N442UA

Service difficulty reports · 120

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 = 'N442UA' 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 CALA2026072718042Light · damagedLIGHT ASSY-EMERGENCY AT SEAT 23C FOUND DAMAGED. REMOVED AND REPLACE EMERGENCY LIGHT ASSY AT SEAT 23C, OPS CHECK GOOD IAW AMM 33-51-19/401 CONFIG 00.Jul 25, 2026 · N442UA · Airbus A320232 · Emergency LightingSDR CALA2026060316770Fuel Cap · missingON ARRIVAL FUEL CAP MISSING INSTALLED UNDERWING FUEL CAP AND LANYARD ASSEMBLY REF AMM 28-45-21Jun 2, 2026 · N442UA · Airbus A320232 · Fuel StorageSDR CALA2026021813868Antenna · faultedWX RADAR R/T ON LOWER RIGHT OF ND WHEN WX RADAR TURNED ON AT TOP OF DESCENT, RADAR IN OPPOSITE, FLIGHT REPORT OPENED RADOME & CHECKED FOR WATER INTRUSION & DAMAGE. NO EVIDENCE OF ANY DAMAGE IAW AMM 53-15-991-00400-00-A. REPLACED THE WEATHER RADAR ANTENNA IAFeb 15, 2026 · N442UA · Airbus A320232 · Weather Radar SystemSDR CALA2026010912832Sign · inoperativeMULTIPLE EMERGENCY EXIT SIGNS AT 1L AND 1R, 2L AND 2R INOP. FOUND DOOR 2L OVERHEAD INOP, ALL OTHER EMERGENCY LIGHTS WORK NORMAL. REPLACED EXIT SIGN 45WL AT DOOR 2L, NO HELP. NOTICED, WHEN EMERGENCY LIGHTS SWITCH IS SELECTED TO ON POSITION, ALL EMERGENCY LIGHTSJan 8, 2026 · N442UA · Airbus A320232 · Emergency LightingSDR CALA2025101009894Power Supply · faultedRIGHT EMERGENCY EXIT LIGHTS POWER SUPPLY CONTROLLER HAS A FAULT. REMOVED AND REPLACED RH EMERGENCY EXIT LIGHT POWER SUPPLY ASSY 12WL, OPS CHECK OK REF AMM 33-51-38.PARTS USED: 31-3350-9-9001, QTY :1 ROTABLE PARTS CHG:TT # 1422891 SN OFF 4242 PN OFF 31-3350-9-9Oct 9, 2025 · N442UA · Airbus A320232 · Emergency LightingSDR CALA2025092609281Girt Bar · dirtyL1 DOOR FLOOR AFT RELEASE CATCH FOR GIRT BAR IS JAMMED. CHECKED CONDITION OF GIRT BAR FITTINGS, CLEANED GIRT BAR FITTINGS, NO DEFECTS NOTED IAW AMM 52-11-00. OK FOR SERVICE.Sep 24, 2025 · N442UA · Airbus A320232 · Emergency EquipmentSDR CALA2025080407256Girt Bar · lack of lubeDURING MEXICAN AVIATION AUTHORITIES AIWORTHINESS INSPECTION THEY FOUND AFT LATCH ESCAPE SLIDE BAR ON FWD L1 DOOR STUCK. SLIDE AFT BAR LATCH ON FWD L1 DORR WAS CLEANED AND LUBED PER AMM 12-22-00. OK FOR SERVICEJul 31, 2025 · N442UA · Airbus A320232 · Emergency EquipmentSDR CALA2025031302792Battery · no testCABIN EMERGENCY LIGHTING BATTERY CAPACITY OPERATIONAL CHECK EPSU BATTERY 1L WAS UNSATISFACTORY EPSU BATTERY REPLACED AS PER AMM 33-51-38-000-002-A AND INSTALLATION OF THE BATTERY OF THE EMERGENCY POWER SUPPLY UNIT (EPSU) A SPER AMM TASK 33-51-38-400-002-A0 TEMar 12, 2025 · N442UA · Airbus A320232 · Emergency LightingSDR CALA2024120601437Proximity