Engine Strut Sample Clauses

The "Engine Strut" clause defines the requirements and standards for the engine strut component in an aircraft or mechanical system. It typically outlines the materials, design specifications, and performance criteria that the engine strut must meet, such as load-bearing capacity and resistance to vibration or fatigue. For example, the clause may require the strut to be constructed from specific alloys and to undergo certain testing procedures before installation. The core function of this clause is to ensure the safety and reliability of the engine mounting system, thereby minimizing the risk of mechanical failure and enhancing overall operational integrity.
Engine Strut. (i) Strut external surface skin and doublers and stiffeners. (ii) Internal strut chords, frames and bulkheads. (iii) Strut to wing fittings and diagonal brace. (iv) Engine mount support fittings attached directly to strut structure and including the engine-mounted support fittings.
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Engine Strut. (a) [CONFIDENTIAL PORTION OMITTED AND FILED SEPARATELY WITH THE COMMISSION PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT]. (b) [CONFIDENTIAL PORTION OMITTED AND FILED SEPARATELY WITH THE COMMISSION PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT]. (c) [CONFIDENTIAL PORTION OMITTED AND FILED SEPARATELY WITH THE COMMISSION PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT]. (d) [CONFIDENTIAL PORTION OMITTED AND FILED SEPARATELY WITH THE COMMISSION PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT]. P.A. No. 3219 SLP1- PA_Supp_Ex_SLP1_787 Rev.: 12/15/06 [Model 787 Only:]
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Engine Strut. Strut external surface skin and doublers and stiffeners.
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Engine Strut. Main Landing Gear. ***
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Related to Engine Strut

  • Engine A. Any internal repairs or replacement of internal components, or replacement of engine assembly.

  • Engines POSITION SERIAL NO. TOTAL HOURS TOTAL CYCLES HRS/CYCLES SINCE LAST SHOP VISIT Time Remaining to Next LIFE LIMITED PART REMOVAL PART NAME HOURS CYCLES MSN MSN

  • AIRCRAFT CONFIGURATION The guarantees defined below ("the Guarantees") are applicable to the A330-200 Aircraft as described in the Technical Specification ***, as amended by the Specification Change Notices ("SCN's") for:

  • Aircraft This peril includes self-propelled missiles and spacecraft.

  • Optional Features The Optional Features Prices selected for the Option Aircraft will be adjusted to Boeing's current prices as of the date of execution of the definitive agreement for the Option Aircraft.