N824AW

Service difficulty reports · 227

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 = 'N824AW' 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 USAA2013082900013Skin · contaminated2S CHECK - WATER INGRESS INDICATION ON RT ELEVATOR UPPER SKIN SURFACE APPROXIMATELY 102 INCHES FROM INBD END & 20.5 INCHES FROM T/E. REPAIRED ELEVATOR SKIN IAW SRM 55-21-11-C1-201, PARA 5.D & EA 250469.Aug 28, 2013 · N824AW · Airbus A319132 · Elevator, Plate/SkinSDR USAA2013082900012Skin · contaminated2S CHECK - WATER INGRESS INDICATION ON RT ELEVATOR UPPER SKIN SURFACE APPROXIMATELY 118 INCHES FROM INBD END & 11 INCHES FROM T/E. REPAIRED ELEVATOR SKIN SURFACE IAW SRM 55-21-11-C1-201, PARA 5.D & EA 250469.Aug 28, 2013 · N824AW · Airbus A319132 · Elevator, Plate/SkinSDR USAA2013082900011Skin · contaminated2S CHECK - WATER INGRESS INDICATION ON RT ELEVATOR UPPER SKIN SURFACE APPROX 44 INCHES FROM INBD END & 22 INCHES FROM T/E. REPAIRED ELEVATOR SKIN IAW SRM 55-21-11-C1-201, PARA 5.D & EA 250469.Aug 28, 2013 · N824AW · Airbus A319132 · Elevator, Plate/SkinSDR USAA2013082900010Skin · saturated2S CHECK - WATER INGRESS INDICATION ON RT ELEVATOR UPPER SKIN SURFACE APPROX 96 INCHES FROM INBD END & 22.5 INCHES FROM T/E. REPAIRED RT ELEVATOR UPPER SKIN SURFACE IAW SRM 55-21-11-C1-201, PARA. 5.D & EA 250469.Aug 28, 2013 · N824AW · Airbus A319132 · Elevator, Plate/SkinSDR USAA2013082900009Skin · contaminated2S CHECK - WATER INGRESS INDICATION ON RT ELEVATOR UPPER SKIN SURFACE APPROX 58 INCHES FROM INBD END & 10 INCHES FROM T/E. REPAIRED RT ELEVATOR UPPER SKIN SURFACE IAW SRM 55-21-11-C1-201, PARA 5.D & EA 250469.Aug 28, 2013 · N824AW · Airbus A319132 · Elevator, Plate/SkinSDR USAA2013082900008Skin · contaminated2S CHECK - WATER INGRESS INDICATION ON RT ELEVATOR UPPER SKIN SURFACE APPROX 110 INCHES FROM INBD END & 11 INHCES FROM T/E. REPAIRED RT ELEVATOR UPPER SKIN SURFACE IAW SRM 55-21-11-C1-201, PARA 5.D & EA 250469.Aug 28, 2013 · N824AW · Airbus A319132 · Elevator, Plate/SkinSDR USAA2013090300009Skin · saturated2S CHECK, INDICATION OF WATER ENGRESS ON LT ELEVATOR UPPER SURFACE APPROX 103" FROM OTBD END & 6" FROM T/E. REPAIRED LT ELEVATOR UPPER SURFACE IAW EA 205493.Aug 26, 2013 · N824AW · Airbus A319132 · Elevator, Plate/SkinSDR USAA2013090300008Skin · saturated2S CHECK, INDICATION OF WATER ENGRESS ON LT ELEVATOR UPPER SURFACE APPROX 90" FROM OTBD END & 9.5" FROM T/E. REPAIRED LT ELEVATOR UPPER SURFACE IAW EA 205493.Aug 26, 2013 · N824AW · Airbus A319132 · Elevator, Plate/SkinSDR USAA2013090300007Skin · saturated2S CHECK - PREVIOUS REPAIR SHOWS SIGNS OF WATER ENGRESS ON LT ELEVATOR UPPER SURFACE APPROX 38.5" FROM INBD END & 5.5" FROM T/E. REPAIRED LT ELEVATOR UPPER SURFACE IAW EA 205493.Aug 26, 2013 · N824AW · Airbus A319132 · Elevator, Plate/SkinSDR USAA2013082700020Floor Panel · delaminated2S CHECK - AREA OF DELAMINATION ON FLOOR