# Service difficulty reports: N473UA

A list on [N473UA](https://openairdocs.org/aircraft/N473UA.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 · 107 reports

- [SDR CALA2026051216192](https://openairdocs.org/sdr/CALA2026051216192.md): Engine · no discrepancy · May 12, 2026 · N473UA · Airbus A320232 · Engine (Turbine/Turboprop)
  > POSSIBLE BIRD STRIKE ON NR 2 ENGINE FAN BLADE AND INTAKE LIP. NO ABNORMAL ENGINE INDICATIONS OR ODORS IN THE FLIGHT DECK. FOUND ON WALK AROUND. ACCOMPLISHED BIRDSTRIKE INSPECTION OF ENGINE 2. NO DAMAGE FOUND WITHIN THE ENGINE OR ON THE FAN BLADES. NO INGEST
- [SDR CALA2026032014710](https://openairdocs.org/sdr/CALA2026032014710.md): Light · inoperative · Mar 19, 2026 · N473UA · Airbus A320232 · Emergency Lighting
  > PROCEDURE - EMERGENCY EXIT ROW LIGHTING AT SEAT 7C INOP REMOVED AND REPLACED SEAT MOUNTED EMERGENCY LIGHT AT SEAT 7C, REF. AMM 33-51-19-000-002-A. OPERATIONAL TESTS OF CABIN EMERGENCY LIGHTING, REF. AMM 33-51-00-710-009-A. CHECKS NORMAL.
- [SDR CALA2025031702873](https://openairdocs.org/sdr/CALA2025031702873.md): Hydraulic Line · leaking · Mar 13, 2025 · N473UA · Airbus A320232 · Hydraulic System, Main
  > HYD Y RSVR LO LVL FOUND MAJOR LEAK UNDER PYLON,YELLOW RESERVOIR AT 0,UNABLE TO REPLENISH HYDRAULIC,,RESERVOIR NOT RETAINING HYDRAULIC PIC UPDATE FOUND HYD LEAK COMING FROM HYD LINE IN PYLON PART # D2901010201200. PARTS ORDER WAITING ON CLAMPS REF AIPC 29-13-
- [SDR CALA2025031102700](https://openairdocs.org/sdr/CALA2025031102700.md): Battery · inoperative · Mar 10, 2025 · N473UA · Airbus A320232 · Emergency Lighting
  > OPERATIONAL CHECK OF CABIN EMERGENCY LIGHTS {A3NB-33-3-6012} - EPSU BATTERY AFT L MSG REPLACEMENT OF THE AFT L EPSU BATTERY WAS PERFORMED IAW AMM 33-51-38/401. OK FOR SERVICE PARTS USED: 18-3351-3-0001,QTY:1
- [SDR CALA2025012702041](https://openairdocs.org/sdr/CALA2025012702041.md): Panel · missing · Jan 25, 2025 · N473UA · Airbus A320232 · Ailerons
  > PANEL 675GB NOTED AS MISSING BY CREW. PANEL MISSING UNDER RIGHT WING INBOARD FROM AILERON PANEL 675GB IS MISSING ON THE RIGHT WING. RECIEVED A NEW PANEL 675GB AND INSTALLED THE PANEL. REF. IPC 57-51-37-12L 002.
