Aircraft Equipment Flashcards
4.1A Subject to paragraphs 4.1B and 4.1C, an aeroplane engaged in:
(a) RPT operations; or
(b) Charter operations; or
(c) Aerial Work operations as an air ambulance or for a flying doctor service;
must not be operated under the IFR unless it is equipped with a serviceable autopilot that has the following capabilities:
(a) the roll and pitch axis;
(b) an automatic heading capability;
(c) an altitude hold capability.
In spite of paragraph 4.1A, an aeroplane without an autopilot may be operated under the IFR if the aeroplane:
(a) equipped with dual controls; and
(b) carries a second pilot who is authorised under CASR Part 61 to conduct the flight.
If the autopilot fitted to an aeroplane engaged in:
(a) Charter operations; or
(b) Aerial Work operations as an air ambulance or for a flying doctor service;
loses a capability referred to in paragraph 4.1A, the aeroplane may, if?
The pilot is satisfied that it is safe to do so, be operated under the IFR by a single pilot within the period of 3 days commencing on the day on which the automatic pilot loses the capability.
When must you have an Assigned Altitude Indicator
- 1 Piston-engined aircraft and unpressurised turbine engine aircraft operating above 15,000 feet in CTA under IFR (except Night VFR) shall be equipped with an altitude alerting system.
- 3 Unless equipped with an altitude alerting system, an aircraft operating in CTA under IFR (except Night VFR) shall be equipped with an assigned altitude indicator.
Instruments required for IFR Aerial Work
AH ASI ALT VSI T & S DG COMPASS CLOCK OAT
Electric lighting for IFR at night (including Night VFR)
Instrument illumination Intensity control 2 × landing lights (Exc. PVT, AWK and CHTR freight only which require only 1 landing light) Passenger compartment lights Pilot compartment lights Position and anti-collision lights Shock-proof torch
Radio Navigation Systems required for AWK
1 x 129 GNSS or later
and 1 x ADF or VOR
Or;
1 x 145 GNSS or later
Or;
1 x Multi-sensor navigation system that includes GNSS and inertial integration