PANEL 231CF BETWEEN FRAMES 20 TO 24, Z-500 & BETWEEN Y765 TO Y254. REPLACED FLOOR PANEL IAW IRM 9701, REV G.Aug 22, 2013 · N824AW · Airbus A319132 · Fuselage Floor PanelSDR USAA2013082300006Floor Panel · delaminatedDURING 2S CHECK, FOUND DELAMINATION ON FLOOR PANEL 262HG BETWEEN FRAMES 64 TO 66, Z-500 & -Y765 TO -Y1589. REPLACED FLOOR PANEL IAW IRM 9701, REV G.Aug 22, 2013 · N824AW · Airbus A319132 · Fuselage Floor PanelSDR USAA2013082300005Floor Panel · delaminatedDURING 2S CHECK, FOUND DELAMINATION ON FLOOR PANEL 241CF BETWEEN FRAMES 35.8 TO 36, Z-500 & -Y765 TO -Y1037. REPLACED FLOOR PANEL IAW IRM 9701, REV G.Aug 22, 2013 · N824AW · Airbus A319132 · Fuselage Floor PanelSDR USAA2013082300004Floor Panel · delaminatedDURING 2S CHECK, FOUND DELAMINATION ON FLOOR PANEL 222DF BETWEEN FRAMES 16 TO 20, Z-500 & -Y81 TO -Y503.2. REPLACED FLOOR PANEL IAW IRM 9701, REV. G.Aug 22, 2013 · N824AW · Airbus A319132 · Fuselage Floor PanelSDR USAA2013082300003Floor Panel · delaminatedDURING 2S CHECK, FOUND DELAMINATION ON FLOOR PANEL 222CF BETWEEN FRAMES 12 TO 16, Z-500 & -Y1379.5 TO -Y81. REPLACED FLOOR PANEL IAW IRM 9701, REV G.Aug 22, 2013 · N824AW · Airbus A319132 · Fuselage Floor PanelSDR USAA2013082000005Floor Panel · damagedDURING 2S CHECK, UPPER SURFACE OF FLOOR PANEL 221EF PEELING BETWEEN FR 16 TO 20, Z-500 & Y765 TO Y1265. REPLACED FLOOR PANEL IAW IRM 9701, REV G.Aug 17, 2013 · N824AW · Airbus A319132 · Fuselage Floor PanelSDR USAA2013080800028Sill · corrodedDURING 2S CHECK, FOUND CORROSION ON RT AFT ENTRYWAY AFT SHAPE SILL AT FR67, -Y1292. REPLACED SILL IAW SRM 53-41-69.Aug 7, 2013 · N824AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR USAA2013061400016Proximity Sensor · faultyAFTER LANDING AT FLAP RETRACTION, CREW RECIEVED ECAM MESSAGE F/CTL FLAPS LOCKED - ALIGNMENT FAULT. MX FOUND FIN 38CV FAULT. R & R FIN 38CV IAW AMM 27-51-44. ACCOMPLISHED ADJUSTMENT OF RT WING INTERCONNECT STRUT IAW AMM 27-51-44-802-001-A. FAULT CLEARED. OPSJun 12, 2013 · N824AW · Airbus A319132 · Trailing Flap Position Indicating SystemSDR USAA2013041800010Power Supply · failedMAINTENANCE REPORTED THE FORWARD CABIN EMERGENCY LIGHT POWER SUPPLY UNIT FAILED INTERNAL & EXTERNAL LOAD TESTS. MAINTENANCE REPLACED FORWARD CABIN EMERGENCY LIGHT POWER SUPPLY UNIT PER AMM 33-51-38, PB 0401. OPS CHECK GOOD.Apr 17, 2013 · N824AW · Airbus A319132 · Emergency LightingSDR USAA2013021800018Girt Bar · dirtyDOOR 2R ARMING HANDLE REPORTED BY CREW AS SPONGY AND DISARMS INTERMITTENTLY DURING FLIGHT. MAINTENANCE CLEANED AND INSPECTED R2 DOOR ARMED HANDLE AND GIRT MECHANISM. NO FAULTS NOTED. COMPLIED WITH OPERATIONAL CHECK. REFERENCE AMM 52-73-00-710-001 AND 52-71Feb 17, 2013 · N824AW · Airbus A319132 · Emergency EquipmentSDR USAA2013021100017Unknown · smokeAFTER LANDING, THE NR 1 FLIGHT ATTENDANT SMELLED AND SAW A THIN LAYER OF SMOKE NEAR ROW 1 (ELECTRICAL