- [SDR CALA2025010601791](https://openairdocs.org/sdr/CALA2025010601791.md): Pump · faulty · Jan 3, 2025 · N473UA · Airbus A320232 · Fuel Controlling System
  > AT 18000FT AT IDLE IN DESCENT ENGINE FLAMMED OUTUPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. PILOT REPORTS IN DESCENT AT FL180 E2 FLAMED OUT, LOSS OF POWER. HE SAID IT WAS LIKE FUEL STARVATION AND FUEL FLOW WENT
- [SDR CALA2024120401400](https://openairdocs.org/sdr/CALA2024120401400.md): Computer · faulted · Dec 1, 2024 · N473UA · Airbus A320232 · Flight Control System
  > F/CTL ELAC PITCH FAULT UPPER ECAM MESSAGE F/CTL ELAC 2 PITCH FAULT,POST FLIGHT REPORT FIN (9CE),FOLLOW TSM 27-93-00-810-836-A PERFORM (B) OPERATIONAL TEST OF THS-ACTUATOR ELECTRICAL CONTROL PER AMM 27-96-00-710-022,WITH THE ENGINE #2 RUNNING ALL TEST PASS.NO
- [SDR CALA2024091300627](https://openairdocs.org/sdr/CALA2024091300627.md): Warning Light · illuminated · Sep 13, 2024 · N473UA · Airbus A320232 · Door Warning System
  > REJECTED TAKE OFF AT 70 KNOTS DUE TO FWD CARGO DOOR INDICATION SHOWING OPEN. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. VISUALLY INSPECT BRAKES. PERFORMED INSP REF AMM 05-51-16 NO DAMAGES NOTED TO BRAKES OR TIR
- [SDR CALA2023100602951](https://openairdocs.org/sdr/CALA2023100602951.md): Fitting · cracked · Sep 13, 2023 · N473UA · Airbus A320232 · Fuselage Structure (General)
  > REF AVO 11163 FOUND 13 HOLES NOT ROUND AFTER ACCOMPLISHING FASTENER REMOVAL, HOLE CLEANING & HFEC ACCOMPLISHED FOR HOLES L8, L10, L11, L12, L13, L14, L15, L16, L17, L18, L19, L20, L21. ORIGINAL LP''S ARE 5711510, 5714505, 5711529, 5711532, 5711538, 5711542, 57
- [SDR CALA2023100602956](https://openairdocs.org/sdr/CALA2023100602956.md): Fitting · cracked · Sep 13, 2023 · N473UA · Airbus A320232 · Fuselage Structure (General)
  > REF AVO 11164. INITIAL HOLE REWORK STARTED SEE LP 5683450. AVO COMPLETION TO INCLUDE HFEC FOR HOLES R2, R3, R8, R10, R11, R12, R13, R14, R15, R16, R17, R18, R19, R20, R21 WILL REQUIRE ACCOMPLISHMENT POST FERRY FLIGHT. ORIGINAL LP''S ARE 5723512, 5723520, 5723
- [SDR CALA2023100602955](https://openairdocs.org/sdr/CALA2023100602955.md): Fitting · cracked · Sep 13, 2023 · N473UA · Airbus A320232 · Fuselage Structure (General)
  > REF AVO 11163, FND 8 HOLES OVR MAXX ALLOWABLE, HFEC ACCOMPLISHED NO INDICATIONS NOTED. THIS IS FOR HOLES L1, L2, L3, L4, L5, L6, L7, L9. ORIGINAL LPS ARE 5711462, 5611474, 5711490, 5714497, 5714485, 5714474, 5711504 & 5714462. LOCK FOR MX FERRY ABOVE REF OR
- [SDR CALA2023070502179](https://openairdocs.org/sdr/CALA2023070502179.md): Seal · damaged · Jul 1, 2023 · N473UA · Airbus A320232 · Flight Compartment Windows
  > PDA 3. CAPTAIN SLIDING WINDOW MISSING 6 INCH SECTION OF PRESSURE SEAL ALONG AFT EDGE. TOMC NOTIFIED AND PDA3 RECORDED PER GMM 02-30-95. CAPTAIN SLIDING WINDOW PRESSURE SEAL WILL REQUIRE AN INTERIM REPAIR PER AMM MT56-003.PERFORMED INTERIM REPAIR OF CAPTAIN SLI
- [SDR CALA2022121903410](https://openairdocs.org/sdr/CALA2022121903410.md): Fuel Cap · missing · Dec 16, 2022 · N473UA · Airbus A320232 · Aircraft Fuel System
  > PDA 2 AIRCRAFT ARRIVED WITH FUEL CAP MISSING. REPLACED MISSING REFUEL COUPLER CAP.
- [SDR CALA2021120102228](https://openairdocs.org/sdr/CALA2021120102228.md): None · none · Dec 1, 2021 · N473UA · Airbus A320232 · Flight Control System
  > FLAPS FAULT DISPLAYED ON UPPER ECAM SCREEN. - F-CTL PLEASE WORK TSM 27-51-00-810-821-A THEN CONTACT TOMC 847-700-9980....TOMC SMITH. FURTHER DETAILS AWAITED.
- [SDR CALA2020032100666](https://openairdocs.org/sdr/CALA2020032100666.md): Attach Angle · gouged · Mar 18, 2020 · N473UA · Airbus A320232 · Wing, Landing Gear Attach Fittings
  > RIGHT WING MAIN LANDING GEAR RETRACT ACTUATOR ATTACHMENT FITTING LOWER FACE GOUGED PER HAECO LCQ NR LP 9294846 GENERATED REMOVED AND REPLACED RIGHT WING MLG RETRACTION JACK ANCHORAGE FI TTING IAW HAECO REO L22568 REV 1R ECRA 5726-01087 PERFORMED INSP.
