Cessna 210B - Landing Emergencies; Forced Landing (Precautionary); Forced Landing (Engine Failure)

Emergency Procedures
(3) Operate the hand pump up and down until the down indicat or (('I
light comes on, and continue pumping until the landing g e,lr hlltHf
returns to neutral.
NOTE
The landing gear cannot be retracted with the emergen cy hllfl,I
pump. If the gear will not retract normally, extend the gear, ln nll
and have the malfunction corrected.
If the wing flaps fail to extend normally, plan to make a fla ps -I ll' I i
ing, unless there is another person aboard to assist. It is impr.1I II
for the pilot alone to hold down the spring-loaded flap handle, optlr.iI. I
hand pump, and fly the airplane at the same time.
LAN DI NG EMER GENCIES {Except Ditchin g }.
FORCED LANDING (Precautionary Landing with Power).
(1) Drag over selected field with flaps 20° and 90 MPH air sp ol'd. 11011
type of terrain and obstruction.
(2) If surface is smooth and hard (pasture, frozen lake , etc). I"
wheels-down landing using full flaps and keeping nose whe el tllf I' "
as long as practical.
(3) If surface is rough or soft, plan a wheels-up landing ali Ifill
a. Approach with flaps down at 75 to 85 MPH.
b. Turn off all switches except ignition switch.
c. Unlatch cabin door prior to flare -out.
d. Reduce power to a minimum during flare-out.
e. Prior to contact, turn ignition switch "OFF. "
f. Land in a slightly tail-low attitude.
g. Attempt to hold the tail low throughout slide.
FORCED LANDING (Complete Engine Failure).
In the event of a complete engine failure, maximum g li dillt~ til flU
can be obtained by maintaining 95 MPH indicated air speed with f h. ' I UIII
gear and wing flaps retracted. Refer to the Maximum Gli de Dill' ,.01
page 4-3 for maximum glide data.
(1) Pull mixture control knob to idle cut-off.
(2) Turn fuel selector valve handle to "BOTH OFF."
(3) Turn off all switches except master switch.
(4) Approach at 85 to 95 MPH.
(5) If field is smooth and bard, extend landing gear within ",1I.lff.
Emergency Procedures
I.IIII·U of field.
IJ) If engine is windmilling, extend flaps as necessary within gliding
,lln l.mee of field.
NOTE
T h ,' wlndmilling engine will provide sufficient power for extending
illI , wing flaps. If the engine is not windmilling, plan to make a
n"ps - up landing.
( '7 ) Turn off master switch.
(II) Make a normal landing, keeping nose wheel off ground as long as
I' .·Ilr llcal.
( II ) If terrain is rough or soft, plan a wheels-up landing as follows:
a. Approach at 85 to 95 MPH with gear and flaps retracted.
u. If practical, extend flaps within gliding distance of field.
c. Turn off master switch.
d. Unlatch cabin door prior to flare-out.
c. Land in a slightly tail-low attitude.
£. Attempt to hold tail low throughout slide.
II
MAXIMUM GLIDE
II SPEED 95 MPH (lAS) • GEAR AND FLAPS RETRACTED
PROPELLER WINDMILLING (LOW RPM) • ZERO WIND
I c:;:::: .......................................................................... ~ .. ~ ....................... . ·.~·.·.·.·.·.·:~··;·;;:~j;;::~lr!!.·
6000
w
: ::: :·····::·::··;::·~:::·;;······-;;;:':"r·
C)
o 4.5 9.0
13.5
18
22.5
w
GROUND DISTANCE (STATUTE MILES)
Figure 4-1.
4-3
4-2