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category aeroplanes used in air commerce in the United States and a11 United States-registered transport
category aeroplanes used in air commerce outside the United States must use an aural speed warning device.
The United States does not require the design of the aircraft operating manual to observe Human Factors
principles. United States aircraft operating manual design requirements are covered by policy and guidance
material.
Engine power, configuration and operation are not recorded on flight data recorders installed in large
aeroplanes having a United States original type certificate issued on or before 30 September 1969, which
are certificated for operations above 25 000 ft altitude or are turbine-engine powered. Engine operation is
not recorded on flight data recorders installed on large aeroplanes having a United States original type
certificate issued before 30 September 1969, which are certificated for operations above 25 000 ft aItitude
or are turbine-powered.
Neither engine power nor configuration of lift and drag devices are recorded on flight data recorders
installed in large aeroplanes having a United States original type certificate issued on or before
30 September 1969, which are certificated for operations above 25 000 ft altitude or are turbine-engine
powered.
The United States does not require flight data recorders that record the referenced parameters for all aircraft
meeting this weight criterion. When operated by commuter and on-demand operators, multi-engine, turbinepowered
aeroplanes that meet this weight criterion and were registered in the United States 11 October 1991
must be equipped with a flight data recorder that records time, altitude, airspeed, normal acceleration and
heading, as well as other parameters.
The United States does not require aeroplanes on VFR flights, when operated as controlled flights, to be
equipped in accordance with the requirements for aeroplanes operated under instrument flight rules.
Seaplanes are not required to have equipment for making the sound signals prescribed in the International
Regulations for Preventing Collisions at Sea.
Seaplanes are not required to be equipped with one sea anchor (drogue).
The United States defines extended over water operations for aircraft other th'an helicopters as an operation
over water at a horizontal distance of more than 50 nautical miles from the nearest shoreline.
Aeroplanes operated over land areas designated as areas in which search and rescue would be especially
difficult are not required to be equipped with signalling devices or life-saving 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.
A ground proximity warning systemis not required on piston-engined aeroplanes of a maximum certificated
take-off mass in excess of 5 700 kg or those authorized to carry more than nine passengers.
The United States has not required ground proximity warning systems having a predictive terrain hazard
warning function to be installed on all turbine-engined aeroplanes of a maximum certificated take-off mass
in excess of 15 000 kg or authorized to carry Inore than 30 passengers, for which the individual certificate
of airworthiness is first issued on or after 1 January 2001. All United States-registered turbine-powered
aeroplanes configured with six or more passenger seats produced after 29 March 2002, must be equipped
with a terrain awareness and warning system.
The United States has not required ground proximity warning systems having a predictive terrain hazard
warning function to be installed on all turbine-engined aeroplanes of a maximum certificated take-off mass
in excess of 15 000 kg or authorized to carry more than 30 passengers from 1 January 2003. All United
States-registered turbine-powered aeroplanes configured with six or more passenger seats produced after
29 March 2002, must be equipped with a terrain awareness and warning system by 29 March 2005.
A ground proximity warning system that has a predictive terrain hazard warning function is not required
on all turbine-engined aeroplanes of a maximum certificated take-off mass in excess of 5 700 kg or
authorized to carry more than nine passengers. All United States-registered turbine-powered aeroplanes
configured with six or more passenger seats produced afkr 29 March 2002, must be equipped with a terrain
awareness and warning system.
Emergency locator transmitters are notrequired for turbo-jet powered aircraft; aircraft engaged in scheduled
flights by scheduled air carriers; or aircraft being used to show compliance with regulations or crew
training.
*Recommended Practice
27/9/02
6.18.1 The United States does not require an aeroplane engaged in cargo operations only to be equipped with an
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