# Service difficulty reports: N462UA

A list on [N462UA](https://openairdocs.org/aircraft/N462UA.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 CALA2026031714626](https://openairdocs.org/sdr/CALA2026031714626.md): Engine · vibration · Mar 13, 2026 · N462UA · Airbus A320232 · Engine Vibration Analyzer
  > SEVERE ENG 2 VIBRATION IN SEVERE ICING COND. FLIGHT CREW REPORT THAT ON DESCENT ENGINE RETURNED TO NORMAL OPE RATIONAL MODE WITH NO VIBRATION NOTED. ACCOMPLISHED INSPECTION OF ENGINE AS REQUIRED PER TSM 77-30-00-810-827-A FOR HIGH N1 VIBRATION LEVEL ON ENGIN
- [SDR CALA2025102110365](https://openairdocs.org/sdr/CALA2025102110365.md): Detector · faulted · Oct 13, 2025 · N462UA · Airbus A320232 · Door Warning System
  > CABIN PRESSURE CABIN DOOR WARNING LIGHTS FRONT/AFT FLASHING ECAM PRESS ZERO. COULD NOT DUPLICATE FAULT, TESTS PASSED, REMOVED AND REPLACED CABIN-PRESSURE DETECTION PRESSURE-SWITCH (FIN 14WN) PER AMM 52-73-12, OPS CHECK GOOD, DOOR FLASHES AND THEN TURNS
- [SDR CALA2025051504700](https://openairdocs.org/sdr/CALA2025051504700.md): Frame · cracked · May 9, 2025 · N462UA · Airbus A320232 · Fuselage Main, Frame
  > CRACKS OF 1.062" AND 0.218" OF LENGTH AT RH SIDE AFT PASSENGER/C REW DOOR CUTOUT UPPER CORNER RADIUS ABOVE STR 8 AND FR 68 WEB JO INT TO DOOR FRAME. GEN BY V947494 ON HAECO LCQ NR 9292561 / 3456 1 ACCOMPLISHED INTERIM RPR AT RH FR68 STRG 8R FR WEB STIFFNER AND
- [SDR CALA2025050904584](https://openairdocs.org/sdr/CALA2025050904584.md): Service Door · damaged · May 8, 2025 · N462UA · Airbus A320232 · Fluid Service Doors
  > AFT LAV SERVICE DOOR HAS OVER SIZED HOLE ON LATCH ATTACH HOLES. REMOVED AND REPLACED AFT LAV SERVICE DOOR IAW A320 AMM 52-42-11- 400-001.
- [SDR CALA2025050704522](https://openairdocs.org/sdr/CALA2025050704522.md): Stringer · corroded · Apr 21, 2025 · N462UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > FWD CARGO CORROSION ON STRINGER 40L FR 30. R & R SECTION OF STRINGER 40LT AND INSTALLED STRINGER REPAI R FR29-32 IAW A320 SRM 53-21-13-300-018 ACP RII INSP AS REQUIRED LC-81.
- [SDR CALA2025043004349](https://openairdocs.org/sdr/CALA2025043004349.md): Door Frame · cracked · Apr 15, 2025 · N462UA · Airbus A320232 · Fuselage Main, Structure
  > CRACK INDICATION AT LH FR 66 DOOR STOP #1 AT 6 OCLOCK POSITION L OWER I/B HOLE. REPAIRED LWR INBD HOLE ON FR 66 DOOR STOP #1 WITH BUSHING AND REPAIR WASHER. FINAL REAM.2820 IAW SRM 53-41-12-300-010 HFEC ACCOMPLISHED WITH NO FINDINGS.
