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Section 7 – Airframe and Systems description
AIRFRAME
2.5. NOSE LANDING GEAR
A Pivoting nose gear is attached to the firewall reinforcement plate. The shock absorber is
fitted on the upper machined component and directly on the nose landing gear structure.
In Figure 10 is shown:
1) Hydraulic shock absorber
2) Firewall
3) Nose wheel (5.00-5 tire, inflated at 32 PSI (2.2 BAR))
Fig. 7-7. NOSE LANDING GEAR