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Becker BD406 - Rear Panel Installation - BD406 with Control Head; Avionic Bay Installation - BD406 Without Control Head; Figure 8: BD406-(XX1) (Front View); Figure 9: Drilling Template -Rear-Panel Installation

Becker BD406
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Installation
Becker Avionics
Installation Requirements
38 BD406/PBD406 DV16401.03 Issue 04 May 2021
Rear Panel Installation - BD406 with Control Head
The BD406 with control head is made for rear panel installation.
The four screws for installation are included with the delivery.
Keep a minimum of 5 mm between the BD406 and other avionics for air circulation.
More information please see: Dimensions, "BD406 with Control Head" page 40.
Dimensions mm (inch)
Figure 8: BD406-(XX1) (front view)
(no scale drawing)
Figure 9: Drilling Template -Rear-Panel Installation
Avionic Bay Installation - BD406 without Control Head
The BD406 without control head and mounting kit MK4401 are for avionic bay installation.
Keep a minimum of 5 mm between the device and other avionics for air circulation.
Order of Installation
Install MK4401 mounting frame in avionic bay environment, using three countersunk
screws.
Remove the two screws from device front plate. Loosen the securing-plate on mounting
frame.
Slide the device into the mounting.
Push the security-plate into the locking slot and tighten the securing-plate. Tighten the
device with the two screws from device front plate.
Dimensions see, "BD406 without Control Head" page 41, "BD406 without Control Head
with Mounting Kit MK4401" page 42.
Figure 10: BD406 without Control Head (front view)
Figure 11: MK4401
58
(2.283 in)
47.3
±0.2
(1.862
±0.008
)
47.3
±0.2
(1.862
±0.008
)
Ø 3.5
(Ø 0.138)

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