Test Flight Sample Clauses

Test Flight. Promptly after completion of the corrections, if any, required under Section 18.3 hereof (relating to the Final Inspection), and at the option of Lessor, a test flight (of up to one (1) hour) based on Manufacturer’s test flight program shall be conducted by Lessee for the purpose of demonstrating to Lessor the compliance of the Aircraft with the provisions of this Section 18. All costs of such test flight shall be paid by Lessee, including without limitation the cost of fuel, flight crew and insurance. Lessor’s representatives may participate in the test flight as observers. All pilot-reported discrepancies and all discrepancies identified by Lessor during the test flight shall be corrected by Lessee at its Lessee’s expense. There shall be no deferred items on the Aircraft except as the parties may mutually agree.
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Test Flight. While developing the application, a “scaled-down” version of the iOS Technology could be released as a test flight for approval, if requested by Licensee. Wait times for approval of the application is a variable and, depending on the reviewer at Apple, could add significant additional time to the expected release dates. If a test flight release is requested, it is anticipated that CannaSys would cease development on the Technology, which could add additional ramp up/ramp down costs yet to be determined. Currently, approval times for iOS apps are approximately seven business days.
Test Flight a. The Aircraft shall undergo an operational test flight, not to exceed two (2) hours which flight shall be conducted by using test flight procedures mutually agreed to by Lessor and Lessee. Lessee shall insure the Aircraft for the purposes of such test flight. Any discrepancies found during the test flight shall be corrected by Lessor at Lessor's expense. b. After any correction required to comply with the aforementioned conditions, Lessee may require Lessor to either (i) conduct an operational ground check on the Aircraft in accordance with the Manufacturer's maintenance manual or (ii) perform another demonstration test flight if required to verify the satisfactory operation of the systems that are normally flight checked after such correction. Lessor shall clear all discrepancies resulting from these ground and flight checks.
Test Flight. No FCM, excluding ACPs, shall be required to perform a Test Flight.
Test Flight. Prior to Delivery of an Aircraft hereunder, Seller shall cause a test flight to be performed in accordance with Seller's test flight procedures as set forth in Exhibit H hereto (the "Test Flight"). Such Test Flight shall be conducted during the Ferry Flight relating to such Aircraft. Seller shall document the Test Flight in a separate written protocol where discrepancies (if any) are indentified in writing to Buyer.
Test Flight. In the event it is necessary to conduct a test flight or any other flight for the verification of systems functionality at any time during the performance of the Services, such test flight ***** Confidential portions of the material have been omitted and filed separately with the Securities and Exchange Commission. shall be carried out by Customer with Customer’s crew and at Customer sole cost, expense and risk. Any discrepancies detected as during such test flight and which are directly and solely attributable to Aeroman’s workmanship shall be corrected by Aeroman at Aeroman’s sole cost and expense. In the event that an additional test flight is required by the OEM Maintenance Manual to verify corrections of the discrepancies directly and solely attributable to the workmanship of Aeroman, Aeroman shall pay the costs of such additional test flight.

Related to Test Flight

  • 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: i) implementation of engines: GENERAL ELECTRIC CF6-80E1A3

  • Configuration The configuration for the Purchase Right Aircraft will be the Detail Specification for Model 767-3S2F aircraft at the revision level in effect at the time of the Supplemental Agreement. Such Detail Specification will be revised to include (i) changes required to obtain required regulatory certificates and (ii) other changes as mutually agreed upon by Boeing and Customer.

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

  • Software Use Case Red Hat Enterprise Linux Developer Suite Subscription Services for Red Hat Enterprise Linux Developer Suite are available for Development Purposes only.

  • Acceptance Testing At the time of installation of a LIS trunk group, and at no additional charge, acceptance tests will be performed to ensure that the service is operational and meets the applicable technical parameters.

  • Service Specification The Parties have agreed upon the scope and specification of the Services provided under this Service Agreement in the Service Specification.

  • Commissioning Commissioning tests of the Interconnection Customer’s installed equipment shall be performed pursuant to applicable codes and standards. The ISO and Connecting Transmission Owner must be given at least five Business Days written notice, or as otherwise mutually agreed to by the Parties, of the tests and may be present to witness the commissioning tests.

  • Meter Testing Company shall provide at least twenty-four (24) hours' notice to Seller prior to any test it may perform on the revenue meters or metering equipment. Seller shall have the right to have a representative present during each such test. Seller may request, and Company shall perform, if requested, tests in addition to the every fifth-year test and Seller shall pay the cost of such tests. Company may, in its sole discretion, perform tests in addition to the fifth year test and Company shall pay the cost of such tests. If any of the revenue meters or metering equipment is found to be inaccurate at any time, as determined by testing in accordance with this Section 10.2 (Meter Testing), Company shall promptly cause such equipment to be made accurate, and the period of inaccuracy, as well as an estimate for correct meter readings, shall be determined in accordance with Section 10.3 (Corrections).

  • Mileage Measurement Where required, the mileage measurement for LIS rate elements is determined in the same manner as the mileage measurement for V&H methodology as outlined in NECA Tariff No. 4.

  • Test The outer surface of the lamp lenses shall be subjected once or more than once to the action of the sand jet produced as described above. The jet shall be sprayed almost perpendicular to the surface to be tested. The deterioration shall be checked by means of one or more samples of glass placed as a reference near the lenses to be tested. The mixture shall be sprayed until the variation in the diffusion of light on the sample or samples measured by the method described in Appendix 2, is such that: Δ d = (T5 - T4) / T2 ≤ 0.0250 ± 0.0025 Several reference samples may be used to check that the whole surface to be tested has deteriorated homogeneously.

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