CFI Instrument Practical Test Standards,
FAA-S-8081-9B, June 2001
VI. Flight by Reference to Instruments
The examiner shall select TASK H and at least one other TASK. The applicant shall select either the primary and supporting or control and performance method for teaching this AREA OF OPERATION.Fundamentals
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Attitude instrument flying means control of the aircraft's spatial position by using instrument's rather than outside visual references
- Control and performance
attitude + power = performance
- Primary and Supporting
Pitch instruments Bank instruments Power instruments-
airspeed indicator (ASI)
engine instruments-
manifold pressure gauge (MP)
tachometer (RPM)-
Primary instruments
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One in each group (pitch, bank, power)
Provide most pertinent and essential information
Indication stable with correct flight (shows greatest change with improper aircraft control)
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Back up and supplement primary instruments
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Emphasized by FAA (Instrument Flying Handbook)
Requires specific knowledge and interpretation of each individual instrument during training
Helps avoid over-dependence on attitude indicator, facilitating partial panel flight - Cross-check
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Continuous, logical observation of instruments for attitude and performance information
Proficient pilot adjusts scan rate and sequence to specific flight situation
Common errors-
Fixation
Omission
Emphasis - Interpretation
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Appled knowledge of
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instrument construction and operating principles
aircraft performance capabilities (POH) - Control
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Four components
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Pitch
Bank
Power
Trim
Two basic methods:
A. Straight-and-Level Flight
To determine that the applicant- Exhibits instructional knowledge of teaching straight-and-level flight by describing
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a. The relationship of pitch, bank and power in straight-and-level flight
- Adjust pitch to maintain assigned ALT with VSI = 0
- Trim to relieve control pressures
- Correct small deviations (< 100 feet) with pitch only
- ½ bar width on AI
- VSI < 200 fpm
- Larger deviations may require use of pitch and power
- Initial 1 bar width on AI
- VSI = 2 x error in alt
- VSI is primary pitch instrument during altitude corrections
- Adjust aileron and rudder pressures to keep HI constant, wings level on AI and TC with ball centered
- Corrections of heading deviations
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Coordinated aileron and rudder
Bank angle < number of degrees off and < standard rate (3°/sec)
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Pitch varies with airspeed and load
At constant airspeed, there is only one specific pitch attitude for level flight
Uncorrected bank leads to decreasing pitch with increasing airspeed-
Full panel
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Maintain constant altitude (+/- 100 ft) and heading (+/- 10°) at a given contstant airpseed (+/- 10 kt)
Constant altitude
Prompt, smooth, small corrections
SLF Pitch Bank Power Primary ALT HI ASI Secondary AI, VSI AI, TC MP, RPM
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Partial panel (AI and HI inoperative)
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Maintain altitude with ALT, VSI, ASI
Hold heading with TC level, centered ball, and MC
SLF-Partial Panel Pitch Bank Power Primary ALT TC ASI Secondary VSI MC MP, RPM
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Keep ball centered
Trim to relieve control pressures - Exhibits instructional knowledge of common errors related to straight-and-level flight by describing
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a. Slow or improper cross-check during straight-and-level flight
- Just enough control pressure to stop needle movement
- A bit more to start smooth correction
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ALT needle tip 0, AI scale pointer (bank index) 0, ASI needle tip on speed,
TC level & centered ball, HI needle tip center of bug, VSI needle tip 0
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Learn/use MP that you know will result in approximate desired airspeed in SLF
If airspeed changes, cross-check VSI, ALT before any power change
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Aim for precision: heading +/- 2°, airspeed +/- 2 knots, altitude +/- 20 feet
Beware overcontrolling
Use two step corrections
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Keep the ball centered
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Trim to relieve control pressures
Small, frequent adjustments - Demonstrates and simultaneously explains straight-and-level flight from an instructional standpoint
- Analyzes and corrects simulated common errors related to straight-and-level flight
References
Aviation Instructor's Handbook, FAA-H-8083-9
Instrument Flying Handbook, FAA-H-8083-15, 1999
Instrument Rating PTS, FAA-S-8081-4D, April 2004