PROPULSION SYSTEMS PRICE REVISION FORMULA. The Reference Price of the Propulsion Systems will be revised to the actual delivery date of the Aircraft on which such Propulsion Systems are installed in accordance with the revision formula set forth in, as applicable, Exhibit "H-1" or Exhibit "H-2" hereto, unless otherwise provided in this Agreement.
PROPULSION SYSTEMS PRICE REVISION FORMULA. CFM INTERNATIONAL *[Four pages have been omitted in accordance with a request for confidential treatment.] AVA - A320 Family PA AMENDED AND RESTATED
PROPULSION SYSTEMS PRICE REVISION FORMULA. (A) CFM INTERNATIONAL
PROPULSION SYSTEMS PRICE REVISION FORMULA. INTERNATIONAL AERO ENGINES * [Three pages have been omitted in accordance with a request for confidential treatment.] EXHIBIT C
PROPULSION SYSTEMS PRICE REVISION FORMULA. XXXXX AND XXXXXXX * [Four pages have been omitted in accordance with a request for confidential treatment.] EXHIBIT D
PROPULSION SYSTEMS PRICE REVISION FORMULA. INTERNATIONAL AERO ENGINES
PROPULSION SYSTEMS PRICE REVISION FORMULA. The Base Price of the Propulsion Systems (excluding the engine configuration option and the nacelles and thrust reversers, when applicable) shall be revised to the month of delivery of the Aircraft on which the Propulsion Systems are installed in accordance with the revision formula set forth in Exhibit "H" or Exhibit "I" (as applicable) hereto.
PROPULSION SYSTEMS PRICE REVISION FORMULA. CFM Price Revision Formula
PROPULSION SYSTEMS PRICE REVISION FORMULA. IAE Price Revision Formula 1 Reference Price of the Propulsion Systems The Reference Price for a set of two (2) INTERNATIONAL AERO ENGINES V2500 series Engines is: IAE V2524-A5: US$ [***] IAE V2527-A5: US$ [***] This Reference Price is subject to adjustment for changes in economic conditions as measured by data obtained from the US Department of Labor, Bureau of Labor Statistics, and in accordance with the provisions hereof.
PROPULSION SYSTEMS PRICE REVISION FORMULA. The Reference Price of the Propulsion Systems shall be revised to the actual delivery date of the Aircraft on which such Propulsion Systems are installed in accordance with the revision formula set forth in Exhibit E hereto.
