675
Federal Aviation Administration, DOT
§ 29.1557
§ 29.1547
Magnetic direction indicator.
(a) A placard meeting the require-
ments of this section must be installed
on or near the magnetic direction indi-
cator.
(b) The placard must show the cali-
bration of the instrument in level
flight with the engines operating.
(c) The placard must state whether
the calibration was made with radio re-
ceivers on or off.
(d) Each calibration reading must be
in terms of magnetic heading in not
more than 45 degree increments.
§ 29.1549
Powerplant instruments.
For each required powerplant instru-
ment, as appropriate to the type of in-
struments—
(a) Each maximum and, if applicable,
minimum safe operating limit must be
marked with a red radial or a red line;
(b) Each normal operating range
must be marked with a green arc or
green line, not extending beyond the
maximum and minimum safe limits;
(c) Each takeoff and precautionary
range must be marked with a yellow
arc or yellow line;
(d) Each engine or propeller range
that is restricted because of excessive
vibration stresses must be marked with
red arcs or red lines; and
(e) Each OEI limit or approved oper-
ating range must be marked to be
clearly differentiated from the mark-
ings of paragraphs (a) through (d) of
this section except that no marking is
normally required for the 30-second
OEI limit.
[Amdt. 29–12, 41 FR 55474, Dec. 20, 1976, as
amended by Amdt. 29–26, 53 FR 34220, Sept. 2,
1988; Amdt. 29–34, 59 FR 47769, Sept. 16, 1994]
§ 29.1551
Oil quantity indicator.
Each oil quantity indicator must be
marked with enough increments to in-
dicate readily and accurately the quan-
tity of oil.
§ 29.1553
Fuel quantity indicator.
If the unusable fuel supply for any
tank exceeds one gallon, or five per-
cent of the tank capacity, whichever is
greater, a red arc must be marked on
its indicator extending from the cali-
brated zero reading to the lowest read-
ing obtainable in level flight.
§ 29.1555
Control markings.
(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 con-
trol must be marked to indicate the po-
sition 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 cor-
responding to each engine controlled.
(c) Usable fuel capacity must be
marked as follows:
(1) For fuel systems having no selec-
tor controls, the usable fuel capacity of
the system must be indicated at the
fuel quantity indicator.
(2) For fuel systems having selector
controls, the usable fuel capacity
available at each selector control posi-
tion must be indicated near the selec-
tor control.
(d) For accessory, auxiliary, and
emergency controls—
(1) Each essential visual position in-
dicator, 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 re-
tractable 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]
§ 29.1557
Miscellaneous markings and
placards.
(a)
Baggage and cargo compartments,
and ballast location.
Each baggage and
cargo compartment, and each ballast
location must have a placard stating
any limitations on contents, including
weight, that are necessary under the
loading requirements.
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