GM1
CAT.IDE.H.125 & CAT.IDE.H.130 Operations under VFR by day & Operations
under IFR or at night – flight and navigational instruments and associated
equipment
SUMMARY
TABLE
Table 1
Flight and navigational instruments and associated
equipment
|
SERIAL |
FLIGHTS UNDER VFR |
FLIGHTS UNDER IFR OR AT
NIGHT |
|||
|
INSTRUMENT |
SINGLE-PILOT |
TWO PILOTS
REQUIRED |
SINGLE-PILOT |
TWO PILOTS
REQUIRED |
|
|
(a) |
(b) |
(c) |
(d) |
(e) |
|
|
1 |
Magnetic direction |
1 |
1 |
1 |
1 |
|
2 |
time |
1 |
1 |
1 |
1 |
|
3 |
Pressure altitude |
1 |
2 |
2 Note (1) |
2 |
|
4 |
Indicated airspeed |
1 |
2 |
1 |
2 |
|
5 |
Vertical speed |
1 |
2 |
1 |
2 |
|
6 |
Slip |
1 |
2 |
1 |
2 |
|
7 |
Attitude |
1 Note (2) |
2 Note(2) |
1 |
2 |
|
8 |
Stabilised direction |
1 Note (2) |
2 Note(2) |
1 |
2 |
|
9 |
Outside air temperature |
1 |
1 |
1 |
1 |
|
10 |
Airspeed icing protection |
1 Note (3) |
2 Note (3) |
1 |
2 |
|
11 |
Airspeed icing protection failure indicating |
|
|
1 Note (4) |
2 Note (4) |
|
12 |
Static pressure source |
|
|
2 |
2 |
|
13 |
Standby attitude |
|
|
1 Note (5) |
1 Note (5) |
|
14 |
Chart holder |
|
|
1 Note (6) |
1 Note (6) |
Note (1) For
single-pilot night operation under VFR, one means of measuring and displaying
pressure altitude may be substituted by a means of measuring and displaying
radio altitude.
Note (2) Applicable
only to helicopters with a maximum certified take-off mass (MCTOM) of more
than 3 175 kg; or helicopters operated over water when out of sight
of land or when the visibility is less than 1 500 m.
Note (3) Applicable
only to helicopters with an MCTOM of more than 3 175 kg, or with an
MOPSC of more than 9.
Note (4) The
pitot heater failure annunciation applies to any helicopter issued with an
individual CofA on or after 1 August 1999. It also applies before that date
when: the helicopter has a MCTOM of more than 3 175 kg and an MOPSC
of more than 9.
Note (5) For
helicopters with an MCTOM of more than 3 175 kg, CS 29.1303(g) may
require either a gyroscopic rate-of-turn indicator combined with a slip-skid
indicator (turn and bank indicator) or a standby attitude indicator satisfying
the requirements. In any case, the original type certification standard should
be referred to determine the exact requirement.
Note (6) Applicable
only to helicopters operating under IFR.
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