Journey Log requirements
Journey log requirements periods are here:
Example log entries:
https://www.md-ra.com/docs/C18E.pdf
Propeller, 5 years:
At intervals of not more than 5 years, the propeller shall be removed from the aircraft and inspected for corrosion or other defects over its entire surface, including the hub faces and the mounting hole bores. While the propeller is removed, it shall also be checked for correct dimensions.
Tachometers - annually
The accuracy of mechanical drag cup type tachometers, for fixed wing propeller driven aircraft, shall be checked on site annually
Weight and Balance - five years
Except as provided for in an approved fleet empty weight and balance control program, all large aircraft shall be reweighed and an updated report prepared every five years.
Non-stabilized Magnetic Direction Indicators (MDIs) (Compass) - 1 year
(a) Except as provided in (b) and (c), non-stabilized magnetic direction indicators shall be calibrated, and a dated correction card installed for each indicator, at at intervals not exceeding 12 months;
Emergency Locator Transmitters (ELTs) - 1 year (many exceptions)
12. Emergency Locator Transmitters (ELTs)
It's 1, 2 or 5 years depending on type
Altimetry Devices - 24 months (pitot static)
(amended 2007/12/30)
(a) Altimeters and other Altimetry devices installed in aircraft operating under Instrument Flight Rules, or under visual flight rules in Class B and C Airspace or Class C and D Airspace that is designated as "Transponder Airspace" shall be calibrated at intervals not exceeding 24 months
the term "altimetry devices" includes any air data computer, or other barometric device, providing a flight crew station, or an auto pilot, or automatic pressure altitude reporting system, or altitude alerting system with altitude data derived from static pressure.
Air Traffic Control (ATC) Transponders - 24 months
ATC Transponders, including any associated altitude sensing reporting mechanisms, where installed, shall be tested every 24 months, in accordance with Appendix F of Chapter 571 of the Airworthiness Manual.
From Johnny:

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