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      جزوه آموزشی دوره ی ESPM و Aircraft Wiring Manual

      ۵۶,۲۰۶ تومان

      The Electrical Standard Practices Manual (ESPM) gives descriptive data and procedures for the electrical
      installations on all aircraft of the AIRBUS family.
      The standard practices information in this manual tells you how to do maintenance and repairs on the standard
      electrical items and thus ensure the continued airworthiness of the aircraft.

      دانلود ترجمه ی کامل انکس 19

      ۴۰,۲۵۰ تومان

      کنفرانس ایمنی سطح بالای ICAO برگذار شده در سال 2010 عزم هایی را جهت ایجاد یک انکس جدید مختص به مدیریت ایمنی فراهم آورد.

      کنفرانس به این جمع بندی رسید که فرآیندهای مدیریت ایمنی تحت مسئولیت مستقیم دولت ها که برای ایمنی هوانوردی تجاری حیاتی می باشند باید در یک انکس جداگانه گنجانده شوند:

      • شامل چهارچوب برنامه ایمنی دولت (SSP) و 8 عنصر مهم یک سیستم نظارت بر ایمنی؛
      • پوشش فعالیت های عمومی و تجاری هوانوردی؛ و

      احراز ملزومات سیستم مدیریت ایمنی (SMS) ویژه یک حیطه از فعالیت های در انکس های جداگانه.

      دانلود جزوه ی SMS (safety management system)

      ۱۰,۹۲۵ تومان

      – جزوه به صورت آماده شده  PDF   میباشد و به زبان انگلیسی .

      • فایل آموزشی جهت ایرلاین های معتبر داخلی

      -SMS (safety management system)

      دانلود جزوه Aircraft fuel systems

      ۷,۳۶۰ تومان

      This chapter is going to address three areas dealing with fuel, these are:

      ۱-The types of aviation fuels used and their physical properties

      ۲-The types of airframe fuel systems

      ۳-The safety regulation regarding refuelling of aircraft

      دانلود جزوه Empennage or Tailplane aircraft

      ۴,۳۷۰ تومان

      Introduction For conventional aircraft, the empennage or tailplane normally takes the form of a single vertical fin and horizontal surface, these are fitted to give the aircraft directional and longitudinal static stability respectively and are mounted at the tail [rear] of the aircraft.

      دانلود جزوه Wing Structures aircraft

      ۶,۶۷۰ تومان

      Wings were previously referred to as main planes; they produce the lift that supports the aircraft in flight. When air flows over the top surface of a wing from the leading edge [Le] to the trailing edge [Te] the distance that it has to travel is increased by the camber [curve] of the surface compared with the distance that it would have to travel when passing under the wing, as shown in diagram 3.1 above. The air flowing over the cambered surface increases its velocity, which results in a decrease in the static pressure above the wing. The amount of lift produced is dependent on the speed of the air over the wing, the camber and the surface area of the wing.

      دانلود Introduction to Structures & fuselage

      ۵,۶۲۱ تومان

      Since the advent of powered flight aircraft designers and manufacturers have made use of available technology, striving to build aircraft that are faster and can carry a greater load a greater distance than their previous design and their rivals. Competition to produce the best machine has fuelled research and development; the dramatic leaps in aviation technology were made in the First, Second and Cold Wars of the twentieth century.

      The fuselage forms the main body of the aircraft to which the wings, tail plane, canards, vertical fin and in the case of a single engine aircraft the engine is attached. In some aircraft designs the landing gear is also directly attached to the fuselage structure.