Document ID: chunk:federal_register_of_legislation:F2024C00332:reg:4:p3
Version: federal_register_of_legislation:F2024C00332
Segment Type: reg
Provision Reference: reg 4 (pt 3/9)
Character Range: 104339–107145

may only be flown with flight crew members who have successfully completed all approved flight crew training and competency checking requirements.
 (2) In this section:
approved flight crew training and competency checking requirements means flight crew training and competency checking requirements for PC2WE flights with the rotorcraft, based on which CASA issued its approval to the rotorcraft's operator to conduct PC2WE flights with the rotorcraft.

Subdivision 3—Information to be included in application for approval

10.17  Purpose of Subdivision 3
  This Subdivision states the information that must be included in an application by a rotorcraft's operator for an approval, under regulation 133.015 of CASR, to conduct PC2WE flights with the rotorcraft.

10.18  Reliability and sudden power loss
 (1) Subject to subsection (4), the information to be provided must be the information mentioned in subsection (2) or (3).
 (2) The information is that:
 (a) an assessment has been made of the incidence of sudden power loss in rotorcraft of the same type and in engines of the same type; and
           (b) as a result of the assessment, rotorcraft of the same type, with engines of the same type, have been approved to conduct a PC2WE flight by:
 (i) CASA under regulation 133.015 of CASR, or
 (ii) the NAA of a recognised foreign State under EASA-OPS Part CAT (EU Regulation n 965/2012), AMC1 CAT.POL.H.305 or an equivalent standard.
 (3) The information is power plant reliability statistics for rotorcraft of the same type, and engines of the same type, which demonstrate:
 (a) the incidence of sudden power loss in the 5-year period ending on the day of the application does not exceed 1 for 100 000 engine hours; or
 (b) the incidence of sudden power loss in the 5-year period ending on the day of the application does not exceed 3 for 100 000 engine hours, and the incidence is trending downwards.
 (4) This section does not apply if neither the information mentioned in subsection (2) nor the information mentioned in subsection (3) exists.
Note: If this section does not apply, CASA will conduct a risk assessment of the power plant reliability of the rotorcraft and its engines when dealing with the application for the approval.

10.19  Type certificate holder's modification standard
 (1) The information to be provided must be the information mentioned in subsection (2) or (3).
 (2) The information is a statement from the holder of the rotorcraft's type certificate, or the holders of the type certificates for the rotorcraft and its engines, of the modification standard designated by the holder or holders to enhance the reliability of the rotorcraft and its engines during an operation.
 (3) The information is a statement from the holder of the rotorcraft's type certificate, or the