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W11105
No. 29
APP 2-2
Appendk 2 Annex 6 - Operation of Aircrafr
abnormal or emergency circumstances, or any other relevant
operational factors.
2.2.6 Instructions and data for mass and balance
calculations.
2.2.7 Instructions for aircraft loading and securing of load.
2.2.8 Aircraft systems, associated controls and instructions
for their use, as required by Chapter 6, 6.1.3.
2.2.9 The minimurn equipment list and configuration
deviation list for the aeroplane types operated and specific
operations authorized, including any requirements relating to
operations in RNP airspace.
2.2.10 Checklist of emergency and safety equipment and
instructions for its use.
2.2.1 1 Emergency evacuation procedures, including typespecific
procedures, crew coordination, assignment of crew's
emergency positions and the emergency duties assigned to
each crew member.
2.2.12 The normal, abnormal and emergency procedures
to be used by the cabin crew, the checklists relating thereto
and aircraft systems information as required, including a
statement related to the necessary procedures for the
coordination between flight and cabin crew.
2.2.13 Survival and emergency equipment for different
routes and the necessary procedures to verify its normal
functioning before take-off, including procedures to determine
the required amount of oxygen and the quantity available.
2.2.14 The ground-air visual signal code for use by
survivors, as contained in Annex 12.
2.3 Routes and aerodromes
2.3.1 A route guide to ensure that the flight crew will
have, for each flight, information relating to communication
facilities, navigation aids, aerodromes, instrument approaches,
instnunent arrivals and instrument departures as applicable for
the operation, and such other information as the operator may
deem necessary for the proper conduct of flight operations.
2.3.2 The minimum flight altitudes for each route to be
flown.
2.3.3 Aerodrome operating minima for each of the
aerodromes that are likely to be used as aerodromes of
intended landing or as alternate aerodromes.
2.3.4 The increase of aerodrome operating minima in case
of degradation of approach or aerodrome facilities.
2.3.5 The necessary information for compliance with all
flight profiles required by regulations, including but not
limited to, the determination of:
a) take-off runway length requirements for dry. wet and
contaminated conditions, including those dictated by
system failures which affect the take-off distance;
b) take-off climb limitations;
c) en-route climb limitations;
d) approach climb limitations and landing climb limitations;
e) landing runway length requirements for dry, wet and
contaminated conditions, including systems failures
which affect the landing distance; and
f ) supplementary information, such as tire speed
limitations.
2.4 Training
2.4.1 Details of the flight crew training programme, as
required by Chapter 9,9.3.
2.4.2 Details of the cabin crew duties training programme
as required by Chapter 12, 12.4.
2.4.3 Details of the flight operations officerlflight
dispatcher training programme when employed in conjunction
with a method of flight supervision in accordance with
Chapter 4, 4.2.1.
Note.- Details of the flight operations oficer/flight
dispatcher training programme are contained in Chapter 10,
10.2.
APP 2-3 24/11/05
No. 29
APPENDIX 3. ADDITIONAL REQUIREMENTS FOR APPROVED
OPERATIONS BY SINGLE-ENGINE TURBINE-POWERED
AEROPLANES AT NIGHT AND/OR IN INSTRUMENT
METEOROLOGICAL CONDITIONS (IMC)
(See Chapter 5, 5.4.1)
Airworthiness and operational requirements provided in a) two separate electrical generating systems, each one
accordance with Chapter 5, 5.4.1, shall satisfy the following: capable of supplying all probable combinations of
continuous in-flight electrical loads for instruments,
equipment and systems required at night andlor in IMC;
1. Turbine engine reliability b) a radio altimeter;
1.1 Turbine engine reliability shall be shown to have a c) an emergency electrical supply system of sufficient
power loss rate of less than 1 per 100 000 engine hours. capacity and endurance, following loss of all generated
power, to as a minimum:
Note.- Power loss in this context is defined as any loss of
power, the cause of which may be traced to faulty engine or 1) maintain the operation of all essential flight instruengine
component design or installation, including design or ments, communication and navigation systems
installation of the fuel ancillary or engine control systems. during a descent from the maximum certificated
　
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