# Service difficulty reports: N464UA

A list on [N464UA](https://openairdocs.org/aircraft/N464UA.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 4 · 151 reports

- [SDR CALA2026092419781](https://openairdocs.org/sdr/CALA2026092419781.md): Light · inoperative · Sep 23, 2026 · N464UA · Airbus A320232 · Emergency Lighting
  > EMERGENCY LIGHT AT SEAT 38ABC INOPERATIVE. R & R AISLE SEAT MOUNTED EMERGENCY LIGHT. OPS CHKD OK.
- [SDR CALA2026060116667](https://openairdocs.org/sdr/CALA2026060116667.md): Unknown · abnormal · May 31, 2026 · N464UA · Airbus A320232 · Cabin Equipment/Furnishings
  > LIQUID FOUND IN LEFT SIDE COMPARTMENT BEHIND O2 MASK CLEANED UP RESIDUAL FLUID ON LH SIDE OF FLIGHT DECK, PERFORMED INSPECTION OF SURROUNDING AREA AND ELEC COMPARTMENTS REF AMM 24-00-00. FOUND NO EVIDANCE OF FLUID OR DAMAGE IN ELEC BAYS, NO DAMAGE TO FLIGHT
- [SDR CALA2026022314020](https://openairdocs.org/sdr/CALA2026022314020.md): Packing · damaged · Feb 19, 2026 · N464UA · Airbus A320232 · Engine Oil Pressure
  > RIGHT ENGINE OIL TEMP FLASHING AMBER ON CLMB AT 155-160 DEG. FL270. OIL PRESSURE 170 COMPR INSPECTED MASTER CHIP DETECTOR REF AMM 79-00-00-200-013-A AND FOUND TO BE CLEAN. WILL NEED NEW ORING INSTALLED FOR MM INSTALLATUON. REPLACED O-RINGS ON MASTER CHIP D
- [SDR CALA2026020513595](https://openairdocs.org/sdr/CALA2026020513595.md): Wire · broken · Feb 2, 2026 · N464UA · Airbus A320232 · Light System Wiring
  > SEAT 36CBA EMERGENCY EXIT LIGHT INOP WIRE IS BROKEN FROM SEAT HARNESS CONNECTOR REQUESTING MEL 3350C FOR SEAT 36CBA EMERGENCY EXIT SEAT LIGHT WIRES HAVE BEEN SECURED OKAY TO DEFER EMERGENCY ESCAPE PATH LIGHT PER MEL 3350C CORRECTION SEAT 36CBA FLOOR PROXIMITY
- [SDR CALA2025122912498](https://openairdocs.org/sdr/CALA2025122912498.md): Lgciu · faulted · Dec 25, 2025 · N464UA · Airbus A320232 · Landing Gear Retraction/Extension System
  > MLG LGCIU 1 FAULTED, NR 1 ENG REVERSER, GEAR DOORS WOULDNT CLOSE I NITIALLY. R & R LGCIU 1 FIN (5GA1) IAW AMM 32-31-71-000-001-A, & 32-31-71-400-001-A.. PERFORMED BITE TEST OF LGCIU IAW AMM 32-69-00-740-001-A. LGCIU. 1/2 BITE TEST GOOD. R & R RT MLG PROX
- [SDR CALA2025122312379](https://openairdocs.org/sdr/CALA2025122312379.md): Fuel Cap · missing · Dec 19, 2025 · N464UA · Airbus A320232 · Fuel Storage
  > FUEL CAP MISSING UPON ARRIVAL. VERIFIED NO FUEL LEAKING FROM COUPLING AND INSTALLED INOP STICKER. REPLACED THE FUEL CAP IAW IPC 28-25-05-42B, AND AMM 28-25-41-400-005-A.
- [SDR CALA2025113011588](https://openairdocs.org/sdr/CALA2025113011588.md): Wire Harness · faulted · Nov 29, 2025 · N464UA · Airbus A320232 · Light System Wiring
  > EMERGENCY PATH LIGHTING INOP AT SEAT 23C. REMOVED AND REPLACED EXIT PATH SEAT MOUNTED LIGHT HARNESS. REF AMM 33-51-19-000/400-002-A. OPS CHECKED GOOD AT THIS TIME.
