Figure 11: Layers of Cloth in the Center Section Top Shells
53-10-00
Stabilizers
AMM
CHAPTER 55
STABILIZERS
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55-TITLE
AMM
Intentionally left blank
55-TITLE
Stabilizers
AMM
TABLE OF CONTENTS
CHAPTER 55
STABILIZERS
1. General ..............................................1
Section 55-10
Horizontal Stabilizer
1.
General ..............................................1
2.
Description............................................1
Maintenance Practices
1.
General ............................................201
2.
Remove/Install the Horizontal Stabilizer....................201
3.
Repair Data for the Horizontal Stabilizer Shells ..............205
Section 55-20
Elevator
1.
General ..............................................1
2.
Description............................................3
Maintenance Practices
1.
General ............................................201
2.
Remove/Install the Elevator.............................201
3.
Remove/Install the Elevator Trim Tab .....................204
4.
Repair Data for the Elevator Shells .......................206
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AMM
Section 55-30
Lower Fin
1.
General ..............................................1
2.
Description............................................1
Maintenance Practices
1.
General ............................................201
2.
Remove/Install the Lower Fin............................201
Section 55-40
Rudder
1.
General ..............................................1
2.
Description............................................3
Maintenance Practices
1.
General ............................................201
2.
Remove/Install the Rudder..............................201
3.
Repair Data for the Rudder Shells ........................203
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55-CONTENTS
Stabilizers
AMM
CHAPTER 55
STABILIZERS
1. General
The DA 40 has the usual stabilizers. The vertical stabilizer is part of the fuselage. The aft part of the left and right fuselage shells make the left and right shells of the vertical stabilizer. See Section 53-10 for data on the fuselage structure.
The horizontal stabilizer has top and bottom shells. Each shell has GFRP skins. The horizontal stabilizer has a front spar and a rear spar. Both spars have mounting brackets. Three pairs of ribs give strength to the center area. Two trailing edge webs hold the hinges for the elevator.
The elevator has top and bottom shells. Each shell has GFRP skins with a rigid foam core. The bottom shell also makes the leading edge spar. The hinges attach to the bottom shell. A large horn with the mass balance weight attaches to the bottom shell at the center. The trailing edge carries a trim tab.
The lower fin is a GFRP molding. Bolts attach the lower fin to the bottom of the fuselage.
The rudder has left and right shells. Each shell has GFRP skins with a rigid foam core. The shells bond together at a flange. The hinges attach to the top face of the rudder and a flat face near the bottom of the leading edge. The horn near the top makes the rudder mass balance.
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