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LS10-s / LS10-st - DG Flugzeugbau

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Flight manual <<strong>st</strong>rong>LS10</<strong>st</strong>rong>-s,-<strong>st</strong><br />

6. Power plant checks (only <<strong>st</strong>rong>LS10</<strong>st</strong>rong>-<strong>st</strong>)<br />

a) Extend engine completely using the manual switch. The extension time<br />

should not exceed 13 seconds!<br />

b) Check the engine extension-retraction mechanism by operating it in both<br />

directions.<br />

c) Check all screwed connections and their securing.<br />

d) Check ignition sy<strong>st</strong>em incl. wires and the spark plug connectors for tight<br />

fit.<br />

e) Check engine retaining cable and its connections in the engine<br />

compartment and at the engine.<br />

f) Check fuel lines, electrical wires, and <strong>st</strong>ructural parts for wear and kinks.<br />

g) Check exhau<strong>st</strong> muffler, mechanical fuel pump and accessories for tight fit<br />

and any cracking.<br />

h) Apply <strong>st</strong>rong pressure to the engine in forward, backward and sideward<br />

directions to check if the bolted connection between the engine block and<br />

the engine mount or any thing else is loose or damaged. Also check the<br />

rubber mounts of the engine.<br />

i) Visual check of the propeller and mounting bolts. Check propeller swivel<br />

bearing for wear of rubber elements and for free swivel travel.<br />

j) Check decompression sy<strong>st</strong>em: Check condition of the decompression<br />

valve bowden cable at the engine mount for no kinks. Check condition of<br />

the cable, thimbles and additional connections.<br />

Move decompress lever into the “open” position. Turn propeller by hand<br />

and check decompression.<br />

k) Move decompress lever in the “closed” position. Turn the propeller 1<br />

revolution by hand, check for compression and li<strong>st</strong>en for abnormal<br />

sounds which may indicate engine damage.<br />

l) Drain condensed water from the fuel tank. The drainer is located behind<br />

main landing gear box.<br />

m) Check the outlet of the fuel tank ventline for cleanliness, the outlet is<br />

located behind the landing gear box.<br />

n) Check fuel sy<strong>st</strong>em see detailed li<strong>st</strong> on next page.<br />

o) Check if the propeller-<strong>st</strong>opper will be pressed forward by its gas-<strong>st</strong>rut.<br />

The powerplant mu<strong>st</strong> be in the position propeller-<strong>st</strong>opper extended for<br />

this check.<br />

p) Check engine bay fire protection paint for cracks and delaminations.<br />

q) Execute fuel sy<strong>st</strong>em check, see in<strong>st</strong>ructions on next page.<br />

r) Retract engine using the manual switch on the DEI-NT. Confirm that the<br />

engine bay doors are closing properly.<br />

Issued: October 2009 EASA app. 4.12

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