# Service difficulty reports: N492UA

A list on [N492UA](https://openairdocs.org/aircraft/N492UA.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 2 · 75 reports

- [SDR CALA2025102210406](https://openairdocs.org/sdr/CALA2025102210406.md): Door · leaking · Oct 22, 2025 · N492UA · Airbus A320232 · Emergency Exits
  > EMERGENCY EXIT DOOR BY SEAT 21F HAS HIGH PITCH SQUEAL ABOVE FL25 0. CAB ALT/VS NORMAL. APPLIED SPEED TAPE TO WTB SEALS 192DT IAW MT 53-004, TAPE RECHECK DAILY, REPLACE SEALS WITHIN 1000 FH, REQUEST CREW COMMENT TO DETERMINE IF VIBRATION ELIMINATED. OK TO DIP T
- [SDR CALA2025090508495](https://openairdocs.org/sdr/CALA2025090508495.md): Cids · faulted · Sep 4, 2025 · N492UA · Airbus A320232 · Lighting System
  > EMER EXIT SIGN ON OVER WING AND OVER MCD STAYS ILLUMINATED ALL OTHER LTS REMAIN EXTIGUISHED TURNED OFF EMEGENCY LIGHT SWITCH AND PERFORMED FULL CIDS SYSTEM RESET. EMERGENCY LIGHTS EXTINGUISHED. CYCLED SWITCH IN ALL POSITIONS 3 TIMES. ALL EMERGENCY LIGHTS NOW O
- [SDR CALA2025090308428](https://openairdocs.org/sdr/CALA2025090308428.md): Plug · deteriorated · Aug 31, 2025 · N492UA · Airbus A320232 · Landing Gear Position and Warning
  > LEFT MLG DOOR AFT PROX SENSOR SWITCH (35GA)HAS DETERIORATED PLUG RUBBER. REPLACED LT MLG AFT PROX SENSOR SWITCH (35GA) AND ADJUSTED GAP REF AMM 32-12-11-820-059-A UP TO STEP 3K(G).. MLG DOOR OPERATIONAL CHECK WILL BE ACCOMPLISHED ON LOG ITEM 606683.
- [SDR CALA2025081107573](https://openairdocs.org/sdr/CALA2025081107573.md): Battery Pack · inoperative · Aug 9, 2025 · N492UA · Airbus A320232 · Emergency Lighting
  > DURING TEST FOUND ERROR MSG "EPSU BATTERY EMER L" ATA 33-51-38 SEE PIC REMOVED AND REPLACED LEFT OVERWING EMERGECNY EXIT LIGHT POWER SUPPLY BATTERY REF AMM 33-51-38/401. OPS CHECK GOOD, BITE TEST PASSES WITH A GREEN SYS OK LIGHT AND NO FAULTS.
- [SDR CALA2025081107572](https://openairdocs.org/sdr/CALA2025081107572.md): Battery Pack · inoperative · Aug 9, 2025 · N492UA · Airbus A320232 · Emergency Lighting
  > WHILE PERFORMING BITE OF EPSU SYSTEM REF AMM 33-51-00-710-001-A RECIEVED AN EPSU BATTERY AFT L MESSAGE REMOVED AND REPLACED THE AFT LEFT EPSU BATTERY REF AMM 33-51-38/401. OPS CHECK GOOD, FAULT IS NO LONGER PRESENT AND THE BITE TEST PASSES.
