# Service difficulty reports: N444UA

A list on [N444UA](https://openairdocs.org/aircraft/N444UA.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 · 130 reports

- [SDR CALA2026072117908](https://openairdocs.org/sdr/CALA2026072117908.md): Oxygen Mask · leaking · Jul 20, 2026 · N444UA · Airbus A320232 · Crew Oxygen System
  > OXYGEN MASK LEAKING. VERIFIED CAPTAINS OXYGEN MASK IS LEAKING AT A RAPID RATE & UNABLE TO STOP FLOW. SWAPPED CAPTAINS & 2ND OBSERVERS OXYGEN MASKS,, OPS CHKD GOOD, IAW AMM 35-12-41; DECLARING 2ND OBSERVERS SEAT INOPE DUE TO MASK. CONFIRMED NO LEAKS IN CURRE
- [SDR CALA2026042715735](https://openairdocs.org/sdr/CALA2026042715735.md): Valve · cracked · Apr 23, 2026 · N444UA · Airbus A320232 · Hydraulic System, Main
  > HYD Y RSVR LO LVL ECAMAFTER TAKEOFF DURING INSPECTION OF YELLOW HYDRAULIC SYSTEM FOUND CRACKED YELLOW PTU MANIFOLD. REMOVED AND REPLACED THE PTU SOLENOID VALVE (3012GL) REF AMM: 29-23-51-400-002-A. COMPLETED INSTALL UP TO AND INCLUDING STEP 4. B. OPS TEST STIL
- [SDR CALA2026032314760](https://openairdocs.org/sdr/CALA2026032314760.md): Lamp · inoperative · Mar 22, 2026 · N444UA · Airbus A320232 · Emergency Lighting
  > ROW 38 EMERGENCY PATHWAY LIGHTING INOPERATIVE. REPLACED THE LAMPS IAW AMM 33-51-38 PG. 601 AND TESTED IAW TASK 33-51-38-400-001-A. ALL EMERGENCY LIGHTS OPS CHECKED GOOD.
- [SDR CALA2025091708999](https://openairdocs.org/sdr/CALA2025091708999.md): Wire Harness · broken · Sep 16, 2025 · N444UA · Airbus A320232 · Light System Wiring
  > SEAT 24C SEAT TRIM BROKEN OFF. EMERGENCY LIGHT WIRING PULLED OUT. EMERGENCY LIGHT WIRING CONNECTOR PULLED OUT OF SEAT SIDE WIRING HARNESS. CAPPED AND STOWED SEAT SIDE EXPOSED WIRES. REPLACED SEAT TRIM REF AMM 25-21-41, REMOVED AND REPLACED SGL LIGHT FIXTURE
- [SDR CALA2025090308418](https://openairdocs.org/sdr/CALA2025090308418.md): Gauge · unknown · Aug 29, 2025 · N444UA · Airbus A320232 · Escape Slide
  > FA REPORT DOOR 2R SLIDE HAS SHIFTED AND MAKES PRESSURE GAUGE UNABLE TO BE SEEN. VERIFIED DOOR 2R SLIDE PRESSURE AS REQUIRED. OK FOR SERVICE PER AMM 52-13-00.
- [SDR CALA2025071806735](https://openairdocs.org/sdr/CALA2025071806735.md): Fuel Cap · missing · Jul 15, 2025 · N444UA · Airbus A320232 · Fuel Storage
  > FUEL CAP MISSING ON ARRIVAL. ACFT DOES NOT HAVE A FUEL CAP. NO DAMAGE AROUND COUPLING NOTED AT THIS TIME. INSTALLED UNDERWING FUEL CAP AS REQUIRED IAW AMM 28-25-41.
- [SDR CALA2025060905357](https://openairdocs.org/sdr/CALA2025060905357.md): Light · inoperative · Jun 3, 2025 · N444UA · Airbus A320232 · Emergency Lighting
  > PROCEDURE - ROW 25 ABC AISLE PATH EMERGENCY LIGHT INOP REMOVED AND REPLACED ISLE EMERGENCY LIGHT ASSY IAW AMM 33-51-19/401 CONFIG 00. OSP CHECK OK.
