CATs & CARs Part 135.08.1 | Regulations & Documentation Flashcards
As prescribed in Part 135.08.1 General Requirements:
(1) Any determination made for _________ of this subpart shall be based on ________ performance ____ set out in the aeroplane flight ______ for the aeroplane concerned.
As prescribed in Part 135.08.1 General Requirements:
(1) Any determination made for purposes of this subpart shall be based on approved performance data set out in the aeroplane flight manual for the aeroplane concerned.
As prescribed in Part 135.08.1 General Requirements:
(2) A person may operate an aeroplane without complying with the requirements of this division if the person -
(a)
is _________ to do so in the air service operator’s operations ___________; and
(b)
complies with the requirements as prescribed in SA-CATS ___.
As prescribed in Part 135.08.1 General Requirements:
(2) A person may operate an aeroplane without complying with the requirements of this division if the person -
(a)
is authorised to do so in the air service operator’s operations specifications; and
(b)
complies with the requirements as prescribed in SA-CATS 135.
As prescribed in Part 135.08.1 General Requirements:
(3) Where an _______ uses _____ or _____ published in the approved aeroplane flight manual, ________ shall be made to ensure any extract errors will be on the side of _____.
As prescribed in Part 135.08.1 General Requirements:
(3) Where an operator uses charts or graphs published in the approved aeroplane flight manual, allowance shall be made to ensure any extract errors will be on the side of safety.
As prescribed in Part 135.08.1 General Requirements:
(4) An _______ shall adopt _______ data sufficient to make accurate and safe __________ calculations.
As prescribed in Part 135.08.1 General Requirements:
(4) An operator shall adopt obstacle data sufficient to make accurate and safe performance calculations.
As prescribed in Part 135.08.1 General Requirements:
(5) Except as authorised by the Director or as provided in regulation 135.07.5, ____-engine aeroplanes shall only be operated in ________ of weather and light, and over such routes and diversions therefrom, that permit a ______ landing to be executed in the event of engine failure.
As prescribed in Part 135.08.1 General Requirements:
(5) Except as authorised by the Director or as provided in regulation 135.07.5, single-engine aeroplanes shall only be operated in conditions of weather and light, and over such routes and diversions therefrom, that permit a forced landing to be executed in the event of engine failure.
As prescribed in Part 135.08.1 General Requirements:
(6) An aeroplane shall be operated in _________ with the terms of its ________ of __________ and within the approved operating _________ contained in its flight manual.
As prescribed in Part 135.08.1 General Requirements:
(6) An aeroplane shall be operated in compliance with the terms of its certificate of airworthiness and within the approved operating limitations contained in its flight manual.
As prescribed in Part 135.08.1 General Requirements:
(7) A flight shall not be commenced unless the ___________ information provided in the ____ ______, supplemented as necessary with other data acceptable to the _______, indicates that the standards ________ in this Subpart can be complied with for the flight to be undertaken.
As prescribed in Part 135.08.1 General Requirements:
(7) A flight shall not be commenced unless the performance information provided in the flight manual, supplemented as necessary with other data acceptable to the Director, indicates that the standards prescribed in this Subpart can be complied with for the flight to be undertaken.
As prescribed in Part 135.08.1 General Requirements:
(8) In complying with any of the provisions in this Subpart, all factors that significantly affect the performance of the aeroplane, as applicable to the phase of flight, shall be taken into account and which shall include as a minimum—
(a) the \_\_\_\_ of the aeroplane; (b) the operating \_\_\_\_\_\_\_\_\_ employed by the operator; (c) the \_\_\_\_\_\_\_-\_\_\_\_\_\_ appropriate to the elevation of the aerodrome; (d) the ambient \_\_\_\_\_\_\_\_\_\_; (e) the \_\_\_; (f) the \_\_\_\_\_\_ slope; and (g) the surface conditions of the \_\_\_\_\_\_. (9) The factors specified in subregulation (6) shall be taken into account either directly as operational parameters or indirectly by means of allowances or margins, which may be provided in the scheduling of performance data or in the comprehensive and detailed code of performance in accordance with which the aeroplane is being operated.
