General Description Flashcards
What is the maximum glide distance speed in autorotation?
69 knots
What are the V(ne) airspeed limitations in Knots indicated air speed?
VFR - 130 KIAS
IMC - 110 KIAS or placard V(ne) whichever is less
VNE for internal gross weight >3200 lbs - 78 KIAS
The procedural word SHOULD is used to mean?
Recommend or preferred, NOT mandatory
The vertical fin is canted 5 1/2 degrees to the right center to
Reduce tail rotor thrust requirements in forward flight
How many degrees of twist are there in the main rotor blade?
-10 degrees
The total capacity of the fuel is ____ with ___ being usable.
84.1, 82.6
An operating procedure, which is essential to highlight is a
NOTE
The procedural word SHALL is used to mean
Mandatory
What type of airfoil are the main rotor blades?
Asymmetrical
The maximum available takeoff power (5 minute limit) is
> 85-100%
State the maximum continuous power (TQ AVAIL CONT) for the TH-67 power plant.
85%
How many switches can be used to control the search light on the A+ configuration
3
An operating procedure, which if not correctly followed could result in personal injury, is
WARNING
The purpose of the horizontal stabilizer is to
Maintain a desirable aircraft altitude in forward flight
How many degrees of pitch are in the tail rotor with full pedal applied?
23 degrees
An operating procedure, which if not strictly observed could result in damage to equipment is called a
CAUTION
What is the diameter of the main rotor system?
33 ft, 4 in
The TH-67 tailboom section uses a _________ type of construction.
Fully monocoque
What are the minimum crew restrictions for the TH-67?
VFR - min 1 pilot
IFR - min 2 pilots IMC
Which section of the aircraft contains the engine?
Intermediate Section
The TH-67 intermediate sections uses a ______ type of construction.
Semi-monocoque
The IFR configuration of the TH-67 has _____ pilot static systems.
2 independent
The _____ supplies ram (impact) air to the ______.
Pilot tube, airspeed indicator
In a conventional helicopter flight control system, the 3 basic controls used to maneuver the aircraft are ___, ____, ____.
Cyclic, collective and anti-torque pedals