- [SDR CALA2025092409193](https://openairdocs.org/sdr/CALA2025092409193.md): Unknown · odor · Sep 23, 2025 · N464UA · Airbus A320232 · Air Distribution System
  > ODD SMELL IN FLIGHT DECK. SIMILAS TO WET SOCK SMELL. REQUESTI NG MW TO CONFIRM/VERIFY CREW REPORTS WET ODOR. CREW SHEET ATTACHED. REF. AMM TASK 05-51-10-200-801-C-1 VERIFIED NO ELECTRICAL SMELL IN THE E&E BAY FLIGHT DECK OR CABIN.
- [SDR CALA2025090908643](https://openairdocs.org/sdr/CALA2025090908643.md): Power Supply · inoperative · Sep 7, 2025 · N464UA · Airbus A320232 · Emergency Lighting
  > CAPTAIN`S FWD LEFT MESSAGE DISPLAYED AFTER CAPACITY TEST WAS PERFORMED. REMOVED AND REPLACED BATTERY FOR EMERGENCY POWER SUPPLY IAW AMM 33-51-38-000-002-A AND 33-51-38-400-002-A.
- [SDR CALA2025071506596](https://openairdocs.org/sdr/CALA2025071506596.md): None · no discrepancy · Jul 13, 2025 · N464UA · Airbus A320232 · Standard Practices/Structures
  > OIL DRIPPING FROM NR 2 ENG DRAIN MAST INSPECTED ENGINE 2 DRAIN MAST, FOUND DRIPS FROM ACOC. OPENED ENGINE FAN COWLINGS, FOUND NO EVIDENCE OF LEAK AT ACOC, ALL SURFACES UNDER COWLING DRY, AIRCRAFT OK FOR SERVICE AT THIS TIME REF TSM 05-50-00-810-822-A
- [SDR CALA2025070806319](https://openairdocs.org/sdr/CALA2025070806319.md): Bottle · abnormal · Jul 4, 2025 · N464UA · Airbus A320232 · Emergency Equipment
  > LEFT SIDE OVERWING ESCAPE SLIDE RESERVOIR REQUIRES PRECAUTIONARY REPLACEMENT DUE TO EXPOSER TO HIGH TEMP REF LOGPAGE 5426683. REMOVED & REPLACED LH OVER WING SLIDE RESERVOIR PER AMM 25-62-46. REMOVAL AND INSTALL OF LH O/W SLIDE BOTTLE, FOR THE ABOVE AMM,
- [SDR CALA2025070706250](https://openairdocs.org/sdr/CALA2025070706250.md): Bottle · faulted · Jul 2, 2025 · N464UA · Airbus A320232 · Emergency Exits
  > CIDS CAUTION LIGHTS ON AFTER ENG START. -CFDS SHOWING SLIDE BOTTLE EMER L INSPECTED BOTTLE FOR LH OVERWING EMERGENCY SLIDE. TS REF TSM 25-62-00-810-805-A. INSPECTED LT OVERWING INFLATION BOTTLE AND FOUND TO BE APPROXIMATELY IN THE RED BAND. CONTACTED TOMC AND
- [SDR CALA2025052905056](https://openairdocs.org/sdr/CALA2025052905056.md): Control Servo · faulted · May 26, 2025 · N464UA · Airbus A320232 · Stabilizer Actuator
  > TEST FLIGHT DISCREPANCY.. RSP3 ON RIGHT SIDE FLOATED WITH BLUE HYD DEPRESSURIZED. REFLY R EQD. REMOVED AND REPLACED RH #3 SPOILER ACTUATOR IAW A320 AMM 27-64-5 1-400-004-A, 27-64-51-000-004-A OP & ADJUSTMENT CHK GOOD. ACMP B Y V914957 INSP BY V925611ROTABLE P
- [SDR CALA2025052704976](https://openairdocs.org/sdr/CALA2025052704976.md): Skin · corroded · May 25, 2025 · N464UA · Airbus A320232 · Fuel Storage