- [SDR CALA2025042304165](https://openairdocs.org/sdr/CALA2025042304165.md): Frame · cracked · Apr 15, 2025 · N462UA · Airbus A320232 · Fuselage Main, Frame
  > DOUBLE JOGGLE AT RT FR 20 HOLE #6 HAS CRACK INDICATION IN FRAME LAYER, 3 DIRECTION, 100% S.H. REPAIRED HOLE #6 AT RH FR20 DOUBLE JOGGLE WITH BUSHING AND RPR WASHER IAW SRM 53-11-12-300-012. FINAL REAM.2800 THIS IS A CAT B. COMPLETED DOUBLE JOGGLE AT RH FR
- [SDR CALA2025041503857](https://openairdocs.org/sdr/CALA2025041503857.md): Rib · corroded · Apr 12, 2025 · N462UA · Airbus A320232 · Elevator, Spar/Rib
  > RH ELEVATOR O/B RIB I/B SIDE HAS CORROSION. REMOVED RIB ON RH ELEVATOR O/B RIB IAW A320 SRM 51-42-11/001, RE PLACED RIB ON RH ELEVATOR O/B RIB IAW A320 SRM 51-42-11/001.
- [SDR CALA2025041103704](https://openairdocs.org/sdr/CALA2025041103704.md): Skin · contaminated · Apr 9, 2025 · N462UA · Airbus A320232 · Elevator, Plate/Skin
  > L/H ELEVATOR HAS LIQUID INGRESS AT 107.5 IN FROM I/B EDGE, 18.5I N FROM TRAILING EDGE, 1.5IN DIAMETER GENERATED BY V061632 ON H ECO LCQ NR 9292772/34772 ESFR ENTRY REPAIRED LH ELEVATOR 107.5 IN FROM I/B 18.5 IN FROM T/E 1.5 IN D IA IAW A320 SRM 55-21-11-300-0
- [SDR CALA2025040703593](https://openairdocs.org/sdr/CALA2025040703593.md): Cleat · corroded · Apr 3, 2025 · N462UA · Airbus A320232 · Fuselage Main, Structure
  > FWD CARGO CLEAT HAS CORROSION FR 31 STR 42R-43R.
- [SDR CALA2025040403533](https://openairdocs.org/sdr/CALA2025040403533.md): Stop Fitting · cracked · Apr 1, 2025 · N462UA · Airbus A320232 · Fuselage Main, Structure
  > CRACK INDICATION AT RH FR68 DOOR STOP #1 AT 6 OCLOCK HRS POSITIO N LOWER I/B HOLE. ESFR COMPLETED
- [SDR CALA2025040203448](https://openairdocs.org/sdr/CALA2025040203448.md): Stringer Splice · corroded · Apr 1, 2025 · N462UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > AFT WET AREA STRG 24RH ANGLE SPLICE CORRODED @ FRM 70. GENERATED BY V937268 ON HAECO LCQ NR 9292694/34694 SFR COMPLETED FOR LP 4361893 REMOVED SPLICE ON AFT AREA STGR 24RH FR 70 IAW A320 SRM 51-42-11 /001 REV 152 REPLACED SPLICE ON AFT AREA STGR 24RH FRM 70 IA
- [SDR CALA2025040103387](https://openairdocs.org/sdr/CALA2025040103387.md): Cleat · corroded · Mar 28, 2025 · N462UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > FWD CARGO CLEAT HAS CORROSION FR 31 STR 42R-F3R. FWD CARGO CLEAT HAS CORROSION FR 31 STR 42R-43R ESFR COMPLETED REMOVED AND REPLACED FWD CARGO CLEAT AT FR31 STR 42R-43R IAW A32 0 SRM 51-72-11-911-001.
