# Service difficulty reports: N466UA

A list on [N466UA](https://openairdocs.org/aircraft/N466UA.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 · 115 reports

- [SDR CALA2026083119035](https://openairdocs.org/sdr/CALA2026083119035.md): Blades · damaged · Aug 27, 2026 · N466UA · Airbus A320232 · Engine (Turbine/Turboprop)
  > NUMBER 1 ENG STALLED ON TAKEOFF, LOW SPEED ABORT ENG 1 VIB 5.4. ALSO METAL ODOR IN FLT DECK SMOKE, POST FLIGHT REPORT IAW TSM 71-00-00-810-808-A, ACP. B.S.I. OF HPC STAGES 3 & 4 ON ENG NR 1 IAW AMM 72-00-00-200-016. FOUND 2 BLADES MISSING ON HPC 3, ONE OF
- [SDR CALA2026062217247](https://openairdocs.org/sdr/CALA2026062217247.md): Button · faulted · Jun 20, 2026 · N466UA · Airbus A320232 · Electrical Power System
  > FAULT ON CLIMB OUT. REPLACED BCL 2, OPS CHECKED GOOD. ELEC BCL 2 FAULT CHECKED PFR, FOUND MESSAGE SDAC1: NO DATA FROM BCL2. REF TSM 24-30-00-810-806-A. PERFORMED OPS TEST OF THE CENTRAL WARNING SYS IAW AMM 31-50-00-710-001-A. VERIFIED FAULT WAS PRESENT. REM
- [SDR CALA2025082208046](https://openairdocs.org/sdr/CALA2025082208046.md): Battery · faulted · Aug 21, 2025 · N466UA · Airbus A320232 · Emergency Lighting
  > BITE FAULT: EPSU BATTERY EMER R REPLACED EPSU BATTERY AT POSITION BATT. EMER R IAW AMM 33-51-38, OPS TEST GOOD.
- [SDR CALA2025082208045](https://openairdocs.org/sdr/CALA2025082208045.md): Battery · faulted · Aug 21, 2025 · N466UA · Airbus A320232 · Emergency Lighting
  > BITE FAULT: AFT L REPLACED EPSU BATTERY AT POSITION AFT L IAW AMM 33-51-38, OPS TEST GOOD.
- [SDR CALA2025080507296](https://openairdocs.org/sdr/CALA2025080507296.md): Light · inoperative · Aug 1, 2025 · N466UA · Airbus A320232 · Emergency Lighting
  > RIGHT FWD DOOR EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE. MOUNTING ON BASE OF LIGHT ALSO BROKEN. REMOVED AND REPLACED EXIT LIGHT IAW AMM 33-51-13. OPS CHECKED GOOD.
- [SDR CALA2025072806984](https://openairdocs.org/sdr/CALA2025072806984.md): Power Supply · no test · Jul 27, 2025 · N466UA · Airbus A320232 · Emergency Lighting
  > PROCEDURE - TEST FAILED WITH MSG "EPSU COMM FWD L" SEE PIC ABOVE SHOULD READ EMERGENCY LIGHTING TEST PROCEDURE- PERFORMED TSM 33-51-00, FOUND EPSU COMM FWD LEFT FAULT. TESTED EPSU 10WL REF STEP 4B-1A NO EPSU LED'S CAME ON. REPLACED EPSU 10WL REF AMM 33-51-38.
- [SDR CALA2025072106779](https://openairdocs.org/sdr/CALA2025072106779.md): Power Supply · no test · Jul 18, 2025 · N466UA · Airbus A320232 · Emergency Lighting
  > OPERATIONAL CHECK OF THE EMERGENCY POWER SUPPLY UNITS BY BITE-CHECK EMERGENCY LIGHTS FAIL TEST AT CIDS PANEL. FAULT EPSU INT LOAD FWD L ATA 33-51-38. CYCLED BREAKERS NO HELP. REMOVED CEILING PANEL AT DOOR 1 LEFT. DID TEST OF LIGHTING BOX FAULTING INTERIOR LIG
- [SDR CALA2025070706232](https://openairdocs.org/sdr/CALA2025070706232.md): Light · faulted · Jul 2, 2025 · N466UA · Airbus A320232 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS REMAIN ILLUMINATED IN ALL MODES. POWERED DOWN AIRCRAFT COMPLETELY FOR 3 MINUTES. POWERED BACK UP, CYCLED NO SMOKING LIGHTS SWITCH AND SEAT BELT LIGHT SWITCH PER TROUBLESHOOTING MANUAL (TSM) 33-51-00-810-881-A. EMERGENCY LIGHTS STAYED OFF
- [SDR CALA2025013002121](https://openairdocs.org/sdr/CALA2025013002121.md): Wire Harness · detached · Jan 28, 2025 · N466UA · Airbus A320232 · Light System Wiring
  > EMERGENCY EXIT PATHWAY LIGHT INOP AT SEAT 21C. FOUND EMERGENCY EXIT PATHWAY LIGHT HARNESS DETACHED AT JUNCTION OF SEAT 21A. REATTACHED HARNESS. OPS CHECKED GOOD.
