CATs & CARs Part 91.08 | Regulations & Documentation + IR Flashcards
As per CAR 91.08.01 General provisions,
- The owner or operator of an aircraft shall ensure that, under all circumstances, the aircraft is operated in compliance with -
(A) The terms and conditions of the ___ and __ issued for such aircraft
A. The terms and conditions of the CofA and AFM issued for such aircraft
As per CAR 91.08.01 General provisions,
- The owner or operator of an aircraft shall ensure that, under all circumstances, the aircraft is operated in compliance with -
(B) The operating limitations, the _____ and _____ as prescribed by the appropriate _____ of the state of registry
As per CAR 91.08.01 General provisions,
(B) The operating limitations, the markings and placards as prescribed by the appropriate authority of the state of registry
As per CAR 91.08.01 General provisions,
- The owner or operator of an aircraft shall ensure that, under all circumstances, the aircraft is operated in compliance with -
(C) The ____ limitations prescribed in ____ or as imposed by compliance with the applicable___ ________ standards unless otherwise authorised.
As per CAR 91.08.01 General provisions,
(C) The mass limitations prescribed in part 21 or as imposed by compliance with the applicable noise certification standards unless otherwise authorised.
As per CAR 91.08.01 General provisions,
(2) In complying with sub-regulation _, the owner or operator shall take account of _____ ________, environmental conditions and the _____ of _____ which may have an effect on the performance of the aircraft, when appropriate, including aircraft ____, operating _______, the pressure altitude appropriate to the elevation of the aerodrome, temperature, wind, runway gradient and condition of runway.
As per CAR 91.08.01 General provisions,
(2) In complying with subregulation (1), the owner or operator shall take account of airframe configuration, environmental conditions and the operation of systems which may have an effect on the performance of the aircraft, when appropriate, including aircraft mass, operating procedures, the pressure altitude appropriate to the elevation of the aerodrome, temperature, wind, runway gradient and condition of runway.
As per CAR 91.08.01 General provisions,
(3) The operator of an aircraft engaged in a ______ air ______ operation, shall comply with the provisions of the appropriate regulations in Part ___, Part ___ or Part ___, as the case may be.
As per CAR 91.08.01 General provisions,
(3) The operator of an aircraft engaged in a commercial air transport operation, shall comply with the provisions of the appropriate regulations in Part 121, Part 127 or Part 135, as the case may be.
As prescribed in Part 91.08.4 Aeroplane performance classification, what aeroplane classifies as Class A?
Part 91.08.4
- Multi-engined aeroplanes powered by turbo-propeller engines with a maximum certified mass exceeding 5700kg; and
- Multi-engined turbo-jet-powered aeroplanes
As prescribed in Part 91.08.4 Aeroplane performance classification, what aeroplane classifies as Class B?
Class B aeroplanes:
Propeller driven aeroplanes, other than single-engined aeroplanes, with a MCM of 5700kg or less
As prescribed in Part 91.08.4 Aeroplane performance classification, what aeroplane classifies as Class C?
Class C aeroplanes:
Aeroplanes powered by two or more reciprocating engines with a MCM exceeding 5700kg
As prescribed in Part 91.08.4 Aeroplane performance classification, what aeroplane classifies as Class D?
Class D aeroplanes:
Single-engined aeroplanes
As prescribed in Part 91.08.5 Performance limitations Class A and Class C aeroplanes
(1) No ____ or _____ of a Class A or C aeroplane shall start a ___-___ unless the aeroplane is able, in the event of a critical power-unit failing at any point in the take-off, either to _______ the take-off and stop within either the __________-____ ______ available or the runway available, or to continue the take-off and clear all _______ along the flight path by an _______ margin until the aeroplane is in a position to safely transition to the __-____ phase of flight.
As prescribed in Part 91.08.5 Performance limitations Class A and Class C aeroplanes
(1) No owner or operator of a Class A or C aeroplane shall start a take-off unless the aeroplane is able, in the event of a critical power-unit failing at any point in the take-off, either to discontinue the take-off and stop within either the accelerate-stop distance available or the runway available, or to continue the take-off and clear all obstacles along the flight path by an adequate margin until the aeroplane is in a position to safely transition to the en-route phase of flight.
As prescribed in Part 91.08.5 Performance limitations Class A and Class C aeroplanes
(2) The ________ margin referred to in subregulation (1) shall be determined as prescribed in Document SA-CATS __
As prescribed in Part 91.08.5 Performance limitations Class A and Class C aeroplanes
(2) The adequate margin referred to in subregulation (1) shall be determined as prescribed in Document SA-CATS 91.
As prescribed in Part 91.08.5 Performance limitations Class A and Class C aeroplanes
(3) For the purposes of subregulation (1), in ________ the length of the ______ _______, account shall be taken of the loss, if any, of runway ______ due to ______ of the aeroplane prior to take-off.
As prescribed in Part 91.08.5 Performance limitations Class A and Class C aeroplanes
(3) For the purposes of subregulation (1), in determining the length of the runway available, account shall be taken of the loss, if any, of runway length due to alignment of the aeroplane prior to take-off.
As prescribed in Part 91.08.5 Performance limitations Class A and Class C aeroplanes
(4) No _____ or ________ of a class A or C aeroplane shall _______ such aeroplane unless it is able, in the event of the critical _____ becoming _________ at any point along the route or planned diversions therefrom, to ________ the flight to an __________ at which the requirements of sub-regulation (_) can be met, without flying below the ________ obstacle ________ altitude at any point. .
As prescribed in Part 91.08._ Performance limitations Class A and Class C aeroplanes
(4) No owner or operator of a class A or C aeroplane shall operate such aeroplane unless it is able, in the event of the critical engine becoming inoperative at any point along the route or planned diversions therefrom, , to continue the flight to an aerodrome at which the requirements of sub-regulation (5) can be met, without flying below the minimum obstacle clearance altitude at any point.
As prescribed in Part 91.08.5 Performance limitations Class A and Class C aeroplanes:
(5) No _____ or ________ of a class A or C aeroplane shall _______ such aeroplane unless it is able, at the aerodrome of intended ______ and at any _______ aerodrome, after _______ all ________ in the approach path by a ____ margin, be able to land, with assurance that it can come to a ____ or, for a _______, to a satisfactorily low _____, within the ______ ______ ________. Allowance shall be made for expected variations in the ________ and ______ techniques, if such allowance was not made during the establishments of the aeroplane’s __________ data.
As prescribed in Part 91.08._ Performance limitations Class A and Class C aeroplanes:
(5) No owner or operator of a class A or C aeroplane shall operate such aeroplane unless it is able, at the aerodrome of intended landing and at any alternate aerodrome, after clearing all obstacles in the approach path by a safe margin, be able to land, with assurance that it can come to a stop or, for a seaplane, to a satisfactorily low speed, within the landing distance available. Allowance shall be made for expected variations in the approach and landing techniques, if such allowance was not made during the establishments of the aeroplane’s performance data.
As prescribed in Part 91.08.5 Performance limitations Class A and Class C aeroplanes:
(6) An _____ or _______ may, in meeting the ___________ of sub-regulations (4) and (5), make allowance for ______ fuel __________ and if applicable, the ability to ______ fuel en-route.
As prescribed in Part 91.08._ Performance limitations Class A and Class C aeroplanes:
(6) An owner or operator may, in meeting the requirements of sub-regulations (4) and (5), make allowance for normal fuel consumption and if applicable, the ability to jettison fuel en-route.