Airplane and Pilot Performance

Slides:



Advertisements
Similar presentations
The Truth… About Stalls
Advertisements

Web site hyperlinks Weather ADDS - Aviation Digital Data Service Homepage FAA tests (FAA web) Pilot Testing FAA web site (General info) FAA Home Page.
Retreating Blade Stall
Regional Gliding School u Occurs when the wing is no longer capable of producing sufficient lift to counteract the weight of the aircraft. A smooth.
Aerodynamic Theory Review 2
Airfoils, Lift and Bernoulli’s Principle
#4908.If, while in level flight, it becomes necessary to use an alternate source of static pressure vented inside the airplane, which of the following.
Theory of Flight Flight Performance
Airplane Flight: X-Plane in the Classroom Wing Loading Ratio of the plane’s weight (w) divided by the surface area of the wing (s)
Bernoulli's Principle It explains why and airplane gets lift
Steep Turns.
P449. p450 Figure 15-1 p451 Figure 15-2 p453 Figure 15-2a p453.
Predicting Performance
Flight Instruments Which way’s up?
6.06 Loads and Load Factor References: FTGU pages 17-18, 34-35
6.06 Loads and Load Factor References: FTGU pages 17-18, 34-35
Aero Engineering 315 Lesson 30 Turn Performance. “Turning” the tables…
6.09 Flight Instruments and Performance Factors
Review Chapter 12. Fundamental Flight Maneuvers Straight and Level Turns Climbs Descents.
Introduction to Aeronautical Engineering
LIFT.
Takeoff Performance Jet Aircraft Performance
Aerodynamic Theory Review 3
Warm-Up – 5/7 – 10 minutes Utilizing your notes and past knowledge answer the following questions: Describe the effect of a tailwind and headwind on an.
MAE 3241: AERODYNAMICS AND FLIGHT MECHANICS
AVAT11001: Course Outline Aircraft and Terminology
Aviation Seminars1 #3248. Which instrument will become inoperative if the pitot tube becomes clogged? A- Altimeter. B- Vertical speed. C- Airspeed.
Bronze C Theory The Principles of Flight. Terms Wing Section Chord line Mean Camber line Airflow Relative Airflow Boundary layer Stagnation point Angle.
Structural Design Considerations and Airspeeds
Airplane Flight: X-Plane in the Classroom Four Forces Of Flight Weight Lift Drag Thrust.
6.07 Stalls References: FTGU pages 18, 35-38
Basic Aeronautics Know the principles of basic aeronautics. 1. Describe the effects of angle of attack. 2. Identify the four forces of flight.
Basic Aeronautics Know the principles of basic aeronautics. 1. Describe the effects of angle of attack. 2. Identify the four forces of flight. Lesson.
The Private Pilot.
Forces in Fluids Chapter 13. Fluid Pressure  Section 13-1.
Performance Charts.
Flight Air Foils and the Angle of Attack. Wings The shape of a wing is called an “airfoil.” Airfoil: a streamlined shape with a rounded front edge and.
Advanced Weight & Balance
Topic of the Month November
ROTARY WING AERODYNAMICS
Flight Instrumentation
Airfoils, Lift and Bernoulli’s Principle
© 2009 Aviation Supplies & Academics, Inc. All Rights Reserved. The Pilot’s Manual – Ground School Aerodynamics Chapter 1 Forces Acting on an Airplane.
 What’s so unusual about it  Rudder the critical understanding!  Nose High  Nose Low  Spiral  Stalls  Spins.
© 2009 Aviation Supplies & Academics, Inc. All Rights Reserved. The Pilot’s Manual – Ground School Airplane and Pilot Performance Chapter 10 En Route Performance.
Simulating Flight Wind Tunnel.
Aerodynamics Chapter 3 Aerodynamics of Flight.
Controls Chapter 6 Lecture 13.
6.05 Lift Theory of Flight 40 Minutes
Theory of Flight 6.08 Loads and Load Factors References:
Airfoil Any surface that provides aerodynamic force through interaction with moving air Aerodynamic force (lift) Moving air Airfoil.
6.07 Stalls References: FTGU pages 18, 35-38
6.09 Flight Instruments and Performance Factors
6.06 Loads and Load Factor References: FTGU pages 17-18, 34-35
Flight Operations Chapter 25 Flight Planning.
Stalls, Spins, Spiral Dives & Load Factor
CAA FE Seminar August 2012 Improving the CPL The Maximum Rate Turn.
DESCRIBE FLIGHT INSTRUMENTS
Warm-Up – 3/16 – 10 minutes Utilizing your notes and past knowledge answer the following questions: Describe the four types of airspeed. Describe the.
Usage Guidelines for Jeopardy PowerPoint Game
Bernoulli’s Principle
Chapter 4 sections 4-5 Projectile Motion.
Principles of Flight Chapter 4 - Stalling.
Using and rearranging the lift calculation
Grab their Attention with Active Learning!
Airfoils.
MISCELLANEOUS PERF. The performance data for takeoff and landing an aircraft can be obtained from the aircraft's flight manual or pilot's operating handbook.
Introduction to Aeronautical Engineering
Chapter 1 Functions.
Theory of Flight Flight Instruments and Performance Factors
Presentation transcript:

Airplane and Pilot Performance Chapter 8 Airplane Performance Factors

Figure 8-1. Examples of airplane registrations.

Figure 8-2. Certificate of Registration.

Figure 8-3. Certificate of Airworthiness.

Table 8-1. Sections of the Flight Manual.

Figure 8-4. Color coding on the airspeed indicator.

Figure 8-5. Gusts can increase or decrease the angle of attack, cause high wing loadings, or cause the wing’s critical angle of attack to be exceeded (stall).

Figure 8-6. The speed range of an airplane.

Figure 8-7. Load factor versus bank angle.

Figure 8-8. A typical V-G diagram related to ASI markings.

Figure 8-9. Performance reduces when air density reduces.

Figure 8-10. The standard atmosphere.

Figure 8-11. Example 8-1.

Figure 8-12. Example 8-2.

Figure 8-13. Example 8-3.

Figure 8-14. Comparing the Fahrenheit and Celsius temperature scales.

Figure 8-15. Density altitude chart.

Figure 8-16. Velocity versus G-loads or V-G diagram.