Common use of GUARANTEE COMPLIANCE Clause in Contracts

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. 5.1. 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. 5.2 Compliance with the take-off, second segment, en-route one engine inoperative, approach segment and landing elements of the Guarantees will be demonstrated with reference to the JAA approved Flight Manual. For demonstration of take-off performance the optimal procedure may be used.CES – A321 – 2010 Private & Confidential 5.3. 5.3 Compliance with those parts of the guarantees Guarantees defined in paragraphs paragraph 2 above 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 ’s discretion) A319A321-100 Aircraft 200 aircraft of the same aerodynamic configuration as those the Aircraft purchased by the Buyer and incorporated in the In-Flight Performance Program and data basis bases (“the IFP”) appropriate to the A319-100 Aircraft. 5.4. 5.4 Compliance with the Manufacturer’s Weight Empty guarantees defined in Paragraph 3 shall be demonstrated with reference to a Weight Compliance Report. 5.5 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. 5.5. 5.6 Compliance with the Guarantees is not contingent on engine performance defined in the engine manufacturer's ’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. 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 ’s Aircraft.

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 inoperative 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 paragraph 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 aircraft of the same aerodynamic configuration as those Aircraft purchased by the Buyer and incorporated in the In-Flight Performance Program and data basis bases (“"the IFP”") appropriate to the A319-100 Aircraft.. 5.4. Compliance with the Manufacturer's Weight Empty guarantee defined in paragraph 3 shall be demonstrated with reference to a weight compliance report. 5.45.5. 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. 5.55.6. 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. 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 inoperative 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 paragraph 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) A319A320-100 Aircraft 200 aircraft of the same aerodynamic configuration as those Aircraft purchased by the Buyer and incorporated in the In-Flight Performance Program and data basis bases (“"the IFP”") appropriate to the A319-100 Aircraft.. 5.4. Compliance with the Manufacturer's Weight Empty guarantee defined in paragraph 3 shall be demonstrated with reference to a weight compliance report. 5.45.5. 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. 5.55.6. 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 A319A320-100 200 Aircraft.

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 inoperative 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 paragraph 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) A319A330-100 Aircraft 200 aircraft of the same aerodynamic configuration as those Aircraft purchased by the Buyer and incorporated in the In-Flight Performance Program and data basis bases (“"the IFP”") appropriate to the A319-100 Aircraft.. 5.4. Compliance with the Manufacturer's Weight Empty guarantee defined in paragraph 3 shall be demonstrated with reference to a weight compliance report. 5.45.5. 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. 5.55.6. 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 A319A330-100 200 Aircraft.

GUARANTEE COMPLIANCE. 5.1. 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. 5.2 Compliance with the take-off, second segment, en-route one engine inoperative, approach segment and landing elements of the Guarantees will be demonstrated with reference to the JAA approved Flight Manual. For demonstration of take-off performance the optimal procedure may be used.CES – A320 – 2010 Private & Confidential 5.3. 5.3 Compliance with those parts of the guarantees Guarantees defined in paragraphs paragraph 2 above 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 ’s discretion) A319A320-100 Aircraft 200 aircraft of the same aerodynamic configuration as those the Aircraft purchased by the Buyer and incorporated in the In-Flight Performance Program and data basis bases (“the IFP”) appropriate to the A319-100 Aircraft. 5.4. 5.4 Compliance with the Manufacturer’s Weight Empty guarantees defined in Paragraph 3 shall be demonstrated with reference to a Weight Compliance Report. 5.5 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. 5.5. 5.6 Compliance with the Guarantees is not contingent on engine performance defined in the engine manufacturer's ’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. 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 ’s Aircraft.

