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All Journal Conference SENATIK STT Adisutjipto Yogyakarta Vortex Journal of International Conference Proceedings Jurnal Manajemen dan Teknologi Rekayasa
Lukito, Indro
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Aerospace Engineering Humanities Computer Science & IT Control & Systems Engineering Decision Sciences, Operations Research & Management Earth & Planetary Sciences Electrical & Electronics Engineering Energy Engineering Industrial & Manufacturing Engineering Languange, Linguistic, Communication & Media Materials Science & Nanotechnology Mechanical Engineering

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Analisis Kegagalan Fungsi Traffic Alert and Collision Avoidance System Boeing 737-800 Next Garuda Indonesia dan Indentifikasi Penyebab Kegagalan Dengan Metode Fault Tree Lukito, Indro; Pambekti, Arif; Budiono, Cyrilus Sukaca; Kurniawan, Riski; Prakoso, Agung; Mizan, Fathkul
SENATIK STT Adisutjipto Vol 7 (2022): Generation Z's Participation in Aerospace
Publisher : Institut Teknologi Dirgantara Adisutjipto

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.28989/senatik.v7i0.459

Abstract

Traffic Alert and Collision Avoidance Systems (TCAS) pada pesawat Boeing 737-800 NG memiliki fungsi utama untuk menghindari dan memberi peringatan dari suatu potensi tabrakan antar pesawat di udara. Dengan menganalisis berbagai input dari sinyal balasan pesawat lain dan kemudian memberikan peringatan visual dan/atau aural kepada crew berdasarkan perintah TA maupun TA/RA yang dipilih. Dengan demikian crew bisa mengambil suatu tindakan sehingga potensi kecelakaan bisa dihindari. Pada penelitian ini metode yang digunakan untuk penelitian adalah dengan melakukan observasi langsung dan melakukan penanganan kegagalan kerusakan pesawat Boeing 737-800 NG Garuda Indonesia di Hanggar 2 PT. GMF AeroAsia. Selain itu dilakukan analisis kegagalan pesawat dengan menggunakan metode fault tree analysis. Hasil  troubleshooting dan  fault  tree analysis  ditemukan kegagalan pada TCAS antenna, coaxial cable dan REU yang berpengaruh pada navigasi pesawat. Proses troubleshooting TCAS mengacu pada FIM Boeing 737-800 NG chapter 34-45 task 803 dan 804 dan juga FIM B737-800 NG chapter 23-51 task 803.
Pendeteksian lightning dan thunderstorm pada area ruang udara bandara Jog/Wahh Adisutjipto International Airport dan Yogyakarta International Airport Lukito, Indro; Pradnjaparamitha, Intan Dyah; Sudibya, Bambang; Dermawan, Denny
SENATIK STT Adisutjipto Vol 6 (2020): Keselamatan Penerbangan di masa Pandemi Covid-19 [ISBN 978-602-52742-2-0]
Publisher : Institut Teknologi Dirgantara Adisutjipto

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.28989/senatik.v6i0.413

Abstract

Daerah Istimewa Yogyakarta have Yogyakarta International Airport and  Adisutjipto International Airport to serve both of civil and military flight mission. Airport must be supported by weather information system for the flight safety. One of any methodes to detect bad weather is using radiosonde to record weather moving in every step of atmospheric level. Using indexes of weather detection can predict the developing weather and presented thunderstorm, lightning and any storm in both of airport area. The significant weather such as thunderstorm and lightning shall be a big danger for the flight which are located n its weather area and must avoid its area. The research focused to operating of radiosonde and how to analyze the becoming weather worst by calculating the weathar indexes of reported radiosonde recording. The result of its analyze is usefull for pilots especially in any steps of the flight, takeoff , approach and landing. Operating of radiosonde equipment which consist of ground equipment, antenna system, Global Positioning System, software of MGPS2, provided any transmission data that can be used to predict possibility bad weather and presented storm. The results of this research are lightning density in Weather Zone A Yogyakarta International Airport is      dA=17,97715 lightning/km2.yr with lightning threat level classified as “MIDDLE”. Lightning density in Weather Zone B Adisutjipto International Airport is dB=9,346163 lightning/km2.yr with lightning threat level classified as “LOW”. There were presented thunderstorm caused by high convection of heat in the atmosphere with possibility presented storm up to 75% in the bad weather condition. 
Handling Post Flight Documents PT XYZ Soekarno-Hatta International Airport: Human Error Analysis Faturrahman, Mochamad Fikri; Prattiwi, Elisabeth Anna; Priyahapsara, Istyawan; Rahmawati, Fajar Khanif; Lukito, Indro
Journal of International Conference Proceedings Vol 8, No 1 (2025): 2025 ICPM Malaysia Proceeding
Publisher : AIBPM Publisher

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.32535/jicp.v8i1.3904

Abstract

PT XYZ organizes the storage of Post Flight Documents in accordance with the applicable SOP. Post Flight Documents are an important part of flight operations that have an influence on company performance and reputation. Errors in managing Post Flight Documents are mostly caused by human error such as input errors and errors in writing document labels. Data input errors can affect the FATA received by the flight crew. To deal with the occurrence of human error problems, the method that can be used is the Human Error Assessment and Reduction Technique (HEART) method, which is a technique for calculating the probability of human error. The type of research used in this research is descriptive. In this study there were 6 respondents. From the results of data collection and processing using the HEART method in the Post Flight Document handling process, it can be concluded that the activity that has the largest possible error value is in the data entry process into the system which has a HEP value of 4.7607966. Meanwhile, the smallest HEP is found in the task of numbering document packages and creating a receipt record which has a HEP value of 0.02912.
Analisa kegagalan sistem beta pesawat Grob G 120TP-A dengan menggunakan metode Mean Time Between Failure Prakoso, Agung; Setyo, Bima Candra Gautama Adi; Dermawan, Denny; Budiono, Cyrilus Sukaca; Lukito, Indro; Kurniawan, Riski
JUMANTARA: Jurnal Manajemen dan Teknologi Rekayasa Vol 3, No 2 (2024): Juli
Publisher : Institut Teknologi Dirgantara Adisutjipto

