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touchdown zone and runway centre line lights).
Category I1 (CAT II) operation. The United States requires that Category 11 provide approaches to
minima of less than 200 ft (60 m) decision height12 400 ft (732 m) runway visual range to as low
as 100 ft (30 m) decision height11 200 ft (365 m) runway visual range.
Category IIIB (CAT IIB) operation. The United States criteria are the same as those adopted in
Annex 6, Part 11. However, the runway visual range is expressed in feet less than 700 ft (200 m)
but not less than 150 A (50 m).
Minimum descent altitude (MDA) or minimum descent height (MDH). The United States does not
use the term MDH (or height above aerodrome) to describe an altitude or height in a non-precision
approach or circling app~oachb elow which descent must be made without the required visual
reference.
The pilot-in-cornmand is not required to have available on board the aeroplane information
concerning search and rescue services.
In addition to the flight preparation requirements of Annex 6, Part 11, Chapter 4, the United States
requkes United States-registered large or twbine-powered multi-engined general aviation,
passenger-carrying aircraft, wherever operated, to adequately secure and stow food, beverage, and
passenger service equipment during aircraft movement on the surface, take-off and landing.
* Recommended Practice
2 UMTEDS TATES SUPPLEMENTA NNEX6 , PARTI 1 (S~~HEDITION)
--
4.3.1 Except for large and turbine-powered multi-engined aeroplanes, the United States does not require
the pilot-in-command to ensure that crew members and passengers are familiar with the location
and use of emergency exits, life jackets, oxygen dispensing equipment or other emergency
equipment provided for individual use.
4.3.2 Except for large and turbine-powered multi-engined aeroplanes, the United States does not require
the pilot-in-command to ensure that all persons on board are aware of the location and general
manner of use of the principal emergency equipment carried for collective use.
4.6.2.1 The United States does not require a destination alternate aerodrome when the weather at the
aerodrome of intended landing is forecast to have a ceiling of at least 2 000 A (600 m) and a
visibility of at least 3 miles (4.8 km). In addition, standard alternate aerodrome minima are
prescribed 600 fl (185 m) ceiling and 2 miles (3.2 km) visibility for precision approaches, and
800 fl (243 m) ceiling and 2 miles (3.2 km) visibility for non-precision approaches.
4.6.2.2 b) Under United States regulations, the forecast period for the destination alternate aerodrome is from
one hour before to one hour after the estimated time of arrival. In addition, the minima for
ceiling/visibility at the aerodrome of intended landing are 2 000 fi (600 m) and 3 miles (4.8 km);
that is, when at least such minima exist, no alternate aerodrome is required.
In addition to the Standard prescribed in Annex 6, Part 11, 4.6.4, the United States prohibits a pilot
from talung off a United States-registered large or turbine-powered multi-engined general aviation
aeroplane if there is frost, snow, or ice adhering to critical systems, components and surfaces of
the aircraft,
The pilot-in-command is not required to ensure that all persons on board the aircraft during an
emergency are instructed in emergency procedures.
The United States does not specify the authority, qualifications or competency of persons
permitted to taxi aeroplanes on the movement area of an aerodrome.
The United States has no provisions concerning aircraft refielling with passengers on board.
Chapter 6
General In addition to the aeroplane instruments and equipment Standards prescribed in Annex 6, Part U,
Chapter 6, the United States requires that all United States-registered turbojet-powered aeroplanes,
wherever operated, be equipped with an altitude alerting system or device. The United States also
requires that all transport category aeroplanes used in air commerce in the United States and all
United States-registered transport category aeroplanes used in air commerce outside the United
States must use an aural speed warning device.
The United States requires that all large and turbine-powered multi-engined general aviation
aircraft of United States registry have the following emergency equipment in addition to the
equipment specified in Annex 6, Part LI, 6.1.3: two fire extinguishers in the passenger
compartment of aircraft accommodating 30 or more passengers; a crash axe for aeroplanes
accommodatrng mbre than 19 passengers; a portable megaphone for aeroplanes s e a m more than
60 but less than 100 passengers, and two megaphones for aeroplanes with a seating capacity of
more than I00 passengers.
　
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