- [SDR CALA2024112201240](https://openairdocs.org/sdr/CALA2024112201240.md): Transmitter · faulty · Nov 20, 2024 · N466UA · Airbus A320232 · Engine Oil Quantity
  > RIGHT ENG OIL QTY DROPPED EXTREMELY LOW THEN 0 AND ECAM ENG WRN REQUESTING MEL 7931B FOR OIL INDICATION ON THE #2 ENGINE INOP VERFIED OIL SERVICE IS FULL AND THERE IS NO OIL LEAKAGE, CONFIRMED WITH CREW OIL PRESSURE AND TEMP. WAS GOOD #2 ENGINE OIL QTY INDICAT
- [SDR CALA2024111401142](https://openairdocs.org/sdr/CALA2024111401142.md): Battery · discharged · Nov 12, 2024 · N466UA · Airbus A320232 · Emergency Lighting
  > OPERATIONAL CHECK OF CABIN EMERGENCY LIGHTS {A3NB-33-3-6012} - EPSU BITE FAIL UNIT EMER R SEE PHOTO. LOCATION R/H OVERWING EXIT. SLAVED NEW EPSU AT R/H EMERGENCY OVERWING EXIT, REF AMM 33-51-38-400-001-A. NO GO. RE-INSTALLED EPSU REF AMM 33-51-38-400-001-A. SW
- [SDR CALA2024110601045](https://openairdocs.org/sdr/CALA2024110601045.md): Control Servo · faulted · Nov 3, 2024 · N466UA · Airbus A320232 · Landing Gear Steering System
  > ECAM WHEEL N/W STRG FAUL T IN CRUISE FL340 T/S PER TSM REF. 32-51-00-810-826-A, REMOVED AND REPLACED N/W STEERING SERVO CTL PER AMM REF. 32-51-51-000-001-A, FOUND CONNECTOR CLOCKED DIFFERENT. ADDED ROTABLE PARTS CHANGE INFORMATION. ROTABLE PARTS CHANGE WAS IND
- [SDR CALA2023122603727](https://openairdocs.org/sdr/CALA2023122603727.md): Frame · cracked · Dec 21, 2023 · N466UA · Airbus A320232 · Fuselage Main, Frame
  > AT C-CHECK IN BFM, DURING INSPECTION OF FWD FACE OF FR 35 LH SIDE BTWN STRG 30 AND STRG 31 WAS FOUND CRACK. REPAIR ACCOMPLISHED IAW ECRA 5331-02600 ON VTMAE N/R 81943. THE LATEST REVISION OF EC/RA 5331-02600. PLANNING TO CONTACT ENGINEERING AFTER APRIL 14, 202
- [SDR CALA2023121803662](https://openairdocs.org/sdr/CALA2023121803662.md): Shock Absorber · unknown · Dec 14, 2023 · N466UA · Airbus A320232 · Main Landing Gear Strut/Axle/Truck
  > RIGHT MAIN LANDING GEAR REQUIRES SHOCK ABSORBER PRESSURE CHECK DUE TO FULL STRUT SERVICING, AFTER FIVE (5) LANDINGS BUT NOT TO EXCEED TWENTY (20) LANDINGS AFTER THE FIRST SUBSEQUENT FLIGHT. 20 LANDINGS PER AMM 12-14-32-614-003-A. REF. GMM 05-30-15. INITIATED D
- [SDR CALA2023112903505](https://openairdocs.org/sdr/CALA2023112903505.md): Skin · corroded · Nov 27, 2023 · N466UA · Airbus A320232 · Nacelle/Pylon, Plate/Skin
  > #2 PYLON AFT FIXED FAIRING SKIN HAS CORROSION ON OTBD SIDE. REPLACED SKIN PANEL AT AFT FIXED FAIRING #2 IAW A-32O SRM 51-72- 11 AND INSTALLED IAW SRM 51-42-11 AND DRAWING D54510054, RECEIVE D SKIN PANEL P/N= D54530052522100, B/N= 0004191346. EMP: V936039 WC: 8
