# Service difficulty reports: N442UA

A list on [N442UA](https://openairdocs.org/aircraft/N442UA.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 3 · 120 reports

- [SDR CALA2026072718042](https://openairdocs.org/sdr/CALA2026072718042.md): Light · damaged · Jul 25, 2026 · N442UA · Airbus A320232 · Emergency Lighting
  > LIGHT 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.
- [SDR CALA2026060316770](https://openairdocs.org/sdr/CALA2026060316770.md): Fuel Cap · missing · Jun 2, 2026 · N442UA · Airbus A320232 · Fuel Storage
  > ON ARRIVAL FUEL CAP MISSING INSTALLED UNDERWING FUEL CAP AND LANYARD ASSEMBLY REF AMM 28-45-21
- [SDR CALA2026021813868](https://openairdocs.org/sdr/CALA2026021813868.md): Antenna · faulted · Feb 15, 2026 · N442UA · Airbus A320232 · Weather Radar System
  > WX 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 IA
- [SDR CALA2026010912832](https://openairdocs.org/sdr/CALA2026010912832.md): Sign · inoperative · Jan 8, 2026 · N442UA · Airbus A320232 · Emergency Lighting
  > MULTIPLE 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 LIGHTS
- [SDR CALA2025101009894](https://openairdocs.org/sdr/CALA2025101009894.md): Power Supply · faulted · Oct 9, 2025 · N442UA · Airbus A320232 · Emergency Lighting
  > RIGHT 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 31-3350-9-9
- [SDR CALA2025092609281](https://openairdocs.org/sdr/CALA2025092609281.md): Girt Bar · dirty · Sep 24, 2025 · N442UA · Airbus A320232 · Emergency Equipment
  > L1 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.
- [SDR CALA2025080407256](https://openairdocs.org/sdr/CALA2025080407256.md): Girt Bar · lack of lube · Jul 31, 2025 · N442UA · Airbus A320232 · Emergency Equipment
  > DURING 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 SERVICE
- [SDR CALA2025031302792](https://openairdocs.org/sdr/CALA2025031302792.md): Battery · no test · Mar 12, 2025 · N442UA · Airbus A320232 · Emergency Lighting
  > CABIN 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 TE
- [SDR CALA2024120601437](https://openairdocs.org/sdr/CALA2024120601437.md): Proximity Switch · out of adjust · Dec 4, 2024 · N442UA · Airbus A320232 · Door Warning System
  > DOOR 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 CH
- [SDR CALA2024120401403](https://openairdocs.org/sdr/CALA2024120401403.md): Proximity Sensor · faulty · Dec 2, 2024 · N442UA · Airbus A320232 · Door Warning System
  > ECAM 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 NA
- [SDR CALA2024120202997](https://openairdocs.org/sdr/CALA2024120202997.md): Beam · cracked · Nov 30, 2024 · N442UA · Airbus A320232 · Fuselage Main, Structure
  > RH 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 IN
- [SDR CALA2023083002661](https://openairdocs.org/sdr/CALA2023083002661.md): Brake Sys · faulted · Aug 30, 2023 · N442UA · Airbus A320232 · Brake
  > BRAKES 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 #
- [SDR CALA2023060701787](https://openairdocs.org/sdr/CALA2023060701787.md): Wheel · unknown · Jun 6, 2023 · N442UA · Airbus A320232 · Wheel/Ski/Float
  > RTO 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
- [SDR CALA2022052501334](https://openairdocs.org/sdr/CALA2022052501334.md): Frame · cracked · May 24, 2022 · N442UA · Airbus A320232 · Fuselage Main, Frame
  > (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.()
- [SDR CALA2022052501333](https://openairdocs.org/sdr/CALA2022052501333.md): Frame · cracked · May 24, 2022 · N442UA · Airbus A320232 · Fuselage Main, Frame
  > (AD2022-02-11) DURING ROTO PROBE OF LH FR16 #7 DOOR STOP CRACK INDICATION NOTED IN HOLE #1 FRAME AND INTERCOASTAL LAYERS.()
- [SDR CALA2022052501331](https://openairdocs.org/sdr/CALA2022052501331.md): Shear Plate · corroded · May 24, 2022 · N442UA · Airbus A320232 · Fuselage Structure (General)
  > (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 INSTAL
- [SDR CALA2022052301317](https://openairdocs.org/sdr/CALA2022052301317.md): None · corroded · May 22, 2022 · N442UA · Airbus A320232 · Fuselage, Wing Attach Fittings
  > (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
- [SDR CALA2022052301316](https://openairdocs.org/sdr/CALA2022052301316.md): Skin · damaged · May 22, 2022 · N442UA · Airbus A320232 · Nacelle/Pylon Structure
