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Canadian Aviation Regulations (SOR/96-433)

Regulations are current to 2024-10-30 and last amended on 2023-06-21. Previous Versions

Part VII — Commercial Air Services (continued)

Subpart 5 — Airline Operations (continued)

Division III — Flight Operations (continued)

Closing and Locking of Flight Deck Door
  •  (1) Subject to subsection (2), after May 1, 2002, the pilot-in-command of an aeroplane that is equipped with a flight deck door shall ensure that at all times from the moment the passenger entry doors are closed in preparation for departure until they are opened on arrival,

    • (a) in the case of an aeroplane referred to in subsection 705.80(1), the flight deck door is closed and locked using the locking device required by subsection 705.80(2); and

    • (b) in the case of any other aeroplane,

      • (i) the flight deck door is closed, and

      • (ii) if the door is equipped with a locking device, it is locked.

  • (2) Subsection (1) does not apply if a Department of Transport air carrier inspector, a crew member or a person authorized under subsection 705.27(4) to access the flight deck is required to enter or leave the flight deck

    • (a) for the performance of their duties;

    • (b) for physiological needs; or

    • (c) for an overriding concern related to the safety of the flight.

  • (3) In all cases, persons entering or leaving the flight deck must comply with the procedures for opening, closing and locking flight deck doors set out in the company operations manual.

Night VFR Flight — Aeroplane

 No person shall operate an aeroplane in night VFR flight unless

  • (a) the flight is conducted within 25 nautical miles of the departure aerodrome; or

  • (b) in the case of an IFR flight, the pilot-in-command establishes visual contact with the intended aerodrome of landing and receives an authorization from the appropriate air traffic control unit or flight service station to conduct a visual approach.

  • SOR/2003-348, s. 1
Instrument Approach Procedures
  •  (1) No person shall conduct a CAT II or CAT III precision approach unless

    • (a) the air operator is authorized to do so in its air operator certificate; and

    • (b) the approach is conducted in accordance with the Manual of All Weather Operations (Categories II and III).

  • (2) No person shall terminate an instrument approach with a landing unless, immediately prior to landing, the pilot-in-command ascertains, by means of radiocommunication or visual inspection,

    • (a) the condition of the runway or surface of intended landing; and

    • (b) the wind direction and speed.

  • SOR/2006-199, s. 21
Approach Bans — Non-precision, APV and CAT I Precision
  •  (1) For the purposes of subsections (2) to (4), the visibility with respect to an aeroplane is less than the minimum visibility required for a non-precision approach, an APV or a CAT I precision approach if, in respect of the advisory visibility specified in the Canada Air Pilot and set out in column I of an item in the table to this section,

    • (a) where the RVR is measured by RVR “A” and RVR “B”, the RVR measured by RVR “A” for the runway of intended approach is less than the visibility set out in column II of the item for the approach conducted;

    • (b) where the RVR is measured by only one of RVR “A” and RVR “B”, the RVR for the runway of intended approach is less than the visibility set out in column II of the item for the approach conducted;

    • (c) where no RVR for the runway of intended approach is available, the runway visibility is less than the visibility set out in column II of the item for the approach conducted; or

    • (d) where the aerodrome is located south of the 60th parallel of north latitude and no RVR or runway visibility for the runway of intended approach is available, the ground visibility at the aerodrome where the runway is located is less than the visibility set out in column II of the item for the approach conducted.

  • (2) No person shall continue a non-precision approach or an APV unless

    • (a) the air operator is authorized to do so in its air operator certificate;

    • (b) the aeroplane is equipped with

      • (i) if the flight crew does not use pilot-monitored-approach procedures, an autopilot capable of conducting a non-precision approach or an APV to 400 feet AGL or lower, or

      • (ii) a HUD capable of conducting a non-precision approach or an APV to 400 feet AGL or lower;

    • (c) the instrument approach procedure is conducted to straight-in minima; and

    • (d) a visibility report indicates that

      • (i) the visibility is equal to or greater than that set out in subsection (1),

      • (ii) the RVR is varying between distances less than and greater than the minimum RVR set out in subsection (1), or

      • (iii) the visibility is less than the minimum visibility set out in subsection (1) and, at the time the visibility report is received, the aeroplane has passed the FAF inbound or, where there is no FAF, the point where the final approach course is intercepted.