Switch · out of adjustDOOR R FWD CABIN ECAM.CABIN PRESSURE IS NORMAL. CREW REPORTS DR 1R INDICATES OPEN AND ARMED AND DOOR PAGE. F-ATTENDANT REPORTS DOOR SHOWS SLIDE ARMED AS WELL. ADJUSTED PROX SWITCHES 11WV2 AND 13WV2 ON RIGHT FWD ENTRY DOOR. REF AMM 52-71-00-820-001-A-01. OP CHDec 4, 2024 · N442UA · Airbus A320232 · Door Warning SystemSDR CALA2024120401403Proximity Sensor · faultyECAM DOOR R FWDOPEN V/S AND CABINALT NORMAL REPEAT WRITEUP PREVIOUS HISTORY FOR DOOR 1R OPEN INDICATION IN FLIGHT. FAULT IS INTERMITTENT. APLYING MEL 5270AX. VERIFIED DOOR 1R IS CLOSED AND SLIDE ARMED LIGHT COMES ON WHEN THE SLIDE ARMED. DISPATCH DESK: 10 NADec 2, 2024 · N442UA · Airbus A320232 · Door Warning SystemSDR CALA2024120202997Beam · crackedRH FR16 UPPER DOUBLE JOGGLE AREA FOUND WITH CRACKS AT MULTIPLE HOLES AT C-CHECK VISIT IN LCQ. ECRA 5311-03317 ON OR BEFORE THE AIRCRAFT REACHES 39,541 TOTAL NOT TO EXCEED 6,800 FLIGHT CYCLES, THEREAFTER. AIRCRAFT FLIGHT CYCLES. PERFORM REPEAT INSPECTIONS AT INNov 30, 2024 · N442UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2023083002661Brake Sys · faultedBRAKES SYS 2 FAULTCYCLED A/SKID SWITCHGOT BRAKES SYS 1 FAULTCOUL D NOT CLEAR REMOVED AND REPLACED BSCU PER AMM 32-42-34-000/400-001-A. OPS 1711515,QTY :1 CHECK GOOD. RANG WIRES FROM BSCU PINS 1A/1B 102.0 OHMS, AND PINS ROTABLE PARTS CHANGE WAS INDICATED - TT #Aug 30, 2023 · N442UA · Airbus A320232 · BrakeSDR CALA2023060701787Wheel · unknownRTO BELOW 40 KNOTSAIRCRAFT PULLING HARD TO THE RIGHT AS POWERRE ACHED TAKEOFF SETTING UPON ARRIVAL, RAN BSCU 1 AND 2 TEST FOR LRU WIRING AND BSCU TEST. NO FAULTS DETECTED. SEE ATTACHED PICS, REF AMM 32-46-00-740-001-A DEBRIEFED CREW UPON ARRIVAL, AT 40 KNOTS Jun 6, 2023 · N442UA · Airbus A320232 · Wheel/Ski/FloatSDR CALA2022052501334Frame · cracked(AD2022-02-11) DURING ROTO PROBE OF RH FR16 #7 DOOR STOP CRACK I NDICATION NOTED IN HOLES #1 AND #3 FRAME AND INTERCOASTAL LAYERS REPAIR BEFORE NEXT FLIGHT.()May 24, 2022 · N442UA · Airbus A320232 · Fuselage Main, FrameSDR CALA2022052501333Frame · cracked(AD2022-02-11) DURING ROTO PROBE OF LH FR16 #7 DOOR STOP CRACK INDICATION NOTED IN HOLE #1 FRAME AND INTERCOASTAL LAYERS.()May 24, 2022 · N442UA · Airbus A320232 · Fuselage Main, FrameSDR CALA2022052501331Shear Plate · corroded(A3NB-53-3-6185) AFT CABIN, FLOOR STRUCTURE BTW FR69-FR70, LEFT SHEAR PLATE CORRODED. DOT 88-044() REMOVED AND REPLACED SHEAR PLATE P/N: D5347112420200 IAW A320 SR BFM ON NR# 0029991 M 57-42-11 AND 2EA BRACKETS REMOVED AND INSTALLED TO FOM. REMOVE D AND INSTALMay 24, 2022 · N442UA · Airbus A320232 · Fuselage Structure (General)SDR CALA2022052301317None · corroded(A3NB-53-4-6179) AFT CARGO PIT DOOR SILL BETWEEN FR52/FR56 HAS C ORROSION IN SEVERAL LOCATIONS. DOT 52-69.