PENENTUAN INTERVAL PENGGANTIAN SUKU CADANG KOMPONEN KRITIS PESAWAT UDARA KALIBRASI
<b>Abstract :</b><p align="justify">The Accurence of Unscheduled Removal for Calibration aircraft Lear Jet 31-A rotable components before TBO (Time Between Overhaul) indicates the low level of component realibility, so that determination of maintenanc reschedule. From the...
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| Format: | Theses |
| Language: | Indonesia |
| Online Access: | https://digilib.itb.ac.id/gdl/view/4972 |
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| Institution: | Institut Teknologi Bandung |
| Language: | Indonesia |
| Summary: | <b>Abstract :</b><p align="justify">The Accurence of Unscheduled Removal for Calibration aircraft Lear Jet 31-A rotable components before TBO (Time Between Overhaul) indicates the low level of component realibility, so that determination of maintenanc reschedule. From the data rotable components damages are collected, and the critical component are further detrmined by both Multi Criteria system and system of VESO ( Vital Category, Essensial Category, Support Category, and Operation Category), sample are obtained <br />
1. Electronic Display Unit. <br />
2. Fuel Pump <br />
3. Main Gear Actuator. <br />
4. Nose Gear Actuator. <br />
5. Compressor Motor. <br />
6. Brake Assembly. <br />
7. Wheel Hub. <br />
Data of samples component damage are then tested their goodness of fit the statitistical distribution, so the Weibull distribution for two parameter can satisfy the suggested model. <br />
The result of data processing, the following are obtained : <br />
Electonic Display Unit 494.79 300 96.82 <br />
Fuel Pump 652.62 600 97.35 <br />
Main Gear Actuator 648.20 300 98.82 <br />
Nose Gear Actuator 802.10 300 99.02 <br />
Compressor Motor 522.17 300 97.52 <br />
Brake Assembly 601.32 300 98.32 <br />
Wheel Hub 721.38 600 0.9792 |
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