MISSION GUARANTEES. 2.1 The A320 Aircraft will be capable of carrying a guaranteed payload of not less than *** over a still air stage distance of 2,610 nautical miles (representative of PHL to SFO with a 65 knot headwind) when operated under the conditions defined below: 2.1.1 The departure airport conditions (representative of PHL 09R) are as follows: Pressure altitude : 21 ft Ambient temperature : 84(degrees)F Take-off run available ("TOR") : 10,499 feet Take-off distance available : 10,499 feet Accelerate-stop distance available : 10,499 feet Slope : 0.10% downhill Wind : Zero Obstacles (height and distance : 17 feet/1,090 feet from end of TOR) : 57 feet/4,306 feet : 178 feet/9,500 feet The destination airport conditions are such as to allow the required landing weight to be used without restriction. Pressure altitude is 11 feet. 2.1.2 An allowance of 220 lb of fuel is included for taxi at the departure airport. 2.1.3 An allowance of 520 lb of fuel is included for take-off and climb to 1,500 ft above the departure airport at 84(degrees)F with acceleration to climb speed. 2.1.4 Climb from 1,500 ft above the departure airport up to cruise altitude using maximum climb thrust and cruise at a fixed Mach number of 0.78 at pressure altitudes of 35,000 ft and 39,000 ft and descent to 1,500 ft above the destination airport are conducted in ISA+10(degrees)C conditions. Climb and descent speeds below 10,000 ft will be 250 knots CAS. 2.1.5 An allowance of 180 lb of fuel is included for approach and land at the destination airport. 2.1.6 Stage distance is defined as the distance covered during climb, cruise and descent as described in Subparagraph 2.1.4 above. 2.1.7 At the end of approach and land 7,210 lb of fuel will remain in the tanks. This represents the estimated fuel required for: 1) Missed approach 2) Diversion consisting of climb and cruise in ISA+10(degrees)C conditions over a still air distance of 150 nautical miles starting at 1,500 ft above the destination airport. 3) Holding for 45 minutes at 20,000 ft pressure altitude in ISA+10(degrees)C conditions.
Appears in 1 contract
Samples: Purchase Agreement (Us Airways Inc)
MISSION GUARANTEES. 2.1 The A320 A321 Aircraft will be capable of carrying a guaranteed payload of not less than *** over a still air stage distance of 2,610 nautical miles (representative of PHL to SFO with a 65 knot headwind) when operated under the conditions defined below:
2.1.1 The departure airport conditions (representative of PHL 09R) are as follows: Pressure altitude : 21 ft Ambient temperature : 84(degrees)F 84(degree)F Take-off run available ("TOR") : 10,499 feet Take-off distance available : 10,499 feet Accelerate-stop distance available : 10,499 feet Slope : 0.10% downhill Wind : Zero Obstacles (height and distance : 17 feet/1,090 feet from end of TOR) : 57 feet/4,306 feet : 178 feet/9,500 feet The destination airport conditions are such as to allow the required landing weight to be used without restriction. Pressure altitude is 11 feet.
2.1.2 An allowance of 220 lb of fuel is included for taxi at the departure airport.
2.1.3 An allowance of 520 530 lb of fuel is included for take-off and climb to 1,500 ft above the departure airport at 84(degrees)F 84(degree)F with acceleration to climb speed.
2.1.4 Climb from 1,500 ft above the departure airport up to cruise altitude using maximum climb thrust and cruise at a fixed Mach number of 0.78 at pressure altitudes of 35,000 ft and 39,000 ft and descent to 1,500 ft above the destination airport are conducted in ISA+10(degrees)C ISA+10(degree)C conditions. Climb and descent speeds below 10,000 ft will be 250 knots CAS.
2.1.5 An allowance of 180 230 lb of fuel is included for approach and land at the destination airport.
2.1.6 Stage distance is defined as the distance covered during climb, cruise and descent as described in Subparagraph 2.1.4 above.
2.1.7 At the end of approach and land 7,210 7,370 lb of fuel will remain in the tanks. This represents the estimated fuel required for:
1) Missed approach approach
2) Diversion consisting of climb and cruise in ISA+10(degrees)C ISA+10(degree)C conditions over a still air distance of 150 nautical miles starting at 1,500 ft above the destination airport. .
3) Holding for 45 minutes at 20,000 ft pressure altitude in ISA+10(degrees)C ISA+10(degree)C conditions.
