# Service difficulty reports: N427UA

A list on [N427UA](https://openairdocs.org/aircraft/N427UA.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 · 123 reports

- [SDR CALA2025072106784](https://openairdocs.org/sdr/CALA2025072106784.md): Wire · pulled · Jul 18, 2025 · N427UA · Airbus A320232 · Light System Wiring
  > SEAT 30C EMERGENCY LIGHTING INOP - WIRE PULLED FROM PLUG REMOVED OLD PIN AND STRIPPED WIRE RE-CRIMPED NEW SOCKET ON TO WIRE AND INSTALLED IN CONNECTOR AT SEAT 30C REF AWM 33-51-08 PAGE 52A. INSTALLED LIGHT AT SEAT 30C REF TASK 33-51-19-400-002-A OPS CHECK GOOD
- [SDR CALA2023102503192](https://openairdocs.org/sdr/CALA2023102503192.md): Unknown · unknown · Oct 24, 2023 · N427UA · Airbus A320232 · Air Distribution System
  > FA REPORTS BURNING PLASTIC SMELL IN AFT ACFTDURING TAXI. ON GATE RETURN DEBRIEF CREW REPORTS ODOR IN AFT CABIN UPON #2 ENGINE START. CREW SHUT DOWN #2 ENGINE AND ODOR DISSIPATED. ACCOMPLISHED WALKAROUND EXTERNAL INSPECTION OF RAM AIR DUCTS AND BOTH ENGINES.
- [SDR CALA2023102303136](https://openairdocs.org/sdr/CALA2023102303136.md): Fuel Cap · missing · Sep 28, 2023 · N427UA · Airbus A320232 · Fuel Storage
  > FUEL CAP MISSING UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. CHECK WITH FUELER TO CONFIRM CAP IS MISSING. CHECK COUPLING FOR LEAKS AND APPLY INOP STICKER IN FLIGHT DECK AS REQUIRED PER CDL 28A. 847-700-9980 MAC
- [SDR CALA2023071702265](https://openairdocs.org/sdr/CALA2023071702265.md): Service Door · missing · Jul 15, 2023 · N427UA · Airbus A320232 · Fluid Service Doors
  > PDA 2 DURING UPON ARRIVAL FOUND POTABLE WATER SERVICE DOOR 171AL MISSING. REF IPC 52-42-04-21A 171AL P/N D5348005700851 WAS UNEXPECTEDLY REMOVED PIC ADDED
- [SDR CALA2023030300618](https://openairdocs.org/sdr/CALA2023030300618.md): Frame · cracked · Mar 2, 2023 · N427UA · Airbus A320232 · Fuselage Main, Frame
  > WHILE PERFORMING INSPECTIONS ON LH CONTINUITY FITTING, A CRACK W AS FOUND. CRACK FINDINGS CALL FOR REPLACEMENT OF LH/RH CONTINUIT Y FITTINGS. CRACKS WERE ALSO FOUND IN THE LH/RH WINDSHIELD FRAME S HOLES COMMON TO CONTINUITY FITTING HOLES AT 2 O?CLOCK AND 7-8 O
- [SDR CALA2023030300594](https://openairdocs.org/sdr/CALA2023030300594.md): Frame · none · Mar 2, 2023 · N427UA · Airbus A320232 · Fuselage Main, Structure
  > FOR THE REPAIR PERFORMED AT FRONT WINDSHIELD FRAME AND LH/RH CONTINUITY FITTINGS ? PLANNING TO CONTACT ENGINEERING AFTER 63,104 TFC BUT BEFORE 64,104 TFC FOR ECRA 5311-02954 PART 2 INSPECTION REQUIREMENTS. REF LP 3976500. 63,104 TFC BUT BEFORE 64,104 TFC FOR E
- [SDR CALA2023021300426](https://openairdocs.org/sdr/CALA2023021300426.md): Stop · cracked · Feb 13, 2023 · N427UA · Airbus A320232 · Fuselage Main, Frame
  > LEFT FR66 DOORSTOP #1 INBD LOWER HOLE HAS CRACK INDICATIONS IN F RAME 1 POSITION. GEN BY V061671 ON HAECO LCQ NR 9298406/42406 CRACKS NOTED.REQUIRES INSP AT 31,600 FC FROM RPR EMBODIMENT WITH 53-41-12-205-010 TABLE 001.THIS IS A CLASS B RPR. ALL WORK ACMP SUBS
