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4.2.9  Details of the aircraft which the applicant wishes to use for flight inspection.
4.2.10  Functional description, technical specification and manufacturer’s type number for all major items of the flight inspection system. This shall include details of the equipment used for calibrating the system.
4.2.11  Location, characteristic and type of all measurement aerials on the aircraft.
4.2.12  Technical description of any parts of the system which the applicant has designed or built.
4.2.13  The design authority for all equipment shall be stated.
4.2.14  Procedures for inspection of equipment.
4.2.15  Details of all uses of software and firmware in the measurement system. Also details of software and firmware support.
4.2.16  Details of a log or record system for faults and maintenance of the measuring system.
4.2.17  Spares holding and control.
4.2.18  Documentation Control. List of documents held and produced.
4.2.19  Personnel training, competency and recency checking arrangements.
4.2.20  Details of any internal and external auditing system e.g. auditing of the organisation by any other organisation not associated with the production of inspection results.
4.2.21  Details of the quality management system.
4.2.22  Details of the history of the organisation.
4.2.23  Details of any formal or implicit approvals which the applicant has received from other Aviation Authorities.
4.2.24  A list of any navigation aids which the applicant regularly inspects under such a formal or implicit approval. This will include: a) Type of navigation aid.
b) Location of navigation aid.
c) Category of navigation aid (if applicable).

4.2.25  Flight inspection operating instructions for the inspector and flight crew.
4.2.26  A typical or test flight inspection report.
4.2.27  A typical or test sample structure measurement for those navigational aids where structure measurements form part of a normal flight inspection.
4.2.28  A statement showing to 95% confidence, the measurement uncertainty which the applicant claims to achieve for each of the measurable parameters.
4.2.29  Details of statistical methods or interpolative techniques which may be applied.
4.2.30  Details of AOC (Air Operator’s Certificate) related approvals held in respect of aircraft operations.
4.2.31  Procedures for the control of sub-contractors.
4.2.32  A statement of compliance with the flight inspection requirements of the CAA.
5  Aircraft
5.1  Safety Objective
The aircraft used shall be appropriate for the purpose of flight inspection and shall be operated in a way which ensures accurate measurement of all parameters (1483).
5.2  The aircraft shall be a multi-engine type capable of safe flight within the intended operational envelope with one engine inoperative, fully equipped and instrumented for night and instrument flight (1484).
5.3  Aircraft conducting Flight Inspection must carry a flight crew adequate in number and description to ensure the safety of the aircraft.
5.4  A cross-wind limit shall be set which will allow measurement accuracies to be within the limits required (1486). This limit shall be shown in the operating instructions (1487).
5.5  The aircraft shall have a stable electrical system with sufficient capacity to operate the additional electronic and recording equipment (1488).
5.6  Measures shall be taken to reduce propeller modulation to an acceptably low level (1489).
NOTE:  As the aircraft may be required to fly abnormal procedures during an inspection, it is normal practice to add markings and/or lights which will increase the visibility of the aircraft against all normal backgrounds.
6  Equipment
　
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本文鏈接地址：CAP 670 Air Traffic Services Safety Requirements 2(56)