# Service difficulty reports: N470UA

A list on [N470UA](https://openairdocs.org/aircraft/N470UA.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 · 101 reports

- [SDR CALA2026032414817](https://openairdocs.org/sdr/CALA2026032414817.md): B-Nut · leaking · Mar 22, 2026 · N470UA · Airbus A320232 · Hydraulic Power Accumulator, Main
  > CREW REPORTED HYD G RSVR LO LEVEL CREW REPORTED THAT THEY TURNED OFF THE PTU AND THE ENG DRIVEN PUMPP WITHIN A MIN OF THE ECAM SERVICED GREEN SYSTEM HYDRAULIC RESERVOIRS TO SERVICEABLE LIMITS REF AMM 12-12-29/301. FOUND GREEN HYD PRESSURE LINE B NUT LOOSE AND
- [SDR CALA2025102910715](https://openairdocs.org/sdr/CALA2025102910715.md): Blade · bird ingestion · Oct 26, 2025 · N470UA · Airbus A320232 · Turbine Engine Air Inlet Section
  > BIRD STRIKE ON T/O AIRFRAME AND ENG VIB RIGHT ENG APPEARS TO H AVE BLADE DAMAGE. PERFORMED AIRFRAME AND ENGINE BIRD STRIKE INSPECTIONS IAW AMM 05-51-14-200-803-A AND AMM 72-00-00-200-010-A. NO AIRFRAME DAMAGE WAS NOTED. NOTED ENGINE DAMAGE LIMITED TO A SI
- [SDR CALA2025080407261](https://openairdocs.org/sdr/CALA2025080407261.md): Slide · deployed · Jul 31, 2025 · N470UA · Airbus A320232 · Escape Slide
  > LH OVERWING SLIDE DEPLOYED. REMOVED LH OVERWING SLIDE IRW AMM 25-65-42. REMOVED AND REPLACED LT OVERWING EMERGENCY SLIDE IRW AMM 25-62-42 UP TO AND INCLUDING STEP 4. B. (20).
- [SDR CALA2025080107183](https://openairdocs.org/sdr/CALA2025080107183.md): Bottle · faulted · Jul 28, 2025 · N470UA · Airbus A320232 · Emergency Exits
  > CIDS CAUTION LIGHT. DEFERRED PER MEL, VERFIED LT EMERGENCY BOTTLE PRESSURE, NEEDLE IS EXACTLY ON THE BORDER BETWEEN GREEN AND RED, REF TSM 25-62-00-810-805 IS OK. INSTALLED INOP STICKER ADJ TO PTP PANEL. DEFERRED PER MEL. REMOVED AND REPLACED LT OVERWING S
- [SDR CALA2025060905360](https://openairdocs.org/sdr/CALA2025060905360.md): Wire Harness · damaged · Jun 6, 2025 · N470UA · Airbus A320232 · Light System Wiring
  > SEAT 38C EMERGENCY LIGHT IS INOP REMOVED AND REPLACED SEAT 38C EMERGENCY LIGHT SEAT HARNESS. PEFORMED OPS CHECK, OPS CHECK GOOD. REF AMM 33-50-00.
- [SDR CALA2024013000258](https://openairdocs.org/sdr/CALA2024013000258.md): Skin · dented · Jan 29, 2024 · N470UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > DIP DENT AFT OF POTABLE WATER DOOR. ACCOMPLISHED PERMENANT REPAIR ON DENT AFT OF POTABLE WATER DOOR (12.375" AFT OF AFT SIDE) IAW A320 SRM 53-41-11-283-059 AND 53-4 1-11-300-093 REPAIR LOCATED AT FR 66-67 STR 39L-40L
- [SDR CALA2024012400214](https://openairdocs.org/sdr/CALA2024012400214.md): Door · cracked · Jan 19, 2024 · N470UA · Airbus A320232 · Emergency Exits
  > RT AFT EMERGENCY EXIT DOOR FWD AND AFT SIDES CRACKED. HAECO LCQ NR 9298309/34309 REMOVED AND REPLACED 2EA SEGMENTS ON RH AFT EMERGENCY EXIT DOOR IAW A320 SRM 51-42-11/001.
