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Old 26th April 2013 | 15:39
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rick1128
 
Joined: Jul 2000
Posts: 409
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From: Toledo, OH
Keepitup

It sounds more like Subpart E of Part 91. That includes the Transponder check and the Altimeter check. Here in the states they are referred to as the 91.411 check for the altimeter and the 91.413 check for the transponder.
Unless the helicopters are being operated under IFR, there is no requirement for the altimeter check.

§ 91.413 ATC transponder tests and inspections.

(a) No persons may use an ATC transponder that is specified in 91.215(a), 121.345(c), or § 135.143(c) of this chapter unless, within the preceding 24 calendar months, the ATC transponder has been tested and inspected and found to comply with appendix F of part 43 of this chapter; and

(b) Following any installation or maintenance on an ATC transponder where data correspondence error could be introduced, the integrated system has been tested, inspected, and found to comply with paragraph (c), appendix E, of part 43 of this chapter.

(c) The tests and inspections specified in this section must be conducted by—

(1) A certificated repair station properly equipped to perform those functions and holding—

(i) A radio rating, Class III;

(ii) A limited radio rating appropriate to the make and model transponder to be tested;

(iii) A limited rating appropriate to the test to be performed;


At least here in the US, you only need to find a radio shop, as they do have the equipment required.

Part 43 Appendix E refers to altimeter checks that are required every 24 calendar months for aircraft operated under IFR.

Appendix E to Part 43—Altimeter System Test and Inspection

Each person performing the altimeter system tests and inspections required by § 91.411 shall comply with the following:

(a) Static pressure system:

(1) Ensure freedom from entrapped moisture and restrictions.

(2) Determine that leakage is within the tolerances established in § 23.1325 or § 25.1325, whichever is applicable.

(3) Determine that the static port heater, if installed, is operative.

(4) Ensure that no alterations or deformations of the airframe surface have been made that would affect the relationship between air pressure in the static pressure system and true ambient static air pressure for any flight condition.


It goes further to lay out standards.

Last edited by rick1128; 26th April 2013 at 16:03.
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