Take-off. JAR take-off field length at an Aircraft gross weight of *** at the start of ground run at sea level pressure altitude in ISA+15°C conditions shall be not more than a guaranteed value of : ***.
Take-off. FAR take-off field length at an A350XWB-800 Aircraft gross weight of 540,132 lb at the start of ground run at sea level pressure altitude at ISA+15°C shall be not more than a guaranteed value of [...***...]
Take-off. 1.1.1 FAR take-off field length at an A319 Aircraft gross weight of 166,450 lb (75,500 kg) at the start of ground run at sea level pressure altitude at a temperature of 84(degree)F will be not more than a guaranteed value of 8,980 feet.
1.1.2 When operated under the following conditions (representative of PHX 08R): Pressure altitude : 1,133 ft Ambient temperature : 100(degree)F Take-off run available ("TOR") : 10,300 feet Take-off distance available : 10,300 feet Accelerate-stop distance available : 10,300 feet Slope : 0.20% uphill Wind : Zero Obstacles (height and distance : 15 feet/1,438 feet from end of TOR) : 418 feet/17,285 feet the maximum permissible weight at the start of ground run will be not less than a guaranteed value of 158,250 lb.
1.1.3 When operated under the following conditions (representative of DEN 09): Pressure altitude : 5,431 ft Ambient temperature : 84(degree)F Take-off run available ("TOR") : 12,000 feet Take-off distance available : 12,000 feet Accelerate-stop distance available : 12,000 feet Slope : 0.01% uphill Wind : Zero Obstacles : None the maximum permissible weight at the start of ground run will be not less than a guaranteed value of 158,700 lb.
Take-off. FAR take-off field length at an A320 Aircraft gross weight of 169,750 lb (77,000 kg) at the start of ground run at sea level pressure altitude at a temperature of 84(degree)F will be not more than a guaranteed value of 7,420 feet.
Take-off. FAR take-off field length at an New A320 (CFM Powered) Aircraft gross weight of **at the start of TORA at sea level pressure altitude in ** shall be not more than a guaranteed value of **.
Take-off. In the event that an Aircraft fails to meet the take-off guarantees set forth in Subparagraph 1.3 or 1.4 of this Part A, the amount of Compensation shall be ***, provided that the Buyer demonstrates to the Seller that such deficiency adversely impacts the Buyer's operation of the affected Aircraft. With respect to Subparagraph 1.4 of this Part A, the amount of Compensation hereunder shall be ***
Take-off. When operated under the following conditions and with Air Conditioning 'ON': Pressure altitude : 21 ft Ambient temperature : 84(degree)F Take-off run available ("TOR") : 10,499 ft Take-off distance available : 10,499 ft Accelerate-stop distance available : 10,499 ft Slope : 0.1% uphill Wind : Zero Obstacles (height and distance : 23 ft/1,054 ft from end of TOR) : 167 ft/14,000 ft : 530 ft/42,472 ft Runway surface : Dry the maximum permissible weight at the start of ground run will be not less than the guarantee value. Nominal: 507,060 lb Guarantee: ***
Take-off. Federal Aviation Regulations (“FAR”) take-off field length at an Aircraft gross weight of 169,756 lb at the start of ground run at sea level pressure altitude and at a temperature of 86°F shall be not more than a guaranteed value of [***] ft.
Take-off. Tow planes and gliders will take-off from Taxiway Alpha, between Runway 18/36 and Taxiway Xxxxxxx in the north-westerly direction, which is referred to as “Alpha 30”;
Take-off. 1.1.1 FAR take-off field length at an New A321 (IAE Powered) Aircraft gross weight of **at the start of TORA at sea level pressure altitude in ** shall be not more than a guaranteed value of **.
1.1.2 When operated under the following conditions **: Pressure altitude : ** Ambient temperature : ** Take-off run available (TORA) : ** Take-off distance available : ** Accelerate-stop distance available : ** Slope : ** Wind : ** Line-up allowance TXX : ** Line-up allowance ASD : ** Obstacles (height and distance : ** from end of TORA) : ** : ** : ** ** Confidential Treatment Requested. USA — Amended and Restated Airbus A320 Family Purchase Agreement LA 8F-2 — 2 of 20 EXECUTION PRIVILEGED AND CONFIDENTIAL : ** : ** : ** the maximum permissible weight at the start of TORA shall be not less than a guaranteed value of **.
1.1.3 When operated under the following conditions **: Pressure altitude : ** Ambient temperature : ** Take-off run available (TORA) : ** Take-off distance available : ** Accelerate-stop distance available : ** Slope : ** Wind : ** Line-up allowance TXX : ** Line-up allowance ASD : ** Obstacles (height and distance : ** from end of TORA) : ** : ** : ** : ** : ** : ** the maximum permissible weight at the start of TORA shall be not less than a guaranteed value of **.
