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Question 1
ప్రశ్న 1
In airport engineering, which description best defines an aeroplane reference field length used for aerodrome reference-code planning?
Explanation:
Aeroplane reference field length is a standardized takeoff-performance characteristic. It uses maximum certificated takeoff mass and defined reference atmospheric and runway conditions. These conditions include sea level, standard atmosphere, still air and zero runway slope. The value helps establish the aerodrome reference code but is not itself the approved length for every actual operation. Actual runway requirements depend on aircraft performance, operating mass, weather, slope and applicable rules.
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Question 2
ప్రశ్న 2
Which method is technically appropriate for identifying the critical design aircraft when planning a new runway?
Explanation:
The critical design aircraft is tied to the intended and reasonably expected airport use. Its runway requirements may depend on operating mass, engine performance and route conditions. Wingspan alone does not establish the required runway length. An occasional exceptional movement does not automatically justify sizing the entire runway for that aircraft. The selected planning aircraft and performance assumptions should be documented and reassessed as demand changes.
వివరణ:
Question 3
ప్రశ్న 3
For a simplified basic runway-length screening with no stopway, clearway or displaced threshold, the supplied required takeoff run is 1900 m, required landing distance is 2050 m and required accelerate-stop distance is 2200 m. Assuming all three requirements must be met by the same paved runway length, what is the minimum length?
Explanation:
The specified screening exercise requires the paved runway to satisfy three independent distances. Without a stopway or clearway, no additional declared takeoff or stopping distance is available. The necessary paved length is therefore the maximum of 1900 m, 2050 m and 2200 m. That maximum is 2200 m, set by the accelerate-stop requirement. The result is valid for the supplied performance data and assumptions, not a general regulatory runway length.
వివరణ:
Question 4
ప్రశ్న 4
Which statement correctly describes how takeoff, landing and rejected-takeoff performance are considered when determining runway length?
Explanation:
Takeoff and landing impose different performance requirements on a runway. The distance for a continued takeoff can differ from the distance needed for a rejected takeoff. The landing requirement is assessed against the available landing distance. Permitted clearways and stopways can affect particular declared distances but not all of them. A compliant design satisfies the applicable requirements separately instead of adding all distances together.
వివరణ:
Question 5
ప్రశ్న 5
What is the central idea of a balanced-field takeoff in the relevant transport-aircraft performance context?
Explanation:
Balanced-field length is an aircraft takeoff-performance concept. It relates a rejected-takeoff case to a continued takeoff case under defined conditions. Selection of an appropriate decision speed can balance the corresponding limiting distances. Stopways and clearways can change the declared-distance constraints and the resulting field analysis. The concept must not be confused with runway geometric levelling or landing-distance determination.
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Question 6
ప్రశ్న 6
Which pairing of the four standard runway declared-distance abbreviations is correct?
Explanation:
Runway declared distances describe distinct portions of an available aerodrome surface or airspace arrangement. TORA applies to the ground run for a takeoff. TODA is associated with the takeoff distance and can include an approved clearway. ASDA addresses the distance available to accelerate and stop after an abandoned takeoff. LDA is the length of runway declared available and suitable for the ground run of a landing aircraft.
వివరణ:
Question 7
ప్రశ్న 7
For one runway direction, TORA is 2400 m, with an approved 300 m clearway and 200 m stopway beyond the takeoff-run end. There are no other declared-distance reductions, and the landing threshold is not displaced. What are TODA, ASDA and LDA, respectively?
Explanation:
TODA consists of TORA plus the approved clearway under the stated arrangement. It is 2400 + 300 = 2700 m. ASDA equals TORA plus the approved stopway, or 2400 + 200 = 2600 m. With no displaced threshold or other landing reduction, LDA is 2400 m. Neither clearway nor stopway can simply be added to the landing distance.
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Question 8
ప్రశ్న 8
A 2500 m runway has a landing threshold displaced 350 m inward at one approach end. For that direction, assume takeoffs may still use the entire 2500 m runway, there is no clearway or stopway, and no other restrictions apply. What are LDA and TORA?
Explanation:
The displaced landing threshold reduces the distance available to land from that approach direction. Its LDA is 2500 minus 350, which equals 2150 m. The question expressly permits takeoffs to use the full runway in that direction. Consequently TORA remains 2500 m. Declared distances can differ by direction, and actual published values must be used in operational planning.
వివరణ:
Question 9
ప్రశ్న 9
Which statement correctly distinguishes a stopway from a clearway in runway design?