- [SDR CALA2020032100665](https://openairdocs.org/sdr/CALA2020032100665.md): Attach Fitting · corroded · Mar 18, 2020 · N473UA · Airbus A320232 · Wing, Landing Gear Attach Fittings
  > LEFT WING LANDING GEAR RETRACT ACTUATOR FITTING UPPER FACE CORRO DED PER HAECO LCQ NR LP 9294843/ 24843 GENERATED REMOVED AND REPLACED LEFT WING LANDING GEAR RETRACT ACTUATOR ATT ACHMENT FITTING ANCHORAGE IAW A320 SRM 57-26-13-300-009 PERFORME D INSP
- [SDR CALA2020030900612](https://openairdocs.org/sdr/CALA2020030900612.md): Stringer · corroded · Mar 8, 2020 · N473UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > INSIDE AFT CARGO COMPT-CORROSION ON STRINGER AT FRAME 56 + 8" ST R 38 RIGHT.(A3NB-53-4-61-79) AT HAECO LCQ PER NR 9294351. GENERA TED REMOVED AND REPLACED STR @ FR 56-58 STR38R IAW A320 SRM 51-72-11 -911-001. WORK PERFORMED.
- [SDR CALA2020032000614](https://openairdocs.org/sdr/CALA2020032000614.md): Skin · dented · Mar 4, 2020 · N473UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > LOWER FUSELAGE EXTERIOR HAS DENT AROUND FASTENER BETWEEN FR 59-6 0 STR 39-40R - GENERATED BY MECH ON NR 9294034 AT HAECO LCQ {A3NB-05-3-6003} HAECO TECHNICIAN AND QC LC-21 MEASURED DENT AT FR59 AND STR40 R/H 1.O"W X 1.0"L X.040"D ORIG THICKNESS.063" OUT OF L
- [SDR CALA2020022400470](https://openairdocs.org/sdr/CALA2020022400470.md): Cover · corroded · Feb 18, 2020 · N473UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > INSIDE AFT CARGO COMPT TORSION BOX COVER SHEET FR52-56 HAS CORROSION SPEC NO A3NB-53-4-6179 GEN BY V892441 AT HAECO LCQ. REMOVED AND REPLACED TORSION BOX COVER SHEET IN AFT CARGO AT FR5 6-56 IAW A320 SRM 51-72-11-911-001 BY MECH V918284 INSP BY LC-21 PER HGR N
- [SDR CALA2020021700456](https://openairdocs.org/sdr/CALA2020021700456.md): Shear Plate · corroded · Feb 16, 2020 · N473UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT RIGHT SIDE OF CABIN FR69+16 STR 23R SHEAR PLATE SUPPORT FITT ING HAS CORROSION ON BOTTOM SIDE OF FITTING (A3NB-05-3-6056) AT HAECO LCQ PER NR NO. 9294601. P REMOVED AND REPLACED R/H SHEAR WEB SUPPORT @ FR 69-70, STR 23R I AW A320 SRM 51-72-11-911-001
- [SDR CALA2019050700711](https://openairdocs.org/sdr/CALA2019050700711.md): Fuel Cap · missing · May 6, 2019 · N473UA · Airbus A320232 · Fuel Storage
  > FUELER REPORT FUEL CAP MISSING REQUEST TO DEFER REF CDL 28A DISPATCH DESK: DD32 NAME: GP DATE: 04-MAY-19- REFUEL/DEFUEL COUPLING CAP MISSING. PDA 2 CARD CREATED ON LOG PAGE 3148613. DEFERRED ITEM REF CDL 28 A DDP CW NO FUEL LEAKAGE OR OTHER DAMAGE TO AIRCRAFT
- [SDR CALA2019050700708](https://openairdocs.org/sdr/CALA2019050700708.md): Fuel Cap · missing · May 6, 2019 · N473UA · Airbus A320232 · Fuel Storage
  > PDA 2 FUELER REPORTED FUEL CAP MISSING TOMC NOTIFIED AND INSTRUCTED TO CLEAR THIS LOG PG AS THEY TAKE CARE OF IT FROM HERE NO FUEL LEAKAGE OR OTHER DAMAGE TO AIRCRAFT.
