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T-34C AIRCRAFT SYSTEMS FAMILIARIZATION
CHAPTER NINETEEN
WORKBOOK
1902. LANDING GEAR SYSTEM
The landing gear system (Figure 19-1) is an electrically operated, fully retractable, tricycle type
landing gear. The main gear retracts inboard into the wings and the nose gear retracts aft into the
fuselage. The landing gear system is actuated by a single reversible DC motor and gearbox
mechanism which is located under the front cockpit. Due to the high speed (10,500 RPM) of the
motor, the gear will extend and retract in four seconds.
Figure 19-1 Landing Gear System
System Operation
When the landing gear handle is moved to the UP or DOWN position, motion of the gear is
achieved by action of the DC motor and gearbox mechanism through a push-pull rod to each
main gear V-brace and the nose gear V-brace. The V-braces further connect to a side brace on
the main gear and a drag brace on the nose gear which then further connects to each landing gear
LANDING GEAR SYSTEMS 19-3


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