Common use of GUARANTEE COMPLIANCE Clause in Contracts

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. 6.1. 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. 6.2 Compliance with the takeoff portion of the mission and landing guarantees shall be based on the FAA approved Airplane Flight Manual for the Model 747737-400 Freighter700. 6.3. 6.3 Compliance with the climb, cruise and descent portions of the mission guarantees range guarantee 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. 6.4 Compliance with the Manufacturer's ’s Empty Weight guarantee shall be based on information in the "“Weight and Balance Control and Loading Manual - Aircraft Report."” 6.6. 6.5 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. 6.6 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 ’s performance specification.

GUARANTEE COMPLIANCE. 6.1. 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. 6.2 Compliance with the takeoff and landing guarantees and the takeoff portion of the mission guarantees guarantee shall be based on the FAA approved Airplane Flight Manual for the Model 747737-400 Freighter800. 6.3. 6.3 Compliance with the speed and cruise fuel mileage guarantees, and the climb, cruise and descent portions of the mission guarantees guarantee 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 specificationSpecification. 6.4. 6.4 The OEW used for compliance with the mission guarantees guarantee shall be the actual MEW plus the Standard and Operational Items Allowance in Paragraph 3-60-0 of the Detail Specification2.5.4. 6.5. 6.5 Compliance with the Manufacturer's ’s Empty Weight guarantee shall be based on information in the "“Weight and Balance Control and Loading Manual - Aircraft Report."” 6.6. 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. 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 ’s performance specification.

GUARANTEE COMPLIANCE. 6.1. 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. 6.2 Compliance with the takeoff portion of the mission and landing guarantees shall be based on the FAA approved Airplane Flight Manual for the Model 747737-400 Freighter800. 6.3. 6.3 Compliance with the climb, cruise and descent portions of the mission guarantees range guarantee 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. 6.4 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. 6.5 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. 6.6 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. 6.1. 5.1 Compliance with the guarantees of Sections Section 2 and 3 shall be based on the conditions specified in those sections, the Aircraft configuration of Section 4 3 and the guarantee conditions of Section 54. 6.2. 5.2 Compliance with the takeoff portion of the mission guarantees guarantee shall be based on the FAA approved Airplane Flight Manual for the Model 747-400 Freighter787‑9. 6.3. 5.3 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 specificationSpecification. 6.4. 5.4 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 03‑60‑00 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. 5.5 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. 5.6 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. * Confidential material omitted and filed separately with the Securities and Exchange Commission pursuant to a request for confidential treatment.

GUARANTEE COMPLIANCE. 6.1. 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. 6.2 Compliance with the enroute one-engine-inoperative altitude, the buffet onset portion of the all-engine altitude capability guarantees, the takeoff portion of the mission guarantee, and the community sound level guarantees shall be based on the FAA approved Airplane Flight Manual for the Model 747787-400 Freighter9. 6.3. 6.3 Compliance with the all-engine altitude capability guarantees, and 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 specificationSpecification. 6.4. 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 303-60-0 00 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. 6.5 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. 6.6 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 ’s performance specification.

GUARANTEE COMPLIANCE. 6.1. 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. 6.2 Compliance with the takeoff portion of the mission and landing guarantees shall be based on the FAA approved Airplane Flight Manual for the Model 747737-400 Freighter.800. Attachment to Letter Agreement No. CEA-PA-4077 LA-1302564 CFM56-7B26E Engines 6.3. 6.3 Compliance with the climb, cruise and descent portions takeoff guarantee shall be shown using an alternate forward center of gravity limit of 15 percent of the mission guarantees mean aerodynamic chord. 6.4 Compliance with the cruise range guarantee 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. 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. 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. 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. 6.1. 5.1 Compliance with the guarantees of Sections Section 2 and 3 shall be based on the conditions specified in those sections, the Aircraft configuration of Section 4 3 and the guarantee conditions of Section 54. 6.2. 5.2 Compliance with the takeoff and landing guarantees and the takeoff portion of the mission guarantees guarantee shall be based on the FAA approved Airplane Flight Manual for the Model 747787-400 Freighter9. 6.3. 5.3 Compliance with the takeoff guarantees and the takeoff portion of the mission guarantee shall be shown using an alternate forward center of gravity limit of 21 percent of the mean aerodynamic chord. 5.4 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 specificationSpecification. 6.4. 5.5 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 Appendix E of the Detail Specification.. Performance Guarantees LA Page 18 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. 5.6 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. 5.7 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. 6.1. 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. 6.2 Compliance with the takeoff and landing guarantees and the takeoff portion of the mission guarantees guarantee shall be based on the FAA approved Airplane Flight Manual for the Model 747777-400 Freighter300ER. 6.3. 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 specificationSpecification. 6.4. 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 303-60-0 00 of the Detail Specification. 6.5. 6.5 Compliance with the Manufacturer's ’s Empty Weight guarantee shall be based on information in the "“Weight and Balance Control and Loading Manual - Aircraft Report."” 6.6. 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. 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 ’s performance specification.

GUARANTEE COMPLIANCE. 6.1. 5.1 Compliance with the guarantees of Sections Section 2 and 3 shall be based on the conditions specified in those sections, the Aircraft configuration of Section 4 3 and the guarantee conditions of Section 54. 6.2. 5.2 Compliance with the takeoff portion of the mission guarantees guarantee shall be based on the FAA approved Airplane Flight Manual for the Model 747737-400 Freighter800. 6.3. 5.3 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 specificationSpecification. 6.4. 5.4 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 Appendix E 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. 5.5 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. 5.6 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 ’s performance specification.

GUARANTEE COMPLIANCE. 6.1. 5.1 Compliance with the guarantees of Sections Section 2 and 3 shall be based on the conditions specified in those sections, the Aircraft configuration of Section 4 3 and the guarantee conditions of Section 54. 6.2. 5.2 Compliance with the takeoff portion of the mission guarantees guarantee shall be based on the FAA approved Airplane Flight Manual for the Model 747-400 Freighter737-***. 6.3. 5.3 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 specificationSpecification. 6.4. 5.4 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 Appendix E 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. 5.5 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. 5.6 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 ’s performance specification.

GUARANTEE COMPLIANCE. 6.1. 5.1 Compliance with the guarantees of Sections Section 2 and 3 shall be based on the conditions specified in those sections, the Aircraft configuration of Section 4 3 and the guarantee conditions of Section 54. 6.2. 5.2 Compliance with the takeoff portion of the mission guarantees guarantee shall be based on the FAA approved Airplane Flight Manual for the Model 747787-400 Freighter.9. * Confidential material omitted and filed separately with the Securities and Exchange Commission pursuant to a request for confidential treatment. AERO-B-BBA4-M13-0372 SS13-0163 Attachment to Letter Agreement No. HAZ-PA-03659-LA-1300864 Trent [*] Engines 6.3. 5.3 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 specificationSpecification. 6.4. 5.4 The OEW used for compliance with the mission guarantees shall be the actual MEW plus the Standard and Operational Items Allowance in Paragraph 303-60-0 00 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. 5.5 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. 5.6 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 ’s performance specification.