- [SDR CALA2024012400213](https://openairdocs.org/sdr/CALA2024012400213.md): Skin · contaminated · Jan 19, 2024 · N470UA · Airbus A320232 · Elevator, Plate/Skin
  > LH ELEVATOR HAS WATER INGRESS AT 36IN FROM I/B EDGE 19IN FROM TRAILING EDGE 2IN IN DIAMETER. HAECO LCQ NR 9298 337/34337 REPAIRED LH ELEVATOR UPPER SKIN 36IN FROM I/B 19IN FROM T/E 2IN DIA ZONE 1 IAW A320 SRM 55-21-11-300-005 CAT A REPAIR.
- [SDR CALA2024012400212](https://openairdocs.org/sdr/CALA2024012400212.md): Door · cracked · Jan 19, 2024 · N470UA · Airbus A320232 · Emergency Exits
  > RT FWD EMERGENCY EXIT DOOR FWD AND AFT SIDES CRACKED. HAECO LCQ NR 9298306/34306 REMOVED AND REPLACED 2EA SEGMENTS ON RH FWD EMERGENCY EXIT DOOR IAW A320 SRM 51-42-11/001.
- [SDR CALA2024012400211](https://openairdocs.org/sdr/CALA2024012400211.md): Door · cracked · Jan 19, 2024 · N470UA · Airbus A320232 · Emergency Exits
  > LT FWD EMERGENCY EXIT DOOR FWD AND AFT SIDES CRACKED. HAECO LCQ NR 9298307/34307 REMOVED AND REPLACED 2EA SEGMENTS ON LH FWD EMERGENCY EXIT DOOR IAW A320 SRM 51-42-11/001
- [SDR CALA2024012400210](https://openairdocs.org/sdr/CALA2024012400210.md): Door · cracked · Jan 19, 2024 · N470UA · Airbus A320232 · Emergency Exits
  > LT AFT EMERGENCY EXIT DOOR FWD AND AFT SIDES CRACKED. ON HAECO LCQ NR 9298308/34308 REMOVED AND REPLACED 2EA SEGMENTS ON LH AFT EMERGENCY EXIT DOOR IAW A320 SRM 51-42-11/001.
- [SDR CALA2024011900143](https://openairdocs.org/sdr/CALA2024011900143.md): Shear Tie · cracked · Jan 16, 2024 · N470UA · Airbus A320232 · Fuselage Internal Mounting Structure
  > AD 2020-1-06, LH FR43 FOOT CRACKED IN FRAME AT 8 O''CLOCK FACEING FWD. GENERATED BY V061632 AT HAECO LCQ PER NR. 9298099/34099 REMOVED AND REPLACED FR43 L/H FRAME AND FOOT IAW AIRBUS REPAIR I NSTRUCTION 15R53370233B.
- [SDR CALA2023062602034](https://openairdocs.org/sdr/CALA2023062602034.md): Lanyard · missing · Jun 22, 2023 · N470UA · Airbus A320232 · Emergency Equipment
  > PDA 1 FUEL CAP MISSING. REMOVED AND REPLACED FUEL CAP LANYARD.
