Horizontal Stabilizer Main Structural Box Sample Clauses
The "Horizontal Stabilizer Main Structural Box" clause defines the requirements and specifications for the main load-bearing structure within the horizontal stabilizer of an aircraft. This clause typically outlines the materials, design standards, and testing procedures that must be followed to ensure the structural integrity of this critical component. For example, it may specify the use of certain alloys, minimum thicknesses, or fatigue testing protocols. Its core practical function is to ensure the safety and reliability of the horizontal stabilizer by mandating robust construction standards, thereby reducing the risk of structural failure during operation.
Horizontal Stabilizer Main Structural Box. 4.1.1 Spars
4.1.2 Ribs
4.1.3 Upper and lower skins and stringers
4.1.4 Support structure and attachment fitting to fuselage and trim screw actuator
4.1.5 Elevator support structure
4.1.5.1 Hinge bracket
4.1.5.2 Servocontrol attachment brackets
Horizontal Stabilizer Main Structural Box. 4.1.1 [*****]
4.1.2 [*****]
4.1.3 [*****]
4.1.4 [*****]
4.1.5 [*****]
4.1.5.1 [*****]
4.1.5.2 [*****]
Horizontal Stabilizer Main Structural Box. 4.1.1 [*CTR*]
4.1.2 [*CTR*]
4.1.3 [*CTR*]
Horizontal Stabilizer Main Structural Box. 4.1.1 [***] CT1707017 PA A321 NEO EXECUTION [***] Confidential portion omitted and filed separately with the Commission Pursuant to a Request for Confidential Treatment. 4.1.2 [***]
Horizontal Stabilizer Main Structural Box. 4.1.1 [***] CT1707017 PA A321 NEO EXECUTION PRIVILEGED AND CONFIDENTIAL Exh F 2 Exhibit F
4.1.2 [***]
4.1.3 [***]
Horizontal Stabilizer Main Structural Box. 4.1.1 Spars
4.1.2 Ribs
4.1.3 Upper and lower skins and stringers
