238
14 CFR Ch. I (1–1–24 Edition)
§ 121.641
for 30 minutes at normal cruising fuel
consumption for day VFR operations.
[Doc. No. 6258, 29 FR 19222, Dec. 31, 1964, as
amended by Amdt. 121–251, 60 FR 65935, Dec.
20, 1995]
§ 121.641 Fuel supply: Nonturbine and
turbo-propeller-powered airplanes:
Flag operations.
(a) No person may dispatch or take
off a nonturbine or turbo-propeller-
powered airplane unless, considering
the wind and other weather conditions
expected, it has enough fuel—
(1) To fly to and land at the airport
to which it is dispatched;
(2) Thereafter, to fly to and land at
the most distant alternate airport
specified in the dispatch release; and
(3) Thereafter, to fly for 30 minutes
plus 15 percent of the total time re-
quired to fly at normal cruising fuel
consumption to the airports specified
in paragraphs (a) (1) and (2) of this sec-
tion or to fly for 90 minutes at normal
cruising fuel consumption, whichever
is less.
(b) No person may dispatch a nontur-
bine or turbo-propeller-powered air-
plane to an airport for which an alter-
nate is not specified under
§ 121.621(a)(2), unless it has enough fuel,
considering wind and forecast weather
conditions, to fly to that airport and
thereafter to fly for three hours at nor-
mal cruising fuel consumption.
§ 121.643 Fuel supply: Nonturbine and
turbo-propeller-powered airplanes:
Supplemental operations.
(a) Except as provided in paragraph
(b) of this section, no person may re-
lease for flight or takeoff a nonturbine
or turbo-propeller-powered airplane un-
less, considering the wind and other
weather conditions expected, it has
enough fuel—
(1) To fly to and land at the airport
to which it is released;
(2) Thereafter, to fly to and land at
the most distant alternate airport
specified in the flight release; and
(3) Thereafter, to fly for 45 minutes
at normal cruising fuel consumption
or, for certificate holders who are au-
thorized to conduct day VFR oper-
ations in their operations specifica-
tions and who are operating non-
transport category airplanes type cer-
tificated after December 31, 1964, to fly
for 30 minutes at normal cruising fuel
consumption for day VFR operations.
(b) If the airplane is released for any
flight other than from one point in the
contiguous United States to another
point in the contiguous United States,
it must carry enough fuel to meet the
requirements of paragraphs (a) (1) and
(2) of this section and thereafter fly for
30 minutes plus 15 percent of the total
time required to fly at normal cruising
fuel consumption to the airports speci-
fied in paragraphs (a) (1) and (2) of this
section, or to fly for 90 minutes at nor-
mal cruising fuel consumption, which-
ever is less.
(c) No person may release a nontur-
bine or turbo-propeller-powered air-
plane to an airport for which an alter-
nate is not specified under § 121.623(b),
unless it has enough fuel, considering
wind and other weather conditions ex-
pected, to fly to that airport and there-
after to fly for three hours at normal
cruising fuel consumption.
[Doc. No. 6258, 29 FR 19222, Dec. 31, 1964, as
amended by Amdt. 121–10, 30 FR 10025, Aug.
12, 1965; Amdt. 121–251, 60 FR 65935, Dec. 20,
1995]
§ 121.645 Fuel supply: Turbine-engine
powered airplanes, other than
turbo propeller: Flag and supple-
mental operations.
(a) Any flag operation within the 48
contiguous United States and the Dis-
trict of Columbia may use the fuel re-
quirements of § 121.639.
(b) For any certificate holder con-
ducting flag or supplemental oper-
ations outside the 48 contiguous United
States and the District of Columbia,
unless authorized by the Administrator
in the operations specifications, no per-
son may release for flight or takeoff a
turbine-engine powered airplane (other
than a turbo-propeller powered air-
plane) unless, considering wind and
other weather conditions expected, it
has enough fuel—
(1) To fly to and land at the airport
to which it is released;
(2) After that, to fly for a period of 10
percent of the total time required to
fly from the airport of departure to,
and land at, the airport to which it was
released;
239
Federal Aviation Administration, DOT
§ 121.646
(3) After that, to fly to and land at
the most distant alternate airport
specified in the flight release, if an al-
ternate is required; and
(4) After that, to fly for 30 minutes at
holding speed at 1,500 feet above the al-
ternate airport (or the destination air-
port if no alternate is required) under
standard temperature conditions.