Explanation:
A stopway is a prepared area available for stopping an aircraft after an aborted takeoff. Its length may be included in ASDA when appropriately declared. A clearway is a defined obstacle-controlled area associated with part of the initial takeoff climb. Its length may be included in TODA subject to applicable rules. Neither area is automatically part of TORA or LDA, and the published declared distances govern.
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Question 10
ప్రశ్న 10
A runway direction has TORA = 2350 m, approved clearway = 200 m, approved stopway = 150 m and LDA = 2350 m. An aircraft requires TORA 2300 m, TODA 2520 m, ASDA 2530 m and LDA 2250 m under the specified conditions. Which assessment is correct?
Explanation:
The runway provides TODA = 2350 + 200 = 2550 m. It provides ASDA = 2350 + 150 = 2500 m. The required ASDA is 2530 m, so the available value is short by 30 m. TORA 2350 m exceeds 2300 m, TODA 2550 m exceeds 2520 m, and LDA 2350 m exceeds 2250 m. All individual requirements must be met, so this takeoff case is unacceptable under the stated assumptions.
వివరణ:
Question 11
ప్రశ్న 11
For an intended takeoff, TORA is 2100 m and TODA is 2400 m because a 300 m approved clearway is available. Aircraft data require a ground takeoff run of 2180 m and a takeoff distance of 2300 m. Ignoring other constraints, which statement is correct?
Explanation:
TORA is the available runway length for the takeoff ground run. The required ground run of 2180 m exceeds the TORA of 2100 m by 80 m. TODA is sufficient because 2400 m exceeds the 2300 m takeoff-distance requirement. A clearway cannot make up for an insufficient ground-run length. The overall takeoff therefore fails the stated separate performance checks.
వివరణ:
Question 12
ప్రశ్న 12
Assuming the same aircraft, takeoff mass, runway surface and wind, how do substantially greater airport elevation and higher air temperature generally affect required takeoff field length?
Explanation:
Air density generally decreases with increasing airport elevation. Higher air temperature also reduces density when other conditions are comparable. Reduced density can impair engine thrust and aerodynamic lift generation at a given true airspeed. The required takeoff distance consequently tends to increase for the same aircraft and mass. Aircraft-specific approved performance data, rather than a universal correction percentage, determine the actual increase.
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Question 13
ప్రశ్న 13
A design exercise specifies a basic field length of 1900 m and an illustrative elevation adjustment of exactly 7% of that basic length. Ignoring all other corrections, what adjusted length results?
Explanation:
The adjustment percentage is expressly supplied as a project exercise assumption. Seven percent of 1900 m is 0.07 times 1900 = 133 m. Adding this to the basic length gives 1900 + 133 = 2033 m. The result is not obtained by adding 7 m for every 100 m of runway elevation. The percentage must not be treated as a universal current aerodrome-design rule without the applicable performance context.
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Question 14
ప్రశ్న 14
For a hypothetical planning exercise, basic runway length is 2000 m. First increase it by 8%, then increase the adjusted result by another 5%, with both corrections explicitly defined as successive. What final length is obtained?
Explanation:
The first correction gives 2000 times 1.08 = 2160 m. The second correction is applied to this already adjusted value. Therefore the result is 2160 times 1.05 = 2268 m. Adding the two percentages directly to the original length would incorrectly give 2260 m. These percentages are illustrative inputs, not mandated corrections for all airport projects.
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Question 15
ప్రశ్న 15
All other operating conditions being equal, which statement about runway longitudinal slope is generally correct for takeoff planning?
Explanation:
An uphill takeoff requires the aircraft to accelerate against an additional component of gravity. This tends to increase the runway ground distance needed under otherwise comparable conditions. A downhill direction can improve acceleration but may introduce other operational issues, including landing and braking performance. Aircraft-approved data establish the quantitative adjustments for a specific operation. Runway slope also remains constrained by the applicable geometric standards.
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Question 16
ప్రశ్న 16
An aerodrome-reference-code 4 runway has a length of 2400 m. The maximum and minimum centreline elevations differ by 14.4 m. What longitudinal slope measure, calculated as elevation range divided by runway length, results, and how does it compare with the ICAO Annex 14 general recommendation of 1% for code 4?
Explanation:
The specified slope measure equals maximum-minus-minimum centreline elevation divided by total runway length. Here it is 14.4/2400 = 0.006. Expressed as a percentage, the result is 0.60%. That is below the stated general 1% recommendation for code 4. This overall test does not replace separate checks of local slopes, slope changes and sight-distance requirements.
