN FR 44 TO 45, -Y1292. REPLACED SEAT TRACK IAW SRM 53-31-15, FIG 103, 51-21-11 & 51-42-11.Aug 6, 2013 · N770UW · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2013080700031Sill · corrodedDURING 2S CHECK, CORROSION WAS FOUND ON SILL BETWEEN FR 66 TO 69, -Y1732. REPLACED SILL IAW SRM 51-42-11 & 51-44-11.Aug 3, 2013 · N770UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2013082700002Floor Support · corroded2S CHECK - CORROSION FOUND ON FLOOR SUPPORT BETWEEN FR69 TO FR70, -Y160. REPLACED FLOOR SUPPORT IAW SRM 53-00-14, FIG 102 & 51-42-11.Aug 2, 2013 · N770UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2013080700034Floor Support · corrodedDURING 2S CHECK, CORROSION WAS FOUND ON LONGITUDINAL BEAM BETWEEN FR 69 TO 70, Y160. REPLACED LONGITUDINAL BEAM IAW SRM 53-00-14, FIG. 102 & 51-42-11.Aug 2, 2013 · N770UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2013080700033Floor Support · corrodedDURING 2S CHECK, CORROSION WAS FOUND ON LONGITUDINAL BEAM BETWEEN FR 66 TO 67, -Y318. REPLACED LONGITUDINAL BEAM IAW SRM 53-00-14, FIG. 102 & 51-42-11.Aug 2, 2013 · N770UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2013080700029Floor Support · corrodedDURING 2S CHECK, FOUND CORROSION ON FLOORBEAM BETWEEN FR 65 - 66, -Y465. REPLACED FLOOR SUPPORT IAW SRM 53-00-14, FIG. 102 & 51-42-11.Aug 2, 2013 · N770UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2013071600001Cylinder · low pressureMX REPORTED THE R-2 DOOR ASSIST PRESSURE LOW - NEEDS SERVICED. MX SERVICED R-2 DOOR EMERGENCY OPERATION CYLINDER TO CORRECT PRESSURE IAW AMM 52-10-00-614-001A.Jul 15, 2013 · N770UW · Airbus A319112 · Service DoorsSDR USAA2013041600003Lens · damagedMAINTENANCE REPORTED THE WALL MOUNTED "EXIT" LENS DAMAGED AT FRONT LEFT ENTRY DOOR AND AFT RIGHT SERVICE DOOR. MAINTENANCE REMOVED AND REPLACED WALL MOUNTED "EXIT" LENSES AT FRONT LEFT ENTRY DOOR AND AFT RIGHT SERVICE DOOR. CABIN EMERGENCY LIGHTING CHECKS GOApr 15, 2013 · N770UW · Airbus A319112 · Emergency LightingSDR USAA2013021300005Linkage · lack of lubeMAINTENANCE REPORTED THE L1 PASSENGER DOOR SLIDE ARMING HANDLE IS STIFF AND DIFFICULT TO OPERATE. MAINTENANCE CHECKED OPERATION OF L1 PASSENGER DOOR SLIDE ARMING HANDLE. LUBRICATED ARMING HANDLE LINKAGE. CHECKS OK. REFERENCE AMM 52-10-00-001.Feb 13, 2013 · N770UW · Airbus A319112 · Passenger/Crew DoorsSDR USAA2013020800024Connector · disconnectedMAINTENANCE REPORTED THE R2 DOOR OVERHEAD EMERGENCY EXIT SIGN INOP. MAINTENANCE FOUND ELECTRICAL CONNECTION BEHIND EXIT SIGN ASSEMBLY DISCONNECTED. RE-SECURED ELECTRICAL CONNECTION AND OPS CHECK GOOD IN REFERENCE AMM 33-51-17.Feb 8, 2013 · N770UW · Airbus A319112 · Light System WiringSDR USAA2013011600007Lens · missingMAINTENANCE REPORTED THE EMERGENCY LIGHT LENS MISSING ON SEAT 1C. MAINTENANCE REPLACED LIGHT LENS.Jan 16, 2013 · N770UW · Airbus A319112 · Emergency LightingSDR USAA2013010700012Strut · wornC9 CHECK - LEFT WING FLAP INTERCONNECT STRUT WORN AT Z581. REPLACED LEFT WING FLAP INTERCONNECT STRUT AT Z581 IAW A319 AMM 27-51-44-000-001-A.Jan 6, 2013 · N770UW · Airbus A319112 · Trailing Edge FlapsSDR USAA2013010700018Plate · out of adjustMAINTENANCE REPORTED THE RIGHT OVERWING SLIDE BALL LOCKS PAINTED OVER