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Annex 6, Part 11, 6.1.3: two fire extinguishers in the passenger compartment of aircraft accommodating
30 or more passengers; a crash ax for aeroplanes accommodating more than 19 passengers; a portable
megaphone for aeroplanes seating more than 60 but less than 100 passengers; and two megaphones for
aeroplanes with a seating capacity of more than 100 passengers.
The United States does not require all aeroplanes to be equipped with: a first-aid kit; portable fire
extinguishers; seat or berth for each person; current and suitable air navigation charts; or spare electrical
fuses for VFR day operations.
"Recommended Practice
30/9/02
6.1.3.1.2* The United States does not require aeroplanes on all flights to be equipped with ground-air slgnal codes
for search and rescue purposes.
6.1.3.1.3* The United States requires all aeroplanes manufactured after 12 December 1986 to be equipped with a
shoulder harness for all crew member seats, in addition to the seat belt. For small civil aeroplanes
manufactured after 18 July 1978, a shoulder harness and seat belt are required for the front seats only.
An accurate timepiece is not required for VFR flight.
The United States does not requirc aeroplanes on VFR flights, when operated as controlled flights, to be
equipped in accordance to the requirements for aircraft operated under instrument flight rules.
The United States does not require all seaplanes on all flights to be equipped with one life jacket or
equivalent individual flotation device for each person on board; equipment for making the sound signals
prescribed in the International Regulations for Preventing Collisions at Sea; and anchor; or a sea anchor
(drogue).
Life jackets or equivalent flotation devices are not required for singlc-engined aeroplanes flying over
water beyond gliding distance from shore unless flying for hire, in which case this equipment and
pyrotechnic devices are required.
Only large and turbine-powered multi-engine aeroplanes are required to cany life preservers or an
approved flotation means for each occupant of an aeroplane on a flight over water more than 50 NM
(93 km) from the nearest shore.
Only large and turbine-powered multi-engine aeroplanes on flights over water more than 30 minutes flying
time or 100 NM (1 85 km) from the nearest shore must be equipped wilh life-saving rafs and pyrotechnic
signalling devices.
Aeroplanes operated over land areas designated as areas in which search and rcscue would be especially
difficult are not required to be equipped with signaling devices or lifesaving equipment. The United
States does not designate areas in which search and rescue would be especially difficult, and therefore
does not require such additional equipment.
6.6 d), h), i) The United States does not require all aeroplanes when operated in accordance with instrument flight rules
andj) or when the aeroplane cannot be maintained in a desired altitude without reference to one or more flight
instruments, to be equipped with:
a) an airspeed indicating system with a means of preventing malfunctioning due to a condensation or
icing;
b) a means of indicating whether the supply of power to the gyroscopic instruments is adequate;
c) an outside air temperature indicator: or
d) a rate-of-climb and descent indicator.
"Recommended Practice
6.7 a) and c) Aeroplanes operated under visual flight rules at night are not required to be equipped with:
to 0
a) a turn and slip indicator;
b) an attitude indicator (artificial horizon);
c) heading indicator (directional gyroscope);
d) a means of indicating whether the supply of power to the gyroscopic instruments is adequate;
e) a senskive pressure altimeter;
f) a means of indicating the outside air temperature;
g) a timepiece with a sweep second hand;
h) an airspeed indicating system with a means of preventing malfunctioning due to condensation or
icing;
i) a rate-of-climb and descent indicator;
j) a landing light;
k) illumination for flight instruments and equipment;
1) lights in passenger compartments; and
m) a flashlight (electric torch) for each crew rncmber station.
Ground proximity warning systems are not required on general aviation aircraft, including turbine-engined
aeroplanes with a take-off weight greater than 5 700 kg or capable of carrying more than nine passengers.
The United Statcs does not base requirements for flight data recorders on aircraft weight, but on passcngcr
and engine configuration.
The United States does not base requirements for cockpit voice recorders on aircraft weight, but on
passenger and engine contiguration.
The United States does not have a specific regulation that requires operational chccks and evaluations of
　
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