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Question 17
ప్రశ్న 17
In a simplified landing-roll model, an aircraft reaches the runway at 70 m/s and starts braking after travelling 250 m. It maintains 70 m/s during those first 250 m and then decelerates uniformly at 2.5 m/s² to rest. Ignoring other effects and margins, what is the total distance from runway arrival to rest?
Explanation:
The kinematic stopping distance from speed v at constant deceleration a is v squared divided by 2a. At 70 m/s and 2.5 m/s squared, the braking distance is 4900/5 = 980 m. The question supplies an additional 250 m before braking begins. The total distance is therefore 980 + 250 = 1230 m. Actual aircraft landing-distance determinations involve approved performance data, runway conditions and the applicable operating margins.
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Question 18
ప్రశ్న 18
Which is the most accurate general statement about determining runway width in a modern aerodrome design?
Explanation:
Runway width is a distinct geometric requirement from runway length. Applicable design criteria depend on the intended aeroplanes and aerodrome reference coding. Relevant aircraft dimensions and operational characteristics influence the required width and shoulders. A 45 m runway may be appropriate for particular categories but is not universal for all aerodromes. Current national adoption and design approval must be checked for the specific airport.
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Question 19
ప్రశ్న 19
Why should a paved runway have suitable transverse slope, surface texture and drainage?
Explanation:
Water ponding on the runway can contribute to hydroplaning and reduced braking effectiveness. Suitable transverse slope helps move surface water toward drainage facilities. Pavement texture and maintenance support wet-surface friction performance. Longitudinal and transverse geometry must be designed within the applicable aerodrome standards. A runway that is geometrically long enough can still be operationally restricted by poor surface conditions.
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Question 20
ప్రశ్న 20
An illustrative project study prescribes a landing-distance factor of 1.40 applied to an aircraft's supplied 1450 m unfactored landing distance. What minimum LDA follows from that stated project factor?
Explanation:
The question expressly supplies the project factor to avoid importing an unstated operating rule. The required LDA is 1450 times 1.40. Multiplication gives 2030 m. This is a landing-distance calculation, not a takeoff-run or accelerate-stop distance. Actual required landing margins depend on aircraft certification, operating rules and runway conditions.
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Question 21
ప్రశ్న 21
Two proposed regular-service design aircraft must be accommodated on a single paved runway with no stopway or clearway. Aircraft P requires 2000 m takeoff run, 2100 m takeoff distance, 2200 m accelerate-stop and 1900 m landing distance. Aircraft Q requires 2050 m takeoff run, 2360 m takeoff distance, 2250 m accelerate-stop and 2150 m landing distance. What minimum paved length satisfies all listed requirements?
Explanation:
With no stopway or clearway, the exercise assumes the paved runway alone must meet every specified distance. For aircraft P the largest required distance is 2200 m. For aircraft Q the largest is 2360 m. The larger of those two governing distances is 2360 m, associated with Q's takeoff-distance requirement. Actual declared distances and approved performance limitations would need to be reviewed before implementation.
వివరణ:
Question 22
ప్రశ్న 22
A runway is planned for heavier aircraft while its available subgrade has relatively low support strength. Which design action best addresses the associated pavement issue?
Explanation:
Runway pavement design is structurally distinct from determining the length needed for aircraft operations. Aircraft wheel loads and repeated traffic affect pavement stresses and fatigue. Subgrade support and moisture conditions strongly influence structural performance. Pavement layer thickness and materials must therefore be designed for the intended fleet and traffic. The runway's length alone does not demonstrate that its pavement can safely sustain those loads.
వివరణ:
Question 23
ప్రశ్న 23
Which statement correctly distinguishes a runway-end safety area from a stopway and a clearway?
Explanation:
The runway-end safety area provides an additional safety function beyond the runway end. It is not intended to serve as routine takeoff-run or landing-roll pavement. A stopway has a defined role in rejected-takeoff stopping performance and may be included in ASDA. A clearway is associated with the initial airborne takeoff path and may contribute to TODA. These functions must remain distinct when calculating or publishing declared distances.
వివరణ:
Question 24
ప్రశ్న 24
A runway is physically 2700 m long, but a displaced threshold reduces the declared LDA for one landing direction by 320 m, with no other reductions. An aircraft requires LDA 2450 m. What is the shortfall relative to the declared LDA?
Explanation:
The LDA for the specified landing direction equals 2700 - 320 = 2380 m. The aircraft requires 2450 m under the stated performance conditions. The difference is 2450 - 2380 = 70 m. Therefore this operation is not supported by the declared landing distance, despite the longer physical pavement. Published declared distances and the applicable aircraft limits govern operational suitability.
