相关题目
CAC 客舱空气压气机的工作由哪个部件控制？
"Scheduled Servicing" includes internal cleaning, etc. Shall not include lubrication procedures required for the accomplishment of maintenance practices. Reference may be made to supplier documents in lieu of component lubrication.
Instructions are included in "Towing and Taxiing "necessary to taxi the aircraft in normal or abnormal conditions such as adverse weather conditions, etc., for maintenance reasons.
Functional Test: That procedure required to ascertain that a system or unit is functioning in all aspects in accordance with minimum acceptable system or unit design specifications . These tests may require supplemental ground support equipment and should be more specific and detailed than an operational test. It should contain all necessary information to perform proficiency test to maintain system or unit reliability at an acceptable level ,without reference to additional documents.
"No-step" areas or walkways leading to any tank in a wing or hull, with necessary precautions, shall be indicated. On some aircraft, a black point strip shows the NO STEP areas. The position of the English or bilingual markings permits to read them when you go near the aircraft from either the front or the rear.
The Obiectives statement contains the following inforination: (1).The relationship of the CAP to existing inspection programs and the manufacturer’s objectives for the CAP. (2).Optional information including (but not limited to) the rationale utilized to select CAPs - how the CAP requirements were determined (discussions of service history, tests and analyses)
The Preface contains the following information: (l) The reasons for establishing the CAP program and the underlying problems to be prevented by compliance with the specific CAP. (2) The relationship of the CAP to normal inspection programs for the airplane.
The Mooring section shall include equipment and materials required such as wheel chocks, mooring blocks, mooring cables, ect.;procedures such as ballasting, etc.;precautions and limitations such as control in high wind conditions, etc., and inspections for gust damage.
SIGNIFICANT INSPECTION CONDITION (detectable crack size, wear limits, corrosion condition, ctc.) specifies, for a crack inspection, the minimum size crack expected to be discovered. Specifies, for other inspection conditions, the wear limits, corrosion pit depth. etc.
Chapter 26 is entitled "Fire Protection", and is about those fixed and portable units and components which detect and indicate fire or smoke, and store and distribute fire extinguishing agent to all protected areas of the aircraft, including bottle, valves, tubing, etc., if furnished as manufacturer designated standard equipment.
