Title: DCO11611 Aviation Operations
1DCO11611Aviation Operations
2 Dr. Joseph Chan email dcjcchan_at_cityu.edu.hk
http//personal.cityu.edu.hk/dcjcchanOffice
P6821 Main Campus Phone 2788-8207
3 Consultation Hours (at Telford)Monday 330
430 pmTuesday 230 330 pm During these
hours you can call me at phone 2707-9086and I
can meet you at the counter
4 Assessments Final Exam 70 Course Work
30 Mid-term Quiz Lab Exercises
5What is this Course About?
- The basic structures and functions of airplane
components - The aerodynamics of flying
- Equipments of a modern plane
- Navigation and communications processes
- Flight regulations and laws
- Meteorology that affects safe flying
- Human physiology and psychology that affects safe
flying - Similar to Private Pilot License (PPL) Exam
6Cathay Pacific Aircadets Training Program
- Structures of airplanes
- Aerodynamics
- Principles of aviation wireless communication
- Aviation Navigation
- Aviation Meteorology
- Principles of Aviation Planning
- (Australian) Aviation Laws and Regulations
- Aviation Physiology
7My academic background
- BSc., M.Sc. and Ph.D. Candidacy in Physics
- M.Engr. in Electrical and Computer Engineering
- Ph.D. in Neuroscience (Physiological Psychology)
8Flight Training Programs in HK
- Cathay Aircadets Training Program
- www.aircadets.org.hk/plttrg_e.html
- Hong Kong Aviation Club
- http//www.hkaviationclub.com.hk/
- Dragonair
- http//www.dragonair.com/icms/servlet/template?ser
ies59langbig5
9Textbooks for the course
- Jeppesen. Private Pilot Manual. Sanderson
Training Products. - (Manual for PPL License Exam, but expensive
U.S. 80). - Kroes and Rardon. Aircraft Basic Science (7th
ed.). McGraw-Hill International Edition. 1993. - (Good for the fundamental principles)
10 - Lecture 1
- Jeppesen. Chapters 1, 2
11Human efforts to try to fly Milestones (1)
- 1783 First manned flight in history hot air
balloon rose near Paris - 1881 Two German brothers flew with a
heavier-than-air machine glider from a
hill - 1903 Wright brothers achieved the first
powered, sustained and controlled airplane
flight in U.S. - 1927 First trans-continental flight from New
York to Paris in 33 hours, 30 minutes and
29.8 seconds - 1932 First woman to pilot an airplane solo
across the Atlantic Ocean
12Human efforts to try to fly Milestones (2)
- 1939 First turbojet in the world in Germany
- 1942 First turbojet in the U.S.
- 1947 First super-sonic flight 700 mph at
42,000 feet - 1961 First manned spaceship from Russia
- 1969 First man on the moon
- 1986 First non-stop-without-refueling flight
around the world. Took 9 days, 3 minutes,
and 44 seconds. The 7,011.5 pounds of fuel was
72.3 of the airplanes gross weight - 2003 Chinas first manned spaceship
13Basic components of airplane
- All planes basically have the same structural
components - Fuselage
- Wings
- Power plant
- Landing gear
- Empennage
14Basic components of airplane
15Basic Components of Airplane
16The fuselage
- Cockpit control of the plane
- Cabin contains seats of passengers
- Room for cargo
- Attachment points for other major airplane
components - Fuselage in early planes used open truss
structure. Modern planes uses stressed skin,
known as - monocogue no supporting truss, for light planes
- semi-monocoque - has truss members for support
17The fuselage Fig 2-3 Open Truss
18The fuselage Fig 2-4 Semi-monocoque
19The Wings
- When air flows around the wings of a plane it
generates a lifting force - Wing are designed to maximize this lift
- Monoplanes have one set of wings. Biplanes have
two sets. Fig 2-4 - Monoplanes wings can be attached to the top of
the fuselage (high-wing), to the middle
(mid-wing), or the lower portion (low-wing).
20Monoplane and Biplanes Fig 2-4
21The Wings
- Attached to the rear edge of each wing are two
types of control surfaces called aileron and flap
respectfully - Ailerons extend from about the mid-point of the
wings to near the tips. - Ailerons of the two wings moves up and down in
opposite directions to create aerodynamic forces
that cause the plane to turn. - When the wheel is turned left the left aileron
moves up and the right moves down. The plane
then turns left.
22The Wings
- The flap extends from the side of the fuselage to
about the mid-point of each wing. - In normal flight the flap is parallel to the
surface of the wings surface. - The flaps move simultaneously downwards to
increase the lifting force of the wings during
takeoffs and landing. - Flaps are controlled by a switch or a handle in
the cockpit.
23The Empennage
- The empennage is the tail of the plane. It
consists of the horizontal stabilizer and the
vertical stabilizer, (the vertical stabilizer is
also referred to as the fin). - These two stabilizers help the plane to maintain
a straight path through the air - The empennage also consists of the rudder which
is attached to the back of the vertical
stabilizer - Also, an elevator is attached to the back of the
horizontal stabilizer (Fig 2-7)
24The Empennage Fig 2-7
25The Empennage - Rudder
- The rudder helps to move the nose of the plane to
left or right - It is used together with the ailerons to turn the
plane - The rudder is controlled by the pilots feet with
pedals. The left pedal moves the rudder to the
left and helps turn the plane to the left. The
right pedal turns the plane to the right.
26The Empennage - Elevator
- An elevator is attached to the back of the
horizontal stabilizer - The elevator is used to move the planes nose up
and down during flight, directing the plane to go
higher or lower - The elevator is controlled by the wheel. When
the pilot pulls the wheel back, the elevator and
the nose move up. When the pilot pushes the
wheel down, the elevator and the nose move down.
