Fixed Wing Aircraft used for Firebombing must be either multi-engined or, if single- engined, must be powered by a gas turbine engine.
Fixed Wing Aircraft and tank-equipped Rotary Wing Aircraft must be capable of being ground filled.
Fixed Wing Aircraft must be either multi-engined or, if single-engined, must be powered by a gas turbine engine.
Fixed Wing Aircraft used for Firebombing must be either multi-engined or, if single- engined, must be powered by a gas turbine engine. Fixed wing Aircraft used for other roles are preferred to be either multi-engined or, if single-engined, powered by a gas turbine engine.
d. Aircraft required to carry passengers must have a Standard Certificate of Airworthiness, or equivalent in the country of registration, for the aircraft configuration used to supply the Services. For Rotary Wing Aircraft with Firebombing tanks where a deployed hover- fill snorkel requires the Aircraft hold a Special Certificate of Airworthiness (e.g. Restricted Category) then a dual Certificate of Airworthiness is acceptable, provided the Standard Certificate of Airworthiness applies when the snorkel is stowed or removed.
e. The Aircraft must use only aviation grade fuel that has been approved by the engine manufacturer and by CASA for use in the Aircraft.
f. The Contractor will be responsible for equipping the Aircraft to meet the requirements of this Contract and to carry out the Services required, and will also be responsible for arranging all appropriate and necessary approvals, authorisations and documentation.
g. The Contractor will ensure the Aircraft is, as far as practicable, configured to optimally provide the Services required under this Contract, and that the payload and range are optimised. For example, this includes, but is not limited to:
i. removing equipment not required for the delivery of the Services; and
ii. equipping the Aircraft with appropriate performance enhancing devices.
h. The Contractor will ensure that the Aircraft is securely locked as a precaution against unauthorised entry into the Aircraft.
i. The Contractor will provide in ARENA the empty weight details of the Aircraft prior to the commencement of the first Service Period or if the empty weight details change during the Contract Period.
j. Where the Aircraft may purge a quantity of fuel to the ground on engine shutdown, start-up or during maintenance, the Aircraft must be equipped with a suitable fuel collection or purging prevention device; or the Contractor must demonstrate to the satisfaction of NAFC or the Member that fuel purging does not otherwise pose a fire or environmental risk.
k. The Contractor must have a trend monitoring system to monitor and record a range of flight, aircraft and engine parameters. The system will enable the storage of the records and the Contractor will maintain the records for at least 90...
Fixed Wing Aircraft shall be developed and manufactured by COI. The design will be in conformance with to the extent possible the ARC System baseline design specifications and expanded and enhanced as required.. This is set forth in the Platforms' proprietary ARC System Confidential Intellectual Property System Design Specifications Document as jointly developed and produced on July 13, 1999 by Platforms and TechnoCom Corporation, under exclusive contract with Platforms, and used by Platforms and TechnoCom as the blueprint for the design, manufacture, and aircraft integration of the ARC ALPHA System, which was successfully demonstrated in September 1999 in Alpine, Texas, and which was the basis for the AMERICEL Contract and the forthcoming BETA Demonstration in Brazil. The ARC System Confidential Intellectual Property System design Specifications Document as developed and produced on July 13, 1999 by Platforms and TechnaCom Corporation was delivered by Platforms to COI on May 31, 2000, under a Proprietary Information Exchange and Non- disclosure Agreement, for use by COI as a Platforms-proprietary source document for the final design and development of the Platforms Airborne Relay Communications "ARC" BETA / Pre-production System to be delivered to Americel and demonstrated in Brazil in 4Q-2000. PIC and COI agree as follows:
1. COI shall support the ARC System Beta Test Demonstration in Brazil, by working to finalize the details of a Memorandum of Understanding MOU by 6-9-00 for the development of the Aerostat Airship and Aircraft TDMA wireless telecommunications payloads, and related System engineering support.
2. PIC will provide COI with a letter contract (Authorization to proceed) by 6-20-00, including funding in the amount of $225,000.00 ($25,000.00 previously owed). Both parties agree to work to establish a definitive contract for a time and material effort within 30 days of execution of this document. The definitive contract will define any exclusivity in the relationship between COI and PIC.
3. COI will host the ARC System overview meeting with Ericsson and Lindstrand on the 12th of June at the Xxxxxx Xxrnardo Payload Facility.
4. The exxxxxxx of any data under this MOU, or any agreement developed as a result of this MOU shall be governed by a Proprietary Information Exchange Agreement dated May 12, 2000 between PIC and COI.
5. In exchange for the agreed compensation set forth above, PIC shall receive the full benefit of COI's design and fabrication labor toward the c...
Fixed Wing Aircraft. Aircraft Classification Minimum amount of liability insurance (for any one occurrence) Helicopters Aircraft Classification Minimum amount of liability insurance (for any one occurrence)