  • (3) No person shall continue an SCDA non-precision approach unless

    • (a) the air operator is authorized to do so in its air operator certificate;

    • (b) the aeroplane is equipped with

      • (i) if the flight crew does not use pilot-monitored-approach procedures, an autopilot capable of conducting a non-precision approach to 400 feet AGL or lower, or

      • (ii) a HUD capable of conducting a non-precision approach to 400 feet AGL or lower;

    • (c) the instrument approach procedure is conducted to straight-in minima with a final approach course that meets the requirements of section 725.48 of Standard 725 — Airline Operations — Aeroplanes of the Commercial Air Service Standards;

    • (d) the final approach segment is conducted using a stabilized descent with a planned constant descent angle specified in section 725.48 of Standard 725 — Airline Operations — Aeroplanes of the Commercial Air Service Standards; and

    • (e) a visibility report indicates that

      • (i) the visibility is equal to or greater than that set out in subsection (1),

      • (ii) the RVR is varying between distances less than and greater than the minimum RVR set out in subsection (1), or

      • (iii) the visibility is less than the minimum visibility set out in subsection (1) and, at the time the visibility report is received, the aeroplane has passed the FAF inbound or, where there is no FAF, the point where the final approach course is intercepted.

  • (4) No person shall continue a CAT I precision approach to a runway with centreline lighting or a CAT I precision approach in an aeroplane equipped with a HUD unless

    • (a) the air operator is authorized to do so in its air operator certificate;

    • (b) in the case of an aeroplane not equipped with a HUD,

      • (i) if the flight crew does not use pilot-monitored-approach procedures, the pilot-in-command and the second-in-command are qualified to conduct a CAT II precision approach,

      • (ii) the aeroplane is equipped with

        • (A) a flight director and autopilot capable of conducting a coupled precision approach to 200 feet AGL or lower, or

        • (B) if the flight crew uses pilot-monitored-approach procedures, a flight director capable of conducting a precision approach to 200 feet AGL or lower, and

      • (iii) the runway is equipped with serviceable high-intensity approach lighting, high-intensity runway centreline lighting and high-intensity runway edge lighting;

    • (c) in the case of an aeroplane equipped with a HUD capable of conducting a precision approach to 200 feet AGL or lower,

      • (i) the pilot-in-command and the second-in-command are qualified to conduct a CAT II precision approach,

      • (ii) the aeroplane is equipped with a flight director and autopilot capable of conducting a coupled precision approach to 200 feet AGL or lower, and

      • (iii) the runway is equipped with serviceable high-intensity approach lighting and high-intensity runway edge lighting; and

    • (d) a visibility report indicates that

      • (i) the visibility is equal to or greater than that set out in subsection (1),

      • (ii) the RVR is varying between distances less than and greater than the minimum RVR set out in subsection (1), or

      • (iii) the visibility is less than the minimum visibility set out in subsection (1) and, at the time the visibility report is received, the aeroplane has passed the FAF inbound or, where there is no FAF, the point where the final approach course is intercepted.

    TABLE

    Approach Bans — Visibility

    Column IColumn II
    Canada Air Pilot Advisory VisibilityVisibility Report
    ItemStatute milesRVR in feetStatute milesFeet
    11/22 6001/41 200
    23/44 0003/82 000
    315 0001/22 600
    41 1/45/83 400
    51 1/23/44 000
    61 3/415 000
    7215 000
    82 1/41 1/46 000
    92 1/21 1/4greater than 6 000
    102 3/41 1/2greater than 6 000
    1131 1/2greater than 6 000
  • SOR/2006-199, s. 21

[705.49 to 705.53 reserved]

Division IV — Aircraft Performance Operating Limitations

Exceptions

 A person may operate an aircraft without complying with the requirements of this Division if the person

  • (a) is authorized to do so in an air operator certificate; and

  • (b) complies with the Commercial Air Service Standards.

General Requirements

 Any determination made for the purposes of sections 705.56 to 705.61 shall be based on approved performance data set out in the aircraft flight manual.

Take-off Weight Limitations
  •  (1) No person shall conduct a take-off in an aircraft if the weight of the aircraft

    • (a) exceeds the maximum take-off weight specified in the aircraft 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 weight specified in the aircraft flight manual for the pressure-altitude and the ambient temperature at the destination aerodrome or alternate aerodrome.

  • (2) In the determination of the maximum take-off weight referred to in subsection (1) for an aeroplane,

    • (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).

  • (3) For the purposes of subsection (2), the following factors shall be taken into account:

    • (a) the pressure-altitude at the aerodrome;

    • (b) the ambient temperature;

    • (c) the runway slope in the direction of take-off; and

    • (d) not more than 50 per cent of the reported headwind component or not less than 150 per cent of the reported tailwind component.

 

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