- [SDR CALA2025060405271](https://openairdocs.org/sdr/CALA2025060405271.md): Unknown · vibration · May 31, 2025 · N444UA · Airbus A320232 · Flight Control System
  > MODERATE LATERAL VIBRATION. STARTED AT 17000-F230. SPEED WAS APP ROX 300 KTS CI 40..SLOWED TO FOUND YELLOW AN GREEN HYD QTY LOW, SERVICED BOTH SYS TO FULL IAW AMM 12-12-29-611-001-A, PREFORMED VISUAL INSP OF ACFT FOR HYD LEAKS NONE FOUND, VERIFIED NO OSCILLATI
- [SDR CALA2025040203443](https://openairdocs.org/sdr/CALA2025040203443.md): Slide · unknown · Mar 29, 2025 · N444UA · Airbus A320232 · Escape Slide
  > FORWARD DOOR ESCAPE SLIDE REMOVE {A3NB-25-3-0020} - L1 DOOR SLIDE REQS REPLACEMENT R/R L1 DOOR ESCAPE SLIDE IAW AMM 25-62-44. CIDS TEST GOOD.
- [SDR CALA2025032503170](https://openairdocs.org/sdr/CALA2025032503170.md): Bleed Air Sys · fluctuates · Mar 23, 2025 · N444UA · Airbus A320232 · Engine Bleed Air System
  > DURING CLIMB AND CRUISE, LT BLEED CYCLING 8-48 PSI AT LVL FLT CABIN RATE CYCLING +/-500FPM. SEE LOG PAGE 4268613 FOR FIX. BLEED AND CABIN ALT CHECKS GOOD.
- [SDR CALA2024112901347](https://openairdocs.org/sdr/CALA2024112901347.md): Cap · missing · Nov 27, 2024 · N444UA · Airbus A320232 · Fuel Storage
  > PDA 2 FOUND FUEL CAP MISSING REF L/P 9916063. INSTALLED NEW CAP REF L/P 9916063 FUEL CAP LANYARD BROKEN. NEEDS CALBE ASSY, CAP USABLE AND INSTALLED. PLACED ON CDL. APPLIED CDL. DISPATCH DESK: 03 NAME: DATE: 19-NOV-24- OKAY TO DEFER FUEL CAP LANYARD PER CDL 28
- [SDR CALA2024112001201](https://openairdocs.org/sdr/CALA2024112001201.md): Battery · no test · Nov 17, 2024 · N444UA · Airbus A320232 · Emergency Lighting
  > OPERATIONAL CHECK OF CABIN EMERGENCY LIGHTS {A3NB-33-3-6012} - EPSU BATTERY AFT L MESSAGE REF TSM 33-51-00-810-802-A, AFT LEFT EPSU 13WL SHOWS BATTERY FAULT. R/R EPSU BATTERY REF AMM 33-51-38, OPS CHECK OK PARTS USED: 18-3351-3-0001,QTY:1
- [SDR CALA2024031200696](https://openairdocs.org/sdr/CALA2024031200696.md): Fuel Cap · missing · Mar 9, 2024 · N444UA · Airbus A320232 · Fuel Storage
  > FUEL CAP MISSING REPORTED BY FUELER. ON INSTALLATION OF NEW REFUEL CAP, NOTED ELEMENT ASSY NOT ORIENTED PROPERLY CAUSING CAP TO LOCK FACING OUTBOARD OR 45 DEGREES INBOARD IAW AMM 28-25-41-000-005-A. ACCOMPLISHED SCEPTRE -9. REPLACED WITH SERVICIABLE FUEL C
- [SDR CALA2024012900254](https://openairdocs.org/sdr/CALA2024012900254.md): Brake Sys · overtemp · Jan 26, 2024 · N444UA · Airbus A320232 · Landing Gear Brake System
  > CREW REPORT LOW SPEED ABORT LESS THAN 50 KTS. AFTER STOPPING BRAKE TEMPS READING 285(1) 260(2) 325(3) 320(4) BRAKES HOT MESSAGE DISPLAYED. AFTER APPROXIMATELY 30 MINUTES MESSAGE CLEARED ALL BRAKE TEMP INDICATIONS NORMAL. TEMPS DID NOT EXCEED OVERHEAT THRESHOLD
- [SDR CALA2024012900247](https://openairdocs.org/sdr/CALA2024012900247.md): Fan · inoperative · Jan 25, 2024 · N444UA · Airbus A320232 · Air Distribution Fan
  > FWD CAB RECIRCULATION FAN INOP. AMBER FAN ON COND PAGE. REMOVED AND REPLACED RH RECIRCULATION FAN, OPS CHECK GOOD.