- [SDR CALA2019040200519](https://openairdocs.org/sdr/CALA2019040200519.md): Lever · missing · Apr 1, 2019 · N473UA · Airbus A320232 · Cargo/Baggage Doors
  > PDA 2 AFT CARGO DOOR OPEN/CLOSE CONTROL LEVER MISSING. VERBAL RAMP REPORT INSTALLED LEVER, SCREW AND WASHER - OPS CHECK NORMAL. REF IPC 52-36-02-02.
- [SDR CALA2018031200879](https://openairdocs.org/sdr/CALA2018031200879.md): Skin · damaged · Mar 9, 2018 · N473UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING INSPECTION OF THE BELLY SKIN PER EA 5300-02120, EXISTING REPAIR DOUBLER, AT FRAME 33-35 AND STRINGER 41R-42R, WAS NOTED WITH CHAFING DUE TO INTERFERENCE WITH WING TO BODY FAIRING. THERE IS NO DAMAGE ALLOWABLES ON THE DOUBLER, THE DOUBLER WAS REMOVED AND
- [SDR CALA2018022700823](https://openairdocs.org/sdr/CALA2018022700823.md): Frame · corroded · Feb 26, 2018 · N473UA · Airbus A320232 · Fuselage Main, Frame
  > CORROSION ON FRAME 68 FWD FA CE AT ANCHOR NUT ABOVE STRINGER 23. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-41-12-283-001, FIG 10102, SHEET 1. REPAIRED THE FRAME IAW SRM 53-41-12-300-001, PRINCIPAL 1.
- [SDR CALA2018022700822](https://openairdocs.org/sdr/CALA2018022700822.md): Door Sill · corroded · Feb 26, 2018 · N473UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > R2 DOOR SILL HAS CORROSION AT FRAME 68. REMOVED AND REPLACED THE DOOR SILL IAW SRM 51-42-11, PARA 2D, E & F.
- [SDR CALA2018022300793](https://openairdocs.org/sdr/CALA2018022300793.md): Shear Plate · corroded · Feb 23, 2018 · N473UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > THE RT SHEAR PLATE AT FRAMES 68 - 7 0 IS CORRODED. REMOVED AND REPLACED THE RT SHEAR PLATE IAW SRM 51-42-11.
- [SDR CALA2018011900246](https://openairdocs.org/sdr/CALA2018011900246.md): Power Supply · faulted · Jan 19, 2018 · N473UA · Airbus A320232 · Emergency Lighting
  > EMERGENCY LIGHT TEST WILL NOT PASS. LEFT EPSU UNIT FAULTED. REMOVED AND RELACED THE LI DOOR EPSU AND BATTERY PACK IAW AMM33-51-38. OPS CHECKED NORMAL, NO FAULTS NOTED.
- [SDR CALA2017112604226](https://openairdocs.org/sdr/CALA2017112604226.md): Lens · missing · Nov 26, 2017 · N473UA · Airbus A320232 · Emergency Lighting
  > DURING 1-SVC CHECK, FOUND MISSING COVER LENS ON OVERHEAD EMERGENCY LIGHT, ROW 11. INSTALLED LENS COVER AND LIGHT BULBS. OPS CHECK NORMAL.
- [SDR CALA2017052701613](https://openairdocs.org/sdr/CALA2017052701613.md): Hydraulic System · low · May 27, 2017 · N473UA · Airbus A320232 · Hydraulic System, Main
  > GREEN HYD SYS LOW. EMERGENCY DECLARED. SERVICED THE GREEN HYD SYS TO FULL, NO LEAKS NOTED, RAN ELECTRIC PUMPS TO LEAK CHECK AND PERFORMED ENGINE RUNS TO VERIFY, NO LEAKS FOUND, SYS OPS CHECKED NORMAL. ACFT OK TO CONTINUE.
- [SDR CALA2015050493651](https://openairdocs.org/sdr/CALA2015050493651.md): Hydraulic Line · unknown · May 2, 2015 · N473UA · Airbus A320232 · Hydraulic System, Main
  > G RSVR LO LVL DISPLAYED ON UPPER ECAM SCREEN AT FL 360. EMER DECLARED & DIVERTED. REPLACED NR 1 ENG HYD PRESS LINE.
