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2.6.3.1 A Right shall not be continued towards the critical components shall be considered and taken inro
heliport of intended landing unless the latest available account when dctcrmining the suitability of the
mcteorological infonnation indicates that conditions at that alternate;
Section ZZZ, Chapter 2 Annex 6 - Operahn of Aircruj?
- one engine inoperative performance capability shall be
attainable prior to amval at the alternate;
- deck availability shall be guaranteed;
-weather information must be reliable and accurate.
Note.- Tire landing technique specified in the flight
manual following control system failure may precl~ide the
nomination of certain helidecks as alternate heliports.
2.7.3 Recommendation.- Off-shore alternates sho~~ld
not be rrsed when it is possible TO carni enough fuel to have an
on-shore alternate. Such circ~imstunces should be exceptions
and should not include payload enhancenlenr in. adverse
\treather conditions.
2.8 Fuel and oil supply
2.8.1 All helicopters. A flight shall not be commenced
unless, taking into account both the meteorological conditions
and any delays that are expected in flight, the helicopter
cames sufficient fuel and oil to ensure that it can safely
complete the flight. In addition, a reserve shall be carried to
provide for contingencies.
2.8.2 Visual flight rilles (VFR) opcmtions. The fuel and
oil carried in order to comply with 2.8.1 shall, in the case of
VFR operations, be at least the amount sufficient to allow the
helicopter:
a) to fly to the heliport to which the flight is planned;
b) to fly thereafter for a period of 20 minutes at best-rangc
speed plus 10 per cent of the planned flight time; and
C) to have an additional amount of fuel, sufficient to
provide Ibr the increased consumption on the occurrence
of potential contingencies, as determined by the State
and specified in the State regulations governing general
aviation.
2.8.3 Instrument flight rules (IFR) operations. The fuel
and oil carried in order to comply with 2.8.1. shall, in the case
of IFR operations, be at least the amount sufficient to allow the
helicopter:
2.8.3.1 When no alternate is required, in terms of 2.6.2.2,
to fly to the heliport to which the flight is planned, and
thereafter:
a) to fly 30 minutes at holding speed at 450 rn (1 500 ft)
above the destination heliport under standard temperature
conditions and approach and land: and
b) to have an additional amount of fuel, sufficient to
provide for thc increascd consumption on the occurrence
of potential contingencies.
2.8.3.2 Whcn an alternate is required, in terms of 2.6.2.1,
to fly to and exccute an approach, and a missed approach, at
the heliport to which the tlight is planned, and ther~after:
a) to fly to the alternate specified in the flight plan; and
then
b) to fly for 30 minutes at holding speed at 450 m
(1500 ft) above the alternate under standard
temperature conditions, and approach and land; and
c) to have an addihonal amounl of fuel sufficient to
provide for the increased consumprion on the occurrence
of potential contingencies.
2.8.3.3 Whcn no suitable alternate is available,, in terms
of 2.7.1 b), to fly to the heliport to which the flight is planned
and thereafter for a period of two hours at holding speed.
2.8.4 In computing the fuel and oil required in 2.8.1, at
least the following shall be considered:
a) meteorological conditions forecast:
b) expected air traffic control routings and traffic delays;
c) for IFR flight, one instrument approach at the
destination heliport, including a misscd approach:
d) the procedures for loss of pressurization, where
applicable? or failure of one power-unit while en route;
and
ej any other conditions that may delay the landing of the
helicopter or increase fuel and/or oil consumption.
Note.- Nothing in 2.8 precludes amendment of a flight
plan inflight in order to re-plan the flight to another heliport,
provided tlzut the requirements of 2.8 can be cornplied with
frunz the point where the flight has been replann.ed.
2.9 Oxygen supply
Note.- Approximate altitudes in the Standard Atmosphere
corresponding to the values of absolute pressure used in the
te.rf are as follo\trs:
Absolute pressure Metres Feet
2.9.1 A flight to be operated at altitudes at which the
atmospheric pressure in personnel compartments will be less
than 700 hPa shall not be commenced unless sufficient s h e d
breathing oxygen is carried to supply:
Annex 6 - Operation ofAircruft Part ZZZ
a) all crew members and 10 per cent of the passengers ibr
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