DG Flugzeugbau DG-500M Onderhoudshandleiding - Pagina 7
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2
Inspections
2.1 Daily inspection
see flight manual DG-500M.
2.2 Regular inspections
A) After 200 flight hours and during the annual inspection
Check the rudder cables for wear especially around the "S" tubes on the
rudder pedals. Worn rudder cables should be replaced (see section 4.2).
Check the sealing of the rudder (see section 1.3.5).
B) Annual inspection (and 100hr inspection – only for USA)
• Execute all items of the daily inspection (see flight manual section 4.3).
Check especially the headrest securing ropes in the rear cockpit
according to "Working instruction No. 1 for TN348/20 issue 3"
(attached to this manual) for correct assembly and for wear.
• Check all control circuits: Inspect all bolted connections and locking
devices ie. locknuts, split pins etc.
• Check all control circuits for adequate greasing and rust prevention. (see
section 3.3).
• Check the control surface deflections (see section 1.2 - 1.4).
• Check the free play in all control circuits (see section 1.2 - 1.6) and the
fore and aft play of the wings (see section 1.10).
• Check the canopy emergency release (see flight manual section 7.15).
• Check the rubber cords in the control system (see section 1.2.6, 1.4.6
and 1.7.5).
• Check the thickness of the wheel brake linings and the thickness of the
wheel brake disc (see section 1.6.1.4).
• Check if the wheel brake fluid has been exchanged (see section 1.6.4).
• Check the complete power plant.
• Check the friction brake of the throttle control (see section 1.11.8).
• Propeller
You have to dismount the propeller for inspection especially for cracks
at the hub boss. After reassembling the propeller you should check the
blade track see section 3.5 of the propeller manual. After the first flight
after reassembling the propeller, you have to check the torque of the
propeller bolts again see section 3.5.1 item 33 of this manual.
• Tow hook
The operating and maintenance instructions for the release mechanisms,
see section 0.4 of this maintenance manual have to be followed.
• All-up weight and centre of gravity These should be checked at least
every 4 years during the yearly inspection.
Issued: September 2011
Copyright DG Flugzeugbau GmbH - any copy or publishing prohibited
Manual valid with the up-to-date cover page only
Maintenance Manual DG-500M
TN500/05
2.1