AND LOWER STAINLESS PLATE IS OUT OF POSITION. MAINTENANCE REMOVED PAINT ON RIGHT OVERWING SLIDE BALL LOCKS PER SRM 51-75-11 AND ADJUSTED STAINLESS PLATE ON SLIDE AS REQUIRED.Jan 4, 2013 · N770UW · Airbus A319112 · Escape SlideSDR USAA2012112600005Diaphragm · leakingC11 CHECK - L2 DOOR ASSIST BOTTLE LEAKING. REMOVED AND REPLACED L-2 DOOR ASSIST BOTTLE DIAPHRAGM SERVICED & LEAK CHECK GOOD, ALL WORK DONE IAW A319 AMM 52-10-00-610-001-A.Nov 24, 2012 · N770UW · Airbus A319112 · Passenger/Crew DoorsSDR USAA2012112600020Floor Support · corrodedC11 CHECK - FLOOR SUPPORT CORRODED BETWEEN FR 20 AND FR 21 AT Y 254. REMOVED AND REPLACED SUPPORT IAW A319 SRM 51-42-11, PARAGRAPHS 7B & 7D, FIGURES 12 & 20.2.Nov 15, 2012 · N770UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012112600051Floor Support · corrodedC11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOOR SUPPORT AT FR20, -Y254. REPLACED FLOOR SUPPORT AT FR20, -Y254 IAW A319 SRM 51-42-11 FIG 105 & 51-42-11 PARA 7D , FIG 20 & 7B FIG 12.Nov 14, 2012 · N770UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012112600041Seat Track · corrodedC11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SEAT TRACK ASSEMBLY BETWEEN FR18 TO FR20, -Y1292. REPLACED SEAT TRACK ASSEMBLY BETWEEN FR18 TO FR20, -Y1292 IAW A319 SRM 51-42-11 PARA 7B+D, FIG 12 & FIG 20.Nov 14, 2012 · N770UW · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012112600040Seat Track · corrodedC11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SEAT TRACK AT FR20, -Y765. REPLACED SEAT TRACK AT FR20, -Y765 IAW A319 SRM 51-42-11 PARA 7D, FIG 20 & 7B & FIG 12.Nov 14, 2012 · N770UW · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012112600026Floorbeam · corrodedC11 CHECK - FLOORBEAM CORRODED BETWEEN FR 66 AND FR 70 AT Y 765. REMOVED AND REPLACED BEAM IAW A319 SRM 51-72-11, P1-2 & AMM 20-21-11-0201.Nov 14, 2012 · N770UW · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012112600025Attach Angle · corrodedC11 CHECK - FLOORBEAM ATTACH ANGLE CORRODED AT FR 20 & Y -1875. REMOVED AND REPLACED ANGLE IAW A319 SRM 51-42-11, FIGURES 2, 4 & 8.Nov 14, 2012 · N770UW · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012111400002Lens · crackedC11/SY6 CHECK - EXIT LIGHT LENS COVER ON RIGHT AFT DOOR IS CRACKED. REPLACED EXIT LIGHT LENS COVER ON RIGHT AFT DOOR IAW A319 AMM 25-23-45-000-004 AND 25-23-45-400-005.Nov 12, 2012 · N770UW · Airbus A319112 · Emergency LightingSDR USAA2012112600050Fitting · corrodedC11 CHECK - LEVEL 2 FILIFORM CORROSION ON L2 AFT CORNER SILL FITTING AT FR66, Y1732. REPLACED L2 AFT CORNER SILL FITTING AT FR66, Y1732 IAW A319 SRM 51-42-11 FIGS 3, 4, 8 & 12.Nov 10, 2012 · N770UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012112600049Sill · corrodedC11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON L2 DOOR SILL BETWEEN FR66 TO FR68, Y1732. REPLACED L2 DOOR SILL BETWEEN FR66 TO FR68, Y1732 IAW A319 SRM 51-42-11 PAR 6 & 7, FIG 9 & 10.Nov 10, 2012 · N770UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012112600048Sill · corrodedC11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON R2 DOOR SILL AT FR66, -Y1732. REPLACED R2 DOOR SILL AT FR66, -Y1732 IAW A319 SRM 51-42-11 PAR 6 & 7, FIG 9 & 10.Nov 