General test requirements. Tests shall be carried out in order to determine whether the materials and apparatus comply with the Specification and to provide the necessary operation data. All tests shall be arranged to represent the working conditions as closely as possible. Unless an alternative place of testing is agreed or specified the tests shall be carried out at the Manufacturer's Works. Not less than fourteen days notice of all tests shall be given to the Engineer, in order that he may be present if he so desires. As many tests as possible shall be arranged together, in accordance with a program to be agreed with the Engineer. One copy of the Contractor's records of all tests shall be submitted to the Engineer for approval immediately after the conclusion of each test. These records shall be clearly marked so that the Contract equipment items or components to which they refer can be readily identified. Type tests will not be required in those cases where the Contractor can produce certified evidence that the required type tests have been performed successfully on identical equipment or equipment which is for practical test purposes similar and produced in the factory where the equipment offered is to be manufactured. Evidence to this effect shall be submitted at the time of tendering, or as practicable thereafter. High voltage tests shall be conducted generally in accordance with IEC 60060. Insulating oil or gas used in any equipment undergoing tests shall comply with the requirements of IEC 60296 or 60376 as appropriate. Except where otherwise indicated all electrical tests shall be carried out at rated frequency and with the supply voltage waveform approximately sinusoidal. The Manufacturer's test equipment shall be of satisfactory quality and condition and where necessary shall be appropriately calibrated at the expense of the Contractor by such other body as may be agreed. Where no tests are detailed for items of equipment a full program of tests shall be agreed with the Engineer. The Engineer reserves the right to call for such additional tests as may be necessary to prove compliance with the Specification.
General test requirements. The pressure of the fuel tank at the beginning of the test shall be within 0.1 MPa of the saturation pressure of LNG in the inner tank. The lapse of time, from the moment that the average temperature first reaches 590 °C until the opening of the primary pressure relief valve, shall be measured. Once the pressure relief valve opens, the test shall continue until the blow off of the pressure relief valve is complete.
General test requirements. Container shall be filled with 80 per cent in volume of LPG (commercial fuel) and tested in the horizontal position at working pressure;
General test requirements. 3.1. Frequency range, dwell times Measurements shall be made in the 20 to 2,000 MHz frequency range with frequency steps according to ISO 11452-1, third edition 2005. The test signal modulation shall be:
(a) AM (amplitude modulation), with 1 kHz modulation and 80 per cent modulation depth in the 20 to 800 MHz frequency range;
(b) PM (pulse modulation), t on 577 µs, period 4,600 µs in the 800 to 2,000 MHz frequency range, if not otherwise agreed between Technical Service and ESA manufacturer. Frequency step size and dwell time shall be chosen according to ISO 11452-1, third edition 2005.
3.2. The Technical Service shall perform the test at the intervals specified in ISO 11452-1, third edition 2005 throughout the frequency range 20 to 2,000 MHz. Alternatively, if the manufacturer provides measurement to data for the whole frequency band from a test laboratory accredited to the applicable parts of ISO 17025, first edition 1999 and recognized by the Approval Authority, the Technical Service may choose a reduced number of spot frequencies in the range, e.g. 27, 45, 65, 90, 120, 150, 190, 230, 280, 380, 450, 600, 750, 900, 1,300, and 1,800 MHz to confirm that the ESA meets the requirements of this annex.
3.3. If an ESA fails the tests defined in this annex, it must be verified as having failed under the relevant test conditions and not as a result of the generation of uncontrolled fields.
General test requirements. Unless specified otherwise, the Contractor shall provide all test beds, equipment and measuring instruments required to complete the appropriate level of factory testing. For site acceptance Inmarsat will provide any necessary COTS RF test equipment (e.g. spectrum analysers etc.), this equipment shall be available at SATR. * Portions of this document marked with **** have been omitted pursuant to a request for confidential treatment submitted with the SEC. The original contracts have been filed separately with the SEC as part of the confidential treatment request. Ref: INMARSAT GLOBALISED VOICE Issue: Draft V2.8h Date: Inmarsat Globalised Voice Project 06-4318 Statement of Work
1. The Contractor shall produce and maintain test plans, test designs and test procedures and test reports for all test levels covering hardware, firmware and software as required by his ISO 9001 standards (or equivalent).