- [SDR CALA2025060405256](https://openairdocs.org/sdr/CALA2025060405256.md): Battery · no test · Jun 3, 2025 · N492UA · Airbus A320232 · Emergency Lighting
  > EPSU BATT FWD L FAULT MESSAGE ON EMERGENCY LIGHT TEST. REPLACED FWD L EPSU BATTERY REF AMM 33-51-38/401. OPS CHECK GOOD. PARTS USED: 18-3351-3-0001, QTY:1
- [SDR CALA2025040903651](https://openairdocs.org/sdr/CALA2025040903651.md): Proximity Switch · faulted · Apr 5, 2025 · N492UA · Airbus A320232 · Door Warning System
  > AFT CARGO ECAM INDICATION REF LP 4404361 DEFERRED IAW MEL 5270D NOC DESK: 320 NAME: ATE: 05-APR-25. APPROVED DEFERRED *DM* SEE TSM 52-32-00-810-801-A & ASM 31-54-05 FOR T/S ASSIST. ADDED PROX SWITCHES (32WV, 34WV) IF NEEDED. PARTS UPDATED. REPLACED AFT CARGO S
- [SDR CALA2024122701681](https://openairdocs.org/sdr/CALA2024122701681.md): Battery · inoperative · Dec 25, 2024 · N492UA · Airbus A320232 · Emergency Lighting
  > DURING OPERATIONAL CHECK OF EPSU BATTERIES, MESSAGES "EPSU BATTERY EMER R" AND "EPSU BATTERY AFT L" PRESENT. REMOVED AND REPLACED RIGHT EPSU BATTERY AND AFT LEFT EPSU BATTERY REF 33-51-38. OPS CHECK GOOD, MESSAGES DID NOT RETURN.
- [SDR CALA2024091700647](https://openairdocs.org/sdr/CALA2024091700647.md): Fuel Cap · missing · Sep 16, 2024 · N492UA · Airbus A320232 · Fuel Storage
  > PDA 2 FUEL CAP FOUND MISSING. ITEM PUT ON CDL 28A. REF LP# 9273271.FUEL CAP MISSING.REQUESTING CDL 28A CDL 28A APPLIED DISPATCH DESK: 14 NAME: BB DATE: 16-SEP-24 28A APPROVED.LOCATED MISSING REFUEL COUPLING CAP IN DEN. REINSTALLED REFUEL COUPLING CAP REF IPC
- [SDR CALA2024062400087](https://openairdocs.org/sdr/CALA2024062400087.md): Actuator · faulted · Jun 20, 2024 · N492UA · Airbus A320232 · Engine Thrust Reverser
  > REVERSER FAULT DISPLAYED ON UPPER ECAM SCREEN. - ENG 2 ENG 2 REVERSER FAULT ON ARRIVAL ENG NO 2 REV FAULTED BOTH CH A AND CH B ON REV LVDT /HC/EEC2 FIN. IF NEEDED ACTUATOR M&E NUMBER IS 31-7832-9-0002. *DM* AVIATAR CONFIRMS FAULT "REV LVDT CHB / HC / EEC2" RE
- [SDR CALA2024032600867](https://openairdocs.org/sdr/CALA2024032600867.md): Fuel Cap · missing · Mar 22, 2024 · N492UA · Airbus A320232 · Fuel Storage
  > PDA 2 FUEL CAP MISSING ON ARRIVAL. FUEL CAP MISSING, VERIFIED NO LEAKS. INSTALLED FUEL CAP AND LANYARD IN REF TO AMM 28-25-41-400-005-A. FUEL CAP SECURE.
