
FMS-D212-725-1
Page 1-9
• COPYRIGHT © 2007 BY DART AEROSPACE LTD •
This document is private and confidential and is supplied on the express condition that it is not to be used for any
purpose or copied or communicated to any other person without written permission from Dart Aerospace Ltd.
Revision:
F
TC Approved Date: 10.05.12
1.5.5 Cargo
1.5.5.1 Internal Cargo Configuration
Allowable deck loading for cargo is 100 pounds per square foot (4.9
kilograms/100 square centimeters). Deck mounted tiedown fittings are
provided and have an airframe structural capacity of 1250 pounds (567.0
kilograms) vertical and 500 pounds (226.8 kilograms) horizontal per fitting.
Provisions for installation of cargo tiedown fittings are incorporated in aft
cabin bulkhead and transmission support structure and have an airframe
structural capacity of 1250 pounds (567.0 kilograms) at 90 degrees to
bulkhead and 500 pounds (226.8 kilograms) in any direction parallel to
bulkhead. Cargo shall be secured by an approved restraint method that will
not impede access to cargo in an emergency. All cargo and equipment shall
be securely tied down when operating with aft cabin doors open or removed.
1.5.5.2 Cargo Compartment
Cargo compartment maximum allowable loading is 400 pounds (181.4
kilograms), not to exceed 100 pounds per square foot (4.9 kilograms/100
square centimeters).
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