SMELL). MAINTENANCE COMPLIED WITH J/C 26L00021001 AND COULD NOT DUPLICATE ANY CABIN ODOR AT THIS TIME. DEACTIVATED AND PLACED AIRCELL ON MEL AS PRECAUTION. Feb 8, 2013 · N824AW · Airbus A319132 · Air Distribution SystemSDR USAA2013011400015Proximity Switch · out of adjustCREW REPORTED DOOR 2R NOT SHOWING ARMED ON ECAM UNLESS PRESSURE IS PUT ON ARMING HANDLE (DOOR SHOWED ARMED AT PUSH BACK). MAINTENANCE TROUBLESHOT 2R DOOR PER TSM 52-13-00-810-805-A. ADJUSTMENT OF THE PROXIMITY SWITCH WAS ACCOMPLISHED PER AMM 52-71-00-820-002Jan 13, 2013 · N824AW · Airbus A319132 · Door Warning SystemSDR USAA2013011400007Girt Bar · obstructedCREW REPORTED DOOR 2R NOT SHOWING ARMED ON ECAM UNLESS PRESSURE IS PUT ON HANDLE. CLEARED DEBRIS (BOTTLE CAP) FROM GIRT BAR AREA. ARMED AND DISARMED DOOR 2R. ECAM INDICATION SHOWS OK AT THIS TIME.Jan 12, 2013 · N824AW · Airbus A319132 · Emergency EquipmentSDR USAA2013011100003Lens · wrong partCREW REPORTS LAV D EMERGENCY LIGHT IS THE WRONG COLOR. MAINTENANCE INSTALLED CORRECT LENS.Jan 10, 2013 · N824AW · Airbus A319132 · Emergency LightingSDR USAA2013010700006Floorbeam · corrodedSY6 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR64 TO FR67, Y1292. REPLACED FLOORBEAM BETWEEN FR64 TO FR67, Y1292 IAW A319 SRM 53-00-14, FIG 102 & SRM 51-42-11.Jan 4, 2013 · N824AW · Airbus A319132 · Fuselage Main, Floor BeamSDR USAA2013010700005Sill · corrodedSY6 CHECK - LEVEL 2 GALVANIC CORROSION ON DOOR SILL AT FR66, Y1732. REPLACED DOOR SILL AT FR66, Y1732 IAW A319 SRM 53-41-14 FIG 101 & 53-41-14 FIG 201.Jan 3, 2013 · N824AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR USAA2013010300021Floor Panel · corrodedSY6 CHECK - CORROSION & DISBONDING ON FLOOR PANEL 222FF BETWEEN FR16 TO FR20 & -Y1732 TO -Y1292. REPLACED FLOOR PANEL 222FF IAW A319 AMM 53-12-12 & SRM 51-73-11.Jan 3, 2013 · N824AW · Airbus A319132 · Fuselage Floor PanelSDR USAA2013010300011Floorbeam · corrodedSY6 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR68 TO FR69, Y1292. REPLACED FLOORBEAM BETWEEN FR68 TO FR69, Y1292 IAW A319 SRM 51-42-11 & 51-75-12.Jan 2, 2013 · N824AW · Airbus A319132 · Fuselage Main, Floor BeamSDR USAA2013010300010Floorbeam · corrodedSY6 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66 TO FR68, -Y1292. REPLACED FLOORBEAM BETWEEN FR66 TO FR68, -Y1292 IAW A319 SRM 51-72-11, 53-00-14, FIG 102 & 51-74-00.Jan 2, 2013 · N824AW · Airbus A319132 · Fuselage Main, Floor BeamSDR USAA2013010300009Floorbeam · corrodedSY6 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR67 TO FR68, Y1292. REPLACED FLOORBEAM BETWEEN FR67 TO FR68, Y1292 IAW A319 SRM 51-42-11.Jan 2, 2013 · N824AW · Airbus A319132 · Fuselage Main, Floor BeamSDR USAA2013010300008Shear Plate · corrodedSY6 CHECK - LEVEL 2 GALVANIC CORROSION ON SHEAR PLATE BETWEEN FR69 TO FR70, S23R. REPLACED SHEAR PLATE BETWEEN FR69 TO FR70, S23R IAW A319 SRM 51-42-11 & 51-72-11.Jan 