వివరణ:
Question 25
ప్రశ్న 25
Which design decision best reflects sound basic runway planning when takeoff, landing and stopping requirements, longitudinal grades and future airport expansion must all be considered?
Explanation:
Runway planning starts with the intended fleet and documented performance requirements. Takeoff run, airborne takeoff distance, rejected-takeoff stopping and landing impose different constraints. Slopes, surfaces, obstacle conditions and pavement strength also influence engineering suitability. Declared distances must be set and communicated for each operating direction. Planning should preserve justified future expansion while maintaining the applicable safety and design requirements.
వివరణ:
Answer Key సమాధానాల పట్టిక
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Question 1 ప్రశ్న 1Answer: B. The minimum takeoff field length at maximum certificated takeoff mass, sea level, standard atmosphere, still air and zero runway slope, according to approved aircraft data. సమాధానం: B.
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Question 2 ప్రశ్న 2Answer: D. Evaluate the aircraft expected to use the airport with sufficient regularity, their operating conditions and the most demanding relevant runway performance requirements. సమాధానం: D.
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Question 3 ప్రశ్న 3Answer: A. 2200 m. సమాధానం: A.
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Question 4 ప్రశ్న 4Answer: C. The runway and its declared distances must satisfy the applicable independent takeoff-run, takeoff-distance, accelerate-stop and landing performance requirements. సమాధానం: C.
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Question 5 ప్రశ్న 5Answer: B. Under the defined conditions and decision-speed selection, accelerate-stop and continued takeoff distance requirements are equal or balanced. సమాధానం: B.
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Question 6 ప్రశ్న 6Answer: A. TORA: takeoff run available; TODA: takeoff distance available; ASDA: accelerate-stop distance available; LDA: landing distance available. సమాధానం: A.
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Question 7 ప్రశ్న 7Answer: D. 2700 m, 2600 m and 2400 m. సమాధానం: D.
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Question 8 ప్రశ్న 8Answer: C. 2150 m and 2500 m. సమాధానం: C.
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Question 9 ప్రశ్న 9Answer: B. A stopway is prepared for stopping during a rejected takeoff and may increase ASDA, whereas an approved clearway may increase TODA but does not add to ground-run TORA. సమాధానం: B.
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Question 10 ప్రశ్న 10Answer: D. The accelerate-stop requirement fails by 30 m, even though the other three requirements are met. సమాధానం: D.
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Question 11 ప్రశ్న 11Answer: A. The takeoff-run criterion fails by 80 m despite sufficient TODA. సమాధానం: A.
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Question 12 ప్రశ్న 12Answer: C. They generally increase the required takeoff field length by reducing air density and aircraft performance margins. సమాధానం: C.
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Question 13 ప్రశ్న 13Answer: B. 2033 m. సమాధానం: B.
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Question 14 ప్రశ్న 14Answer: D. 2268 m. సమాధానం: D.
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Question 15 ప్రశ్న 15Answer: A. A takeoff in the uphill direction tends to require more ground distance than a comparable level-runway takeoff. సమాధానం: A.
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Question 16 ప్రశ్న 16Answer: C. 0.60%, below the recommendation. సమాధానం: C.
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Question 17 ప్రశ్న 17Answer: B. 1230 m. సమాధానం: B.
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Question 18 ప్రశ్న 18Answer: A. Runway width is chosen using the applicable aerodrome reference-code and aircraft dimensional criteria, not a single width for all aircraft. సమాధానం: A.
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Question 19 ప్రశ్న 19Answer: D. To limit surface-water accumulation and preserve suitable wheel-runway friction and operational safety. సమాధానం: D.
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Question 20 ప్రశ్న 20Answer: C. 2030 m. సమాధానం: C.
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Question 21 ప్రశ్న 21Answer: A. 2360 m, governed by aircraft Q's takeoff-distance requirement. సమాధానం: A.
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Question 22 ప్రశ్న 22Answer: B. Design the pavement structure using expected aircraft loading, traffic repetitions, material properties, drainage and subgrade support rather than runway length alone. సమాధానం: B.
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Question 23 ప్రశ్న 23Answer: D. A runway-end safety area is intended to mitigate consequences of overruns or undershoots and is not automatically counted in declared operating distances. సమాధానం: D.
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Question 24 ప్రశ్న 24Answer: C. 70 m shortfall. సమాధానం: C.
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Question 25 ప్రశ్న 25Answer: A. Check the relevant aircraft performance requirements against each declared distance, verify geometric and pavement conditions, and protect feasible development options. సమాధానం: A.