- [SDR CALA2025040103384](https://openairdocs.org/sdr/CALA2025040103384.md): Fitting · corroded · Mar 28, 2025 · N462UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > R2 PAX DOOR LOWER FWD CORNER ANGLE FITTING CORRODED. GENERATED B Y V937268 PER HAECO LCQ NR 9292674/34674. REMOVED AND REPLACED CORNER FITTING AT R-2 PAX DOOR LOWER FWD IAW A320 SRM 51-42-11, SRM 51-72-11 REMOVED AND REPLACED CORNER FITTING AT R2 PAX DOOR LOWE
- [SDR CALA2025040103381](https://openairdocs.org/sdr/CALA2025040103381.md): Cleat · corroded · Mar 28, 2025 · N462UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > FWD CARGO CLEAT HAS CORROSION FR 31 STR 43R-43L. REMOVED AND REPLACED DISCREPANT FWD CARGO CLEAT AT FR31 STR 43R-43R IAW A320 SRM 51-72-11-911-001 WPB V061616. REMOVED AND REPLACED DISCREPANT FWD CARGO CLEAT AT FR31 STR 43R- 43A IAW A320 SRM 51-72-11-911-00
- [SDR CALA2025032803281](https://openairdocs.org/sdr/CALA2025032803281.md): Stringer Splice · corroded · Mar 27, 2025 · N462UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > FWD CARGO STRINGER SPLICE HAS CORROSION FR 31 STR 41L. REMOVED AND REPLACED FISHPLATE (SPLICE) @ FWD CARGO FR31 STR41L I/A/W A320 SRM 51--42-11-001. W/P/B V075620 REMOVED AND REPLACED FISHPLATE(SPLICE) @ FWD CARGO FR31 STR 41L IAW A320 SRM 51-42-11/001.
- [SDR CALA2025032703247](https://openairdocs.org/sdr/CALA2025032703247.md): Stringer Splice · corroded · Mar 25, 2025 · N462UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > FWD CARGO STRINGER SPLICE HAS CORROSION FR 31 SRT 43L. REMOVED AND REPLACED FISHPLATE (SPLICE) @ FWD CARGO FR31 STR43L IAW 51-72-11. REMOVED AND REPLACED FISHPLATE SPLICE @ FWD CARGO FR 31 STR 43L IAW A320 SRM 51-72-11-911-00.
- [SDR CALA2025032603211](https://openairdocs.org/sdr/CALA2025032603211.md): Cleat · corroded · Mar 24, 2025 · N462UA · Airbus A320232 · Fuselage Main, Structure
  > FWD CARGO CLEAT HAS CORROSION FR 31 STR 41R-42R. INSTALLED CLEAT @ FWD CARGO FR 31 STR 41R-42R I/A/W A320 SRM 51-72-11. W/P/B V075620 REMOVED AND REPLACED CLEAT FWD CARGO FR31 STR 41R-42R IAW A320 S RM 51-42-11-001 P6.
- [SDR CALA2025032603205](https://openairdocs.org/sdr/CALA2025032603205.md): Door Frame · cracked · Mar 23, 2025 · N462UA · Airbus A320232 · Fuselage Main, Structure
  > R/H AFT EMERGENCY EXIT DOOR FWD VERTICAL FRAME IS CRACKED. COMPLETED RH AFT EMERGENCY EXIT DOOR FWD VERTICAL SEGMENT REMOVED AND REPL ACED IAW A320 SRM 51-42-11/001 51-72-11-911-002.
- [SDR CALA2025032603204](https://openairdocs.org/sdr/CALA2025032603204.md): Door Frame · cracked · Mar 23, 2025 · N462UA · Airbus A320232 · Fuselage Main, Structure
  > L/H FWD EMERGENCY EXIT HATCH FWD. VERTICAL FRAME IS CRACKED. COMPLETED L/H FWD EMERGENCY EXIT FWD VERTICAL FRAME SEGMENT REMOVED AND RE PLACED IAW A320 SRM 51-42-11/001 AND 51-72-11-911-002.
- [SDR CALA2025032603203](https://openairdocs.org/sdr/CALA2025032603203.md): Door Frame · cracked · Mar 23, 2025 · N462UA · Airbus A320232 · Fuselage Main, Structure
  > R/H AFT EMERGENCY EXIT DOOR AFT VERTICAL FRAME IS CRACKED. COMPLETED RH AFT EMERGENCY EXIT DOOR AFT VERTICAL FRAME SEGMENT REMOVED AN D REPLACED IAW A320 SRM 51-42-11/001 AND 51-75-11-911-002.
