Flight Instrument Systems Flashcards
IFR instruments mandatory list.
GRABCARD
- Generator
- Radio
- Altimeter
- Ball, slip skid indicator
- Clock
- Attitude
- Rate of turn indicator
- Directional gyro (turn indicator)
Standard rate turn
- 3 degrees per second.
- Takes 60 seconds to turn 180 degree turn
Angle of bank
Angle of bank = [true airspeed in knots / 10] + 5
14 degrees at 90KIAS
Precession
- when an outside force tried to tilt a spinning gyro, the gyro responds as if the force has been applied 90 degrees further around the direction of rotation.
Rigidity in space
- Principle that a wheel with a heavily weighted rim spun rapidly tends to remain fixed in the plane in which it is spinning. This creates a resistance to reflection. Physics dictates that an object along a trajectory in a certain direction ( combined with centrifugal force) tend to continue on said path independently of surroundings.
Pendulous Vanes
- Are the mechanisms use to reerect the gyro if it is not parallel to the ground or horizon. Four air jets are spaced out at 90 degree angles. They’re placed under gyro wheel. Each outlet is partially blocked by a tiny door called a pendulous gain. If gyro begins to stray from horizon the doors will open or close to re erect gyro.
Variation
- Magnetic variation, variations in angular differences between the true and magnetic poles. East is least west is best.
Deviation
Deviation
- Magnetic compass interference with airplane engine, avionics and other instruments. Corrected by “swinging the compas”. Remaining errors are written on deviation card.
FACT: IFR en route charts are published as magnetic headings. White winds a loft are published in true winds aloft direction and must be converted to magnetic heading for flight planning.
Magnetic dip
OSUN - Over shoot south undershoot north.
- Turning off north, indication in opposite direction
- Turning off south, indication exaggerated in given direction.
Pitot-static instruments
- airspeed
- altimeter
- VSI vertical speed indicator
IAS
- indicated air speed (IAS)
CAS
- Calibrated airspeed (CAS) is indicated corrected for installation and instrument error.
EAS
- Equivalent air speeds (EAS) is calibrated adjusted for adiabatic compression flow at a particular altitude.
- Happens as 200KIAS and at above 20,000 ft
- Air compression in front of the aircraft abuses abnormally high readings.
TAS
- True airspeed (TAS) is calibrated airspeed corrected for nonstandard temperature and pressure.
- TIP add 2% to CAS for every 1000ft
V-speeds
- (V)ne. Red. Structural damage
- (V)no. Green/yellow arch interception. Maximum cruising speed.
- (V)so. Lower white arch limit. Stalling speed in landing configuration under max weight.
- (V)s1. Lower green arch. Minimum stalling speed in clean configuration. (Power off stall speed) at maximum weight.
- (V)fe. Upper white arch limit. Maximum speed with fully extended flaps.
- (V)a. Maneuvering speed. Airplane will stall before enduring structural damage.
- (V)le. Maximum speed with landing gear extended.
- (V)lo. Maximum speed in which one can extend or retract landing gear.