instrumentation 9 february 2005. instrumentation pitot-static system altimiter vertical speed...

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Instrumentation 9 February 2005

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Page 1: Instrumentation 9 February 2005. Instrumentation  Pitot-static system Altimiter Vertical Speed Indicator Airspeed Indicator  Gyroscopic Instruments

Instrumentation

9 February 2005

Page 2: Instrumentation 9 February 2005. Instrumentation  Pitot-static system Altimiter Vertical Speed Indicator Airspeed Indicator  Gyroscopic Instruments

Instrumentation

Pitot-static system Altimiter Vertical Speed Indicator Airspeed Indicator

Gyroscopic Instruments Turn coordinator Artificial horizon Heading indicator

Magnetic Compass OAT Gauge

Page 3: Instrumentation 9 February 2005. Instrumentation  Pitot-static system Altimiter Vertical Speed Indicator Airspeed Indicator  Gyroscopic Instruments

Pitot-static system Operates in response to air pressure Two air pressures:

Static pressure Taken from static vents, powers all three pitot-

static system instruments (ASI, VSI, Altimeter) Impact pressure

Powers airspeedindicator only

Page 4: Instrumentation 9 February 2005. Instrumentation  Pitot-static system Altimiter Vertical Speed Indicator Airspeed Indicator  Gyroscopic Instruments

Static System & Altimetry Static system powers altimeter Altimeter operates as a barometer Set altimeter on the ground to local settings Air pressure decreases at a constant rate per

foot increased in lower atmosphere (approximately 1000’ per 1” Hg)

Nonstandard temperature and pressure affect altimeter

Page 5: Instrumentation 9 February 2005. Instrumentation  Pitot-static system Altimiter Vertical Speed Indicator Airspeed Indicator  Gyroscopic Instruments

Altimeter As static pressure decreases, indicated altitude increases Altimeter setting is adjustable in “Kohlsman Window”,

aka Altimeter Setting Window Local altimeter setting will

cause the instrument to readthe approximate fieldelevation when located onthe ground at the airport

Reset altimeter to 29.92when climbing through18,000 feet.

Page 6: Instrumentation 9 February 2005. Instrumentation  Pitot-static system Altimiter Vertical Speed Indicator Airspeed Indicator  Gyroscopic Instruments

Altitude Terminology Indicated Altitude

Altitude read on the altimeter when it is set to the current local altimeter setting

Absolute altitude Height above the surface

True altitude True height above Mean Sea Level (MSL)

Pressure altitude Altitude indicated whenever the altimeter setting dial is set

to 29.92 (Standard Datum Plane) Density altitude

Pressure altitude corrected for non-standard temperature and/or pressure.

Page 7: Instrumentation 9 February 2005. Instrumentation  Pitot-static system Altimiter Vertical Speed Indicator Airspeed Indicator  Gyroscopic Instruments

Altimetry

Standard day 29.92” Hg and +15 deg. C On a standard day at sea level, pressure

altitude, true altitude, indicated altitude, and density altitude are all equal.

Page 8: Instrumentation 9 February 2005. Instrumentation  Pitot-static system Altimiter Vertical Speed Indicator Airspeed Indicator  Gyroscopic Instruments

“High to low…look out below” When flying from an area of low

pressure/low temperature to an area of higher pressure/higher temperature without adjusting the altimeter setting, the altimeter will indicate lower than the true altitude setting…and vice versa.

Page 9: Instrumentation 9 February 2005. Instrumentation  Pitot-static system Altimiter Vertical Speed Indicator Airspeed Indicator  Gyroscopic Instruments

Density vs. True Altitude

Page 10: Instrumentation 9 February 2005. Instrumentation  Pitot-static system Altimiter Vertical Speed Indicator Airspeed Indicator  Gyroscopic Instruments

Vertical Speed Indicator (VSI) Operates only on static

pressure, but is a differential pressure instrument

Operates on the principle of a calibrated leak…

Face of VSI outputs change in pressure over time displayed in feet per minute.

Page 11: Instrumentation 9 February 2005. Instrumentation  Pitot-static system Altimiter Vertical Speed Indicator Airspeed Indicator  Gyroscopic Instruments

Airspeeds and Airspeed Indicator

Airspeed Indicator Displays difference

between pitot (impact) pressure and static pressure

Pressures are equal when airplane is parked on ground in calm air.

Page 12: Instrumentation 9 February 2005. Instrumentation  Pitot-static system Altimiter Vertical Speed Indicator Airspeed Indicator  Gyroscopic Instruments

Airspeeds Indicated airspeed (IAS)

Uncorrected reading from the airspeed indicator Calibrated airspeed (CAS)

Indicated airspeed corrected for installation and instrument error.

True airspeed (TAS) Calibrated airspeed corrected for temperature and

pressure variations. Groundspeed (GS)

Actual speed of the airplane over the ground – this is the TAS adjusted for wind.