As prescribed in Part 135.08.1 General Requirements:
(8) In complying with any of the provisions in this Subpart, all factors that significantly affect the performance of the aeroplane, as applicable to the phase of flight, shall be taken into account and which shall include as a minimum—
(a) the mass of the aeroplane; (b) the operating procedures employed by the operator; (c) the pressure-altitude appropriate to the elevation of the aerodrome; (d) the ambient temperature; (e) the wind; (f) the runway slope; and (g) the surface conditions of the runway. (9) The factors specified in subregulation (6) shall be taken into account either directly as operational parameters or indirectly by means of allowances or margins, which may be provided in the scheduling of performance data or in the comprehensive and detailed code of performance in accordance with which the aeroplane is being operated.
As prescribed in Part 135.08.2 Take-off Mass limitations
(1) No person shall conduct a take-off in an aeroplane if the mass of the aeroplane—
(a)
_______ the maximum ___-___ ___ specified in the aeroplane ____ ______ for the pressure altitude and the ambient _________ at the aerodrome where the take-off is to be made; or
(b)
after allowing for planned ___ __________ during the flight to the destination aerodrome or alternate aerodrome, _______ the ______ mass specified in the aeroplane flight manual for the _______ altitude and the ambient __________ at the destination aerodrome or alternate aerodrome.
As prescribed in Part 135.08.2 Take-off Mass limitations
(1) No person shall conduct a take-off in an aeroplane if the mass of the aeroplane—
(a)
exceeds the maximum take-off mass specified in the aeroplane flight manual for the pressure altitude and the ambient temperature at the aerodrome where the take-off is to be made; or
(b)
after allowing for planned fuel consumption during the flight to the destination aerodrome or alternate aerodrome, exceeds the landing mass specified in the aeroplane flight manual for the pressure altitude and the ambient temperature at the destination aerodrome or alternate aerodrome.
As prescribed in Part 135.08.2 Take-off Mass limitations
(2) In the determination of the _________ ___-___ mass referred to in subregulation (1)—
(a)
the required ________-___ _______ shall not exceed the ________-___ ______ available (ASDA);
(b)
the required take-off run shall___ ______ the take-off run available (____); and
(c)
the required take-off distance shall not ______ the take-off distance available (TODA).
As prescribed in Part 135.08.2 Take-off Mass limitations
(2) In the determination of the maximum take-off mass referred to in subregulation (1)—
(a)
the required accelerate-stop distance shall not exceed the accelerate-stop distance available (ASDA);
(b)
the required take-off run shall not exceed the take-off run available (TORA); and
(c)
the required take-off distance shall not exceed the take-off distance available (TODA).
As prescribed in Part 135.08.2 Take-off Mass limitations
(3) For the purposes of subregulation (2), the factors to be taken into account are—
(a)
____ of the aeroplane;
(b)
specific operating _________;
(c)
the _______ altitude at the aerodrome
(d)
the ambient _________;
(e)
the _____ ____ in the direction of take-off
(f)
not more than __ percent of the reported ________ component or not less than ___ percent of the reported ______ component;
(g)
loss of effective ____ during runway alignment except where rolling take-offs are approved; and
(h)
where the runway condition is other than bare and dry, the appropriate penalty based upon the runway condition or contaminates such as slope, ice, snow, slush, standing water or water surfaces for seaplanes shall be factored into the performance calculation; and
(i)
any other factor that may significantly affect aeroplane performance
As prescribed in Part 135.08.2 Take-off Mass limitations
(3) For the purposes of subregulation (2), the factors to be taken into account are—
(a)
mass of the aeroplane;
(b)
specific operating procedures;
(c)
the pressure altitude at the aerodrome
(d)
the ambient temperature;
(e)
the runway slope in the direction of take-off
(f)
not more than 50 percent of the reported headwind component or not less than 150 percent of the reported tailwind component;
(g)
loss of effective TORA during runway alignment except where rolling take-offs are approved; and
(h)
where the runway condition is other than bare and dry, the appropriate penalty based upon the runway condition or contaminates such as slope, ice, snow, slush, standing water or water surfaces for seaplanes shall be factored into the performance calculation; and
(i)
any other factor that may significantly affect aeroplane performance
As prescribed in Part 135.08.3 Net take-off flight path
(1) No person shall conduct a take-off in an aeroplane if the ____ of the aeroplane is ______ than the ____ specified in the aeroplane ____ _____ as allowing a net take-off flight path that clears all _______ by at least __ feet vertically or at least __ metres horizontally within the aerodrome boundaries and by at least __ metres horizontally outside those boundaries.