2, 2013 · N824AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR USAA2013010300007Shear Plate · corrodedSY6 CHECK - LEVEL 2 GALVANIC CORROSION ON SHEAR PLATE BETWEEN FR69 TO FR70, S23L. REPLACED SHEAR PLATE BETWEEN FR69 TO FR70, S23L IAW A319 SRM 51-72-11.Jan 2, 2013 · N824AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR USAA2013010300005Plate · crackedSY6 CHECK - CRACK ON WEB PLATE BETWEEN FR68 TO FR69, S23R. REPLACED WEB PLATE BETWEEN FR68 TO FR69, S23R IAW A319 SRM 51-42-11.Jan 2, 2013 · N824AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR USAA2013010300006Dummy Rail · corrodedSY6 CHECK - LEVEL 2 GALVANIC CORROSION ON DUMMY RAIL AT FR16-2 INCHES, Y503.2. REPLACED DUMMY RAIL AT FR16-2 INCHES, Y503.2 IAW A319 SRM 53-11-14 FIG 103 & 51-42-11.Dec 31, 2012 · N824AW · Airbus A319132 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012111900016Battery Pack · dischargedFORWARD LEFT FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK LEFT FORWARD FLASHLIGHT. OPS CHECKED GOOD.Nov 16, 2012 · N824AW · Airbus A319132 · Emergency EquipmentSDR USAA2012102600005Power Supply · inoperativeEMERGENCY LIGHTS FAIL TEST "EPSU INT LOAD AFT L". REMOVED AND REPLACED AFT LEFT (EPSU) EMERGENCY POWER SUPPLY UNIT PER AMM 33-58-30-401.Oct 25, 2012 · N824AW · Airbus A319132 · Emergency LightingSDR USAA2012072600007Battery · dischargedFORWARD MEGAPHONE INOPERATIVE. REPLACED FORWARD MEGAPHONE BATTERIES.Jul 24, 2012 · N824AW · Airbus A319132 · Emergency EquipmentSDR USAA2012030500010Cable · defectiveSEAT ROW 22ABC EMERGENCY SEAT MOUNTED LIGHT INOPERATIVE. REMOVED AND REPLACED SEAT CABLE 5409VB IAW TR320-3350-11-0541. OPS CHECKED GOOD PER AMM 33-51-00-501.Mar 2, 2012 · N824AW · Airbus A319132 · Light System WiringSDR USAA2011081900004Unknown · malfunctionedR1 DOOR DOES NOT SHOW SLIDE ARMED INDICATION ON ECAM WITH DOOR CLOSED & ARMED. PERFORMED OPS CHECK OF SLIDE INDICATION OF R1 DOOR. AIRBUS MAINTENANCE MANUAL 52-73-00-710-00. OPS CHECKED GOOD.Aug 18, 2011 · N824AW · Airbus A319132 · Escape SlideSDR USAA2010111992620Battery · dischargedFLT 634 - PHX-PIT - EEL - EMERGENCY EXIT LIGHTS 1L & 1R ARE NOT ILLUMINATING. MAINTENANCE REMOVED AND REPLACED FORWARD EMERGENCY LIGHT BATTERY IAW AIRBUS MAINTENANCE MANUAL 33-51-38.Nov 15, 2010 · N824AW · Airbus A319132 · Emergency LightingSDR USAA2010021090328Skin · contaminatedSAL - MAJOR REPAIR - C6 CHECK - RT ELEVATOR UPPER SKIN. TRAPPED WATER WAS FOUND IN HONEY COMB CORE STRUCTURE BETWEEN RIB 1 AND 4, STAB STA 227- STAB STA 271. REPAIRED RT ELEVATOR UPPER SKIN BETWEEN RIB 1 AND 4, STAB STA 227- STAB STA 271 IAW A319 SRM 51-77-1Feb 9, 2010 · N824AW · Airbus A319132 · Elevator, Plate/SkinSDR USAA2010021090327Skin · contaminatedSAL - MAJOR REPAIR - C6 CHECK - RT ELEVATOR UPPER SKIN. TRAPPED WATER WAS FOUND IN HONEY COMB CORE STRUCTURE BETWEEN RIB 1 AND 4, STAB STA 181- STAB STA 227. REPAIRED