Textron 172R180HP, Pilot Operating Handbook

Page: 64 / 396

(
SECTION 3
EMERGENCY PROCEDURES
CESSNA
MODEL 172R (180 HP)
TABLE OF CONTENTS (Continued)
Page
Electrical Power Supply System Malfunctions . . . . . . . . . . . 3-11
Ammeter Shows Excessive Rate of Charge
(Full Scale Deflection) . . . . . . . . . . . . . . . . . . . . . . . . . . 3-11
Low Voltage Annunciator (VOL TS) Illuminates During Flight
(Ammeter Indicates Discharge) . . . . . . . . . . . . . . . . . . . 3-11
Vacuum System Failure . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-12
AMPLIFIED EMERGENCY PROCEDURES
Engine Failure ................................. .
Forced Landings ............................... .
Landing Without Elevator Control ................... .
Fires ........................................ .
Emergency Operation In Clouds (Vacuum System Failure)
Executing A 180
°
Turn In Clouds ................ .
Emergency Descent Through Clouds .............. .
I
Recovery From Spiral Dive In The Clouds .......... .
Inadvertent Flight Into Icing Conditions ............... .
Static Source Blocked ......................... .
Spins ....................................... .
I
Rough Engine Operation Or Loss Of Power ........... .
Spark Plug Fouling ........................... .
Magneto Malfunction .......................... .
I
Engine Driven Fuel Pump Failure ................ .
Low Oil Pressure ............................ .
Electrical Power Supply System Malfunctions ......... .
Excessive Rate of Charge ...................... .
Insufficient Rate Of Charge ..................... .
Other Emergencies ............................. .
Windshield Damage .......................... .
3-13
3-15
3-15
3-16
3-16
3-16
3-17
3-17
3-18
3-18
3-19
3-19
3-19
3-20
3-20
3-20
3-21
3-21
3-22
3-22
3-22
3-2
Oct 4/01
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