  > (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 ACCO
- [SDR CALA2022052001304](https://openairdocs.org/sdr/CALA2022052001304.md): None · corroded · May 20, 2022 · N442UA · Airbus A320232 · Fuselage, Wing Attach Fittings
  > (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 M
- [SDR CALA2022052001303](https://openairdocs.org/sdr/CALA2022052001303.md): None · damaged · May 20, 2022 · N442UA · Airbus A320232 · Nacelle/Pylon Structure
  > (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 ACCO
- [SDR CALA2022051601253](https://openairdocs.org/sdr/CALA2022051601253.md): Angle · cracked · May 15, 2022 · N442UA · Airbus A320232 · Emergency Exits
  > (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#
- [SDR CALA2022051601252](https://openairdocs.org/sdr/CALA2022051601252.md): Skin · dented · May 15, 2022 · N442UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > A3NB-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 4
- [SDR CALA2022051601250](https://openairdocs.org/sdr/CALA2022051601250.md): Angle · cracked · May 15, 2022 · N442UA · Airbus A320232 · Emergency Exits
  > (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 WOR
- [SDR CALA2022051601249](https://openairdocs.org/sdr/CALA2022051601249.md): Angle · cracked · May 15, 2022 · N442UA · Airbus A320232 · Emergency Exits
  > (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 WOR
- [SDR CALA2022051601246](https://openairdocs.org/sdr/CALA2022051601246.md): Angle · cracked · May 15, 2022 · N442UA · Airbus A320232 · Emergency Exits
  > (A3NB-52-4-6031) RH FWD EMERGENCY EXIT DOOR HAS A CRACK AT LH LO AD TRANSMITTING PROFIL. DOT NO.17-48.()
- [SDR CALA2022051601245](https://openairdocs.org/sdr/CALA2022051601245.md): Angle · cracked · May 15, 2022 · N442UA · Airbus A320232 · Emergency Exits
  > (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#0029818
- [SDR CALA2022051601239](https://openairdocs.org/sdr/CALA2022051601239.md): None · corroded · May 13, 2022 · N442UA · Airbus A320232 · Fuselage, Wing Attach Fittings
  > (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#0029746
- [SDR CALA2022051301230](https://openairdocs.org/sdr/CALA2022051301230.md): None · none · May 13, 2022 · N442UA · Airbus A320232 · Emergency Exits
  > (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 WOR
- [SDR CALA2022051301229](https://openairdocs.org/sdr/CALA2022051301229.md): None · none · May 13, 2022 · N442UA · Airbus A320232 · Emergency Exits
  > (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 WOR
- [SDR CALA2022051101211](https://openairdocs.org/sdr/CALA2022051101211.md): None · cracked · May 11, 2022 · N442UA · Airbus A320232 · Emergency Exits
  > (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#
- [SDR CALA2022050601151](https://openairdocs.org/sdr/CALA2022050601151.md): Floor Support · corroded · May 4, 2022 · N442UA · Airbus A320232 · Fuselage Structure (General)
  > A3NB-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" M
- [SDR CALA2022050601150](https://openairdocs.org/sdr/CALA2022050601150.md): Intercostal · cracked · May 4, 2022 · N442UA · Airbus A320232 · Emergency Exits
  > (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#V93434
- [SDR CALA2022050401137](https://openairdocs.org/sdr/CALA2022050401137.md): None · dented · May 4, 2022 · N442UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > A3NB-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 4
- [SDR CALA2022050201120](https://openairdocs.org/sdr/CALA2022050201120.md): Floor Support · corroded · May 1, 2022 · N442UA · Airbus A320232 · Fuselage Main, Structure
  > (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 8
- [SDR CALA2022050201119](https://openairdocs.org/sdr/CALA2022050201119.md): Beam · corroded · May 1, 2022 · N442UA · Airbus A320232 · Fuselage Structure (General)
  > (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 W
- [SDR CALA2022050201118](https://openairdocs.org/sdr/CALA2022050201118.md): Intercostal · cracked · May 1, 2022 · N442UA · Airbus A320232 · Emergency Exits
  > A3NB-52-4-6031 RH AFT EMERGENCY EXIT DOOR HAS CRACK AT RH LOAD T RANSMITTING PROFIL.