- [SDR CALA2023021300417](https://openairdocs.org/sdr/CALA2023021300417.md): Stop · cracked · Feb 12, 2023 · N427UA · Airbus A320232 · Fuselage Main, Frame
  > LEFT FR66 DOORSTOP #1 OTBD UPPER HOLE HAS A CRACK INDICATION IN FRAME AT 8:30 POSITIONS. GEN BY V061671 ON HAECO LCQ NR 9298407( 42407) AMED BUSHING TO FINAL ID OF.2815? IAW SRM 53-41-12-300-010. LEF UIRES INSPECTION AT 33,000 FC AND SUBSEQUENT INSPECTION AT
- [SDR CALA2023021300414](https://openairdocs.org/sdr/CALA2023021300414.md): Stop · cracked · Feb 11, 2023 · N427UA · Airbus A320232 · Fuselage Main, Frame
  > LEFT FR66 DOORSTOP #1 INBD LOWER HOLE HAS CRACK INDICATIONS IN F RAME AT 6 POSITION. GEN BY V061671 ON HAECO LCQ NR 9298406/42406 EMBODIMENT AT 60,000 FC IAW SRI 53-41-12-205-010 TABLE 001 AREA 3.THIS IS A CAT B RPR.ALL WRK ACMP ON HAECO NR 9298406. ACMP BATHT
- [SDR CALA2022123003527](https://openairdocs.org/sdr/CALA2022123003527.md): Structure · cracked · Dec 29, 2022 · N427UA · Airbus A320232 · Emergency Exits
  > REMOVED AND REPLACED CRACKED INTERNAL STRUCTURE EDGE ON RH FWD O /W EMERGENCY EXIT IAW SRM 51-72-911-001 GEN BY V061682 ON H AECO LCQ NR #9298446
- [SDR CALA2022122603490](https://openairdocs.org/sdr/CALA2022122603490.md): Fitting · corroded · Dec 24, 2022 · N427UA · Airbus A320232 · Passenger/Crew Doors
  > L2 DOOR AFT LOWER CORNER FITTING HAVE CORR AROUND FASTENER HEAD. REMOVED AND REPLACED CORRODED AFT LOWER CORNER FITTING AT L2 DOO R IAW A320 SRM 51-72-11-911-002, 53-41-79-283-002.
- [SDR CALA2022120203268](https://openairdocs.org/sdr/CALA2022120203268.md): Line · damaged · Dec 2, 2022 · N427UA · Airbus A320232 · Hydraulic System, Main
  > HYD Y RSVR LO LVL ON ECAM UPON ACFT VISUAL INSPECTION FOUND O RING DAMAGED ON YELLOW HYD ITEM 40. SYSTEM MANIFOLD PRESS LINE R/ R O RING AS REQUIRED REF AMM 29-13-14-000-001-A. RUN BOTH ENG AND PRESSURIZED ALL THREE SYST, NO LEAKS NOTED. ALL IND SHOWED NOR
- [SDR CALA2022113003258](https://openairdocs.org/sdr/CALA2022113003258.md): Liner · damaged · Nov 30, 2022 · N427UA · Airbus A320232 · Turbine Engine Air Inlet Section
  > NR 1 ENGINE FAN BLADE ATTRITION LINER ONE, SEGMENT AT APPOX 3 O`CLOCK POSITION, AFT LOOKING FWD IS MISSING MAITERIAL APPOX 3 X 3.5 IN. REQUEST 20 CYCLE DIP. REF MT 72-017. DAMAGE, MISSING MATERIAL ON ATTRITION LINER IS LESS THAN 20%. WITHIN DIP LIMITS, F
- [SDR CALA2022092302459](https://openairdocs.org/sdr/CALA2022092302459.md): Fuel Cap · missing · Sep 23, 2022 · N427UA · Airbus A300* · Aircraft Fuel System
  > FUELER REPORTS FUEL CAP LANYARD MISSING. FEKYIBELU, SHOAREGA (V941348)DEFERRED REF CDL 28A INOP PLACARD INSTALLED. DISPATCH DESK: 23 NAME: V.O. DATE: 21-SEP-22- DEFERRED DIRECTLY BY TOMC UPDATED MAA CODE FIX USING VENDOR MAA SCREEN UPDATED MAA CODE FIX USING
- [SDR CALA2021111802136](https://openairdocs.org/sdr/CALA2021111802136.md): Check Valve · leaking · Nov 18, 2021 · N427UA · Airbus A320232 · Hydraulic System, Main
