ICAO recommends that basic runway length should be increased at the rate of 7% per 300 m rise in elevation above mean sea level.
2) Temperature correction
Airport reference Temperature (ART)
T m = Monthly mean of the maximum daily temperature of the hottest month.
T a = Monthly mean of the average daily temperature of the hottest month
Rise in temperature = ART - SAT
SAT is Standard Atmospheric Temperature
NOTE: Due to the elevation, there is a decrease in standard temperature at the rate of -6.5 0 c per 1000 m rise.
As per ICAO, Basic runway length after correction for elevation should be further increased at the rate of 1% for every 1° C rise of the airport reference temperature
Correction for temperature
Note: As per ICAO, the cumulative connection for elevation and temperature Cumulative (%) correction together should not be ≯35%
If exceeds modify, I 2 = 1.35 x I
3) Gradient correction
For every 1% effective gradient, runway length will be increased by 20%
India’s #1 Learning Platform Start Complete Exam Preparation Daily Live MasterClasses Practice Question Bank Mock Tests & Quizzes Trusted by 6.1 Crore+ StudentsThe point of intersection of the obstruction clearance line and the extended plane of the runway surface and the other end of the runway is called as:
Explanation:
Effective length of runway:
For takeoff, effective length of the runway means the distance from the end of the runway at which the takeoff is started to a point at which the obstruction clearance plane associated with the other end of the runway intersects the runway centerline.
Additional Information
Basic Runway Length:
What is the airport reference temperature, if the monthly mean of average daily temperature for the hottest month of a study year = 24 ° C and the monthly mean of the maximum daily temperature for the same month of the same year = 30°C
Explanation:
The airport reference temperature is calculated using the following formula:
Ta is the monthly mean of the average daily temperature for the hottest month of the year
Tm is the monthly mean of the maximum daily temperature for the same month of the same year
Ta = 24 0 C and Tm = 30 0 C
Substitute these values in the given formula:
ART = 24 + 2 = 26 0 C
Additional Information
Procedure to find Ta
Step 1: Select any month for a given year.
Step 2: Evaluate the average daily temperature variation for a day and this will be called the daily average temperature for that day. This procedure is repeated for all the other days of that month.
Step 3: Evaluate the month's mean temperature as;
Step 4: Repeat the above procedure (Step 2 and Step 3) for all other months of the year. The hottest month is that which has the maximum monthly mean temperature and that will be called Ta.
India’s #1 Learning Platform Start Complete Exam Preparation Daily Live MasterClasses Practice Question Bank Mock Tests & Quizzes Trusted by 6.1 Crore+ StudentsMatch the items in List 1 (Purpose) with those in List 2 (Designed Component used in Airport, and select the answer using codes given below.
List – I | List – II | ||
A. | Basic Runway length | 1. | Width and length of Safety area of airport |
B. | Runway Capacity | 2. | Housing, Servicing of aircrafts |
C. | Runway geometric design | 3. | Location of exit taxiways |
D. | Hangar | 4. | Engine failure class |
Explanation:
The basic runway length is determined in three cases
Runway Capacity:
The following items are to be considered in the geometric design of the runway.
Hanger
A taxiway is to be designed for operating large subsonic aircraft. Which has the following details. Wheelbase = 20m Tread of main landing gear = 6.62 m Turning speed = 45 Kmph Width of taxiway = 22 m Determine the turning radius of the taxiway.
Concept:
The turning radius of the taxiway is the maximum of the following three criteria.
1). R = \(v^2\over 125f\)
2). According to the horonjeff equation
3). The minimum value of the radius of the taxiway for,
Subsonic jets = 120 m.
Supersonic jets = 180 m.
V = Exit/ Turning speed (Kmph)
f = coefficient of friction = 0.13
T = width of the taxiway
S = Distance between the midway point of the main gear and the edge of the taxiway.
Calculation:
V = 45 Kmph, W = 17.7 m, T = 22 m, f = 0.13, tread = 6.62 m
2. S = \(6+ <6.62\over2>= 9.31\space m\)
3. R = 120 m (Subsonic aircraft)
R = 124.6 m
India’s #1 Learning Platform Start Complete Exam Preparation Daily Live MasterClasses Practice Question Bank Mock Tests & Quizzes Trusted by 6.1 Crore+ StudentsAt a certain station, the mean of the average temperature is 25° C and mean of the maximum daily temperature is 40° C. What is the airport reference temperature (ART) ?
Concept:
Ta = Avg. temp of the hottest month
Tm = Monthly mean of maximum daily temp. of same month.
Calculation:
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India’s #1 Learning Platform Start Complete Exam Preparation Daily Live MasterClasses Practice Question Bank Mock Tests & Quizzes Trusted by 6.1 Crore+ StudentsThe point of intersection of the obstruction clearance line and the extended plane of the runway surface and the other end of the runway is called as:
Explanation:
Effective length of runway:
For takeoff, effective length of the runway means the distance from the end of the runway at which the takeoff is started to a point at which the obstruction clearance plane associated with the other end of the runway intersects the runway centerline.