GUARANTEE COMPLIANCE. 5.1. 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. 5.2 Compliance with the take-off, second segment, en-route one engine inoperative, approach segment and landing elements of the Guarantees will be demonstrated with reference to the JAA approved Flight Manual. For demonstration of take-off performance the optimal procedure may be used. 5.3. 5.3 Compliance with those parts of the guarantees Guarantees defined in paragraphs paragraph 2 above 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) A319A330-100 Aircraft 300 aircraft of the same aerodynamic configuration as those the Aircraft purchased by the Buyer and incorporated in the In-Flight Performance Program and data basis bases (“"the IFP”") appropriate to the A319-100 Aircraft. 5.4. 5.4 Compliance with the Manufacturer's Weight Empty guarantees defined in Paragraph 3 shall be demonstrated with reference to a Weight Compliance Report. 5.5 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. 5.5. 5.6 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. 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. 5.1. 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. 5.2 Compliance with the take-off, second segment, en-route one engine inoperative, approach segment and landing elements of the Guarantees will be demonstrated with reference to the JAA approved Flight Manual. For demonstration of take-off performance the optimal procedure may be used.CT1001939 Private & Confidential 5.3. 5.3 Compliance with those parts of the guarantees Guarantees defined in paragraphs 2 Clause above 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) A319A320-100 Aircraft 200 aircraft of the same aerodynamic configuration as those the Aircraft purchased by the Buyer and incorporated in the In-Flight Performance Program and data basis (“the IFP”) bases appropriate to the A319-100 Aircraft. 5.4. 5.4 Compliance with the Manufacturer's Weight Empty guarantee defined in Clause 3 shall be demonstrated with reference to a Weight Compliance Report. 5.5 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. 5.5. 5.6 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. 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 ’s Aircraft.

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 inoperative 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.CT1102624 APPENDIX 1 - GE Private & Confidential 5.3. Compliance with those parts of the guarantees defined in paragraphs Clause 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) A319A330-100 Aircraft 300 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”) bases appropriate to the A319-100 Aircraft.. 5.4. Compliance with the Manufacturer's Weight Empty guarantee defined in Clause 3 shall be demonstrated with reference to a weight compliance report. 5.45.5. 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. 5.55.6. 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 A319A330-100 300 Aircraft.

GUARANTEE COMPLIANCE. 5.1. 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. 5.2 Compliance with the take-off, second segment, en-route one engine inoperative, approach segment and landing elements of the Guarantees will be demonstrated with reference to the JAA approved Flight Manual. For demonstration of take-off performance the optimal procedure may be used. 5.3. 5.3 Compliance with those parts of the guarantees Guarantees defined in paragraphs paragraph 2 above 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) A319A320-100 Aircraft 200 aircraft of the same aerodynamic configuration as those the A320 Aircraft purchased by the Buyer and incorporated in the In-Flight Performance Program and data basis bases (“"the IFP”") appropriate to the A319-100 A320 Aircraft. 5.4. 5.4 Compliance with the Manufacturer's Weight Empty guarantees defined in Paragraph 3 shall be demonstrated with reference to a Weight Compliance Report. 5.5 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. 5.5. 5.6 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. 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.A320

GUARANTEE COMPLIANCE. 5.1. 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. 5.2 Compliance with the take-off, second segment, en-route one engine inoperative, approach segment and landing elements of the Guarantees will be demonstrated with reference to the JAA approved Flight Manual. For demonstration of take-off performance the optimal procedure may be used. 5.3. 5.3 Compliance with those parts of the guarantees Guarantees defined in paragraphs paragraph 2 above 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) A319A330-100 Aircraft 200 aircraft of the same aerodynamic configuration as those the Aircraft purchased by the Buyer and incorporated in the In-Flight Performance Program and data basis bases (“"the IFP”") appropriate to the A319-100 Aircraft. 5.4. 5.4 Compliance with the Manufacturer's Weight Empty guarantees defined in Paragraph 3 shall be demonstrated with reference to a Weight Compliance Report. 5.5 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. 5.5. 5.6 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. 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. 5.1. 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. 5.2 Compliance with the take-off, second segment, en-route one engine inoperative, approach segment and landing elements of the Guarantees will be demonstrated with reference to the JAA approved Flight Manual. For demonstration of take-off performance the optimal procedure may be used. 5.3. 5.3 Compliance with those parts of the guarantees Guarantees defined in paragraphs paragraph 2 above 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 ’s discretion) A319A321-100 Aircraft 200 aircraft of the same aerodynamic configuration as those the Aircraft purchased by the Buyer and incorporated in the In-Flight Performance Program and data basis bases (“the IFP”) appropriate to the A319-100 Aircraft. 5.4. 5.4 Compliance with the Manufacturer’s Weight Empty guarantees defined in Paragraph 3 shall be demonstrated with reference to a Weight Compliance Report. 5.5 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. 5.5. 5.6 Compliance with the Guarantees is not contingent on engine performance defined in the engine manufacturer's ’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. 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 ’s Aircraft.

