IL.II.N.S1
SkillOperate the pressurization system, if equipment is installed.
From the FAA library
- Chapter 8: Flight Instruments › Static Pressure Chamber and Lines
Operating Handbook (POH) to determine the amount of error that is introduced into the system when utilizing the alternate static source. In an aircraft not equipped with an alternate static source, an alternate method of introducing static pressure into ... aircraft above a given pressure level. Pressure levels are discussed later in detail. Since the altimeter is the only instrument that is capable of indicating altitude, this is one of the most vital instruments installed in the aircraft…
- Chapter 7: Aircraft Systems › Superchargers and Turbosuperchargers › Turbosuperchargers
supercharger control is switched to the high blower position. The throttle is then reset to the desired manifold pressure. An engine equipped with this type of supercharger is called an altitude engine. [Figure 7-14] Turbosuperchargers The most efficient method ... supercharged engine. Installed on an engine, this booster uses the engine’s exhaust gases to drive an air compressor to increase the pressure of the air going into the engine through the carburetor or fuel injection system to boost power…
- Chapter 7: Aircraft Systems › Oxygen Systems › Servicing of Oxygen Systems
installed oxygen tanks usually require two persons to accomplish servicing of the system. One should be stationed at the service equipment control valves, and the other stationed where he or she can observe the aircraft system pressure gauges. Oxygen system ... servicing is not recommended during aircraft fueling operations or while other work is performed that could provide a source of ignition. Oxygen system servicing while passengers are on board the aircraft is not recommended. Figure 7-46. EDS-011 portable…
- 14 CFR § 91.219 Altitude alerting system or device: Turbojet-powered civil airplanes.
that is in operable condition and meets the requirements of paragraph (b) of this section. (b) Each altitude alerting system or device required by paragraph (a) of this section must be able to— (1) Alert the pilot— (i) Upon approaching ... highest operating altitude approved for the airplane in which it is installed; (3) Preselect altitudes in increments that are commensurate with the altitudes at which the aircraft is operated; (4) Be tested without special equipment to determine proper operation…
- Chapter 12: Hydraulic & Pneumatic Power Systems › Valves › Pressure Control Valves
efficient operation of fluid power systems, system components, and related equipment requires a means of controlling pressure. There are many types of automatic pressure control valves. Some of them are an escape for pressure that exceeds a set pressure; some ... pressure to a lower pressure system or subsystem; and some keep the pressure in a system within a required range. Relief Valves Hydraulic pressure must be regulated in order to use it to perform the desired tasks. A pressure relief…
- Chapter 8: Engine Removal & Replacement › Checks & Adjustments After Engine Runup & Operation
electrically actuated may be checked before the engine is operated. Propellers whose pitch-changing mechanisms are oil actuated must be checked during engine operation after the normal operating oil temperature has been reached. In addition to checking the increase ... Runup & Operation After the engine has been ground operated, and again after flight test, operational factors must be adjusted, as necessary, and the entire installation given a thorough visual inspection. These adjustments often include fuel pressure and oil pressure…