Document ID: chunk:federal_register_of_legislation:F2014L01579:body:0:p2
Version: federal_register_of_legislation:F2014L01579
Segment Type: other
Provision Reference: 
Character Range: 2654–5340

below any of the minima determined for the aircraft.

Schedule 1 Take-off minima for aircraft

Part A  Take-off minima for certain multi-engine I.F.R. aeroplanes
      1 Part A applies to a multi-engine I.F.R. aeroplane that meets each of the following requirements (a qualifying multi-engine aeroplane):
(a) the aeroplane is:
 (i) 2 pilot operated; or
 (ii) a single pilot operated jet aeroplane; or
           (iii) a single pilot operated propeller aeroplane with operative auto feather; and
(b) for an aeroplane with a MTOW exceeding 5 700 kg — the aeroplane is able to meet the relevant obstacle clearance requirements of CAO 20.7.1B; and
(c) for an aeroplane with a MTOW not exceeding 5 700 kg:
           (i) the gross climb gradient performance is at least 1.9% under ambient conditions with the loss of the most critical engine; and
           (ii) the aeroplane engine-out climb gradient under ambient conditions specified in the manufacturer's data is at least 0.3% greater than the obstacle free gradient for the runway length required; and
           (iii) the pilot in command uses published obstacle free gradients only if such gradients are surveyed to at least a distance of 7 500 m from end of TODA; and
        Note   All runways with strip widths of 150 m or greater are surveyed to 7 500 m unless otherwise annotated in the AIP.
 (iv) an operator-established obstacle free gradient is used only if:
(A) the gradient (having a 150 m baseline at the end of TODA), 12.5% splays, and 7 500 m distance) is established not more than 30° from runway heading; and
(B) the procedures involve not more than 15° of bank to track within the splay; and
(d) for a 2-pilot operation — each pilot is:
 (i) endorsed on type; and
 (ii) multi-crew trained on type; and
 (iii) multi-crew proficiency checked within the previous 13 months; and
 (iv) instrument rated.
      2 The take-off minima for a qualifying multi-engine aeroplane are:
(a) a ceiling of zero feet; and
(b) visibility of:
           (i) 550 m — but only if the following conditions are complied with:
(A) the runway must have illuminated edge lighting at spacing intervals not exceeding 60 m, and centreline lighting or centreline markings; and
(B) if the aerodrome is a non-controlled aerodrome, or a controlled aerodrome without ATC in operation — the take-off must be conducted by day only, and the aerodrome must be one at which carriage of radio is mandatory; or
 (ii) 800 m.
      3 It is a condition of the 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 —