- [SDR CALA2025032603202](https://openairdocs.org/sdr/CALA2025032603202.md): Door Frame · cracked · Mar 23, 2025 · N462UA · Airbus A320232 · Fuselage Main, Structure
  > L/H AFT EMERGENCY EXIT HATCH AFT. VERTICAL FRAME IS CRACKED. COMPLETED L/H AFT EMERGENCY EXIT AFT VERTICAL FRAME SEGMENT REMOVED AND RE PLACED IAW A320 SRM 51-42-11/001 AND 51-75-11-911-002
- [SDR CALA2025032103055](https://openairdocs.org/sdr/CALA2025032103055.md): Skin · contaminated · Mar 20, 2025 · N462UA · Airbus A320232 · Elevator, Plate/Skin
  > R/H ELEVATOR HAS LIQUID INGRESS AT 146IN FROM I/B END, 5IN FROM TRAILING EDGE, 1.5IN DIAMETER.
- [SDR CALA2025032003016](https://openairdocs.org/sdr/CALA2025032003016.md): Skin · contaminated · Mar 19, 2025 · N462UA · Airbus A320232 · Elevator, Plate/Skin
  > R.H ELEVATOR HAS LIQUID INGRESS AT 180.5IN FROM I/B END, 10IN FR OM TRAILING EDGE. 1IN DIAMETER. REPAIRED RH ELEVATOR 180.5 IN FROM I/B 10IN FROM T/E 1.5IN DIAME TER ZONE A IAW A320 SRM 55-21-11-300-005 CATEGORY A REPAIR
- [SDR CALA2025032003008](https://openairdocs.org/sdr/CALA2025032003008.md): Skin · contaminated · Mar 19, 2025 · N462UA · Airbus A320232 · Elevator, Plate/Skin
  > R/H ELEVATOR HAS LIQUID INGRESS AT 168.5IN FROM I/B END, 4.5IN F ROM TRAILING EDGE, 1IN DIAMETER.
- [SDR CALA2025032002995](https://openairdocs.org/sdr/CALA2025032002995.md): Skin · dented · Mar 19, 2025 · N462UA · Airbus A320232 · Elevator, Plate/Skin
  > R/H ELEVATOR HAS LIQUID INGRESS AT 74.5 FROM I/B END, 8IN FROM T RAILING EDGE, 1IN DIAMETER. GENERATED BY V061632 ON HAECO LCQ NR 9292782/34782 ESFR COMPLETE REPAIRED RH ELEVATOR 74.5 IN FROM I/B 8 IN FROMT/E 1.5IN DIAMETE R IAW A320 SRM 55-21-11-300-005 CATEG
- [SDR CALA2025031902957](https://openairdocs.org/sdr/CALA2025031902957.md): Skin · contaminated · Mar 17, 2025 · N462UA · Airbus A320232 · Elevator, Plate/Skin
  > LH ELEVATOR HAS LIQUID INGRESS AT 138 IN FROM INBOARD EDGE, 5.5I NIN FROM TRAILING EDGE, 1IN DIAMETER REPAIRED LH ELEVATOR IAW A320 SRM 55-21-11-300-005
- [SDR CALA2025031702900](https://openairdocs.org/sdr/CALA2025031702900.md): Skin · contaminated · Mar 17, 2025 · N462UA · Airbus A320232 · Elevator, Plate/Skin
  > LH ELEVATOR HAS LIQUID INGRESS AT 52 IN FROM INBOARD EDGE, 5 IN FROM TRAILING EDGE, 2 IN DIAMETER.
- [SDR CALA2025031702853](https://openairdocs.org/sdr/CALA2025031702853.md): Angle · cracked · Mar 14, 2025 · N462UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > RH AFT TI-ANGLE IS CRACKED. ESFR COMPLETED REMOVED SECTION-CONNECTING (TI-ANGLE) ON RH AFT FR41-42 KEEL BEA M IAW A320 SRM 51-42-11/001 REV 152 REPLACED SECTION CONNECTING (TI-ANGLE) IAW A320 SRM 51-42-11/001 REV 152.