Appears in 1 contract
Samples: Purchase Agreement (Us Airways Inc)
MISSION GUARANTEES. 2.1 The A320 A319 Aircraft will be capable of carrying a guaranteed payload of not less than *** lb over a still air stage distance of 2,610 nautical miles (representative of PHL to SFO with a 65 knot headwind) when operated under the conditions defined below:
2.1.1 The departure airport conditions (representative of PHL 09R) are as follows: Pressure altitude : 21 ft Ambient temperature : 84(degrees)F 84(degree)F Take-off run available ("TOR") : 10,499 feet Take-off distance available : 10,499 feet Accelerate-stop distance available : 10,499 feet Slope : 0.10% downhill Wind : Zero Obstacles (height and distance : 17 feet/1,090 feet from end of TOR) TOR : 57 feet/4,306 feet : 178 feet/9,500 feet The destination airport conditions are such as to allow the required landing weight to be used without restriction. Pressure altitude is 11 feet.
2.1.2 An allowance of 220 lb of fuel is included for taxi at the departure airport.
2.1.3 An allowance of 520 505 lb of fuel is included for take-off and climb to 1,500 ft above the departure airport at 84(degrees)F 84(degree)F with acceleration to climb speed.
2.1.4 Climb from 1,500 ft above the departure airport up to cruise altitude using maximum climb thrust and cruise at a fixed Mach number of 0.78 at pressure altitudes of 35,000 ft and 39,000 ft and descent to 1,500 ft above the destination airport are conducted in ISA+10(degrees)C ISA+10(degree)C conditions. Climb and descent speeds below 10,000 ft will be 250 knots CAS.
2.1.5 An allowance of 180 190 lb of fuel is included for approach and land at the destination airport.
2.1.6 Stage distance is defined as the distance covered during climb, cruise and descent as described in Subparagraph 2.1.4 above.
2.1.7 At the end of approach and land 7,210 7,110 lb of fuel will remain in the tanks. This represents the estimated fuel required for:
1) Missed approach approach
2) Diversion consisting of climb and cruise in ISA+10(degrees)C ISA+10(degree)C conditions over a still air distance of 150 nautical miles starting at 1,500 ft above the destination airport. .
3) Holding for 45 minutes at 20,000 ft pressure altitude in ISA+10(degrees)C ISA+10(degree)C conditions.
2.2 The A319 Aircraft will be capable of carrying a guaranteed payload of not less than *** lb over a still air stage distance of 1,545 nautical miles (representative of STT to PHL with a 37 knot headwind) when operated under the conditions defined below:
2.2.1 The departure airport conditions (representative of STT 10) are as follows: Pressure altitude : 24 ft Ambient temperature : 84(degree)F Take-off run available ("TOR") : 7,000 feet Take-off distance available : 7,000 feet Accelerate-stop distance available : 7,000 feet Slope : 0.20% downhill Wind : Zero Obstacle (height and distan : 151 feet/2,083 feet from end of TOR) The destination airport conditions are such as to allow the required landing weight to be used without restriction. Pressure altitude is 21 feet.
2.2.2 An allowance of 220 lb of fuel is included for taxi at the departure airport.
2.2.3 An allowance of 380 lb of fuel is included for take-off and climb to 1,500 ft above the departure airport at 84(degree)F with acceleration to climb speed.
2.2.4 Climb from 1,500 ft above the departure airport up to cruise altitude using maximum climb thrust and cruise at a fixed Mach number of 0.78 at pressure altitudes of 35,000 ft and 39,000 ft and descent to 1,500 ft above the destination airport are conducted in ISA+10(degree)C conditions. Climb and descent speeds below 10,000 ft will be 250 knots CAS.
2.2.5 An allowance of 200 lb of fuel is included for approach and land at the destination airport.
2.2.6 Stage distance is defined as the distance covered during climb, cruise and descent as described in Subparagraph 2.2.4 above.
2.2.7 At the end of approach and land 6,630 lb of fuel will remain in the tanks. This represents the estimated fuel required for:
1) Missed approach
2) Diversion consisting of climb and cruise in ISA+10(degree)C conditions over a still air distance of 150 nautical miles starting at 1,500 ft above the destination airport.
3) Holding for 45 minutes at 20,000 ft pressure altitude in ISA+10(degree)C conditions.
2.3 In carrying a fixed payload of 26,760 lb over a still air stage distance of 2,000 nautical miles when operated under the conditions defined below the Block Fuel will be not more than a guaranteed value of *** lb.
2.3.1 The departure airport conditions are such as to allow the required take-off weight to be used without restriction. The destination airport conditions are such as to allow the required landing weight to be used without restriction.
2.3.2 An allowance of 220 lb of fuel is included for taxi at the departure airport.
2.3.3 An allowance of 430 lb of fuel is included for take-off and climb to 1,500 ft pressure altitude with acceleration to climb speed at a temperature of 84(degree)F.
