If a gyroscopic instrument is toppled, becomes unserviceable or the power sources for the instruments fails, you will have to continue the flight using partial panel.
Review
Gyroscopic Instruments may be powered by:
A vacuum/ pressure system
Electrically powered.
Typical training aircraft will have vacuum attitude and heading indicator and electric turn coordinator.
Vacuum failure (suction 0):
Attitude indicator tumble.
heading indicator spin (some of them have a red flag).
Partial panel instruments
The term partial panel refers to instrument flying while the attitude indicator and heading indicator are either not fitted on the panel or are unserviceable.
Pitch instruments – partial panel
Altimeter (ALT).
Airspeed indicator (ASI).
Vertical speed indicator (VSI).
Bank instruments – partial panel
Turn coordinator (TC).
Magnetic compass (M).
Power instruments – partial panel
Airspeed indicator (ASI).
Engine instruments.
Manifold pressure gauge (MP).
Tachometer (RPM).
Straight and level flight: full panel
Pitch:
Primary: Attitude indicator.
Secondary: Altimeter, Vertical Speed Indicator.
Bank:
Primary: Attitude Indicator.
Secondary: Heading Indicator, Turn Coordinator.
Power:
Primary: Airspeed Indicator.
Secondary: Manifold pressure gauge, Tachometer.
Straight and level flight: partial panel
Pitch:
Primary: Altimeter.
Secondary: Vertical Speed Indicator.
Bank:
Primary: Turn Coordinator.
Secondary: Magnetic Compass.
Power:
Primary: Airspeed Indicator.
Secondary: Manifold pressure gauge, Tachometer.
Scan technique: Straight and Level flight partial panel
What information do I need ?
Pitch, speed, altitude, heading.
Which instrument give me the needed?
Turn Coordinator.
Altimeter.
Aispeedindicator.
Is the Information reliable ?
Confirm the reliability of the turncoordinator by referring to the magnetic compass.
Confirm the reliability of the altimeter by referring to the vertical speed indicatorandthe airspeed indicator.
Climb or descent straight, constant airspeed: full panel
Pitch:
Primary: Attitude Indicator, Airspeed Indicator.
Secondary: Vertical Speed Indicator.
Bank:
Primary: Attitude Indicator.
Secondary: Heading Indicator, Tunr Coordinator.
Power:
Primary: Tachometer.
Secondary: Airspeed Indicator.
Climb or descent straight, constant airspeed: partial panel
Pitch:
Primary: Airspeed Indicator.
Secondary: Altimeter, Vertical Speed Indicator.
Bank:
Primary: Turn Coordinator.
Secondary: Magnetic Compass.
Power:
Primary:
Secondary: Airspeed Indicator.
Scan technique: Climb or Descent constant airspeed partial panel
What information do I need ?
Pitch, speed, altitude, heading.
Which instrument give me the needed?
Altimeter.
Aispeed indicator.
Is the Information reliable ?
Confirm the reliability of the turncoordinator by referring to the magnetic compass.
Confirm the reliability of the airspeed indicator by referring to the altimeter and the vertical speed indicator.
Climb or Descent straight constant rate: full panel
Pitch:
Primary: Attitude Indicator.
Secondary: Vertical speed Indicator.
Bank:
Primary: Attitude indicator.
Secondary: Heading Indicator, Turn Coordinator.
Power:
Primary: Airspeed indicator.
Secondary: Tachometer.
Climb or Descent straight constant rate: partial panel
Pitch:
Primary: Vertical speed Indicator.
Secondary: Altimeter.
Bank:
Primary: Turn Coordinator.
Secondary: Magnetic Compass.
Power:
Primary: Airspeed indicator.
Secondary: Tachometer.
Scan technique: Climb or Descent Level off partial panel
What information do I need?
Heading, Altitude
Which instruments give me the needed information?
Turn coordinator.
Altimeter.
Is the information reliable?
Confirm the reliability of the Turn coordinator by referring to the Magnetic compass.
Confirm the reliability of the altimeter by referring to the vertical speed indicator and the airspeed indicator.
Timed turn partial panel
The compass, is useless during a turn—therefore we have to time standard-rate turns using the turn coordinator and a clock or watch.
Use the following method:
Find the number of degrees required to turn (left or right) to the prescribed heading and divide this number by 3—that is 3° per second. Then begin the timed turn.
At rate one 360° will take 120 sec (360/3 = 120)
180 ° = 60 sec
90 ° = 30 sec
30 ° – 10 sec
Step by step:
Be sure to in straight and level flight, check:
Airspeed indicator-stabilize
Turn coordinator-wing level.
Altimeter-stabilize.
Check compass for heading.
Calculate the time to turn at the heading desired.
Start clock and roll in.
Check turn coordinator for rate one.
At the end of the clock roll out and wing level.
Confirm wing level with TC, airspeed indicator, altimeter.
Check compass.
Scan technique: Timed turn partial panel
What information do I need ?
Time and altitude.
Which instrument give me the needed?
Clock or watch.
Altimeter.
Turn coordinator.
Is the Information reliable ?
Confirm the reliability of the turncoordinator by referring to the magnetic compass.
Confirm the reliability of the altimeter by referring to the vertical speed indicator and the Airspeed indicator.
Review questions
What is the scan technique for partial panel leveling off?
What is the scan technique for partial panel leveling off?
What is the scan technique for partial panel Climb or descentstraight, constant airspeed ?
What is the scan technique for partial panel Timed turn?
What instrument will be affected if you lose suction (vacuum gauge 0) ?
What are the pitch, bank and power instruments in a partial panel ?