() REPLACED DOOR SILL SHEET IAW A320 SRM 51-42-11. P/N: D5347556521 200 BATCH: 0003946991. EMP# V934700 WORK ACCOMPLISHED AT ST ENGI NEERING AEROSPACE OF May 22, 2022 · N442UA · Airbus A320232 · Fuselage, Wing Attach FittingsSDR CALA2022052301316Skin · damaged(A3NB-71-3-6011) LEFT PYLON AFT FIXED FAIRING RH EXTERNAL SKIN H AS DAMAGE.(REMOVE DAMAGE.) REMOVED AND REPLACED SKIN PANEL ON LEFT SIDE FIXED FAIRING IAW S RM 54-54-11-300-038. REMOVED AND REPLACED ANGLE SUPPORT PANEL IA W SRM 51-42-11. EMP# V933866 WORK ACCOMay 22, 2022 · N442UA · Airbus A320232 · Nacelle/Pylon StructureSDR CALA2022052001304None · corroded(A3NB-53-4-6179) AFT CARGO PIT DOOR SILL BETWEEN FR52/FR56 HAS CORROSION IN SEVERAL LOCATIONS. DOT 52-69.() REPLACED DOOR SILL SHEET IAW A320 SRM 51-42-11. P/N: D5347556521 200 BATCH: 0003946991. EMP# V934700 WORK ACCOMPLISHED AT ST ENGI NEERING AEROSPACE OF MMay 20, 2022 · N442UA · Airbus A320232 · Fuselage, Wing Attach FittingsSDR CALA2022052001303None · damaged(A3NB-71-3-6011) LEFT PYLON AFT FIXED FAIRING RH EXTERNAL SKIN H AS DAMAGE.(REMOVE DAMAGE.) REMOVED AND REPLACED SKIN PANEL ON LEFT SIDE FIXED FAIRING IAW S RM 54-54-11-300-038. REMOVED AND REPLACED ANGLE SUPPORT PANEL IA W SRM 51-42-11. EMP# V933866 WORK ACCOMay 20, 2022 · N442UA · Airbus A320232 · Nacelle/Pylon StructureSDR CALA2022051601253Angle · cracked(A3NB-52-4-6031) RH AFT EMERGENCY EXIT DOOR HAS CRACK AT LH LOAD TRANSMITTING PROFIL. DOT NO. 17-46() REMOVED AND INSTALLED NEW SEGMENT ANGLE (P/N: D5227902620451) IA W SRM 51-42-11. REMOVED AND REINSTALLED BRACKET SUPPORT (FOR ACC ESS) IAW SRM 51-42-11. EMP# May 15, 2022 · N442UA · Airbus A320232 · Emergency ExitsSDR CALA2022051601252Skin · dentedA3NB-53-3-6358, RH FWD LOWER FUSELAGE 1EA DENT TO OUT SIDE BETWE EN FR31-FR32 AND STR28R AND STR29R. DOT #54-46() M ON NR# 0029972. REPETITIVE INSPECTIONS REQUIRED PER SRI 53-21 TH SUBSEQUENT INSPECTIONS EVERY 1700 FC OR 3400 FH WHICH EVER O -11-205-071 AT 4May 15, 2022 · N442UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2022051601250Angle · cracked(A3NB-52-4-6031) LH AFT EMERGENCY EXIT DOOR HAS CRACK AT LH LOAD TRANSMITTING PROFIL. DOT NO.17-51() REMOVED AND INSTALLED NEW ANGLE SEGMENT PN #D227902620451, IAW S RM 51-42-11. REINSTALLED SUPPORT BRACKET REMOVED FOR ACCESS IAW SRM 51-42-11. EMP# V934344 WORMay 15, 2022 · N442UA · Airbus A320232 · Emergency ExitsSDR CALA2022051601249Angle · cracked(A3NB-52-4-6031) LH AFT EMERGENCY EXIT DOOR HAS CRACK AT RH LOAD TRANSMITTING PROFIL. DOT NO.17-52() REMOVED AND INSTALLED NEW ANGLE SEGMENT PN #D5227902620551 IAW S RM 51-42-11. REINSTALLED SUPPORT BRACKET REMOVED FOR ACCESS IAW SRM 51-42-11. EMP# V934377 WORMay 15, 2022 · N442UA · Airbus A320232 · Emergency ExitsSDR CALA2022051601246Angle · cracked(A3NB-52-4-6031) RH FWD EMERGENCY EXIT DOOR HAS A CRACK AT LH LO AD TRANSMITTING PROFIL. DOT NO.17-48.