Aerosonic OASIS Manuel utilisateur
Aerosonic Corporation September 18, 2012
1212 N. Hercules Ave.
Clearwater, FL 33765 USA
OASIS
Standby Instrument System
Installation Manual
Aerosonic Corporation September 18, 2012
1212 N. Hercules Ave.
Clearwater, FL 33765 USA
INSTALLATION MANUAL
OASIS
Original Aerosonic Standby Instrument System
Document No:
Revision: X
Title and Name
Signature and Date
OASIS Installation Manual
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OASIS Installation Manual
1 Table of Contents
1 .......................................................................................................Table of Contents
.................................................................................................................................. 4
1 ........................................................................................ GENERAL DESCRIPTION
.................................................................................................................................. 6
1.1 Introduction.................................................................................................................. 6
1.2 Scope .......................................................................................................................... 6
2 ......................................................................................................... INSTALLATION
.................................................................................................................................. 6
2.1 UNPACKING AND INSPECTING ................................................................................ 6
2.2 INSTALLATION PROCEDURES ................................................................................. 6
2.2.1 Location................................................................................................................ 6
2.2.2 Electrical Connections .......................................................................................... 6
2.2.3 Installation ............................................................. Error! Bookmark not defined.
2.2.4 Installation Guidelines for the SLZ7367................................................................19
OASIS Installation Manual
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OASIS Installation Manual
1 GENERAL DESCRIPTION
1.1 Introduction
This manual covers the OASIS standby instrument system, which includes the
Display Unit (DU), Aerosonic Sensor Unit (ASU) and the optional Magnetometer
(MSU).
NOTE
Installation must be made by qualified personnel, in conformance with applicable
government regulations. Standard installation practices described in FAA Advisory
Circular No. 43.1.-2B –Acceptable Methods, Techniques, and Practices –Aircraft
Alterations must be followed. The information furnished is for convenience only.
1.2 Scope
This manual applies to the installation of the OASIS standby display, remote sensor
unit and the optional external magnetometer.
2 INSTALLATION
2.1 UNPACKING AND INSPECTING
Carefully unpack the unit and note any damage to shipping containers or equipment.
Visually inspect each component for evidence of damage. Compare the equipment
received with that noted on the packing list. Immediately report any missing items or
evidence of damage to the carrier making delivery.
Every effort should be made to retain the original shipping containers for storage. If
the original containers are not available, a separate cardboard container should be
prepared that is large enough to accommodate sufficient packing material to prevent
movement.
2.2 GENERAL INSTALLATION PROCEDURES
NOTES
1. Standard installation practices prescribed in FAA Advisory
Circular Number AC 43.13-2B must be followed.
2.3 Electrical Connections
1. The installer must take the following into consideration before installation.
All wiring must be in accordance with industry-accepted methods, techniques,
and practices. Refer to FAA Advisory Circular AC43.13-2B, Section 4 and
Section 8 for aircraft wiring requirements.
The installer is responsible for supplying wires, cables and connectors.
All wires should be 22 AWG unless otherwise noted. Use IL-DTL16878 or
equivalent wire and M27500 or equivalent for twisted shielded wired for
installation.
The length and routing of the external cables must be carefully studied and
planned before attempting installation of equipment.
OASIS Installation Manual
Wire-marking identification is at the discretion of the installer.
The OASIS system should be placed on it’s own spare circuit breaker.
Use of any cable not meeting specifications voids all warranties.
2. Refer to the appropriate Interconnect Wiring Diagram in Figures #-# and :
3. Wires and cables associated with the OASIS installation shall be fabricated from,
Shielded cable shall be in accordance with MIL-C-27500 and non-shielded wire shall be
in accordance with MIL-W-22759/16.
Wires shall be cut to length as required at the time of installation. Wires shall be cut with
sufficient length to adhere to the main aircraft wire runs while maintaining specific aircraft
installation practices in accordance with the specific aircraft maintenance manual.
Reference the specific aircraft maintenance manual as the primary source for wiring
identification and installation practices. Wires are installed and terminated in accordance
with the system wiring diagrams in figures XX and XX
Figure #-# shows specific recommendation for shield termination for the MIL-27500
shielded cables for the OASIS system mating connectors.
It is recommended that no more than four shield wires be connected to a lug.
Solder sleeves shown in illustration are S03-03-R-100 from Allied Electronics/Tyco
FIGURE 1SHIELD TERMINATIONS
OASIS Installation Manual
2.4 DISPLAY UNIT INSTALLATION
When locating the OASIS DU in the instrument panel, take the following information
into consideration.
1. The OASIS DU should be located in an area where the softkey buttons are
within easy reach of the pilot.
2. The OASIS should be accessible for inspection , maintenance, or removal
and free from instrument panel structural flexure and excessive vibration or
heat.
3. The OASIS wiring cable should not run adjacent to heaters, engine exhaust,
heat sources or any high energy electrical sources that may cause
electromagnetic interference.
4. Compare the space requirements of the OASIS with the installation area
being considered. Refer to Figure 3 for dimensional requirements.
FIGURE 2OASIS DU
OASIS Installation Manual
FIGURE 3DU DIMENSIONS
OASIS Installation Manual
Perform the following installation procedures to install the OASIS standby
display.
5. See figures 4 and 5 for typical instrument panel mounting location for the
Oasis DU.
FIGURE 4TYPICAL FIXED WING INSTRUMENT PANEL
FIGURE 5TYPICAL ROTARY WING INSTRUMENT PANEL
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