2.3.4 Climb from 1,500 ft pressure altitude up to cruise altitude using maximum climb thrust and cruise at a fixed Mach number of 0.78 at pressure altitudes of 35,000 ft and 39,000 ft and descent to 1,500 ft pressure altitude are conducted in ISA+10(degree)C conditions. Climb and descent speeds below 10,000 ft will be 250 knots CAS.
2.3.5 An allowance of 200 lb of fuel is included for approach and landing at the destination airport.
2.3.6 An allowance of 70 lb of fuel is included for taxi at the destination airport.
2.3.7 Stage distance is defined as the distance covered during climb, cruise and descent as described in Subparagraph 2.3.4 above.
Appears in 1 contract
Samples: Airbus A319/A320/A321 Purchase Agreement (Us Airways Inc)
MISSION GUARANTEES. 2.1 The A320 A321 Aircraft will be capable of carrying a guaranteed payload of not less than *** over a still air stage distance of 2,610 *** nautical miles (representative of PHL to SFO with a 65 knot headwind) when operated under the conditions defined below:
2.1.1 The departure airport conditions (representative of PHL 09R) are as follows: Pressure altitude : 21 ft Ambient temperature : 84(degrees)F 84(degree)F Take-off run available ("TOR") : 10,499 feet Take-off distance available : 10,499 feet Accelerate-stop distance available : 10,499 feet Slope : 0.10% downhill Wind : Zero Obstacles (height and distance : 17 feet/1,090 feet from end of TOR) : 57 feet/4,306 feet : 178 feet/9,500 feet The destination airport conditions are such as to allow the required landing weight to be used without restriction. Pressure altitude is 11 feet.
2.1.2 An allowance of 220 lb of fuel is included for taxi at the departure airport.
2.1.3 An allowance of 520 530 lb of fuel is included for take-off and climb to 1,500 ft above the departure airport at 84(degrees)F 84(degree)F with acceleration to climb speed.
2.1.4 Climb from 1,500 ft above the departure airport up to cruise altitude using maximum climb thrust and cruise at a fixed Mach number of 0.78 at pressure altitudes of 35,000 ft and 39,000 ft and descent to 1,500 ft above the destination airport are conducted in ISA+10(degrees)C ISA+10(degree)C conditions. Climb and descent speeds below 10,000 ft will be 250 knots CAS.
2.1.5 An allowance of 180 230 lb of fuel is included for approach and land at the destination airport.
2.1.6 Stage distance is defined as the distance covered during climb, cruise and descent as described in Subparagraph 2.1.4 above.
2.1.7 At the end of approach and land 7,210 7,370 lb of fuel will remain in the tanks. This represents the estimated fuel required for:
1) Missed approach approach
2) Diversion consisting of climb and cruise in ISA+10(degrees)C ISA+10(degree)C conditions over a still air distance of 150 nautical miles starting at 1,500 ft above the destination airport. .
3) Holding for 45 minutes at 20,000 ft pressure altitude in ISA+10(degrees)C ISA+10(degree)C conditions.
2.2 The A321 Aircraft will be capable of carrying a guaranteed payload of not less than *** over a still air stage distance of *** nautical miles (representative of STT to PHL with a 37 knot headwind) when operated under the conditions defined below:
2.2.1 The departure airport conditions (representative of STT 10) are as follows: Pressure altitude : 24 ft Ambient temperature : 84(degree)F Take-off run available ("TOR") : 7,000 feet Take-off distance available : 7,000 feet Accelerate-stop distance available : 7,000 feet Slope : 0.20% downhill Wind : Zero Obstacle (height and distance : 151 feet/2,083 feet from end of TOR) The destination airport conditions are such as to allow the required landing weight to be used without restriction. Pressure altitude is 21 feet.
2.2.2 An allowance of 220 lb of fuel is included for taxi at the departure airport.
2.2.3 An allowance of 570 lb of fuel is included for take-off and climb to 1,500 ft above the departure airport at 84(degree)F with acceleration to climb speed.
2.2.4 Climb from 1,500 ft above the departure airport up to cruise altitude using maximum climb thrust and cruise at a fixed Mach number of 0.78 at pressure altitudes of 31,000 ft and 35,000 ft and descent to 1,500 ft above the destination airport are conducted in ISA+10(degree)C conditions. Climb and descent speeds below 10,000 ft will be 250 knots CAS.
2.2.5 An allowance of 270 lb of fuel is included for approach and land at the destination airport.
2.2.6 Stage distance is defined as the distance covered during climb, cruise and descent as described in Subparagraph 2.2.4 above.
2.2.7 At the end of approach and land 7,940 lb of fuel will remain in the tanks. This represents the estimated fuel required for:
1) Missed approach
2) Diversion consisting of climb and cruise in ISA+10(degree)C conditions over a still air distance of 150 nautical miles starting at 1,500 ft above the destination airport.