()May 15, 2022 · N442UA · Airbus A320232 · Emergency ExitsSDR CALA2022051601245Angle · cracked(A3NB-52-4-6031) RH FWD EMERGENCY EXIT DOOR HAS CRACK AT RH LOAD TRANSMITTING PROFIL. DOT NO.17-49() REMOVED & REPLACED SEGMENT ANGLE ON R/H FWD EMERGENCY EXIT DOOR R/H IAW SRM 51-42-11. ACCOMPLISHED BY EMP#V934342 AT ST BFM AERO SPACE MOBILE. NR#0029818May 15, 2022 · N442UA · Airbus A320232 · Emergency ExitsSDR CALA2022051601239None · corroded(A3NB-53-4-6179) AFT CARGO PIT BETWEEN FR56/FR59 STRG 42LH HAS CORROSION. DOT 52-72.() REPLACED STRINGER 42L BETWEEN FR53 TO FR60, IAW A320 SRM 51-42-1 1 P/N:DAN50B09 BATCH: 0003906803. ACCOMPLISHED BY EMP#V934585 AT ST BFM AEROSPACE MOBILE. NR#0029746May 13, 2022 · N442UA · Airbus A320232 · Fuselage, Wing Attach FittingsSDR CALA2022051301230None · none(A3NB-52-4-6031) LH AFT EMERGENCY EXIT DOOR HAS CRACK AT RH LOAD TRANSMITTING PROFIL. DOT NO.17-52() REMOVED AND INSTALLED NEW ANGLE SEGMENT PN #D5227902620551 IAW S RM 51-42-11. REINSTALLED SUPPORT BRACKET REMOVED FOR ACCESS IAW SRM 51-42-11. EMP# V934377 WORMay 13, 2022 · N442UA · Airbus A320232 · Emergency ExitsSDR CALA2022051301229None · none(A3NB-52-4-6031) LH AFT EMERGENCY EXIT DOOR HAS CRACK AT LH LOAD TRANSMITTING PROFIL. DOT NO.17-51() REMOVED AND INSTALLED NEW ANGLE SEGMENT PN #D227902620451, IAW S RM 51-42-11. REINSTALLED SUPPORT BRACKET REMOVED FOR ACCESS IAW SRM 51-42-11. EMP# V934344 WORMay 13, 2022 · N442UA · Airbus A320232 · Emergency ExitsSDR CALA2022051101211None · cracked(A3NB-52-4-6031) RH AFT EMERGENCY EXIT DOOR HAS CRACK AT LH LOAD TRANSMITTING PROFIL. DOT NO. 17-46() REMOVED AND INSTALLED NEW SEGMENT ANGLE (P/N: D5227902620451) IA W SRM 51-42-11. REMOVED AND REINSTALLED BRACKET SUPPORT (FOR ACC ESS) IAW SRM 51-42-11. EMP# May 11, 2022 · N442UA · Airbus A320232 · Emergency ExitsSDR CALA2022050601151Floor Support · corrodedA3NB-53-3-6183: CORROSION ONLY AFT ENTRY DOOR, LOWER SILL PLATE, GIRT BAR FITTING PLATE. DOT 66-05.() REMOVED CORROSION ON LH ENTRY DOOR LOWER SILL IAW SRM 51-74-00. 