Airbus Filton’s wing design centre answers in 3 seconds
AS9100, EASA Part 21 design approval and composite manufacturing specifications for the A350 and A320 family: documentation indexed and instantly retrievable.
Wing design authority, not assembly
Filton designs and manufactures composite wing components — the physical assembly of complete wing boxes happens 200 miles away at Broughton. Each stage has its own documentation and compliance focus.
2
Airbus aircraft families supported: A350 and A320 family wing structures
AS9100
aerospace quality standard governing design engineering and composite manufacturing
-40%
audit response time with indexed design and process documentation
The Filton industrial fabric
Wing design engineering
Structural design authority for A350 and A320 family wings, working under EASA Part 21 design organisation approval.
Composite wing manufacturing
Carbon fibre layup, autoclave curing and NDT of wing components before shipment to Broughton for assembly.
AS9100 quality management
Configuration management, risk assessment and first article inspection governing design and manufacturing changes.
EASA Part 21 design approval
Design organisation approval documentation for wing structure and composite process changes.
UK CAA certification overlap
Parallel certification pathway for components entering aircraft certified under the UK regime post-Brexit.
Bristol aerospace cluster
Engineering talent pipeline from the University of Bristol and the wider West of England aerospace ecosystem.
Use cases in Filton’s design and manufacturing teams
AS9100 design audit
Auditor requests the design change record for a wing rib modification. Exact document returned in seconds.
Composite cure cycle lookup
Manufacturing engineer confirms the autoclave cure cycle parameters for a specific wing panel batch.
EASA Part 21 change approval
Design engineer retrieves the DOA approval record for a recent wing structure modification.
NDT report retrieval
Quality inspector pulls the ultrasonic scan results for a composite panel before shipment to Broughton.
UK CAA/EASA dual certification
Certification team confirms which regulator’s documentation applies to a component destined for a UK-registered aircraft.
New design engineer onboarding
Centralised AS9100 and Part 21 documentation accelerates onboarding for engineers joining the wing design team.
Frequently asked questions
What makes Airbus Filton distinct from Airbus Broughton?+
Filton, near Bristol, is Airbus UK’s centre for wing design engineering and composite wing component manufacturing, supporting the A350 and A320 family programmes. It is a design authority and composite manufacturing site, producing wing structures and components that are then shipped to Broughton in North Wales for major wing box assembly. Broughton, by contrast, performs the physical assembly of complete wing boxes from components sourced across the Airbus supply chain, including from Filton. IgeraIndustria indexes each site’s documentation separately, reflecting their distinct roles in the same wing value chain.
What is AS9100 and why is it central to Filton’s operations?+
AS9100 is the aerospace quality management standard built on ISO 9001, adding requirements for configuration management, risk management and first article inspection specific to aerospace manufacturing. Filton’s design engineering and composite manufacturing teams work under AS9100 to ensure wing components meet exacting structural and safety requirements before shipment to final assembly. IgeraIndustria indexes AS9100 procedures and design records for immediate retrieval.
How does EASA Part 21 apply to design work carried out at Filton?+
EASA Part 21 governs the certification of aircraft design and production organisations within the European aviation system. As a wing design authority, Filton must demonstrate compliance with Part 21 design organisation approval (DOA) requirements for any changes to wing structure or composite manufacturing processes. IgeraIndustria indexes design approval documentation and change records by component and revision.
How does UK CAA certification overlap with EASA at Filton post-Brexit?+
Since Brexit, the UK Civil Aviation Authority (CAA) operates its own certification regime in parallel with EASA, though the two remain closely aligned for aircraft type certification given the shared Airbus European production network. Filton’s design and manufacturing documentation must satisfy both regulators for components entering aircraft certified under either system. IgeraIndustria indexes both EASA and CAA-relevant documentation and cites which applies to a given certification pathway.
What composite manufacturing processes does IgeraIndustria support at Filton?+
Filton’s composite wing manufacturing involves layup, autoclave curing and non-destructive testing of carbon fibre wing components for the A350 and A320 family. Engineers can query cure cycle parameters, NDT results and material batch certificates directly, with IgeraIndustria returning the exact process specification and revision in seconds.
How does IgeraIndustria support an AS9100 audit of Filton’s design engineering function?+
The auditor can query design change records, risk assessments and first article inspection reports directly, and IgeraIndustria returns the exact document with citation in under 3 seconds, distinguishing Filton’s design-and-composite-manufacturing scope from Broughton’s wing box assembly scope within the same indexed Airbus documentation set.
Why does IgeraIndustria offer separate pages for Filton and Broughton rather than one combined Airbus UK page?+
Filton and Broughton perform genuinely different manufacturing stages with different day-to-day compliance questions: Filton engineers query design change control and composite cure specifications, while Broughton engineers query wing box structural assembly and major component fit tolerances. Combining them into one page would blur these distinct workflows, so IgeraIndustria indexes each site’s documentation as a separate, focused knowledge base.
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