- [SDR CALA2023051701545](https://openairdocs.org/sdr/CALA2023051701545.md): Manifold · warning message · May 14, 2023 · N470UA · Airbus A320232 · Hydraulic System, Main
  > FLIGHT CREW REPORTS TO DISPATCH VIA ARINC, HYD Y RSVR LO LVL, HYD Y SYS LO PR HYD Y ENG 2 PUMP LO PR ECAM, VARGAS TOMC FOUND LEAK AT PTU VALVEBLOCK AT BOTTOM PLUG (NOTED IN PICTURE). REMOVED AND REPLACED PTU VALVEBLOCK MANIFOLD PER AMM 29-13-15-400-001-A NO L
- [SDR CALA2023042801284](https://openairdocs.org/sdr/CALA2023042801284.md): Landing Light · detached · Apr 28, 2023 · N470UA · Airbus A320232 · Exterior Lighting
  > RIGHT MAIN LANDING LIGHT HAS BEEN TORN OFFCOMPLETLY GONE WIRESHAN GING. REQUESTING CDL 33G FOR RT RETRACTABLE LANDING LIGHT GASKET AND HOLD DOWN RING MISSING. PLACED MISSING LANDING LIGHT ON CDL 33G. NO DAMAGED FOUND ON AIRCRAFT. DDP C/W. TAPED OVER OPENING AS
- [SDR CALA2022113003256](https://openairdocs.org/sdr/CALA2022113003256.md): Pressure Switch · shorted · Nov 30, 2022 · N470UA · Airbus A320232 · Hydraulic System, Main
  > ECAM AT CRUISE HYD Y SYS LOW PRESSURE. Y SYSTEM PRESSURE STEADY AT 3100. FOUND SWITCH INTERNALLY SHORTED ON PINS B & C. R & R SYSTEM PRESSURE SWITCH. OPS AND LEAK CHECKED GOOD.
- [SDR CALA2022092602502](https://openairdocs.org/sdr/CALA2022092602502.md): Fuel Cap · unknown · Sep 25, 2022 · N470UA · Airbus A300* · Aircraft Fuel System
  > FUELER REPORTED FUEL CAP MISSING PLACED ON CDL PLACARD INSTALLED NO FUEL LEAKS NOTED PLACED ON CDL PLACARD INSTALLED NO FUEL LEAKS NOTED DISPATCH DESK: 14 NAME: D S DATE: 25-SEP-22- OK TO DEFER FUEL CAP PER CDL 28A. REF LP 9619608 FOR PDA EN
- [SDR CALA2022042501073](https://openairdocs.org/sdr/CALA2022042501073.md): Hook · out of tolerance · Apr 25, 2022 · N470UA · Airbus A320232 · Doors
  > LOUD SQUEAL COMING FROM THE R1 DOOR AT THE TOP CENTER UPPER FLAP AREA. SQUEAL BECAME LOUDER WITH AIRSPEED AND ALT.... REPORTED BY CREW TOMC SMITH FOLLOWED FLOW CHART IN MT 52-020. INSPECTED SEAL, NO DEFECTS PERFORMED PRESSURIZATION CHECK UP TO 4.0 PSI. NO L
- [SDR CALA2022042101044](https://openairdocs.org/sdr/CALA2022042101044.md): None · inoperative · Apr 21, 2022 · N470UA · Airbus A320232 · Cabin Equipment/Furnishings
  > 1R DOOR NOT SHOWING ARMED INFLIGHT. ALSO FASAID CABIN PRESS LI GHTFLASHING. REPEAT WRITEU REF MEL 2560AJ SEE LOG PG 8424486 FOR THE CABIN PRESS REF MEL 2560AJ DOOR 1R ECAM INDICATIONS NORMAL. SLIDE ARMED INDICATOR LIGHT INOP ONLY. PLACING ON MEL 2560MA. DIS
- [SDR CALA2022032100712](https://openairdocs.org/sdr/CALA2022032100712.md): Lens · cracked · Mar 19, 2022 · N470UA · Airbus A320232 · Lighting System
  > (A3NB-33-3-6016) SEAT ROW 12 LEFT FWD EMERGENCY LIGHT DAMAGED (R EPLACE)
- [SDR CALA2022032100710](https://openairdocs.org/sdr/CALA2022032100710.md): Frame · cracked · Mar 18, 2022 · N470UA · Airbus A320232 · Standard Practices/Structures
  > (AD 2018-03-12) L/H FR 68 DOOR STOP #1 HAS A CRACK INDICATION IN BOT I/B I/B HOLE MARKED IN RED, REPAIR BEFORE NEXT FLIGHT () 008 SHEET 01, 02 & 03. INSTALLED FRAME SPLICE & FREEZE PLUG. REI IAW SRI 53-41-12-205-010 REPAIRED ZONE AREA 2 INSP THRESHOLD FRO SUBS
