Langit Biru: Jurnal Ilmiah Aviasi
1. Flight Operation a) Pilot performance b) Flight Operation Officer performance c) Aerodynamics d) delays, aircraf changes and operational limitation e) flight deck 2. Aircraft Maintenance a) Aircraft Maintenance b) Aircraft Maintenance Engineering c) Maintenance, Repair, and Overhaul Industri 3. CNS/ATM a) Communications b) Navigations c) Surveillance d) Air traffic management e) Aerodrome Information Service f) PANS-OPS g) Air navigations economic h) Flight data processing i) Remotely control [AFIS/TWR] j) ATFM/CDM k) Airspace management l) AIM dan SWIM m) Performance based navigations 4. Airport Engineering, Operation and Service a) Airport operation and management b) Airport eletricity c) Airport design, planning and maintenance d) runway maintenance e) KKOP f) Water Aerdrome g) Airport Mechanical h) Airport elektronics 5. Airline Industry a) Future airline industry b) Airline customer satisfaction c) Collaborative 6. Safety & Human Factor a) Safety management system b) Human fatigue risk management system c) Human factor d) Aviation Human resources Management 7. Aviation Business a) Logistic management b) Supply chain management c) Airport Business d) Airline Business e) Regulated Agent Business f) Multi mode transportation 8. Aviation Sustainability & Environment a) Environment sustainability b) Organization sustainability c) Noise management d) Carbon offsetting and reduction scheme for internasional aviation (CORSIA) e) Aviation meteorology 9. Aviation Educational Technology a) Instructional design b) Educational evaluation c) Advance learning d) Long life learning (elderly students) e) Aviation English 10. Innovation of Aviation Technology a) Unmanned vehicle b) Vehicle innovation c) Cyber technology d) Artificial Intelligent in Air transport system e) Airframe and power plant f) Aircraft technology 11. Aviation Rules and Regulation a) Air Law b) National Aviation Regulation c) International Aviation Regulation
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517 Documents
<![CDATA[PENGARUH ADMINISTRASI KEARSIPAN DAN PROFESIONALISME PEGAWAI TERHADAP KUALITAS PELAYANAN SUBAGIAN ADMINISTRASI PENDIDIKAN SEKOLAH TINGGI PENERBNAGAN INDONESIA CURUG TANGERANG ]]>
<![CDATA[Dini Wagini]]>
<![CDATA[ Langit Biru: Jurnal Ilmiah Aviasi Vol 12 No 1 (2019): Langit Biru: Jurnal Ilmiah Aviasi ]]>
Publisher : <![CDATA[Politeknik Penerbangan Indonesia Curug ]]>
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<![CDATA[Good service quality is a multidimensional assessment given to a service provider organization. To achieve optimal service quality need to be supported by some of the factors that influence it. This research was conducted in order to determine how much influence the archival and professionalism of employees to service quality subpart Administration Indonesia Civil Aviation Institute. The method used in this research is quantitative method, using statistics to help analyze the data obtained from the field. The main data was obtained by spreading questionnaires to a sample of 50 respondents, then processed using a correlation formula, determination and F test (Anova). The results showed that administration of archieves and competence of the employees have a strong correlation, evident from the calculation of 0.738. This shows the positive and significant correlation, then the coefficient of determination obtained for 54.5%while the remaining 45.5% influenced by other factors.]]>
<![CDATA[PERANAN SUMBER DAYA MANUSIA UNTUK MENDUKUNG MENINGKATKAN PRODUKTIFITAS PENELITIAN BIDANG PENERBANGAN PADA PUSAT PENELITIAN DAN PENGABDIAN MASYARAKAT DI SEKOLAH TINGGI PENERBANGAN INDONESIA ]]>
<![CDATA[Pribadi Asih]]>
<![CDATA[ Langit Biru: Jurnal Ilmiah Aviasi Vol 12 No 1 (2019): Langit Biru: Jurnal Ilmiah Aviasi ]]>
Publisher : <![CDATA[Politeknik Penerbangan Indonesia Curug ]]>
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<![CDATA[The research was aimed at finding out: first the background that made human resources of lecturer and the lower productivity in the field of aviation. Second, the steps that should be taken in solving such problems. Third, formulation that had been constructed by Pusat PPM STPI in improving productivity in the field of aviation. Data of the research had been collected though a qualitative methode by interviewing STPI lectures and, or researchers as informan. It had been found that most of informan were very low in research productivity due to various reasons. It could be because of their low interest in that field or they got less incentives compare that they obtained in teaching. Besides, a number of them still faced some problem in research methodology. It was suggested that unit PPM STPI should take an active role in improving the productivity of research in the field of aviation by conducting seminar, training, workshop, and other activities. Pusat PPM STPI should have strategic, planning for focusing on the environmental problems and involving more lectures and, or researchers progressing researchs. It is expected that in future more lectures and, or researchers would take active role in the field of research or other scientific activities..]]>
