Maneuver Objectives & Definitions Flashcards
Objectives & Tolerances Commercial ACS
Turns Around a Point Obj
teach keep constant radius around point
correcting for wind
using inside & outside refs
ALT 100
ASPD 10
S- Turns Obj
fly a series of S- Turns across linear ground feature
with semicircles equal size & shape
account for wind effects
constant altitude & airspeed
ALT 100
ASPD 10
Rectangular Course Obj
fly ground track equidistant from all sides of rectangular area on ground
account for wind
constant airspeed & altitude
using inside & outside refs
ALT 100
ASPD 10
Steep Turns Obj
fly steep bank, maximum performance turns while using inside & outside refs
ALT 100
ASPD 10
BANK 5
Hdg Rllout 10
Slow Flight Obj
teach positive aircraft control at speed in which any increase AOA, increase load factor, or reduction power result in stall warning or aerodynamic buffet
Alt 50
Hdg 10
Aspd +5/-0
Bank 5*
Power Off Stall Obj
recognize & recover from stall in landing config
Alt
Hdg 10 (straight flight)
Aspd
Bank 5* not exceed 20* (turning)
Power On Stall Obj
recognize & recover from stall in Takeoff/Departure config
Alt
Hdg 10* (S&L)
Aspd
Bank 5* not exceed 20* (turning)
Accelerated Stall Demonstration Obj
demonstrate acft will stall at higher airspeed under increased load factor
Coordinated 45* bank (ACS)
Vmc Demo Obj
teach student to recognize & recover from loss of directional control
Recover +/- 20* entry heading
aspd 5 of VSSE/VYSE during recovery
Drag Demo
demonstrate effects on acft performance under various configs
Vmc
Calibrated Airspeed at which directional control can be maintained with the critical engine inop
Critical Engine
Engine that, when it fails, has the most adverse effects on directional control of the airplane
“Middle Name”
I know have lost directional control when I have full rudder deflection into the operating engine and aircraft begins to yaw toward inop engine.
To Recover I will simultaneously reduce power on operating engine as needed and reduce AOA to regain directional control and then smoothly re-apply full power on the operating engine
Maneuvering Speed
Max airspeed at which full, abrupt control inputs can be made without structural damage to the aircraft.
At airspeeds below maneuvering speed, the aircraft will stall before exceeding design limit load factor.
At airspeeds above maneuvering speed the design limit load factor will be exceeded before the aircraft stalls.
Stabilized Approach
Is an approach in which the pilot establishes and maintains a constant angle glide path towards a predetermined point on the landing runway. Based on pilot’s judgement on certain visual cues, and depends on constant final descent airspeed and configuration
AFH 8-9