- [SDR CALA2022081002009](https://openairdocs.org/sdr/CALA2022081002009.md): Sensor · faulty · Aug 10, 2022 · N466UA · Airbus A320232 · Fuel Control/Reciprocating Engines
  > **RTBL** LOW SPEED RTO ENGINE 1 ACCELERATION ABNORMAL TROUBLESHOOT NO FAILURE MESSAGES ON MAINTENANCE POST FLIGHT REPORT AFFILIATED WITH NUMBER 1 ENGINE. GROUND SCANNING AND LAST LEG REPORT SHOWS NO FAULT. SCHEDULED MAINTENANCE REPORT HAS P2 T2/ ADIRS1/2/EE
- [SDR CALA2022013100269](https://openairdocs.org/sdr/CALA2022013100269.md): Connector · unsafetied · Jan 31, 2022 · N466UA · Airbus A320232 · Engine Oil System (Airframe Furnished)
  > *EMERGENCY DECLARED* ENGINE 1 H.O.C. DUE TO 10 QTS OF OIL ADDED. RUN ENGINE AT IDLE FOR 5 MINUTES ENGINE REQUIRES EXTERNAL INSPECTION FOR OIL LEAKS, IF NONE FOUND CONTACT TOMC EMC FOR FURTHER INSTRUCTIONS.. LOCKED FOR TROUBLESHOOTING UNLOCKED LOGPAGE TO DOCUME
- [SDR CALA2022011000082](https://openairdocs.org/sdr/CALA2022011000082.md): Intercostal · cracked · Jan 8, 2022 · N466UA · Airbus A320232 · Fuselage Structure (General)
  > R/H FR 16 DOORSTOP FITTING #7 HAS CRACK INDICATION NOTED IN HOLE #1 & #3 TO READ AS FOLLOWS: "ACCOMPLISH INSPECTION REQUIREMENTS PER PART AFT REACHES 39,510 TOTAL FLIGHT CYCLES. ACCOMPLISH REPEAAT INSPE R." REFF VT MAE NRC 0020970 FOR WORK PERFORMED. 2A OF LAT
- [SDR CALA2022011000080](https://openairdocs.org/sdr/CALA2022011000080.md): None · cracked · Jan 7, 2022 · N466UA · Airbus A320232 · Fuselage Structure (General)
  > L/H FR 16 DOORSTOP FITTING #7 HAS CRACK INDICATION NOTED IN HOLE #1 & #3 READ AS FOLLOWS: "ACCOMPLISH INSPECTION REQUIREMENTS PER PART 2A AFT REACHES 39,510 TOTAL FLIGHT CYCLES. ACCOMPLISH REPEAT INSPEC " REFF VT MAE NRC 0020933 FOR WORK PERFORMED. 2A OF LATES
- [SDR CALA2022011000079](https://openairdocs.org/sdr/CALA2022011000079.md): None · cracked · Jan 7, 2022 · N466UA · Airbus A320232 · Fuselage Structure (General)
  > R/H FR 16 DOORSTOP FITTING #1 HAS CRACK INDICATION NOTED IN HOLE #3 D AS FOLLOWS: "ACCOMPLISH INSPECTION REQUIREMENTS PER PART 2A OF ACHES 39,510 TOTAL FLIGHT CYCLES. ACCOMPLISH REPEAT INSPECTIONS VT MAE NRC 0020971 FOR WORK PERFORMED. LATEST REVISION OF EC/RA
- [SDR CALA2022011000078](https://openairdocs.org/sdr/CALA2022011000078.md): None · none · Jan 7, 2022 · N466UA · Airbus A320232 · Cabin Equipment/Furnishings
  > (A3NB-21-3-6032) WATER FOUND COMING FROM LAV DRAINS BETWEEN FR 8 THRU FR21.() ACCOMPLISHED ECRA 2011-01000 "SPILLAGE WAS ONLY POTABLE WATER" E MP# V936637 WORK ACCOMPLISHED AT ST ENGINEERING AEROSPACE OF MOB ILE AT BFM ON NR# 0021202.