- [SDR CALA2023120103532](https://openairdocs.org/sdr/CALA2023120103532.md): Fuel Cap · missing · Nov 17, 2023 · N444UA · Airbus A320232 · Fuel Storage
  > DURING WALK AROUND FOUND MISSING FUEL CAP NEEDS INSTALL FUEL CAP, NO PARTS AT MEXJL, NO LEAKS NOTED OK TO DEFER AS PER 28A. INSTALLED NEW FUEL CAP TO UNDERWING REF MM 28-25-41. NO LEAK NOTED. REMOVED STICKER FROM FD.
- [SDR CALA2023090602726](https://openairdocs.org/sdr/CALA2023090602726.md): Skin · dented · Sep 5, 2023 · N444UA · Airbus A320232 · Passenger/Crew Doors
  > CARTERING REPORTED CANNOT CLOSE DOOR 2L SRM 52-00-00-283-002 EVALUATED DAMAGE DIMENSIONS LENGTH 1.1 X WIDTH.5 X DEPTH.015 ALLOWED TO CONTINUE FLIGHT REPAIR AT 200 FLIGHT CYCLES AS PER DIP 52-DIP UPDATE DENT LOCATION. REFER TO SRM 52-10-00-283-002 FOR ALLOWA
- [SDR CALA2023020800369](https://openairdocs.org/sdr/CALA2023020800369.md): Fuel Cap · missing · Feb 8, 2023 · N444UA · Airbus A320232 · Aircraft Fuel Distribution System
  > PDA 2 UPON ARRIVAL FUELER REPORT MISSING FUEL CAP. INSTALLED FUEL CAP.
- [SDR CALA2022120203267](https://openairdocs.org/sdr/CALA2022120203267.md): Controller · faulted · Dec 2, 2022 · N444UA · Airbus A320232 · Cabin Cooling System
  > ECAM AIR PACK 2 OVRHTAT CRUZ FL360...FOLLOWED ECAM-TURNED PACK O FF REF L/P''S 3200835 AND 3174149 FOR REPAIR. PER LP 3200835 REMOVE AND REPLACE PACK 2 TEMP CONTROLLER, IAW AMM. PER LP 3174149 RPL''D AFT CABIN TRIM AIR VALVE PER AMM
- [SDR CALA2022112503232](https://openairdocs.org/sdr/CALA2022112503232.md): Accumulator · leaking · Nov 25, 2022 · N444UA · Airbus A320232 · Hydraulic Power Accumulator, Main
  > HYD G RSVR LO LVL IN CRUSE FL380ECAM COMPLETE FOUND GREEN POWER ACCUMULATOR LEAKING AT UPPER CONNECTION. COMPLETED INSTALLATION OF GREEN SYSTEM ACCUMULATOR. LEAK CHECK STARTED REMOVAL OF ACCUMULATOR PER AMM 29-11-42-000-001-A UP OK. GEAR DOORS WILL NOT CLOSE
- [SDR CALA2021120802291](https://openairdocs.org/sdr/CALA2021120802291.md): Plate · none · Dec 7, 2021 · N444UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > REFERENCE LP 7553624 PALNNING TO CONTACT ENGINEERING AFTER 22APR 22 BUT BEFORE 01MAY22 FOR THE ECRA 5330-06890 PART 3- PERMANENT REPAIR REFERENCE LP 7553624 PLANNING TO CONTACT ENGINEERING AFTER 22APR 22 BUT BEFORE 01MAY22 FOR THE ECRA 5330-06890 PART 3- PERMA
- [SDR CALA2021120802290](https://openairdocs.org/sdr/CALA2021120802290.md): Plate · cracked · Dec 7, 2021 · N444UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > FRAME 36 PRESSURE PANEL HOLES 1, 2, 3, 4, 5, 6, 7 AND 8 BETWEEN Y1523 AND Y1292. PRESSURE PANEL HOLES 13, 14, 15, 16, 17, 19, 21, 22, 24, 25 AND 28 BETWEEN Y1292 AND Y765 HAVE CRACK INDICATION S ON THE PRESSURE PANEL. L23423 & ECRA 5330-05216 OP002 WITH NO DE
