GUARANTEE COMPLIANCE. 5.1. Compliance with the Guarantees shall be demonstrated using operating procedures and limitations in accordance with those defined by the certifying Airworthiness Authority and by the Seller unless otherwise stated.
5.2. Compliance with the take-off, second segment, en-route one engine inoperative, approach and landing elements of the Guarantees will be demonstrated with reference to the approved Flight Manual. For demonstration of take-off performance the optimal procedure may be used.
5.3. Compliance with those parts of the guarantees defined in paragraphs 2 not covered by the requirements of the certifying Airworthiness Authority shall be demonstrated by calculation based on data obtained during flight tests conducted on one (or more, at the Seller's discretion) A319-100 Aircraft of the same aerodynamic configuration as those Aircraft purchased by the Buyer and incorporated in the In-Flight Performance Program and data basis (“the IFP”) appropriate to the A319-100 Aircraft.
5.4. Data derived from tests will be adjusted as required using conventional methods of correction, interpolation or extrapolation in accordance with established aeronautical practices to show compliance with the Guarantees.
5.5. Compliance with the Guarantees is not contingent on engine performance defined in the engine manufacturer's specification.
5.6. Compliance with the Manufacturer's Weight Empty guarantee defined in paragraph 3 shall be demonstrated with reference to a weight compliance report.
5.7. The Seller undertakes to furnish the Buyer with a report or reports demonstrating compliance with the Guarantees at, or as soon as possible after, the delivery of each of the Buyer's A319-100 Aircraft.
GUARANTEE COMPLIANCE. 6.1. Compliance with the guarantees of Sections 2 and 3 shall be based on the conditions specified in those sections, the Aircraft configuration of Section 4 and the guarantee conditions of Section 5.
6.2. Compliance with the takeoff portion of the mission guarantees shall be based on the FAA approved Airplane Flight Manual for the Model 747-400 Freighter.
6.3. Compliance with the climb, cruise and descent portions of the mission guarantees shall be established by calculations based on flight test data obtained from an aircraft in a configuration 4, similar to that defined by the Detail specification.
6.4. The OEW used for compliance with the mission guarantees shall be the actual MEW plus the Standard and Operational Items Allowance in Paragraph 3-60-0 of the Detail Specification.
6.5. Compliance with the Manufacturer's Empty Weight guarantee shall be based on information in the "Weight and Balance Control and Loading Manual Aircraft Report."
6.6. The data derived from tests shall be adjusted as required by conventional methods of correction, interpolation or extrapolation in accordance with established engineering practices to show compliance with these guarantees.
6.7. Compliance shall be based on the performance of the airframe and engines in combination, and shall not be contingent on the engine meeting its manufacturer's performance specification.
GUARANTEE COMPLIANCE. 5.1 Compliance with the Guarantees shall be demonstrated using operating procedures and limitations in accordance with those defined by the certifying Airworthiness Authority and by the Seller unless otherwise stated.
5.2 Compliance with the take-off, second segment, en-route one engine inoperative, approach and landing elements of the Guarantees will be demonstrated with reference to the approved Flight Manual. For demonstration of take-off performance the optimal procedure may be used.
5.3 Compliance with those parts of the guarantees defined in paragraphs 2 not covered by the requirements of the certifying Airworthiness Authority shall be demonstrated by calculation based on data obtained during flight tests conducted on one (or more, at the Seller's discretion) A319-100 Aircraft of the same aerodynamic configuration as those Aircraft purchased by the Buyer and incorporated in the In-Flight Performance Program and data basis (“the IFP”) appropriate to the A319-100 Aircraft.
5.4 Data derived from tests will be adjusted as required using conventional methods of correction, interpolation or extrapolation in accordance with established aeronautical practices to show compliance with the Guarantees.
5.5 Compliance with the Guarantees is not contingent on engine performance defined in the engine manufacturer's specification.
5.6 Compliance with the Manufacturer's Weight Empty guarantee defined in paragraph 3 shall be demonstrated with reference to a weight compliance report.
5.7 The Seller undertakes to furnish the Buyer with a report or reports demonstrating compliance with the Guarantees at, or as soon as possible after, the delivery of each of the Buyer's A319-100 Aircraft.
GUARANTEE COMPLIANCE. Compliance with the guarantees of Section 2 shall be based on the conditions specified in those sections, the Aircraft configuration of Section 3 and the guarantee conditions of Section 4.
GUARANTEE COMPLIANCE. Compliance with the Guarantees shall be demonstrated using operating procedures and limitations in accordance with those defined by the certifying Airworthiness Authority and by the Seller unless otherwise stated.
GUARANTEE COMPLIANCE. 5.1 Compliance with the guarantees of Section 2 shall be based on the conditions specified in that section, the Aircraft configuration of Section 3 and the guarantee conditions of Section 4.
5.2 Compliance with the takeoff and landing guarantees and the takeoff portion of the mission guarantee shall be based on the FAA approved Airplane Flight Manual for the Model 737-8.