- [SDR CALA2025031702852](https://openairdocs.org/sdr/CALA2025031702852.md): Angle · corroded · Mar 13, 2025 · N462UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > L2 PAX DOOR LOWER FWD ANGLE FITTING CORRODED. ESFR COMPLETE R & R CORNER FITTING AT L2 PAX DOOR LWR FWD IAW A320 SRM 51 -42-11 + SRM 51-72-11
- [SDR CALA2025031702851](https://openairdocs.org/sdr/CALA2025031702851.md): Floor Support · corroded · Mar 13, 2025 · N462UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT WET AREA FLOOR SUPPORT Y160.5 FASTENER HOLES CORRODED APPROX. 5 " FWD OF FRM 70. ESFR COMPLETE RMVD CORROSION ON FLOOR SUPPORT Y160.5 FOUND OUT OF LIMITS RMVD DMG FLOOR SUPPORT Y160.5 RECEIVED NEW FLOOR SUPPORT RPLCD COMPONENTS TRANSFERRED DRILL HOLES +
- [SDR CALA2025031702850](https://openairdocs.org/sdr/CALA2025031702850.md): Angle · corroded · Mar 13, 2025 · N462UA · Airbus A320232 · Service Doors
  > R2 DOOR LOWER AFT CORNER ANGLE FITTING CORRODED. ESFR COMPLETE RMVD + RPLCD CORNER FITTING AT RE PAX DOOR LWR AFT IAW A320 SRM 51-42-11 + SRM 51-72-11.
- [SDR CALA2025031402804](https://openairdocs.org/sdr/CALA2025031402804.md): Angle · cracked · Mar 13, 2025 · N462UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > LH AFT TI-ANGLE IS CRACKED. RMVD TI-ANGLE IAW A320 SRM 51-42-11/001 REV.152 RPLCD TI-ANGLE O N LH AFT FRM 41-42 KEEL BEAM IAW A320 SRM 51-42-11/001 REV.152
- [SDR CALA2025021702349](https://openairdocs.org/sdr/CALA2025021702349.md): Battery · no test · Feb 14, 2025 · N462UA · Airbus A320232 · Emergency Lighting
  > OPERATIONAL CHECK OF CABIN EMERGENCY LIGHTS {A3NB-33-3-6012} - FAILED TEST. EPSU BATTERY AFT L MESSAGE CAME UP. REPLACED EMER LIGHT BATTERY AT DOOR 2L. EMER LIGHT TEST AT PTP PANEL PASSED.PARTS USED: 18-3351-3-0001,QTY:1
- [SDR CALA2025010201742](https://openairdocs.org/sdr/CALA2025010201742.md): Outflow Valve · faulted · Dec 31, 2024 · N462UA · Airbus A320232 · Pressure Regulator/Outflow Valve
  > PRESSURIZATION OUTFLOW VALVE STUCK FULL OPEN. UNABLE TO PRESSURI ZE IN AUTO OR MANUAL. ON TAXI OUT, DEICE, TAKE OFF OUTFLOW VALVE STUCK OPEN, FLIGHTCREW HIT DITCHING SWITCH WHILE DEICING STILL DID NOT CLOSE. ON GROUND CABIN PRESSURE SWITCHED TO MANUAL CLOSE AN
- [SDR CALA2023112403459](https://openairdocs.org/sdr/CALA2023112403459.md): Fuel Cap · missing · Nov 23, 2023 · N462UA · Airbus A320232 · Aircraft Fuel System
  > FUEL CAP MISSING AT DEPARTURE. FUEL CAP MISSING AT ARRIVAL. REFUEL CAP NON STOCK SFO. M&E COMPLIED WITH IAW CDL 28A 18-2825-3-0037. REQUEST CDL 28A ADD EMP:401062 DISPATCH DESK: S11 NAME: D.C. DATE: 23-NOV-23- OKAY TO CDL 28A.
