Presentation on theme: "Aerodrome Training Course"— Presentation transcript:
1Aerodrome Training Course Module 3 Aerodrome Physical Characteristics
2Learning OutcomeParticipants will gain an overview of the required physical characteristics for aerodromes including:Application aerodrome reference codeRunwaysTaxiwaysApronsWith the access to reference documents they will be able to determine the physical characteristics required for specific aircraft types.
3Aerodrome Reference Code Provides a simple method for interrelating the numerous specifications concerning the characteristics of aerodromes to ensure they are suitable for aeroplanes that are intended to operate at the aerodrome.Consists of 2 elementsCode number element 1 corresponding to aeroplane reference field length(Definition -Aeroplane reference field length. The minimum field length required for take-off at maximum certificated take-off mass, sea level, standard atmospheric conditions, still air and zero runway slope, as shown in the appropriate aeroplane flight manual prescribed by the certificating authority or equivalent data from the aeroplane manufacturer. Field length means balanced field length for aeroplanes, if applicable, or take-off distance in other cases.)Code Letter element 2 corresponds to the wing span or the outer main gear wheel span, whichever is more demanding
5Runways Location and Orientation Type of intended operation (non-instrument or instrument)Need to ensure that the required take-off and approach obstacle limitation surfaces are not infringedEnvironmental impact – minimize noise on residential areasPrevailing winds – 20kts max x-wind component for runways 1500m and overUsability factor of the aerodrome to be not less than 95% for aeroplanes that the aerodrome is intended to serve
6RunwaysLength - Adequate to meet operational requirements of the aeroplanes for which the runway is intendedWidth -
8Runway Slopes - Longitudinal The slope computed by dividing the difference between the maximum and minimum elevation along the runway centre line by the runway length should not exceed:— 1 per cent where the code number is 3 or 4; and— 2 per cent where the code number is 1 or 2.Along no portion of a runway should the longitudinal slope exceed:— 1.25 per cent where the code number is 4, except that for the first and last quarter of the length of the runway the longitudinal slope should not exceed 0.8 per cent;— 1.5 per cent where the code number is 3, except that for the first and last quarter of the length of a precision approach runway category II or III the longitudinal slope should not exceed 0.8 per cent; and
9Runways – Sight Distances Where slope changes cannot be avoided, they should be such that there will be an unobstructed line of sight from:— any point 3 m above a runway to all other points 3 m above the runway within a distance of at least half the length of the runway where the code letter is C, D, E or F;— any point 2 m above a runway to all other points 2 m above the runway within a distance of at least half the length of the runway where the code letter is B; and— any point 1.5 m above a runway to all other points 1.5 m above the runway within a distance of at least half the length of the runway where the code letter is A.
10Runways slopes - Transverse To promote the most rapid drainage of water, the runway surface should, if practicable, be cambered except where a single crossfall from high to low in the direction of the wind most frequently associated with rain would ensure rapid drainage. The transverse slope should ideally be:— 1.5 per cent where the code letter is C, D, E or F; and— 2 per cent where the code letter is A or B;but in any event should not exceed 1.5 per cent or 2 per cent, as applicable, nor be less than 1 per cent except at runway or taxiway intersections where flatter slopes may be necessary.For a cambered surface the transverse slope on each side of the centre line should be symmetrical
11Runways - Surface Design objectives Constructed without irregularities that would adversely affect take-off or landings or loss of frictionConstructed to provide good friction characteristics when runway is wetSurface texture depth should not be less than 1.0mmMaintenance objectivesKept clear of loose objects (FOD)Prevent formation of harmful irregularitiesFriction testing and corrective action to remain above minimum friction level
13Runway/Pavement Strength ACN- Aircraft Classification Number (Number expressing the relative effect of an aircraft on a pavement for a specified standard subgrade strength)PCN – Pavement Classification Number (Number expressing the bearing strength of a pavement for unrestricted operations)ACN/PCN meant as means for publishing pavement strength in AIP it is not a design or an evaluation toolRequires reporting ofPavement type R or FSubgrade categoryMaximum tyre pressurePavement evaluation method
15Runways - ShouldersProvided – when code is D or E and runway width less than 60m when code is FWidth – extend symmetrically each side so that overall width of runway and shoulders is – 60m Code D or E; 75m code FSlope – flush with surface it abuts and not to exceed 2.5% transverseStrength – capable of supporting aeroplane without inducing structural damage and supporting ground vehicles
16Runways Turn PadsRequired for code D, E, F where end of runway not served by taxiway to facilitate 180° turns.May be located on either side but left preferableIntersection angle with runway should not exceed 30°
17Runway StripsA defined area including the runway and stopway, if provided, intended:To reduce the risk of damage to aircraft running off the runwayTo protect aircraft flying over it during take-off or landing operationsGraded portion in event of an aeroplane running off the runwayWidth graded portion – extend 75m either side centreline Code 3, 4- extend 40m either side centreline Code 1, 2Surface graded portion - flush with runway or shoulder- longitudinal slope 1.5% code 4, 1.75% code 3- transverse slope 2.5% code 3,4 (5% 1st 3m drainage)- strength to minimize hazards in event aircraft running off runwayObjects – shall satisfy the relevant frangibility requirement in chapter 5 Annex 14 volume 1.
