Document ID: chunk:federal_register_of_legislation:F2014L01579:body:0:p3
Version: federal_register_of_legislation:F2014L01579
Segment Type: other
Provision Reference: 
Character Range: 5138–7831

use of the take-off minima in Part A that the pilot in command of the aeroplane must ensure that:
(a) if a return to land at the departure aerodrome will be necessary in the event of an engine failure — the meteorological conditions must be at, or above, instrument approach and landing minima for the aerodrome or such as to allow a visual approach; and
(b) if engine failure occurs at any time after V1, lift-off, or encountering non‑visual conditions — terrain clearance is assured until reaching either en route LSALT or departure aerodrome MSA; and
(c) if a return to the departure aerodrome is not possible — the aeroplane's performance and fuel availability must each be adequate to enable the aeroplane to proceed to a suitable aerodrome, having regard to terrain, obstacles and route distance limitations.

Part B  Take-off minima for other I.F.R. aeroplanes
      1 Part B applies to an I.F.R. aeroplane that is NOT a qualifying multi-engine aeroplane within the meaning of Part A.
      2 The take-off minima for the aeroplane are:
(a) a ceiling of 300 ft; and
(b) visibility of 2 000 m.
      3 It is a condition of the use of the minima in Part B that the pilot in command of the aeroplane must ensure that:
(a) terrain clearance is assured until reaching either en route LSALT or departure aerodrome MSA; and
(b) if a return to the departure aerodrome is not possible — the aeroplane's performance and fuel availability are each adequate to enable the aeroplane to proceed to a suitable aerodrome, having regard to terrain, obstacles and route distance limitations.
      4 It is a condition of the use of the minima in Part B by a multi-engine aeroplane that:
(a) if a return to land at the departure aerodrome will be necessary in the event of an engine failure — the meteorological conditions must be at or above instrument approach and landing minima for the aerodrome or such as to allow a visual approach; and
(b) if engine failure occurs at any time after V1, lift-off, or encountering non‑visual conditions terrain clearance must be assured until reaching either en route LSALT or departure aerodrome MSA.

Part C  Take-off minima for certain multi-engine I.F.R. helicopters
      1 Part C applies to a multi-engine I.F.R. helicopter operating in PC1 or PC2 (a qualifying multi-engine helicopter).
      2 The minima for a qualifying multi-engine helicopter are:
(a) clear of cloud:
           (i) for helicopters operating in PC1 — until attaining the greater of Vyse or Vmin I.M.C.; or
           (ii) for helicopters operating in PC2 — until attaining the greater of Vyse or Vmin I.M.C., and passing the defined point after take-off; and
(b) visibility of:
 (i) 800 m;