27The Empennage - Stabilator
- Some planes combine the horizontal stabilizer and
the elevators into one piece called the
stabilator. - The stabilator is hinged up and down at a center
point. - When the control wheel is pulled back, the
stabilator and the nose move up. When the wheel
is pushed down, the stabilator and the nose move
down.
28The Empennage Trim Devices
- Some planes use small pieces of surfaces attached
to the control surfaces mentioned above. These
are generally called trim devices. (Fig 2-10) - Trim devices exploit aerodynamic force of the air
to adjust the workload needed to move the other
control surfaces or to maintain those surfaces at
a desired position.
29Trim Devices Fig 2-10
30The Empennage Trim Devices
- An example of trim devices is the trim tab which
is attached at the tail edge of the elevator and
is commonly used in many training planes. It
lessens the air resistance the pilot feels when
moving the elevator. - Another example is the trim used in a stabilator
to provide more resistant feel so that the
control feels more like that of an elevator.
31Landing Gear
- The landing gear absorbs the shock upon landing
and supports the plane on the ground. - Typically the landing gear consists of three
wheels two main wheels on either side of the
fuselage, and a third wheel either at the front
or at the rear. Landing gear using a rear wheel
is called a conventional landing gear and a plane
using conventional landing gear is called a
tailwheel airplane. (Fig 2-11)
32Tailwheel airplane 2-11
33Landing Gear - Nosewheel
- When the third wheel is located at the front it
is called a nosewheel. Most modern plane uses
this design. (Fig 2-12) - Nosewheels are either steerable or castering.
- Steerable nosewheels are connected to the rudder
through cables and rods while castering
nosewheels are not.
34Nosewheel airplane 2-12
35Landing Gear - nosewheels
- The pilot steers the plane using the rudder
pedals in both types of nosewheels. - If the nosewheel is of the steerable type,
pushing the left rudder forward will turn that
wheel to the left, thus turning the plane left
while taxiing - If the nosewheel is of the castering type the
pilot may have to combine the use of the rudder
pedals with independent use of the brakes
(pushing the rudder downwards) on the main
wheels, particularly on tight turns.
36Landing Gear Fixed or Retractable
- Landing gears can be classified as either fixed
or retractable depending whether the landing gear
can be retracted or not. - Fixed gear always remains extended.
- The advantage is simplicity and low cost.
- The disadvantage is having more air resistance.
- Retractable gear is designed to streamline the
airplane to reduce friction. - The disadvantage is increased weight and cost.
It is normally used only in high performance
planes.
37Landing Gear Water Operation
- Long time ago, before runways were available,
planes took off and descended over water. - Nowadays many landplanes are still fitted with
twin floats that support them on water for use in
remote areas where runways or even long strip of
land are not available. These type of airplanes
are referred to as seaplanes.
38Landing Gear Water Operation
- Some airplanes can be operated both on land and
on sea, and are called an amphibian. - Amphibian planes have the fuselage designed like
a boat, with floats attached to the wings to
increase support during water operations. They
use retractable wheels for land operations.
39Landing Gear Struts
- The wheels are attached to the fuselage through
struts, which reduce the sudden shocks during
landing or taxiing on rough grounds. - Spring steel and bungee struts do not actually
absorb shocks but reduce their suddenness. (Fig.
2-14) - Most planes nowadays use oleo struts which are
true shock absorbers. - An oleo strut uses a piston enclosed in a
cylinder with oil and compressed air to absorb
the shock. (Fig. 2-15)
40Struts spring steel bungee (2-14)
41Struts Oleo absorber (2-15)
42Brakes
- Typical training planes use disc brakes on the
main wheels - Equal pressure can be applied to the two brakes
simultaneously by pressing (downwards) equally on
the top of each rudder pedal, in order to slow
down the plane in a straight line. - The brakes can also be applied to varying degrees
independent of each other. This would help steer
the plane during ground operation. This
technique is called differential braking.
43The Powerplant
- In small planes the powerplant consists of the
engine and the propeller. - The engine provides the power to turn the
propeller, which in turn, provides the thrust to
move the plane through the air. - The engine is enclosed by a cowling, which, in
addition to provide streamlining for the nose,
helps cool the engine by ducting outside air
around the engine cylinders. (Fig. 2-18)
44A cowling (opening) is seen behind the propeller
(2-18)
45POH, AFM, and PIM
- Most of the pertinent information about a
particular plane in contained by the Pilots
Operation Handbook (POH) provided by the planes
manufacturer. The format of POH for all planes
are standardized. - The Federal Aviation Administration (FAA)
requires that all planes built after March 1,
1979 be equipped with an FAA approved airplane
flight manual (AFM) which is specifically
assigned to the individual airplane. - The FAA requires that the AFM for each plane be
accessible by the pilot all the time when
operating that plane.
46POH, AFM, and PIM
- To compile with the FAAs requirement
manufacturers then write their POH just like the
AFM. - The POH/AFM has to stay with the plane all the
time during operation and is therefore not
available to others to review for a lengthy
period of time. As a result the manufacturer
also publish a pilots information manual (PIM). - The PIM contains the same information as the
POH/AFM except for precise weight and balance
data and optional equipment specific to the
particular plane.
47Contents of AFM 10 Sections
- General basic information terminology
- Limitations includes operating limitations
- Emergency procedures
- Normal procedures
- Performance
- Weight and balance
- Airplane and system description
- Handling, Service and maintenance
- Supplements
- Safety and operational tips
48Summary
- An airplane generally contains the following
- Fuselage
- Wings
- Empennage
- Landing gear
- Powerplant
- Airplane flight manual (AFM)