- [SDR CALA2024012300204](https://openairdocs.org/sdr/CALA2024012300204.md): Accumulator · leaking · Jan 16, 2024 · N492UA · Airbus A320232 · Hydraulic Power Accumulator, Main
  > BLUE SYSTEM LOST HYD FLUID IN FLIGHT BOTTOM OF AIRCRAFT WET WITH HYD FLUID. ACCUMULATOR, HY OFF 31-2912-9-9001 7440 ON 0000 ACCUMULATOR, HY OFF 31-2912-9-9001 7440 ON 31-2912-9-9001 7098 REPLACED BLUE SYSTEM ACCUMULATOR REF 29-12-00,OP CHECKS GOOD NO LEAKS FOU
- [SDR CALA2024010500035](https://openairdocs.org/sdr/CALA2024010500035.md): Accumulator · leaking · Jan 3, 2024 · N492UA · Airbus A320232 · Hydraulic Indicating System
  > ECAM CAUTION MESSAGE - B RSVR LO LVL MESSAGE INOP - HYD FOUND HYDRAULIC FLUID LEAKING SCHRADER AT TOP OF BLUE SYSTEM ACCUMULATOR. ORDERED ACCUMULATOR, SCHRADER VALVE,PRESSURE GAUGE, AND O-RINGS.. PLACED PARTS IN GALLEY. LOGPAGE FLAGGED FOR SDR REPORTING ROT
- [SDR CALA2022102802980](https://openairdocs.org/sdr/CALA2022102802980.md): Stringer · corroded · Oct 27, 2022 · N492UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > AFT CARGO PIT R/H BETWEEN FR63-64 STRINGER 41R HAS CORROSION DOT M026. PER HAECO LCQ NR 9296400/20400 REMOVED AND REPLACED STRINGER 41RT IN AFT CARGO PIT FR 58-64 IAW A320 SRM 51-72-11-911-001
- [SDR CALA2022102702965](https://openairdocs.org/sdr/CALA2022102702965.md): Fitting · cracked · Oct 26, 2022 · N492UA · Airbus A320232 · Fuselage Main, Frame
  > LEFT AND RIGHT CONTINUITY FITTINGS HAVE CRACK INDICATIONS AT AFT EDGE OF HORIZONTAL LEG 15/16 INCHES OTBD OF WINDOW FRAME INBD ED GE (CENTER POST LINE) PER HAECO LCQ N/R 9296249/20249 GEN BY V06 1671 REMOVED AND REPLACED 2EA L/H AND R/H CONTINUITY FITTINGS IAW
- [SDR CALA2022102402909](https://openairdocs.org/sdr/CALA2022102402909.md): None · cracked · Oct 21, 2022 · N492UA · Airbus A320232 · Fuselage Structure (General)
  > REV B (AD 2022-02-11) L/H FR20 DOOR STOP FITTING #7 UPPER INBD H OLE (H1) FOUND CRACKED AFTER HFEC ROTO INSPECTION. CRACK APPEARS IN INTERCOASTAL LAYER AT APPROXIMATELY 4 O''CLOCK "REPAIR BEFORE NEXT FLIGHT" REMOVED AND REPLACED CRACKED INTERCOASTAL AT FR20 LH
- [SDR CALA2022101402799](https://openairdocs.org/sdr/CALA2022101402799.md): None · corroded · Oct 13, 2022 · N492UA · Airbus A300* · Standard Practices/Structures
  > FWD CARGO FRAME 25 STRINGER 41RT-42RT CLEAT HAS CORROSION PER HA ECO LCQ N/R 9296371/20371 GEN BY V052030
- [SDR CALA2022101202766](https://openairdocs.org/sdr/CALA2022101202766.md): Stringer · corroded · Oct 11, 2022 · N492UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > AFT CARGO PIT L/H BETWEEN FR58-59 STRINGER 42L HAS CORROSION DOT M015 A3NB-53-4-6179 GENERATED BY V929150 AT HAECO LCQ PER NR 929 6396 (20396) REMOVED AND REPLACED AFT CARGO L/H FR58-59 STRINGER42L PER A320 SRM 51-72-11-911-002 AND SRM 51-42-11/001 PERFORMED B
- [SDR CALA2020120901349](https://openairdocs.org/sdr/CALA2020120901349.md): Skin · damaged · Dec 7, 2020 · N492UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > UPON ARRIVAL ORD, GOUGE WAS BLENDED, PER SRM 53-11-11-283-001 AND HFEC ACCOMPLISHED PER NTM 51-10-08 WITH NO CRACKS FOUND. ULTRA SOUND WAS ACCOMPLISHED, PER NTM PT4-00-04-02 AND MEASURMENTS ISSUED ON MATRIX. BLEND IS LOCATED APPROXIMATELY 11.5" AFT OF STATIC
- [SDR CALA2020011900157](https://openairdocs.org/sdr/CALA2020011900157.md): Fitting · corroded · Jan 15, 2020 · N492UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > UPON REMOVAL OF R2 DOOR SILL, FOUND FR68 CORNER FITTING CORRODED -SUPPORT TASK. REMOVED AND REPLACED CORNER FITTING AT FR68 AT R2 DOOR SILL IAW SRM 51-72-11-911-001 WORK ACCOMPLISHED, INSPECTED.
