Cart
0
Product
Products
(empty)
No products
To be determined
Shipping
$0.00
Total
Product successfully added to your shopping cart
Quantity
Total
There are 0 items in your cart.
There is 1 item in your cart.
Total products
Total shipping
To be determined
Total
Reduced price!
View larger
View larger
FAA FO 8110.105
New product
FAA FO 8110.105 2008 Edition, July 16, 2008 Simple And Complex Electronic Hardware Approval Guidance
More info
Description / Abstract:
Purpose of this Order.
a. We've written this order to supplement RTCA/DO-254, and give you guidance for approving both simple and complex custom micro-coded components. This guidance applies to airborne systems and equipment, and the airborne electronic hardware of those systems when you work in a certification project (type, supplemental, amended, and amended supplemental) or technical standard order authorization. This order accepts RTCA/DO-254 as the means by which an applicant can seek FAA approval. If an applicant proposes another means, including achieving acceptable design assurance for these components by using verification and/or architectural strategies at the system or equipment level, we may need to develop more guidance (such as issue papers) on a project-byproject basis.
b. If an applicant follows RTCA/DO-254 for level D components, we don't need to review the life cycle data. However, we will review it if the applicant chooses to use their existing design assurance practices, as allowed by Advisory Circular (AC) 20-152, RTCA, Inc., Document RTCA/DO-254, Design Assurance Guidance For Airborne Electronic Hardware, Paragraph 1.b. Refer to FAA part- specific policy for exceptions.
a. We've written this order to supplement RTCA/DO-254, and give you guidance for approving both simple and complex custom micro-coded components. This guidance applies to airborne systems and equipment, and the airborne electronic hardware of those systems when you work in a certification project (type, supplemental, amended, and amended supplemental) or technical standard order authorization. This order accepts RTCA/DO-254 as the means by which an applicant can seek FAA approval. If an applicant proposes another means, including achieving acceptable design assurance for these components by using verification and/or architectural strategies at the system or equipment level, we may need to develop more guidance (such as issue papers) on a project-byproject basis.
b. If an applicant follows RTCA/DO-254 for level D components, we don't need to review the life cycle data. However, we will review it if the applicant chooses to use their existing design assurance practices, as allowed by Advisory Circular (AC) 20-152, RTCA, Inc., Document RTCA/DO-254, Design Assurance Guidance For Airborne Electronic Hardware, Paragraph 1.b. Refer to FAA part- specific policy for exceptions.