Tap any paragraph to write a margin note. Your notes collect in the Desk below the text and file under cases with @. The side-by-side margin rail opens on a larger screen.

Code · CFR · Title 14 — Aeronautics and Space · Part 29 — Airworthiness Standards: Transport Category Rotorcraft · § 29.1555

§ 29.1555. Control markings.

311 words·~1 min read·/us/cfr/t14/s§ 29.1555·

A research copy — for the controlling text, always check the official state or federal source. Not legal advice.

(a)Each cockpit control, other than primary flight controls or control whose function is obvious, must be plainly marked as to its function and method of operation.
(b)For powerplant fuel controls—
(1)Each fuel tank selector valve control must be marked to indicate the position corresponding to each tank and to each existing cross feed position;
(2)If safe operation requires the use of any tanks in a specific sequence, that sequence must be marked on, or adjacent to, the selector for those tanks; and
(3)Each valve control for any engine of a multiengine rotorcraft must be marked to indicate the position corresponding to each engine controlled.
(c)Usable fuel capacity must be marked as follows:
(1)For fuel systems having no selector controls, the usable fuel capacity of the system must be indicated at the fuel quantity indicator unless it is:
(i)Provided by another system or equipment readily accessible to the pilot; and
(ii)Contained in the limitations section of the rotorcraft flight manual.
(2)For fuel systems having selector controls, the usable fuel capacity available at each selector control position must be indicated near the selector control.
(d)For accessory, auxiliary, and emergency controls—
(1)Each essential visual position indicator, such as those showing rotor pitch or landing gear position, must be marked so that each crewmember can determine at any time the position of the unit to which it relates; and
(2)Each emergency control must be red and must be marked as to method of operation.
(e)For rotorcraft incorporating retractable landing gear, the maximum landing gear operating speed must be displayed in clear view of the pilot. [Doc. No. 5084, 29 FR 16150, Dec. 3, 1964, as amended by Amdt. 29-12, 41 FR 55474, Dec. 20, 1976; Amdt. 29-24, 49 FR 44440, Nov. 6, 1984; Amdt. 29-59, 88 FR 8740, Feb. 10, 2023]
Connections1 cite this
Citation graph
cites case law
§ 29.1555
Control markings.
Fed. Reg.×1
Cites 0Cited by 1 across 1 source
★   the supreme law of the land   ★
Don't Tread on Me
E Pluribus Unum — out of many, one

"If you don't know your rights, you don't have any."

Marginalia · a citizen's law index
A research desk, not legal advice. Always read the cited source before relying on a summary.
Questions or an issue? support@self-law.org
disclaimerMarginalia is a research index, not a law firm. Nothing on this site is legal, tax, or financial advice and no attorney–client relationship is formed by using it. Statutes, regulations, and case law change; summaries, search results, AI output, and member posts may be incomplete, out of date, or wrong. Any interpretation drawn from material on this site should be validated by a licensed attorney in your jurisdiction before you act on it.