- [SDR CALA2020011900159](https://openairdocs.org/sdr/CALA2020011900159.md): Door Sill · corroded · Jan 15, 2020 · N492UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT CABIN R2 DOOR SILL IS CORRODED AT FR68 SUPPORT TASK PER NR 9296179 GENERATED. REMOVED AND REPLACED DOOR SILL AT R2 DOOR IAW SRM 51-72-11- 911-002 WORK ACCOMPLISHED, INSPECTED.
- [SDR CALA2020011300133](https://openairdocs.org/sdr/CALA2020011300133.md): Shear Plate · corroded · Jan 12, 2020 · N492UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT MAIN CABIN R/H SHEER PLATE FR69-70 HAS CORROSION-(SUPPORT TA SK) AT HAECO LCQ REF. NO. 9296137, GENERATED. REMOVED AND REPLACED 1EA CORRODED SHEAR WEB IN THE AFT MAIN CABI N FR 69-70 IAW AIRBUS A320 SRM 51-72-11-911-001 REMOVED DOT G9 W ORK ACCOMPLISHED IN
- [SDR CALA2020011300130](https://openairdocs.org/sdr/CALA2020011300130.md): Shear Web · corroded · Jan 11, 2020 · N492UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT CABIN SHEAR WEB FR 69-70 IS CORRODED - (SUPPORT TASK), AT HA ECO LCQ REF. NO. 9296176, GENERATED. REMOVED AND REPLACED SHEAR WEB P/N D5347112420200 INSTALL NEW SH EAR AT L/H SIDE FR 69-70 APPLIED TOP COAT AND CIC IAW A320 UAL S RM 51-72-11-911-001 AND 51-2
- [SDR CALA2019032500470](https://openairdocs.org/sdr/CALA2019032500470.md): Fmu · faulty · Mar 25, 2019 · N492UA · Airbus A320232 · Fuel Control/Turbine Engines
  > CREW REPORTS: AFTER A NORMAL FLEX T/O 800 FT IN CLIMB CREW THROTTLED BACK ENG 1 DID NOT RESPOND TO THE THROTTLE MOVEMENT STAYED AT T/O EPR. NEXT A ECAM WARNING TO SHUT DOWN ENGINE APPEARED & CREW ACP A NORMAL SHUT DOWN. THEY ALSO STATED THERE WAS NO VIBRATION,
- [SDR CALA2018012700357](https://openairdocs.org/sdr/CALA2018012700357.md): Unknown · odor · Jan 27, 2018 · N492UA · Airbus A320232 · Air Distribution System
  > SMELL OF BURNT TOAST AFT GALLEY REPORTED BY F/A VERIFIED BY CAPT INSPECTED ENTIRE AFT SECTION OF A/C AND FOUND NO OBVIOUS ODOR OF ELECTRICAL SMELL OR SMOKE INSPECTED LAV, COFFEE MAKERS WARMERS, OVENS ECT. ALSO RAN PACKS AND STILL NO OBVIOUS SMELLS NOTED AT TH
- [SDR CALA2017092203302](https://openairdocs.org/sdr/CALA2017092203302.md): Battery · discharged · Sep 22, 2017 · N492UA · Airbus A320232 · Emergency Lighting
  > EMERGENCY LIGHT TEST FAILED AT PTP PANEL. REPLACED BATTERY AT EPSU 12WL NOW OK TEST OK FOR SERVICE REF AMM 33-51-38 PB401.
- [SDR CALA2015100594565](https://openairdocs.org/sdr/CALA2015100594565.md): Apu · malfunctioned · Oct 2, 2015 · N492UA · Airbus A320232 · APU Core Engine
  > PACKS ON WITH APU, CABIN FILLED WITH SMOKE & APU AUTO SHUTDOWN. REPLACED APU IAW AMM 49-11-98-890-001-A.