- [SDR CALA2022011000077](https://openairdocs.org/sdr/CALA2022011000077.md): None · cracked · Jan 7, 2022 · N466UA · Airbus A320232 · Fuselage Structure (General)
  > L/H FR 20 DOORSTOP FITTING #1 HAS CRACK INDICATION NOTED IN HOLE #1 & #3 READ AS FOLLOWS: "ACCOMPLISH INSPECTION REQUIREMENTS PER PART 2B REACHES 40,010 TOTAL FLIGHT CYCLES. ACCOMPLISH REPEAT INSPECTION FF VT MAE NRC 0020973 FOR WORK PERFORMED. OF LATEST REVIS
- [SDR CALA2022011000076](https://openairdocs.org/sdr/CALA2022011000076.md): Fitting · cracked · Jan 7, 2022 · N466UA · Airbus A320232 · Fuselage Structure (General)
  > WHILE AT VT AREOSOACE BFM DURING C-1 CHECK REF NR0021094 ROTO PROBE OF RH FR66 #5 DOOR STOP FITTING HOLE D1 FOUND CRACK INDICA TION. PLUG & WASHER IAW SRM 53-73-12-001. RE-INSTALLED DOORSTOP FITTIN EMBODIMENT 33000FC (FH NOT RELAVENT) SUBSEQUENT INSP AT INTERV
- [SDR CALA2022011000075](https://openairdocs.org/sdr/CALA2022011000075.md): Intercostal · corroded · Jan 7, 2022 · N466UA · Airbus A320232 · Fuselage Structure (General)
  > L/H FR 20 DOORSTOP FITTING #7 HAS CRACK INDICATION NOTED IN HOLE #3 AS FOLLOWS: "ACCOMPLISH INSPECTION REQUIREMENTS PER PART 2B OF L AS FOLLOWS: "ACCOMPLISH INSPECTION REQUIREMENTS PER PART 2B OF L CHES 40,010 TOTAL FLIGHT CYCLES. ACCOMPLISH REPEAT INSPECTIONS
- [SDR CALA2022010700066](https://openairdocs.org/sdr/CALA2022010700066.md): Stop Fitting · cracked · Jan 6, 2022 · N466UA · Airbus A320232 · Fuselage Main, Structure
  > RH-FR66, DOOR STOP #1, LOWER INBOARD HOLE HAS CRACK INDICTION.() SUPPORT TASK AD 2018-03-12. R/H FR66 #1 LOWER I/B HOLE. REPAIED AND REAMED IAW SRM 53-41-12- ATTACHED EMP# V934344 WORK ACCOMPLISHED AT ST ENGINEERING AEROSP 300-10. ORG REAMED.394 FINAL DIA..4
- [SDR CALA2022010700065](https://openairdocs.org/sdr/CALA2022010700065.md): Stop Fitting · cracked · Jan 6, 2022 · N466UA · Airbus A320232 · Fuselage Main, Structure
  > RH-FR66, DOOR STOP #4, UPPER INBOARD HOLE HAS CRACK INDICATION.() SUPPORT TASK AD 2018-03-12 R/H FR66 #4 DOOR STOP UPPER I/B HOLE. REPAIRED AND REAMED IAW SR FORM 44-0008 ATTACHED. EMP# V934344 WORK ACCOMPLISHED AT ST ENGI M 53-41-12-300-10. ORG. REAMED.394
- [SDR CALA2022010700064](https://openairdocs.org/sdr/CALA2022010700064.md): Drain · leaking · Jan 6, 2022 · N466UA · Airbus A320232 · Ice/Rain Protection System
  > WITHIN 36 MONTHS, ACCOMPLISH ECRA 2011-01000, CARGO COMPARTMENT SPILL SECTION 2.C. SUPPLEMENTAL INSPECTION,IN THE AREA FROM BODY STATION 8 TO BODY STATION 21 BETWEEN STRINGERS 10 AND STRINGER 12. THE AREA FROM BODY STATION 8 TO BODY STATION 21 BETWEEN STRING