3) Holding for 45 minutes at 20,000 ft pressure altitude in ISA+10(degree)C conditions.
2.3 In carrying a fixed payload of 37,690 lb over a still air stage distance of 2,000 nautical miles when operated under the conditions defined below the Block Fuel will be not more than a guaranteed value of ***.
2.3.1 The departure airport conditions are such as to allow the required take-off weight to be used without restriction. The destination airport conditions are such as to allow the required landing weight to be used without restriction.
2.3.2 An allowance of 220 lb of fuel is included for taxi at the departure airport.
2.3.3 An allowance of 630 lb of fuel is included for take-off and climb to 1,500 ft pressure altitude with acceleration to climb speed at a temperature of 84(degree)F.
2.3.4 Climb from 1,500 ft pressure altitude up to cruise altitude using maximum climb thrust and cruise at a fixed Mach number of 0.78 at a pressure altitude of 35,000 ft and descent to 1,500 ft pressure altitude are conducted in ISA+10(degree)C conditions. Climb and descent speeds below 10,000 ft will be 250 knots CAS.
2.3.5 An allowance of 260 lb of fuel is included for approach and landing at the destination airport.
2.3.6 An allowance of 70 lb of fuel is included for taxi at the destination airport.
2.3.7 Stage distance is defined as the distance covered during climb, cruise and descent as described in Subparagraph 2.3.4 above.
Appears in 1 contract
Samples: Airbus A319/A320/A321 Purchase Agreement (Us Airways Inc)
MISSION GUARANTEES. 2.1 The A320 Aircraft will be capable of carrying a guaranteed payload of not less than *** over a still air stage distance of 2,610 nautical miles (representative of PHL to SFO with a 65 knot headwind) when operated under the conditions defined below:
2.1.1 The departure airport conditions (representative of PHL 09R) are as follows: Pressure altitude : 21 ft Ambient temperature : 84(degrees)F 84(degree)F Take-off run available ("TOR") : 10,499 feet Take-off distance available : 10,499 feet Accelerate-stop distance available : 10,499 feet Slope : 0.10% downhill Wind : Zero Obstacles (height and distance : 17 feet/1,090 feet from end of TOR) : 57 feet/4,306 feet : 178 feet/9,500 feet The destination airport conditions are such as to allow the required landing weight to be used without restriction. Pressure altitude is 11 feet.
2.1.2 An allowance of 220 lb of fuel is included for taxi at the departure airport.
2.1.3 An allowance of 520 lb of fuel is included for take-off and climb to 1,500 ft above the departure airport at 84(degrees)F 84(degree)F with acceleration to climb speed.
2.1.4 Climb from 1,500 ft above the departure airport up to cruise altitude using maximum climb thrust and cruise at a fixed Mach number of 0.78 at pressure altitudes of 35,000 ft and 39,000 ft and descent to 1,500 ft above the destination airport are conducted in ISA+10(degrees)C ISA+10(degree)C conditions. Climb and descent speeds below 10,000 ft will be 250 knots CAS.
2.1.5 An allowance of 180 lb of fuel is included for approach and land at the destination airport.
2.1.6 Stage distance is defined as the distance covered during climb, cruise and descent as described in Subparagraph 2.1.4 above.
2.1.7 At the end of approach and land 7,210 lb of fuel will remain in the tanks. This represents the estimated fuel required for:
1) Missed approach 2) Diversion consisting of climb and cruise in ISA+10(degrees)C ISA+10(degree)C conditions over a still air distance of 150 nautical miles starting at 1,500 ft above the destination airport. 3) Holding for 45 minutes at 20,000 ft pressure altitude in ISA+10(degrees)C ISA+10(degree)C conditions.
2.2 The A320 Aircraft will be capable of carrying a guaranteed payload of not less than *** lb over a still air stage distance of 1,545 nautical miles (representative of STT to PHL with a 37 knot headwind) when operated under the conditions defined below:
2.2.1 The departure airport conditions (representative of STT 10) are as follows: Pressure altitude : 24 ft Ambient temperature : 84(degree)F Take-off run available ("TOR") : 7,000 feet Take-off distance available : 7,000 feet Accelerate-stop distance available : 7,000 feet Slope : 0.20% downhill Wind : Zero Obstacle (height and distance : 151 feet/2,083 feet from end of TOR) The destination airport conditions are such as to allow the required landing weight to be used without restriction. Pressure altitude is 21 feet.
2.2.2 An allowance of 220 lb of fuel is included for taxi at the departure airport.
2.2.3 An allowance of 410 lb of fuel is included for take-off and climb to 1,500 ft above the departure airport at 84(degree)F with acceleration to climb speed.
