- Page 3: Airplane Flying Handbook 2016 U.S.
- Page 7 and 8: Acknowledgments The Airplane Flying
- Page 9 and 10: Table of Contents Preface..........
- Page 11 and 12: Constant Radius During Turning Flig
- Page 13 and 14: Short-Field Landing................
- Page 15 and 16: Chapter 1 Introduction to Flight Tr
- Page 17 and 18: for the certification of airmen and
- Page 19 and 20: Figure 1-5 shows an example of some
- Page 21 and 22: the need arises, to private individ
- Page 23 and 24: Figure 1-9. FAA Form 8000-4, Air Ag
- Page 25 and 26: encompassed by, the tasks within ea
- Page 27 and 28: Figure 1-13. Three major areas cont
- Page 29 and 30: Figure 1-18. A sample before landin
- Page 31 and 32: Chapter 2 Ground Operations Introdu
- Page 33 and 34: Figure 2-3. Airplane Flight Manuals
- Page 35 and 36: deck reference guide is in the airc
- Page 37 and 38: Figure 2-9. An AVGAS fuel filler no
- Page 39 and 40: • Brakes and brake systems should
- Page 41 and 42: • Take a pilot who is more experi
- Page 43 and 44: the position (navigation) lights sh
- Page 45 and 46: SW-2, 12 JAN 2012 to 09 FEB 2012 SW
- Page 47 and 48: the weathervaning tendency is less
- Page 49 and 50: • Install chocks and release park
- Page 51 and 52: Chapter 3 Basic Flight Maneuvers In
- Page 53 and 54: Elevator—Pitch Lateral axis Rudde
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the airplane’s vertical axis (yaw
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30 W OBS W OBS W 30 W OBS W OBS NAV
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Nose high Natural horizon reference
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D195I D212I HDG UP A212I TAS 100KT
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Skid Coordinated Turn Slip D.C. ELE
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D195I D212I HDG UP A212I 130 120 11
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Best angle-of-climb airspeed (V X )
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W W S S E E TAS 106KT OAT 7°C 2 1
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14 Too fast Best glide speed Too sl
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• Cross-controlling during glidin
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Chapter 4 Maintaining Aircraft Cont
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therefore closer to the higher spee
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• Excessive back-elevator pressur
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manufactured with a certain amount
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stall occurring during approach to
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a given airplane consistently stall
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left. With the throttle fully advan
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Stall Less stalled Incipient Spin
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Unfortunately, accident records sho
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The ability to separate time-critic
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Aerobatics vs. UPRT Flight Training
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while in flight. For these reasons,
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Chapter 5 Takeoffs and Departure Cl
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Take-off Distance vs. Density Altit
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Each type of airplane has a best pi
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Apply full aileron into wind Rudder
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• Using less than full aileron pr
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diminishes the pilot's ability to s
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point is reached and the airplane i
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Chapter 6 Ground Reference Maneuver
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clearing turns looking to the left
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Actual ground path Intended ground
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Exit Turn more than 90° rollout wi
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To perform a turn around a point, t
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the bank angle should be increased
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To successfully perform eights alon
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Wind Entry Gaining altitude Gaining
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Too high Pivotal altitude Too low F
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Chapter 7 Airport Traffic Patterns
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Crosswind WIND Entry 18 Left-Hand T
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Since in most cases the takeoff is
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Chapter 8 Approaches and Landings I
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stalling speed with power off, land
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No flaps; flatter descent angle Hal
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10° to 15° 27 Figure 8-7. To obta
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The ailerons serve the same purpose
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power. Once again, the airspeed mus
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the go-around/rejected landing is.
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WIND longitudinal axis aligned with
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component decreases and the relativ
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34 Obstacle clearance Effective run
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• Unstable approach • Undue del
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1 36 2 3 1. Strong Wind Set up clos
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When abreast of or opposite the des
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Spiral over landing field WIND Retr
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Intercept normal glidepath, resume
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34 Figure 8-34. Floating during rou
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Decreasing angle of attack Rapid in
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on these airplanes, any time a swer
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Chapter 9 Performance Maneuvers Int
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should realize load factors increas
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maneuver. During practice of the ma
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90° point 1. Bank 30° (approximat
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Chapter 10 Night Operations Introdu
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enlarge to receive as much of the a
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It is recommended that prior to a n
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for this possibility. Hold or lock
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to round out too high until attaini
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Chapter 11 Transition to Complex Ai
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L = 1 pV 2 SC L 2 L = Lift produced
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Center of pressure - Lift Center of
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in climb. Consequently, engine powe
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Turbocharger The turbocharger incor
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• Operate the engine in such a ma
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GEAR UP GEAR UP GEAR DOWN TAXI LAND
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the airplane could no longer be lan
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eceived to ensure a complete unders
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Chapter 12 Transition to Multiengin
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140 200 180 260 250 200 160 160 140
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1 Counterweight action 6 6 2 3 5 4
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The entire flight director/autopilo
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Performance and Limitations Discuss
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Weight and Balance The weight and b
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airplane to pivot about a stationar
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3 500 feet 1. Accelerate to cruise
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increasing application of aileron i
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from a bad bounce, as well as a go-
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operative engine is the only altern
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the airplane may not maintain altit
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Drag TAS 106KT OAT 7°C 2 1 1 2 Dra
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Stall Recovery Template 1. Wing lev
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Chapter 13 Transition to Tailwheel
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length, if desired. While taxiing,
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Landing The difference between nose
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combination of inertia acting on th
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Chapter 14 Transition to Turboprope
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The turboprop engine offers several
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NAV1 108.00 113.00 NAV2 108.00 110.
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ITT 50 TORO 0 0 PROP 0 ITT 0 FF 0 5
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The distribution of DC and AC power
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1. Before takeoff checks .. Complet
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Chapter Summary Transitioning from
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Chapter 15 Transition to Jet-Powere
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Fan air Fan air Combustion Inlet ai
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TAT 13° C 2.00 2.00 2.00 2.00 EPR
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In not having propellers, the jet-p
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Stick force in pounds 70 60 50 40 3
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C 19,000 lbs 18,000 lbs 17,000 lbs
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of the airplane as the stall develo
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OC Relative wind Pre-stall OC Initi
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everse thrust increases with speed;
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adequately repaired or replaced. In
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Captain’s Briefing I will advance
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• Natural contaminants (standing
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acceleration during this phase of t
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• Poor acceleration response in a
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If the flare is extended (held off)
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In the event of an engine failure i
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Chapter 16 Transition to Light Spor
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Maximum gross weight of 1,320 pound
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• After landing, parking, and sec
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[Figure 16-8] While this is not a l
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Regardless, a pilot must become fam
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Takeoff and Climb Takeoff and climb
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LSA’s controls become ineffective
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Chapter 17 Emergency Procedures Eme
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Avoiding forcible contact with inte
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from an irregularly running engine;
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300 feet AGL 4,480 feet 180° 1,016
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two immediate demands: attacking th
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If the landing gear malfunction is
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140 NAV1 108.00 113.00 NAV2 108.00
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point where attention is focused on
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140 NAV1 108.00 113.00 NAV2 108.00
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Glossary Numbers and Symbols 100-ho
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Axes of an aircraft. Three imaginar
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Compressor stall. In gas turbine en
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Environmental systems. In an aircra
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Gust penetration speed. The speed t
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Limit load factor. Amount of stress
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Pivotal altitude. A specific altitu
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Shock waves. A compression wave for
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Thrust. The force which imparts a c
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Vertical stability. Stability about
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Index A Abnormal engine instrument
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Gliding turns......................
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Initial climb......................