  > CENTER FUEL TANK TOP SKIN, LH CABIN SIDEWALL, AT FR 41 AROUND APU FUEL FEED LINE HAS CORROSION. ACCOMPLISHED REPAIR INSTRUCTIONS PER HAECO REO-L25437 REV IR ON CENTER FUEL TANK TOP SKIN, LH CABIN AT FR41 AROUND APU FUEL FEED LINE WITH NO DEVIATIONS. ACMP REPA
- [SDR CALA2025052704981](https://openairdocs.org/sdr/CALA2025052704981.md): Window Frame · cracked · May 6, 2025 · N464UA · Airbus A320232 · Fuselage Main, Structure
  > FLIGHTDECK WINDSHIELD CTR POST LOWER NODE, LH SIDE I/B MOST HOLE HAS CRACK INDICATION @ 6 OCLOCK AFT DIRECTION, 90% SH APPROX.0 80 LONG LOWER SURFACE ONLY. INTERIM REPAIR HAS BEEN ACCOMPLISHED PER PART 1 OF ECRA 5311-03362 WITHOUT DEVIATIONS. ORIGINAL DISCRE
- [SDR CALA2025050504449](https://openairdocs.org/sdr/CALA2025050504449.md): Stringer · corroded · May 2, 2025 · N464UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > AFT CARGO LH STRINGER 43 AT FR 56 HAS CORROSION. REMOVED AFT CARGO LH STRINGER 43 CORROSION IAW A320 SRM 51-74-00. PERFORMED NDT INSPECTION IAW NTM51-10-4 AND 51-50-00 STRINGER FOUND OUT OF LIMITS IAW SRM 53-41-13-283-002 FIG 1, ORIGINA L THICKNESS 0.108" R
- [SDR CALA2025052704980](https://openairdocs.org/sdr/CALA2025052704980.md): Door · cracked · May 1, 2025 · N464UA · Airbus A320232 · Passenger/Crew Doors
  > CRACK OF 0.625" APPROX AT LH AFT PASSENGER/CREW DOOR CUTOUT UPPE R RADIUS AT STR 8 AFT FACE INTERIM REPAIR HAS BEEN ACCOMPLISHED PER PART 1 OF ECRA 5341-01489 WITHOUT DEVIATIONS. ORIGINAL DISCREPANCY FOUND ON LCQ 9290288. INSPECTIONS AT INTERVALS NOT TO EX
- [SDR CALA2025050104386](https://openairdocs.org/sdr/CALA2025050104386.md): Door Sill · corroded · Apr 30, 2025 · N464UA · Airbus A320232 · Fuselage Main, Structure
  > AFT CARGO ENTRY DOOR SILL HAS CORROSION. MARKED. BLENDED OUT AND SMOOTHED 03 EACH CORRODED AREA, AT AFT CARGO ENTRY DOOR SILL SKIN, WERE FOUND WITHIN LIMIT LIMITS IAW A320 SRM 53-41-49. REMOVED AND PLACED INTERNAL INTERCOSTAL AT FR 53 AND BTW STR 39R/ 41 R IA
- [SDR CALA2025042404187](https://openairdocs.org/sdr/CALA2025042404187.md): Shear Tie · corroded · Apr 22, 2025 · N464UA · Airbus A320232 · Fuselage Internal Mounting Structure
  > FWD CARGO SHEAR TIE AT FR.30 BETWEEN STR 40R-41R HAS CORROSION. R & R THE SHEAR TIE AT FR30 BETWEEN STR40R-41R IAW A320 SRM 51- 72-11-911-001.
- [SDR CALA2025042404186](https://openairdocs.org/sdr/CALA2025042404186.md): Shear Tie · corroded · Apr 22, 2025 · N464UA · Airbus A320232 · Fuselage Internal Mounting Structure
  > FWD CARGO SHEAR TIE AT FR 31 STR 41R-40R HAS CORROSION. R & R SHEAR TIE AT FR3 BETWEEN STR41R-40R.