As prescribed in Part 135.08.3 Net take-off flight path
(1) No person shall conduct a take-off in an aeroplane if the mass of the aeroplane is greater than the mass specified in the aeroplane flight manual as allowing a net take-off flight path that clears all obstacles by at least 35 feet vertically or at least 62 metres horizontally within the aerodrome boundaries and by at least 95 metres horizontally outside those boundaries.
As prescribed in Part 135.08.3 Net take-off flight path
(2) In the determination of the ________ ____, minimum distances and flight path referred to in subregulation (1)—
(a) corrections shall be made for— (i) the \_\_\_\_\_\_ to be used; (ii) the \_\_\_\_\_\_ slope in the direction of take-off; (iii) the \_\_\_\_\_\_\_-altitude at the aerodrome; (iv) the ambient \_\_\_\_\_\_\_\_\_; and (v) the wind component at the time of take-off, where not more than 50 percent of the reported headwind component or not less than 150 percent of the reported tailwind component may be considered; and
(b)
calculations shall be based on the pilot—
(i)
not banking the aeroplane before reaching an altitude of __ feet;
(ii)
subject to subregulation (3), using __ degrees or less of bank at or below ___ feet; and
(iii)
using not more than __degrees of bank thereafter, aeroplane speed and configuration permitting.
As prescribed in Part 135.08.3 Net take-off flight path
(2) In the determination of the maximum mass, minimum distances and flight path referred to in subregulation (1)—
(a)
corrections shall be made for—
(i)
the runway to be used;
(ii)
the runway slope in the direction of take-off;
(iii)
the pressure-altitude at the aerodrome;
(iv)
the ambient temperature; and
(v)
the wind component at the time of take-off, where not more than 50 percent of the reported headwind component or not less than 150 percent of the reported tailwind component may be considered; and
(b)
calculations shall be based on the pilot—
(i)
not banking the aeroplane before reaching an altitude of 50 feet;
(ii)
subject to subregulation (3), using 15 degrees or less of bank at or below 400 feet; and
(iii)
using not more than 25 degrees of bank thereafter, aeroplane speed and configuration permitting.
As prescribed in Part 135.08.3 Net take-off flight path
(3) A bank angle ______ than the 15 degrees referred to in subregulation (2) (b) (ii) may be used if it is authorised by the Director.
As prescribed in Part 135.08.3 Net take-off flight path
(3) A bank angle greater than the 15 degrees referred to in subregulation (2) (b) (ii) may be used if it is authorised by the Director.
As prescribed in Part 135.08.7 Dispatch limitations: landing at destination and alternate aerodromes
(1) Subject to subregulation (3), no person shall dispatch or conduct a take-off in an aeroplane unless—
(a)
the ____ of the aeroplane on landing at the destination aerodrome will allow a ___-___ landing—
(i)
in the case of any turbojet- or turbofan-powered aeroplane, within __ percent of the landing distance available (LDA); or
(ii)
in the case of a large propeller-driven aeroplane, within __ percent of the ___; and
(b)
the ___ of the aeroplane on landing at any alternate aerodrome will allow a full-stop landing—
(i)
in the case of a turbojet- or turbofan-powered aeroplane, within 60 percent of the LDA; and
(ii)
in the case of a propeller-driven aeroplane, within 70 percent of the LDA.
As prescribed in Part 135.08.7 Dispatch limitations: landing at destination and alternate aerodromes
(1) Subject to subregulation (3), no person shall dispatch or conduct a take-off in an aeroplane unless—
(a)
the mass of the aeroplane on landing at the destination aerodrome will allow a full-stop landing—
(i)
in the case of any turbojet- or turbofan-powered aeroplane, within 60 percent of the landing distance available (LDA); or
(ii)
in the case of a large propeller-driven aeroplane, within 70 percent of the LDA; and
(b)
the mass of the aeroplane on landing at any alternate aerodrome will allow a full-stop landing—
(i)
in the case of a turbojet- or turbofan-powered aeroplane, within 60 percent of the LDA; and
(ii)
in the case of a propeller-driven aeroplane, within 70 percent of the LDA.