- [SDR CALA2015011692985](https://openairdocs.org/sdr/CALA2015011692985.md): Plate · damaged · Jan 13, 2015 · N473UA · Airbus A320232 · Wing, Plate/Skin
  > FIVE EACH HOLES FOUND DAMAGED ON LT WING LOWER SKIN PANEL NR 3 PYLON SYS MOUNTING PLATE. HOLES REPAIRED REO L18663 REV IR & ECRA 5720-02626. RECEIVED A - B RDAS 80018161-003-2014 ISSUE A THAT THIS IS AN INTERIM REPAIR APPROVED FOR 6 MONTHS. A NEW RDAS MUST
- [SDR CALA2015010692902](https://openairdocs.org/sdr/CALA2015010692902.md): Skin Panel · damaged · Jan 3, 2015 · N473UA · Airbus A320232 · Wing, Plate/Skin
  > 5 EACH HOLES FOUND DAMAGED ON LT WING LOWER SKIN PANEL NR 3 PYLON SYS MOUNTING PLATE. HOLES REPAIRED IAW ECRA 5720-02626. RECEIVED A - B RDAS 80018161-003-2014 ISSUE. THIS IS AN INTERIM REPAIR APPROVED FOR 6 MONTHS. A NEW RDAS MUST BE RECEIVED PRIOR TO 01J
- [SDR CALA2014011690166](https://openairdocs.org/sdr/CALA2014011690166.md): Battery · discharged · Jan 16, 2014 · N473UA · Airbus A320232 · Emergency Lighting
  > EMERGENCY LIGHT TEST THRU CIDS FAILED GIVING A 33-51-18 EPSU EMERGENCY BATTERY RT. REPLACED RT MID BATTERY IAW MM 33-51-38, OPERATIONS CHECKED OK.
- [SDR CALA2013123094049](https://openairdocs.org/sdr/CALA2013123094049.md): Limiter · faulty · Dec 29, 2013 · N473UA · Airbus A320232 · Battery/Charger System
  > BCL 2 FAULT DISPLAYED ON UPPER ECAM SCREEN. ELEC REPLACED BCL 2 MESSAGE CLEARED.
- [SDR CALA2013120693508](https://openairdocs.org/sdr/CALA2013120693508.md): Switch · defective · Dec 6, 2013 · N473UA · Airbus A320232 · Fuel Boost Pump
  > NR 1 FUEL PUMP WILL NOT STAY ON UNLESS SWITCH IS HELD MANUALLY. REPLACED FUEL PUMP SWITCH, OPERATION & CHECK OF THE NR 1 LT FUEL PUMP OK.
- [SDR CALA2013110792705](https://openairdocs.org/sdr/CALA2013110792705.md): Slide · out of tolerance · Oct 27, 2013 · N473UA · Airbus A320232 · Escape Slide
  > DOOR 1L SLIDE RAFT REMOVED IAW AMM FOR JOB CARD CHANGED SLIDE RAFT IAW MM, MR OFF MR25114-035. ON, MR25120-022 OFF.
- [SDR CALA2013100891835](https://openairdocs.org/sdr/CALA2013100891835.md): Nut Plate · unsecure · Oct 6, 2013 · N473UA · Airbus A320232 · Emergency Equipment
  > LEFT OVERWING SLIDE HAS ONE STUD HANGING OUT IN LOWER AFT CORNER. REMOVED SLIDE & REPLACED NUTPLATE, REINSTALLED LT OVERWING SLIDE IAW MM.
- [SDR CALA2013090591021](https://openairdocs.org/sdr/CALA2013090591021.md): Cover · cracked · Sep 5, 2013 · N473UA · Airbus A320232 · Passenger/Crew Doors
  > CRACK IN DOOR 2L COVER PLATE BEYOND LIMITS. REMOVED DOOR 2L COVER PLATE. CLEANED & PRIMED DOOR SURFACE.
- [SDR CALA2013080590121](https://openairdocs.org/sdr/CALA2013080590121.md): Duct · split · Jul 29, 2013 · N473UA · Airbus A320232 · Air Distribution System
  > VIBRATION FELT IN FLOORBOARD AT ROW 22, RT BY THE SIDEWALL WHEN PACKS OR RECIRCULATION FANS ARE OPERATING. REMOVED FLOORBOARD AND FOUND BAD DUCT, SEAM SPLIT. REPLACED DUCT IAW 21-20-00-410-001A.
- [SDR UALA2013071905077](https://openairdocs.org/sdr/UALA2013071905077.md): Sill · damaged · Jul 16, 2013 · N473UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > L2 DOOR BOTTOM LEFT HAS A PRESSURE LEAK. LOUD WHISTLE. REPLACED SILL IAW AMM.
- [SDR UALA2013071104840](https://openairdocs.org/sdr/UALA2013071104840.md): Warning Buzzer · malfunctioned · Jul 10, 2013 · N473UA · Airbus A320232 · Interphone/Passenger Announcement (PA) System
  > CONSTANT RINGING OF CALL BUZZER IN COCKPIT. FOUND WHEN SELCAL BREAKER PULLED NOISE STOPPED. BREAKER IS ONLY FOR SELCAL PULLED AND SECURED.
- [SDR UALA2013071004806](https://openairdocs.org/sdr/UALA2013071004806.md): Amu · faulty · Jul 9, 2013 · N473UA · Airbus A320232 · Audio Integrating System
  > CABIN TO COCKPIT HORN ON CONTINUOUSLY ALL CALL LIGHTS ON. REPLACED AUDIO MANAGEMENT UNIT IAW AMM, OPS CHECKED OK.
- [SDR UALA2013070304661](https://openairdocs.org/sdr/UALA2013070304661.md): Threshold · misinstalled · Jul 2, 2013 · N473UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > L2 DOOR PRODUCING A LOUD SQUEAL FROM SURFACE TO FL 350. STOPPED SQUEAL ON DESCENT AT FL 310. FOUND NEW THRESHOLD PLATE INSTALLED WITH EDGES BENT UP CAUSING LARGE BUMP, STRAIGHTENED IAW MT N52-020.
- [SDR UALA2013062604466](https://openairdocs.org/sdr/UALA2013062604466.md): Lens · damaged · Jun 24, 2013 · N473UA · Airbus A320232 · Escape Slide
  > L1 DOOR SLIDE PACK VIEW PORT OBSTRUCTED. FOUND LENS HAZED. REMOVED AND REPLACED LENS, SLIDE BOTTLE PSI CAN BE VERIFIED AS NORMAL.
- [SDR UALA2013062504412](https://openairdocs.org/sdr/UALA2013062504412.md): Landing Gear · lack of lube · Jun 23, 2013 · N473UA · Airbus A320232 · Nose/Tail Landing Gear
  > CAPTAIN`S STEERING TILLER, FEELS STIFF IN TURNS TO RIGHT. LUBED NLG AND CHECKED TIRE PRESSURE. TAXIED ACFT CHECKED OK IAW AMM.
- [SDR UALA2013061804217](https://openairdocs.org/sdr/UALA2013061804217.md): Latch · out of adjust · Jun 18, 2013 · N473UA · Airbus A320232 · Emergency Equipment
  > OVERWING EXIT LANYARD DOOR, LT SIDE, POPS OPEN. ADJUSTED STOW BIN LATCH FOR OVER WING EXIT LANYARD, OPS CHECK NORMAL.
- [SDR UALA2013061304054](https://openairdocs.org/sdr/UALA2013061304054.md): Skin · damaged · Jun 12, 2013 · N473UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING HMV VISIT, REPAIR DOUBLER WITH LESS THAN SRM ALLOWED EDGE DISTANCE WAS INSTALLED & SUBSEQUENTLY REMOVED ON FUSELAGE SKIN FR33-34, STR41L-41R. REPAIRED IAW SRM 53- 21-11, FIG 215.
- [SDR UALA2013061304053](https://openairdocs.org/sdr/UALA2013061304053.md): Sill · corroded · Jun 12, 2013 · N473UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > 2R DOOR SILL BEAM HAS SPOTS OF CORROSION MIGRATING UNDER FWD GIRT FITTING PLATE, AFTER BLENDING FOUND TO BE OUT OF SRM ALLOWABLE LIMITS. REPAIRED IAW SRM 53-41-14, FIG 201.
- [SDR UALA2013061304052](https://openairdocs.org/sdr/UALA2013061304052.md): Structure · debonded · Jun 12, 2013 · N473UA · Airbus A320232 · Rudder Miscellaneous Structure
  > RT SIDE OF RUDDER HAS A DISBOND INDICATION 18" FROM TOP OF RUDDER AND 14" FROM T/E, 4" IN DIAMETER. CLEANED, PREPPED AND REPAIRED AREA OF DISBOND ON RT SIDE OF RUDDER AND REAPPLIED FINISH AS REQUIRED IAW ECRA 5540-01348.

Next page: https://openairdocs.org/aircraft/N473UA/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 = 'N473UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N473UA/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.