P I L O T ’ S O P E R A T I N G H A
N D B O O K
V I P E R J E T M K I I
Revision 1
3-6
June 1, 2008
EMERGENCY LANDING GEAR EXTENSION
1.
AIRSPEED .............................................................................................. < 125 KIAS
2.
LANDING GEAR HANDLE ............................................................................ DOWN
3.
LANDING GEAR LIGHTS PTT ............................ PRESS (VERIFY LIGHTS WORKING)
4.
DCS CIRCUIT BREAKER .................................................................................. PULL
5.
EMERGENCY GEAR HANDLE ................................................. ROTATE CLOCKWISE
......................................................... until resistance is felt, pause for 2 seconds;
............................................ continue to turn clockwise until completely turned.
IF LANDING GEAR DOES NOT INDICATE DOWN
6.
AIRCRAFT ............................................................... YAW / PITCH TO ASSIST GEAR
NOTE: IF “GEAR UNSAFE” LIGHT IS LIT CONTINUOUSLY OR REPEATEDLY
DURING FLIGHT,
THIS INDICATES THAT THE HYDRAULIC PUMP IS RUNNING. TO AVOID OVERHEATING
PUMP, PULL DCS CIRCUIT BREAKER UNTIL SUCH TIME AS PUMP IS NEEDED (i.e., lower
landing gear, flaps, drag brakes, etc.) SO AS TO AVOID DAMAGE TO THE HYDRAULIC
PUMP.
INADVERTENT ICING
1.
PITOT HEAT ...................................................................................................... ON
2.
ALTITUDE .................................... CHANGE TO TEMP. LESS CONDUCIVE TO ICING
3.
DIRECTION ............................. TURN BACK TO TEMP. LESS CONDUCIVE TO ICING
4.
CABIN HEAT ...................................................................................................... ON
5.
DEFROST ........................................................................................................... ON
6.
OBSERVE.......................................................................... SIGNS OF INTAKE ICING
**LAND AS SOON AS PRACTICAL**
7.
APPROACH .............................................................................................. 120 KIAS
8.
LAND .......................................................................................... LEVEL ATTITUDE
STATIC SOURCE BLOCKED
1.
ALTERNATE STATIC SOURCE VALVE ................................................................. ON
2.
AIRSPEED ....................... CLIMB AND APPROACH 10 KTS FASTER THAN NORMAL
3.
ALTITUDE ........... CRUISE AND APPROACH 25
–
50 FEET HIGHER THAN NORMAL
Summary of Contents for ViperJet MkII
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