Relevant bibliographies by topics / Aerodrome manual

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  2. Dissertations / Theses
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Academic literature on the topic 'Aerodrome manual'

Author: Grafiati
Published: 4 June 2021
Last updated: 4 February 2022

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Journal articles on the topic "Aerodrome manual"

1

Tolstykh, S. A., and V. D. Sharov. "METHOD OF SMS BASIC ELEMENTS DEVELOPMENT FOR THE AERODROME OPERATOR." Civil Aviation High TECHNOLOGIES 21, no. 4 (August 28, 2018): 29–38. http://dx.doi.org/10.26467/2079-0619-2018-21-4-29-38.

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In developing and implementing the safety management System (SMS), which is mandatory in accordance with ICAO SARPs and the requirements of the air legislation of the Russian Federation, civil aviation aerodrome operators face methodological problems mainly in two components of the SMS – risk management and calculation of the safety performance indicators. To solve these problems, the article proposes to use a new approach for risk management in the airlines, developed by the Airline Risk Management Solution Group (ARMS). When adapting the method to the activities of the airport operator, the specifics of aviation events at the airport are taken into account. Manifestations of hazard factors in the form of events and deviations from the norms are proposed to be structured in accordance with the classification of activities in ground handling according to ISAGO Manual. A method for calculating and monitoring the safety performance indicator for the airport operator having extremely rare aviation events is proposed. The advantages of the ARMS approach in the implementation of the main prognostic part of the risk assessment, which directly considers the ability of the system to counteract the dangerous situation under the influence of hazards are shown. A threelevel scheme of safety management at the airport is proposed. The method proposed in the article was used as a basis for SMS implemented at two international aerodromes of the Russian Federation.
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2

Idyaningsih, Nining. "Tinjauan Runway Occupancy Time Landing Terhadap Konfigurasi Taxiway di Bandar Udara Haluoleo Kendari." AIRMAN: Jurnal Teknik dan Keselamatan Transportasi 1, no. 2 (December 20, 2018): 37–45. http://dx.doi.org/10.46509/ajtk.v1i2.64.

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Keteraturan Lalu lintas Udara di Bandar Udara Haluoleo Kendari belum sepenuhnya terpenuhi karena terbukti masih sering terjadi pesawat yang menggunakan opposite runway harus delay. konflik antara depature and arrival aircraft pada kondisi dimana pesawat akan take-off dari runway 08 dan landing runway 26. Tujuan penelitian untuk mengetahui pengaruh Runway Occupancy Time landing setiap Pesawat yang beroprasi di Bandar Udara Haluoleo Kendari. Metode yang digunakan yaitu membandingkan antara konfigurasi taxiway dan Runway Occupancy Time landing dengan ICAo Doc 9157 - Aerodome design manual part 2 taxiway, keseimbangan antara kapasitas maksimum dan efisiensi dari sebuah aerodrome itu terletak pada balance between runway and apron is taxiway sebagai penghubung. Hasilnya ROTL pesawat yang beroperasi terlalu besar dan untuk efisiensi penerbangan harus dikurangi karena sering menghambat pesawat yang akan lepas landas.
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3

Idyaningsih, Nining. "Tinjauan Runway Occupancy Time Landing terhadap Konfigurasi Taxiway diBandar Udara Haluleo Kendari." Airman: Jurnal Teknik dan Keselamatan Transportasi 1, no. 2 (August 22, 2020): 30–37. http://dx.doi.org/10.46509/ajtkt.v1i2.27.

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Keteraturan Lalu lintas Udara di Bandar Udara Haluoleo Kendari belum sepenuhnya terpenuhi karena terbukti masih sering terjadi pesawat yang menggunakan opposite runway harus delay. konflik antara depature and arrival aircraft pada kondisi dimana pesawat akan take-off dari runway 08 dan landing runway 26. Tujuan penelitian untuk mengetahui pengaruh Runway Occupancy Time landing setiap Pesawat yang beroprasi di Bandar Udara Haluoleo Kendari. Metode yang digunakan yaitu membandingkan antara konfigurasi taxiway dan Runway Occupancy Time landing dengan ICAo Doc 9157 - Aerodome design manual part 2 taxiway, keseimbangan antara kapasitas maksimum dan efisiensi dari sebuah aerodrome itu terletak pada balance between runway and apron is taxiway sebagai penghubung. Hasilnya ROTL pesawat yang beroperasi terlalu besar dan untuk efisiensi penerbangan harus dikurangi karena sering menghambat pesawat yang akan lepas landas.
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4

