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Embraer KC-390
EMBRAER KC-390

CEIIA IS A KEY PARTNER IN THE ENTIRE DEVELOPMENT CYCLE OF THE NEW KC-390, THE LARGEST AIRCRAFT EVER PRODUCED BY EMBRAER.

 

 

This participation is focused on two primary structures (the elevator and the central fuselage) and on the sponson and included activities such as Design, Stress Analysis, Weight Reduction, Manufacturing Support, the production of the First Flight Documentation and Certification Documentation and the definition and execution of tests.

 

ELEVATOR

ENTIRE DEVELOPMENT CYCLE OF KC-390 ELEVATOR STRUCTURE
FROM CONCEPTUAL TO CERTIFICATION PHASE (BOTH INCLUDED)

MAIN ACTIVITIES

Design

Stress Analysis including F&DT

Weight Reduction Campaign

Manufacturing Support

First Flight Documentation

Certification Documentation

Definition & execution Tests

Tooling
and GSE

PERIOD

2011 - Ongoing

LOCATION

Brazil (until PDR) and Portugal

CENTRAL FUSELAGE

DETAIL DESIGN OF THE KC-390 CENTRAL FUSELAGE
AND RE-DESIGN IN ORDER TO IMPLEMENT A WEIGHT REDUCTION CAMPAIGN

MAIN ACTIVITIES (DETAILED DESIGN)

3D models
& FTA

Configuration Control

Installation drawings

PERIOD

2013

LOCATION

Portugal and Spain

MAIN ACTIVITIES (WEIGHT REDUCTION)

3D models
& FTA

Configuration Control

Installation drawings

Production
Support

PERIOD

2014

LOCATION

Portugal

SPONSON

ENTIRE DEVELOPMENT CYCLE OF KC-390 SPONSON STRUCTURE (WITH MAIN LANDING GEAR DOOR) FROM CONCEPTUAL TO CERTIFICATION PHASE (BOTH INCLUDED)

MAIN ACTIVITIES

Design

Stress Analysis including F&DT

Weight Reduction Campaign

Certification Documentation

Definition & execution Tests

Tooling
and GSE

PERIOD

2011 - Ongoing

LOCATION

Brazil (until PDR) and Portugal

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