2. At ****, the Contractor shall deliver a comprehensive end-to-end Test Plan ****.
3. The Contractor shall develop a comprehensive set of test procedures for each acceptance test activity.
4. Test procedures developed for the acceptance phase shall require Inmarsat approval.
5. The test procedures shall **** demonstrate that the system is able to deliver contract end-to-end functionality in accordance with the Contractor’s work scope in accordance with Section 2.1 of this Statement of Work.
6. Test procedures shall be presented to Inmarsat before the testing is conducted.
General test requirements. 7.1. Variables While performing the tests described in this Regulation, the following variables shall be measured:
7.1.1. Brake pedal force, Fp ;
7.1.2. Vehicle velocity, vx ;
7.1.3. Vehicle deceleration, ax ;
7.1.4. Brake temperature, Td ;
7.1.5. Brake pressure, P, where applicable;
General test requirements. 1. Piping shall be adequately restrained against movement before testing. Pressure line shall have thrust blocks installed and the concrete shall have attained full design strength before test pressure is applied to the line.
2. Piping system shall be flushed clean, and sediment, scale, dirt, and debris removed before piping is tested.
3. Adequate provision shall be made for carrying off flushing water without causing erosion or other damage.
4. Piping shall be tested before joints are concealed or made inaccessible.
5. Tests shall be made in the presence of an Inspector of the authority having jurisdiction.
General test requirements. Unless specified otherwise, the Contractor is expected to provide all test beds, equipment and measuring instruments required to complete the appropriate levels of testing.
1. The Contractor shall produce and maintain test plans, test designs, test procedures and test reports for all identified testing levels.
2. By PDR, the Contractor shall deliver a complete and comprehensive Test Plan defining the test approach to be adopted, acceptance test mapping (i.e. Verification Requirements Traceability Matrix - VCRM) and associated test document structure to demonstrate coverage of all contracted requirements.
3. The Contractor shall develop a comprehensive set of test procedures for each testing level identified. For standard products then existing product test results or product conformance statements may be suitable in places.
4. Developed test procedures shall require Inmarsat approval.
General test requirements. Unless specified otherwise, the Contractor is expected to provide all test beds, equipment and measuring instruments required to complete the appropriate level of factory testing. For site acceptance Inmarsat will provide any necessary COTS equipment (e.g. spectrum analysers).
1. The Contractor shall produce and maintain test plans, test designs and test procedures and test reports for all test levels covering hardware, firmware and software as required by his ISO 9001 standards (or equivalent).
2. By PDR, the Contractor shall deliver a complete and comprehensive RAN Test Plan defining the test approach to be adopted, acceptance test mapping (i.e. Verification Requirements Traceability Matrix - VCRM) and associated test document structure to demonstrate coverage of all contracted requirements as required by his ISO 9001 standards.
3. The Contractor shall develop a comprehensive set of test procedures for each acceptance test activity. For switching system standard products, existing product test results or product conformance statements may be provided in lieu of new tests to demonstrate network element requirement conformance.
4. Test procedures developed for the acceptance phase shall require Inmarsat approval.
General test requirements. 6.3.1. All the belt anchorages of the same group of seats shall be tested simultaneously. However, if there is a risk that non-symmetrical loading of the seats and/or anchorages may lead to failures, an additional test may be carried out with non- symmetrical loading.
6.3.2. The tractive force shall be applied in a direction corresponding to the seating position at an angle of 10° ± 5° above the horizontal in a plane parallel to the median longitudinal plane of the vehicle.
6.3.3. Full application of the load shall be achieved as rapidly as possible. The belt anchorages must withstand the specified load for not less than 0.2 second.
6.3.4. Traction devices to be used in the tests described in paragraph 6.4. below are shown in annex 5.
6.3.5. The belt anchorages for seats for which upper belt anchorages are provided shall be tested under the following conditions:
