# Service difficulty reports: N402UA

A list on [N402UA](https://openairdocs.org/aircraft/N402UA.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 · 143 reports

- [SDR CALA2023061601896](https://openairdocs.org/sdr/CALA2023061601896.md): Cover · missing · Jun 6, 2023 · N402UA · Airbus A320232 · Doors
  > RAMP REPORTS, RIGHT FORWARD PASSENGER DOOR HAS HOIST POINT COVER MISSING. SEE ATTACHED PHOTO. SPEED TAPED OVER MISSING HOIST PLUG CAP. REPLACE COVER AT NEXT C-CHECK OR BEFORE 668 DAYS. OK TO CARRY DOOR HOIST POINT COVER MISSING AND SPEED TAPE TOMC-APPROVAL FRO
- [SDR CALA2023050301347](https://openairdocs.org/sdr/CALA2023050301347.md): Cover · missing · May 3, 2023 · N402UA · Airbus A320232 · Spoilers
  > PDA 3 MISSING LH OUTBOARD #4 FLAP TRACK MOVABLE FAIRING PIVOT COVER DURING WALKAROUND. COMPLETED WALKAROUND; NO DAMAGED FOUND.
- [SDR CALA2023041201095](https://openairdocs.org/sdr/CALA2023041201095.md): Power Supply · unknown · Apr 10, 2023 · N402UA · Airbus A320232 · Lighting System
  > DURING EMERGENCY LIGHT TEST AMM 33-51-00-710-001-A FAULT EPSU BATTERY AFT L WAS RECORDED. USING TSM 33-51-00-810-802-A VERIFIED AFT L BATTERY OF EPSU 13WL IS AT FAULT. VEREFIED BATTERY REPLACEMENT AND OPS CHECK GOOD REMOVED AND REPLACED BATTERY OF THE EMERGENC
- [SDR CALA2023031300725](https://openairdocs.org/sdr/CALA2023031300725.md): Cap · missing · Mar 13, 2023 · N402UA · Airbus A320232 · Aircraft Fuel System
  > PDA 1 FUEL CAP MISSING ITEM ON CDL NOW
- [SDR CALA2023021600456](https://openairdocs.org/sdr/CALA2023021600456.md): None · corroded · Feb 16, 2023 · N402UA · Airbus A320232 · Fuselage Main, Structure
  > GEN BY NRC: SUPPORT TASK: DURING CLEANING OF AFT CABIN UNDER FLO OR FOUND CORROSION AT BILGE AREA FR67 AFT FACE BETWEEN STGR42L T O STGR42R. REMOVED & REPLACED FR67 P/N:D5348021221002 IAW SRM 51-42-11 D534802212 ST ENG BFM WC:49846 V935774
- [SDR CALA2022011000101](https://openairdocs.org/sdr/CALA2022011000101.md): Engine · stalled · Jan 9, 2022 · N402UA · Airbus A320232 · Compressor Bleed Valve
  > LEFT ENG COMP STALLSEVERAL JOLTS CLBINGTHRU 13000 FT.. ENG1 SN. V10291 (TSI= 12833) CFDS SHOW ENG1 COMP STALL IN CRZ. WITH VSV MECH/BLD VLV/LPC1. RE. TSM 71-00-00-810-808-A FOR T/SHOOTING AND DISPOSITION. WHQLM-EMC ARSHAD. 08JAN2022. ACCOMPLISHED FUNCTIONAL CH
- [SDR CALA2020120201314](https://openairdocs.org/sdr/CALA2020120201314.md): Battery Pack · inoperative · Dec 1, 2020 · N402UA · Airbus A320232 · Emergency Lighting
  > EMERGENCY LIGHTS BATTERY PACK (11WL) FAILS TO ILLUMINATE WITH THE SWITCH IN THE ARM POSITION AND THE C/B'S PULLED, PER HAECO LCQ NON ROUTINE. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK, IAW A319/320 MM 38-51-38-000-002A 33-51-38-400-002A OPERATIONS TE
- [SDR CALA2020111601278](https://openairdocs.org/sdr/CALA2020111601278.md): Intercostal · cracked · Nov 15, 2020 · N402UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > RT FWD EMERGENCY EXIT DOOR INTERNAL STRUCTURE FWD VERTICAL INTERCOSTAL CRACKED AT FASTENER HOLES. REMOVED AND REPLACED RT FWD EMERGENCY EXIT DOOR INTERNAL STRUCTURE FWD VERTICAL INTERCOSTAL SEGMENT, IAW A320 SRM 51-72-11-911-0 01.
