TM 1-1500-204-23-1Figure 8-21. Fuel Line Disconnect(8) Disconnect the power control rod, as shownin figure 8-22, from the power control lever cross-shaftlinkage at the threaded end disconnect. Secure thepower control rod to the nacelle structure.b.Removal. The powerplant may be removedfrom the aircraft by either of the two methods. Onemethod involves lowering the powerplant from thenacelle by using an engine dolly. The other methodrequires hoists and a special sling to lower thepowerplant to a movable engine stand. Refer to theapplicable aircraft maintenance manual.Figure 8-22. Power Lever Disconnectc.PreparationforInstallation. Installation ofaircraft powerplants will be installed in accordance withthe applicable maintenance manual.d.Installation. Install engine in accordance withapplicable maintenance manual8-21/(8-2 blank)
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