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.28989/jumantara.v3i2.2378

Abstract

Pesawat Grob G 120TP-A merupakan jenis pesawat latih dengan engine single turbo propeller. Dalam kinerja engine pesawat Grob G 120TP-A tersebut memiliki komponen yang dinamakan sistem beta untuk mengubah sudut riverse pada propeller dan menghasilkan gaya drag. Rata-rata kegagalan sistem beta banyak terjadi sebelum mecapai usia 3000 jam terbang. Berdasarkan hal tersebut dilakukan observasi kegagalan sistem beta pesawat Grob G 120TP-A dalam kurun waktu tahun 2016-2023, kemudian dilakukan analisis dengan Mean Time Between Failure (MTBF) dan dibandingkan dengan nilai probabilitas yang didapatkan dari pengalokasian Fault Tree Analysis (FTA). Hasil dari nilai mean time between failure paling tinggi pada sistem beta adalah terjadinya kegagalan N2 Fluctuate yang bernilai 961 cycle dan pesawat dengan nilai paling tinggi adalah pada pesawat LD 1201 dengan nilai 157 cycle, selanjutnya dibandingkan dengan probabilitas faul tree, maka kegagalan pada sistem beta dari total keseluruhan yang tidak bisa diterima hanya pada kegagalan vibration dan N2 fluctuate.
Penanganan Vibration Propeller menggunakan Metode Fault Tree Analysis pesawat KT-IB Woong Bee Kurniawan, Riski; Pamungkas, Sunu Aditya; Prakoso, Agung; Lukito, Indro; Budiono, Cyrilus Sukaca; Soemarwoto, Wahyudi
Vortex Vol 5, No 2 (2024)
Publisher : Institut Teknologi Dirgantara Adisutjipto

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.28989/vortex.v5i2.2418

Abstract

Propeller yang diputar oleh engine dapat menghasilkan gaya dorong, karena bentuk blade propeller sendiri yang menyerupai airfoil pada wing pesawat jika dilihat dari penampangnya. Pada pesawat KT-1B Woong Bee, propeller yang digunakan adalah HC-E4N-2/E9512CB-1, jenis adjustable pitch dengan 4 blade. Agar propeller berfungsi optimal, putaran harus stabil untuk memastikan gaya dorong dan kenyamanan penerbangan. Vibration pada propeller sering disebabkan oleh ketidakseimbangan blade, yang bisa terjadi akibat perbedaan berat blade atau perbedaan angle of attack. Analisis kegagalan vibration propeller dilakukan dengan observasi dan data kegagalan dari pesawat KT-1B Woong Bee dalam tiga tahun terakhir (2021-2023). Data tersebut dianalisis menggunakan metode Fault Tree Analysis (FTA) untuk menemukan basic event vibration yang kemudian dianalisa kembali untuk menentukan modus kegagalan yang berupa different weight pada blade yang kemudian dilakukan penanganan berupa balancing propeller, yang mencakup penambahan beban pada blade untuk menyeimbangkan berat blade propeller.
CASE ANALYSIS ON FLIGHT CONTROL SYSTEM SIKORSKY S76 C++ FAILURE FROM YAW CONTROL ASPECT Rahmawati, Fajar Khanif; Lukito, Indro; Baihaqi, M Imam
Vortex Vol 3, No 1 (2022)
Publisher : Institut Teknologi Dirgantara Adisutjipto

Show Abstract | Download Original | Original Source | Check in Google Scholar | Full PDF (495.451 KB) | DOI: 10.28989/vortex.v3i1.1155

Abstract

Flight Control is a system that functions as a helicopter control center. Failure that occurs in flight control would certainly result inconvenience of the pilot in operating the helicopter, even the movement of the helicopter can out of control causing incident or accident. The continuity of the helicopter operation is affected by the maintenance system applied. One of mode moving system helicopter is yaw control, that could control the nose helicopter to move right and left. Fault Tree Diagram could described  analytical technique, whereby an undesired state of the system is specified (usually a state that is critical from a safety or reliability standpoint). The system then analyzed in the context of its environment and operation to find the solution. Based on the analysis results of failures that occurred in the Sikorsky S76 C ++ helicopter flight control from yaw control aspect in the period of January 2015 to May 2018 with an average use of helicopter’s 2092.05 flight hours, there were 46 failures which caused by yaw control. Based on diagram, there were 4 basic events which caused unschedule maintenance on Sikorsky S76 C ++ helicopter flight control system because of yaw fail control,  so that a replacement or repair was needed for the components that affected to the system failure.
Co-Authors Agung Prakoso Arif Pambekti Baihaqi, M Imam Bambang Sudibya, Bambang Budiono, Cyrilus Sukaca Denny Dermawan Faturrahman, Mochamad Fikri Istyawan Priyahapsara Mizan, Fathkul Pamungkas, Sunu Aditya Pradnjaparamitha, Intan Dyah Prattiwi, Elisabeth Anna Rahmawati, Fajar Khanif Riski Kurniawan Setyo, Bima Candra Gautama Adi Soemarwoto, Wahyudi