51-42-11. FORM 44-0008 ATTACHED EMP# V933866 WORK ACCOMPLISHED A MEASURED AT THICKNESS:0315" MMay 4, 2022 · N442UA · Airbus A320232 · Fuselage Structure (General)SDR CALA2022050601150Intercostal · cracked(A3NB-52-4-6031) LH FWD EMERGENCY EXIT DOOR HAS CRACK AT LH LOAD TRANSMITTING PROFIL BETWEEN RIVETS. (DOT NO. 17-45 () REMOVED & REPLACED 1EA SEGMENT ANGLE AND 1EA BRACKET SUPPORT ON L/H FWD EMERGENCY EXIT DOOR L/H IAW SRM 51-42-11. ACCOMPLISHED B Y EMP#V93434May 4, 2022 · N442UA · Airbus A320232 · Emergency ExitsSDR CALA2022050401137None · dentedA3NB-53-3-6358, RH FWD LOWER FUSELAGE 1EA DENT TO OUT SIDE BETWE EN FR31-FR32 AND STR28R AND STR29R. DOT #54-46() M ON NR# 0029972. REPETITIVE INSPECTIONS REQUIRED PER SRI 53-21 TH SUBSEQUENT INSPECTIONS EVERY 1700 FC OR 3400 FH WHICH EVER O -11-205-071 AT 4May 4, 2022 · N442UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2022050201120Floor Support · corroded(A3NB-53-3-6299) RH AFT PAX/CREW DOOR CUTOUT LOWER SILL UPPER SU RFACE CORRODED AT FR66. DOT #54-31.() REMOVED CORROSION AT R2 DOOR LOWER SILL IAW SRM 51-74-00/001. L= LE AT BFM ON NR# 0029826. 300" W=2" D=0.060". FOUND TO BE OUT OF LIMITS IAW SRM 53-41-14-2 8May 1, 2022 · N442UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2022050201119Beam · corroded(A3NB-53-3-6185) AFT CABIN, FLOOR STRUCTURE, FR66, Y-765, BEAM W ITH CORROSION. DOT 88-048.() AFT CABIN, FLOOR STRUCTURE FR66 Y-765 BEAM CORROSION FOUND OUT O F LIMITS IAW SRM 51-41-15-283. REMOVED AND INSTALLED NEW FLOOR B EAM IAW SRM 51-42-11. EMP# V936636 WMay 1, 2022 · N442UA · Airbus A320232 · Fuselage Structure (General)SDR CALA2022050201118Intercostal · crackedA3NB-52-4-6031 RH AFT EMERGENCY EXIT DOOR HAS CRACK AT RH LOAD T RANSMITTING PROFIL.May 1, 2022 · N442UA · Airbus A320232 · Emergency ExitsSDR CALA2022050201117Seat Track · corroded(A3NB-53-3-6038) FWD CABIN, FLOOR STRUCTURE, FR20, Y-765, BEAM W ITH CORROSION. DOT 88-040 ()May 1, 2022 · N442UA · Airbus A320232 · Fuselage Main, FrameSDR CALA2022042901102Skin · dentedA3NB-53-3-6358, RH FWD LOWER FUSELAGE 1EA DENT TO OUT SIDE BETWE EN FR31-FR32 AND STR28R-STR29R. DOT #54-46() DENT FOUND OUT OF LIMITS IAW A320 SRM 53-21-11-283-020 FIG 004. ENGINEERING AEROSPACE OF MOBILE AT BFM ON NR# 0029972. PERFORMED SKIN REPAIR IAW A320 Apr 29, 2022 · N442UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2022042701089Frame · corroded(A3NB-53-3-6299) RH AFT PAX/CREW DOOR CUTOUT LOWER SILL UPPER SU RFACE CORRODED AT FR66. DOT #54-31.() REMOVED CORROSION AT R2 DOOR LOWER SILL IAW SRM 51-74-00/001. L= LE AT BFM ON NR# 0029826. 