Air

The Canadian Transportation Accident Investigation and Safety Board Act requires that federal Ministers provide formal responses to the TSB as to action taken or planned in response to our recommendations.

The Board also makes recommendations to other organizations and will assess all these responses and evaluate the degree to which they address the safety issues and deficiencies using an Assessment Rating Guide.

For recommendations and assessments made prior to January 1, 2005, please refer to our Annual Reports.

Air Recommendations and Assessments of Responses

Recommendation A06-04
That the Federal Aviation Administration require that Cessna 208 operators maintain a minimum operating airspeed of 120 knots during icing conditions and exit icing conditions as soon as performance degradations prevent the aircraft from maintaining 120 knots. (A05C0187)
Awaiting Response

Recommendation A06-03
That the Federal Aviation Administration take action to revise the certification of Cessna 208, 208A, and 208B aircraft to prohibit flight into forecast or in actual icing meteorological conditions exceeding "light," until the airworthiness of the aircraft to operate in such conditions is demonstrated. (A05C0187)
Awaiting Response

Recommendation A06-02
That the Department of Transport require that Canadian Cessna 208 operators maintain a minimum operating airspeed of 120 knots during icing conditions and exit icing conditions as soon as performance degradations prevent the aircraft from maintaining 120 knots. (A05C0187)
Awaiting Response

Recommendation A06-01
That the Department of Transport take action to restrict the dispatch of Canadian Cessna 208, 208A, and 208B aircraft into forecast icing meteorological conditions exceeding "light," and prohibit the continued operation in these conditions, until the airworthiness of the aircraft to operate in such conditions is demonstrated. (A05C0187)
Awaiting Response

Recommendation A04-04
That the Department of Transport ensure the continued airworthiness of Canadian-registered aircraft fitted with the CFM56-5 series engine by developing an appropriate safety assurance strategy to make certain that, in the event of a permanent magnet alternator failure, the electronic control unit will revert to aircraft power. (A02P0261)
Response      Assessment      Rating: Fully Satisfactory

Recommendation A04-03
That the Direction Générale de l'Aviation Civile and the Federal Aviation Administration issue airworthiness directives to require the implementation of all CFM56-5 series jet engine service bulletins whose purpose is to incorporate software updates designed to ensure that, in the event of a permanent magnet alternator failure, the electronic control unit will revert to aircraft power. (A02P0261)
Response      Assessment      Rating: Satisfactory in Part

Recommendation A04-02
That the Department of Transport re-evaluate the standard weights for passengers and carry-on baggage and adjust them for all aircraft to reflect the current realities. (A04H0001)
Response      Assessment      Rating: Fully Satisfactory

Recommendation A04-01
That the Department of Transport require that actual passenger weights be used for aircraft involved in commercial or air taxi operations with a capacity of nine passengers or fewer. (A04H0001)
Response      Assessment      Rating: Satisfactory Intent