- [SDR CALA2025052304921](https://openairdocs.org/sdr/CALA2025052304921.md): Fitting · cracked · Apr 19, 2025 · N464UA · Airbus A320232 · Fuselage Main, Structure
  > FLIGHTDECK WINDSHIELD CTR POST CONTINUITY FITTINGS LH AND RH HAV E CRACK INDICATIONS APPROX.400 IN FRON CTR POST ON HORIZONTAL L EG GENERATED BY V892444 ON HAECO LCQ NR 9290704/42704 ENTERED ESFR COMPLETE RMVD+RPLCD LH RH + LWR CONTINUITY FITTINGS IAW AIRBUS
- [SDR CALA2025041803994](https://openairdocs.org/sdr/CALA2025041803994.md): Channel · broken · Apr 17, 2025 · N464UA · Airbus A320232 · Wing Main, Frame Structure
  > L/H WING FUEL PANEL CUT OUT BETWEEN RIBS 15-16 HAS BROKEN GANG CHANNEL. REMOVED AND REPLACED LH WING FUEL PANEL GANG CHANNEL BETWEEN RIB 15 AND RIB 16 IAW A320 SRM 51-72-11 AND SRM 51-42-11.
- [SDR CALA2025041803993](https://openairdocs.org/sdr/CALA2025041803993.md): Floor Panel · corroded · Apr 17, 2025 · N464UA · Airbus A320232 · Fuselage Floor Panel
  > FWD CARGO SLOPING FLOOR PROFILE AT FR34 STR38R HAS CORROSION. REMOVED AND REPLACED NEW PROFILE ON FWD CARGO PIT FR34 STR 38R-3 5R IAW A320 SRM 51-42-11-001.
- [SDR CALA2025041803991](https://openairdocs.org/sdr/CALA2025041803991.md): Floor Panel · corroded · Apr 17, 2025 · N464UA · Airbus A320232 · Fuselage Floor Panel
  > FWD CARGO FLOOR PROFILE HAS CORROSION BETWEEN FR 33-34 STR38L. REMOVED AND REPLACED NEW PROFILE ON FWD CARGO PIT FROM FR 34 LH TO RH STR 38 IAW A320 SRM 51-42-11-001.
- [SDR CALA2025041803990](https://openairdocs.org/sdr/CALA2025041803990.md): Skin · broken · Apr 17, 2025 · N464UA · Airbus A320232 · Wing, Plate/Skin
  > L/H WING FUEL PANEL CUT OUT BETWEEN RIBS 15-16 HAS BROKEN GANG CHANNEL. REMOVED AND REPLACED LH WING FUEL PANEL GANG CHANNEL BETWEEN RIB 16 AND RIB 17 IAW A320 SRM 51-72-11 AND SRM 51-42-11.
- [SDR CALA2025041803989](https://openairdocs.org/sdr/CALA2025041803989.md): Seat Track · corroded · Apr 17, 2025 · N464UA · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK RH Y-765 PREVIOUS REPAIR FROM FR24-FR25 IS CORRODED OUT OF LIMITS. REPAIRED SEAT TRACK RH Y-768 BETWEEN FR 24-25 IAW A320 SRM 53-11 -15-300-006.
- [SDR CALA2025041803988](https://openairdocs.org/sdr/CALA2025041803988.md): Floor Panel · corroded · Apr 17, 2025 · N464UA · Airbus A320232 · Fuselage Floor Panel
  > FWD CARGO FLOOR PROFILE AT STR38R FR31-34 HAS CORROSION IN MULTI PLE SPOTS. REMOVED AND REPLACED NEW PROFILE PANEL ON FWD CARGO COMPT AT STR 38R FR 31-34 IAW A320 SRM 51-42-11-001.
- [SDR CALA2025041103707](https://openairdocs.org/sdr/CALA2025041103707.md): Floorbeam · cracked · Apr 10, 2025 · N464UA · Airbus A320232 · Fuselage Main, Floor Beam
  > FLIGHT DECK RH FLOOR BEAM WEB ASSEMBLY CRACKED @ FRM 11. REMOVED AND REPLACED FLOOR BEAM WEB BETWEEN FR 8 AND FR 11 Y-765 FLIGHT DECK IAW A320 SRM 51-72-11-911-001 AND SRM 51-42-11.