- [SDR CALA2021120602245](https://openairdocs.org/sdr/CALA2021120602245.md): Plate · cracked · Dec 3, 2021 · N444UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > FRAME 36 PRESSURE PANEL HOLES 102,103,106 AND 120 BETWEEN Y765 A ND Y1292 HAVE CRAC INDICATIONS IN THE PRESSURE PANEL. A3NB-53-4- 6324; AD2019-23-01 PER HAECO LCQ N/R 9297008/31008 GENERATED BY V061633. ECRA 5331-02786 & REO-L23431 REV I & ECRA 5330-05216 OP00
- [SDR CALA2021112902177](https://openairdocs.org/sdr/CALA2021112902177.md): Fitting · cracked · Nov 27, 2021 · N444UA · Airbus A320232 · Fuselage Structure (General)
  > LT MLG DOOR ACTUATOR FITTING HAS CRACK INDICATION IN FWD OB HOLE (IN ACT FITTING LAYER) AD RELATED SUPPORT TASK: PER HAECO LCQ N/ R 9296413/30413 GENERATED BY V892444. ACCOMPLISHED REPAIR LT MLG DOOR ACTUATOR FITTING IAW ECRA 5330-0 6886/REO-L23354 REV 1R. REQ
- [SDR CALA2021112302164](https://openairdocs.org/sdr/CALA2021112302164.md): Joint · corroded · Nov 23, 2021 · N444UA · Airbus A320232 · Fuselage Structure (General)
  > AFT VARGO COMPT BILGE AREA EXISTING STRINGER REPAIR AT FRAME 55- 56 STR 43LH HAS CORRISION. TABLE 008. REPAIRED AFT CARGO STRINGER SPLICE AT FRAME 55-56 STR 43 LH IAW A320 SRM 53-00-13-300-001. INSPECTION THERSHOLD FROM TIME OF ADL /REPAIR EMBODIMENT 60,000FC/
- [SDR CALA2021111102086](https://openairdocs.org/sdr/CALA2021111102086.md): Handle · contaminated · Nov 10, 2021 · N444UA · Airbus A320232 · Landing Gear Actuator
  > LANDING GEAR FREE FALL HANDLE WILL NOT UNLOCK TO DROP GEAR A3NB- 32-3-6063 PER HAECO LCQ NR 9297125/31125 GENERATED BY V039736. UPON EVALUATION, CLEANED FREEFALL HANDLE AND ATTACHED COMPONENTS REMOVED DIRT AND OLD GREASE (HANDLE WORKS SMOOTHLY) IAW A320 AMM 12
- [SDR CALA2021102901993](https://openairdocs.org/sdr/CALA2021102901993.md): Skin · corroded · Oct 28, 2021 · N444UA · Airbus A320232 · Fuselage Main, Frame
  > CORROSION ON FUSELAGE INTERNAL SIDE OF THE SKIN PANEL JUST BEFOR E FR 20 AT STRINGER 28R. ACCOMPLISHED REPAIR AT FUSELAGE INTERNAL SIDE OF THE SKIN PANEL JUST BEFORE FR 20 AT STRG 28R IAW ECRA 5311-02682. ALL WORK ACCO MPLISHED ON HAECO NR 9296298.
- [SDR CALA2021102901992](https://openairdocs.org/sdr/CALA2021102901992.md): Bracket · corroded · Oct 27, 2021 · N444UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT FR56 STR41L-40L CLEAT HAS CORROSION. (A3NB-53-4-6179) PER NR 929707 (31075) GENERATED BY V039746 AT HAECO LCQ. REMOVED AND REPLACED FR56 BETWEEN ST 40L - 41L CLIP IAW A320 SRM 51-72-11-911-001. PERFORMED BY V061619 INSP BY V892443.
