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. 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. 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. 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 A319-100 Aircraft as described in the Standard Specification Ref. J 000 01000 Issue 6 dated 1st March 2007 equipped with:

  • 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.

  • Minimum Customer Support Requirements for TIPS Sales Vendor shall provide timely and commercially reasonable support for TIPS Sales or as agreed to in the applicable Supplemental Agreement.

  • 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.

  • 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.

  • Configuration Management The Contractor shall maintain a configuration management program, which shall provide for the administrative and functional systems necessary for configuration identification, control, status accounting and reporting, to ensure configuration identity with the UCEU and associated cables produced by the Contractor. The Contractor shall maintain a Contractor approved Configuration Management Plan that complies with ANSI/EIA-649 2011. Notwithstanding ANSI/EIA-649 2011, the Contractor’s configuration management program shall comply with the VLS Configuration Management Plans, TL130-AD-PLN-010-VLS, and shall comply with the following:

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