- [SDR CALA2020111301270](https://openairdocs.org/sdr/CALA2020111301270.md): Intercostal · cracked · Nov 12, 2020 · N402UA · Airbus A320232 · Emergency Exits
  > RIGHT AFT EMERGENCY EXIT DOOR INTERNAL STRUCTURE AFT VERTICAL INTERCOSTAL CRACKED AT FASTENER HOLE, PER NR9296358 GEN BY V052030. REMOVED AND REPLACED RT AFT EMERGENCY EXIT DOOR INTERNAL STRUCTURE AFT VERTICAL INTERCOSTAL SEGMENT, IAW SRM 51-72-11-911-001 BY
- [SDR CALA2020111301268](https://openairdocs.org/sdr/CALA2020111301268.md): Intercostal · cracked · Nov 12, 2020 · N402UA · Airbus A320232 · Doors
  > RT AFT EMERGENCY EXIT DOOR INTERNAL STRUCTURE FWD VERTICAL INTERCOSTAL CRACKED AT FASTENER HOLES GEN BY V061623 NR9296332 (44332) A3NB-52-4-6031 AT HAEC LCQ. REMOVED AND REPLACED RT AFT EMERGENCY EXIT DOOR INTERNAL STRUCTURE FWD VERTICAL INTERCOSTAL SEGMENT,
- [SDR CALA2020111301266](https://openairdocs.org/sdr/CALA2020111301266.md): Intercostal · cracked · Nov 12, 2020 · N402UA · Airbus A320232 · Emergency Exits
  > LT FWD EMERGENCY EXIT INTERAL STRUCTURE AFT VERTICAL INTERCOSTAL CRACKED AT FASTENER HOLES (A3NB-52-4-6031), PER HAECO LCQ NON ROUTINE 9296329 GENERATED BY V061623.
- [SDR CALA2020111301265](https://openairdocs.org/sdr/CALA2020111301265.md): Intercostal · cracked · Nov 12, 2020 · N402UA · Airbus A320232 · Emergency Exits
  > LT AFT EMERGENCY EXIT DOOR INTERNAL STRUCTURE FWD VERTICAL INTERCOSTAL CRACKED AT FASTENER HOLES (A3NB-52-4-6031), PER HAECO LCQ NON ROUTINE 9296331 GENERATED BY V061623.
- [SDR CALA2020111301264](https://openairdocs.org/sdr/CALA2020111301264.md): Intercostal · cracked · Nov 12, 2020 · N402UA · Airbus A320232 · Emergency Exits
  > LT FWD EMERGENCY INTERNAL STRUCTURE FWD VERTICAL INTERCOSTAL CRACKED AT FASTENER HOLES (A3NB-52-4-6031), PER HAECO LCQ NON ROUTINE 9296328 GENERATED BY V061623.
- [SDR CALA2020111301263](https://openairdocs.org/sdr/CALA2020111301263.md): Intercostal · cracked · Nov 12, 2020 · N402UA · Airbus A320232 · Emergency Exits
  > LT AFT EMERGENCY EXIT DOOR INTERNAL STRUCTURE AFT VERTICAL INTERCOSTAL CRACKED AT FASTENER HOLES (A3NB-52-4-6031), PER HAECO LCQ NON ROUTINE 9296330 GENERATED BY V061623.
