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.
MISSION GUARANTEES. Mission Payload [*CTR*] The A321 Aircraft will be capable of carrying a Payload of not less than Nominal: [*CTR*] Tolerance: [*CTR*] Guarantee: [*CTR*] [*CTR*]
MISSION GUARANTEES. The Original A320 Aircraft will be capable of carrying a guaranteed payload of not less than ** over a still air stage distance of ** when operated under the conditions defined below:
MISSION GUARANTEES. 3.1 Mission Payload [*CTR] The A319 NEO Aircraft will be capable of carrying a Payload of not less than [*CTR]
3.1.1 The departure airport conditions are such as to allow the required Take-Off Weight to be used without restriction. Pressure altitude is [*CTR] at departure airport. The destination airport conditions are such as to allow the required Landing Weight to be used without restriction. Pressure altitude is [*CTR] at destination airport.
3.1.2 An allowance of [*CTR]
3.1.3 An allowance of [*CTR]
3.1.4 [*CTR]
3.1.5 An allowance of [*CTR]
3.1.6 An allowance of [*CTR]
3.1.7 Stage distance is defined as the distance [*CTR] Block fuel is defined as the fuel [*CTR]
3.1.8 At the end of approach and landing [*CTR] of fuel will remain in the tanks. This represents the estimated fuel required for:
a) [*CTR]
b) [*CTR]
c) [*CTR]
d) [*CTR]
e) [*CTR] [*CTR]=[CONFIDENTIAL PORTION OMITTED AND FILED SEPARATELY WITH THE COMMISSION PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT]
3.2 Mission Payload [*CTR] The A319 NEO Aircraft will be capable of carrying a Payload of not less than [*CTR]
3.2.1 The departure airport conditions [*CTR] are as follows: Pressure altitude : [*CTR] Temperature : [*CTR] Take-Off Run Available (TORA) : [*CTR] Take-Off Distance Available (TODA) : [*CTR] Accelerate-Stop Distance Available (ASDA) : [*CTR] Slope : [*CTR] Wind : [*CTR] Obstacle : [*CTR] (height and distance from beginning of TORA) The destination airport conditions are such as to allow the required Landing Weight to be used without restriction. Pressure altitude is [*CTR] at destination airport.
3.2.2 An allowance of [*CTR]
3.2.3 An allowance of [*CTR]
3.2.4 [*CTR]
3.2.5 An allowance of [*CTR]
3.2.6 An allowance of [*CTR]
3.2.7 Stage distance is defined as the distance [*CTR] Block fuel is defined as the fuel [*CTR]
3.2.8 At the end of approach and landing [*CTR] of fuel will remain in the tanks. This represents the estimated fuel required for:
a) [*CTR]
b) [*CTR]
c) [*CTR]
d) [*CTR]
e) [*CTR]
MISSION GUARANTEES. The A330-300 Aircraft will be capable of carrying a payload of not less than the guarantee value over a still air stage distance of 3,653 nautical miles (representative of PHL to FCO with a 28 knots tailwind) when operated under the conditions defined below: Nominal: 101,450 lb Guarantee: ***
MISSION GUARANTEES. Mission Payload [****] The A321 NEO Aircraft will be capable of carrying a Payload of not less than [****]
MISSION GUARANTEES. 3.2 Mission fuel burn: ** **
3.3 Mission Payload: ** ** ** Confidential Treatment Requested. USA — Amended and Restated Airbus A350 XWB Purchase Agreement EXECUTION LA 8-1.A — 6 of 21 PRIVILEGED AND CONFIDENTIAL
3.4 Mission fuel burn: **
3.5 Mission Payload: **
3.5.3 3.5.4 **
MISSION GUARANTEES. The New A321 (CFM Powered) Aircraft will be capable of carrying a guaranteed payload of not less than ** over a still air stage distance of **when operated under the conditions defined below:
MISSION GUARANTEES. 2.1 The New A321 (IAE Powered) Aircraft will be capable of carrying a guaranteed payload of not less than ** over a still air stage distance of **when operated under the conditions defined below:
2.1.1 The departure airport conditions are as described in paragraph 1.1.
MISSION GUARANTEES. The A319 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:
