SECTION
3
CESSNA
,.=
EMERGENCY PROCEDURES
MODEL
2088 (675 SHP)
I
FLAP SYSTEM MALFUNCTION PROCEDURES
(Continued)
,
~
FLAPS
FAIL
TO EXTEND OR RETRACT
(Continued)
,
.
Later Airolanes:
A. ~u~rded and Safetied Standby Flap Motor Switch (Overhead)
,
.
-
MOVE GUARD, breaking safety wire, and POSITION
SWITCH TO
STBY.
,
~
~
~
6.
Guarded and Safetied Standby Flap Motor UplDown Switch
(Overhead)
-
MOVE GUARD, breaking safety wire, and
position switch UP or DOWN (hold switch until flaps reach
desired position, except release switch before flaps reach full
up or full down travel).
CAUTION
WlTH THE STANDBY FLAP SYSTEM IN USE, LIMIT
SWITCHES, WHICH NORMALLY SHUT OFF THE
PRIMARY FLAP MOTOR WHEN REACHING THE FLAP
TRAVEL LIMITS, ARE ELECTRICALLY INACTIVATED.
THEREFORE, THE PILOT MUST RELEASE THE
STANDBY FLAP MOTOR
UPIDOWN SWITCH BEFORE
THE FLAPS REACH THEIR TRAVEL
LIMIT TO PREVENT
OVERLOADING AND DAMAGE TO THE FLAP SYSTEM.
3.
Guarded Standby Flap Motor Switch
-
Leave in STBY position
until after landing when maintenance action can be
accomplished.
LANDING GEAR MALFUNCTION PROCEDURES
LANDING WlTH FLAT MAIN TlRE
1.
Airplane
-
FLY as desired to lighten fuel load.
2. Fuel Selectors
-
POSITION ONE SlDE OFF TO LIGHTEN LOAD
ON
SlDE OF FLAT TlRE (maximum fuel unbalance of 200
pounds).
3. Approach
-
NORMAL (flaps FULL).
4.
Touchdown
-
INFLATED TlRE FIRST. Hold airplane off flat tire as
long as possible with aileron control.
5. Directional Control
-
MAINTAIN using brake on wheel with
inflated tire as required.
(Continued Next Page)
-.
Revision 23
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