2.2.4 Climb from 1,500 ft above the departure airport up to cruise altitude using maximum climb thrust and cruise at a fixed Mach number of 0.78 at a pressure altitude of 35,000 ft and descent to 1,500 ft above the destination airport are conducted in ISA+10(degree)C conditions. Climb and descent speeds below 10,000 ft will be 250 knots CAS.
2.2.5 An allowance of 190 lb of fuel is included for approach and land at the destination airport.
2.2.6 Stage distance is defined as the distance covered during climb, cruise and descent as described in Subparagraph 2.2.4 above.
2.2.7 At the end of approach and land 6,930 lb of fuel will remain in the tanks. This represents the estimated fuel required for:
1) Missed approach 2) Diversion consisting of climb and cruise in ISA+10(degree)C conditions over a still air distance of 150 nautical miles starting at 1,500 ft above the destination airport. 3) Holding for 45 minutes at 20,000 ft pressure altitude in ISA+10(degree)C conditions.
2.3 In carrying a fixed payload of 31,665 lb over a still air stage distance of 2,000 nautical miles when operated under the conditions defined below the Block Fuel will be not more than a guaranteed value of ***.
2.3.1 The departure airport conditions are such as to allow the required take-off weight to be used without restriction. The destination airport conditions are such as to allow the required landing weight to be used without restriction.
2.3.2 An allowance of 220 lb of fuel is included for taxi at the departure airport.
2.3.3 An allowance of 470 lb of fuel is included for take-off and climb to 1,500 ft pressure altitude with acceleration to climb speed at a temperature of 84(degree)F.
2.3.4 Climb from 1,500 ft pressure altitude up to cruise altitude using maximum climb thrust and cruise at a fixed Mach number of 0.78 at a pressure altitude of 35,000 ft and descent to 1,500 ft pressure altitude are conducted in ISA+10(degree)C conditions. Climb and descent speeds below 10,000 ft will be 250 knots CAS.
2.3.5 An allowance of 190 lb of fuel is included for approach and landing at the destination airport.
2.3.6 An allowance of 70 lb of fuel is included for taxi at the destination airport.
2.3.7 Stage distance is defined as the distance covered during climb, cruise and descent as described in Subparagraph 2.3.4 above.
Appears in 1 contract
Samples: Airbus A319/A320/A321 Purchase Agreement (Us Airways Inc)
MISSION GUARANTEES. 2.1 The A320 A319 Aircraft will be capable of carrying a guaranteed payload of not less than *** lb over a still air stage distance of 2,610 nautical miles (representative of PHL to SFO with a 65 knot headwind) when operated under the conditions defined below:
2.1.1 The departure airport conditions (representative of PHL 09R) are as follows: Pressure altitude : 21 ft Ambient temperature : 84(degrees)F 84(degree)F Take-off run available ("TOR") : 10,499 feet Take-off distance available : 10,499 feet Accelerate-stop distance available : 10,499 feet Slope : 0.10% downhill Wind : Zero Obstacles (height and distance : 17 feet/1,090 feet from end of TOR) TOR : 57 feet/4,306 feet : 178 feet/9,500 feet The destination airport conditions are such as to allow the required landing weight to be used without restriction. Pressure altitude is 11 feet.
2.1.2 An allowance of 220 lb of fuel is included for taxi at the departure airport.
2.1.3 An allowance of 520 505 lb of fuel is included for take-off and climb to 1,500 ft above the departure airport at 84(degrees)F 84(degree)F with acceleration to climb speed.
2.1.4 Climb from 1,500 ft above the departure airport up to cruise altitude using maximum climb thrust and cruise at a fixed Mach number of 0.78 at pressure altitudes of 35,000 ft and 39,000 ft and descent to 1,500 ft above the destination airport are conducted in ISA+10(degrees)C ISA+10(degree)C conditions. Climb and descent speeds below 10,000 ft will be 250 knots CAS.
2.1.5 An allowance of 180 190 lb of fuel is included for approach and land at the destination airport.
2.1.6 Stage distance is defined as the distance covered during climb, cruise and descent as described in Subparagraph 2.1.4 above.
2.1.7 At the end of approach and land 7,210 7,110 lb of fuel will remain in the tanks. This represents the estimated fuel required for:
1) Missed approach 2) Diversion consisting of climb and cruise in ISA+10(degrees)C ISA+10(degree)C conditions over a still air distance of 150 nautical miles starting at 1,500 ft above the destination airport. 3) Holding for 45 minutes at 20,000 ft pressure altitude in ISA+10(degrees)C ISA+10(degree)C conditions.
