Document ID: chunk:federal_register_of_legislation:F2016C00118:clause:1_35:p12
Version: federal_register_of_legislation:F2016C00118
Segment Type: clause
Provision Reference: sch 1 cl 35 (pt 12/14)
Character Range: 40364–43148

if:
 (a) the registered operator:
 (i) operates the aeroplane; or
 (ii) permits a person to operate the aeroplane; and
 (b) a requirement in this regulation is not met while the aeroplane is operating.
Penalty: 50 penalty units.
 (3) The aeroplane must have an indication system to indicate to the flight crew if the flight instrument pitot heating system is not operating.
 (4) The indication system must comply with the following requirements:
 (a) the indication system must incorporate an amber light that is in clear view of a flight crew member;
 (b) the indication system must be designed to alert the flight crew if either of the following conditions exists:
 (i) the flight instrument pitot heating system is switched off;
 (ii) the flight instrument pitot heating system is switched on and any pitot tube heating element is inoperative.
Source   FARs section 121.342 modified.
 (5) An offence against subregulation (2) is an offence of strict liability.
Note: On and after 1 March 2012, there will also be a requirement for certain aeroplanes to which this Subpart applies to have landing gear aural warning systems that meet the standard set out in the Part 90 Manual of Standards.

Subpart 90.D—Small aeroplanes engaged in air transport operations

90.400  Applicability
  This Subpart applies to small aeroplanes engaged in air transport operations.

90.405  Cargo and baggage compartments
 (1) The registered operator of an aeroplane that has 10 or more passenger seats and to which this Subpart applies commits an offence if:
 (a) the registered operator:
 (i) operates the aeroplane; or
 (ii) permits a person to operate the aeroplane; and
 (b) a requirement in this regulation is not met while the aeroplane is operating.
Penalty: 50 penalty units.
 (2) Each compartment for cargo, baggage or both (goods) in the aeroplane must:
 (a) display a placard showing the maximum load for which the compartment has been designed; and
 (b) have a means to prevent goods creating a hazard by shifting, or by damaging the aeroplane; and
 (c) have a means to restrain goods to protect the aeroplane's occupants from injury in the event of the aeroplane being subjected to a forward inertial load of up to 9 g when the compartment is carrying the maximum weight of goods.
 (3) If goods are in the passenger compartment of the aeroplane, the compartment must have a means to prevent the passengers being injured by the goods during the emergency landing conditions mentioned in the aeroplane's type certification basis.
Source   FARs Part 135 Appendix A modified.
 (4) An offence against subregulation (1) is an offence of strict liability.

90.410  Emergency exits
 (1) This regulation applies to an aeroplane that:
 (a) is an aeroplane to which this Subpart applies; and
 (b) has