Additional Information
Basic Runway Length:
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India’s #1 Learning Platform Start Complete Exam Preparation Daily Live MasterClasses Practice Question Bank Mock Tests & Quizzes Trusted by 6.1 Crore+ StudentsEnd – to – end runway (m) | Gradient (%) |
0 to 300 | + 1.2 |
300 to 600 | - 0.7 |
600 to 1100 | + 0.6 |
1100 to 1400 | - 0.8 |
1400 to 1700 | - 1.0 |
Explanation As the airport is at MSL and the airport temperature is the same, the elevation and temperature correction is zero. Along the runway the gradient is different, Determining the entire gradient correction Gradient correction: Effective rise or fall \( = \frac> \times 300 - \frac>> \times \left( \right) + \frac>> \times \left( \right) - \frac> \times \left( \right) - \frac>> \times \left( \right)\) = 3.6 - 2.1 + 3 - 2.4 - 3 = - 0.9 ∴ Cumulative rise/fall is - 0.9 m
End – to – end runway (m) | Gradient (%) | Rise/Fall | Cumulative |
0 to 300 | + 1.2 | + 3.6 | + 3.6 |
300 to 600 | - 0.7 | - 2.1 | + 1.5 |
600 to 1100 | + 0.6 | 3 | + 4.5 |
1100 to 1400 | - 0.8 | - 2.4 | + 2.1 |
1400 to 1700 | - 1.0 | -3 | - 0.9 |
\(Effective\;gradient = \frac>>\) \( = \frac \right)>>> \times 100 = 0.3176\;\% \) ∴ The effective gradient is 0.3176 %
Share on Whatsapp India’s #1 Learning Platform Start Complete Exam Preparation Daily Live MasterClasses Practice Question Bank Mock Tests & Quizzes Trusted by 6.1 Crore+ StudentsAt a certain station, the mean of the average temperature is 30°C and mean of the maximum daily temperature is 45° C. What is the airport reference temperature ?
Concept:
Airport reference temperature (ART) \(= + \frac - >>\)
T a = monthly mean of the average daily temperature for the hottest month of the year
T m = monthly mean of the maximum daily temperature for the same month
Calculation:
∴ ART = 35 ° C
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India’s #1 Learning Platform Start Complete Exam Preparation Daily Live MasterClasses Practice Question Bank Mock Tests & Quizzes Trusted by 6.1 Crore+ StudentsWhich one of the following instances of performance of aircraft is not considered for determining basic runway length?
Factors affecting basic runway length
Safety requirements
Important point:
Basic runway length is calculated with the following assumptions:
i) It is calculated at Mean sea level (MSL)
ii) It is calculated for standard temp 15°C at MSL.
iii) The gradient is assumed to be zero.
Due to the variance of these assumptions, some corrections are applied.
i) Elevation Correction: 7% increase in basic runway length for every 300 m rise above MSL
ii) Temperature correction: 1% increase for every 1°C rise in airport reference temperature with respect to standard temperature at elevation.
Standard temperature at elevation = Temperature at MSL – 0.0065 × Elevation
This increase is made on the already corrected runway length for elevation.
iii) Gradient correction: 20% increase for 1% of effective gradient.
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India’s #1 Learning Platform Start Complete Exam Preparation Daily Live MasterClasses Practice Question Bank Mock Tests & Quizzes Trusted by 6.1 Crore+ StudentsAccording to ICAO recommendation, while selecting the site for a runway, as the elevation of the locality changes, the rate at which runway length has to be modified is:
Correction for basic Runway length (l)
i) Elevation correction
For every 300-meter rise above MSL, the length will be increased by 7%
ii) Temperature correction
Airport reference Temperature (ART)
T m → monthly mean of maximum daily temp of hottest month
T a → monthly mean of average daily temp of hottest month
For energy 1°C rise of ART above (SAT x i.e. Standard Airport Temperature) length will be increased by 1%
Note: As per ICAO, the cumulative connection for elevation and temperature together should not be ≯ 35%.
Cumulative (%) correction \(= \frac>_2> - >_1>>>>> \times 100 \not > 35\% \)
If exceeds modify, l 2 = 1.35 × l
iii) Gradient correction
For every 1% effective gradient, runway length will be increased by 20%
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India’s #1 Learning Platform Start Complete Exam Preparation Daily Live MasterClasses Practice Question Bank Mock Tests & Quizzes Trusted by 6.1 Crore+ StudentsIdentify the mis-matched pair about type of Airport and the maximum value of longitudinal gradient of a taxiway, as per ICAO.
Explanation:
Taxiway:
Design criteria for taxiway:
1) Longitudinal gradient as per ICAO
Type or Class of airport | Permissible gradient |
A/B | 1.5 % |
C/D/E | 3 % |
2) Transverse gradient as per ICAO
Type/Class of airport | Permissible gradient |
A/B/C | 1.5 % |
D/E | 2 % |
3) Rate of change of longitudinal gradient as per ICAO
Rate of change | Class of airport |
1% / 30 m of vertical curve | A/B/C |
1.2% / 30 m of vertical curve | D/E |
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India’s #1 Learning Platform Start Complete Exam Preparation Daily Live MasterClasses Practice Question Bank Mock Tests & Quizzes Trusted by 6.1 Crore+ StudentsThe base length of the runway at the mean sea level (MSL) is 1500 m. If the runway is located at an altitude of 300 m above the MSL, the actual length (in m) of the runway to be provided is _________. (round off to the nearest integer)
Explanation: Basic runway length is based on some assumptions:- a) Derived at Mean Sea level b) Derived for a standard temperature of 15°C c) The gradient must be zero. The actual runway need not follow all these guidelines and hence we must apply some corrections. The sequential correction is applied in the basic runway length. The first correction is altitude correction, the second correction is temperature correction and the last correction is gradient correction. Altitude Correction: Basic runway length is increased by 7% for every 300 m rise above mean sea level. This is done due to the decrease in drag force on the aircraft owing to the decrease in density of air as the altitude increases. Given: Height above MSL = 300 m, and Basic Runway length = 1500 m After applying elevation correction, \(> = 1500 \times \frac> \times \frac>> = 105>\) Corrected Runway Length = 1500 + 105 = 1605 m Important Points Temperature correction and gradient corrections are applied on the subsequently corrected runway length.