<![CDATA[METODA CRAMER UNTUK SOLUSI ANALISA RANGKAIAN LISTRIK MENGGUNAKAN SCILAB ]]>
<![CDATA[Khoirul Anam]]>;
<![CDATA[Yenni Arnas]]>
<![CDATA[ Langit Biru: Jurnal Ilmiah Aviasi Vol 12 No 1 (2019): Langit Biru: Jurnal Ilmiah Aviasi ]]>
Publisher : <![CDATA[Politeknik Penerbangan Indonesia Curug ]]>
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<![CDATA[Many problems in electrical circuit analysis are widely used mathematical models in their completion. The mathematical model is then formulated numerically in the Linear Equation System. The linear equation can be solved using several Numerical Methods, namely the Gauss Elimination Method, the Cramer method, the Inverse Matrix Method, the Gauss-Jordan Elimination Method and others. To calculate m equations with an unknown number of n variables from large and complex systems, it takes a long time and is not efficient. to complete large and complex mathematical calculations with an easy way to use the Scilab program. At this writing the authors limit only the completion of the Linear Equation System using Scilab with the Cramer Method.]]>
<![CDATA[RANCANGAN SISTEM HIDROLIK ALAT BANTU PENGANGKAT DAN PENURUN INTEGRATED DRIVE GENERATOR PADA PESAWAT AIRBUS 320 DI PT. GARUDA MAINTANANCE FACILITY AERO ASIA ]]>
<![CDATA[Ade Alfiansyah. S]]>;
<![CDATA[Ego Widoro]]>;
<![CDATA[Djudjur Prasodjo]]>
<![CDATA[ Langit Biru: Jurnal Ilmiah Aviasi Vol 12 No 1 (2019): Langit Biru: Jurnal Ilmiah Aviasi ]]>
Publisher : <![CDATA[Politeknik Penerbangan Indonesia Curug ]]>
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<![CDATA[When lowering and lifting the IDG with a weight of 56 kilograms in the IDG replacement process is done by positioning body that is not in a safe position. This is due to the unavailability of tools for IDG installation on Airbus 320 aircraft. Based on these problems, it is necessary to use IDG lifting and lowering devices with a hydraulic system. The first step to complete the design of the hydraulic system in this tool is to know the weight of the upper frame and the load from IDG so that the hydraulic system components needed such as actuators, hand pumps, flexible hoses, hydraulic fluids and fluid storage tanks can be calculated. The design of this tool uses an actuator with an inside diameter of 2.216 inch, an outside diameter of 2,294 inches and a length of 5 inches. Hydraulic hose with 0.223 inch inside diameter and outside diameter of 0.236 inch. Hand pump with a capacity of 1,376 inch3 and tank volume 19,811 inch3 . This tool can be used to assist the remove and installation of integrated drive generators on Airbus A320 aircraft at PT. Garuda Maintenance Facility after going through several test.]]>
<![CDATA[PERENCANAAN SALURAN LIMBAH CAIR DI GEDUNG TERMINAL BANDAR UDARA INTERNASIONAL AHMAD YANI SEMARANG ]]>
<![CDATA[Nurhedhi Desryanto]]>;
<![CDATA[Megananda Saraswati]]>;
<![CDATA[Oka Fatra]]>
<![CDATA[ Langit Biru: Jurnal Ilmiah Aviasi Vol 12 No 1 (2019): Langit Biru: Jurnal Ilmiah Aviasi ]]>
Publisher : <![CDATA[Politeknik Penerbangan Indonesia Curug ]]>
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<![CDATA[The planning of sewage system in terminal building of Internastional Ahmad Yani Semarang Airport is motivated by the process of building a new terminal building, so the procurement of sewerage facilities needs to be planned. The sewage channel is one of the supporting facilities at the airport. Planning of sewerage facilities must be in accordance with the rules of technical and operational standards. Based on the result of analysis and calculation, it can be concluded that the pipe length of sewage system is 916 m; diameter 12 inch. The soil elevation between the terminal Building and STP is increase 0,077%. The pipe elevation between the manhole is decrease 1% . The result of sewage of treatment will be streamed to ponding with capacity 106.702,08 m3. The data which is needed in this planning are the total passangers, soil polygon measurement, rainfall data and flight schedule of the airport.]]>
