TM 1-1520-240-MTF2-12EXTERIOR (CONT.)Aft Cabin (Cont.)c. Shock strut for proper extension,cleanliness, and static lock unlocked.d. Power steering actuator, wheel brakes, andhoses for leakage, chafing, and security.e. Electrical connections for condition andsecurity.f. Landing gear proximity switch — Condition,linkage adjustment, and security.5. Hydraulic system test panel — Check all capssecure.6. No. 2 engine — Check lower side as follows:NOTEIf TEAC/PAC is to be performed, all preflightinspection requirements/checks required prior toTEAC/PAC must be accomplished. In this case,EAPS must be moved forward of the engine togain access for inspection. If TEAC/PAC is notrequired, EAPS will remain locked into position infront of the engine.a. Inlet for foreign objects, hinges, latchsecured, and condition.O b. EAPS for general condition. Check vortextubes for erosion and damage. Check sealsfor condition. Check rail and slidemechanisms. Inspect blower fan blades fordamage and erosion. Check condition ofelectrical connectors, harness.c. Check fuel, oil, hydraulic, electrical, wash kitand drain lines for connection and leaks.d. Check engine for chafing lines and conditionand security of components.
Integrated Publishing, Inc. - A (SDVOSB) Service Disabled Veteran Owned Small Business
