Cessna C172S Nav III Training Manual
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Cessna C172S Nav III Training Manual

Cessna C172S Nav III Training Manual

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C172S Nav III

Training Manual
Crosswinds Aviation
1st
Edition


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Summary of Contents for Cessna C172S Nav III

  • Page 1 C172S Nav III
 Training Manual Crosswinds Aviation Edition
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  • Page 2: Table Of Contents

    ........................................Electrical System......................................Ignition System....................................... G1000 System (and other avionics)................................Performance, Weight & Balance ..................Cessna 172s V speeds..................................... Weight and Balance...................................... C172S Procedures guide ......................C172s Standard operaton procedures (SOP’s).............................. Take off Procedures.

  • Page 3: Aircraft Systems

    Aircraft Systems Engine The C172S is equipped with a Lycoming, 4-cylinder, IO-360-L2A (Fuel injected, opposed, 360 cubic inch displacement) engine rated at 180 horsepower at 2700 RPM. The engine is direct drive (crankshaft connected directly to the propeller), horizontally opposed (pistons oppose each other), piston driven, fuel injected and normally aspirated (no turbo or supercharging).

  • Page 4: Landing Gear

    Landing Gear The C172S is equipped with fixed tricycle type landing gear. The main gear is mounted to tubalar spring struts mounted to the fuselage below the wings. The nose wheel consists of an air oil type strut and is steerable with linkage to the rudder pedals. Brakes he airplane has a single-disc, hydraulically actuated brake on each main landing gear wheel.

  • Page 5: Fuel System

    windshield, and associated plumbing. As the airplane approaches a stall, the low pressure on the upper surface of the wings moves forward around the leading edge of the wings. This low pressure creates a differential pressure in the stall warning system which draws air through the warning horn, resulting in an audible warning at 5 to 10 knots above stall in all flight conditions.

  • Page 6: Electrical System

    Electrical System. The airplane is equipped with a 28-volt direct current (DC) electrical system consisting of a belt-driven 60-ampere alternator and a 24- volt main storage battery. Individual system circuit breakers are found on the circuit breaker panel below the pilot's control wheel. All circuit breakers are "pullable"...

  • Page 7: Ignition System

    If the alternator system fails, the MASTER switch may be set to the OFF position to preserve Main Battery capacity for later in the flight. With the MASTER switch OFF and the STBY BATT switch in the ARM position, the standby battery will power the Essential Bus for a limited time.
  • Page 8 Attitude Heading Reference System (AHRS, sensors replace traditional gyros) Magnetometer (supplies heading information to AHRS, located in left wing) Air Data Computer (ADC, compiles info from pitot/static system and OAT) Engine Monitor (compiles engine info and sends it to avionics unit)
 Transponder (ADS-B transponder that is operated on PFD) XM data link (provides weather and radio data to MFD) 
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  • Page 10: Performance, Weight & Balance

    Performance, Weight & Balance Cessna 172s V speeds. Speeds listed below are in Knots Indicated Airspeed (KIAS). Speed Description Airspeed indicator markings Stall speed in landing configuration Stall speed with zero flaps Bottom of White Line Rotation speed (start rotation)

  • Page 11: C172S Procedures Guide

    Maximum weight in the baggage areas A and B combined: 120lbs (120lbs for area A, 50 lbs for area B) C172S Procedures guide C172s Standard operaton procedures (SOP’s). Passenger Briefing SAFETY 
 3. Fire Extinguisher 5. Traffic and Talking 1. Safety Belt/Harness Usage Location/Usage 6.
  • Page 12 • Mixture to cutoff • Fuel selector, magnetos, and battery master off • Touchdown at lowest speed possible
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  • Page 13: Take Off Procedures

    Take off Procedures. Normal Takeoff (Flaps 0°) Maneuver standards: Vy +10-5kts to a safe altitude. 1. Line up on centerline positioning controls for wind 2. Smoothly apply full power 3. Check engine gauges 4. Right rudder as required for turning tendencies 5.

  • Page 14: Short Field Takeoff (Flaps 10°)

    Short field Takeoff (Flaps 10°) Maneuver standards: Vx +10-5kts over obstacle then Vy +10-5kts 1. Select flaps 10° 2. Line up on centerline positioning controls for wind 3. Hold brakes 4. Increase throttle to Full 5. Check engine gauges 6. Release brakes 7.

  • Page 15: Soft Field Takeoff (Flaps 10)

    Soft field Takeoff (Flaps 10°) Maneuver standards: Maintain Vx or Vy +10-5kts 1. Flaps 10° 2. Roll onto runway with full aft yoke – minimum braking – do not stop 3. Smoothly apply full power holding full AFT on the yoke - check engine gauges 4.

  • Page 16: Landing Procedures

    Landing Procedures. VFR Landing briefing procedure. Announce verbally
 1. Type of Approach & Landing Runway 3. Wind Direction & Speed Pattern Altitude 2. Aiming & Touchdown Point 4. Go-Around Criteria & Plan
 Example: “This will be a normal flaps full landing on runway 13 with an intended touchdown point of the one thousand foot markers, aiming point will be 3 stripes prior, we can expect a left crosswind of 5 knots”.

