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7.5 For measurements which can only be derived from recordings, the accuracy and resolution of the recording equipment shall be included in calculating the expected measurement uncertainty (1508).
7.6 When modifications are made which will affect the uncertainty of measurement of any parameter, new calculations shall be submitted (1509).
7.7 Temperature Stability
7.7.1 The uncertainties stated in section 3 shall be maintained under the specified environmental conditions for a flight inspection procedure (1510). The operator shall define the environmental conditions (temperature range, humidity range, etc.) (1511).
7.7.2 Details of measurement uncertainty with respect to temperature shall be available for all the measuring equipment (1512). This may be in the form of test results made by the operator, or manufacturer’s specifications. If manufacturer’s specifications are quoted, the proposer shall be prepared to produce manufacturer’s test results as evidence (1513).
7.7.3 If the measuring equipment requires any warm-up or cooling time, this shall be clearly indicated in the operating instructions (1514).
NOTE: If necessary, any temperature dependent apparatus may be fitted in a temperature controlled enclosure. An indicator/alarm shall be fitted to inform the navigation aid inspector of any error in temperature (1515).
7.8 Position Marking of Flight Inspection Data
The accuracy of marking shall be commensurate with the accuracy required in the final figure (1516). Specific requirements are given in paragraph 7.2 of the appropriate annex to FLI 02.
8 Inspection Procedures and Standards
8.1 Safety Objective
All measuring equipment used for flight inspection shall be calibrated to defined standards (1517).
8.2 Clearly defined inspection procedures shall be applied to all equipment involved in the measurement of parameters in paragraph 6 of the appropriate annex of FLI 02 (1518). All equipment and standards used in the inspection process shall have traceability to national or international standards (1519).
8.3 When any equipment used is claimed to be self calibrating, the internal processes involved shall be clearly defined (1520). This involves showing how the equipment’s internal standard is applied to each of the parameters which it can measure or generate. The internal standard shall have traceability to national or international standards (1521).
8.4 Details of inspection intervals required shall be contained in the inspection records (1522). The proposer shall be prepared to produce evidence in support of the quoted inspection intervals (1523).
9 Software - Refer to SW01
10 Operating Instructions
10.1 Safety Objective
The operating instructions shall ensure that all measurements are made to defined and documented procedures (1524).
10.2 This documentation will include concise details of: a) The flight profile to be used for each individual measurement (1525). b) Pre-flight inspection of measuring equipment (1526).
c) Siting of any necessary ground tracking or position fixing equipment (1527).
d) Scheduled maintenance and inspection of the measuring equipment (1528).
e) Operation of the measuring equipment (1529).
f) Production of the flight inspection report (1530).
g) Certification (1531).
h) The method of calculating any results which are not directly output by the
measuring equipment (1532).
11 Personnel Training and Qualification Requirements
11.1 Safety Objective
All personnel concerned with the flight inspection shall be adequately trained and qualified for their job functions (1533).
11.2 The proposer must show that all personnel concerned with the flight inspection are adequately qualified for their job functions (1534).
11.3 The proposer must be prepared to submit CVs for all personnel directly concerned with the flight inspection, from which each person’s experience and suitability can be determined (1535).
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本文链接地址：CAP 670 Air Traffic Services Safety Requirements 2(58)