  > Y HYD SYSTEM LOSS OFFLUID. LOW PRESSURE UPDATED MAA CODE FIX USING VENDOR MAA SCREEN MAC METER INITIATED FOR WITH VENDOR ID V834237 PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. ADVISED LOCAL MAC RELATED WORK ORDER 000000003027239 AND PRTR FBO TO PERFORM
- [SDR CALA2021043000565](https://openairdocs.org/sdr/CALA2021043000565.md): Transceiver · inoperative · Apr 28, 2021 · N427UA · Airbus A320232 · Weather Radar System
  > RADAR/PRED WS APPEARINOP REPLACED WXR TRANSCEIVER REF MM34-41-33-400-003-A AND IPC 34-41-33-991-00300-C ITM 1B OPS CHECKED NORMAL. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1993500 SN OFF 2280 TRANSCEIVER, WX OFF 31-2311-9-0001 2280 ON 31-2311-9-0001 2104
- [SDR CALA2021010600010](https://openairdocs.org/sdr/CALA2021010600010.md): Battery Pack · no test · Jan 4, 2021 · N427UA · Airbus A320232 · Emergency Lighting
  > EPSU BATTERY 12WL (RT) FAILS CAP CHECK A3NB-33-3-6013 ON HAECO LCQ, REF 9298007.
- [SDR CALA2020112501301](https://openairdocs.org/sdr/CALA2020112501301.md): Actuator · leaking · Nov 23, 2020 · N427UA · Airbus A320232 · Emergency Equipment
  > R1 DOOR EMERGENCY ASSIST ACTUATOR IS LEAKING. REMOVED AND REPLACED R1 DOOR ACTUATOR ON AERSALE NON ROUTINE 516704. MECH V931327 QC- ASI QC-50. ROTABLE PARTS CHANGE WAS INDICATED-TT NR 1651579 S/N OFF 3153 IPC REFERENCE NR 52-11-01D.
- [SDR CALA2019020200205](https://openairdocs.org/sdr/CALA2019020200205.md): Hinge Fitting · cracked · Feb 2, 2019 · N427UA · Airbus A320232 · Landing Gear Doors
  > LT FWD MLG DOOR HINGE FWD LUG FWD FACE IS FRETTING ON LCQ REF 9294327 AD 2015-02-14. R&R LT MLG FWD HINGE FTG IAW SRM 51-42-11 PARA 2F4C PGS 19 & 20.
- [SDR CALA2019012100135](https://openairdocs.org/sdr/CALA2019012100135.md): Skin · corroded · Jan 21, 2019 · N427UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > LAV EXHAUST VENT INTERIOR SKIN HAS CORROSION BETWEEN FR69 AND FR 70 AND RST 32 EA 5100-02750002 PER LCQ NR 9294417 REPAIRED LAV EXHAUST VENT SKIN BETWEEN FR69-70 STR 31R-32R IAW SRM 53-41-11-300-004 THIS REPAIR TASK IS CATEGORY A PERMANEN T REPAIR BY MECH.
- [SDR CALA2019012100130](https://openairdocs.org/sdr/CALA2019012100130.md): Hinge Fitting · cracked · Jan 19, 2019 · N427UA · Airbus A320232 · Fuselage, Door Hinge
  > RT MLG FWD HINGE FWD LUG FWD FACE IS FRETTING ON LCQ REF 9 294329 AD 2015-02-14. REMOVED & REPLACED RT MLG FWD HINGE FTG IAW SRM 51-42-11 PARA 2F4C PGS 19 & 20 AT LCQ ON HANGAR NR 9294329.
- [SDR CALA2019012100127](https://openairdocs.org/sdr/CALA2019012100127.md): Stringer · corroded · Jan 18, 2019 · N427UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > STRINGER 23R FROM FRAME 68-69 HAS CORROSION AT SHEAR WEB TRAY REF LCQ NR 9295247 REMOVED & REPLACED STRINGER 23R FROM FR68-69 IAW SRM 51-42- 11-001 & 51-72-11-911-001 AT LCQ ON HANGAR NR 9295247.
- [SDR CALA2019011800112](https://openairdocs.org/sdr/CALA2019011800112.md): Tray · corroded · Jan 14, 2019 · N427UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > SHEAR WEB TRAY AT FR68-69 RT SIDE IS CORRODED PER LCQ NR 9 295137. FABRICATED NEW SHEAR WEB TRAY AT FR 68-69 RT REMOVED AND REPLAC ED IAW SRM 51-72-11-911-001.