- [SDR CALA2022010700063](https://openairdocs.org/sdr/CALA2022010700063.md): Stop Fitting · cracked · Jan 6, 2022 · N466UA · Airbus A320232 · Fuselage Main, Structure
  > RH-FR66, DOOR STOP #5, LOWER INBOARD HOLE HAS CRACK INDICATION.() SUPPORT TASK AD 2018-03-12 R/H FR66 #5 DOOR STOP LOWER HOLE. REPAIRED AND REAMED IAW SRM 53 44-0008 ATTACHED EMP# V934344 WORK ACCOMPLISHED AT ST ENGINEERIN -41-12-300-10. ORG. REAMED.394 FIN
- [SDR CALA2022010700062](https://openairdocs.org/sdr/CALA2022010700062.md): Stop Fitting · cracked · Jan 6, 2022 · N466UA · Airbus A320232 · Fuselage Main, Structure
  > RH-FR68, DOOR STOP #6, LOWER INBOARD HOLE HAS CRACK INDICATION.() SUPPORT TASK AD 2018-03-12. R/H FR68 #6 DOOR STOP LOWER I/B HOLE REPAIRED AND REAMED IAW SRM FORM 44-0008 ATTACHED EMP# V934344 WORK ACCOMPLISHED AT ST ENGIN 53-41-12-300-10 ORG. REAMED.394 FI
- [SDR CALA2022010700061](https://openairdocs.org/sdr/CALA2022010700061.md): Stop Fitting · cracked · Jan 6, 2022 · N466UA · Airbus A320232 · Fuselage Main, Structure
  > RH- FR66, DOOR STOP #6, LOWER INBOARD HOLE HAS CRACK INDICATION. () SUPPORT TASK AD 2018-03-12 R/H FR66 #6DOOR STOP LOWER I/B HOLE. REPAIRED AND REAMED IAW SRM FORM 44-0008 ATTACHED. EMP# V934344 WORK ACCOMPLISHED AT ST ENGI 53-14-12-300-10. ORG. REAMED.394 F
- [SDR CALA2021112302168](https://openairdocs.org/sdr/CALA2021112302168.md): Drain Line · cracked · Nov 23, 2021 · N466UA · Airbus A320232 · Engine Oil System (Airframe Furnished)
  > #2 ENG DRAIN MAST HAS DRAIN LINE( A.C.O.C) CRACKED THRU TUBE OVER 180 DEGREES. LOCATED A BRAZED AREA. UPDATE TO SDR. REMOVED #2 ENGINE DRAIN MAST AND REPLACED IT WITH A NEW ONE
- [SDR CALA2020091501096](https://openairdocs.org/sdr/CALA2020091501096.md): Pump · failed · Sep 8, 2020 · N466UA · Airbus A320232 · Hydraulic Pump (Electric/Engine), Main
  > Y ENG 2 PUMP LO PR DISPLAYED ON UPPER ECAM SCREEN. HYD APPEARED AT CRUISE FL350 PARTS UPDATE INSTALL KIT. REPLACED CASE DRAIN FILTER, THRUST REVERSER HCU FILTER AND HP FILTER, NO PARTICLES FOUND. REMOVED AND REPLACED NR 2 ENG HYD PUMP, IAW 29-13-51. OPS C
- [SDR CALA2020020800344](https://openairdocs.org/sdr/CALA2020020800344.md): Frame · cracked · Feb 5, 2020 · N466UA · Airbus A320232 · Fuselage Main, Frame
  > FR35 AND 10 CM, AT STR30 L/H SIDE, HOLE NO. 2 HAS A CRACK INDICA TION ON HAECO LCQ REF 9298240 SPEC A3NB-53-3-6315. ACCOMPLISHED INTERIM REPAIR PER EC/RA 5331-02600. ACCOMPLISH PERMANENT REPAIR AT HOLE 2 FR 35 STR 30LH PER PART 3 OF EC/RA ON OR BEFORE 30JUL20
- [SDR CALA2020020870332](https://openairdocs.org/sdr/CALA2020020870332.md): Door Frame · corroded · Feb 3, 2020 · N466UA · Airbus A320232 · Fuselage Main, Structure
