Category
Designators &
Features CONT.
Turbulence
Turbulence Cont.
100

Define what type of aircraft, or requirements are needed for Category 1? What is the speed and climb rate?

Weight: 12,500 pounds or less 

 Single-engine 

 Propeller-driven 

Speed -100-160knots; climb up to 1000ft per/min

 All helicopters

speed- 90-160knots; climb 500-2150ft p/min


100

Designators may have as many as ________ characters, but no less than ________.

4; 2

100

Wing Configuration type?

Straight, swept, and Delta

100

What is wake turbulence?

phenomenon resulting from the passage of an aircraft through the atmosphere

100

____ generated by the creation of pressure differential over the wing surface. How?

Lift;  lowest pressure above and highest pressure below the wing

200

Define what type of aircraft, or requirements needed for Category 2? What is the speed and climb rate?

Weight: 12,500 pounds or less 

 Twin-engine 

 Propeller-driven

Speed -160-250knots; climb 1000-2000ft per/min.

200

What is generally the first character in an aircraft designator?

Letter

200

What are the three types of engines?

reciprocating - operates on gas and with a propeller 

turboprop - has 2 metal exhaust on propeller, use jet fuel

turbojet - jet engine no propeller

200

Circular patterns of air created by wake turbulence  called?

wake vortex, wingtip vortices

200

vortex circulation off wingtip for aircraft and wingtip vortices for helicopters?

counterclockwise off right wing, clockwise off the left wing, drifting laterally 2-3knots when close to the ground for aircrafts 

during forward flight

300

Define what type of aircraft, or requirements are needed for Category 3? What is the speed and climb rate?

Any other aircraft not in CAT 1 or 2

All large multi-engine turbojet

Speed -300-550 knots; climb 2000-4000ft p/min.

300

What are the 9  Aircraft Identification Features?

Size 

 Wing placement 

 Windows 

 Engine location and number 

 Wing configuration 

 Fuselage 

 Engine type 

 Tail configuration 

 Landing gear

300

What are the types of windows on an aircraft?

Bubble canopy

oval

square

round

teardrop

300

Three factors that affect the strength of a vortex?


Weight, speed, shape of wing


300

When do vortices begin for a fixed-wing aircraft?

At rotation or when lift begins

400

What are the 9 factors that affect aircraft performance?

Weather conditions 

 Aircraft configuration 

 Altitude 

 Load 

 Pilot’s ability 

 Climb rate 

 Engine performance 

 Speed 

 Weight class

400

4 engine location and number?

on fuselage

under wing

through tail

through vertical stabilizer

400

3 main types of wing placements? Two rare types?

High, Mid, and low-wing.

Bi-wing and Canard - (on nose of cockpit)

400

The greatest strength of a vortex is when the aircraft is ___ and strength diminishes with___

heavy, clean and slow

time and distance

400

Vortices from larger aircraft will sink approximately _____ per minute and level off approximately __________ feet below the flight path. Counter control is most effective and roll is minimal when the wingspan and the ailerons extend beyond the __________ of the vortex 

300-500ft

500-1000ft

outer edges

500

What are the 4 weight classes and take off weight?

Small - 41000 lbs or less

Large - over 41000lbs up to but not including 300,000lbs

Heavy -300,000lbs and more

Super - no specific weight -  only 2 aircrafts: A225 & A380

500

What are the types of tail configurations?

Conventional

Forward slant vertical stabilizer

horizontal stabilizer above fuselage

"T" tail

"V" tail

500

Types of landing gear?

Fixed or retractable

Tricycle or conventional

500

Assuming similar aircraft, which aircraft would create a greater wake turbulence effect? 

 Aircraft cruising en route 

 Aircraft on approach to the airport 

 Aircraft on takeoff from airport

 Aircraft on approach to the airport 


500

What causes helicopter downwash and how long is the spread distance?

slow hover taxi or stationary hover

spread outward 3 times the diameter of the rotor in all directions