Approvals; Conventions Used In This Manual - Sandel SN4500 Pilot's Manual

Primary navigation display with reversionary attitude mode
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Approvals

The FAA has approved the SN4500 under the following TSOs:
C3d:
Turn and Slip Instrument
C4c:
Bank and Pitch Instruments
C6d:
Direction Instrument, Magnetic (Gyroscopically
Stabilized
C34e: ILS Glide Slope Receiving Equipment
C35d: Airborne Radio Marker Receiving Equipment
C36e: Airborne ILS Localizer Receiving Equipment
C40c: VOR Receiving Equipment
C41d: Airborne ADF Equipment
C113: Airborne Multipurpose Electronic Displays
C118: Traffic Alert and Collision Avoidance System
Airborne Equipment, TCAS I
C119b: Traffic Alert and Collision Avoidance System
Airborne Equipment, TCAS II
The following RTCA certification levels also apply to this product:
DO-160E: Environmental (Categories listed in Chapter 11)
DO-178B: Software Level C
DO-254:
Hardware Level C
Installation of the SN4500 in a type-certificated aircraft must be
performed in accordance with the Sandel SN4500 Installation
Manual, document number 82009-IM applicable revision.
82009-PG, REV D1
SANDEL SN4500 PILOT'S GUIDE
WELCOME TO THE SN4500
PAGE
V

Conventions Used in This Manual

The name of a button is placed within square brackets when the
button is described in text.
For example, "...press the [VUE]
selection button to ..."
This manual uses terms, which should be familiar to aviation-
minded readers, such as "selected radial" and "magnetic heading".
Terms, which are specific to the SN4500, will be placed in the
glossary.
82009-PG, REV D1
SANDEL SN4500 PILOT'S GUIDE
WELCOME TO THE SN4500
PAGE
VI

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