(c) No person may release a turbine-
engine powered airplane (other than a
turbo-propeller airplane) to an airport
for which an alternate is not specified
under § 121.621(a)(2) or § 121.623(b) unless
it has enough fuel, considering wind
and other weather conditions expected,
to fly to that airport and thereafter to
fly for at least two hours at normal
cruising fuel consumption.
(d) The Administrator may amend
the operations specifications of a cer-
tificate holder conducting flag or sup-
plemental operations to require more
fuel than any of the minimums stated
in paragraph (a) or (b) of this section if
he finds that additional fuel is nec-
essary on a particular route in the in-
terest of safety.
(e) For a supplemental operation
within the 48 contiguous States and
the District of Columbia with a turbine
engine powered airplane the fuel re-
quirements of § 121.643 apply.
[Doc. No. 6258, 29 FR 19222, Dec. 31, 1964, as
amended by Amdt. 121–10, 30 FR 10025, Aug.
12, 1965; Amdt. 121–144, 43 FR 22649, May 25,
1978; Amdt. 121–253, 61 FR 2615, Jan. 26, 1996]
§ 121.646 En-route fuel supply: flag and
supplemental operations.
(a) No person may dispatch or release
for flight a turbine-engine powered air-
plane with more than two engines for a
flight more than 90 minutes (with all
engines operating at cruise power)
from an Adequate Airport unless the
following fuel supply requirements are
met:
(1) The airplane has enough fuel to
meet the requirements of § 121.645(b);
(2) The airplane has enough fuel to
fly to the Adequate Airport—
(i) Assuming a rapid decompression
at the most critical point;
(ii) Assuming a descent to a safe alti-
tude in compliance with the oxygen
supply requirements of § 121.333; and
(iii) Considering expected wind and
other weather conditions.
(3) The airplane has enough fuel to
hold for 15 minutes at 1500 feet above
field elevation and conduct a normal
approach and landing.
(b) No person may dispatch or release
for flight an ETOPS flight unless, con-
sidering wind and other weather condi-
tions expected, it has the fuel other-
wise required by this part and enough
fuel to satisfy each of the following re-
quirements:
(1) Fuel to fly to an ETOPS Alternate
Airport.
(i) Fuel to account for rapid decom-
pression and engine failure. The air-
plane must carry the greater of the fol-
lowing amounts of fuel:
(A) Fuel sufficient to fly to an
ETOPS Alternate Airport assuming a
rapid decompression at the most crit-
ical point followed by descent to a safe
altitude in compliance with the oxygen
supply requirements of § 121.333 of this
chapter;
(B) Fuel sufficient to fly to an
ETOPS Alternate Airport (at the one-
engine-inoperative cruise speed) as-
suming a rapid decompression and a si-
multaneous engine failure at the most
critical point followed by descent to a
safe altitude in compliance with the
oxygen requirements of § 121.333 of this
chapter; or
(C) Fuel sufficient to fly to an
ETOPS Alternate Airport (at the one
engine inoperative cruise speed) assum-
ing an engine failure at the most crit-
ical point followed by descent to the
one engine inoperative cruise altitude.
(ii) Fuel to account for errors in wind
forecasting. In calculating the amount
of fuel required by paragraph (b)(1)(i) of
this section, the certificate holder
must increase the actual forecast wind
speed by 5% (resulting in an increase in
headwind or a decrease in tailwind) to
account for any potential errors in
wind forecasting. If a certificate holder
is not using the actual forecast wind
based on a wind model accepted by the
FAA, the airplane must carry addi-
tional fuel equal to 5% of the fuel re-
quired for paragraph (b)(1)(i) of this
section, as reserve fuel to allow for er-
rors in wind data.
(iii) Fuel to account for icing. In cal-
culating the amount of fuel required by
paragraph (b)(1)(i) of this section (after
completing the wind calculation in