10, 2012 · N770UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA2012112600047Floorbeam · corrodedC11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR64 TO FR66, Y1292. REPLACED FLOORBEAM BETWEEN FR64 TO FR66, Y1292 IAW A319 SRM 53-00-14 FIG 102, 51-72-11 & 51-49-00 TABLE II.Nov 10, 2012 · N770UW · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012112600046Floorbeam · corrodedC11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR66 TO FR68, -Y1292. REPLACED FLOORBEAM BETWEEN FR66 TO FR68, -Y1292 IAW A319 SRM 51-42-11 FIG 20, 51-72-11 & 51-49-00 TABLE II.Nov 10, 2012 · N770UW · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012112600045Floorbeam · corrodedC11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR66 TO FR68, Y1292. REPLACED FLOORBEAM BETWEEN FR66 TO FR68, Y1292 IAW A319 SRM 51-42-11 FIG 20, 51-72-11 & 51-49-00 TABLE II.Nov 10, 2012 · N770UW · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012112600044Floorbeam · corrodedC11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR68 TO FR69, -Y1292. REPLACED FLOORBEAM BETWEEN FR68 TO FR69, -Y1292 IAW A319 SRM 51-42-11 FIG 20, 51-72-11 & 51-49-00 TABLE II.Nov 10, 2012 · N770UW · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012112600043Floorbeam · corrodedC11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR68 TO FR69, Y1292. REPLACED FLOORBEAM BETWEEN FR68 TO FR69, Y1292 IAW A319 SRM 51-42-11 FIG 20, 51-72-11 & 51-49-00 TABLE II.Nov 10, 2012 · N770UW · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012112600038Seat Track · corrodedC11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SEAT RAIL BEAM ASSEMBLY BETWEEN FR64 TO FR66, -Y765. REPLACED SEAT RAIL BEAM ASSEMBLY BETWEEN FR64 TO FR66, -Y765 IAW A319 SRM 51-42-11 PAR 7D, FIG 20.Nov 10, 2012 · N770UW · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012112600037Seat Track · corrodedC11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SEAT RAIL BEAM BETWEEN FR64 TO FR66, -Y1292. REPLACED SEAT RAIL BEAM BETWEEN FR64 TO FR66, -Y1292 IAW A319 SRM 51-42-11 FIG 20, 51-72-11 & 51-49-00 TABLE II.Nov 10, 2012 · N770UW · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012112600036Floorbeam · corrodedC11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR64 TO FR66, Y765. REPLACED FLOORBEAM BETWEEN FR64 TO FR66, Y765 IAW A319 SRM 51-42-11 PAR 7D, FIG 20,10,11,12.Nov 10, 2012 · N770UW · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012112600029Floor Panel · delaminatedC11 CHECK - FLOOR PANEL DELAMINATED BETWEEN FR 24 AND FR 28 AT Y -1732. REMOVED AND REPLACED PANEL IAW A319 AMM 53-22-12-0401 AND A319 AMM 53-22-12-400-001-A.Nov 10, 2012 · N770UW · Airbus A319112 · Fuselage Floor PanelSDR USAA2012112600021Floorbeam · corrodedC11 CHECK - FLOORBEAM CORRODED BETWEEN FR 66 & FR 70 AT Y -765. REMOVED AND REPLACED BEAM IAW A319 SRM 51-72-11, PARAGRAPH 6 AND AMM 20-21-11-0201.Nov 10, 2012 · N770UW · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA2012112600030Floor Panel · corrodedC11 CHECK - FLOOR PANEL 261FF CORRODED. REMOVED AND REPLACED PANEL IAW JOB CARD 26C26053014.Nov 9, 2012 · N770UW · Airbus A319112 · Fuselage Floor Panel
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