TM  1-1520-240-10            8-2-5 ness and release cable connected and dust caps stowed. If hook not installed, check for dust caps on the electrical and release cable receptacles. 5.   Lower anti-collision light — Check condition. 6.   Static port — Check unobstructed. * 7.   Fuel system — Check as required, caps se- cure. O 8.   ERFS  II  Installed.  Aircraft  Overboard  Drain Outlets — Check. Check for any fuel seepage. O 9.   ERFS   II   Installed.   Aircraft   Overboard   Vent Outlets — Check. Check for signs of exces- sive fuel venting. 10.   NO. 1 Engine. a.   Inlet for foreign objects. Check condi- tion and security of FOD screens. O b.   EAPS   —   Check   general   condition, check vortex tubes for erosion and da- mage.  Check  seals  for  condition  and damage. Check rail and slide mecha- nisms. Inspect blower fan blades dam- age and erosion. c.   Check fuel, oil, hydraulic, electrical, (O) wash  kit,  and  drain  lines  connections and leaks. d.   Cowling for security. 11.   Left aft landing gear area — Check condition and security of all components as follows: a.   Gear support structure. b.   Tire. c.   Shock   strut   extension   and   static   lock stowed. d.   Static ground wire contacting the ground. e.   Fluid lines. f.   Electrical wiring. g.   Ground proximity switch and linkage. h.   Brakes. i.   Swivel lock. 12.   Vent  and  fluid  drain  lines  —  Check  unob- structed. O 13.   M-130 Safety Pin — Installed with streamer. 8-2-15.  Top of Fuselage. * 1.   No. 2 engine — Check as follows: a.   Inlet for foreign objects. Check condition and security of FOD screens. b.   EAPS  —  Check  for  foreign  objects, condition  and  security.  Seals  around driveshaft  fairing  and  engine  inlet  for damage. Rails and slide mechanisms for damage. c.   Oil level and cap secure. d.   Cowling for security. e.   Tailpipe condition and security, presence of fuel, oil, and foreign objects. 2.   Anticollision  light  and  formation  lights  — Check condition. * 3.    Aft rotor (right side) — Check blades for con- dition and reservoir levels. O 4.    Droop stop shrouds — Check condition and security. Check inspection cover closed. 5.    Upper boost actuator — Check for extended jam  indicators  and  exposed  piston  rods  for cleanliness. L 6.   Hydraulic compartment — Check as follows: a.   Condition   and   security   of   lines   and coolers. b.   No. 2 flight control system accumulator for proper indication (see figure 2-15-3). c.   Utility reservoir pressurization accumula- tor for 2500 to 3500 psi charge. * 7.   Combining transmission area — Check for obstructions.  Check  filter  buttons  for  en- gines and combining transmission. * 8.   Aft rotor (left side) — Check blades for con- dition and reservoir oil levels. O 9.   Droop stop shrouds — Check condition and security. 10.   Upper boost actuator — Check for extended jam  indicators  and  exposed  piston  rods  for cleanliness. * 11.    No. 1 engine — Check, same as NO. 2.. 12.   Drive shaft area — Check condition and secu- rity as follows: a.   Drive shaft, couplings, and mounts. b.   Fluid lines. c.   Control linkage. d.   Foreign objects. e.   Drive shaft fairing. * 13.   Forward rotor (right side) — Check same as aft rotor. 14.   Forward transmission oil cooler inlet — Check for obstructions.