2.2 The A319 Aircraft will be capable of carrying a guaranteed payload of not less than *** lb over a still air stage distance of 1,545 nautical miles (representative of STT to PHL with a 37 knot headwind) when operated under the conditions defined below:
2.2.1 The departure airport conditions (representative of STT 10) are as follows: Pressure altitude : 24 ft Ambient temperature : 84(degree)F Take-off run available ("TOR") : 7,000 feet Take-off distance available : 7,000 feet Accelerate-stop distance available : 7,000 feet Slope : 0.20% downhill Wind : Zero Obstacle (height and distance : 151 feet/2,083 feet from end of TOR) The destination airport conditions are such as to allow the required landing weight to be used without restriction. Pressure altitude is 21 feet.
2.2.2 An allowance of 220 lb of fuel is included for taxi at the departure airport.
2.2.3 An allowance of 380 lb of fuel is included for take-off and climb to 1,500 ft above the departure airport at 84(degree)F with acceleration to climb speed.
2.2.4 Climb from 1,500 ft above the departure airport up to cruise altitude using maximum climb thrust and cruise at a fixed Mach number of 0.78 at pressure altitudes of 35,000 ft and 39,000 ft and descent to 1,500 ft above the destination airport are conducted in ISA+10(degree)C conditions. Climb and descent speeds below 10,000 ft will be 250 knots CAS.
2.2.5 An allowance of 200 lb of fuel is included for approach and land at the destination airport.
2.2.6 Stage distance is defined as the distance covered during climb, cruise and descent as described in Subparagraph 2.2.4 above.
2.2.7 At the end of approach and land 6,630 lb of fuel will remain in the tanks. This represents the estimated fuel required for:
1) Missed approach 2) Diversion consisting of climb and cruise in ISA+10(degree)C conditions over a still air distance of 150 nautical miles starting at 1,500 ft above the destination airport. 3) Holding for 45 minutes at 20,000 ft pressure altitude in ISA+10(degree)C conditions.
2.3 In carrying a fixed payload of 26,760 lb over a still air stage distance of 2,000 nautical miles when operated under the conditions defined below the Block Fuel will be not more than a guaranteed value of *** lb.
2.3.1 The departure airport conditions are such as to allow the required take-off weight to be used without restriction. The destination airport conditions are such as to allow the required landing weight to be used without restriction.
2.3.2 An allowance of 220 lb of fuel is included for taxi at the departure airport.
2.3.3 An allowance of 430 lb of fuel is included for take-off and climb to 1,500 ft pressure altitude with acceleration to climb speed at a temperature of 84(degree)F.
2.3.4 Climb from 1,500 ft pressure altitude up to cruise altitude using maximum climb thrust and cruise at a fixed Mach number of 0.78 at pressure altitudes of 35,000 ft and 39,000 ft and descent to 1,500 ft pressure altitude are conducted in ISA+10(degree)C conditions. Climb and descent speeds below 10,000 ft will be 250 knots CAS.
2.3.5 An allowance of 200 lb of fuel is included for approach and landing at the destination airport.
2.3.6 An allowance of 70 lb of fuel is included for taxi at the destination airport.
2.3.7 Stage distance is defined as the distance covered during climb, cruise and descent as described in Subparagraph 2.3.4 above.
Appears in 1 contract
Samples: Airbus A319/A320/A321 Purchase Agreement (Us Airways Inc)
MISSION GUARANTEES. 2.1 The A320 A321 Aircraft will be capable of carrying a guaranteed payload of not less than *** over a still air stage distance of 2,610 *** nautical miles (representative of PHL to SFO with a 65 knot headwind) when operated under the conditions defined below:
2.1.1 The departure airport conditions (representative of PHL 09R) are as follows: Pressure altitude : 21 ft Ambient temperature : 84(degrees)F 84(degree)F Take-off run available ("TOR") : 10,499 feet Take-off distance available : 10,499 feet Accelerate-stop distance available : 10,499 feet Slope : 0.10% downhill Wind : Zero Obstacles (height and distance : 17 feet/1,090 feet from end of TOR) : 57 feet/4,306 feet : 178 feet/9,500 feet The destination airport conditions are such as to allow the required landing weight to be used without restriction. Pressure altitude is 11 feet.
2.1.2 An allowance of 220 lb of fuel is included for taxi at the departure airport.
2.1.3 An allowance of 520 530 lb of fuel is included for take-off and climb to 1,500 ft above the departure airport at 84(degrees)F 84(degree)F with acceleration to climb speed.
2.1.4 Climb from 1,500 ft above the departure airport up to cruise altitude using maximum climb thrust and cruise at a fixed Mach number of 0.78 at pressure altitudes of 35,000 ft and 39,000 ft and descent to 1,500 ft above the destination airport are conducted in ISA+10(degrees)C ISA+10(degree)C conditions. Climb and descent speeds below 10,000 ft will be 250 knots CAS.