Sonhaji, Imam, Dimas Arya, and Paramitha Dwi nastiti. "Optimalisasi Metode Pembelajaran Taruna Program Studi Lalu Lintas Udara menggunakan Computerized Aerodrome Control Tower (ADC) Artmacs Simulator di Politeknik Penerbangan Surabaya." Jurnal Penelitian 5, no. 1 (April 27, 2020): 68–77. http://dx.doi.org/10.46491/jp.v5e1.488.68-77.

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Kemajuan teknologi mendorong Politeknik Penerbangan Surabaya untuk meningkatkan kualitas lulusannya. Lalu Lintas Udara merupakan salah satu program studi yang terdapat di Poltekbang Surabaya. Dengan berbekal ilmu pengetahuan dan teknologi yang diberikan dalam masa pendidikan, diharapkan seluruh lulusan Poltekbang Surabaya dapat menjadi handal di bidangnya masing-masing pada saat bekerja. Poltekbang Surabaya juga melengkapi sarana praktik yang berbasis teknologi yaitu ADC Artmacs Simulator untuk Program Studi Lalu Lintas Udara. Sistem simulasi ini merupakan pengembangan dari system simulasi manual yang masih menggunakan layout aerodrome sebagai proses pembelajaran secara langsung pada objek yang tidak sebenarnya. ADC Artmacs Simulator dirancang sesuai dengan kondisi yang sebenarnya dan dapat mensimulasikan traffic pesawat maupun keadaan cuaca yang diinginkan, sehingga membuat taruna bisa merasakan seolah-olah berada dilapangan sebenarnya dan taruna diharapkan lebih mudah memahami sistem pelatihan. Namun peralatan ini belum digunakan secara maksimal karena beberapa faktor teknis operasional dan diharapkan dengan perbaikan dan penyempurnaan, sistem ini bisa digunakan sebagai sarana utama pelatihan taruna LLU di Politeknik Surabaya serta dapat meningkatkan kualitas metode pembelajaran.
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5

Kiselev, M. A., S. V. Levitsky, and V. A. Podobedov. "Safe engine-out landing of a passenger plane under the wind conditions." Civil Aviation High Technologies 22, no. 5 (October 28, 2019): 76–84. http://dx.doi.org/10.26467/2079-0619-2019-22-5-76-84.

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The engine failure, according to the flight safety inspection of the Federal Air Transport Agency, caused 4 of 6 aviation accidents in 2017, including 2 air disasters. In general, from 2001 to 2017, events related to the engine failure became the second most frequent cause of aviation accidents (13% of aviation accidents and 12% of air disasters). The worst consequences are associated with the engine failure at the most difficult and crucial stage of the flight landing. For example, it was the engine failure on the final approach that caused the crash of the L-410UVP-E20 RA-67047 aircraft near the Nelkan airfield on November 15, 2017. The article discusses a limiting situation in some sense – the landing of an aircraft with all failed engines under the wind conditions. The authors have proposed for this situation a methodology of calculating the landing approach of an aircraft under the wind conditions in case of failure of all engines of its power plant to an aerodrome equipped with an outer marker. The key features of such methodology are, firstly, the absence of necessity to link the path to the landmarks in the landing aerodrome area, and, secondly, the simplicity of the synthesis and the implementation of the aircraft control based on the proposed methodology during landing in both manual and director or automatic modes. To calculate the approach using the proposed methodology, the crew only needs to know the following values: the minimum drag airspeed on final approach, the height of the flight over an outer marker before landing and spiral approach leg. The content of the methodology in the article is illustrated by the results of the approach calculation when all of the main engines of the Russian short-medium-range MS-21 aircraft fail under the wind conditions.
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6

Melnik, D. M. "Search for critical elements in an integrated quality management system and safety management system." Quality. Innovation. Education, no. 5 (2020): 41–50. http://dx.doi.org/10.31145/1999-513x-2020-5-41-50.