GUARANTEE COMPLIANCE. 5.1. Compliance with the Guarantees shall be demonstrated using operating procedures and limitations in accordance with those defined by the certifying Airworthiness Authority and by the Seller unless otherwise stated. *** This information is subject to confidential treatment and has been omitted and filed separately with the Commission.
GUARANTEE COMPLIANCE. 8.1 Compliance with the Guarantees shall be demonstrated using operating procedures and limitations in accordance with those defined by the certifying Airworthiness Authority and by the Seller unless otherwise stated.
8.2 Compliance with the take-off [DELETED]and landing elements of the Guarantees shall be demonstrated with reference to the approved Flight Manual.
8.3 Compliance with those parts of the Guarantees not covered by the requirements of the certifying Airworthiness Authority shall be demonstrated by calculation based on data obtained during flight tests conducted on one (or more, at the Seller's discretion) [DELETED] Aircraft of the same configuration as those Aircraft purchased by the Buyer.
8.4 Compliance with the Manufacturer's Weight Empty Guarantee shall be demonstrated with reference to a weight compliance report. [DELETED]
8.5 Data derived from tests [DELETED]surveys shall be adjusted as required using conventional methods of correction, interpolation or extrapolation in accordance with established aeronautical practices to show compliance with the Guarantees.
8.6 Compliance with the Guarantees is based but not contingent on the engine performance defined in the engine manufacturer's specification.
8.7 The Seller undertakes to furnish the Buyer with a report or reports demonstrating compliance with the Guarantees at, or as soon as possible after, the delivery of each of the Buyer's [DELETED]Aircraft.
GUARANTEE COMPLIANCE. 6.1 Compliance with the Guarantees shall be demonstrated using operating procedures and limitations in accordance with those defined by the FAA and, if not inconsistent with those defined by the FAA, those defined by the Seller.
6.2 Compliance with the take-off, second segment and landing elements of the Guarantees will be demonstrated with reference to the FAA approved Flight Manual.
6.3 Compliance with those parts of the Guarantees not covered by the requirements of the FAA shall be demonstrated by calculation based on data obtained during flight tests conducted on one (or more, at the Seller’s discretion) A319-100 aircraft of the same aerodynamic configuration as the A319 Aircraft.
6.4 Compliance with the Manufacturer’s Weight Empty Guarantee defined in Paragraph 4 shall be demonstrated with reference to a weight compliance report.
6.5 Data derived from tests will be adjusted as required using conventional methods of correction, interpolation or extrapolation in accordance with established aeronautical practices to show compliance with the Guarantees.
6.6 Compliance with the Guarantees is not contingent on engine performance defined in the Propulsion System manufacturer’s specification.
6.7 The Seller undertakes to furnish the Buyer with a report or reports demonstrating compliance with the Guarantees at, or as soon as possible after, the delivery of each of the A319 Aircraft.
GUARANTEE COMPLIANCE. 8.1 Compliance with the Guarantees will be demonstrated using operating procedures and limitations in accordance with those defined by the certifying Airworthiness Authority and by the Seller unless otherwise stated.
8.2 Compliance with the take-off, second segment, en-route one engine inoperative, approach climb and landing elements of the Guarantees will be demonstrated with reference to the approved Flight Manual.
8.3 Compliance with those parts of the Guarantees defined in paragraph 2 and 3 above not covered by the requirements of the certifying Airworthiness Authority will be demonstrated by calculation based on data obtained during flight tests conducted on one (or more, at the Seller’s discretion) aircraft of the same aerodynamic configuration as the Aircraft and incorporated in the In-Flight Performance Program and data bases (“the IFP”) appropriate to the Aircraft.
8.4 Compliance with the Structure Usable Load guarantee defined in Paragraph 4 will be demonstrated with reference to a weight compliance report.
8.5 The approved A350-900 XWB Aircraft flight manual will be used to demonstrate compliance with the guarantees of certification noise levels. ** Confidential Treatment Requested. USA — Amended and Restated Airbus A350 XWB Purchase Agreement LA 8-2.A — 19 of 23 EXECUTION PRIVILEGED AND CONFIDENTIAL
8.6 Compliance with the APU noise and interior noise guarantees will be demonstrated with reference to noise surveys conducted on one (or more, at the Seller’s discretion) A350-900 XWB Aircraft of an acoustically equivalent standard to those A350-900 XWB Aircraft purchased by the Buyer.
8.7 Data derived from flight tests and noise surveys will be adjusted as required using conventional methods of correction, interpolation or extrapolation in accordance with established aeronautical practices to show compliance with the Guarantees.
8.8 Compliance with the Guarantees is not contingent on engine performance defined in the engine manufacturer’s specification.
8.9 The Seller undertakes to furnish the Buyer with a report or reports demonstrating compliance with the Guarantees at, or as soon as possible after, the delivery of each of the A350-900 XWB Aircraft.
