463
Federal Aviation Administration, DOT
§ 135.177
when current weather reports indicate
that thunderstorms or other poten-
tially hazardous weather conditions
that can be detected with airborne
thunderstorm detection equipment, re-
quired by paragraph (a) or (b) of this
section, may reasonably be expected
along the route to be flown, unless the
airborne thunderstorm detection equip-
ment is in satisfactory operating con-
dition.
(d) If the airborne thunderstorm de-
tection equipment becomes inoperative
en route, the aircraft must be operated
under the instructions and procedures
specified for that event in the manual
required by § 135.21.
(e) This section does not apply to air-
craft used solely within the State of
Hawaii, within the State of Alaska,
within that part of Canada west of lon-
gitude 130 degrees W, between latitude
70 degrees N, and latitude 53 degrees N,
or during any training, test, or ferry
flight.
(f) Without regard to any other provi-
sion of this part, an alternate elec-
trical power supply is not required for
airborne thunderstorm detection equip-
ment.
[Doc. No. 16097, 43 FR 46783, Oct. 10, 1978, as
amended by Amdt. 135–20, 51 FR 40710, Nov. 7,
1986; Amdt. 135–60, 61 FR 2616, Jan. 26, 1996]
§ 135.175 Airborne weather radar
equipment requirements.
(a) No person may operate a large,
transport category aircraft in pas-
senger-carrying operations unless ap-
proved airborne weather radar equip-
ment is installed in the aircraft.
(b) No person may begin a flight
under IFR or night VFR conditions
when current weather reports indicate
that thunderstorms, or other poten-
tially hazardous weather conditions
that can be detected with airborne
weather radar equipment, may reason-
ably be expected along the route to be
flown, unless the airborne weather
radar equipment required by paragraph
(a) of this section is in satisfactory op-
erating condition.
(c) If the airborne weather radar
equipment becomes inoperative en
route, the aircraft must be operated
under the instructions and procedures
specified for that event in the manual
required by § 135.21.
(d) This section does not apply to air-
craft used solely within the State of
Hawaii, within the State of Alaska,
within that part of Canada west of lon-
gitude 130 degrees W, between latitude
70 degrees N, and latitude 53 degrees N,
or during any training, test, or ferry
flight.
(e) Without regard to any other pro-
vision of this part, an alternate elec-
trical power supply is not required for
airborne weather radar equipment.
§ 135.177 Emergency equipment re-
quirements for aircraft having a
passenger seating configuration of
more than 19 passengers.
(a) No person may operate an aircraft
having a passenger seating configura-
tion, excluding any pilot seat, of more
than 19 seats unless it is equipped with
the following emergency equipment:
(1) At least one approved first-aid kit
for treatment of injuries likely to
occur in flight or in a minor accident
that must:
(i) Be readily accessible to crew-
members.
(ii) Be stored securely and kept free
from dust, moisture, and damaging
temperatures.
(iii) Contain at least the following
appropriately maintained contents in
the specified quantities:
Contents
Quantity
Adhesive bandage compresses, 1-inch .................
16
Antiseptic swabs .....................................................
20
Ammonia inhalants .................................................
10
Bandage compresses, 4-inch .................................
8
Triangular bandage compresses, 40-inch ..............
5
Arm splint, noninflatable .........................................
1
Leg splint, noninflatable ..........................................
1
Roller bandage, 4-inch ...........................................
4
Adhesive tape, 1-inch standard roll ........................
2
Bandage scissors ...................................................
1
Protective nonpermeable gloves or equivalent ......
1 pair
(2) A crash axe carried so as to be ac-
cessible to the crew but inaccessible to
passengers during normal operations.
(3) Signs that are visible to all occu-
pants to notify them when smoking is
prohibited and when safety belts must
be fastened. The signs must be con-
structed so that they can be turned on
during any movement of the aircraft
on the surface, for each takeoff or land-
ing, and at other times considered nec-
essary by the pilot in command. ‘‘No
smoking’’ signs shall be turned on
when required by § 135.127.