Mission Block Fuel. The block fuel for a stage length of 2,050 nautical miles in still air (representative of a route with a 4.4 hour flight time from a sea level airport) with a zero fuel weight of 154,221 kilograms, using the conditions and operating rules defined below, shall not be more than the following guarantee value: NOMINAL: [*] Kilograms TOLERANCE: [*] Kilograms GUARANTEE: [*] Kilograms Conditions and operating rules:
Mission Block Fuel. The block fuel for a stage length of [*CTR] pound payload using the conditions and operating rules defined below, shall not be more than the following guarantee value: [*CTR] Conditions and operating rules: Stage Length: The stage length is defined as the sum of the distances for the climbout maneuver, climb, cruise, and descent.
Mission Block Fuel. The block fuel for a stage length of 4,315 nautical miles in still air (equivalent to a distance of 3,750 nautical miles with a 66 knot headwind, representative of an Hong Kong to Bahrain route) with a 260,000 pound payload using the conditions and operating rules defined below, shall not be more than the following guarantee value: 77 Attachment to Letter Agreement No. 6-1162-DSF-082 CF6-80C2BIF Engines Page 13 NOMINAL: [ ] TOLERANCE: [ ] GUARANTEE: [ ]
Mission Block Fuel. The block fuel for a stage length of [*CTR] pound payload using the conditions and operating rules defined below, shall not be more than the following guarantee value: [*CTR] Conditions and operating rules:
Mission Block Fuel. In carrying a fixed payload of [*CTR*] of the A319 NEO Aircraft will be not more than CT1001520_LA11C_AAL_A320Family_EXECUTION LA11C - 4 of 10 Nominal: [*CTR*] Tolerance: [*CTR*] Guarantee: [*CTR*] when the A319 NEO Aircraft is operated as defined here below.
Mission Block Fuel. The block fuel for a stage length of [***] nautical miles in still air (equivalent to a distance of [***] nautical miles with a 33 knot headwind, representative of a [***] route) with a 24,480 kilogram payload (including tare) using the conditions and operating rules defined below, shall not be more than the following guarantee value: NOMINAL: [***] TOLERANCE: [***] GUARANTEE: [***]
Mission Block Fuel. The block fuel for a stage length of *** nautical miles in still air with a *** pound payload using the conditions and operating rules defined below, shall not be more than the following guarantee value: NOMINAL: *** Pounds TOLERANCE: *** Pounds GUARANTEE: *** Pounds BOEING / UNITED AIR LINES, INC. PROPRIETARY P.A. No. 03784 AERO-B-BBA4-M12-0320C SS12-0153 Attachment to Letter Agreement No. UAL-PA-03784-LA-1207868 *** Conditions and operating rules:
Mission Block Fuel. The block fuel for a stage length of [***************] in still air with a [***************] using the conditions and operating rules defined below, shall not be more than the following guarantee value: NOMINAL: [***************] TOLERANCE: [***************] GUARANTEE: [***************] “[***]” This information is subject to confidential treatment and has been omitted and filed separately with the commission BOEING PROPRIETARY Conditions and operating rules:
Mission Block Fuel. In carrying a fixed payload of [****] of the A321 NEO Aircraft will be not more than Nominal: [****] Tolerance: [****] Guarantee: [****] when the A321 NEO Aircraft is operated as defined here below.
Mission Block Fuel. The block fuel for a stage length of [****] pound payload using the conditions and operating rules defined below, shall not be more than the following guarantee value: [****][****][****] Conditions and operating rules: Stage Length: The stage length is defined as the sum of the distances for the climbout maneuver, climb, cruise, and descent. P.A. No. 3219 SA-6 AERO-B-BBA4-M12-0713A SS12-0343 BOEING PROPRIETARY Attachment to Letter Agreement No. AAL-PA-3219-LA-08837R1 [****] Block Fuel: The block fuel is defined as the sum of the fuel used for taxi-out, takeoff and climbout maneuver, climb, cruise, descent, approach and landing maneuver, and taxi-in. Takeoff: [****] The takeoff gross weight is not limited by the airport conditions. Maximum takeoff thrust is used for the takeoff. The takeoff gross weight shall conform to FAA Regulations. Climbout Maneuver: [****] Climb: [****] [****] [****] [****] [****] [****] Cruise: [****] [****] [****] [****] [****] Descent: [****] [****] P.A. No. 3219 SA-6 AERO-B-BBA4-M12-0713A SS12-0343 BOEING PROPRIETARY Attachment to Letter Agreement Xx. XXX-XX-0000-XX-00000X0 [****] Page 7 [****] Approach and Landing Maneuver: [****] [****] Fixed Allowances: For the purpose of this guarantee and for the purpose of establishing compliance with this guarantee, the following shall be used as fixed quantities and allowances: Taxi-Out: [****] Takeoff and Climbout Maneuver: [****] [****] Approach and Landing Maneuver: [****] Taxi-In (shall be consumed from the reserve fuel): [****] Usable reserve fuel remaining upon completion of the approach and landing maneuver: [****] [****]
