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(See Attachment I.) altitude in a glide configuration to the completion of
a landing;
1.2 The operator shall be responsible for engine trend
monitoring.
1.3 To minimize the probability of in-flight engine
failure, the engine shall be equipped with:
a) an ignition system that activates automatically, or is
capable of being operated manually, for take-off and
landing, and during flight, in visible moisture;
b) a magnetic particle detection or equivalent system that
moniton the engine, accessories gearbox, and reduction
gearbox, and which includes a flight deck caution
indication; and
c) an emergency engine power control device that permits
continuing operation of the engine through a sufficient
power range to safely complete the flight in the event of
any reasonably probable failure of the fuel conbol unit.
2. Systems and equipment
2) lower the flaps and landing gear, if applicable;
3) provide power to one pitot heater, which must serve
an air speed indicator clearly visible to the pilot;
4) provide for operation of the landing light specified
in 2 j);
5) provide for one engine restart, if applicable; and
6) provide for the operation of the radio altimeter;
d) two attitude indicators, powered from independent
sources:
e) a means to provide for at least one attempt at engine
re-start:
f) airborne weather radar;
g) a certified area navigation system capable of being
programmed with the positions of aerodromes and safe
forced landing areas, and providing instantly available
back and distance information to those locations;
Single-engine turbine-powered aemplanes approved to operate h) for passenger operations, passenger seats and mounts
at night andor in IMC shall be equipped with the following which meet dynamically-tested performance standards
systems and equipment intended to ensure continued safe and which are fitted with a shoulder harness or a safety
flight and to assist in achieving a safe forced landing after an belt with a diagonal shoulder strap for each passenger
engine failure, under all allowable operating conditions: seat;
ANNEX 6 - PART I APP 3-1 241 1105
No. 29
Annex 6 - Operation of Aircrqfr
i) in pressurized aeroplanes, sufficient supplemental
oxygen for all occupants for descent following engine
failure at the maximum glide performance from the
maximum certificated altitude to an altitude at which
supplemental oxygen is no longer required;
j) a landing light that is independent of the landing gear
and is capable of adequately illuminating the touchdown
area in a night forced landing; and
k) an engine fk warning system.
3. Minimum equipment list
The State of the Operator shall require the minimum equipment
list of an operator approved in accordance with
Chapter 5, 5.4 to specify the operating equipment required for
night and/or IMC operations, and for dayNMC operations.
4. Flight manual information
The flight manual shall include limitations, procedures,
approval status and other information relevant to operations by
singleengine turbinepowered aeroplanes at night andor in
IMC.
5. Event reporting
5.1 An operator approved for operations by single-engine
turbine-powered aeroplanes at night andor in IMC shall report
all significant failures, malfunctions or defects to the State of
the Operator who in turn will not@ the State of Design.
5.2 The State of the Operator shall review the safety data
and monitor the reliability information so as to be able to take
any actions necessary to ensure that the intended safety level
is achieved. The State of the Operator will notify major events
or trends of particular concern to the appropriate Type
Certificate Holder and the State of Design.
6. Operator planning
6.1 Operator route planning shall take account of all
relevant information in the assessment of intended routes or
areas of operations, including the following:
a) the nature of the terrain to be overflown, including the
potential for carrying out a safe forced landing in the
event of an engine failure or major malfunction;
b) weather information, including seasonal and other
adverse meteorological influences that may affect the
flight; and
C) other criteria and limitations as specified by the State of
the Operator.
6.2 An operator shall identify aerodromes or safe forced
laxiding areas available for use in the event of engine failure,
and the position of these shall be programmed into the area
navigation system.
Note I.- A 'safe' forced landing in this context means a
landing in an area at which it can reasonably be expected that
　
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