ANALISIS DRIFT DOWN PESAWAT ATR 72-500 RUTE LAMPUNG-PADANG PADA KONDISI ONE ENGINE INOPERATIVE

FAJRI, KHAIRUL (2019) ANALISIS DRIFT DOWN PESAWAT ATR 72-500 RUTE LAMPUNG-PADANG PADA KONDISI ONE ENGINE INOPERATIVE. Skripsi thesis, Institut Teknologi Dirgantara Adisutjipto.

[img] Text (ABSTRAK)
14050056_ABSTRAK.pdf

Download (148kB)
[img] Text (BAB I)
14050056_BAB I.pdf

Download (156kB)
[img] Text (DAFTAR PUSTAKA)
14050056_DAFTAR PUSTAKA.pdf

Download (85kB)
[img] Text (FULL SKRIPSI)
14050056 - converted.pdf
Restricted to Repository staff only

Download (1MB)

Abstract

ATR 72-500 is an aircraft used for flights with short routes. On the island of Sumatra many types of ATR 72-500 aircraft are used for inter-provincial flights. Sumatra Island itself has hilly and mountainous contours. When planes fly through this area, the aircraft can experience one engine inoperative, and the aircraft will experience a drift down. In this study carried out on the Lampung-Padang flight route. Calculation of drift down needs to be done to find out how much decrease occurs when the aircraft experiences one engine inoperative. Drift-down analysis is done by considering take-off weight, wind, fuel consumption, and water temperature. Based on the calculations and analysis carried out when the aircraft drift - down, the aircraft will slowly decrease in height to a certain distance, a certain time, and a certain weight and then the aircraft will maintain its altitude. The decrease with the largest vertical speed of 69.7 ft / min occurs when the aircraft weight in take-off weight (TOW) is 22,000 kg and drift down occurs at a distance of 36 NM from the origin airport. The lowest vertical speed occurs when TOW 20843 kg with a large vertical speed of 38,1 ft / min at 316 NM from the origin airport. On the Lampung-Padang route, the aircraft was declared safe to continue the flight to the destination airport when the aircraft experienced a single engine and drift down with 100% load at a distance after 196 NM from the departure airport. In the condition of 95% load, the aircraft will be safe at a distance after 136 NM. With an 90% load and with a small a distance of 36 NM

Item Type: Thesis (Skripsi)
Subjects: T Technology > T Technology (General)
Divisions: Institut Teknologi Dirgantara Adisujtipto > Teknik Dirgantara
Depositing User: Mr KHAIRUL FAJRI
Date Deposited: 20 Jun 2024 06:13
Last Modified: 20 Jun 2024 06:13
URI: http://eprints.stta.ac.id/id/eprint/1951

Actions (login required)

View Item View Item

Downloads

Downloads per month over past year