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checklist - ERAU ETA - Embry-Riddle Aeronautical University

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38 PA-28R-201 SOP<br />

3. FUEL TANK VENT CHECK<br />

CHECK that the FUEL TANK VENT (located on underside of wing) is<br />

unobstructed. The fuel tank vent provides a venting source to<br />

accommodate changing pressure in the fuel tank to ensure proper fuel flow.<br />

It is normal to see fuel or evidence of fuel (blue staining) at the vent due<br />

fuel expansion as its temperature increases.<br />

4. TIE-DOWN/CHOCKS REMOVE<br />

Slowly REMOVE the TIE-DOWN to avoid any under wing damage and<br />

place the chain adjacent to, but not in, the indentation of the concrete<br />

around the chain’s ramp securing points (water accumulation in these<br />

areas will rust the chains). Place the CHOCKS over the chain’s ramp<br />

securing point to keep them away from the landing gear and propeller.<br />

5. FUEL QUANTITY VERIFY (CHECK)<br />

VERIFY that the FUEL QUANTITY has been checked at least once since<br />

the last refueling. If the aircraft has been refueled since originally sampling<br />

the fuel, CHECK the fuel again for proper grade and for any debris.<br />

6. LEADING EDGE INSPECT<br />

INSPECT the LEADING EDGE of the wing for dents and cracks.<br />

7. STALL WARNING VANE CHECK<br />

CHECK the STALL WARNING VANE for freedom of movement and ensure<br />

that it is unobstructed. Listen for microswitch contact.<br />

8. PITOT MAST CHECK<br />

CHECK the PITOT MAST mounting and verify that the ram air intake and<br />

the drain hole are free of obstructions, and, if applicable, that the static port,<br />

located on the back of the mast, is free of any obstruction.<br />

9. WING TIP/LIGHTS INSPECT<br />

INSPECT the WING TIP for dents and cracks. If a crack exists, verify that<br />

is has been stop drilled to prevent further cracking. INSPECT the condition<br />

of the strobe and position LIGHTS.<br />

10. AILERON/FLAP INSPECT<br />

INSPECT the AILERON and FLAP, checking for freedom of movement<br />

and/or security of the hinges and actuators.<br />

Revised 07-01-2012 © <strong>Embry</strong>-<strong>Riddle</strong> <strong>Aeronautical</strong> <strong>University</strong> Rev 06

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