300" W=2" D=0.060". FOUND TO BE OUT OF LIMITS IAW SRM 53-41-14-2 8Apr 27, 2022 · N442UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2019051700777Switch · faultyHYD GREEN RSV LOW LVL ECAM ON ARRIVALGREEN HYD QUANTITY APPEARED NORMAL ON S/D VERIFIED GREEN HYD RSV LEVEL WAS AT NORMAL OPERATING LEVEL. INSPECTED FOR LEAKS, NO LEAKS NOTED. SUSPECT GREEN HYD SYSTEM RSV LOW LEVEL SWITCH TO AT FAULT. SUGGEST REPLACING GREEN HMay 16, 2019 · N442UA · Airbus A320232 · Hydraulic Quantity SensorSDR CALA2018082701860Power Supply · inoperativeTHE EMERGENCY LIGHTS FAILED TO ILLUMINATE. REMOVED AND REPLACED THE POWER SUPPLY.Aug 27, 2018 · N442UA · Airbus A320232 · Emergency LightingSDR CALA2017091503207Light · missingSEAT 29C EMERGENCY LIGHT MISSING. INSTALLED THE EMERGENCY LIGHT. OPS CHECKED GOOD.Sep 15, 2017 · N442UA · Airbus A320232 · Emergency LightingSDR CALA2016121901125Battery Pack · failedLEFT OVERWING EMER BATTERY AND AFT LEFT BATTERY FAILED. REMOVED AND REPLACED LT OVERWING AND AFT LEFT EMER BATTERY PACKS REF AMM 33-51-38 PB 0401, OPS CHK GOOD, A/C OK FOR SERVICE.Dec 19, 2016 · N442UA · Airbus A320232 · Emergency LightingSDR CALA2016083095698Battery Pack · no testLEFT OVERWING EMERGENCY LIGHT BATTERY FAULT DURING 2SVC, REPLACED THE BATTERY, TEST PASSEDAug 26, 2016 · N442UA · Airbus A320232 · Emergency LightingSDR CALA2015042093581Skin · dentedFROM CF 9001 REPAIR DENT AT STRINGER 41, FRAME 56RT. REPAIRED IAW SRM 53-41-11 FIGURE 204 SHEET 4. SRI53-41-11-2-012-00 TABLE 215 REQUIRES FIRST INSPECTION AT 45,800C FROM REPAIR EMBODIMENT. THEN SUBSEQUENT INSPECTION AT 11,40 0C INTERVALS THEREAFTER. THENApr 16, 2015 · N442UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2015033093487Door Sill · corrodedR1 DOOR SILL FRAME 16 - 20 FWD & AFT GIRT BAR FITTING ATTACH AREAS HAVE CORROSION AT FASTENER HOLES. REWORKED IAW SRM 53-11-14 PAR 4 E FIG 108.Mar 28, 2015 · N442UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2015033093486Door Sill · corrodedL2 DOOR SILL FRAME 66 HAS TWO EACH CORRODED FASTENER HOLES. REPAIRED IAW SRM 53- 41-14 PAR 5 A FIG 201.Mar 28, 2015 · N442UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2015033093485Stringer · corrodedSTRINGER 31R AT FRAME 64 - 67 HAS CORROSION. REPLACED IAW SRM 51-72-11.Mar 27, 2015 · N442UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2013120993540Seal · tornLOWER FWD HORIZONTAL STAB LE SEAL TORN 3 INCHES FROM THE NOSE OF THE HORIZONTAL STAB. TRIMMED SEAL IAW ECRA 5512 01011. INSPECTED REMAINING SEAL & RETAINER NO DAMAGE FOUND.Dec 6, 2013 · N442UA · Airbus A320232 · Horizontal Stabilizer Miscellaneous StructureSDR CALA2013120693511Sensor · faultyLGCIU 2 FAULT DISPLAYED ON UPPER ECAM SCREEN. CFDS FAULTING 25GA, PCN 565-1759, IAW TSM 32-31-00- 810-815A. R & R SENSOR 25GA IAW MM 32-21-00, ALL OPERATIONS & RIG CHECKED NORMAL.Dec 5, 2013 · N442UA · Airbus A320232 · Landing Gear Position and Warning
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