- [SDR CALA2020102901219](https://openairdocs.org/sdr/CALA2020102901219.md): Skin · damaged · Oct 25, 2020 · N402UA · Airbus A320232 · Cargo/Baggage Doors
  > FWD CARGO DOOR DAMAGED BY LADDER. EVALUATED DAMAGE TO FWD CARGO DOOR, IAW SRM52-30-00-283-005 FIG 001. DEPTH.050 LENGTH 1.0 MATERIAL THICKNESS.063. FOUND TO BE OUT OF LIMITS. REPAIRED DAMAGE, IAW SRM 52-31-00-300-010 FIG 001 SHEET 1. THIS IS A CATAGORY
- [SDR CALA2018082001821](https://openairdocs.org/sdr/CALA2018082001821.md): Door Frame · corroded · Aug 17, 2018 · N402UA · Airbus A320232 · Fuselage Main, Structure
  > CORROSION WAS FOUND ON THE FWD CABIN R1 DOOR LWR FWD CORNER, FRAME 16 JUST ABOVE THE DOOR SILL. REPAIRED IAW REO-L20420, REV IR, AND ECRA 5310-06995.
- [SDR CALA2018082001820](https://openairdocs.org/sdr/CALA2018082001820.md): Skin · corroded · Aug 17, 2018 · N402UA · Airbus A320232 · Wing, Plate/Skin
  > RIGHT WING UPPER SURFACE, FROM RIBS 7 - 8, AND 4 INCHES FWD OF WING T /E WAS CORRODED. REPAIRED THE RT WING SKIN IAW ECRA 5725-01012, & REO L21513 REV IR.
- [SDR CALA2018011900245](https://openairdocs.org/sdr/CALA2018011900245.md): Slide · out of position · Jan 19, 2018 · N402UA · Airbus A320232 · Escape Slide
  > R1 DOOR WILL NOT ARM. ARM/DISARM LEVER BINDS IN ARM POSITION, WILL NOT STAY ARMED. OPS CHECKED THE DOOR ARM LEVER, DETERMINED THAT SLIDE PACK IS RESTING ON THE GIRT BAR CAUSING ARMING LEVER TO MOVE UP. REPLACED THE SLIDE IAW AMM 25-62-44, OPS CHECKED
- [SDR CALA2018011400193](https://openairdocs.org/sdr/CALA2018011400193.md): Girt Bar · out of position · Jan 14, 2018 · N402UA · Airbus A320232 · Emergency Equipment
  > R1 DOOR ARMS INTERMITTENTLY, REMOVED THE SLIDE, REPOSITIONED THE GIRT BAR TO ALLEVIATE BINDING, REINSTALLED THE SLIDE IAW AMM 25-62-44-000-804-A, AND 25-62- 44-400-803-A.
- [SDR CALA2018010700092](https://openairdocs.org/sdr/CALA2018010700092.md): Plate · dirty · Jan 7, 2018 · N402UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > SLIDE DIFFICULT TO ARM AT DOOR 1R FOUND DEBRIS IN THRESHOLD PLATES, CLEANED AND LUBED AND FOUND OPERATION NORMAL.
- [SDR CALA2017072102338](https://openairdocs.org/sdr/CALA2017072102338.md): Battery Pack · failed · Jul 21, 2017 · N402UA · Airbus A320232 · Emergency Lighting
  > AFT LT EMER LIGHT BATTERY PACK FAILS CAP CHECK. REMOVED AND REPLACED AFT LT EMER LIGHT BATTERY PACK. OPS CHECK GOOD. REF 33-51-38-400-002-A.
- [SDR CALA2017072102337](https://openairdocs.org/sdr/CALA2017072102337.md): Battery Pack · failed · Jul 21, 2017 · N402UA · Airbus A320232 · Emergency Lighting
  > LT EMER LIGHT BATTERY PACK FAILS CAP CHECK. REMOVED AND REPLACED LT EMER LIGHT BATTERY PACK, OPS CHECK GOOD REF 33-51-38-400-002-A.
- [SDR CALA2017072102336](https://openairdocs.org/sdr/CALA2017072102336.md): Battery Pack · failed · Jul 21, 2017 · N402UA · Airbus A320232 · Emergency Lighting
  > RT EMER EXIT BATTERY PACK FAILS CAP CHECK. REPLACED RT EMER EXIT BATTERY PACK PER AMM 33-51-38-400-002-A. OPS CHECK GOOD.
- [SDR CALA2017072102335](https://openairdocs.org/sdr/CALA2017072102335.md): Battery Pack · failed · Jul 21, 2017 · N402UA · Airbus A320232 · Emergency Lighting
  > LT FWD EMER LIGHT BATT PACK FAILS CAP CHECK. REPLACED LT FWD EMER LIGHT BATTERY PACK PER AMM 33-51-38-400-002 -A. OPS CHECK GOOD.
