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.
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.;
Corrosion. (a) 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. (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
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;
Corrosion. (a) The Aircraft will have been inspected and treated with respect to corrosion as defined in the Agreed Maintenance Program;
Corrosion. Lessee shall have maintained corrosion control through its approved maintenance program as required;
Corrosion. Test Reference number Description of parts tested Description of results:
Corrosion. (1) The Aircraft will have been inspected and treated with respect to corrosion as defined in FAA Advisory Circular AC43-4A, Corrosion Control for Aircraft. Reference 1900C Structural Repair Manual for repairs.
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.
