Engine Takeoff. Thrust Rating at return: pounds per FAA type certificate data sheet
Engine Takeoff Sample Clauses
Related to Engine Takeoff
Aircraft Basic Price The Aircraft Basic Price is listed in Table 1 and is subject to escalation in accordance with the terms of this Purchase Agreement.
Airframe The Airbus A300F4-605R aircraft (excluding the Engines or engines from time to time installed thereon) to be leased by the Lessor to the Lessee pursuant to the Lease and the initial Lease Supplement and having the United States FAA Registration Number initially and manufacturer's serial number specified in the initial Lease Supplement, including (i) all Parts in respect thereof and (ii) any Replacement Airframe which may be substituted pursuant to Section 11.03
Aircraft The Airframe to be sold by AVSA to the Owner Trustee as provided in the Participation Agreement and to be leased under the Lease (or any permitted substitute airframe thereunder) together with two Engines (whether either is an initial Engine or a Replacement Engine) whether or not any of such initial or Replacement Engines may from time to time be installed on such Airframe or may be installed on any other airframe or on any other aircraft, including any aircraft substituted pursuant to Section 11.03
Engines POSITION SERIAL NO. TOTAL HOURS TOTAL CYCLES HRS/CYCLES SINCE LAST SHOP VISIT Time Remaining to Next LIFE LIMITED PART REMOVAL PART NAME HOURS CYCLES MSN MSN
AIRCRAFT CONFIGURATION The guarantees defined in Paragraphs 2 and 3 below (the “Guarantees”) are applicable to the A321 Aircraft as described in the A321 Standard Specification ***** as amended by the following SCNs:
Climb cruise and descent performance associated with the Guarantees will include allowances for normal electrical load and for normal engine air bleed and power extraction associated with maximum cabin differential pressure as defined in Section 21-30.31 of the Specification. Cabin air conditioning management during performance demonstration as described in Subparagraph 5.3 below may be such as to optimize the Aircraft performance while meeting the minimum air conditioning requirements defined above. Unless otherwise stated no air will be bled from the engines for anti-icing.
Aircraft Description The Option Aircraft are described by Boeing Detail Specification D6-38808, Revision E, dated September 15, 1995, as amended and revised pursuant to the Agreement.
Aircraft Documents The following documentation and information is part of the Aircraft, and is the property of the Lessor. The documentation shall be in English, complete, current, accurate and include the latest revisions, in good condition, readable and capable of being reproduced using standard reproduction processes. All documentation shall have the necessary stamps, endorsements, certifications and signatures where appropriate. Bulk storage media (microfilm, CD, DVD) shall be in an industry standard format, requiring no proprietary or “fee added” software to access. One set of any such bulk storage media or one set of paper documentation shall be provided. All records listed in this Exhibit B shall be provided notwithstanding any policies of the Aviation Authority or the Reference Regulatory Agency that may allow the disposal of such records.
Spares Boeing will revise, as applicable, the customized Recommended Spares Parts List (RSPL) and Illustrated Parts Catalog (IPC).
Cockpit (a) Fairing panels shall be free of stains and cracks, will be clean secure and repainted as necessary;