- [SDR CALA2023071002210](https://openairdocs.org/sdr/CALA2023071002210.md): Computer · unknown · Jul 8, 2023 · N462UA · Airbus A320232 · Trailing Edge Flap Control System
  > F/CTL FLAP SYS 1 FAULT ON CLB OUT. FLAP IND FLAPS2 AND INDICATI NG NOT RETRACTED. ADDED PHOTO OF PFR PER TSM 27-51-00-810-811-A, PERFORMED SFCC SYSTEM OPERATIONAL AND AMM 27-51-34-400-001. PERFORMED BOTH OPERATIONAL TEST OF THE 31-2750-9-0001,QTY:1 TESTS REF
- [SDR CALA2023050501364](https://openairdocs.org/sdr/CALA2023050501364.md): Hinge · cracked · May 5, 2023 · N462UA · Airbus A320232 · Fuselage, Door Hinge
  > TOILET SERVICE PANEL HAS 2EA CRACKS ONE ABOVE EACH HINIGE REPAIRED TOILET SERVICE PANEL (2EA CRACKS) PER SRM 53-41-79-300- 001. EMP: V934143 WC: 54348 STA: ST ENG BFM ALL INSPECTIONS ACCOMPLISHED ON STENGINEERING NRC 54348 AT BFM
- [SDR CALA2023050501363](https://openairdocs.org/sdr/CALA2023050501363.md): Shear Tie · cracked · May 5, 2023 · N462UA · Airbus A320232 · Fuselage Internal Mounting Structure
  > DURINIG ROTO INSP OF THE FRAME FOOT AT RH FR43. CRACK INDICATION NOTED IN THE FASTNER HOLE AT 3 O''CLOCK (VIEW LOOKING FWD) ON BO TH LAYERS REPAIR BEFORE NEXT FLIGHT REAMED HOLE INCRENNETALLY STEP BY STEPS WITH NDT INSPECTION AFTE R EACH REAMED TO MAX SIZE (0.
- [SDR CALA2023050301323](https://openairdocs.org/sdr/CALA2023050301323.md): Skin · unknown · May 2, 2023 · N462UA · Airbus A320232 · Elevator, Plate/Skin
  > DURING THE THERMOGRAPHIC INSPECTION OFTHE RIGHT ELEVATOR UPPER S URFACE 8EA. WATER INDICATION WERE NOTED AND MARKED IN RED. REMOVED RH ELEVATOR, REPAIRED AND INSTALLED IAW AMM 27-34-41-000 SRM 55-21-11-300-003; SRM 51-75-12; SRM 51-21-11; SRM 55-21-15; -001A;
- [SDR CALA2023050101296](https://openairdocs.org/sdr/CALA2023050101296.md): Panel · cracked · Apr 28, 2023 · N462UA · Airbus A320232 · Fuselage Main, Structure
  > TOILET SERVICE PANEL HAS 2EA CRACKS ONE ABOVE EACH HINIGE
- [SDR CALA2023042401236](https://openairdocs.org/sdr/CALA2023042401236.md): Skin · unknown · Apr 23, 2023 · N462UA · Airbus A320232 · Doors
  > RH FWD AVIONICS DOOR HAS LIGHTING STRIKE REPAIRED FWD AVIONICS DOOR IAW A-320 SRMM 52-41-00-300-001 FIG 01 SHEET 02, THIS REPAIR IS CATEGORY "A" WC# 54341 EMP V936039
- [SDR CALA2023042101213](https://openairdocs.org/sdr/CALA2023042101213.md): Shear Tie · cracked · Apr 21, 2023 · N462UA · Airbus A320232 · Fuselage Internal Mounting Structure
  > DURINIG ROTO INSP OF THE FRAME FOOT AT RH FR43. CRACK INDICATION NOTED IN THE FASTNER HOLE AT 3 O''CLOCK (VIEW LOOKING FWD) ON BO TH LAYERS REPAIR BEFORE NEXT FLIGHT
- [SDR CALA2023041701149](https://openairdocs.org/sdr/CALA2023041701149.md): Door · damaged · Apr 17, 2023 · N462UA · Airbus A320232 · Doors
  > RH FWD AVIONICS DOOR HAS LIGHTING STRIKE REPAIRED FWD AVIONICS DOOR IAW A-320 SRMM 52-41-00-300-001 FIG 01 SHEET 02, THIS REPAIR IS CATEGORY "A" WC# 54341 EMP V936039
- [SDR CALA2023032000800](https://openairdocs.org/sdr/CALA2023032000800.md): Union · defective · Mar 18, 2023 · N462UA · Airbus A320232 · Hydraulic Power System
  > ECAM CAUTION MESSAGE - Y RSVR LO LVL MESSAGE INOP - HYD ECAM PROC COMPLETEDACCUMULATOR STILL OK STARTED PARTIAL REMOVAL OF ACCUMULATOR AS PER AMM TASK 29-13-42-000-001-A UP TO AND INCLUDING STEP 3. D. LOCKING LOG FOR MX TO DETERMINE SOURCE OF LOSS. SERVICED YE
- [SDR CALA2023020600321](https://openairdocs.org/sdr/CALA2023020600321.md): Director · unserviceable · Feb 3, 2023 · N462UA · Airbus A320232 · Communications System
  > EVAC COMMAND ALARMSOUNDED DURING TAKEOFFROLL AT HIGH SPEED. LOCKING DUE TO MULTI CIDS 1 & 2 FAULT AFTER T/O UNLOCKING FOR UPDATE UNABLE TO PRODUCE FAULTS. FOUND FAULT HISTORY OF COMMUNICATION ERRORS IN POST FLIGHT REPORT. PRECAUTIONARILY R&R BOTH CIDS DIRECTOR
- [SDR CALA2022042701091](https://openairdocs.org/sdr/CALA2022042701091.md): Fastener · missing · Apr 27, 2022 · N462UA · Airbus A320232 · Nacelle/Pylon Structure
  > PDA 3 REF LP 8457922 MISSING FASTENER #1 ENGINE PYLON PANEL 472BR LOG GENERATED UNDER GMM 02-30-95.REMOVED PANEL AND INSTALLED NEW NUT PLATE. RE INSTALLED PANEL AS PER LP 8457922
- [SDR CALA2021031500317](https://openairdocs.org/sdr/CALA2021031500317.md): Intercostal · cracked · Mar 12, 2021 · N462UA · Airbus A320232 · Fuselage Main, Frame
  > L1 FR 16, DOOR STOP #7, IB UPPER AND LOWER HOLES HAVE CRACK INDI CATIONS IN INTERCOSTAL @ 5 O''CLOCK DIRECTION PER HAECO LCQ NON R OUTINE 9294084. OPEN
- [SDR CALA2020101601196](https://openairdocs.org/sdr/CALA2020101601196.md): Window · damaged · Oct 16, 2020 · N462UA · Airbus A320232 · Flight Compartment Windows
  > FLY #349 ORD TO IAD. ABOUT 20 MILES OUT OF ORD HEADING EAST. FLEW INTO A HAIL STORM, OUT OF NOWHERE. WAS FLYING AT 250 KNOTS, AT 13,000 FEET. CAPTAINS WINDOW WAS DAMAGED ALMOST EVERY WHERE. FIRST OFFICERS WINDOW HAS A LARGE CRACKS ACROSS WHOLE WINDOW AND 4 HI
- [SDR CALA2020030900613](https://openairdocs.org/sdr/CALA2020030900613.md): Fuel Cap · missing · Mar 8, 2020 · N462UA · Airbus A320232 · Fuel Storage
  > PDA 2 ON WALK AROUND FOUND FUEL CAP MISSING MADE LOGPAGE SDR ADDED PARTS NEEDED PLACED MISSING FUEL CAP ON CDL. DDP COMPLIED WITH. DISPATCH DESK: 12 DATE: 07-MAR-20- CDL APPROVED. PLACED MISSING FUEL CAP ON CDL. DDP COMPLIED WITH. REPLACED MISSING FUEL PANEL

Next page: https://openairdocs.org/aircraft/N462UA/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 = 'N462UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N462UA/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.