<![CDATA[KAJIAN KAPASITAS RUANG TUNGGU KEBERANGKATAN DOMESTIK DI BANDAR UDARA INTERNASIONAL SULTAN SYARIF KASIM II PEKANBARU ]]>
<![CDATA[Dien Amalia Putri]]>;
<![CDATA[Satiti Utami]]>;
<![CDATA[Kardi]]>
<![CDATA[ Langit Biru: Jurnal Ilmiah Aviasi Vol 12 No 1 (2019): Langit Biru: Jurnal Ilmiah Aviasi ]]>
Publisher : <![CDATA[Politeknik Penerbangan Indonesia Curug ]]>
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<![CDATA[Increasing the number of passengers every year and the limited capacity of the waiting room will affect the comfort level of service users, especially in the domestic departure lounge of Sultan Syarif Kasim II Pekanbaru Airport. During peak hours between 2:00 p.m. and 3:00 p.m. WIB, the density of passengers in the waiting room for domestic departures is seen. The piled up flight schedule adds to the density of the waiting room. In addition, many passengers who are standing and passenger space are uncomfortable, this is related to the capacity of the waiting room and the area of the waiting room per passenger. For this reason, the management of Pekanbaru's Sultan Syarif Kasim II Airport needs to increase the capacity of domestic departure waiting rooms through the addition of additional space or the addition of waiting rooms and facilities to support activities in the waiting room at present. The use of international departure waiting rooms can also be an alternative to accommodate departing (domestic) passengers during rush hour so that the density in the domestic departure lounge can be reduced. With this research, it is expected that the manager of Pekanbaru Sultan Syarif Kasim II Airport can realize a comfortable departure lounge atmosphere in accordance with service level standards in accordance with the Director General of Civil Aviation Decree Number: SKEP 347 / XII / 1999 concerning Design Build and / or Engineering Airport Facilities and Equipment as well as the Minister of Transportation Regulation of the Republic of Indonesia Number PM 178 of 2015 concerning Standards for Airport Service Users.]]>
<![CDATA[RANCANGAN ALAT MONITORING PERUBAHAN SUHU PADA SHELTER VOR (VHF OMNIDIRECTIONAL RANGE), SHELTER GLIDE PATH DAN SHELTER LOCALIZER BERBASIS SMS GATEWAY DI BANDAR UDARA INTERNASIONAL HANG NADIM BATAM ]]>
<![CDATA[Ahmad Rizaldy]]>;
<![CDATA[Feti Fatonah]]>;
<![CDATA[Bambang Wijaya Putra]]>
<![CDATA[ Langit Biru: Jurnal Ilmiah Aviasi Vol 12 No 1 (2019): Langit Biru: Jurnal Ilmiah Aviasi ]]>
Publisher : <![CDATA[Politeknik Penerbangan Indonesia Curug ]]>
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<![CDATA[By looking at the current conditions the author tries to design a tool that can find out the temperature when an alarm occurs in the equipment room over long distances so that it can be immediately known by the technician to then check the location of the equipment. The working principle of this tool is when the temperature sensor detects temperature changes above the specified limit then the sensor will provide input to the Arduino which then Arduino will turn on the buzzer that is in the VOR shelter, Glide Path and Localizer. Then the transmission media can send SMS warning messages to the technician. After that to make sure whether the SMS is correct, the technician can see the alarm indicator on the VOR shelter, Glide Path and Localizer, because there are cameras installed in the VOR shelter, Glide Path and Localizer. So that technicians can immediately find out without having to come to the location of the equipment and can immediately overcome it. With this temperature detection design it is expected that the temperature conditions at VOR shelter, Glide Path and Localizer can be monitored at any time over long distances by the technician without having to come to the equipment location, this means that it will facilitate the technician's work in knowing the condition of the equipment's room temperature and in anticipation of damage to the equipment.]]>
<![CDATA[RANCANGAN SIMULASI APPRAOCH LIGHTING SYSTEM BANDAR UDARA MENGGUNAKAN MICROSOFT VISUAL STUDIO 2015 DI SEKOLAH TINGGI PENERBANGAN INDONESIA ]]>
<![CDATA[Muhammad Fajar]]>;
<![CDATA[Zulina Kurniawati]]>;
<![CDATA[Agus Herianto]]>
<![CDATA[ Langit Biru: Jurnal Ilmiah Aviasi Vol 12 No 1 (2019): Langit Biru: Jurnal Ilmiah Aviasi ]]>
Publisher : <![CDATA[Politeknik Penerbangan Indonesia Curug ]]>