- [SDR CALA2021102601984](https://openairdocs.org/sdr/CALA2021102601984.md): Frame · corroded · Oct 26, 2021 · N444UA · Airbus A320232 · Fuselage Main, Attach Fittings
  > FR 69-70 BETWEEN STGR 2L-2R HAS SURFACE CORROSION ON FUSELAGE CR OWN SKIN,WHERE (2EA) COAX CABLES PASS THROUGH. BEFORE THE AIRCRAFT REACHES 113,200 TOTAL AIRCRAFT FLIGHT CYCLES ALL WORK ACCOMPLISHED ON HAECO NR 9296415. ACCOMPLISHED INTERIM REPAIR AT FR 69-70
- [SDR CALA2021102501966](https://openairdocs.org/sdr/CALA2021102501966.md): None · corroded · Oct 24, 2021 · N444UA · Airbus A320232 · Fuselage Structure (General)
  > AFT CARGO COMPT BILGE AREA EXISTING STRINGER REPAIR AT FRAME 58- 59 STR 43LH HAS CORROSION. PER HAECO LCQ NR 9296565/30565 GENERA TED BY V061595 REPAIRED AFT CARGO STRINGER SPLICE AT FR 58-59 STR 43L/H IAW 320 CORRECTING DIP LIMITS TO THE FOLLOWING 60,000FC /
- [SDR CALA2021102501965](https://openairdocs.org/sdr/CALA2021102501965.md): Skin · corroded · Oct 24, 2021 · N444UA · Airbus A320232 · Fuselage Main, Attach Fittings
  > FR 69-70 BETWEEN STGR 2L-2R HAS SURFACE CORROSION ON FUSELAGE CR OWN SKIN,WHERE (2EA) COAX CABLES PASS THROUGH. BEFORE THE AIRCRAFT REACHES 113,200 TOTAL AIRCRAFT FLIGHT CYCLES ALL WORK ACCOMPLISHED ON HAECO NR 9296415. ACCOMPLISHED INTERIM REPAIR AT FR 69-70
- [SDR CALA2021102501964](https://openairdocs.org/sdr/CALA2021102501964.md): None · corroded · Oct 24, 2021 · N444UA · Airbus A320232 · Fuselage Structure (General)
  > AFT CARGO COMPT BILGE AREA EXISTING STRINGER REPAIR AT FRAME 56- 57 STR 41LH HAS CORROSION. REPAIR EMBODIMENT IAW SRI 53-00-13-205-001 TABLE 006.ALL WORK AC COMPLISHED ON HAECO NR 9296564. REMOVED AND REPLACED STRINGER REPAIR DOUBLER IN AFT CARGO AREA F R 56-5
- [SDR CALA2021100401769](https://openairdocs.org/sdr/CALA2021100401769.md): Beam · corroded · Oct 2, 2021 · N444UA · Airbus A320232 · Fuselage Main, Floor Beam
  > PER NR 9296437/30437. CABIN FLOOR STRUCTURE HAS CORROSION ON R2 DOOR SILL IN SEVERAL PLACES. GENERATED BY V892443 REMOVED AND REPLACED AFT CABINR2 DOOR SILL BEAM FR66-68 STR23R I AW A320 SRM 51-72-11-911-001. MECH V061619 INSP BY V892443
- [SDR CALA2021100101743](https://openairdocs.org/sdr/CALA2021100101743.md): None · corroded · Sep 30, 2021 · N444UA · Airbus A320232 · Fuselage Structure (General)
  > AFT CABIN, R/H SIDE BETWEEN FR69-70 FRAME SUPPORT HAS HEAVY CORR OSION ON UPPER AND LOWER SURFACES IN SEVERA AND IS RUNNING UNDER SHEAR PLATE PER 9296979 / 30979 GEN V913126 REMOVED AND REPLACED FR69-70 FRAME SUPPORT STR23R IAW A320 SRM 5 1-72-11-911-001 BY ME
- [SDR CALA2021100101739](https://openairdocs.org/sdr/CALA2021100101739.md): Plate · corroded · Sep 30, 2021 · N444UA · Airbus A320232 · Fuselage Structure (General)
  > R/H SHEAR PLATE FR69-70 CORRODED WITH 100% MATERIAL LOSS AROUND FASTENER HOLE PER NR 9296982 / 30982 GEN BY V061619 REMOVED AND REPLACED R/H FR69-70 STR23R SHEAR PLATE IAW A320 SRM 51-72-11-911-001 BY MECH V915153 INSP BY V901665
