Optional Equipment
Rotorcraft Cargo Hook Kit
CSP–900RFM206E–1
ROTORCRAFT FLIGHT MANUAL
MD900 With PW 206E
FAA Approved
Original
10–20
PART VII
SYSTEM DESCRIPTION
Cargo Hook Installation (Figure 10−9):
Align cargo hook cable attaching hardware with landing gear saddle clamp assem6
blies.
Install FWD link assemblies into FWD saddle clamps.
Install FWD pin links into link assemblies and quick release pins into FWD
pin links.
Connect cargo hook electrical connector, load indicator electrical connector and
mechanical release control cable connector.
Repeat procedure for aft link assembly attachment.
Perform cargo hook preflight and operational checks.
Cargo Hook Removal (Figure 10−9):
Remove quick release pins from Aft pin links and remove cable assembly from
aft saddle clamps.
Disconnect cargo hook electrical connector, load indicator electrical connector
and manual release control cable connector.
Remove pin links attaching cargo hook cables and cargo hook to FWD landing
gear saddle clamp assemblies.
Remove cargo hook and bridle assembly.
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