Registered owner
United Airlines Inc
Location
Chicago, IL
Owner type
Corporation
Serial number
2435
Year built
2005
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Standard, transport
Airworthiness date
September 27, 2019
Certificate issued
August 21, 2026
Expires
August 31, 2033
Mode S code
AC234F

From the FAA registry file of October 24, 2026.

On this page

Airworthiness directives that may apply · 301

Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.

1997In forceSuperseded2026
ADs by the year they took effect: 449 ADs
19971
19982
19998
200015
20017
200211
20036
200422
200513
200614
200713
200811
200911
20107
201111
201212
201314
201417
201521
201620
201723
201827
201920
202029
202120
202222
202317
202414
202524
202617
See all 449 ADs

Information bulletins that may apply · 7

Advisory, not mandatory.

NTSB investigations

No NTSB investigations matched to N881UAMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Airbus A319-132 aircraft

FAA incident reports

No FAA accident or incident reports matched to N881UAMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Airbus A319-132 aircraft

Service difficulty reports · 15

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

SDR CALA2026010512663Lug · wornLEFT ELEVATOR, INBD ACTUATOR LOCKING LUG WORN. EVALUATED DAMAGE ON LOCKING LUG LT ELEVATOR INB ACTUATOR FOUND TO BE OUT OF LIMITS IAW SRM 55-26-47-300-001. FABRICATED A REPAIR ANGLE IAW SRM 51-27-11-911-001. INSTALLED IAW SRM 55-26-47-300-001.Jan 2, 2026 · N881UA · Airbus A319132 · Elevator StructureSDR CALA2026010512662Lug · wornLEFT ELEVATOR OTBD ACTUATOR LOCKING LUG WORN. EVALUATED DAMAGE ON LOCKING LUG LT ELEVATOR OTBD ACTUATOR FOUN D TO BE OUT OF LIMITS IAW SRM 55-26-47-300-001. FABRICATED REPAIR ANGLE IAW SRM 51-27-11-911-001, INSTALLED IAW SRM 55-26-47-300-001.Jan 2, 2026 · N881UA · Airbus A319132 · Elevator StructureSDR CALA2025090508493Wire · brokenFLOOR PROXIMITY EMERGENCY LIGHT AT ROW 35 ABC INOPERATIVE. REPLACED THE LAMP, OPS CHECK FAIL ROW 34, SUSPECT HARNESS UNDER SEAT. FOUND BROKEN WIRE. SPLICED WIRE AND LIGHTS CHECKED GOOD. IAW ESPM 20-43-10Sep 3, 2025 · N881UA · Airbus A319132 · Light System WiringSDR CALA2025040403519Light · malfunctionedEMER EXIT LIGHTS ON SHORT FINAL FOR UNKNOWN REAS ON. PERFORMED RESET AND OPS TEST REF AMM 33-51-00 OPS CHECK GOOD AT THIS TIMEApr 2, 2025 · N881UA · Airbus A319132 · Emergency LightingSDR CALA2025020202164Unknown · odorVERY STRONG FUEL ODOR ENTIRE CABIN AND FLT DECK AFTER SHUTDOWN AT GATE DEBRIEF CREW PILOT SAID THE STRONG FUEL SMELL/ODOR IN THE FLIGHT DECK AND BACK OF THE CABIN THE ODOR LASTED FOR AT LEAST FIVE MINUTES 5 DURING SHORT DOWM AT THE GATE, HE SAID TAXI WAS NORMAJan 30, 2025 · N881UA · Airbus A319132 · Air Distribution SystemSDR CALA2024092300670Brake Assy · faultedBRAKES SYSTEM 2 FAULT MESSAGE ON ECAM. PFR INDICATE 9GG BSCU 2.... REF LOGPAGE 9306044 FOR EMERGENCY BRAKING INSPECTION. PERFORMED NORMAL BRAKING TEST, NO