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Using this technique the aircraft can easily be turned and pushed backward. If additional assistance is required, a second person may push on the leading edge of the wings.
8.4.2. Parking
For short time parking, the airplane must be positioned in a headwind direction, the parking brake must be engaged, the wing flaps must be in the retracted position and the wheels must be chocked.
For extended and unattended parking, as well as in unpredictable wind conditions, the airplane must be anchored to the ground or placed in a hangar.
When parking the airplane, the flight controls lock, P/N 20-1000-01-00 must be installed and pitot static probe cover and stall warning plug should be fitted (refer to Chapter 7, Aircraft Description).
NOTE
WHEN ADJUSTING RUDDER PEDALS TO INSTALL FLIGHT CONTROLS LOCK, PULL STRAIGHT BACK ON T-GRIP. DO NOT PULL UP.
Parking in a hangar is recommended.
8.4.3. Mooring
The tail skid of the airplane has a tie down hole which can be used to moor airplane. Tie-down rings are also installed near the midpoint on each wing for tie-down mooring ropes. See Figure
8.2.
Figure 8.2. Mooring Points Location
8.4.4. Jacking
The DA20-C1 can be jacked at the two jack points located on the lower side of the fuselage's root ribs and at the tail fin. See Figure 8.3.
Figure 8.3. Jacking Point Location
8.4.5. Road Transport
When transporting the airplane on the road, it is recommended that you use an open trailer. All airplane components must be stored on a cushioned surface and secured to avoid any movement during transport.
A. Fuselage
The fuselage should be secured on the trailer standing on its wheels. Ensure that the propeller has sufficient free space so it cannot be damaged if the fuselage were to move.
B. Wings
For transportation, both wings must be removed from the fuselage.
To avoid any damage, the wings are stored in upright position on the leading edge with the root rib area positioned on an upholstered profiled surface of at least 1 ft. 4 in. (400 mm) width. The outside wing area (approximately 10 ft. (3 m) from the root rib area) is placed on an upholstered profiled surface of a minimum of 12 in. (305 mm) width.
The wings must be secured against movement rearward or forward.
C. Horizontal Stabilizer
The horizontal stabilizer is stored flat on the trailer and secured, or in an upright position sitting on the leading edge on a profiled surface. All supports must be upholstered with felt or foam rubber.
8.5. CLEANING AND CARE
CAUTION
Excessive dirt deteriorates the flight performance.
8.5.1. Painted Surfaces
CAUTION
DO NOT USE ANY CLEANING AGENTS CONTAINING SILICON BASED MATERIALS. ONCE APPLIED, SILICONE IS DIFFICULT TO REMOVE. SILICONE MAY RESULT IN CONTAMINATED BONDING SURFACES IF THE AIRCRAFT WERE EVER IN NEED OF STRUCTURAL REPAIR.
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本文链接地址：钻石20系列飞机维护手册 DA 20 SERIES AIRPLANE MAINTENANCE MANUAL(61)
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