- Page 4: PrefaceThis Instrument Flying Handb
- Page 7 and 8: inquiries regarding the available t
- Page 9 and 10: Chapter 3Flight Instruments .......
- Page 12 and 13: Chapter 10IFR Flight ..............
- Page 15 and 16: The only effective way to counter t
- Page 17 and 18: aircraft tends to lose altitude in
- Page 19 and 20: disoriented and the instructor pilo
- Page 21 and 22: 5. Utilize the visual descent point
- Page 23 and 24: antihistamines, blood pressure drug
- Page 25: Figure 1-7B illustrates the ADM pro
- Page 29 and 30: Figure 2-1. Newton’s First Law of
- Page 31 and 32: altitude, you must lower the pitch
- Page 33 and 34: The force of the airflow striking t
- Page 35 and 36: speed is constant, increasing the b
- Page 37 and 38: The most hazardous aspect of struct
- Page 39 and 40: the fuselage or the vertical fin. T
- Page 41 and 42: A sensitive altimeter is one with a
- Page 43 and 44: Extreme differences between ambient
- Page 45 and 46: Mach NumberAs an aircraft approache
- Page 47 and 48: This is done to correct for deviati
- Page 49 and 50: To find the true course that is bei
- Page 51 and 52: Figure 3-21. A vertical card magnet
- Page 53 and 54: Gyroscopic SystemsFlight without re
- Page 55 and 56: Figure 3-28. Twin-engine instrument
- Page 57 and 58: Directional gyros are almost all ai
- Page 59 and 60: The inclinometer, similar to the on
- Page 61 and 62: After Engine Start1. When you turn
- Page 63 and 64: Figure 4-1. Control/Performance cro
- Page 65 and 66: Figure 4-2. Primary/Supporting cros
- Page 67 and 68: This cross-checking method gives eq
- Page 69 and 70: 4-8
- Page 71 and 72: Figure 5-1. Pitch attitude and airs
- Page 73 and 74: Figure 5-7. Using the altimeter for
- Page 75 and 76: Vertical Speed IndicatorThe vertica
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Figure 5-16. Instruments used for b
- Page 79 and 80:
airspeed constant, the airplane wil
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Figure 5-23. Straight-and-level fli
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You will have developed a high leve
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3. Faulty sequence in trim techniqu
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Figure 5-27. Stabilized climb at co
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EntryThe following method for enter
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Common Errors in Straight Climbs an
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Figure 5-34. Turn coordinator calib
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Figure 5-36. Steep left turn.Steep
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Climbing and Descending TurnsTo exe
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have a specific reason to turn the
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Figure 5-40. Unusual attitude—nos
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except as a last resort, as it usua
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Figure 5-43. 80/260 procedure turn
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Figure 6-1. In most situations, the
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Figure 6-2. The flight instruments
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lowered. A rapid change in airspeed
- Page 113 and 114:
Power Control During Straight-and-L
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Common Errors During Airspeed Chang
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Figure 6-10. Flight instrument indi
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To recover to straight-and-level fl
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Figure 6-12. Flight instrument indi
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Instrument TakeoffThe procedures an
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Sky WaveThe sky wave, at frequencie
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Function of ADFThe ADF can be used
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7-6330°WIND015°306912152118243027
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2. Positively identifying any malfu
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TO/FROM indicator. The TO/FROM indi
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Course interception is illustrated
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selection assures reception of azim
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Without an RMI, orientation is more
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2. MODE select switch used to selec
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The Aeronautical Information Manual
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Function of GPSGPS operation is bas
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To determine the aircraft position
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the FAWP. As sensitivity changes fr
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Figure 7-23. Instrument landing sys
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Marker BeaconsTwo VHF marker beacon
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Runway end identifier lights (REIL)
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Figure 7-29. Glide-slope receiver i
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Approach Azimuth StationThe approac
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to this target can be instantly det
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7-40