Kodiak 100 Series Information Manual page 331

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Dual Actuated Inertial Particle Separator System
(This section applies to Serial Numbers 100-00043 and up OR airplanes
equipped with the KODIAK TKS Ice Protection System.)
The Dual Actuated Inertial Particle Separator (DIPS) system employs two
mechanically linked moveable doors, a fixed turning vane, and an ice
shedder, all housed in a fiberglass composite intake duct. The first door
pivots about the top forward edge of the duct and the trailing edge comes to
rest on the upper surface of the turning vane in its deployed position. When
stowed, the first door retracts to serve as the upper surface of the intake duct
immediately prior to the exit from the diffuser section of the air intake system.
The basic function of the rear door (also termed the bypass door) is to block
off the bypass ducts during NORMAL operation (thereby increasing the ram
air recovery), and to direct debris and bypass airflow overboard in BYPASS
mode. The figure below shows the basic features of the IPS.
FIGURE KEY:
1. Dual Actuators
2. Three position switches,
one limit switch
3. Interconnecting rod
4. Adjustable FOD Door
Actuating Arm
5. Adjustable length Bypass
Door Actuating Arm
6. Two-Piece Ice Shedder
7. Slider Mechanism
Manual Actuator Override Switch for Dual Actuated IPS
The Inertial Separator on your aircraft is equipped with an actuator override.
This actuator override allows the pilot to advance the system to BYPASS in
the event of a failure of the normal engine inlet BYPASS function.
ENGINE INLET OVERRIDE
P i l o t 's O p e r a t i n g H a n d b o o k
1 0 0 S E R I E S
2
4
5
3
6
1
7
Figure 7-71 – Dual Actuated IPS
Figure 7-72 – Dual Actuated IPS
D O N OT U S E FO R FL I G H T O PE R AT I O N S
AIRPLANE & SYSTEMS DESCRIPTIONS
PRIMARY INLET OPERATION
S e c t i o n 7
7- 91