- [SDR CALA2022050201117](https://openairdocs.org/sdr/CALA2022050201117.md): Seat Track · corroded · May 1, 2022 · N442UA · Airbus A320232 · Fuselage Main, Frame
  > (A3NB-53-3-6038) FWD CABIN, FLOOR STRUCTURE, FR20, Y-765, BEAM W ITH CORROSION. DOT 88-040 ()
- [SDR CALA2022042901102](https://openairdocs.org/sdr/CALA2022042901102.md): Skin · dented · Apr 29, 2022 · N442UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > A3NB-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
- [SDR CALA2022042701089](https://openairdocs.org/sdr/CALA2022042701089.md): Frame · corroded · Apr 27, 2022 · N442UA · Airbus A320232 · Fuselage Main, Structure
  > (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 8
- [SDR CALA2019051700777](https://openairdocs.org/sdr/CALA2019051700777.md): Switch · faulty · May 16, 2019 · N442UA · Airbus A320232 · Hydraulic Quantity Sensor
  > HYD 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 H
- [SDR CALA2018082701860](https://openairdocs.org/sdr/CALA2018082701860.md): Power Supply · inoperative · Aug 27, 2018 · N442UA · Airbus A320232 · Emergency Lighting
  > THE EMERGENCY LIGHTS FAILED TO ILLUMINATE. REMOVED AND REPLACED THE POWER SUPPLY.
- [SDR CALA2017091503207](https://openairdocs.org/sdr/CALA2017091503207.md): Light · missing · Sep 15, 2017 · N442UA · Airbus A320232 · Emergency Lighting
  > SEAT 29C EMERGENCY LIGHT MISSING. INSTALLED THE EMERGENCY LIGHT. OPS CHECKED GOOD.
- [SDR CALA2016121901125](https://openairdocs.org/sdr/CALA2016121901125.md): Battery Pack · failed · Dec 19, 2016 · N442UA · Airbus A320232 · Emergency Lighting
  > LEFT 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.
- [SDR CALA2016083095698](https://openairdocs.org/sdr/CALA2016083095698.md): Battery Pack · no test · Aug 26, 2016 · N442UA · Airbus A320232 · Emergency Lighting
  > LEFT OVERWING EMERGENCY LIGHT BATTERY FAULT DURING 2SVC, REPLACED THE BATTERY, TEST PASSED
- [SDR CALA2015042093581](https://openairdocs.org/sdr/CALA2015042093581.md): Skin · dented · Apr 16, 2015 · N442UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > FROM 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. THEN
- [SDR CALA2015033093487](https://openairdocs.org/sdr/CALA2015033093487.md): Door Sill · corroded · Mar 28, 2015 · N442UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > R1 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.
- [SDR CALA2015033093486](https://openairdocs.org/sdr/CALA2015033093486.md): Door Sill · corroded · Mar 28, 2015 · N442UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > L2 DOOR SILL FRAME 66 HAS TWO EACH CORRODED FASTENER HOLES. REPAIRED IAW SRM 53- 41-14 PAR 5 A FIG 201.
- [SDR CALA2015033093485](https://openairdocs.org/sdr/CALA2015033093485.md): Stringer · corroded · Mar 27, 2015 · N442UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > STRINGER 31R AT FRAME 64 - 67 HAS CORROSION. REPLACED IAW SRM 51-72-11.
- [SDR CALA2013120993540](https://openairdocs.org/sdr/CALA2013120993540.md): Seal · torn · Dec 6, 2013 · N442UA · Airbus A320232 · Horizontal Stabilizer Miscellaneous Structure
  > LOWER 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.
- [SDR CALA2013120693511](https://openairdocs.org/sdr/CALA2013120693511.md): Sensor · faulty · Dec 5, 2013 · N442UA · Airbus A320232 · Landing Gear Position and Warning
  > LGCIU 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.

Next page: https://openairdocs.org/aircraft/N442UA/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/aircraft/N442UA/reports

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