Aquila A211 Instructions d'exploitation Page 115

  • Télécharger
  • Ajouter à mon manuel
  • Imprimer
  • Page
    / 146
  • Table des matières
  • MARQUE LIVRES
  • Noté. / 5. Basé sur avis des utilisateurs
Vue de la page 114
Aviation
AIRPLANE FLIGHT MANUAL
AQUILA AT01
Section 7
SYSTEM DESCRIPTION
Document No.: Issue: Supersedes Issue: Date: Page:
FM-AT01-1010-100E
A.12 A.05 (30/09/2003) 17/09/2008 7 - 11
7.4.3 Cabin Heat
For the cabin heating, ram air is heated in a shrouded chamber at the exhaust muffler
and flows through a duct into the cabin if the heat control valve is opened. Behind the
firewall, the heated air is subdivided for windshield defrosting and cabin heating.
The control element to open or close the heat control valve is located in the control
panel below the midsection of the instrument panel.
7.4.4 Cabin Ventilation
Two adjustable ventilation nozzles are located on both sides of the instrument panel to
supply the cabin with fresh air. The amount and direction of fresh airflow can be
adjusted individually for each seat by pivot-mounted nozzle outlets. If required, the sash
windows of the canopy may additionally be opened for the ventilation of the cabin.
7.5 UNDERCARRIAGE
The landing gear consists of a steerable nose gear that is equipped with a shock
absorber and a main landing gear. To provide precise control of the aircraft while taxiing
on ground, the nose gear strut is directly linked with the rudder pedals.
The main gear struts are designed as leaf springs to absorb the touch-down loads
during landing. Hydraulically actuated disc brakes are provided on the main gear wheels
which are activated by tilting the rudder pedals in the forward direction.
Because of the robust landing gear and the 5.00 x 5 wheels on the nose and main
landing gear in combination with sturdy wheel fairings, the aircraft is suitable for the
operation on airfields with grass runway.
7.5.1 Nose Landing Gear and Nose Gear Steering
The nose landing gear consists of a tubular steel strut that is attached pivot-mounted to
the engine frame support.
A portion of the nose gear loads is directly transferred into the front structure of the
fuselage via the lower attachment fittings of the engine frame support by two support
struts.
Good shock absorption and suspension characteristics are provided by a shock
absorber unit equipped with stacked rubber springs which acts directly on the nose
wheel fork.
The steering of the nose wheel is accomplished by a spring loaded steering rod
assembly that connects the nose gear steering arm at the upper end of the nose gear
Vue de la page 114
1 2 ... 110 111 112 113 114 115 116 117 118 119 120 ... 145 146

Commentaires sur ces manuels

Pas de commentaire