Document ID: chunk:federal_register_of_legislation:F2024C01173:reg:7:p3
Version: federal_register_of_legislation:F2024C01173
Segment Type: reg
Provision Reference: reg 7 (pt 3/11)
Character Range: 231098–233777

Subsection 11.07(2) of the Part 91 Manual of Standards requires RVSM operations to be conducted in accordance with the requirements of the authorised aeronautical information. For an aeroplane that does not have an automatic pilot with the altitude hold function serviceable, operations in RVSM airspace may be restricted as a result of these requirements.

11.12  Internal doors and curtains
 (1) If an aeroplane has any of the following:
 (a) an internal door;
 (b) a curtain;
through which a passenger in a passenger seat must pass to reach a passenger emergency exit, the door or curtain must be fitted in accordance with this section.
 (2) An internal door, or curtain, must have a means of being secured open.
 (3) There must be:
 (a) a placard placed on an internal door indicating that the door must be secured open during take-off and landing; and
 (b) a means for a crew member to open a door that is normally accessible to, and lockable by, a passenger.
 (4) There must be a placard adjacent to a curtain indicating that the curtain must be secured open during take-off and landing.

11.13  Survival equipment—remote areas and over water
 (1) A flight of an aeroplane that will be conducted in or through a remote area (within the meaning given by section 26.63 of the Part 91 MOS) must carry survival equipment that is appropriate for sustaining life in the area in or through which the flight will be conducted.
 (2) A flight of an aeroplane that will be conducted over water where the aeroplane is required to carry a life raft under Division 12 of this Chapter must carry the following:
 (a) survival equipment that is appropriate for sustaining life in the area in, or through which, the flight will be conducted;
 (b) signalling equipment such that the distress signals set out in Appendix 1 to ICAO Annex 2, Rules of the Air, can be made if required.

11.14  Equipment to measure and record cosmic radiation
 (1) An aeroplane for a flight above FL 490 must be fitted with equipment to measure and display, in a unit that is readily visible to a flight crew member piloting the aeroplane, the total cosmic radiation received in the aeroplane's cabin.
 (2) For the purposes of subsection (1), the equipment must continuously measure and display:
 (a) the dose rate of total cosmic radiation being received during the flight; and
 (b) the cumulative dose of total cosmic radiation received on each flight.
 (3) In this section:
total cosmic radiation means the sum total of ionizing and neutron radiation of galactic and solar origin.

Division 5—Lighting systems

11.15  Cockpit and cabin lighting requirements
 (1) An aeroplane operating by night must be fitted