  > AFT CARGO COMPARTMENT DOOR CUTOUT, BOX BEAM UPPER SKIN, FR 52.5- 56 STGR 39R-41R, MULTIPLE AREAS OF CORROSION - {A3NB-53-4-6179} - REMOVED AND REPLACED AFT CARGO COMPARTMENT DOOR CUTOUT BOX BEAM UPPER SKIN AT FR52.5-56 STR 39R-41R IAW A320 SRM 51-72-11-911-00
- [SDR CALA2020020200306](https://openairdocs.org/sdr/CALA2020020200306.md): Skin · corroded · Jan 29, 2020 · N466UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > LAV EXHAUST VENT EXTERIOR SKIN HAS CORROSION AT LOWER SURFACE AN D AROUND THE EDGE (EA 5100-02750 REV. A). BLEND CORRODED AREA LAV VENT EXHAUST. FOUND TO BE BEYOND ALLOWAB LE LIMITS AND REPAIRED AREA IAW A320 SRM 53-41-11-300-004 FIG 00 1 PG 1-6. ORG THICKNE
- [SDR CALA2020020200290](https://openairdocs.org/sdr/CALA2020020200290.md): Door Frame · corroded · Jan 27, 2020 · N466UA · Airbus A320232 · Fuselage Main, Structure
  > AFT CABIN DOOR CUTOUT FR68 ST22L-23L FWD FACE HAS CORROSION PER HAECO LCQ NR LP 9299010 CORROSION FOUND OUT OF LIMITS AROUND ANCHOR NUT AT FR 68 STRG 22 L-23L.ACCOMPLISHED REPAIR IAW SRM 53-41-12-300-002 PARAGRAPH 2 F IG 001.REQUIRES DETAILED VISUAL INSPECTIO
- [SDR CALA2020020200280](https://openairdocs.org/sdr/CALA2020020200280.md): Shear Tie · not reported · Jan 26, 2020 · N466UA · Airbus A320232 · Fuselage Internal Mounting Structure
  > REMOVED AND REPLACED CLEAT AT FR 3 STR 39R-40R IAW A320 SRM 51-7 2-11-911-001-A PARA 2 (D) - REMOVED AND REPLACED CLEAT AT FR 3 STR 39R-40R IAW A320 SRM 51-7 2-11-911-001-A PG 2 (D)-
- [SDR CALA2020020210274](https://openairdocs.org/sdr/CALA2020020210274.md): Intercostal · corroded · Jan 24, 2020 · N466UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > REMOVED AND REPLACED CORRODED INTERCOSTAL IAW A320 SRM 51-72-11- 911-001. REMOVED AND REPLACED CORRODED INTERCOSTAL IAW A320 SRM 51-72-11- 911-001.
- [SDR CALA2020012600255](https://openairdocs.org/sdr/CALA2020012600255.md): Fitting · corroded · Jan 23, 2020 · N466UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > L2 DOOR CUTOUT LOWER FWD CORNER FITTING HAD CORROSION ON THE SURFACE. REMOVED AND REPLACED AFT CABIN L2 DOOR SILL LOWER FWD CORNER FITTING AT FRAME 66, STRINGER 23L IAW SRM 51-72-11-911-001, PARAGRAPH 20.
- [SDR CALA2020012600260](https://openairdocs.org/sdr/CALA2020012600260.md): Door Sill · corroded · Jan 23, 2020 · N466UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > L-2 DOOR SILL HAS SEVERAL AREAS OF CORROSION PRESENT ON FWD AND AFT SURFACES. REMOVED AND REPLACED L-2 DOOR SILL IN AFT CABIN BETWEEN FRAME 66 TO FRAME 68 AT STRINGER 23L IAW SRM 51-72-11-911-001 PARA D.