2.1.5 An allowance of 180 230 lb of fuel is included for approach and land at the destination airport.
2.1.6 Stage distance is defined as the distance covered during climb, cruise and descent as described in Subparagraph 2.1.4 above.
2.1.7 At the end of approach and land 7,210 7,370 lb of fuel will remain in the tanks. This represents the estimated fuel required for:
1) Missed approach 2) Diversion consisting of climb and cruise in ISA+10(degrees)C ISA+10(degree)C conditions over a still air distance of 150 nautical miles starting at 1,500 ft above the destination airport. 3) Holding for 45 minutes at 20,000 ft pressure altitude in ISA+10(degrees)C ISA+10(degree)C conditions.
2.2 The A321 Aircraft will be capable of carrying a guaranteed payload of not less than *** over a still air stage distance of *** nautical miles (representative of STT to PHL with a 37 knot headwind) when operated under the conditions defined below:
2.2.1 The departure airport conditions (representative of STT 10) are as follows: Pressure altitude : 24 ft Ambient temperature : 84(degree)F Take-off run available ("TOR") : 7,000 feet Take-off distance available : 7,000 feet Accelerate-stop distance available : 7,000 feet Slope : 0.20% downhill Wind : Zero Obstacle (height and distance : 151 feet/2,083 feet from end of TOR) The destination airport conditions are such as to allow the required landing weight to be used without restriction. Pressure altitude is 21 feet.
2.2.2 An allowance of 220 lb of fuel is included for taxi at the departure airport.
2.2.3 An allowance of 570 lb of fuel is included for take-off and climb to 1,500 ft above the departure airport at 84(degree)F with acceleration to climb speed.
2.2.4 Climb from 1,500 ft above the departure airport up to cruise altitude using maximum climb thrust and cruise at a fixed Mach number of 0.78 at pressure altitudes of 31,000 ft and 35,000 ft and descent to 1,500 ft above the destination airport are conducted in ISA+10(degree)C conditions. Climb and descent speeds below 10,000 ft will be 250 knots CAS.
2.2.5 An allowance of 270 lb of fuel is included for approach and land at the destination airport.
2.2.6 Stage distance is defined as the distance covered during climb, cruise and descent as described in Subparagraph 2.2.4 above.
2.2.7 At the end of approach and land 7,940 lb of fuel will remain in the tanks. This represents the estimated fuel required for:
1) Missed approach 2) Diversion consisting of climb and cruise in ISA+10(degree)C conditions over a still air distance of 150 nautical miles starting at 1,500 ft above the destination airport. 3) Holding for 45 minutes at 20,000 ft pressure altitude in ISA+10(degree)C conditions.
2.3 In carrying a fixed payload of 37,690 lb over a still air stage distance of 2,000 nautical miles when operated under the conditions defined below the Block Fuel will be not more than a guaranteed value of ***.
2.3.1 The departure airport conditions are such as to allow the required take-off weight to be used without restriction. The destination airport conditions are such as to allow the required landing weight to be used without restriction.
2.3.2 An allowance of 220 lb of fuel is included for taxi at the departure airport.
2.3.3 An allowance of 630 lb of fuel is included for take-off and climb to 1,500 ft pressure altitude with acceleration to climb speed at a temperature of 84(degree)F.
2.3.4 Climb from 1,500 ft pressure altitude up to cruise altitude using maximum climb thrust and cruise at a fixed Mach number of 0.78 at a pressure altitude of 35,000 ft and descent to 1,500 ft pressure altitude are conducted in ISA+10(degree)C conditions. Climb and descent speeds below 10,000 ft will be 250 knots CAS.
2.3.5 An allowance of 260 lb of fuel is included for approach and landing at the destination airport.
2.3.6 An allowance of 70 lb of fuel is included for taxi at the destination airport.
2.3.7 Stage distance is defined as the distance covered during climb, cruise and descent as described in Subparagraph 2.3.4 above.
Appears in 1 contract
Samples: Airbus A319/A320/A321 Purchase Agreement (Us Airways Inc)
MISSION GUARANTEES. 2.1 The A320 Aircraft will be capable of carrying a guaranteed payload of not less than *** over a still air stage distance of 2,610 nautical miles (representative of PHL to SFO with a 65 knot headwind) when operated under the conditions defined below:
2.1.1 The departure airport conditions (representative of PHL 09R) are as follows: Pressure altitude : 21 ft Ambient temperature : 84(degrees)F 84(degree)F Take-off run available ("TOR") : 10,499 feet Take-off distance available : 10,499 feet Accelerate-stop distance available : 10,499 feet Slope : 0.10% downhill Wind : Zero Obstacles (height and distance : 17 feet/1,090 feet from end of TOR) : 57 feet/4,306 feet : 178 feet/9,500 feet The destination airport conditions are such as to allow the required landing weight to be used without restriction. Pressure altitude is 11 feet.