- [SDR CALA2022032100709](https://openairdocs.org/sdr/CALA2022032100709.md): Frame · cracked · Mar 18, 2022 · N470UA · Airbus A320232 · Standard Practices/Structures
  > (AD 2018-03-12) L/H FR68 DOOR STOP #4 HAS CRACK INDICATION IN BO T I/B I/B HOLE MARKED AND DOOR STOP #1 BOT I/B HOLE IN RED, REPA IR BEFORE NEXT FLIGHT () IAW SRM 53-41-12-300-010 FIG 001. REINSTALLED #4 DOOR STOP FITTI REPAIRED ZONE AREA 2 INSP THRESHOLD FROM
- [SDR CALA2022032100708](https://openairdocs.org/sdr/CALA2022032100708.md): Frame · cracked · Mar 18, 2022 · N470UA · Airbus A320232 · Standard Practices/Structures
  > (AD 2018-03-12) R/H FR68 DOOR STOP #1 HAS A CRACK INDICATION IN BOT I/B AND TOP O/B HOLE MARKED IN RED, REPAIR BEFORE NEXT FLIGH T. 011 FIG 008 SHEET 01, 02 & 03. INSTALLED FRAME SLPICE & FREEZE P INSP IAW SRI 53-41-12-205-010 REPAIRE ZONE AREA 2 INSP THRESHOL
- [SDR CALA2022032100707](https://openairdocs.org/sdr/CALA2022032100707.md): Frame · cracked · Mar 18, 2022 · N470UA · Airbus A320232 · Doors
  > (AD 2018-03-12) R/H FR66 DOOR STOP #7 HAS A CRACK INDICATION IN TOP I/B HOLE MARKED IN RED, REPAIR BEFORE NEXT FLIGHT INSTALLED FREEZE PLUG & WASHER, REINSTALLED #7 DOOR STOP FITTING THRESHOLD FROM TIME OF ADL/REPAIR EMBODIMENT 33000FC FH NOT RELE INSP METHOD
- [SDR CALA2022031700699](https://openairdocs.org/sdr/CALA2022031700699.md): Frame · cracked · Mar 17, 2022 · N470UA · Airbus A320232 · Fuselage Structure (General)
  > (AD 2018-03-12) L/H FR68 DOOR STOP #4 HAS CRACK INDICATION IN BO T I/B I/B HOLE MARKED AND DOOR STOP #1 BOT I/B HOLE IN RED, REPA IR BEFORE NEXT FLIGHT () IAW SRM 53-41-12-300-010 FIG 001. REINSTALLED #4 DOOR STOP FITTI REPAIRED ZONE AREA 2 INSP THRESHOLD FROM
- [SDR CALA2022031700698](https://openairdocs.org/sdr/CALA2022031700698.md): Stop · cracked · Mar 17, 2022 · N470UA · Airbus A320232 · Fuselage Structure (General)
  > (AD 2018-03-12) R/H FR66 DOOR STOP #7 HAS A CRACK INDICATION IN TOP I/B HOLE MARKED IN RED, REPAIR BEFORE NEXT FLIGHT INSTALLED FREEZE PLUG & WASHER, REINSTALLED #7 DOOR STOP FITTING THRESHOLD FROM TIME OF ADL/REPAIR EMBODIMENT 33000FC FH NOT RELE INSP METHOD
- [SDR CALA2022031700694](https://openairdocs.org/sdr/CALA2022031700694.md): Stop · cracked · Mar 17, 2022 · N470UA · Airbus A320232 · Fuselage Structure (General)
  > (AD 2018-03-12) L/H FR 68 DOOR STOP #1 HAS A CRACK INDICATION IN BOT I/B I/B HOLE MARKED IN RED, REPAIR BEFORE NEXT FLIGHT () 008 SHEET 01, 02 & 03. INSTALLED FRAME SPLICE & FREEZE PLUG. REI IAW SRI 53-41-12-205-010 REPAIRED ZONE AREA 2 INSP THRESHOLD FRO SUBS
- [SDR CALA2022031700693](https://openairdocs.org/sdr/CALA2022031700693.md): Stop · cracked · Mar 17, 2022 · N470UA · Airbus A320232 · Fuselage Structure (General)
  > (AD 2018-03-12) R/H FR68 DOOR STOP #1 HAS A CRACK INDICATION IN BOT I/B AND TOP O/B HOLE MARKED IN RED, REPAIR BEFORE NEXT FLIGH T. 011 FIG 008 SHEET 01, 02 & 03. INSTALLED FRAME SLPICE & FREEZE P INSP IAW SRI 53-41-12-205-010 REPAIRE ZONE AREA 2 INSP THRESHOL