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<![CDATA[At this time cadets experienced some problems in the implementation of practice in Airfield Lighting System subject, due to the props that can not be used properly. The designed Approach Lighting System Simulation is intended as one solution to the problem, and it is a new idea to be used in practical activities, especially regarding to the Approach Lighting System configuration. This simulation design was created using Microsoft Visual Studio 2105 programming language where its result will be able to describe some configuration of Approach Ligthing System. In the end the authors hope this simulation design can provide benefits in the enrichment of subject matter practice materials in Airfield Lighting System course of Airport Electrical Engineering, Department of Aviation Engineerring, Indonesian Civil Aviation Institute. It is also suggested that the application programming language Microsoft Visual Studio 2015 can be developed further in designing learning simulations for other subjects in the Airfield Lighting System subject.]]>
<![CDATA[ANALISIS KESALAHAN PENUNJUKAN INDIKATOR TEKANAN BAHAN BAKAR DITINJAU DARI KERUSAKAN TRANSDUCER PADA PESAWAT SOCATA TB-10 DI SEKOLAH TINGGI PENERBANGAN INDONESIA CURUG-TANGERANG ]]>
<![CDATA[Bela Firmantoyo]]>;
<![CDATA[Sihono]]>
<![CDATA[ Langit Biru: Jurnal Ilmiah Aviasi Vol 12 No 1 (2019): Langit Biru: Jurnal Ilmiah Aviasi ]]>
Publisher : <![CDATA[Politeknik Penerbangan Indonesia Curug ]]>
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<![CDATA[Trainer aircraft type Socata TB-10 is one of the types of aircraft piston engine (engine) used by Indonesian Civil Aviation Institute. The aircraft began to be used for flight training for cadets STPI Airmen Department since August 1997. During operation of the Socata TB-10 aircraft within a certain time there is a mistake appointing fuel pressure indicator on all Socata TB-10 aircraft that existed at Indonesian Civil Aviation Institute Curug-Tangerang. This designation errors either low pressure, high pressure in the run-up both positions, climbing cruising and landing. To support error analysis designation fuel pressure indicator required some theories that the aircraft fuel system TB-10, the designation system fuel pressure, transducer, transducer sensitivity. To solve these problems required transducer calibration test of the fuel components. Testing was conducted at the Indonesian Institute of Sciences Research Center Instrumentation Calibration and Metrology (KIM-LIPI). Based transducer calibration test and results analysis is, the cause of the error designation fuel pressure indicator in terms of damage to the fuel pressure transducer is rated third transducer sensitivity tested had a sensitivity value greater than the allowed value sensitivity (standard). Resulting voltage change corresponding outgoing errors resulting in the appointment of a fuel pressure indicator on the Socata TB-10 aircraft owned by Indonesian Civil Aviation Institute Curug-Tangerang.]]>
<![CDATA[RANCANGAN JADWAL BUKA TUTUP OPERASI OTOMATIS BERBASIS ARDUINO UNO DI GERBANG CEWAMA ASRAMA CURUG 1 SEKOLAH TINGGI PENERBANGAN INDONESIA .pdf ]]>
<![CDATA[Dena Farasi]]>;
<![CDATA[KGS. M. Ismail]]>;
<![CDATA[R.B. Budi Kartika W]]>
<![CDATA[ Langit Biru: Jurnal Ilmiah Aviasi Vol 12 No 1 (2019): Langit Biru: Jurnal Ilmiah Aviasi ]]>
Publisher : <![CDATA[Politeknik Penerbangan Indonesia Curug ]]>
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<![CDATA[In the Curug 1 ICAI Dormitory, there is a gate which connect between the main road and the dormitory. The gate is the main access for cadet to enter and exit the dormitory. The system work with Arduino 4 Input Microcontroller (2 analogs, 2 digitals), Real Time Clock module with CR2032 battery type and I2C Communication (SDA, SCL). Microcontroller will activate relay that capable to handle 220 volts of voltage and 10 Ampere of currents. Then Relay will give a cue to contactor and activate the Electric Motor as Prime Mover. The cable which used to connect RTC module to Arduino UNO is AWG cable 39 for 0.018 Ampere of Currents and AWG cable 11 for 12 Ampere of Currents to connect between Relay and Electric Motor. This following steps to program Arduino UNO : Activate the RTC module, Relay 1 and Relay 2 according to the specified time, download the DS3231 file, display the time planting program, and display the “current time”. With the application of the automation gate, it’s expected open-close gate automatically according to schedule which has specified.]]>
