565
Federal Aviation Administration, DOT
§ 27.1585
contents if the complexity of the man-
ual indicates a need for it.
(Secs. 313(a), 601, 603, 604, and 605 of the Fed-
eral Aviation Act of 1958 (49 U.S.C. 1354(a),
1421, 1423, 1424, and 1425); and sec. 6(c) of the
Dept. of Transportation Act (49 U.S.C.
1655(c)))
[Amdt. 27–14, 43 FR 2325, Jan. 16, 1978]
§ 27.1583
Operating limitations.
(a)
Airspeed and rotor limitations.
In-
formation necessary for the marking of
airspeed and rotor limitations on, or
near, their respective indicators must
be furnished. The significance of each
limitation and of the color coding must
be explained.
(b)
Powerplant limitations.
The fol-
lowing information must be furnished:
(1) Limitations required by § 27.1521.
(2) Explanation of the limitations,
when appropriate.
(3) Information necessary for mark-
ing the instruments required by
§§ 27.1549 through 27.1553.
(c)
Weight and loading distribution.
The weight and center of gravity limits
required by §§ 27.25 and 27.27, respec-
tively, must be furnished. If the vari-
ety of possible loading conditions war-
rants, instructions must be included to
allow ready observance of the limita-
tions.
(d)
Flight crew.
When a flight crew of
more than one is required, the number
and functions of the minimum flight
crew determined under § 27.1523 must be
furnished.
(e)
Kinds of operation.
Each kind of
operation for which the rotorcraft and
its equipment installations are ap-
proved must be listed.
(f) [Reserved]
(g)
Altitude.
The altitude established
under § 27.1527 and an explanation of
the limiting factors must be furnished.
(Secs. 313(a), 601, 603, 604, and 605 of the Fed-
eral Aviation Act of 1958 (49 U.S.C. 1354(a),
1421, 1423, 1424, and 1425); and sec. 6(c) of the
Dept. of Transportation Act (49 U.S.C.
1655(c)))
[Doc. No. 5074, 29 FR 15695, Nov. 24, 1964, as
amended by Amdt. 27–2, 33 FR 965, Jan. 26,
1968; Amdt. 27–14, 43 FR 2325, Jan. 16, 1978;
Amdt. 27–16, 43 FR 50599, Oct. 30, 1978]
§ 27.1585
Operating procedures.
(a) Parts of the manual containing
operating procedures must have infor-
mation concerning any normal and
emergency procedures and other infor-
mation necessary for safe operation,
including takeoff and landing proce-
dures and associated airspeeds. The
manual must contain any pertinent in-
formation including—
(1) The kind of takeoff surface used
in the tests and each appropriate
climbout speed; and
(2) The kind of landing surface used
in the tests and appropriate approach
and glide airspeeds.
(b) For multiengine rotorcraft, infor-
mation identifying each operating con-
dition in which the fuel system inde-
pendence prescribed in § 27.953 is nec-
essary for safety must be furnished, to-
gether with instructions for placing
the fuel system in a configuration used
to show compliance with that section.
(c) For helicopters for which a V
NE
(power-off) is established under
§ 27.1505(c), information must be fur-
nished to explain the V
NE
(power-off)
and the procedures for reducing air-
speed to not more than the V
NE
(power-
off) following failure of all engines.
(d) For each rotorcraft showing com-
pliance with § 27.1353 (g)(2) or (g)(3), the
operating procedures for disconnecting
the battery from its charging source
must be furnished.
(e) If the unusable fuel supply in any
tank exceeds five percent of the tank
capacity, or one gallon, whichever is
greater, information must be furnished
which indicates that when the fuel
quantity indicator reads ‘‘zero’’ in
level flight, any fuel remaining in the
fuel tank cannot be used safely in
flight.
(f) Information on the total quantity
of usable fuel for each fuel tank must
be furnished.
(g) The airspeeds and rotor speeds for
minimum rate of descent and best glide
angle as prescribed in § 27.71 must be
provided.
(Secs. 313(a), 601, 603, 604, and 605 of the Fed-
eral Aviation Act of 1958 (49 U.S.C. 1354(a),
1421, 1423, 1424, and 1425); and sec. 6(c) of the
Dept. of Transportation Act (49 U.S.C.
1655(c)))
[Amdt. 27–1, 32 FR 6914, May 5, 1967, as
amended by Amdt. 27–14, 43 FR 2326, Jan. 16,
1978; Amdt. 27–16, 43 FR 50599, Oct. 30, 1978;
Amdt. 27–21, 49 FR 44435, Nov. 6, 1984]
VerDate Sep<11>2014
12:50 Apr 30, 2019
Jkt 247046
PO 00000
Frm 00575
Fmt 8010
Sfmt 8010
Y:\SGML\247046.XXX
247046
spaschal on DSK3GDR082PROD with CFR