(ii) Squitter: Verify that the Mode S transponder generates a correct squitter approximately once per second.

(iii) Records: Comply with the provisions of Schedule 5 as to content, form, and disposition of the records.

Appendix 3 to 5.105:   VOR Receiver Tests and Inspections
 

(a) Each VOR system of radio navigation used in IFR operations must be;-

(1) maintained, checked, and inspected under an approved procedure; or

(2) has been operationally checked within the preceding 30 days, and was found to be within the limits of the permissible indicated bearing error set forth in paragraph (b) or (c) of this section.

(b) Except as provided in paragraph (c) of this section, each person conducting a VOR   check under paragraph (a)(2) of this section shall -

(1) use, at the airport of intended departure, an approved test signal or a test signal radiated by a certificated and appropriately rated radio approved maintenance organization or, outside Jamaica a test signal operated or approved by an appropriate authority to check the VOR equipment (the maximum permissible indicated bearing error is ±4°); or

(2) use, at the airport of intended departure, a point on the airport surface designated as a VOR system checkpoint by the Authority, or, outside Jamaica, by an appropriate authority (the maximum permissible bearing error is ±4°);

(3) if neither a test signal nor a designated checkpoint on the surface is available, use an airborne checkpoint designated by the Authority or, outside Jamaica, by an appropriate authority (the maximum permissible bearing error is ±6°); or

(4) if no check signal or point is available, while in flight -

(i) a VOR radial that lies along the centerline of an established VOR airway;

(ii)    select a prominent ground point along the selected radial preferably more  than 20 nautical miles from the VOR ground facility and manoeuvre the aircraft directly  over the point at a reasonably low altitude; and

(iii) note the VOR bearing indicated by the receiver when over the ground point (the   maximum permissible variation between the published radial and the indicated  bearing is 6°).

(c) Where dual system VOR (units independent of each other except for the antenna) is installed in the aircraft, the person checking the equipment may check one system against the other in place of the check procedures specified in paragraph (b) of this section. Both systems shall be tuned to the same VOR ground facility and note the indicated bearings to that station. The maximum permissible variation between the two indicated bearings is 4°.

(d) Every person making the VOR operational check, as specified in paragraph (b) or (c) of this section, shall enter the date, place, bearing error, and sign the aircraft log or other record. In addition, if a test signal radiated by an approved maintenance organization, as specified in paragraph (b)(1) of this section, is used, an entry must be made in the aircraft log or other record by the organization’s representative certifying to the bearing transmitted by the approved maintenance organization for the check and the date of transmission.
 
Appendix 1 to 5.165:  Performance Rules – Annual and 100-hour Inspections

(e) Every person performing an annual or 100-hour inspection shall, before that inspection, thoroughly clean the aircraft and aircraft engine and remove or open all necessary inspection plates, access doors, fairings, and cowlings.

(f) Every person performing an annual or 100-hour inspection shall inspect, where applicable, the following components —

(1) fuselage and hull group —

(i) fabric and skin - for deterioration, distortion, other evidence of failure, and 

              defective or insecure attachment of fittings;
　
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：飛機持續適航 CONTINUING AIRWORTHINESS OF AIRCRAFT(23)