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21 

Note

Engine Roughness 

1.

 

Carb Heat...................................................................................................................... On 

 

If Roughness Continues After 1 Minute:

 

2.

 

Mixture.................................................................................................... Max Smoothness 

3.

 

Carb Heat.......................................................................................................... ............ Off 

4.

 

Fuel Pump...................................................................................................................... On 

5.

 

Fuel Selector.................................................................................................. Switch Tanks 

6.

 

Engine Indicators.................................................................................... Monitor/DECIDE 

7.

 

Magnetos................................................................................................ Verify Singlularly 

 

Prepare for Engine Power Loss (In Flight)

 

 

Description: 

Engine roughness can be caused by several factors including carburetor or intake icing, ice build up over the air intake, carbon 

build up on the spark plugs, fuel contamination, fuel deficiencies, excessive leaning, and more. 

 
Common Errors: 

o

 

Failure to respond quickly to engine roughness 

o

 

Misdiagnosis of the prevailing issues 

o

 

Lack of planning for emergency maneuvers  

o

 

Failure to aviate, navigate, communicate  

 

Emergency Descent 

1.

 

Power............................................................................................................................ Idle 

2.

 

Mixture......................................................................................................................... Full 

3.

 

Carb Heat.......................................................................................................... ............. On 

4.

 

Airspeed.................................................................................................................. 73 KTS 

5.

 

Bank.......................................................................................................................... 35-45

o

 

6.

 

Landing Spot.................................................................. Recover from Descent Downwind  

 

Prepare for Landing (No Engine Power)

 

 

Description: 

A spiraling descent is made as rapidly as possible to lower alitutde or to the ground for an emergency landing. A fire, sickness, 

loss of cabin pressurization, or other situations may demand this maneuver.  

 
Common Errors: 

o

 

Failure to respond quickly to the emergency 

o

 

Failure to properly configure the airplane 

o

 

Lack of coordination and control (airspeed or rate of descent) 

o

 

Loss of reference point or becoming disoriented 

o

 

Failure to aviate, navigate, communicate  

 

Содержание Skyhawk 172N

Страница 1: ...only the basic steps and sequences This guide should be used in conjunction with most current versions of FAA H 8083 3 the FAA Airmen Certification Standards Practical Test Standards and the Pilot s O...

Страница 2: ...2 1 Preflight Normal Operations 2 Engine Starting 3 Takeoff Operations 4 Performance Maneuvers 5 Ground Reference Maneuvers 6 Landing Operations 7 Instrument Procedures 8 Emergency Procedures...

Страница 3: ...1 Max Gross Weight 2550 lbs 2 Taxi Fuel Burn 8 lbs V Speeds VS0 41 VS1 47 VFE 85 VNO 128 VNE 160 VX 59 VG 65 VY 73 VA 89 97 X Wind 17 Leaning Procedures 1 Lean Assist Hold 2 Mixture Level Lean Until...

Страница 4: ...n engine roughness hot spots and detonation Common Errors Not leaning the mixture while on the ground Engine overheating due to high oil temperatures during prolonged runup Failure to hold the brakes...

Страница 5: ...getting the airplane airborne as quickly as possible to eliminate surface drag Shift weight from the landing gear to the wings via a high AOA to accomplish this Then fly within ground effect increases...

Страница 6: ...icted by obstructions the airplane must be flown precisely at its maximum limit of takeoff performance This results in the shortest ground roll and steepest angle of climb Common Errors Failure to uti...

Страница 7: ...rspeed 47 KTS Just Above Stall 5 Throttle As Required 2200 RPM 6 Recovery 7 Throttle Full 8 Flaps Retract Incrementally Description Low airspeed and high AOA attitudes while at altitude simulates the...

Страница 8: ...iance on instrument instead of visual references Power On Stall Perform Flow Checklist 1 Altitude Above 1500 AGL 2 Throttle 1700 RPM 3 Airspeed 65 KTS 4 Throttle Full 5 Pitch As Required to Induce Sta...

Страница 9: ...laps Up Incrementally Carb Heat Off Description Practiced to develop awareness and corrective responses to improper control inputs during a turn simulating landing or when trying to stretch a glide wh...

Страница 10: ...gross weight airplane configuration and power setting an airplane will consistently stall at the same indicated airspeed However a stall will ooccur at a higher indicated airspeed with excessive mane...

Страница 11: ...on The objective is to rapidly dissipate excessive altitude necessary during emergencies while remaining over top of a selected landing spot Common Errors Inadequate pitch on entry or rollout Gaining...

Страница 12: ...ding 180 o From Entry 4 Resume Normal Cruise Establish Description This maximum performance climbing turn finishes 180 from the initial altitude below and just above stalling speed The goal is to obta...

Страница 13: ...try Level d Heading 180 o From Entry E Reverse Direction Repeat Maneuver 5 Resume Normal Cruise Establish Description Intended to enhance proper coordination of the flight controls throughout a wide r...

Страница 14: ...l Altitude Groundspeed 11 3 1000 PA 2 Airspeed Established at 90 kts 3 Enter Downwind Between Pylons A Above pivotal altitude reference line move rearward B At pivotal altitude aircraft pivots on refe...

Страница 15: ...irplane by holding backpressure as long as practicable Common Errors Unstable approach excessive descent rate or airspeed Round out too high Poor power management during round out and touch down Hard...

Страница 16: ...ain directional control Failure to abort an unsafe approach Power Off 180 o Pre Landing GUMPPS Checklist 1 Abeam Power Idle 65 KTS Trim 2 Base Flaps 10 o as Necessary 3 Final 65 KTS Flaps as Necessary...

Страница 17: ...and or landing configuration conditions cannot safely be assured a landing must aborted The earlier a go around can be initiated the safer its execution becomes Common Errors Pride believing a rejecte...

Страница 18: ...Radio Radial Nav Source Reaching MDA DA Level Off 1 Throttle As Required 2 Pitch Level Flight 3 Trim Adjust 4 Time Monitor At MDA if runway is in sight per 91 175 continue and land If requirements ar...

Страница 19: ...Ahead C Brakes As Required 2 Insufficient Runway Remains A Perform ABCD Checklist B Landing Straight Ahead Avoid Obstacles C Flaps As Necessary 3 Sufficient Altitude Gained Attempt Restart A Perform A...

Страница 20: ...ding No Engine Power Perform ABCD Checklist 1 Airspeed 65 KTS 2 Landing Pattern Established 1000 AGL When Committed to Landing 3 Airspeed 65 KTS 4 Flaps As Necessary 5 Throttle Idle 6 Mixture Cut off...

Страница 21: ...sdiagnosis of the prevailing issues o Lack of planning for emergency maneuvers o Failure to aviate navigate communicate Emergency Descent 1 Power Idle 2 Mixture Full 3 Carb Heat On 4 Airspeed 73 KTS 5...

Страница 22: ...22 Notes...

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