- [SDR CALA2019010600039](https://openairdocs.org/sdr/CALA2019010600039.md): Stop Fitting · cracked · Jan 5, 2019 · N427UA · Airbus A320232 · Passenger/Crew Doors
  > R1 DOOR FRAME 16 STOP FITTING NR 7 INBOARD UPPER HOLE IS CRACKED AT 6:00 AND THOUGHT TO BE IN THE INTERCOSTAL FITTING A3NB-4-630 4 AD 2017-22-03. REAMED NR 7 FR16 UPPER HOLE TO 0.264 (R1 DOOR), REMOVED AND REPLACED WITH NEW INNERCOSTAL AND INSTALLED NR 7 DOOR
- [SDR CALA2019010600029](https://openairdocs.org/sdr/CALA2019010600029.md): Support · corroded · Jan 4, 2019 · N427UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT CABIN LT FR 69-70 SHEAR PLATE SUPPORT HAS CORROSION. REMOVED & REPLACED SHEAR PLATE SUPPORT LT FR69-70 IAW SRM 51-42-11 & 51-44-11.
- [SDR CALA2019010600028](https://openairdocs.org/sdr/CALA2019010600028.md): Door Sill · corroded · Jan 4, 2019 · N427UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > L2 DOOR SILL IS CORRODED. REMOVED & REPLACED L2 DOOR SILL IAW SRM 51-72-11-911-001.
- [SDR CALA2019010600027](https://openairdocs.org/sdr/CALA2019010600027.md): Door Sill · corroded · Jan 4, 2019 · N427UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > R2 DOOR SILL IS CORRODED. REMOVED & REPLACED R2 DOOR SILL IAW SRM 51-72-11-911-001.
- [SDR CALA2019010600019](https://openairdocs.org/sdr/CALA2019010600019.md): Intercostal · cracked · Jan 3, 2019 · N427UA · Airbus A320232 · Passenger/Crew Doors
  > R1 DOOR FRAME 16 STOP FITTING NR 7 INBOARD UPPER HOLE IS CRACKED AT 6:00 AND THOUGHT TO BE IN THE INTERCOSTAL FITTING A3NB-4-630 4 AD 2017-22-03. REAMED NR 7 FR16 UPPER HOLE TO 0.264 (R1 DOOR), REMOVED AND REPLACED WITH NEW INTERCOSTAL AND INSTALLED NR 7 DOOR
- [SDR CALA2018123102687](https://openairdocs.org/sdr/CALA2018123102687.md): Door Frame · cracked · Dec 30, 2018 · N427UA · Airbus A320232 · Fuselage Main, Structure
  > L1 DOOR FRAME 16STOP FITTING NO.7 INBOARD UPPER HOLE IS CRACKED AND THOUGHT TO BE IN INTERCOSTAL AT 6:00 A3NB-53-4-6304, AD 2017 -22-03 PER HAECO LCQ NON ROUTINE 9294400 GENERATED BY V061633 REMOVED INTERCOSTAL AT NO.7 STOP FITTING ON FR16 AND STOP FITTIN G NO
- [SDR CALA2018122902683](https://openairdocs.org/sdr/CALA2018122902683.md): Door Frame · cracked · Dec 29, 2018 · N427UA · Airbus A320232 · Fuselage Main, Structure
  > L1 DOOR FRAME 16STOP FITTING NO.7 INBOARD UPPER HOLE IS CRACKED AND THOUGHT TO BE IN INTERCOSTAL AT 6:00 A3NB-53-4-6304, AD 2017 -22-03 PER HAECO LCQ NON ROUTINE 9294400 GENERATED BY V061633 REMOVED INTERCOSTAL AT NO.7 STOP FITTING ON FR16 AND STOP FITTIN G NO
- [SDR CALA2018022000705](https://openairdocs.org/sdr/CALA2018022000705.md): Computer · faulty · Feb 20, 2018 · N427UA · Airbus A320232 · Drag Control System
  > GND SPOILER 3 AND 4 FAULT DISPLAYED ON UPPER ECAM SCREE N. F-CTL EMERGENCY DECLARED. REMOVED AND REPLACED SEC 1 COMPUTER PER MM27-94-00. OPS CHECK NORMAL.
