EasyManua.ls Logo

Eclipse Aviation Eclipse 500 - Empennage; Lower Fuselage; Upper Fuselage; Variable Outlet Ram Exhaust

Default Icon
88 pages
Print Icon
To Next Page IconTo Next Page
To Next Page IconTo Next Page
To Previous Page IconTo Previous Page
To Previous Page IconTo Previous Page
Loading...
36
9. Variable Outlet Ram Exhaust (VORE) CONDITION
Inspect the variable outlet ram exhaust for damage/blockage.
10. Pylon Panels CONDITION
Inspect both upper and lower surface of the pylon panels for damage. All pylon
surfaces should be smooth and free of deformities.
FUSELAGE
LOWER FUSELAGE
1. VCS Drain FWD CLEAR
Inspect forward VCS drain for blockage and damage.
2. Antennas CONDITION
Inspect all antennas for damage.
3. VCS Drain AFT CLEAR
Inspect aft VCS drain for blockage and damage.
4. Pressurization Outflow Static Ports L/R CLEAR
Inspect pressurization outflow ports damage which could result in a reduction of
proper airflow.
UPPER FUSELAGE
1. Antennas CONDITION
Inspect all antennas for damage.
EMPENNAGE
1. Tailstrike Fitting and Bumper Block CONDITION
Inspect tailstrike fitting and bumper block for wear or structural damage.
2. Right VOR Antenna CONDITION
Inspect VOR antenna for damage to the antenna and mounting surface.
3. Right Horizontal Boot CONDITION
Inspect boot for cracks, holes, chips, and wear. A damaged boot may not
inflate/deflate properly which could result in the inability to shed ice. In addition, a
damaged boot may not be held tight against the stabilizer which could result in a
significant loss in aircraft performance.
4. Tail Cone and Anti-Collision Lights CONDITION
Inspect anti-collision light/tail cone light for damage to lens and internal
components.

Table of Contents