- [SDR CALA2025041103706](https://openairdocs.org/sdr/CALA2025041103706.md): Frame · worn · Apr 10, 2025 · N464UA · Airbus A320232 · Fuselage Main, Frame
  > FWD CARGO FWD BULKHEAD SUPPORT STRUT WORN/HAS PLAY AT UPPER ATTACH POINT. REMOVED AND REPLACED NEW VERTICAL MEMBER ASSY ON FWD CARGO FWD B ULK HEAD SUPPORT STRUT IAW A320 AMM 25-54-81-400-801-A.
- [SDR CALA2025041403758](https://openairdocs.org/sdr/CALA2025041403758.md): Floor Support · cracked · Apr 9, 2025 · N464UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > FWD CARGO FLOOR PROFILE FROM FR25-27 STR38L CRACKED IN 2 PLACES. D REMOVED AND REPLACED NEW PROFILE PNL ON FWD CARGO FROM FR 25 TO FR 28 STR 38L IAW A320 SRM 51-42-11-001.
- [SDR CALA2025041103701](https://openairdocs.org/sdr/CALA2025041103701.md): Seat Track · corroded · Apr 8, 2025 · N464UA · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK RH Y-1292 PREVIOUS REPAIR FROM FR25-FR26 IS CORRODED OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK RH Y-1292 BETWEEN FR 24 TO FR 25 IAW A320 SRM 51-12-11-911-001.
- [SDR CALA2025041103700](https://openairdocs.org/sdr/CALA2025041103700.md): Floor Support · corroded · Apr 8, 2025 · N464UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > FWD CABIN WET AREA FLOOR SUPPOR +Y765 CORRODED IN MULTIPLE SPOTS AT FR20-24. REPLACED FWD CABIN WET AREA FLOOR SUPPORT Y-765 CORROED AT FR 20-29 IAW A320 SRM 51-42-11-001.
- [SDR CALA2025041103699](https://openairdocs.org/sdr/CALA2025041103699.md): Floor Support · corroded · Apr 8, 2025 · N464UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > FWD CABIN WET AREA FLOOR SUPPORT +Y1292 CORRODED IN MULTIPLE SPOTS AT FR18-24. FLOOR SUPPORT -Y1292 REPLACED FWD CABIN WET AREA FLOOR SUPPORT -Y1292 FR 18-24 IAE A320 SRM 51-42-11-001.
- [SDR CALA2025041103690](https://openairdocs.org/sdr/CALA2025041103690.md): Floor Support · cracked · Apr 8, 2025 · N464UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > FLIGHT DECK UNDERFLOOR WEB ASSY, UNDER PILOT SEAT, AT FR 10-11 IS CRACKED. REMOVED AND REPLACED UNDERFLOOR WEB ASSY AT FR 10-11 IAW A320 SR M 51-42-11-001. RESTORED SURFACE PROTECTION ON WEB ASSY IAW A320 SRM 51-75-12.
- [SDR CALA2025040803642](https://openairdocs.org/sdr/CALA2025040803642.md): Frame · cracked · Apr 4, 2025 · N464UA · Airbus A320232 · Fuselage Main, Frame
  > LH DOUBLE JOGGLE, HOLE #7 HAS A CRACK INDICATION IN FRAME LAYER AT 9 OCLOCK POSITION. GENERATED BY V061632 ON HAECO LCQ NR 92905 26/42526CRACKS IN HOLE #7 (LEADER HOLE) AND HOLE #8 (ASSOCIATED HOLE) RE MOVED IAW EA5311-02442 AND SRM 53-11-12-300-012. AFTER OVE
- [SDR CALA2025032603201](https://openairdocs.org/sdr/CALA2025032603201.md): Door Frame · cracked · Mar 22, 2025 · N464UA · Airbus A320232 · Fuselage Main, Structure
  > LEFT HAND FWD EMER. EXIT FWD FRAME CRACKED. REMOVED AND REPLACED FWD FRAME AT LEFT HAND FWD EMERGENCY EXIT DOOR IAW A320 SRM 51-21-11-911-001. WPB V947030. REMOVED AND REPLACED FWD FRAME AT LEFT HAND FWD EMER EXIT DOOR I AW A320 SRM 51-42-11-911-001.
