Corrosion Sample Clauses

Corrosion. 7.1.1.1. The metal items of the Enhanced Child Restraint System shall be positioned in a test chamber as prescribed in Annex 4. In the case of an Enhanced Child Restraint System incorporating a retractor, the strap shall be unwound to full length less 100 ± 3 mm. Except for short interruptions that may be necessary, for example, to check and replenish the salt solution, the exposure test shall proceed continuously for a period of 50 ± 0.5 hours. 7.1.1.2. On completion of the exposure test the metal items of the Enhanced Child Restraint System shall be gently washed, or dipped, in clean running water with a temperature not higher than 38 °C to remove any salt deposit that may have formed and then allowed to dry at room temperature of 18 °C to 25 °C for 24 ± 1 hours before inspection in accordance with paragraph 6.6.1.2. above.

Corrosion. (a) The Aircraft will have been inspected and treated with respect to corrosion as defined in the Agreed Maintenance Programme and/or Boeing Document No.D6-38528 relative to compliance with the Corrosion Prevention and Control Program (CPCP). The entire fuselage will be substantially free from corrosion and will be adequately treated and an approved corrosion prevention programme will be in operation; and (b) Fuel tanks will be free from contamination and corrosion and a tank treatment programme will be in operation. Notwithstanding anything contained in this Schedule 3, Lessor shall not be required to make any payments to Lessee in the event that any or all of the Airframe, the Engines, the Landing Gear, any time, cycle or calendar controlled component is returned to Lessor in a condition better than that specified in Clause 12 and this Schedule 3.

Corrosion. (a) The Aircraft shall be in compliance with the Manufacturer's corrosion prevention and control program (CPCP) requirements. All CPCP inspections which would normally be accomplished while access is provided during structural inspection in accordance with the Lessee's Maintenance Program during the Term shall have been accomplished; (b) The entire fuselage will be substantially free from corrosion and will be adequately treated in accordance with Lessee's corrosion prevention program and the Manufacturer's Maintenance Planning Document; and (c) Fuel tanks will be free from contamination and corrosion and a tank treatment program will be in operation.

Corrosion. (a) Entire fuselage shall be substantially free from corrosion and shall be adequately treated and an approved corrosion prevention program shall be in operation; (b) Fuel tanks shall be free from contamination and corrosion and a tank treatment program shall be in operation. APPENDIX F

Corrosion. The Aircraft will be in compliance with the CPCP and will have been inspected and treated with respect to corrosion as required by the CPCP; and

Corrosion. Lessee shall have maintained corrosion control through its approved maintenance program as required;

Corrosion. (a) The Aircraft shall be in compliance with the Manufacturer’s CPCP document, the CPCP requirements of the Maintenance Planning Document and FAA CPCP airworthiness directive requirements. (b) The entire fuselage will be substantially free from corrosion and all mild and moderate corrosion found will be adequately cleaned and treated and all severe or exfoliated corrosion shall be repaired in accordance with the Manufacturer’s structural repair manual.

Corrosion. (a) The Aircraft shall be in compliance with the Manufacturer's corrosion prevention and control program (CPCP) requirements. All CPCP inspections which would normally be accomplished while access is provided during structural inspection in accordance with Lessee's Maintenance Program during the Term shall have been accomplished.; (b) The entire fuselage will be substantially free from corrosion and will be adequately treated and an approved corrosion prevention program will be in operation; and (c) Fuel tanks will be free from contamination and corrosion and a tank treatment program will be in operation. SCHEDULE 4

Corrosion. Test Reference number Description of parts tested Description of results:

Corrosion. (a) The Aircraft shall be in compliance with the Manufacturer's corrosion prevention and control program (CPCP) requirements as implemented in Lessee's Maintenance Program. All CPCP inspections which would normally be accomplished while access is provided during structural inspection in accordance with the Lessee's Maintenance Program during the Term shall have been accomplished; (b) The entire fuselage will be substantially free from corrosion and will be adequately treated in accordance with Lessee's corrosion prevention program (which shall include the requirements of the Manufacturer's Maintenance Planning Document); and (c) Fuel tanks will be free from contamination and corrosion and a tank treatment program will be in operation.