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basis. The event reporting process should cover all items relevant
to the ability to operate safely at night and/or in IMC. The
data should be available for use by the operator, the Type Certificate
Holder and the State so as to establish that the intended
reliability levels are being achieved. Any sustained adverse
trend should result in an immediate evaluation by the operator
in consultation with the State and manufacturer with a view to
determining actions to restore the intended safety level. The
operator should develop a parts control programme with
support from the manufacturer that ensures that the proper
parts and configuration are maintained for single-engine
turbine-powered aeroplanes approved to conduct these operations.
The programme includes verification that parts placed
on an approved single-engine turbine-powered aeroplane
during parts borrowing or pooling arrangements, as well as
those parts used after repair or overhaul, maintain the necessary
configuration of that aeroplane for operations approved in
accordance with Chapter 5, 5.4.
2.3 Power loss rate should be determined as a moving
average over a specified period (e.g. a 12-month moving
average if the sample is large). Power loss rate, rather than
in-flight shut-down rate, has been. used as it is considered to be
more appropriate for a single-engine aeroplane. If a failure
occurs on a multi-engine aeroplane that causes a major, but not
total, loss of power on one engine, it is likely that the engine
will be shut down as positive engine-out performance is still
available, whereas on a single-engine aeroplane it may well be
decided to make use of the residual power to stretch the glide
distance.
a) an oil consumption monitoring programme based on 2.4 The actual period selected should reflect the global
manufacturers' recommendations; and utilization and the relevance of the experience included
(e.g. early data may not be relevant due to subsequent
b) an engine condition monitoring programme describing mandatory modifications which affected the power loss rate).
the parameters to be monitored, the method of data after the introduction of a new engine variant and whilst
collection and the corrective action process; this should global utilization is relatively low, the total available experibe
based on the manufacturer's recommendations. The ence may have to be used to try to achieve a statistically
monitoring is intended to detect turbine engine meaningful average.
ANNEX 6 - PART I ATT 1-1 2i1/11/05
No. 29
Annex 6 - Operation of AircrafC
3. Operations manual
The operations manual should include all necessary
information relevant to operations by single-engine
turbine-powered aeroplanes at night and/or in IMC. This
should include all of the additional equipment, procedures and
training required for such operations, route and/or area of
operation and aerodrome information (including planning and
operating minima).
4. Operator certification or validation
The certification or validation process specified by the State of
the Operator should ensure the adequacy of the operator's
procedures for normal, abnormal and emergency operations,
including actions following engine, systems or equipment
failures. In addition to the normal requirements for operator
certification or validation, the following items should be
addressed in relation to operations by single-engine
turbine-powered aeroplanes:
a) proof of the achieved engine reliability of the aeroplane
engine combination (see Appendix 3, paragraph 1);
b) specific and appropriate training and checking
procedures including those to cover engine failure/
malfunction on the ground, after take-off and en-route
and descend to a forced landing from the nonnal
cruising altitude;
c) a maintenance programme which is extended to address
the equipment and systems referred to in Appendix 3,
paragraph 2;
d) an MEL modified to address the equipment and systems
necessary for operations at night and/or in IMC;
e) planning and operating minima appropriate to the operations
at night andlor in IMC;
f) departure and arrival procedures and any route limitations;
g) pilot qualifications and experience; and
h) the operations manual, including limitations, emergency
procedures, approved routes or areas of operation, the
MEL and normal procedures related to the equipment
referred to in Appendix 3, paragraph 2.
5. Operational and maintenance
programme requirements
5.1 Approval to undertake operations by singleengine
turbine-powered aeroplanes at night and/or in IMC specified in
an air operator certificate or equivalent document should
　
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