- [SDR CALA2014101392397](https://openairdocs.org/sdr/CALA2014101392397.md): Spar · mechanic error · Oct 10, 2014 · N492UA · Airbus A320232 · Nacelle/Pylon, Frame/Spar/Rib
  > NUMBER 2 PYLON LOWER SPAR WEB MIS DRILLED DURING ACCOMPLISHMENT OF SRM 54-51-12. ACCOMPLISHED INSPECTION REQUIREMENTS IAW RDAS, SPAR HAS INTERIM REPAIR ACCOMPLISHED IAW ECRA 5450-02258. REPAIR HAS BEEN APPROVED AS INTERIM FOR 1 MONTH IAW RDAS 80003171-003-20
- [SDR CALA2014111092671](https://openairdocs.org/sdr/CALA2014111092671.md): Spar · mechanic error · Sep 15, 2014 · N492UA · Airbus A320232 · Nacelle/Pylon, Frame/Spar/Rib
  > NUMBER 2 PYLON LOWER SPAR WEB MIS-DRILLED DURING ACCOMPLISHMENT OF SRM 54-51-12. INTERIM REPAIR ACCOMPLISHED IAW ECRA 5450-02258. REPAIR HAS BEEN APPROVED AS INTERIM FOR 1 MONTH IAW RDAS 80003171-003-2014 DATED 9-10-14. A NEW RDAS THAT PROVIDES THE INSPECT
- [SDR CALA2014091892227](https://openairdocs.org/sdr/CALA2014091892227.md): Spar · mechanic error · Sep 13, 2014 · N492UA · Airbus A320232 · Nacelle/Pylon, Frame/Spar/Rib
  > NUMBER 2 PYLON LOWER SPAR WEB MIS-DRILLED DURING ACCOMPLISHMENT OF SRM 54-51-12. INTERIM REPAIR ACCOMPLISHED IAW ECRA 5450-02258. REPAIR APPROVED FOR 1 MONTH IAW RDAS 80003171-003-2014 DATED 9-10-14. A NEW RDAS THAT PROVIDES THE INSPECTION & THRESHOLD MUST
- [SDR CALA2014090992097](https://openairdocs.org/sdr/CALA2014090992097.md): Skin · damaged · Sep 6, 2014 · N492UA · Airbus A320232 · Elevator, Plate/Skin
  > LEFT ELEVATOR UPPER SURFACE HAD A 2.0 INCH BY 1.5 INCH AREA OF WATER INGRESS, 30 INCHES FROM THE OTBD END OF THE ELEVATOR & 13 INCHES FWD OF THE TE, ZONE 1. DAMAGE WAS R & R ACP IAW SRM 55-21-11 PARA 5 E FIG 205 CONFIG 1. REPAIR REQUIRES INSPECTION IAW SRI55
- [SDR CALA2014090392057](https://openairdocs.org/sdr/CALA2014090392057.md): Threshold · corroded · Aug 31, 2014 · N492UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > R2 DOOR THRESHOLD BEAM CORRODED AT FRAME 68 IN AFT CABIN. MATERIAL LOSS WAS 100% AT FRAME 68 NUTPLATE. OUT OF LIMITS IAW SRM 53-41-14 FIG 101. FABRICATED REPAIR ANGLE & FILLER & INSTALLED IAW SRM 53- 41-14 FIG 201 & MT.
- [SDR CALA2014091892239](https://openairdocs.org/sdr/CALA2014091892239.md): Stringer · corroded · Aug 30, 2014 · N492UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > STRINGER 41L IS CORRODED BETWEEN FRAME 63 - 64 IN AFT CARGO PIT. REMOVED DAMAGED SECTION. FABRICATED & INSTALLED STRINGER & REPAIR SPLICE IAW SRM 53-00-13 FIG 201. REPAIR REQUIRES SRI INSPECTIONS IAW SRI 53-00-13-2-001-00 TABLE 205. 1ST INSPECTION DUE AT 6
- [SDR CALA2014090392056](https://openairdocs.org/sdr/CALA2014090392056.md): Stringer · corroded · Aug 30, 2014 · N492UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > STRINGER 41L IS CORRODED BETWEEN FRAME 63 - 64 IN AFT CARGO PIT. REMOVED DAMAGED SECTION. FABRICATED & INSTALLED STRINGER & REPAIR SPLICE IAW SRM 53-00-13 FIG 201. REPAIR REQUIRES SRI INSPECTIONS IAW SRI 53-00-13-2-001-00 TABLE 205. 1ST INSPECTION DUE AT 6
- [SDR CALA2014090392055](https://openairdocs.org/sdr/CALA2014090392055.md): Stringer · corroded · Aug 30, 2014 · N492UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > STRINGER 42L IS CORRODED BETWEEN FRAME 63 - 64 IN AFT CARGO PIT. REMOVED DAMAGED PART. FABRICATED & INSTALLED NEW STRINGER & REPAIR SPLICE IAW SRM 53-00-13 FIG 201.