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The International Civil Aviation Organization, in its document Safety Manual (Doc 9859), notes the importance of integrating a safety management system and a quality management system, which takes into account all areas of the civil aviation organization and the formation of interrelated processes to achieve common safety goals. There are discusses the method of searching for critical elements of an aviation enterprise based on risk events in an integrated management system, the main principle of which is the establishment of quality indicators and fiight safety indicators. With this approach, the distribution of indicators by type of activity (classes) is carried out, which in turn allows the study of elements of the aerodrome operator system based on the theory of fuzzy sets (Fuzzy Sets), in accordance with the concept of reliability, risks, safety from the theory of system safety. The results obtained allow us to proactively develop and implement measures that exclude the occurrence of a negative event in the activities of an aviation enterprise, such as a catastrophe, accident, emergency, or a serious aviation incident.
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7

Hutchison, Keith, and Barbara Iisager. "Creating Truth Data to Quantify the Accuracy of Cloud Forecasts from Numerical Weather Prediction and Climate Models." Atmosphere 10, no. 4 (April 3, 2019): 177. http://dx.doi.org/10.3390/atmos10040177.

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Clouds are critical in mechanisms that impact climate sensitivity studies, air quality and solar energy forecasts, and a host of aerodrome flight and safety operations. However, cloud forecast accuracies are seldom described in performance statistics provided with most numerical weather prediction (NWP) and climate models. A possible explanation for this apparent omission involves the difficulty in developing cloud ground truth databases for the verification of large-scale numerical simulations. Therefore, the process of developing highly accurate cloud cover fraction truth data from manually generated cloud/no-cloud analyses of multispectral satellite imagery is the focus of this article. The procedures exploit the phenomenology to maximize cloud signatures in a variety of remotely sensed satellite spectral bands in order to create accurate binary cloud/no-cloud analyses. These manual analyses become cloud cover fraction truth after being mapped to the grids of the target datasets. The process is demonstrated by examining all clouds in a NAM dataset along with a 24 h WRF cloud forecast field generated from them. Quantitative comparisons with the cloud truth data for the case study show that clouds in the NAM data are under-specified while the WRF model greatly over-predicts them. It is concluded that highly accurate cloud cover truth data are valuable for assessing cloud model input and output datasets and their creation requires the collection of satellite imagery in a minimum set of spectral bands. It is advocated that these remote sensing requirements be considered for inclusion into the designs of future environmental satellite systems.
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8

Jiménez, Helena Isabel Lacalle, and Jessica Tuck. "Laboratory Trials Of Cold Recycled Foamed Bitumen Asphalt: Raf Waddington." International Journal on Pavement Engineering & Asphalt Technology 16, no. 1 (May 1, 2015): 82–95. http://dx.doi.org/10.1515/ijpeat-2015-0005.

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Abstract The Defence Infrastructure Organisation requested a pavement evaluation on RAF Waddington and the results indicated that runway rehabilitation and reprofiling was needed in order to meet the physical design requirements set out in the Manual of Aerodrome Design & Safeguarding. The presence of tar in a layer of the old pavement promoted the option of cold recycling this material into the new structure. This paper presents the results from a laboratory investigation into the suitability of cold recycled foamed bitumen asphalt to be used in the structural layers of an airfield pavement. Laboratory mixture designs with foamed bitumen, incorporating asphalt planings from RAF Waddington runway, were produced in URS Infrastructure and Environment Ltd. laboratory. Specimens were used to assess mix performance and in order to add confidence to the design. The last objective of the research was to demonstrate that asphalt planings from RAF Waddington could be recycled into foamed asphalt for incorporation in the runway rehabilitation works. The optimum binder content was determined from Indirect Tensile Stiffness Modulus tests and Indirect Tensile Strength tests, concluding that the optimum binder content was 3.3% by mass. As a common practice in the UK, up to 1.5% by mass of cement was added to the mixture to improve early life performance. To assess the foamed bitumen samples’ performance with time, specimens were prepared and cured for 28, 180 and 360 days at different temperatures. Post curing, the specimens were tested for a range of performance criteria including fatigue, stiffness and durability. The study found that asphalt sampled from the runway at RAF Waddington can be recycled into foamed asphalt, meeting the requirements of Defence Infrastructure Organisation Specification 050.
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9

Pavlin, Stanislav, Vedran Sorić, Dragan Bilać, Igor Dimnik, and Daniel Galić. "Safety Management System in Croatia Control Ltd." PROMET - Traffic&Transportation 21, no. 4 (March 2, 2012): 279–84. http://dx.doi.org/10.7307/ptt.v21i4.239.

