Start Discovering Solved Questions and Your Course Assignments
TextBooks Included
Active Tutors
Asked Questions
Answered Questions
maintenance of aircraft under ldquobrdquo conditions the maintenance of aircraft flying under b conditions must be adequate in relation to the
aircraft weighingnote the caa will consider applications from aircraft constructors and operators to weigh certain types of aircraft on
aircraft weight and balance - reference bcar a5-4 or jar-2523 -29after an aircraft has been constructed painted and can be said to be
aircraft internal and external markingssmoking in aircraft - reference ano article 66 and jar-25791every aircraft registered in the uk must have a
aviation legislation - registration of aircraftall aircraft must be registered in the uk before they are permitted to fly they must also have their
aviation legislation - certificate of designduring the construction the manufacturer has to provide the caa with a certificate of design and also a
design construction and type certificatethe following chapter covers the initial design construction registration and test flying of the first
static electricity in aircraftas mentioned earlier the effects of static electricity are of considerable importance in the design of aircraft and
fuel system inhibiting the fuel used in turbine engines usually contains a small quantity of water which if left in the system could cause corrosion
engine firesthere are two main types of engine fire that can occur when running gas turbine engines and they are dealt with in different ways1 fire
re-heat after burningre-heat is a system fitted to a gas turbine engine as a means of increasing the total thrust as much as twice the thrust can be
external air tappingsengines vary as to the number of external air tappings and their usage the following notes are taken from the pratt and whitney
fuel properties of aircraftease of flowthe ease of flow of a fuel is mainly a question of viscosity but impurities such as ice dust wax etc may cause
gas turbine fuel properties and specificationin the earliest days of the gas turbine engine kerosene was regarded as the most suitable fuel it
combustion sectionthe combustion chamber has the difficult task of burning large quantities of fuel supplied through the fuel burners with extensive
application to the axial flow compressorin order for the compressor to deliver a high mass airflow for a minimum effort required to drive it it is
compressor stall and surgelsquosurge can occur in both centrifugal and axial flow compressors and is the reversal of the airflow in the compressor
ideal intake conditionsfor air to flow smoothly through a compressor its velocity should be about 05 mach at the compressor inlet this includes
equivalent shaft horsepower ehpin practice there is always a certain amount of jet thrust in the total output of the turbo-propeller engine and this
choked nozzleconsidering the formula for thrust under quotchokedquot nozzle conditions thrust p-p0 a wvj g where p pressure p
thrust calculationthe amount of thrust produced depends upon two things-the mass of air which is moved rearwards in a given time the acceleration
principles of jet propulsionnewtons laws of motion to understand the basic principles of jet propulsion it is necessary to understand the practical
reliability design scientifically allocate the reliability for the target product and subsystems all the way down to their component and partsconduct
the pn junction region of the junction diode has the following significant characteristicssemiconductors contain two types of mobile charge carriers