Job Description (JD)
| Nama Program | OPERASI PENYELENGGARAAN PESAWAT DAN PERSIJILAN [TP-060-4:2013] |
|---|---|
| Kod CU | TP-060-4:2013-E02 |
| Competency | Elektif |
| Tajuk CU | Aeroplane Piston Maintenance ATA 72(R), 73-80 (Module 11B, 16 & 17) |
| Penerangan CU | Aeroplane piston maintenance is to maintain aircraft piston system (with limited release approval) in accordance with the requirement of the Original Equipment Manufacturer (OEM), Department of Civil Aviation Malaysia (DCAM) and other regulatory bodies such as European Aviation Safety Agency (EASA), Federal Aviation Administration (FAA), Civil Aviation Authority (CAA), Civil Aviation Safety Authority (CASA). The Competency Unit (CU) of Aeroplane piston maintenance is developed based on Air Transport Association (ATA) System Chapter 100. The relevant chapters under ATA 100 are the following: - Chapter 72(R) (Engine) (Reciprocating/ Piston) The personnel who are competent in aeroplane piston maintenance shall be able to identify, inspect, replace, and test, record and certify piston systems to meet continuous airworthiness standards. The outcome of this competency is to develop competent manpower in accordance with company’s Standard Operating Procedures (SOP) and job description. |
| Tempoh Latihan | 400 |
| Objektif Pembelajaran | Aeroplane piston turbine maintenance is to maintain aeroplane piston turbine system (with limited release approval) in accordance with the requirement of the Original Equipment Manufacturer (OEM), Department of Civil Aviation Malaysia (DCAM) and other regulatory bodies such as European Aviation Safety Agency (EASA), Federal Aviation Administration (FAA), Civil Aviation Authority (CAA), Civil Aviation Safety Authority (CASA). The personnel who are competent in aeroplane piston turbine maintenance shall be able to:- • Identify basic requirement on aircraft maintenance • Identify aeroplane piston turbine components • Inspect aeroplane piston turbine component • Replace aeroplane piston turbine component • Test aeroplane piston turbine component |
| Pra-Syarat | 0 |