TM 55-1520-240-PM PHASE NO. _____ Area Name and No. Aircraft Serial No. Date NO. 2 ENGINE AREA #5 Inspect Phase No’s Inspection Requirements Status Faults and/or Remarks Action Taken Initial 2, 4, C 5.24 Drain and reservice engine oil. Do not overfill. ALL 5.25 Forward and aft engine mount and drag link for condition.  (Installed.) If drag link has play, refer to TM 55-1520-240-23. ALL 5.26 Tailpipe, exhaust diffuser, inner cone, and power turbine for cracks, hot spots, and burned areas. Tailpipe for security and for presence of fuel, oil, or foreign objects. ALL 5.27 Engine cowling for cracks, chafing, twisting and loose or missing fasteners. Hinges and adjacent structures for loose or missing hinge pins, cracks, wear, and loose or missing rivets. Chafing strips and seals for deterioration and security. Cowling closed and latched. NOTE If EAPS is installed, perform the following inspections with EAPS module slid forward, away from engine. Do quickly to avoid getting sand into engine. "FOD REMINDER" Check work area for tools and parts after completion of maintenance and inspection. 2-32