- [SDR CALA2022031000626](https://openairdocs.org/sdr/CALA2022031000626.md): Fitting · none · Mar 9, 2022 · N470UA · Airbus A320232 · Fuselage Structure (General)
  > (SUPPORT TASK) LH FR20 PASSENGER DOOR STOP FITTING #7 IB #1 HOLE HAS CRACK INDICATION AT 12 O''CLOCK IN THE INTERCOSTAL FITTING () REMOVED AND REPLACED NEW INTERCOSTAL FITTING P/N:D5311424320091 BATCH# 0003912259, AND REINSTALLED STOP FITTING #7 IAW SRM 51-42
- [SDR CALA2022030900614](https://openairdocs.org/sdr/CALA2022030900614.md): Fitting · none · Mar 8, 2022 · N470UA · Airbus A320232 · Fuselage Structure (General)
  > (SUPPORT TASK) RH FR16 PASSENGER DOOR STOP FITTING #7 IB #3 HOLE HAS A CRACK INDICATION AT 3 O''CLOCK IN THE INTERCOSTAL FITTING() REMOVED AND REPLACED INTERCOSTAL FITTING P/N:D5311423620191 AND REINSTALLED DOOR STOP FITTING #7 FR16R IAW SRM 51-42-11 DWG11422
- [SDR CALA2022030900613](https://openairdocs.org/sdr/CALA2022030900613.md): Fitting · cracked · Mar 8, 2022 · N470UA · Airbus A320232 · Fuselage Structure (General)
  > (SUPPORT TASK) LH FR16 PASSENGER DOOR STOP FITTING #7 IB #1 HOLE HAS CRACK INDICATION AT 6 O''CLOCK IN THE INERCOSTAL FITTING() REMOVED AND REPLACED NEW INTERCOSTAL FITTING P/N D5311423620091 BATCH#0003913326 IAW SRM 51-42-11 AND DWG #D53114223000 TOOL USE D T
- [SDR CALA2022030900612](https://openairdocs.org/sdr/CALA2022030900612.md): Fitting · cracked · Mar 8, 2022 · N470UA · Airbus A320232 · Fuselage Structure (General)
  > (SUPPORT TASK) LH FR16 PASSENGER DOOR STOP FITTING #1 IB #3 HOLE HAS CRACK INDICATION AT 2 O''CLOCK IN THE INTERCOSTAL FITTING.() REMOVED AND REPLACED INTERCOSTAL FITTING P/N D5311423020091 IAW A320 SRM 51-42-11/001. ACCOMPLISHED BY AT ST BFM AER OSPACE MOBILE
- [SDR CALA2020021200410](https://openairdocs.org/sdr/CALA2020021200410.md): Plug · missing · Feb 10, 2020 · N470UA · Airbus A320232 · Passenger/Crew Doors
  > AAR NR 9827792 (A3NB-52-3-6092) L-28 NO DOT L2 DOOR DAMPER CYLIN DER GUAGE MISSING RUBBER PLUG REMOVED AND REPLACED L2 DOOR DAMPER CYLINDER I/A/W A320 AMM''S 52 -13-14-000-001, AND 52-13-14-400-001. ADJUSTMENT OF PERCUSSION B ELLCRANK FINGER GOOD. CHARGING OF
- [SDR CALA2020011900152](https://openairdocs.org/sdr/CALA2020011900152.md): Skin · corroded · Jan 14, 2020 · N470UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > (SUPPORT TASK) EXTERIOR SKIN FOR LAV EXHAUST VENT SHOWS SIGNS OF CORROSION. REFER TO N/R: 9827064. REMOVED DAMAGE AT LAV EXHAUST VENT BETWEEN FR69-70 RT, MAX MATERIAL LOSS.010, MAX ALLOWED.004 AND IS OUT OF LIMITS IAW SRM 53-41-11-283-006, REMOVED AND REINST
- [SDR CALA2020011900149](https://openairdocs.org/sdr/CALA2020011900149.md): Spring · broken · Jan 14, 2020 · N470UA · Airbus A320232 · Passenger/Crew Doors
  > NR 9827767 (A3NB-52-3-6005)L-27 NO DOT, L1 DOOR AFT GIRT BAR FITTING SPRING BROKEN REMOVED AND REPLACED L1 DOOR AFT GIRT BAR FITTING SPRING AND PIN IAW AMM 52-13-31-400-003 STEP 3B.