18Runway StripsLength - Strip shall extend before the threshold and beyond the end of the runway or stopway for a distance 60m code 2,3,4,Width –-Instrument Code 3 & 4 = 150m (either side centreline)- Instrument Code 1, 2 = 75m- Non-instrument Code 3 & 4 =75m- Non-instrument code 2 = 40m- Non-instrument code 1 = 30m
19Runway End Safety Areas Length – Shall extend 90m from end of runway strip- Should extend as far as practicable and at least 240mWidth – At least twice that of the runway- Should wherever practicable be equal to graded portionSlopes – Longitudinal below OLS & max 5% downward- Transverse 5%Surface – clear graded,Strength – reduce the risk of damage to aircraft and facilitate movement RFFS vehicles
20ClearwaysOnly need to be provided where operating advantage is required by aircraft using unbalanced performance –TODA greater than TORALength – Should not exceed half the length of TORAWidth – 75m either side of centrelineSlope – not to exceed 1.25% upwards
21StopwaysOnly need to be provided where operating advantage is required by aircraft using unbalanced performance –ASDA greater than TORAWidth – Same width as runwaySlopes – Same as for runwayStrength – supporting aircraft without inducing structural damage to the aircraftSurface – Coefficient of friction to be compatible with runway
22TaxiwaysDesign to ensure critical aeroplane when remaining over centrelinemarkings that the following outer main wheel clearances achievedCodeABCDEFClearance1.5m2.25m3m*4.5m
24Taxiways - Width Curves/Intersections CodeABCDEFWidth7.5m10.5m15m*18m**23m25m*18m if wheel base greater than 18m**23 if outer main gear wheel span greater than 9mCurves/IntersectionsNeed to implement fillets based on critical aircraft
26Taxiways – Rapid ExitTurn-off curve radius – Code 3 & 4 550m (exit speed 93kph/50kts) Code 1 & 2 275m (exit speed 65kph/35kts)Intersection angle – optimum 30°, max 45°, min 25°Straight distance – sufficient for aircraft to come to full stop clear intersecting taxiway
27Taxiways Shoulders SLOPES Longitudinal – 1.5% code C, D, E, F; 3% code A, B.Sight Distance – code C, D, E, F 3m above taxiway see wholesurface for distance of at least 300mTransverse – 1.5% code C, D, E, F; 2% code A, BShouldersShould be provided each side for code C to F so overall width taxiway and shouldersCodeCDEFWidth25m38m44m60m
28Taxiways - StripsWidth – Extend symmetrically each side to achieve minimumdistance from centreline as per table 3-1 column 11CodeABCDEFSemi-width16.5m21.5m26m40.5m47.5m57.5mGraded Portion – Extend symmetrically each as belowCodeABCDEFSemi-width11m12.5m19m22m30m
30Aprons Slopes – maximum 1% on aircraft stands Clearances – between aircraft using stand and other aircraft building object or other aircraftCodeABCDEFClearance3m4.5m7.5m**May be reduced in special circumstances between terminal and noseof aircraft and over any portion of stand provided with visual dockingguidance system
31Isolated Parking Position An isolated aircraft parking position shall be designated or the aerodrome control tower shall be advised of an area or areas suitable for the parking of an aircraft which is known or believed to be the subject of unlawful interference, or which for other reasons needs isolation from normal aerodrome activities.The isolated aircraft parking position should be located at the maximum distance practicable and in any case never less than 100 m from other parking positions, buildings or public areas, etc. Care should be taken to ensure that the position is not located over underground utilities such as gas and aviation fuel and, to the extent feasible, electrical or communication cables.
32Practical Exercise The minimum runway width for a Code 4C runway is? The distance that a runway strip should extend beyond the end of a Code 2 runway isA minimum length RESA for a Code 4 runway strip shall extend to at least (a) 90m, (b) 150m (c) 240m past the end of the runway?Calculate the minimum distances between taxiway centrelines for a Taxiway handling Code D aircraft an a taxiway handling only Code A and B aircraft.