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International Civil Aviation Organization and other international aviation organizations regulate the safety in civil aviation. In the recent years the International Civil Aviation Organization has introduced the concept of the safety management system through several documents among which the most important is the 2006 Safety Management Manual. It treats the safety management system in all the segments of civil aviation, from carriers, aerodromes and air traffic control to design, construction and maintenance of aircraft, aerodromes, those who produce instruments, equipment and parts for the needs of civil aviation and others. This paper presents and partly deals with the documents from the safety management system domain and the system implementation in Croatia with special focus on the Croatia air navigation service provider, Croatia Control Ltd. KEY WORDS: safety management system, safety, air traffic control
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10

Sandhyavitri, Ari, and Fiqri Fansyuri. "Evaluation and Projection of Airport Landing Movement Areas based on Statistical Analyses, ICAO 2013 Manuals and KM 44, 2002 Regulation." Journal of Innovation and Technology 1, no. 2 (October 30, 2020): 12–17. http://dx.doi.org/10.31629/jit.v1i2.3167.

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This article demonstrated how to calculate an airport landing movement in systematic five main stages encompassing; (i) data collection (including passengers data, aircraft movements, population, GDP, per capita income, cargos movement, temperatures, ground elevation, slope surface, wind speed, and aircraft characteristics), (ii) forecasting the future traffic demands, (iii) calculating aerodrome reference field length (ARFL), (iv) define aerodrome reference code (ARF), and (v) calculate runway dimensions, taxiways, and apron areas. This article has selected Hang Nadim International Airport (HIA) as a case study. It was identified that the aircraft movements in this airport have increased by an average of 7.30% every year in the periods of 2007 to 2016. This Airport has an existing apron with a capacity of 13 aircraft, while the apron currently has to accommodate 19 aircraft. Therefore, to anticipate future demand. This research evaluated and forecasted the requirements standard for the airport landing movement areas in 2026. Based on the International Civil Aviation Organization (ICAO) 2013 manuals and KM 44, 2002 regulation concerning the National Airport Regulation. This article recommended that the existing runway and taxiways would be adequate to facilitate future aircraft movements up to 2026. However, the apron requires to be expanded to 1,600 m x 150 m (which a capacity of 31 aircraft) for accommodating the apron requirements standard in 2026.
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Dissertations / Theses on the topic "Aerodrome manual"

1

Jaša, Marek. "Procedury certifikace letišť, dle požadavků EASA." Master's thesis, Vysoké učení technické v Brně. Fakulta strojního inženýrství, 2015. http://www.nusl.cz/ntk/nusl-232019.

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The master´s thesis targets to compile summary document for aerodrome certification by EASA requirements and to create methodology for application of these documents. Master´s thesis consists of three main parts. In the first part is described national legislation, which in general regulates condition for civil aviation. There is also specified current legislation, by which the conditions for aerodrome certification are set. The second part of the thesis involves EASA requirements in field of aerodrome certification. There is described organisation structure of agency, information about its emergence and field of occupation. The certification process is analysed in the main part of the thesis. Moreover there is demonstrated the probable schedule of the certification process in the Czech republic and the documents, that should be issued.
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Books on the topic "Aerodrome manual"

1

Organization, World Meteorological, ed. Aerodrome reports and forecasts: A user's handbook to the codes. Genera, Switzerland: WMO, 1992.

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2

Aerodrome Reports and Forecasts: A Users' Handbook to the Codes. Not Avail, 2005.

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3

Aerodrome reports and forecasts: A user's handbook to the codes. 3rd ed. Geneva, Switzerland: WMO, 2001.

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4

Organization, World Meteorological, ed. Aerodrome reports and forecasts: A user's handbook to the codes. Geneva, Switzerland: WMO, 1996.

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Organization, World Meteorological, ed. Aerodrome reports and forecasts: A users' handbook to the codes. 3rd ed. Geneva: World Meteorological Organization, 2001.

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6

Baldwin, Breck. DIY RC Airplanes from Scratch: The Brooklyn Aerodrome Bible for Hacking the Skies. McGraw-Hill Education, 2013.

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