FAULTS DETECTED FOR BSCU 1 OR 2 REF AMM 32-42-00-710-001-A. ALSO PERFORMED ALTERNATIVE BRAKING TEST, ALLSep 19, 2024 · N881UA · Airbus A319132 · Landing Gear Brake SystemSDR CALA2024040800996Fuel Cap · missingPDA 2 UPON ARRIVAL FOUND FUEL CAP MISSING. INSTALLED NEW FUEL CAP.Apr 6, 2024 · N881UA · Airbus A319132 · Fuel StorageSDR CALA2024010500045Frame · damagedRH FRAME 16 DOUBLE JOGGLE FASTENER HOLES DAMAGE INDICATIONS AT HOLE 1 AND 2 FRAME SIDE. HOLE 3 SKIN SIDE, HOLE 11 AND 12 SKIN SIDE AND HOLE 18 FRAME SIDE. RH FR16 DOUBLE JOGGLE FASTENERS HOLES DAMAGED, REPAIRED IAW EC/R A # 5311-03136. EMP: V933868 WC: 82813 SJan 4, 2024 · N881UA · Airbus A319132 · Fuselage Main, FrameSDR CALA2024010400026Frame · corrodedAPU EXHAUST TAIL CONE PANEL MOUNTING STRUCTURE HAS CORROSION. REMOVED AND REPLACEMENT LOWER SECTION FR86 IAW SRM 51-72-11 AND SRM 51-42-11 REMOVED AND RE-INSTALLED APU EXHAUST MUFFLER FOR ACCESS IAW AMM TASKS 49-81-41-000-002-A AND 49-81-41-400-003-A.Dec 29, 2023 · N881UA · Airbus A319132 · Fuselage Main, FrameSDR CALA2024010400022Frame · crackedCRACK IN UPPER TACK HOLE ON FR59 LH BETWEEN STR 33LH AND 34LH. TRANSCRIBED FROM MAE NR 82785. ACCOMPLISHED INTERIM REPAIR PER INSTRUCTIONS IN ECRA 5340-02178 PART 1 WITH NO DEVIATIONS.Dec 29, 2023 · N881UA · Airbus A319132 · Fuselage Main, FrameSDR CALA2023012500195Fitting · damagedL/H MLG JACK ANCHORAGE FITTING WITH POTENTIAL ADDITIONAL INSPECTION REQUIRED ACCOMPLISH A PERMA ON OR BEFORE 18JULY2023 NENT REPAIR PER PART 3 OF THE LATEST REVISION OF ECRA 5726-01104 LH MLG JACK ANCHORAGE FITTING WAS REPLACED + INNER REAR SPAR WAS REOAIRED AJan 23, 2023 · N881UA · Airbus A319132 · Wing, Landing Gear Attach FittingsSDR CALA2022100302651Lanyard · missingPDA 3 FUELER REPORTED FUEL CAP LANYARD IS MISSING .REMOVED AND REPLACED FUEL COUPLING CAP LANYARD.Oct 3, 2022 · N881UA · Airbus A319132 · Aircraft Fuel SystemSDR CALA2022010300005Frame · crackedL/H FR68 DOOR STOP #1 LOWER I/B HOLE HAS A CRACK INDICATION SUPP ORT TASK: AD 2018-03-12. PER HAECO LCQ N/R 9294109/ 32109 GENERA TED BY V061632. "B", REAMED TO .506" INSTALLED FREEZE PLUG REAMED TO .281"BOLT S CTION THRESHOLD FROM THE TIME OF ADL/REPAIR EMBODDec 31, 2021 · N881UA · Airbus A319132 · Fuselage Main, FrameSDR CALA2022010300004Stringer · corrodedCORROSION ON STRINGER 43R AT FR60 AFT CARGO PIT GENERATED BY V89 2443 ON HAECO LCQ NR 9294225/32225 REMOVED AND REPLACED STRINGER 43R FR60-64 IAW A319 SRM 51-72-11- 911-001 AND SRM 51-42-11 THIS IS A CATEGORY A REPAIR ESFR #10273 30. BY MECH V077956 INSP BY V8Dec 31, 2021 · N881UA · Airbus A300* · Fuselage Structure (General)SDR CALA2021122902475Frame · crackedR/H FR68 DOOR STOP #1 LOWER I/B HOLE HAS A CRACK INDICATION- SUP PORT TASK: AD 2018-03-12. PER HAECO LCQ NR 9294110/32110 GENERAT ED BY V061632.Dec 29, 2021 · N881UA · Airbus A300* · Fuselage Main, Frame

STCs that may be installed · 212

Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.

See all 212 STCs