- [SDR CALA2018020500483](https://openairdocs.org/sdr/CALA2018020500483.md): Fuel Cap · missing · Feb 5, 2018 · N427UA · Airbus A320232 · Fuel Storage
  > UPON ARRIVAL TO SNA, FUEL CAP IS MISSING. REF L/P 6011001. REPLACED FUEL CAP.
- [SDR CALA2017120804332](https://openairdocs.org/sdr/CALA2017120804332.md): Coffeemaker · odor · Dec 8, 2017 · N427UA · Airbus A320232 · Buffet/Galleys
  > COFFEE MAKER M42 AFT GALLEY HAS A BURNING PLASTIC SMELL. REMOVED AND CLEANED PLASTIC FROM HOT PLATE ON COFFEE MAKER M42 OPS CHECKS NORMAL
- [SDR CALA2017082102838](https://openairdocs.org/sdr/CALA2017082102838.md): Hinge Bracket · detached · Aug 21, 2017 · N427UA · Airbus A320232 · Escape Slide
  > ONE OF THE HINGES BRACKETS AT TOP OF SLIDE MECHANISM AT THE L2 DOOR NOT CONNECTED. THE BRACKET WAS REINSTALLED
- [SDR CALA2016103195880](https://openairdocs.org/sdr/CALA2016103195880.md): Battery Pack · no test · Oct 28, 2016 · N427UA · Airbus A320232 · Emergency Lighting
  > EMERGENCY EXIT LIGHT BATTERY FWD LEFT FAILED CAP TEST REPLACED THE BATTERY 10WL, OPS TEST PASSED
- [SDR CALA2016081895652](https://openairdocs.org/sdr/CALA2016081895652.md): Acm · seized · Aug 15, 2016 · N427UA · Airbus A320232 · Cabin Cooling System
  > AIRCRAFT DIVERED TO DUE TO SMOKE IN THE COCKPIT. CREW REPORTED LOUD NOISE AND HUM. NO DEFECTS WITH ELECTRICAL SYSTEM. FOUND NR 1 PACK SEIZED. R & R THE ACM, AND FILTERS. OPS CHECKED GOOD.
- [SDR CALA2015061593916](https://openairdocs.org/sdr/CALA2015061593916.md): Battery · discharged · Jun 12, 2015 · N427UA · Airbus A320232 · Emergency Lighting
  > EMERGENCY LIGHT TEST FAILS. MSG IS BATTERY FWD LT & BATTERY AFT LT. REPLACED FWD LT & AFT LT BATTERY. OPERATIONS CHECKED GOOD IAW AMM 33-51-38 & 33-51-39.
- [SDR CALA2014041790844](https://openairdocs.org/sdr/CALA2014041790844.md): Unknown · malfunctioned · Apr 16, 2014 · N427UA · Airbus A320232 · Emergency Lighting
  > WILL NOT PASS THE EMERGENCY LIGHTS TEST. REPLACED TB 7225VT IAW AW WM 33-51-02. PERFORMED EMERGENCY LIGHT TEST, TEST PASSED.
- [SDR CALA2014033190727](https://openairdocs.org/sdr/CALA2014033190727.md): Power Supply · faulty · Mar 31, 2014 · N427UA · Airbus A320232 · Emergency Lighting
  > LT EMERGENCY LIGHTS PSU FAULTED. REPLACED PSU IAW AMM 33- 51-38-000-001-A, OPERATIONS NORMAL.
- [SDR CALA2013121693733](https://openairdocs.org/sdr/CALA2013121693733.md): Screw · sheared · Dec 14, 2013 · N427UA · Airbus A320232 · Wing Miscellaneous Structure
  > SCREW HEAD SHEARED AFT EDGE OF SMALL COVER PANEL JUST AFT OF PANEL 191CT, LT WING ROOT AREA. REMOVED DAMAGED SCREW, REPLACED WITH NEW FASTENER, ALL SECURE.
- [SDR CALA2013112093119](https://openairdocs.org/sdr/CALA2013112093119.md): Retainer Seal · missing · Nov 19, 2013 · N427UA · Airbus A320232 · Passenger Oxygen System
  > PASSENGER SEAT OVERHEAD 02 MASK FELL AT 34DEF. PANEL HANGING DOWN, O2 CONTAINER ASSEMBLY LOOSE DUE TO APPROXIMATE 1 FT OF RETAINING SEAL MISSING. CONTAINER TRACK & J HOOK INTACT & CONTAINER SECURE. INTERIM REPAIR WITH TAPE IAW ECRA 2525-01548. SEATS 32DEF
- [SDR CALA2013111892983](https://openairdocs.org/sdr/CALA2013111892983.md): Rod End · sheared · Nov 15, 2013 · N427UA · Airbus A320232 · Passenger/Crew Doors
  > L1 DOOR TELESCOPIC ARM ROD SHEARED. REMOVED & INSTALLED NEW ROD END ASSEMBLY ON L1 DOOR IAW MM.