RT ELEVATOR. UPPER SKIN BETWEEN RIB 1 AND 4, STAB STA 181- STAB STA 227 IAW A319 SRM 51-77Feb 9, 2010 · N824AW · Airbus A319132 · Elevator, Plate/SkinSDR USAA2010020890305Damper · low pressureSAL - EES - C6 CHECK - R1 DOOR CYLINDER DOOR DAMPER PRESSURE LOW. SERVICED R1 DOOR CYLINDER DOOR DAMPER IAW A319 AMM 52-10-00-614-050.Feb 4, 2010 · N824AW · Airbus A319132 · Passenger/Crew DoorsSDR USAA2010020590283Damper · low pressureSAL - EES - C6 CHECK - L1 DOOR EMERGENCY CYLINDER DOOR DAMPER PRESSURE LOW. SERVICED THE L1 DOOR EMERGENCY CYLINDER DOOR DAMPER IAW A319 AMM 52-10-00.Feb 4, 2010 · N824AW · Airbus A319132 · Passenger/Crew DoorsSDR USAA2010020490276Striker · out of adjustSAL - EES - C6 CHECK - PASSENGER / CREW DOOR 842, DOOR DAMPER AND EMERGENCY OPERATION STRIKER FOUND TO BE OUT OF ADJUSTMENT. ADJUSTED THE PASSENGER / CREW DOOR 842, DOOR DAMPER AND EMERGENCY OPERATION STRIKER IAW A319 AMM 52-13-14.Jan 31, 2010 · N824AW · Airbus A319132 · Passenger/Crew DoorsSDR USAA2010020290258Striker · out of adjustSAL - C6 - EES - OUT OF ADJUSTMENT DIMENSION B BETWEEN FINGER & STRIKER AT AFT ENTRANCE DOOR DAMPER PERCUSSION BELL CRANK FINGER. PERFORMED ADJUSTMENT OF DIMENSION B BETWEEN FINGER & STRIKER AT AFT ENTRANCE DOOR DAMPER PERCUSSION BELL CRANK FINGER IAW A319 AMJan 30, 2010 · N824AW · Airbus A319132 · Passenger/Crew DoorsSDR USAA2010020290252Striker · out of adjustSAL - C6 - EES - OUT OF ADJUSTMENT DIMENSION B BETWEEN FINGER & STRIKER AT FORWARD ENTRANCE DOOR DAMPER PERCUSSION BELL CRANK FINGER. PERFORMED ADJUSTMENT OF DIMENSION B BETWEEN FINGER & STRIKER AT FORWARD ENTRANCE DOOR DAMPER PERCUSSION BELL CRANK FINGER IAWJan 30, 2010 · N824AW · Airbus A319132 · Passenger/Crew DoorsSDR USAA2010021290347Hinge Fitting · excess playSAL - C6 - MAJOR REPAIR - EXCESSIVE PLAY ON RUDDER HINGE FITTING NR 3 AT STAB STA 2279 / RIB 5. REPLACED RUDDER HINGE FITTING NR 3 AT STAB STA 2279 / RIB 5 IAW A319 AMM 27-21-00.Jan 28, 2010 · N824AW · Airbus A319132 · Rudder StructureSDR USAA2010020290260Damper · low pressureSAL - C6 - EES - LOW PRESSURE AT AFT ENTRY DOOR EMERGENCY CYLINDER DAMPER. CHARGED THE EMERGENCY CYLINDER DAMPER AT AFT ENTRY DOOR IAW A319 AMM 52-10-00.Jan 28, 2010 · N824AW · Airbus A319132 · Passenger/Crew DoorsSDR USAA2010020290259Damper · low pressureSAL - C6 - EES - LOW PRESSURE AT FORWARD SERVICE DOOR EMERGENCY CYLINDER DAMPER. CHARGED THE EMERGENCY CYLINDER DAMPER AT FORWARD SERVICE DOOR IAW A319 AMM 52-10-00-614-057.Jan 28, 2010 · N824AW · Airbus A319132 · Service DoorsSDR USAA2010021290346Elevator · contaminatedSAL - C6 - MAJOR REPAIR - TRAPPED WATER FOUND IN LEFT ELEVATOR UPPER SKIN BETWEEN STAB STA 181 TO STAB STA 404 BETWEEN ELEV RIB 3 TO ELEV RIB 6. REPAIRED ELEVATOR UPPER SKIN IAW A320 SRM 51-77-13.Jan 27, 2010 · N824AW · Airbus A319132 · Elevator, Plate/Skin
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