2.1.2 An allowance of 220 lb of fuel is included for taxi at the departure airport.
2.1.3 An allowance of 520 lb of fuel is included for take-off and climb to 1,500 ft above the departure airport at 84(degrees)F 84(degree)F with acceleration to climb speed.
2.1.4 Climb from 1,500 ft above the departure airport up to cruise altitude using maximum climb thrust and cruise at a fixed Mach number of 0.78 at pressure altitudes of 35,000 ft and 39,000 ft and descent to 1,500 ft above the destination airport are conducted in ISA+10(degrees)C ISA+10(degree)C conditions. Climb and descent speeds below 10,000 ft will be 250 knots CAS.
2.1.5 An allowance of 180 lb of fuel is included for approach and land at the destination airport.
2.1.6 Stage distance is defined as the distance covered during climb, cruise and descent as described in Subparagraph 2.1.4 above.
2.1.7 At the end of approach and land 7,210 lb of fuel will remain in the tanks. This represents the estimated fuel required for:
1) Missed approach approach
2) Diversion consisting of climb and cruise in ISA+10(degrees)C ISA+10(degree)C conditions over a still air distance of 150 nautical miles starting at 1,500 ft above the destination airport. .
3) Holding for 45 minutes at 20,000 ft pressure altitude in ISA+10(degrees)C ISA+10(degree)C conditions.
2.2 The A320 Aircraft will be capable of carrying a guaranteed payload of not less than *** lb over a still air stage distance of 1,545 nautical miles (representative of STT to PHL with a 37 knot headwind) when operated under the conditions defined below:
2.2.1 The departure airport conditions (representative of STT 10) are as follows: Pressure altitude : 24 ft Ambient temperature : 84(degree)F Take-off run available ("TOR") : 7,000 feet Take-off distance available : 7,000 feet Accelerate-stop distance available : 7,000 feet Slope : 0.20% downhill Wind : Zero Obstacle (height and distance : 151 feet/2,083 feet from end of TOR) The destination airport conditions are such as to allow the required landing weight to be used without restriction. Pressure altitude is 21 feet.
2.2.2 An allowance of 220 lb of fuel is included for taxi at the departure airport.
Appears in 1 contract
Samples: Airbus A319/A320/A321 Purchase Agreement (Us Airways Inc)
MISSION GUARANTEES. 2.1 The A320 Aircraft will be capable of carrying a guaranteed payload of not less than *** over a still air stage distance of 2,610 nautical miles (representative of PHL to SFO with a 65 knot headwind) when operated under the conditions defined below:
2.1.1 The departure airport conditions (representative of PHL 09R) are as follows: Pressure altitude : 21 ft Ambient temperature : 84(degrees)F 84(degree)F Take-off run available ("TOR") : 10,499 feet Take-off distance available : 10,499 feet Accelerate-stop distance available : 10,499 feet Slope : 0.10% downhill Wind : Zero Obstacles (height and distance : 17 feet/1,090 feet from end of TOR) : 57 feet/4,306 feet : 178 feet/9,500 feet The destination airport conditions are such as to allow the required landing weight to be used without restriction. Pressure altitude is 11 feet.
2.1.2 An allowance of 220 lb of fuel is included for taxi at the departure airport.
2.1.3 An allowance of 520 lb of fuel is included for take-off and climb to 1,500 ft above the departure airport at 84(degrees)F 84(degree)F with acceleration to climb speed.
2.1.4 Climb from 1,500 ft above the departure airport up to cruise altitude using maximum climb thrust and cruise at a fixed Mach number of 0.78 at pressure altitudes of 35,000 ft and 39,000 ft and descent to 1,500 ft above the destination airport are conducted in ISA+10(degrees)C ISA+10(degree)C conditions. Climb and descent speeds below 10,000 ft will be 250 knots CAS.
2.1.5 An allowance of 180 lb of fuel is included for approach and land at the destination airport.
2.1.6 Stage distance is defined as the distance covered during climb, cruise and descent as described in Subparagraph 2.1.4 above.
2.1.7 At the end of approach and land 7,210 lb of fuel will remain in the tanks. This represents the estimated fuel required for:
1) Missed approach 2) Diversion consisting of climb and cruise in ISA+10(degrees)C ISA+10(degree)C conditions over a still air distance of 150 nautical miles starting at 1,500 ft above the destination airport. 3) Holding for 45 minutes at 20,000 ft pressure altitude in ISA+10(degrees)C ISA+10(degree)C conditions.
Appears in 1 contract
Samples: Purchase Agreement (Us Airways Inc)