- [SDR CALA2018040301060](https://openairdocs.org/sdr/CALA2018040301060.md): Shear Panel · cracked · Mar 29, 2018 · N470UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT PASSENGER CABIN RT SHEAR PLATE FOUND CRACKED AND CORRODED. REMOVED DAMAGE AND INSTALLED A NEW SHEAR PLATE IAW SRM 51-42-11, DWG D53474180000, AND ECRA 5346-01008.
- [SDR CALA2017060901785](https://openairdocs.org/sdr/CALA2017060901785.md): Power Supply · inoperative · Jun 9, 2017 · N470UA · Airbus A320232 · Emergency Lighting
  > EMERGENCY LIGHTS FAIL OPS CHECK. REF AMM33-51-38, REPLACED LEFT WING EMERGENCY BATTERY SUPPLY. TESTED GOOD.
- [SDR CALA2017052601600](https://openairdocs.org/sdr/CALA2017052601600.md): Power Supply · no test · May 26, 2017 · N470UA · Airbus A320232 · Emergency Lighting
  > FORWARD SECTION EMERGENCY LIGHTS FAILED TEST. REPLACED THE POWER SUPPLY IAW AMM 33-51-38-000-001-A, 33-51-38-400-0 01-A, AND 333-51-38-200-902-A. OPS CHECKED GOOD.
- [SDR CALA2017041701031](https://openairdocs.org/sdr/CALA2017041701031.md): Power Supply · faulty · Apr 17, 2017 · N470UA · Airbus A320232 · Emergency Lighting
  > EMERGENCY LIGHT TEST FAILED, MSG "EPSU BATTERY AFT L" DISPLAYED ON CIDS. REPLACED EPSU PER AMM 33-51-38. EMERGENCY LIGHT TESTED OK PER AMM TASK 33-51-38-400-001-A, MESSAGE CLEAR.
- [SDR CALA2016122601172](https://openairdocs.org/sdr/CALA2016122601172.md): Wire · broken · Dec 26, 2016 · N470UA · Airbus A320232 · Light System Wiring
  > FLOOR PROXIMITY EMERGENCY LIGHT AT SEAT 38C WIRES BROKE FROM LIGHT ASSY ON SEAT BUMPER PANELS. REPLACED EEL PATH LIGHT HARNESS. OPS CHECKED NORMAL.
- [SDR CALA2016122201158](https://openairdocs.org/sdr/CALA2016122201158.md): Power Supply · faulty · Dec 22, 2016 · N470UA · Airbus A320232 · Emergency Lighting
  > FAILED EMERGENCY EXIT LIGHT TEST. FOUND EPSU FAULTED. LT OVERWING 11WL. REPLACED THE EPSU AND BATTERY IAW AMM 33-51-38. OPS CHECKED GOOD.
- [SDR CALA2016071895566](https://openairdocs.org/sdr/CALA2016071895566.md): Bracket · damaged · Jul 17, 2016 · N470UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > ISP BRACKET ON LEFT SIDE BETWEEN FRAMES 28 AND 29 HAS A MISDRILLED HOLE, 13" AFT OF FRAME 28. STRINGER 22 - 23L. CUT OUT DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 53-00-13 FIG 202 (SHEET 2) PG 227. T.
