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[BLUEMAX INSTALLATION INSTRUCTIONS]

 

13

 

 

Document number 2456-05 Revision 3 

 

 

10.3

 

DAU G2 Aircraft 

a)

 

Remove MFD to gain access behind the instrument panel. 

b)

 

Locate P1426 and J1426. These will be directly behind the MFD. Disconnect 
P1426 and J4126 from each other and re-connect to the DAU harness p/n 4370-
2720. 

c)

 

If GPS data is to be connected to the BlueMAX module, locate connector pair 
P518/J518, disconnect, and remove the backshell from J518. Pin 9 in P518 
should be empty.  

d)

 

The adapter harness has a shielded wire attached terminated with a pre-
crimped female pin. Insert this pin into J518 in the pin 9 position. 

e)

 

 Replace the backshell on J518, securing all cables. Reconnect P518 and J518. 

f)

 

If GPS data is not to be connected, cap and stow the shielded cable, or remove 
from the BlueMAX connector. 

g)

 

Run the power wire in the DAU harness to the circuit breaker panel and 
terminate to the convenience power breaker currently labeled “12VDC 
OUTLET”. Relabel the breaker “12VDC OUTLET/BLUETOOTH”. 

h)

 

Plug the BlueMAX module into the other end of the adapter harness. 

i)

 

Secure the module and cabling to existing structure or wire bundles using cable 
ties. 

j)

 

Replace MFD IAW the Cirrus AMM. 

10.4

 

G3 Aircraft 

a)

 

Remove MFD to gain access behind the instrument panel. 

b)

 

Locate P1047 and J1047. These will be directly behind the MFD. Disconnect 
P1047 and J1047 from each other and re-connect to the G3 harness p/n 4370-
8434. 

c)

 

Run the power wire in the DAU harness to the circuit breaker panel and 
terminate to the convenience power breaker currently labeled “12VDC 
OUTLET”. Relabel the breaker “12VDC OUTLET/BLUETOOTH”. 

d)

 

Plug the BlueMAX module into the other end of the adapter harness. 

e)

 

Secure the module and cabling to existing structure or wire bundles using cable 
ties. 

f)

 

Replace MFD IAW the Cirrus AMM. 

11

 

Post install checks 

 

Power up the aircraft and verify that the analog instruments (if fitted) or the PFD 
display primary engine data. 

 

Verify that the MFD (if fitted) displays supplementary engine data. 

 

Using a BLE scanner verify that the BlueMAX module is advertising (the default 
device name is EMAX.) This confirms that the module is powered up. Pull the 
breaker supplying the module and confirm that it stops advertising. 

12

 

Weight and balance 

The installed weight of the BlueMAX adapter and harness is approximately 80g (less 
than 3 ounces) and results in a change in the CG position of approximately 0.008% MAC. 

Содержание BlueMAX

Страница 1: ...LUEMAX INSTALLATION INSTRUCTIONS i BlueMAX Bluetooth Adapter Installation Instructions Document no 2456 05 Date 2017 03 20 Revision 3 Approved Control J Pty Ltd 100 Hursley Rd Redbank NSW 2446 Austral...

Страница 2: ...ii BLUEMAX INSTALLATION INSTRUCTIONS Document number 2456 05 Revision 3 Copyright 2017 Control J Pty Ltd...

Страница 3: ...ION INSTRUCTIONS iii Document number 2456 05 Revision 3 iii Revision History Date Revision Document Changes 2017 02 17 1 Initial Draft 2017 02 22 2 Revised document list 2017 02 22 3 Placard CB Flight...

Страница 4: ...in SIU aircraft 9 6 3 Verify primary engine data on PFD for DAU aircraft 9 7 Installation with MFD permanently removed 10 8 Parts required 11 9 Tools required 11 9 1 Probing connector P1426B 11 10 In...

Страница 5: ...List of Tables Table 1 BlueMAX Technical specifications 7 Table 2 Referenced Documents 8 Table 3 Engine monitor types 10 Table 4 BlueMAX part numbers 11 List of Figures Figure 1 Analog engine instrum...

Страница 6: ...e in Cirrus SR22 and SR20 aircraft and these instructions relate specifically to those models 2 Definitions The following abbreviations and acronyms are used in this document BLE Bluetooth Low Energy...

Страница 7: ...hould be 20AWG which is rated to 7 5A per AC 43 13 1B 6 Preparation for installation 6 1 Aircraft identification Cirrus aircraft fitted with Perspective avionics are not eligible for BlueMAX installat...

Страница 8: ...IRPLANE WIRING MANUAL FOR THE CIRRUS SR20 12129 001 C5 2016 01 01 AIRPLANE MAINTENANCE MANUAL FOR THE CIRRUS SR20 12137 001 B7 2016 01 01 AIRPLANE MAINTENANCE MANUAL FOR THE CIRRUS SR22 AND SR22T 1377...

Страница 9: ...if those connectors are installed in accordance with the Cirrus Wiring Manual chapter 77 00 01 The necessary connectors can be ordered from Control J as part number 4370 9869 Figure 1 Analog engine i...

Страница 10: ...gine data displayed on PFD G1 G2 SR20 1005 1581 SIU SIU must be fitted G2 SR20 1582 1877 1879 1885 DAU G2 Verify primary engine data displayed on PFD G3 SR20 with Avidyne Avionics 1878 1886 subsequent...

Страница 11: ...ere may be cable ties wire splices and other common electrical parts required these are not included in the kit Installation type BlueMAX module Adapter Harness Connectors Kit SIU 4370 2730 4370 5146...

Страница 12: ...D977 22 running from the SIU to the MFD and install P719 and J719 in accordance with the Cirrus Wiring Manual c Disconnect P719 and J719 from each other and re connect to the SIU harness p n 4370 5146...

Страница 13: ...ing structure or wire bundles using cable ties j Replace MFD IAW the Cirrus AMM 10 4 G3 Aircraft a Remove MFD to gain access behind the instrument panel b Locate P1047 and J1047 These will be directly...

Страница 14: ...ons for continued airworthiness No routine maintenance or inspection of the BlueMAX module is required Correct display of primary and supplementary engine data should be monitored during normal operat...

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