- [SDR CALA2013102392302](https://openairdocs.org/sdr/CALA2013102392302.md): Nose Cowl · damaged · Oct 22, 2013 · N427UA · Airbus A320232 · Engine Cowling System
  > NR 1 ENGINE NOSE COWL HAS A 1 INCH DIAMETER HOLE IN ABRADABLE LINER AT THE 6 OCLOCK POSITION 1ST STAGE FAN LINER. IAW MAINT TIP 2717, PARTS 841-0591 ADH3002-48 ADHESIVE
- [SDR CALA2013102392301](https://openairdocs.org/sdr/CALA2013102392301.md): Oxygen Mask · malfunctioned · Oct 22, 2013 · N427UA · Airbus A320232 · Crew Oxygen System
  > CAPTS O2 MASK STUCK IN EMERGENCY CONT FLOW, UNABLE TO SHUT OFF UNTIL RESTOWED. R & R CAPTAIN'S O2 MASK IAW AMM. TESTED IAW AMM.
- [SDR CALA2013091891269](https://openairdocs.org/sdr/CALA2013091891269.md): Smoke Warning · false activation · Sep 17, 2013 · N427UA · Airbus A320232 · Smoke Detection
  > LAVATORY F SMOKE DETECTOR. AFT LAVATORY 136 SMOKE HORN SOUNDED. ACCOMPLISHED TEST PER MM 26-00-00 OPS CKS GOOD NO FAULTS FOUND.
- [SDR CALA2013080890270](https://openairdocs.org/sdr/CALA2013080890270.md): Line · kinked · Aug 8, 2013 · N427UA · Airbus A320232 · Hydraulic System, Main
  > GROUNDING CLIP STUCK IN GEAR. HYD LINE IS KINKED. REPLACED GREEN SYS BRAKE LINE FWD SIDE OF RT MLG, NO LEAKS NOTED. BRAKE OPS NORMAL.
- [SDR UALA2013072505236](https://openairdocs.org/sdr/UALA2013072505236.md): Light · damaged · Jul 24, 2013 · N427UA · Airbus A320232 · Emergency Lighting
  > EMERGENCY PATH LIGHT FOUND DAMAGED. REPLACED EMERGENCY LIGHT ASSY,
- [SDR UALA2013071705006](https://openairdocs.org/sdr/UALA2013071705006.md): Unknown · unknown · Jul 16, 2013 · N427UA · Airbus A320232 · Fuselage Structure (General)
  > VERY LOUD SQUEALING NOISE IN BACK OF ACFT. SEEMS LOUDEST IN-BETWEEN DOORS. PRESSURIZED ACFT AND NO FAULTS FOUND. INSPECTED L2 AND R2 DOORS AND VHF ANTENNA AND NO DEFECTS NOTED.
- [SDR UALA2013070304663](https://openairdocs.org/sdr/UALA2013070304663.md): Oxygen Box · no test · Jul 3, 2013 · N427UA · Airbus A320232 · Crew Oxygen System
  > CAPTAIN`S OXYGEN BOX WILL NOT TEST. REPLACED OXYGEN BOX, OPS CHECKED GOOD IAW MM.
- [SDR UALA2013070304662](https://openairdocs.org/sdr/UALA2013070304662.md): Exhaust Duct · cracked · Jul 2, 2013 · N427UA · Airbus A320232 · Engine Collector/Tailpipe/Nozzle
  > NR 1 ENGINE EXHAUST TAILCONE HAS A CRACK APPROX 6 INCHES LONG AT THE 3 O'CLOCK POSITION FWD EDGE. FOUND A CRACK AT 9:00 POS THAT IS "Y" SHAPED WITH LEGS MEASURING 3.5 X 3.5X 2.5 INCHES FOR A TOTAL OF COMBINED LENGTH OF 9.5 INCHES. FOUND CRACK AT 3:00 POS AT

Next page: https://openairdocs.org/aircraft/N427UA/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 = 'N427UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N427UA/reports

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