- [SDR CALA2021092001616](https://openairdocs.org/sdr/CALA2021092001616.md): Support · corroded · Sep 20, 2021 · N444UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > PER NR 9296437/30437. CABIN FLOOR STRUCTURE HAS CORROSION ON R2 DOOR SILL IN SEVERAL PLACES. GENERATED BY V892443 REMOVED AND REPLACED AFT CABINR2 DOOR SILL BEAM FR66-68 STR23R I AW A320 SRM 51-72-11-911-001. MECH V061619 INSP BY V892443
- [SDR CALA2021092001608](https://openairdocs.org/sdr/CALA2021092001608.md): Fitting · corroded · Sep 19, 2021 · N444UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > CABIN FLOOR STRUCTURE HAS CORROSION ON R2 DOOR SILL FWD CORNER F ITTING. REMOVED AND REPLACED R2 DOOR FWD CARNER FITTING AT FR66 ST23R IA W A320 SRM 51-42-11-001 REMOVED AND REPLACED R2 DOOR FWD CORNER FITTING AT FR66 ST 23R I AW A320 SRM 51-42-11-001
- [SDR CALA2021092001604](https://openairdocs.org/sdr/CALA2021092001604.md): Fitting · corroded · Sep 18, 2021 · N444UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > CABIN FLOOR STRUCTURE HAS CORROSION ON R2 DOOR SILL AFT CORNER F ITTING. PER HAECO LCQ NR 9296438/30438 GENERATED BY V892443 REMOVED & REPLACED R2 DOOR AFT CORNER FITTING AT FR68 ST 23R IAW A320 SRM 51-42-11-001 REMOVED AND REPLACED R2 DOOR CORNER FITTING AT F
- [SDR CALA2021090801526](https://openairdocs.org/sdr/CALA2021090801526.md): Panel · corroded · Sep 7, 2021 · N444UA · Airbus A320232 · Fuselage Main, Structure
  > CABIN FLOOR STRUCTURE LH AFT SHEAR PLATE HAS CORROSION AT FR70 A 3NB-53-3-6222 PER HAECO LCQ N/R 9296447/30447. C/W REMOVED AND REPLACED LH AFT SHEAR PLATE FR70 IAW A320 SRM 51 -72-11-911-001.
- [SDR CALA2021090801525](https://openairdocs.org/sdr/CALA2021090801525.md): Support Angle · corroded · Sep 7, 2021 · N444UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > L/H AFT CABIN FR69-70 SHEAR PLATE SUPPORT ANGLE HAS EXFOLIATE CO RROSION SUPPORT TASK PER HAECO LCQ N/R 9296848/30848. REMOVED AND REPLACED LH FR 69-70 SHEAR PLATE SUPPORT BEAM IAW A3 20 SRM 51-72-11-911-001.
- [SDR CALA2019082601440](https://openairdocs.org/sdr/CALA2019082601440.md): Door Frame · cracked · Aug 26, 2019 · N444UA · Airbus A320232 · Fuselage Main, Structure
  > LEFT FRAME 16 DOOR STOP NR 1, HOLE NR 3 CRACKED IN FRAME AT THE 3:00 POSITION. DOOR STOP FITTING NR 1 HOLE 3 REPAIRED IAW ECRA 5311-02236 PART 1.
- [SDR CALA2019083001443](https://openairdocs.org/sdr/CALA2019083001443.md): Skin · dented · Aug 22, 2019 · N444UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > FUSELAGE TAIL SECTION, R/H SIDE EXTERIOR SKIN, BETWEEN FR 74-75 STRG HAS DENT (A3NB-05-3-6062) AT HAECO LCQ REF. NO. 9290272 (44 272). GENERATED BY V917055. DENT LOCATED AT FUSELAGE SKIN BETWEEN FR74-75 AND BETWEEN S31R A ND S32R. DENT MEASURES 1.0" X.5" OUT
- [SDR CALA2017080802496](https://openairdocs.org/sdr/CALA2017080802496.md): Power Supply · faulty · Aug 8, 2017 · N444UA · Airbus A320232 · Emergency Lighting
  > 23WL1 AND 11WL EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED POWER SUPPLIES 10WL AND 11WL. OPS TESTED OK IAW AMM 33-51-38.