- [SDR CALA2014090392054](https://openairdocs.org/sdr/CALA2014090392054.md): Threshold · corroded · Aug 30, 2014 · N492UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > L2 DOOR THRESHOLD BEAM CORRODED AT FRAME 68 IN AFT CABIN. CORROSION AROUND 2 NUTPLATES WAS EXFOLIATED. CUT OUT DAMAGED PART & INSTALLED REPAIR PARTS IAW SRM 53-11-14 PG 203 PARA 5 FIG 201.
- [SDR CALA2013102992494](https://openairdocs.org/sdr/CALA2013102992494.md): Handset · intermittent · Oct 28, 2013 · N492UA · Airbus A320232 · Interphone/Passenger Announcement (PA) System
  > INTERPHONE IS INTERMITTENT AT DOOR 1L. CABIN INTERPHONE INTERMITTENT THROUGHOUT CABIN & FROM CABIN TO COCKPIT. REPLACED FWD HANDSET, OPERATIONS CHECKED OKAY.
- [SDR CALA2013102892419](https://openairdocs.org/sdr/CALA2013102892419.md): Valve · inoperative · Oct 27, 2013 · N492UA · Airbus A320232 · Fuel Storage
  > RT WING TANK REFUEL VLV INOPERATIVE.
- [SDR CALA2013102992460](https://openairdocs.org/sdr/CALA2013102992460.md): Hydraulic Line · leaking · Oct 26, 2013 · N492UA · Airbus A320232 · Hydraulic System, Main
  > EVIDENCE OF FLUID LEAK FROM VICINITY OF HYD SERVICE PANEL TO TAIL OF AIRCRAFT. BOTH LINES TO BRAKE VLV ON WW CEILING CENTERLINE LEAKING. TIGHTENED BOTH LINES NO LEAKS NOTED.
- [SDR CALA2013092791535](https://openairdocs.org/sdr/CALA2013092791535.md): Microphone · intermittent · Sep 27, 2013 · N492UA · Airbus A320232 · Communications System
  > FIRST OFFICER`S OXYGEN MASK COMMUNICATION IS INTERMITTENT. REPLACED MASK, OPERATIONS OKAY.
- [SDR CALA2013090991118](https://openairdocs.org/sdr/CALA2013090991118.md): Selector Valve · leaking · Sep 8, 2013 · N492UA · Airbus A320232 · Landing Gear Selector
  > OI-HYDRAULIC STREAMING FROM GEAR DOORS TO TAIL, RIGHTSIDE MOSTLY. LEAKING RT WW AFT WALL, AT INBD END OF VALVE NEAR ALLEN BOLTS MATING SURFACE. REPLACED AUTOMATIC SELECTOR 2576GM. PRESSURIZED SYSTEM LEAK CHECKED OK.
- [SDR CALA2013082690739](https://openairdocs.org/sdr/CALA2013082690739.md): Switch · loose · Aug 23, 2013 · N492UA · Airbus A320232 · Audio Integrating System
  > FIRST OFFICER`S SIDESTICK COMMUNICATIONS TRIGGER VERY LOOSE. RESECURED FIRST OFFICER`S PUSH TO TALK, OPERATIONS GOOD.