- [SDR CALA2017042301122](https://openairdocs.org/sdr/CALA2017042301122.md): Cover · loose · Apr 23, 2017 · N402UA · Airbus A320232 · Emergency Equipment
  > DOOR 2R SLIDE COVER OFF FOUND BUSTLE LOOSE SECURED SAME.
- [SDR CALA2016120901061](https://openairdocs.org/sdr/CALA2016120901061.md): Power Supply · faulty · Dec 9, 2016 · N402UA · Airbus A320232 · Emergency Lighting
  > EMERGENCY LIGHT TEST SHOWS EPSU EMERGENCY LIGHT FAULT. REPLACED EMERGENCY LEFT POWER SUPPLY AND BATTERY IAW MM 33-51-38 PG.0401. EMERGENCY LIGHT TEST OPS CHECKED NORMAL. REPLACED EMERGENCY LEFT EPSU AND BATTERY IAW MM 33-51-38, PG401.
- [SDR CALA2016112395985](https://openairdocs.org/sdr/CALA2016112395985.md): Stiffener · damaged · Nov 18, 2016 · N402UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT OF FRAME 68 AT STRINGER 23R HAS A ENONGATED HOLE IN FRAME STIFFNER. REMOVED AND REPLACED THE STIFFENER IAW SRM 53-11-13 FIG 11 AND 51-42-11.
- [SDR CALA2016111695976](https://openairdocs.org/sdr/CALA2016111695976.md): Stringer · corroded · Nov 12, 2016 · N402UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > FWD CARGO STR42R CORRODED 8" FWD OF FR34. STR 42R BETWEEN FR33-34 REPAIRED IAW SRM53-21-13 PARA 5D FG204.
- [SDR CALA2016110495970](https://openairdocs.org/sdr/CALA2016110495970.md): Frame · corroded · Nov 2, 2016 · N402UA · Airbus A320232 · Fuselage Main, Frame
  > AFT FACE OF FR66 HAS CORROSION JUST ABOVE R2 DOOR SILL BEAM. BLENDED AFT FACE OF FR66 JUST ABOVE DOOR SILL BEAM AND FOUND TO BE OUT OF LIMITS ACP NDT OF HOLES AND SURFACE AREA IAW NTM 51-10-08 & 51-10-04 & NO DEFECTS FOUND. FABBED FR66 REPAIR FROM 7075-T7.
- [SDR CALA2016110295893](https://openairdocs.org/sdr/CALA2016110295893.md): Cleat · corroded · Nov 2, 2016 · N402UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > FWD CARGO UNDER FLOOR BILGE AREA CLEAT ON FR29 AND STR 42R HAS CORROSION ON THE SURFACE. REMOVED AND REPLACED CLEAT IAW SRM 51-72-11.
- [SDR CALA2016110295892](https://openairdocs.org/sdr/CALA2016110295892.md): Cleat · corroded · Nov 2, 2016 · N402UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > FWD CARGO FR33 STR42R CLEAT HAS CORROSION. REMOVED AND REPLACED CLEAT AT STR 42R FR29 IAW SRM 51-72-11.
- [SDR CALA2016110295891](https://openairdocs.org/sdr/CALA2016110295891.md): Door Sill · corroded · Nov 1, 2016 · N402UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > RT DOOR SILL HAS CORROSION IN FWD GIRT BAR AREA AT FR66. REPLACED R2 DOOR SILL IAW SRM 51-42-11.
- [SDR CALA2016110295884](https://openairdocs.org/sdr/CALA2016110295884.md): Cleat · corroded · Oct 27, 2016 · N402UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > FWD BILGE AREA HAS CORROSION ON CLEAT BETWEEN STR-41L AND STR-40L AT FRAME 34. REMOVED AND REPLACED CLEAT BETWEEN STR41L AND STR40L AT FR 34 IAW SRM 51-72-11.
- [SDR CALA2016110295882](https://openairdocs.org/sdr/CALA2016110295882.md): Door Sill · corroded · Oct 26, 2016 · N402UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > L2 DR SILL HAS CORROSION NEAR FWD GIRT BAR FITTING. L2 DOOR SILL REPAIRED IAW SRM 53-41-14 PARA 5A FG201.
