🔵✈️ 137. Important Characteristics of an Aircraft Empennage 🚁🎞️
Source: FAA-H-8083-31A, Aviation Maintenance Technician Handbook– Airframe, Volume 1, Pag
: 1-22
Aircraft: Empennage
The empennage of an aircraft is also known as the tail section. Most empennage designs consist of a tail cone, fixed aerodynamic surfaces or stabilizers, and movable aerodynamic surfaces.
The tail cone serves to close and streamline the aft end of most fuselages. The cone is made up of structural members like those of the fuselage; however, cones are usually of lighter construction since they receive less stress than the fuselage.
The other components of the typical empennage are of heavier construction than the tail cone. These members include fixed surfaces that help stabilize the aircraft and movable surfaces that help to direct an aircraft during flight.
The fixed surfaces are the horizontal stabilizer and vertical stabilizer. The movable surfaces are usually a rudder located at the aft edge of the vertical stabilizer and an elevator located at the aft edge the horizontal stabilizer.
The structure of the stabilizers is very similar to that which is used in wing construction. Figure shows a typical vertical stabilizer. Notice the use of spars, ribs, stringers, and skin like those found in a wing. They perform the same functions shaping and supporting the stabilizer and transferring stresses.
Bending, torsion, and shear created by air loads in flight pass from one structural member to another. Each member absorbs some of the stress and passes the remainder on to the others. Ultimately, the spar transmits any overloads to the fuselage. A horizontal stabilizer is built the same way.
| Component Name PDF | Type of Surface PDF | Primary Function PDF | Construction Weight PDF | Structural Members PDF | Load Transfer Mechanism PDF |
Vertical Stabilizer | Fixed Surface | Stabilize the aircraft during flight | Heavier construction than the tail cone | Spars, ribs, stringers, and skin | Bending, torsion, and shear stress pass between members; spars transmit overloads to the fuselage |
Horizontal Stabilizer | Fixed Surface | Stabilize the aircraft during flight | Heavier construction than the tail cone | Spars, ribs, stringers, and skin | Bending, torsion, and shear stress pass between members; spars transmit overloads to the fuselage |
Rudder | Movable Surface | Direct the aircraft during flight | Heavier construction than the tail cone | Spars, ribs, stringers, and skin | Distributes aerodynamic loads through the vertical stabilizer to the fuselage |
Elevator | Movable Surface | Direct the aircraft during flight | Heavier construction than the tail cone | Spars, ribs, stringers, and skin | Distributes aerodynamic loads through the horizontal stabilizer to the fuselage |
Tail Cone | Fixed (Non-aerodynamic) | Close and streamline the aft end of the fuselage | Lighter construction than the fuselage | Structural members similar to the fuselage | Receives less stress than the fuselage; distributes loads through internal structural members to the aft fuselage |