- [SDR CALA2015083194262](https://openairdocs.org/sdr/CALA2015083194262.md): Unknown · odor · Aug 31, 2015 · N470UA · Airbus A320232 · Air Distribution System
  > CREW REPORTED THAT ONE PAX AT ROW 29 SMELLED SMOKE, WHICH THEN DISSIPATED. AFTER REVIEW OF SMOKE ODOR QUESTIONNAIRE, AN INSPECTION WAS ACCOMPLISHED WITH ALL CABIN SYSTEMS POWERED & GALLEY CHILLERS ON. NO SMELL OR SMOKE NOTED. ACFT BACK TO NORMAL CONFIGURATI
- [SDR CALA2014072191480](https://openairdocs.org/sdr/CALA2014072191480.md): Battery · discharged · Jul 18, 2014 · N470UA · Airbus A320232 · Emergency Lighting
  > AFT EPSU FAIL EMER LIGHT TEST FOUND BATTERY WOULD NOT STAY CHARGED. REPLACED BATTERY AMM 33-51-38, GND CHECKED NORMAL.
- [SDR CALA2014072191479](https://openairdocs.org/sdr/CALA2014072191479.md): Power Supply · inoperative · Jul 18, 2014 · N470UA · Airbus A320232 · Emergency Lighting
  > LEFT EPSU FAILED EMER LIGHT TEST. FOUND PSU INOPERATIVE. REPLACED IAW AMM 33-50-51, GND CHECKED NORMAL.
- [SDR CALA2014012090184](https://openairdocs.org/sdr/CALA2014012090184.md): Apu · shutdown · Jan 20, 2014 · N470UA · Airbus A320232 · APU Core Engine
  > ECAM MESSAGE APU AUTO SHUTDOWN DISPLAYED ON UPPER ECAM SCREEN, APU. TAXI IN APU SHUT DOWN HIGH EGT. ACCOMPLISHED NORMAL APU START. FUNCTION WITH ELECTRICAL & PNEUMATIC LOADS OPERATION NORMAL.
- [SDR CALA2014010290004](https://openairdocs.org/sdr/CALA2014010290004.md): Oxygen Mask · unsecure · Dec 31, 2013 · N470UA · Airbus A320232 · Passenger Oxygen System
  > 38DEF O2 MASKS HAVE FALLEN OUT. RESTOWED O2 MASK, NEEDS DROP CHECK.
- [SDR CALA2013103192545](https://openairdocs.org/sdr/CALA2013103192545.md): Shelf · damaged · Oct 27, 2013 · N470UA · Airbus A320232 · Buffet/Galleys
  > SHARP METAL EDGE ON AFT GALLEY SHELF. REPAIRED DAMAGE.
- [SDR CALA2013092391370](https://openairdocs.org/sdr/CALA2013092391370.md): Computer · faulty · Sep 23, 2013 · N470UA · Airbus A320232 · Autopilot Computer
  > CAT SINGLE ONLY MESSAGE, WITH LOWER ECAM CAT 3 DUAL INOPERATIVE. CYCLED FMGC CB B2 & 17 WITH NO CHANGE, CYCLED MMR 1 & 2 CBS G12 & L7 WITH NO CHANGE, CYCLED ELAC #1 SW & FAULT CLEARED BUT CAME BACK ON & ELAC CB B11 NO HELP. SHUT DOWN BOTH DENGES & CYCLED BOT
- [SDR CALA2013082690723](https://openairdocs.org/sdr/CALA2013082690723.md): Blade · damaged · Aug 23, 2013 · N470UA · Airbus A320232 · Turbine Engine Compressor Section
  > NR 21 FAN BLADE, NR 1 ENGINE, FAILED TRANSIENT ACOUSTIC PROPAGATION TEST PER JOB CARDNR 4-2215. REMOVED & REPLACED NR 21 FAN BLADE PER AMM 72-31-11. PERFORMED NR 1 ENGINE RUNUP VIBRATION TEST PER AMM 71-00-00, VIBRATIONS WITHIN SERVICEABLE LIMITS.

Next page: https://openairdocs.org/aircraft/N470UA/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 = 'N470UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N470UA/reports

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