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Airbus A350-1000 in flight
NEW-GENERATION LONG-RANGE WIDEBODY

A350

The Airbus A350 is a long-range twin-engine widebody family built around composite structure, advanced aerodynamics, integrated avionics and Rolls-Royce Trent XWB powerplants.

Airbus A350-1000 · © Airbus 2018, S. Ramadier
AIRCRAFT FACTS

A350 at a glance

Source-labelled facts can be updated from the aircraft-family administration page.

LOLaunch operatorQatar Airways

Launch customer and first commercial operator.

OPOperators worldwide41

Operator count shown by Airbus on the A350 family product page.

ENEngine familyRolls-Royce Trent XWB

Trent XWB-84 powers the A350-900 and Trent XWB-97 powers the A350-1000.

SAHull-loss accidents1

ASN lists one A350-900 write-off and no A350-1000 write-off at the review date.

AIRCRAFT OVERVIEW

About A350

The A350 family was developed as Airbus’s clean-sheet long-range widebody platform. Its architecture combines a carbon-fibre-intensive airframe, high-aspect-ratio wings, integrated modular avionics and the Rolls-Royce Trent XWB engine family.

For maintainers and learners, the A350 is especially valuable because its aircraft systems demonstrate modern distributed control, extensive data-network integration, centralized maintenance functions and strong cross-system dependencies. This hub connects those aircraft-level ideas to TechOpsBase ATA resources, learning paths, creator videos and community discussions.

MODEL STRUCTURE

Variants, engines and applicability

Directory context only. Confirm the exact variant, engine, modification state and effectivity with current approved aircraft data.

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ACTIVEProfile being developed

A350-900

Open variant profile →
first flight entry to service Variant profile being developed profile state
INDEXED ENGINE OPTIONS
Rolls-Royce Trent XWB
Applicability context

Confirm the exact model code, installed engine, modification state, equipment configuration and approved effectivity before applying technical information to an aircraft.

ACTIVEProfile being developed

A350-900ULR

Open variant profile →
first flight entry to service Variant profile being developed profile state
INDEXED ENGINE OPTIONS
Rolls-Royce Trent XWB
Applicability context

Confirm the exact model code, installed engine, modification state, equipment configuration and approved effectivity before applying technical information to an aircraft.

ACTIVEProfile being developed

A350-1000

Open variant profile →
first flight entry to service Variant profile being developed profile state
INDEXED ENGINE OPTIONS
Rolls-Royce Trent XWB
Applicability context

Confirm the exact model code, installed engine, modification state, equipment configuration and approved effectivity before applying technical information to an aircraft.

Compare up to three variants.Use the comparison for orientation only—not maintenance effectivity.
QUICK REFERENCE

Fast revision for A350

Short, source-grounded memory refreshers. These complement the deeper resources and never replace approved maintenance data.

All Quick Reference notes →
No published Quick Reference note is mapped to this aircraft yet.
WATCH AND LEARN

A350 video learning

Published creator videos mapped to this aircraft family appear here automatically. ATA-mapped videos keep their system context.

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KNOWLEDGE BASE

Resources linked to this family

Every card opens the complete internal TechOpsBase resource.

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SYSTEM GUIDEATA 28

A350 ATA 28 Fuel System - Complete Study Overview

An original system-level map of A350 fuel storage, safety, measurement, feed, transfer, refuel/defuel, jettison, control and monitoring.

TechOpsBase EditorialOpen resource →
SYSTEM GUIDEATA 29

Airbus A350 ATA 29 Hydraulic Power - System Study Guide

An original, system-level familiarization guide to the A350 Green and Yellow hydraulic systems, covering architecture, power generation, reservoirs, ground operatio…

TechOpsBase EditorialOpen resource →
SYSTEM GUIDEATA 36

A350 ATA 36 Engine Bleed Temperature Regulation and Precooler

Fan-air valve, remote-servo control, precooler heat exchange, dual temperature sensing and thermal protection.

TechOpsBase EditorialOpen resource →
SYSTEM GUIDEATA 36

A350 ATA 36 BAS, BAM, BOMU and Remote-Control Architecture

Normal BAS control, independent BAM monitoring, BOMU segregation, CRDC gateways, AFDX/CAN paths and remote servo commands.

TechOpsBase EditorialOpen resource →
SYSTEM GUIDEATA 36

A350 ATA 36 Engine Bleed Operation, Protection and Indication

Electronic/pneumatic regulation modes, source transitions, protective closure, pressure/temperature monitoring and ECAM indications.

TechOpsBase EditorialOpen resource →
SYSTEM GUIDEATA 36

A350 ATA 36 Overheat Detection System Architecture and Zones

Dual sensing loops, BOMU/OHDC monitoring, CPIOM gateways and fuselage, wing and pylon detection zones.

TechOpsBase EditorialOpen resource →
SYSTEM GUIDEATA 36

A350 ATA 36 Leak Detection, Automatic Isolation and Localization

Leak confirmation, staged valve isolation, crew backup action, reset behavior and CMS/TSM localization workflow.

TechOpsBase EditorialOpen resource →
SYSTEM GUIDEATA 36

A350 ATA 36 Pneumatic Ducting and Environmental Protection

Insulated ducts, joints, supports, relief features, structural heat protection and post-leak inspection reasoning.

TechOpsBase EditorialOpen resource →
SYSTEM GUIDEATA 36

A350 ATA 36 Cockpit Controls and ECAM BLEED Indications

AIR panel controls, engine/APU bleed pushbuttons, three-position crossbleed selector, BLEED page and fault interpretation.

TechOpsBase EditorialOpen resource →
SYSTEM GUIDEATA 36

A350 ATA 36 Pneumatic System Maintenance, Tooling and Access

Bleed-test equipment, heavy-component handling, precooler and valve access, manual deactivation and leak-localization practices.

TechOpsBase EditorialOpen resource →
SYSTEM GUIDEATA 36

A350 ATA 36 Pneumatic Interfaces and User-System Demand

Pneumatic interfaces with packs, service air, ice protection, engine start, water pressurization, ventilation and aircraft data systems.

TechOpsBase EditorialOpen resource →
SYSTEM GUIDEATA 36

A350 ATA 36 Operating Modes and Source-Transition Workshop

Normal two-engine supply, APU supply, ground supply, single-engine crossfeed, pneumatic backup and leak-isolated modes.

TechOpsBase EditorialOpen resource →
MAINTENANCE BOUNDARY

Learn here. Maintain with approved data.

Aircraft facts, videos, resources and community discussions are provided for education and discovery. They do not establish effectivity, maintenance limits, approved procedures, dispatch status, regulatory compliance or authorization.

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REVIEWED TECHNICAL CASES

A350 troubleshooting lessons

Privacy-cleared and technically reviewed cases connected to this aircraft family.

View all related cases →
Lesson learned TOB-DEMO-320-003

Intermittent electrical indication: build a condition map before replacing hardware

CurrentEducational exampleEducational example

A training example showing how intermittent faults require condition, timing and correlation evidence before a component conclusion.

What happenedAn electrical indication appeared intermittently and could not be reproduced during the first …
What was foundThe defect report lacked the operating phase, power-source configuration, duration, related me…
What solved itThe investigation was reframed around reproducibility and correlated evidence rather than imme…
Airbus A350 ATA 24
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