- [SDR CALA2025022402435](https://openairdocs.org/sdr/CALA2025022402435.md): Arming Lever · stiff · Feb 20, 2025 · N464UA · Airbus A320232 · Passenger/Crew Doors
  > ARMING LEVED DOOR 2R IS JAMMED. DOOR NOT ARMED. OPERATED DOOR, OPS CHECKED GOOD. CLEANED AND LUBED PRECAUTIONARY ARMING LEVER. OK TO FOR SERVICE. OPERATED DOOR, OPS CHECKED GOOD. CLEANED AND LUBED PRECAUTIONARY ARMING LEVER. OK TO FOR SERVICE.
- [SDR CALA2025021102285](https://openairdocs.org/sdr/CALA2025021102285.md): Battery · inoperative · Feb 10, 2025 · N464UA · Airbus A320232 · Emergency Lighting
  > OPERATIONAL CHECK OF CABIN EMERGENCY LIGHTS {A3NB-33-3-6012} - EPSU BATTERY AFT L MAINTENACE MSG ON PTP PERFORMED OPS CHECK OF EPSU REF AMM 33-51-00-710-001-A. MSG WENT AWAY. OPS CHECK GOOD AT THIS TIME.
- [SDR CALA2025012802096](https://openairdocs.org/sdr/CALA2025012802096.md): Line · leaking · Jan 28, 2025 · N464UA · Airbus A320232 · Hydraulic System, Main
  > HYD G RSVR LO LVL NO GREEN SYS HYDRAULICS ALT GEAR EXT AND ALT B RAKING PRECURSORY INSPECTION REVEALED FLUID LEAKING OUT OF NO.1 ENGINE PYLON DRAIN-- EVIDENCE OF FLUID ON PYLON-- REQUIRES PYLON ACCESS PANEL REMOVAL TO ISOLATE LEAK. CREW STATED AS PER THEIR QRH
- [SDR CALA2024123001707](https://openairdocs.org/sdr/CALA2024123001707.md): Battery · failed · Dec 27, 2024 · N464UA · Airbus A320232 · Emergency Lighting
  > FAILED SYSTEM TEST OF EMERGENCY LIGHTS SHOWING EPSU LEFT AND RIGHT FAULTS REPLACE FAULTED EPSU PER TSM 33-51-00-810-801-A PERFORMED ON UNIT BUTE TEST AND VERIFIED BATTERY FAULTS. REMOVED AND REPLACED BATTERIES IAW AMM TASK 33-51-38-400-002-A. PERFORMED EMERGEN
- [SDR CALA2024012300206](https://openairdocs.org/sdr/CALA2024012300206.md): Fuel Cap · missing · Jan 19, 2024 · N464UA · Airbus A320232 · Fuel Storage
  > FUEL CAP MISSING ON AIRCRAFT ARRIVAL AT STATION DFW. PARTS NIS AT DFW. NO LEAKS NOTED AFTER FUELING AT DFW. CDL APPLIED. CONDITION DEFERRED. INSTALLED NEW FUEL CAP REF 28-25-45.