- [SDR CALA2020012600259](https://openairdocs.org/sdr/CALA2020012600259.md): Fitting · corroded · Jan 23, 2020 · N466UA · Airbus A320232 · Fuselage Main, Attach Fittings
  > L-2 PASS/CREW DOOR CUTOUT LWR AFT CORNER FITTING HAS CORROSION O N SURFACE. REMOVED AND REPLACED AFT CABIN L-2 DOOR SILL LOWER AFT CORNER FI TTING AT FRAME 68 AT STRINGER 23L IAW SRM 51-72-11-911-001 PARA 2D
- [SDR CALA2020011000115](https://openairdocs.org/sdr/CALA2020011000115.md): Fitting · cracked · Jan 8, 2020 · N466UA · Airbus A320232 · Fuselage Main, Keel
  > RMLG DOOR ACTUATOR KEEL BEAM FITTING AFT SECTION UPPER SURFACE P RODUCED A CRACK INDICATION DURING HFEC INSPECTION EA 5330-04821 AD 2015-02-14 PER HAECO LCQ NR 9298541 GENERATED REMOVED AND REPLACED RMLG DOOR ACTUATOR KEEL BEAM FITTING AFT IA W A320 SRM 51-72-
- [SDR CALA2020010600105](https://openairdocs.org/sdr/CALA2020010600105.md): Shear Plate · corroded · Jan 6, 2020 · N466UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > R/H AFT CABIN SHEAR PLATE AND FRAME SUPPORT STRUCTURE LOCATED BE NEATH FLOOR BOARDS BETWEEN FR 69-70 HAS CORROSION PRESENT ON BOT H SURFACES SUPPORT TASK PER HAECO LCQ NR 9294809 GENERATED REMOVED AND REPLACED R/H AFT CABIN SHEAT PLATE BETWEEN FR69-FR70 IAW A3
- [SDR CALA2020010600099](https://openairdocs.org/sdr/CALA2020010600099.md): Fitting · corroded · Jan 5, 2020 · N466UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > R2 DOOR AT FR68 AFT CORNER FITTING HAS CORROSION PER HAECO LCQ N R LP 9299034 GENERATED REMOVED CORROSION FROM R2 DOOR AFT CORNER FITTING IAW A320 SRM 5 1-74-00-801 PARA 5.A4 FOUND TO BE OUT OF LIMITS WITH.140IN MATE RIAL LOSS FROM EDGE OF FITTING LEAVING INS
- [SDR CALA2020010600035](https://openairdocs.org/sdr/CALA2020010600035.md): Support · corroded · Dec 24, 2019 · N466UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > RH AFT SHEAR PLATE SUPPORT HAS CORROSION ON UPPER SURFACE UNDER SHEAR PLATE SUPPORT TASK PER HAECO LCQ NR 9298900 GENERATED REMOVED AND REPLACED R/H AFT SHEAR PLATE SUPPORT IAW A320 SRM 51 -72-11-911-001 WORK ACCOMPLISHED INSPECTED
- [SDR CALA2019121902241](https://openairdocs.org/sdr/CALA2019121902241.md): Stringer · corroded · Dec 18, 2019 · N466UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > AFT CARGO PITT ON STGR 42 BTWEEN FRAMES 55 TO FRAME 58 STGR IS C ORRODED SEE DOT DD01 (A3NB-05-3-6026). REMOVED AND REPLACED WITH NEW STRINGER 42L FROM FR53 TO FR60 ON AFT CARGO COMPARTMENT IAW A320 SRM 51-42-11-801 AND 51-22-11-911 -001.
- [SDR CALA2019121702224](https://openairdocs.org/sdr/CALA2019121702224.md): Shear Plate · corroded · Dec 16, 2019 · N466UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > L/H AFT CABIN SHEAR PLATE LOCATED BENEATH FLOOR BOARDS BETWEEN F R69-70 HAS CORROSION PRESENT ON SURFACE. REMOVED AND REPLACED SHEAR PLATE AT LH AFT CABIN LOCATED BENEATH FLOOR BOARD BETWEEN FR69-FR70 IAW A320 SRM 51-72-11-911-001.
- [SDR CALA2018012700364](https://openairdocs.org/sdr/CALA2018012700364.md): Bottle · defective · Jan 27, 2018 · N466UA · Airbus A320232 · Escape Slide
  > SLIDE BOTTLE EMER L MESSAGE ON POSTTEST FLT. R&R SLIDE RESERVOIR EMERG OVER WING LT IAW AMM 25-62-46-000-001-A.
- [SDR CALA2017100903574](https://openairdocs.org/sdr/CALA2017100903574.md): Battery Pack · no test · Oct 9, 2017 · N466UA · Airbus A320232 · Emergency Lighting
  > EMERGENCY LIGHT BATTERY FAILED A BITE CHECK. REPLACED THE BATTERY PACK. SYSTEM CHECKED OK. VERIFIED BITE TEST, SYSTEM CHECKED OK.
- [SDR CALA2017071702260](https://openairdocs.org/sdr/CALA2017071702260.md): Slat · obstructed · Jul 17, 2017 · N466UA · Airbus A320232 · Leading Edge Devices
  > ECAM FOR F/CTL SLATS FAULT APPEARED AFTER TAKEOFF. EMERGENCY DECLARED. FOUND FUEL DOOR CAUGHT IN BETWEEN SLAT NR 3 AND WING. REMOVED AND REPLACED RIGHT WING SLAT NR 3 IAW MM-27-84-65-000-001-A AND DOOR ASSY.

Next page: https://openairdocs.org/aircraft/N466UA/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 = 'N466UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N466UA/reports

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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.