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14 CFR Ch. I (1–1–14 Edition)
§ 23.1587
protect against the occurrence, as a re-
sult of gusts, of structural damage to
the airplane and loss of control (for ex-
ample, stalling);
(4) Procedures for restarting any tur-
bine engine in flight, including the ef-
fects of altitude; and
(5) Procedures, speeds, and configura-
tion(s) for making a normal approach
and landing, in accordance with §§ 23.73
and 23.75, and a transition to the
balked landing condition.
(6) For seaplanes and amphibians,
water handling procedures and the
demonstrated wave height.
(b) In addition to paragraph (a) of
this section, for all single-engine air-
planes, the procedures, speeds, and con-
figuration(s) for a glide following en-
gine failure, in accordance with § 23.71
and the subsequent forced landing,
must be furnished.
(c) In addition to paragraph (a) of
this section, for all multiengine air-
planes, the following information must
be furnished:
(1) Procedures, speeds, and configura-
tion(s) for making an approach and
landing with one engine inoperative;
(2) Procedures, speeds, and configura-
tion(s) for making a balked landing
with one engine inoperative and the
conditions under which a balked land-
ing can be performed safely, or a warn-
ing against attempting a balked land-
ing;
(3) The V
SSE
determined in § 23.149;
and
(4) Procedures for restarting any en-
gine in flight including the effects of
altitude.
(d) In addition to paragraphs (a) and
either (b) or (c) of this section, as ap-
propriate, for all normal, utility, and
acrobatic category airplanes, the fol-
lowing information must be furnished:
(1) Procedures, speeds, and configura-
tion(s) for making a normal takeoff, in
accordance with § 23.51 (a) and (b), and
§ 23.53 (a) and (b), and the subsequent
climb, in accordance with § 23.65 and
§ 23.69(a).
(2) Procedures for abandoning a take-
off due to engine failure or other cause.
(e) In addition to paragraphs (a), (c),
and (d) of this section, for all normal,
utility, and acrobatic category multi-
engine airplanes, the information must
include the following:
(1) Procedures and speeds for con-
tinuing a takeoff following engine fail-
ure and the conditions under which
takeoff can safely be continued, or a
warning against attempting to con-
tinue the takeoff.
(2) Procedures, speeds, and configura-
tions for continuing a climb following
engine failure, after takeoff, in accord-
ance with § 23.67, or enroute, in accord-
ance with § 23.69(b).
(f) In addition to paragraphs (a) and
(c) of this section, for normal, utility,
and acrobatic category multiengine
jets weighing over 6,000 pounds, and
commuter category airplanes, the in-
formation must include the following:
(1) Procedures, speeds, and configura-
tion(s) for making a normal takeoff.
(2) Procedures and speeds for car-
rying out an accelerate-stop in accord-
ance with § 23.55.
(3) Procedures and speeds for con-
tinuing a takeoff following engine fail-
ure in accordance with § 23.59(a)(1) and
for following the flight path deter-
mined under § 23.57 and § 23.61(a).
(g) For multiengine airplanes, infor-
mation identifying each operating con-
dition in which the fuel system inde-
pendence prescribed in § 23.953 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.
(h) For each airplane showing com-
pliance with § 23.1353 (g)(2) or (g)(3), the
operating procedures for disconnecting
the battery from its charging source
must be furnished.
(i) Information on the total quantity
of usable fuel for each fuel tank, and
the effect on the usable fuel quantity,
as a result of a failure of any pump,
must be furnished.
(j) Procedures for the safe operation
of the airplane’s systems and equip-
ment, both in normal use and in the
event of malfunction, must be fur-
nished.
[Doc. No. 27807, 61 FR 5194, Feb. 9, 1996, as
amended by Amdt. 23–62, 76 FR 75763, Dec. 2,
2011]
§ 23.1587
Performance information.
Unless otherwise prescribed, perform-
ance information must be provided
over the altitude and temperature
ranges required by § 23.45(b).
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