- [SDR CALA2023122103701](https://openairdocs.org/sdr/CALA2023122103701.md): Controller · faulty · Dec 18, 2023 · N464UA · Airbus A320232 · Cabin Pressure Controller
  > SYS 1 AND 2 FAULT DISPLAYED ON UPPER ECAM SCREEN. - CAB PR UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. PERFORM CPC TESTING AND ADVISE TOMC UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE
- [SDR CALA2023071202236](https://openairdocs.org/sdr/CALA2023071202236.md): Fuel Cap · missing · Jul 7, 2023 · N464UA · Airbus A320232 · Fuel Storage
  > PDA 3 REFUEL CAP MISSING ON ARRIVAL. NO FUEL LEAK NOTED. INSTALLED NEW CAP COUPLER REFUEL REF AMM 28-25-41 PARTS USED: 31-2825-9-0001. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1507625 SN OFF 0001
- [SDR CALA2023052901685](https://openairdocs.org/sdr/CALA2023052901685.md): Frame · cracked · May 26, 2023 · N464UA · Airbus A320232 · Fuselage Main, Frame
  > REV B (AD 2020-18-06) HFEC ROTO INSPECTION OF L/H FRAME FOOT 43 FASTENER HOLE FOUND HOLE CRACKED AT 3 AND 9 OCLOCK POSITIONS IN FRAME. CRACK, EXTREAMLY LARGE, APPEARS VISUALLY AS WELL. REPAIR BEFOR NEXT FLIGHT (EA 5330-06692 001) GENERATED AT HAECO LCQ PER NR
- [SDR CALA2023052601660](https://openairdocs.org/sdr/CALA2023052601660.md): Fitting · unknown · May 25, 2023 · N464UA · Airbus A320232 · Fuselage Main, Attach Fittings
  > PERFORM A INTERIM REPAIR AT R/H KEEL BEAM AND MLG DOOR ACTUATOR FITTING AS PER ECRA #5300-02905
- [SDR CALA2023052601659](https://openairdocs.org/sdr/CALA2023052601659.md): Fitting · unknown · May 25, 2023 · N464UA · Airbus A320232 · Fuselage Main, Attach Fittings
  > PERFORM A INTERIM REPAIR AT R/H KEEL BEAM AND MLG DOOR ACTUATOR FITTING AS PER ECRA #5300-02905.
- [SDR CALA2023052601658](https://openairdocs.org/sdr/CALA2023052601658.md): Skin · damaged · May 25, 2023 · N464UA · Airbus A320232 · Elevator, Plate/Skin
  > R/H ELEVATOR UPPER SKIN PANEL PRODUCED AN INDICATION OF WATER IN GRESS 117 INCHES OTBD FROM THE INBD EDGE AND 11.25 INCHES FWD OF T/E DURING IRT THERMOGRAGHIC INSPECTION PER HAECO LCQ NON ROUTI NE CARD 9296373/42373. DRILLED WITTNESS HOLES IN RH ELEVATOR UPPE
- [SDR CALA2023052401636](https://openairdocs.org/sdr/CALA2023052401636.md): Door Sill · corroded · May 23, 2023 · N464UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT MAIN CABIN R2 DOOR SILL HAS CORROSION AT NUT PLATE HOLE FR68 A3NB-53-3-6222 PER HAECO LCQ NON ROUTINE 9296365/42365 GENERATE D BY V052030 REMOVED AND REPLACED R2 DOOR SILL IAW A320 SRM 51-72-11 ACMP BY MECH V052030 INSP BY V061771
- [SDR CALA2023052401634](https://openairdocs.org/sdr/CALA2023052401634.md): Fitting · corroded · May 23, 2023 · N464UA · Airbus A320232 · Fuselage Main, Attach Fittings
  > MAIN CABIN R2 DOOR SILL AFT CORNER FITTING HAS CORROSION. GEN AT HAECO LCQ BY V052030 PER NR 9296366(42366) REMOVED AND REPLACED AFT MAIN CABIN R2 DOOR SILL AFT CORNER FITT ING IAW A320 SRM 51-72-11-911-001. ACMP BY V929087
- [SDR CALA2023052201601](https://openairdocs.org/sdr/CALA2023052201601.md): Door Sill · corroded · May 21, 2023 · N464UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT MAIN CABIN L2 DOOR SILL HAS CORROSION AT NUT PLATE HOLE FRAM E 68 (A3NB-53-3-6222) GENERATED AT HAECO LCQ PER NR 9296416 (424 16). INSTALLED/REPAIRED ANGLE AR FR68 AFT NUTPLATE, AFTER CABIN L2 DO OR SILL IAW A320 SRM 53-41-14-300-001. SRM 51-42-11/001,F, S

Next page: https://openairdocs.org/aircraft/N464UA/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 = 'N464UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N464UA/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.