Page 193 - Jupiter Product Guide 2025 Rev N
P. 193
Specifications
Installation
4.00in
101.6mm
A 0.065in
1.7mm
2.00in 50.8mm
A
SECTION A-A
0.31in 7.9mm
2.87in 0.37in 0.20in
72.9mm 9.4mm 5.1mm
4 x 0.14 3.7
1.31in 33.3mm 3.03in
77mm
2.33in
59.2mm
2.63 MAX 66.8 MAX 0.61in 15.5mm 1.48in 37.5mm 1.50in 38.1mm
1.31in 33.3mm
3.19in
81.1mm
5.37in
136.3mm 0.13in
5.75 MAX 3.3mm
146.1 MAX
Weight: 0.28 lb. [0.13 Kg] Max
© 2019 Jupiter Avionics Corporation
TM
1959 Kirschner Rd, Kelowna, BC V1Y 4N7
Tel: +1 778-478-2232 Toll-Free 1 855-478-2232
Printed in Canada www.jupiteravionics.com
UNLESS OTHERWISE SPECIFIED PREPARED TAT
DIMENSIONS ARE IN INCHES
ANGLES ARE IN DEGREES
TOLERANCES:
1 DEC PLACE: 0.1
2 DEC PLACE: 0.01 CHECKED TITLE
CENTER OF GRAVITY 3 DEC PLACE: 0.005 One Half 3 ATI Mounting Plate - 7 Dzus
ANGLES:
0.5 DEG
0.03in [0.8mm]
WEIGHT: 0.28 lbs [0.13 kg] MAX. APPROVED NCAGE CODE PART NO. SHEET
JA71-A17
1/1
L00N3
MATERIAL: N/A CONFIDENTIAL & PROPRIETARY DOC. NO.
TO JUPITER AVIONICS CORP.
FINISH: N/A DRAWING NOT TO SCALE JA71-A17 Rev A.SLDDRW
JUPITER AVIONICS TEMPLATE SOLIDWORKS PORTRAIT SIZEB REV B.DRWDOT