Page 264 - Overseas Territories Aviation Requirements Consolidated - Total AOC

Regulation OTAR Part 135 - CAT - Helicopters and Small Aeroplanes

(e) That part of the landing after which the requirement of (b)(1) cannot be met shall be conducted
with the surface in sight.

OTAR.135.E9.005 (APP E9) Operations without an assured safe forced landing capability
(a) Provided the operator has conducted and recorded risk assessments as described in E8.005 (a)
(1) and (b), operations may be conducted to/from an aerodrome or operating site located outside
a congested hostile environment without an assured safe forced landing capability:
(1) during take-off, before reaching Vy (speed for best rate of climb) or 200 ft above the
take-off surface; or
(2) during landing, below 200 ft above the landing surface.

OTAR.135.E9.010 (APP E9) Take-off
(a) The take-off mass shall be the lower of:
(1) the MTOM; or
(2) the maximum take-off mass specified for a hover in ground effect with all engines
operating at take- off power, or if conditions are such that a hover in ground effect is not
likely to be established, the take-off mass specified for a hover out of ground effect with
all engines operating at take-off power.
(b) Except as provided in E9.005, in the event of an engine failure the helicopter shall be able to
perform a safe forced landing.

OTAR.135.E9.015 (APP E9) En-route
(a) The helicopter shall be able, with all engines operating within the maximum continuous power
conditions, to continue along its intended route or to a planned diversion without flying at any point
below the appropriate minimum flight altitude.
(b) In the event of an engine failure the helicopter shall be able to perform a safe forced landing.

OTAR.135.E9.020 (APP E9) Landing
(a) The landing mass of the helicopter at the estimated time of landing shall be the lower of:
(1) the maximum certified landing mass; or
(2) the maximum landing mass specified for a hover in ground effect, with all engines
operating at take-off power, or if conditions are such that a hover in ground effect is not
likely to be established, the landing mass for a hover out of ground effect with all
engines operating at take-off power.
(b) Except as provided in E9.005, in the event of an engine failure, the helicopter shall be able to
perform a safe forced landing.

Overseas Territories Aviation Requirements 264 of 386