Page 13: Instrumentation 9 February 2005. Instrumentation  Pitot-static system Altimiter Vertical Speed Indicator Airspeed Indicator  Gyroscopic Instruments

Airspeeds – color coded VSO – stall speed / minimum

steady flight in landing configuration (lower limit of white arc)

VFE – max. flap-extended speed (upper limit of white arc)

VS1 – stall speed in specified configuration (lower limit of green arc)

VNO – max. structural cruising speed (top of green arc, bottom of yellow arc)

VNE – never exceed speed (upper limit of yellow arc, marked in red)

Page 14: Instrumentation 9 February 2005. Instrumentation  Pitot-static system Altimiter Vertical Speed Indicator Airspeed Indicator  Gyroscopic Instruments

Airspeeds, others VLE – max. landing gear-extended speed. VA – design maneuvering speed (flown in rough

air or turbulence to prevent overstressing airframe)

VY – Best rate-of-climb airspeed (creates most altitude in a given period of time)

VX – Best angle-of-climb speed (airspeed resulting in most altitude in a given distance.)

Page 15: Instrumentation 9 February 2005. Instrumentation  Pitot-static system Altimiter Vertical Speed Indicator Airspeed Indicator  Gyroscopic Instruments

Gyroscopic Principles Rigidity in spaceAxis of rotation points in a

constant direction regardless of the position of its base.

PrecessionTilting or turning of a gyro in

response to a deflective force.

Page 16: Instrumentation 9 February 2005. Instrumentation  Pitot-static system Altimiter Vertical Speed Indicator Airspeed Indicator  Gyroscopic Instruments

The Attitude Indicator Relies on rigidity in space

Direction of bank determined by relationship of miniature airplane to the horizon bar.

Miniature airplane remains stationary – horizon moves

Page 17: Instrumentation 9 February 2005. Instrumentation  Pitot-static system Altimiter Vertical Speed Indicator Airspeed Indicator  Gyroscopic Instruments

Turn Coordinator Relies on precession

As an airplane enters a turn, the TC indicates rate of roll. When bank is held constant, TC indicates rate of turn.

Most TCs display an index on the “Standard-rate turn”, wherein the airplane takes 2 minutes to turn 360 degreers.

The “ball” or inclinometer indicates quality of turn (skid/slip status).

Page 18: Instrumentation 9 February 2005. Instrumentation  Pitot-static system Altimiter Vertical Speed Indicator Airspeed Indicator  Gyroscopic Instruments

Heading indicator

“Gyroscopic compass” Magnetic compasses are difficult to read and suffer

from errors; the heading indicator (also known as a directional gyro or DG)

DGs suffer from precession due to bearing friction – the indicator must be realigned with the magnetic compass during straight-and-level, unaccelerated flight.

Page 19: Instrumentation 9 February 2005. Instrumentation  Pitot-static system Altimiter Vertical Speed Indicator Airspeed Indicator  Gyroscopic Instruments

Magnetic Compass Compass points to magnetic north Susceptible to several errors

Page 20: Instrumentation 9 February 2005. Instrumentation  Pitot-static system Altimiter Vertical Speed Indicator Airspeed Indicator  Gyroscopic Instruments

Compass Errors Variation Deviation Magnetic Dip

Page 21: Instrumentation 9 February 2005. Instrumentation  Pitot-static system Altimiter Vertical Speed Indicator Airspeed Indicator  Gyroscopic Instruments

Dip errors Magnetic dip:

When turning north from an easterly or westerly heading, the compass lags behind the actual aircraft heading. When a turn is initiated while on a northerly heading, the compass first indicates a turn in the opposite direction.

When turning south from an easterly or westerly heading, the compass leads the actual heading. When a turn is initiated on a southerly heading, the compass immediately leads ahead.

Mnemonic: UNOS – undershoot north, overshoot south

Page 22: Instrumentation 9 February 2005. Instrumentation  Pitot-static system Altimiter Vertical Speed Indicator Airspeed Indicator  Gyroscopic Instruments

Dip errors continued Accelerating or decelerating while heading

either east or west will also cause compass errors.

When accelerating on an east or west heading, the compass indicates a turn to the north.

When decelerating on an east or west heading, the compass indicates a turn to the south.

Mnemonic: ANDS – accelerate north, decelerate south.

Compass accurate only in S&L, unaccelerated flight.

Page 23: Instrumentation 9 February 2005. Instrumentation  Pitot-static system Altimiter Vertical Speed Indicator Airspeed Indicator  Gyroscopic Instruments

Variation Errors Magnetic poles do not coincide with geographic

poles. Most places on Earth, the

compass needle does notpoint to True North. Angulardifferences betweenmagnetic north and truenorth are called variationsand are displayed onaeronautical charts.

Page 24: Instrumentation 9 February 2005. Instrumentation  Pitot-static system Altimiter Vertical Speed Indicator Airspeed Indicator  Gyroscopic Instruments

Deviation Errors The metal, electrical systems, and

operating engine all create magnetic fields from the aircraft.

Aircraft manufacturers install compensatory magnets to prevent most errors. Remaining errors are called deviation.

A card in the aircraft will list the deviation at various different compass points.

Page 25: Instrumentation 9 February 2005. Instrumentation  Pitot-static system Altimiter Vertical Speed Indicator Airspeed Indicator  Gyroscopic Instruments

Next Week…

- Regulations- (FAR/AIM & Test Prep)