- [SDR CALA2013081990506](https://openairdocs.org/sdr/CALA2013081990506.md): Sensor · dirty · Aug 16, 2013 · N492UA · Airbus A320232 · Cabin Temperature Control System
  > COCKPIT TEMP CONTROL INOP COCKPIT TEMP AT 84 WITH ALL 3 SELECTORS AT FULL COLD. CLEANED COCKPIT TEMP SENSOR. GROUND AND SYS MCDU TEST OK.
- [SDR UALA2013071805036](https://openairdocs.org/sdr/UALA2013071805036.md): Container · open · Jul 17, 2013 · N492UA · Airbus A320232 · Passenger Oxygen System
  > OXYGEN PANEL OVER SEATS 21 ABC OPEN. SECURED EMERGENCY OXYGEN CONTAINER.
- [SDR UALA2013061904238](https://openairdocs.org/sdr/UALA2013061904238.md): Line · leaking · Jun 19, 2013 · N492UA · Airbus A320232 · Hydraulic System, Main
  > RIGHT MLG HYD LEAK. FOUND THE PRESSURE LINE LEAKING JUST ABOVE THE BRAKE SERVO VALVE. REPLACED LINE, LEAK CHECKED GOOD.
- [SDR UALA2013032902027](https://openairdocs.org/sdr/UALA2013032902027.md): Switch · faulty · Mar 28, 2013 · N492UA · Airbus A320232 · Audio Integrating System
  > F/O SIDE STICK PTT TRIGGER SENSATIVE TO LATERAL MOVEMENT. INCONSISTENT HOT MICS. REMOVED AND REPLACED F/O'S PTT SWITCH & OPS CHECK AS PER MM, OK FOR SERVICE.
- [SDR UALA2012112006701](https://openairdocs.org/sdr/UALA2012112006701.md): Starter · faulty · Nov 19, 2012 · N492UA · Airbus A320232 · Engine Starter
  > CREW REPORT: DURING ENGINE 2 START USING APU PNEU DUCT PRESSURE DROPPED BELOW 10PS AND WOULD NOT START. CREW TRIED A CROSSBLEED START WITH THE SAME RESULT DUCT PRESS DROPPED BELOW 10 PSI DURING START ATTEMPT. REPLACED STARTER PER MM, OPS CHECKED GOOD.
- [SDR UALA2012112006700](https://openairdocs.org/sdr/UALA2012112006700.md): Igniter · faulty · Nov 19, 2012 · N492UA · Airbus A320232 · APU Start/Ignition System
  > APU WILL NOT CRANK ON START - APU. STARTED APU, OPS OK. MCDU REPORTS, APU FAULT CONDITION: IGNITION UNIT (8030KM) AND FUEL CONTROL UNIT.(8022KM) NO PARTS SFO. APU SYSTEM SELF TEST FAULTS SPEED SNSR1 (8060KM1) NOT IN STOCK. SPEED SENSOR ATA: 49-71-13 AND IG
- [SDR UALA2012102606151](https://openairdocs.org/sdr/UALA2012102606151.md): Life Vest · unserviceable · Oct 26, 2012 · N492UA · Airbus A320232 · Life Jacket
  > NEED 8 TOTAL ADULT LIFE VESTS FOR THE MISSING DATE STICKER ON THE PULL STRAP. SIX ARE IN THE SPARE POUCH AND TWO AT SEATS 27D AND 27E. LIFE VESTS ARE NOT OUT OF DATE. REPLACED ALL 8 LIFE VESTS.
- [SDR UALA2012100905726](https://openairdocs.org/sdr/UALA2012100905726.md): Engine · leaking · Oct 9, 2012 · N492UA · Airbus A320232 · Engine (Turbine/Turboprop)
  > NR 1 ENGINE OIL LEAK AT TOWERSHAFT. MAINTENANCE REPORTS OIL LEAK UNDER NR 1 ENG, OPENED FAN COWLS AN DID VISUAL CHECK, APPEARS TO BE COMING FROM ACOC DRAIN PORT ON DRAIN MAST. THERE IS CURRENTLY NO RELIEF FOR LEAKS AT TOWER SHAFT AREA. REFERENCE MT71-017 FO

Next page: https://openairdocs.org/aircraft/N492UA/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 = 'N492UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N492UA/reports

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