  • Page 17: Normal Landing Procedure (Flaps 20°-Full)

    Normal Landing procedure (Flaps 20°-FULL) Maneuver standards: +10-5 1.3x Vso approach, touchdown within 400’ of selected point. 1. Complete the “Approach Checklist” before entering the airport; devote full attention to aircraft control and traffic avoidance. 2. Slow to 90 KIAS prior to entering downwind or traffic pattern and complete the before landing checklist.

  • Page 18: Short Field Landing Procedure (Flaps Full)

    Short field Landing procedure (Flaps FULL) 
 Maneuver standards: +10-5 1.3x Vso approach, touchdown within 200 feet of selected point. 1. Complete the “Approach Checklist” before entering the airport; devote full attention to aircraft control and traffic avoidance. 2. Slow to 90 KIAS prior to entering downwind or traffic pattern and complete the before landing checklist.

  • Page 19: Soft Field Landing Procedure (Flaps Full)

    Soft field Landing procedure (Flaps FULL) Maneuver standards: +10-5 1.3x Vso approach, touchdown with minimum sink rate. 1. Complete the “Approach Checklist” before entering the airport; devote full attention to aircraft control and traffic avoidance. 2. Slow to 90 KIAS prior to entering downwind or traffic pattern and complete the before landing checklist.

  • Page 20: Power Off 180 Procedure (Flaps As Required)

    Power off 180 procedure (Flaps as required) Maneuver standards: N/A 1. Complete the “Approach Checklist” before entering the airport; devote full attention to aircraft control and traffic avoidance. 2. Slow to 90 KIAS prior to entering downwind or traffic pattern. 3.

  • Page 21: Forward Slips To Land

    Forward slips to land Maneuver standards: touchdown within 400 feet of selected point. 1. Complete the “Approach Checklist” before entering the airport; devote full attention to aircraft control and traffic avoidance. 2. Slow to 90 KIAS prior to entering downwind or traffic pattern and complete the before landing checklist.

  • Page 22: Emergency Procedures

    Emergency Procedures. Emergency Descent 1. Throttle closed and mixture rich for the practice manuever (SIMULATE emergency checklist) 2. Get air speed above 100kts 3. Roll into a 45 degree bank, allowing the nose to drop and initiating a descent 4. Allow the airspeed to stabilize at Vno execute medium bank 90 degree turns. 5.

  • Page 23: Slow Flight

    Slow Flight Maneuver standards: ALT +/- 100’ Bank 5°+/-5° HDG +/-10° Speed +10 -0kts NOTE: Minimum safe altitude for this maneuver is 1500’ AGL, Crosswinds Aviation requires a minimum altitude of 3,500’ AGL. Slow flight is performed in the landing Configuration 1.

  • Page 24: Power Off Stalls

    5. Slow to V R (55 KIAS) 6. Add 10 of bank if performing turning stalls ° 7. Simultaneously pitch up and increase power to 2200 RPM 8. Maintain coordination at all times 9. Recognize and announce symptoms of approaching stall 10.Sight, sound, feel 11.Stall warning horn activates 12.Aerodynamic buffeting...

  • Page 25: Ground Reference Maneuvers

    10.Complete both CLIMB and CRUISE checklists after leveling off Note: If engine appears to drop below 1,000 RPM, add throttle to ensure engine will not stop. Ground Reference Maneuvers. NOTE: All ground reference maneuvers are performed at 1,000’ AGL, and are entered on a downwind leg simulating traffic pattern altitude and are performed in the “Clean”...

  • Page 26: Turns Around A Point

    Turns around a point 5. Select a reference point 6. Set power to maintain an airspeed of 90kts 7. Maintain 1000 AGL 8. Clear the area of other aircraft 9. Trim the airplane for level, hands-off flight 10.First turn to the left at the highest groundspeed and steepest bank angle (max 45 degrees) 11.Bank angle will gradually need to be decreased to the upwind point (slowest groundspeed) 12.From the upwind point, bank angle will need to gradually increase to the 13.downwind point (fastest groundspeed)

  • Page 27: S-Turns

    S-Turns 1. Select a line feature that lies crosswind 2. Set power to maintain an airspeed of 90kts 3. Maintain 1000 AGL 4. Trim the airplane for level, hands-off flight 5. Approach the line feature downwind 6. Cross the line feature wings level 7.

  • Page 29: C172S Quiz Questions

    C172S Quiz Questions. Students must have 100% prior to check ride References: C172S POH, C172S Training guide
 The C172S engine is made by How many volts is the C172S electrical A. Lycoming system? B. Continental A. 12 C. Diamond Aircraft corp. B.
  • Page 30 A. True A. True B. False B. False How much usable fuel does the C172S Brake fluid is what color? hold? A. Red A. 56 gallons B. Clear B. 53 gallons C. Yellow C. 35 gallons List all the V speeds for the C172S. The C172S has two separate fuel pumps for pump and prime? A.
  • Page 31 B. False...

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