GUARANTEE COMPLIANCE. 5.1. 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. 5.2 Compliance with the take-off, second segment, en-route one engine inoperative, approach segment and landing elements of the Guarantees will be demonstrated with reference to the JAA approved Flight Manual. For demonstration of take-off performance the optimal procedure may be used. 5.3. 5.3 Compliance with those parts of the guarantees Guarantees defined in paragraphs paragraph 2 above 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 aircraft of the same aerodynamic configuration as those the Aircraft purchased by the Buyer and incorporated in the In-Flight Performance Program and data basis bases (“"the IFP”") appropriate to the A319-100 Aircraft. 5.4. 5.4 Compliance with the Manufacturer's Weight Empty guarantees defined in Paragraph 3 shall be demonstrated with reference to a Weight Compliance Report. 5.5 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. 5.5. 5.6 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. 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. 5.1. 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. 5.2 Compliance with the take-off, second segment, en-route one engine inoperative, approach segment and landing elements of the Guarantees will be demonstrated with reference to the JAA approved Flight Manual. For demonstration of take-off performance the optimal procedure may be used.CT1001939 Private & Confidential 5.3. 5.3 Compliance with those parts of the guarantees Guarantees defined in paragraphs Clause 2 above 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) A319A321-100 Aircraft 200 aircraft of the same aerodynamic configuration as those the Aircraft purchased by the Buyer and incorporated in the In-Flight Performance Program and data basis (“the IFP”) bases appropriate to the A319-100 Aircraft. 5.4. 5.4 Compliance with the Manufacturer's Weight Empty guarantee defined in Clause 3 shall be demonstrated with reference to a Weight Compliance Report. 5.5 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. 5.5. 5.6 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. 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 ’s Aircraft.

GUARANTEE COMPLIANCE. 5.1. 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. 5.2 Compliance with the take-off, second segment, en-route one engine inoperative, approach segment and landing elements of the Guarantees will be demonstrated with reference to the JAA approved Flight Manual. For demonstration of take-off performance the optimal procedure may be used. 5.3. 5.3 Compliance with those parts of the guarantees Guarantees defined in paragraphs paragraph 2 above 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 ’s discretion) A319-100 Aircraft aircraft of the same aerodynamic configuration as those the Aircraft purchased by the Buyer and incorporated in the In-Flight Performance Program and data basis bases (“the IFP”) appropriate to the A319-100 Aircraft. 5.4. 5.4 Compliance with the Manufacturer’s Weight Empty guarantees defined in Paragraph 3 shall be demonstrated with reference to a Weight Compliance Report. 5.5 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. 5.5. 5.6 Compliance with the Guarantees is not contingent on engine performance defined in the engine manufacturer's ’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. 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 ’s Aircraft.

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 inoperative 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 Clause 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) A319A330-100 Aircraft 300 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”) bases appropriate to the A319-100 Aircraft.. 5.4. Compliance with the Manufacturer's Weight Empty guarantee defined in Clause 3 shall be demonstrated with reference to a weight compliance report. 5.45.5. 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. 5.55.6. 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 A319A330-100 300 Aircraft.

GUARANTEE COMPLIANCE. 5.1. 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. 5.2 Compliance with the take-off, second segment, en-route one engine inoperative, approach segment and landing elements of the Guarantees will be demonstrated with reference to the JAA approved Flight Manual. For demonstration of take-off performance the optimal procedure may be used. 5.3. 5.3 Compliance with those parts of the guarantees Guarantees defined in paragraphs paragraph 2 above 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) A319A321-100 Aircraft 200 aircraft of the same aerodynamic configuration as those the Aircraft purchased by the Buyer and incorporated in the In-Flight Performance Program and data basis bases (“"the IFP”") appropriate to the A319-100 Aircraft. 5.4. 5.4 Compliance with the Manufacturer's Weight Empty guarantees defined in Paragraph 3 shall be demonstrated with reference to a Weight Compliance Report. 5.5 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. 5.5. 5.6 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. 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. 5.1. 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. 5.2 Compliance with the take-off, second segment, en-route one engine inoperative, approach segment and landing elements of the Guarantees will be demonstrated with reference to the JAA approved Flight Manual. For demonstration of take-off performance the optimal procedure may be used. 5.3. 5.3 Compliance with those parts of the guarantees Guarantees defined in paragraphs paragraph 2 above 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, more at the Seller's discretion) A319A330-100 Aircraft 200 aircraft of the same aerodynamic configuration as those the Aircraft purchased by the Buyer and incorporated in the In-Flight Performance Program and data basis bases (“"the IFP”") appropriate to the A319-100 Aircraft. 5.4. 5.4 Compliance with the Manufacturer's Weight Empty guarantees defined in Paragraph 3 shall be demonstrated with reference to a Weight Compliance Report. 5.5 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. 5.5. 5.6 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. 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.