Runways are generally dimensioned to accommodate the aircraft considered to be the “critical aircraft” that is anticipated to utilize the runways most frequently. The “critical aircraft” is defined as being the aircraft type which the airport is intended to serve and which requires the greatest runway length. To identify the “critical aircraft”, flight manual performance data of a variety of aircraft are examined. Once the “critical aircraft” has been determined, the longest distance determined from analyzing both take-off and landing performance is used as the basis for runway dimensions. Generally, the runway width is increased to a maximum of 60 m as a function of length.
Each runway is bounded on the sides and ends by a prepared “graded” area. This graded area is provided to prevent catastrophic damage to aircraft leaving the runway sides and to protect aircraft that overfly the runway at very low altitudes during a balked approach for landing. The graded area at the end of the runway is not considered a normal stopway for accelerate-to-stop calculations.
Occasionally, natural and human-made obstacles penetrate the obstacle limitation surfaces of the take-off and approach paths to runways.
To ensure that a safe clearance from these obstacles is maintained, it is necessary to displace the runway thresholds. In the case of runways for which instrument approach procedures are published in the CAP, the usable runway distances for landings and takeoffs are specified as declared distances. The displacements are also depicted on the aerodrome or airport diagram in both the CAP and the CFS. For other runways not having published CAP approaches, the requisite data is given in the CFS. Where a threshold is displaced, it is marked as shown in AGA 5.4.1.
When the portion of the runway before the displaced threshold is marked with displaced threshold arrows (see AGA 5.4.1), it is permissible to use that portion of the runway for taxiing, for takeoff and for the landing roll-out from the opposite direction. In addition, this displaced portion of the runway may be used for landing; however, it is the pilot’s responsibility to ensure that the descent path can be safely adjusted to clear all obstacles. When taking off from the end opposite to the displaced threshold, pilots should recognize the fact that there are obstacles present that penetrated above the approach slope to the physical end of the runway, which resulted in the threshold being displaced.
When a section of a runway is closed, either temporarily because of construction or permanently because the full length is no longer required, the closed portion of the runway will not be available for the surface movement of aircraft for taxiing, take-off or landing purposes and is marked with an “X”, indicating that the area is not suitable for aircraft use.
The closed portion of the runway may be shown on the aerodrome or airport diagram in the CFS and the CAP for identification purposes; however, declared distances will only include runway length starting at the new threshold position.
Some runways have thresholds not served directly by taxiways. In such cases, there may be a widened area which can be used to facilitate turnaround. Pilots are cautioned that these bays do not give sufficient clearance from the runway edge to allow their use for holding while other aircraft use the runway.
A paved, non load-bearing surface that precedes a runway threshold is marked over the entire length with yellow chevrons, as shown in AGA 5.4.2, when its length exceeds 60 m.
A stopway is a rectangular area on the ground at the end of the runway, in the direction of takeoff, prepared as a suitable area in which an aeroplane can be stopped in the case of an abandoned takeoff. It is marked over the entire length with yellow chevrons as shown in AGA 5.4.2 (when its length exceeds 60 m) and is lighted with red edge and end lights in the take-off direction. Its length is included in the ASDA declared for the runway.
A clearway is a rectangular area above the ground or water selected as a suitable area over which an aeroplane may make a portion of its initial climb.
The CAP provides declared distance information which is defined as follows:
(a) Take-off Run Available (TORA): The length of runway declared available and suitable for the ground run of an aeroplane taking off.
(b) Takeoff Distance Available (TODA): The length of the takeoff run available plus the length of the clearway, if provided.
NOTE: Maximum clearway length allowed is 300 m. The clearway length allowed must lie within the aerodrome or airport boundary.
(c) Accelerate Stop Distance Available (ASDA): The length of the takeoff run available plus the length of the stopway, where provided.
(d) Landing Distance Available (LDA): The length of runway which is declared available and suitable for the ground run of an aeroplane landing.
To reduce the aircraft runway occupancy time, some aerodromes or airports provide rapid-exit taxiways which are angled at approximately 30 degrees to the runway.
The bearing strength of some aerodrome or airport pavement surfaces (runways, taxiways and aprons) to withstand continuous use by aircraft of specific weights and tire pressures has been assessed at specific locations. The TC Pavement Load Rating (PLR) and ICAO Pavement Classification Number (PCN) define the weight limits at or below which the aircraft may operate on pavements without prior approval of the aerodrome or airport authority. The tire pressure and Aircraft Load Rating (ALR)/Aircraft Classification Number (ACN) must be equal to or less than the PLR/PCN figures published for each aerodrome or airport. Aircraft exceeding published load restrictions may be permitted limited operations following an engineering evaluation by the airport operator. Requests to permit such operations should be forwarded to the airport operator and include the type of aircraft, operating weight and tire pressure, frequency of proposed operation and pavement areas required at the aerodrome or airport.
3.10.1 Pavement Load Rating Charts
Operators requiring information respecting aircraft weight limitations in effect at an aerodrome or airport can contact the airport operator.
Because of the unique operational characteristics of helicopters, heliport physical characteristics are significantly different from the physical characteristics of aerodromes. For instance, there is no requirement for a runway at a heliport. In addition, the heliport FATO size is 1.5 times larger than the longest helicopter for which the heliport is certified. A safety area surrounds the FATO, which is to be kept free of obstacles other than visual aids.
3.11.1 FATO
Obstacle-free arrival and departure paths to and from a FATO are always required. In some cases, a FATO can be offset from the intended landing area. In this case, helicopter parking positions are established on an apron area and pilots will hover taxi to transition between the FATO and the parking position.
3.11.2 Heliport Classification
Non-instrument heliports have three classifications: H1, H2 and H3. H1 heliports have no available emergency landing areas within 625 m from the FATO and are restricted for use by multi-engined helicopters capable of remaining 4.5 m above all obstacles within the defined approach/departure pathways when operating with one engine inoperative and in accordance with their aircraft flight manual (AFM).
H2 heliports have available emergency landing areas within 625 m from the FATO; however, due to high obstacles within the approach/departure pathways, the associated approach slopes are higher, requiring the use of multi-engined helicopters. H3 heliports have available emergency landing areas within 625 m from the FATO and no obstacles that penetrate the obstacle limitation surfaces, and as such, may be used by single- or multi-engined helicopters. Heliport classifications are specified in the CFS.
3.11.3 Heliport Operational Limitations
All heliports have three operational limitations. The limitations for each specific heliport are listed in the CFS.
The load bearing strength shall be identified for each elevated or rooftop FATO or floating supporting structure. Surface-level heliports need not list a load bearing strength.
The maximum helicopter overall length shall be identified for each FATO. This is calculated as the width or diameter of each FATO, divided by 1.5. This number represents the largest size helicopter for which the FATO is certified.
The heliport category (instrument or non-instrument) and classification, as detailed in section 3.11.2, above, shall also be listed.