Flight Performance Sample Clauses
The FLIGHT PERFORMANCE clause sets out the standards and requirements for how an aircraft must operate during a flight. It typically details the expected performance metrics such as speed, altitude, fuel efficiency, and safety parameters that must be met throughout the journey. For example, it may require the aircraft to maintain certain operational thresholds or comply with regulatory guidelines. The core function of this clause is to ensure that flights are conducted safely and efficiently, minimizing risks and clarifying expectations for both operators and passengers.
Flight Performance. 2.1 Takeoff
2.1.1 Takeoff Performance at [***] When the Aircraft is operated in departure airport conditions as defined below [***]: [***] The FAA dry permissible Takeoff Weight shall not be less than [***].
2.1.2 Takeoff Performance at [***] When the Aircraft is operated in departure airport conditions as defined below [***]: [***] The FAA dry permissible Takeoff Weight shall not be less than [***].
2.1.3 Takeoff Performance at [***] When the Aircraft is operated in departure airport conditions as defined below [***]: [***] The FAA dry permissible Takeoff Weight shall not be less than [***].
2.2 Speed The level flight speed at a gross weight of [***], on an ISA+15°C day, at an [***] and using not more than maximum cruise thrust, shall not be less than the following guarantee value: [***]
2.3 [***]
2.3.1 [***]
2.3.2 [***]
2.3.3 [***]
2.4 [***] The guarantees set forth in Paragraphs 2.4.1, 2.4.2 and 2.4.3 herein are hereinafter referred to as the “[***] Guarantees”.
2.4.1 [***]
2.4.2 [***]
2.4.3 [***]
2.5 [***] The guarantees set forth in Paragraphs 2.5.1 and 2.5.2 below are hereinafter referred to as the “[***] Guarantees”).
2.5.1 [***] The [***], in nautical miles in still air using the conditions and operating rules defined below, shall not be less than the following guarantee value: [***] Conditions and operating rules: [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***]
2.5.2 [***] The [***] in nautical miles in still air using the conditions and operating rules defined below, shall not be less than the following guarantee value: [***] Conditions and operating rules: [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***]
Flight Performance. [***] The guarantees set forth in Paragraphs 2.1.1, 2.1.2 and 2.1.3 herein shall be referred to as the [***].
Flight Performance. 2.1 Enroute One-Engine-Inoperative Altitude The FAA approved gross weight at an enroute one-engine-inoperative altitude of *** feet at which the available gross climb gradient equals *** percent on an ISA+10°C day using not more than maximum continuous thrust with engine and wing anti-ice bleed on, shall not be less than the following guarantee value: NOMINAL: *** Pounds TOLERANCE: *** Pounds GUARANTEE: *** Pounds
Flight Performance a Enroute One-Engine-Inoperative Altitude
Flight Performance. 2.1 [***] The guarantees set forth in Paragraphs 2.1.1, 2.1.2 and 2.1.3 herein shall be referred to as the [***]. [***] Confidential portion omitted and filed separately with the Commission Pursuant to a Request for Confidential Treatment.
2.1.1 [***] [***]:
2.1.2 [***] [***]
2.1.3 [***] [***]:
2.2 [***] The guarantees set forth in Paragraphs 2.2.1 and 2.2.2 herein shall be referred to as the [***].
2.2.1 [***] [***]
2.2.2 [***] [***] [***]
(i) [***],
(ii) [***], and
(iii) [***].
2.3 [***] [***]: (the [***]).
2.4 [***] [***] Confidential portion omitted and filed separately with the Commission Pursuant to a Request for Confidential Treatment. [***]: (the [***]).
2.5 [***] [***]: (the [***]). [***]:
(i) [***]
(ii) [***]
(iii) [***]
2.6 [***] The guarantees set forth in Paragraphs 2.6.1, 2.6.2 and 2.6.3 herein shall be referred to as the [***].
2.6.1 [***]: [***]
2.6.2 [***]: [***]
2.6.3 [***]: [***]
2.7 [***] The guarantees set forth in Paragraphs 2.7.1, 2.7.2 and 2.7.3 herein shall be referred to as the [***].
2.7.1 [***] [***]: [***] [***]: [***] Confidential portion omitted and filed separately with the Commission Pursuant to a Request for Confidential Treatment. [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***]
2.7.2 [***] [***]: [***] [***]: [***] [***] [***] [***] [***] [***] [***] [***] Confidential portion omitted and filed separately with the Commission Pursuant to a Request for Confidential Treatment. [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***]
2.7.3 [***] [***]: [***] [***]: [***] [***] [***] [***] [***] [***] [***] [***] Confidential portion omitted and filed separately with the Commission Pursuant to a Request for Confidential Treatment. [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***]
2.7.4 [***] [***] [***]: [***] [***]: [***] [***] [***] [***] [***] [***] [***] Confidential portion omitted and filed separately with the Commission Pursuant to a Request for Confidential Treatment. [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [***] [*...
Flight Performance. 2.1 TAKEOFF
2.1.2 PA NO. 3032 S.A. 1 AERO-B-BBA4-M05.1009A SS06-0130
2.1.3 The FAA approved takeoff gross weight at the start of ground roll, at a temperature of 35 degrees C, at an altitude of 75 feet, from a 11,811 foot runway, and satisfying the conditions defined below, and using maximum takeoff thrust, shall not be less than the following guarantee value: *** Conditions: ***
2.2 Landing ***
2.3 Speed ***
Flight Performance