- [SDR CALA2016110295881](https://openairdocs.org/sdr/CALA2016110295881.md): Cleat · corroded · Oct 26, 2016 · N402UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > FWD CARGO BILGE CLEAT AT STR 43R AND FR32 HAS CORROSION. REPLACED CLEAT AT STR 43R AND FR32 IAW SRM51-42-11.
- [SDR CALA2016102495853](https://openairdocs.org/sdr/CALA2016102495853.md): Stringer · corroded · Oct 24, 2016 · N402UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > AFT CARGO INTERIOR BILGE AREA, STRINGER 42L HAS SURFACE CORROSION BETWEEN FRAMES 56-57. REMOVED AND REPLACED THE STRINGER IAW SRM 51-72-11.
- [SDR CALA2016102495838](https://openairdocs.org/sdr/CALA2016102495838.md): Stringer · corroded · Oct 21, 2016 · N402UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > FWD CARGO UNDER FLOOR BILGE AREA REPAIR SPLICE ON STR41 R BETWEEN FR30-31 HAS SURFACE CORROSION. REMOVED AND REPLACED SPLICE ON STR 41R BETWEEN FR30-31 FWD CARGO UNDER FLOOR BILGE AREA IAW A320 SRM 51-72-11 PARA 5.
- [SDR CALA2016101995819](https://openairdocs.org/sdr/CALA2016101995819.md): Cleat · corroded · Oct 14, 2016 · N402UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > FWD CARGO CLEAT AT FR27 AND STR 43R HAS CORROSION. REMOVED AND REPLACED CLEAT AT FR27 AT STR 43R IAW SRM 51-72-11.
- [SDR CALA2016081195622](https://openairdocs.org/sdr/CALA2016081195622.md): Light · malfunctioned · Jun 18, 2016 · N402UA · Airbus A320232 · Emergency Lighting
  > NUMEROUS CIDS PA LIGHTS INTERMITTENT. CABIN LIGHTS TO FULL BRIGHT ON T/O. BITE CHECK OF CIDS SYSTEM AND OPS CHECKS OF LIGHTS ALL CHECK GOOD. OK TO CONT.
- [SDR CALA2016061795462](https://openairdocs.org/sdr/CALA2016061795462.md): Director · faulty · Jun 14, 2016 · N402UA · Airbus A320232 · Audio/Video Monitoring
  > ON CLIMB, CONTINUOUS EVAC HORN, AND CI DS 1 & 2 FAULTS ON ECAM. REPLACED 1 & 2 CIDS DIRECTORS REF AMM 23-73-34-400, NO FAULTS AT THIS TIME.
- [SDR CALA2015121794896](https://openairdocs.org/sdr/CALA2015121794896.md): Director · faulty · Dec 15, 2015 · N402UA · Airbus A320232 · Audio/Video Monitoring
  > EVAC ALARM, CANT SILENCE. REPLACED NR 2 CIDS DIRECTOR IAW AMM 23-73-34-400-001-A. BITE TEST OK IAW AMM 23-73-00-740-003.
- [SDR CALA2015050493652](https://openairdocs.org/sdr/CALA2015050493652.md): Battery · discharged · May 3, 2015 · N402UA · Airbus A320232 · Emergency Lighting
  > FORWARD LT & AFT LT EMER LIGHT BATTERIES FAIL CAPACITY TEST. REPLACED 10WL & 13WL BATTERIES IAW AMM 33-51-38-000-002-A & 33-51-38-400-002-A. CAPACITY TESTED OK IAW AMM 33-51-00-710-003.
- [SDR CALA2015031793429](https://openairdocs.org/sdr/CALA2015031793429.md): Connector · not seated · Mar 12, 2015 · N402UA · Airbus A320232 · Emergency Lighting
  > INTERIOR LOADS EMER R FAULT WHEN PERFORMING EMER LIGHTS TEST. REMOVED & INSTALLED SAME BATTERY PACK & RESEATED CONNECTOR ON POWER SUPPLY UNIT. RETESTED & CHECKED OKAY.
- [SDR CALA2015030993408](https://openairdocs.org/sdr/CALA2015030993408.md): Skin · damaged · Feb 28, 2015 · N402UA · Airbus A320232 · Wing, Plate/Skin
  > LEFT WING LOWER SURFACE OPENING FOR FUEL PANEL 540JB HAS ELONGATED SCREW HOLE. REPAIRED HOLE IAW ECRA 5720-02637.
- [SDR CALA2015030993407](https://openairdocs.org/sdr/CALA2015030993407.md): Door Frame · cracked · Feb 28, 2015 · N402UA · Airbus A320232 · Fuselage Main, Structure
  > AFT PAX DOOR CUT OUT, DOOR STOP FITTING HOLES AT FRAME 68 WEB, RT POSITION 7 LOWER INBD HOLE IS CRACKED AT APPROX 6 O'CLOCK & 12 O'CLOCK POSITIONS. HOLE WAS OPENED UP TO.417 & CRACK FREE VIA NTM51 -10-01-PB6. FINAL REAM TO.438 & FREEZE PLUG INSTALLED IAW S
- [SDR CALA2015030493206](https://openairdocs.org/sdr/CALA2015030493206.md): Skin · damaged · Feb 28, 2015 · N402UA · Airbus A320232 · Wing, Plate/Skin
  > LEFT WING LOWER SURFACE OPENING FOR FUEL PANEL 540JB HAS ELONGATED SCREW HOLE. REPAIRED HOLE IAW ECRA 5720-02637. REQUIRES 1ST INSPECTION AFTER ACFT 1ST FLIGHT AT 31.1K FC 54.6K FH & SUBSEQUENT INSPECTIONS A T 3.6K FC 4.5K FH IAW SRI 57-21-11 TBL 203. CURRE
- [SDR CALA2015030493205](https://openairdocs.org/sdr/CALA2015030493205.md): Door Frame · cracked · Feb 28, 2015 · N402UA · Airbus A320232 · Fuselage Main, Structure
  > AFT PAX DOOR CUT OUT, DOOR STOP FITTING HOLES AT FRAME 68 WEB RT POSITION 7 LOWER INBD HOLE IS CRACKED AT APPROX 6 O'CLOCK & 12 O'CLOCK POSITIONS. HOLE WAS OPENED UP TO.417 & CRACK FREE VIA NTM51-10-01-PB6. FINAL REAM TO.438 & FREEZE PLUG INSTALLED IAW SRM
- [SDR CALA2014082692023](https://openairdocs.org/sdr/CALA2014082692023.md): Skin · damaged · Aug 22, 2014 · N402UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > UPPER FUSELAGE SKIN FRAME 60 STRINGER 2L - 3L HAS EXISTING EXT REPAIR IN AREA OF WIFI DOUBLER INSTALLATION. INT SKIN IN SAME AREA HAS EXISTING SCRIBE MARKS AROUND SHEAR TIES & DRILL START. REPLACED EXISTING DOUBLER IAW ECRA 5340-01571 & REO-L01421. BLENDED
- [SDR CALA2014062091311](https://openairdocs.org/sdr/CALA2014062091311.md): Cover · unsecure · Jun 18, 2014 · N402UA · Airbus A320232 · Emergency Equipment
  > SLIDE PACK AT DOOR 1L IS PREVENTING THE DOOR FROM BEING CLOSED. SECURED DOOR 1L DECORATIVE COVER IAW AMM 25-62-44-000-012-A.
- [SDR CALA2014040890772](https://openairdocs.org/sdr/CALA2014040890772.md): Wire · damaged · Apr 7, 2014 · N402UA · Airbus A320232 · Light System Wiring
  > REF 2 SVC EMERGENCY LIGHTS OPERATIONAL TEST MSG DISPLAYED WHEN TEST FAILED. ATA 33-51-38 EXT LOADS FWD L. TESTED AT EPSU, STILL FAILED. ALSO FAILED WITH TESTER CONNECTED AT EACH FWD SLIDE. RANG WIRING FROM 2871VC ON DOOR 1L TO GND & NO GND FOUND. BETWEEN

Next page: https://openairdocs.org/aircraft/N402UA/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 = 'N402UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N402UA/reports

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