- [SDR CALA2017050801292](https://openairdocs.org/sdr/CALA2017050801292.md): Connector · dirty · May 8, 2017 · N444UA · Airbus A320232 · Hydraulic Power System Wiring
  > Y RSVR LO LVL MESSAGE INOPERATIVE, HYD. EMERGENCY DECLARED. ACCOMPLISHED TROUBLESHOOTING OF YELLOW HYD SYSTEM FOR LOSS OF PRESSURE AND QUANTITY IAW TSM52-36-00-810-805-A, 29-13-00-810-801 & 29-13-00- 810-805A. UNABLE TO GENERATE OR DUPLICATE ERROR. CLEANED
- [SDR CALA2017032400701](https://openairdocs.org/sdr/CALA2017032400701.md): Power Supply · faulty · Mar 24, 2017 · N444UA · Airbus A320232 · Emergency Lighting
  > GETTING L EPSU MESSAGE. REMOVED AND REPLACED EPSU IAW MM 33-51-38 EMER LIGHTS TEST OK ON CIDS BITE PANEL.
- [SDR CALA2017021000313](https://openairdocs.org/sdr/CALA2017021000313.md): Concentrator · faulty · Feb 10, 2017 · N444UA · Airbus A320232 · Central Warning
  > B ELEC PUMP LO PR DISPLAYED ON UPPER ECAM SCREEN. EMERGENCY DECLARED. RANG OUT PSI SWITCH CIRCUIT REF WD29-12-01PG1 2074GJ. CIRCUIT CHECKS OUT GOOD. REPLACED SDAC2 PER MM31-55-34-400-001-A PERFORMED OP TEST OF SDAC PER AMM TASK 31-50-00-710-003-A TEST OK. PERF
- [SDR CALA2015070994073](https://openairdocs.org/sdr/CALA2015070994073.md): Epsu · faulty · Jul 8, 2015 · N444UA · Airbus A320232 · Emergency Lighting
  > EMERGENCY POWER SUPPLY UNIT INTERIOR LOAD AFT LT, MSG FOUND DURING 2 SVC. R & R AFT LT EPSU IAW AMM 33-51-38-400-001-A, CHECKED OK.
- [SDR CALA2015051593782](https://openairdocs.org/sdr/CALA2015051593782.md): Engine · shutdown · May 13, 2015 · N444UA · Airbus A320232 · Engine (Turbine/Turboprop)
  > AT CRUISE ALTITUDE, ENG 1 UNCOMMANDED SHUTDOWN WITH ENG 1 FAIL ECAM. FOLLOWED FM PROCEDURE & SELECTED ENG 1 MASTER SWITCH TO OFF. DID NOT FEEL OR HEAR COMPRESSOR STALL. REPLACED ENG IAW AMM M T71-017.
- [SDR CALA2015012393020](https://openairdocs.org/sdr/CALA2015012393020.md): Charger · inoperative · Jan 21, 2015 · N444UA · Airbus A320232 · Emergency Lighting
  > D1L EMER EXIT LIGHT CHARGER INOPERATIVE, CICS. CHANGED CHARGER & BATTERY IAW MM33-51-38-401. OPERATIONS CHECKED GOOD.
- [SDR CALA2014041090796](https://openairdocs.org/sdr/CALA2014041090796.md): Sill · corroded · Apr 10, 2014 · N444UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > R2 DOOR SILL IS CORRODED ON FWD GIRT BAR PLATE & AT AFT AREA. DOOR SILL WAS WORN OUT OF LIMITS IAW SRM 53-41-11. R & R R2 DOOR SILL IAW SRM 51-42-11 PGS 1, 7 & 25.

Next page: https://openairdocs.org/aircraft/N444UA/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 = 'N444UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N444UA/reports

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