A
A
B
B
C
C
D
D
E
E
4
4
3
3
2
2
1
1
26VAC 400HZ MAIN INVERTER
26VAC 400HZ SECONDARY INVERTER
Title
Size
Document Number
Rev
Create:
Sheet of
Category
Mod:
Sunday, May 03, 1998
D
POWER AND INVERTER
Vista, Ca.
B
1
29
SN3500 INSTALLATION DRAWING
Wednesday, July 23, 2008
Title
Size
Document Number
Rev
Create:
Sheet of
Category
Mod:
Sunday, May 03, 1998
D
POWER AND INVERTER
Vista, Ca.
B
1
29
SN3500 INSTALLATION DRAWING
Wednesday, July 23, 2008
Title
Size
Document Number
Rev
Create:
Sheet of
Category
Mod:
Sunday, May 03, 1998
D
POWER AND INVERTER
Vista, Ca.
B
1
29
SN3500 INSTALLATION DRAWING
Wednesday, July 23, 2008
P3
16 400HZ REF
NOTE 1
1
9
5 AMP
14/28 VDC AVIONICS BUS
ACFT GROUND
3
11
ACFT POWER
ACFT POWER
POWER GROUND
POWER GROUND
P1
COMMENTS
DATE
INITIAL RELEASE
A
REV
SANDEL SN3500
82005-10
16 400HZ REF
P2
NOTE 2
NOTE 3
NOTES:
1. USE 20AWG WIRE. BOTH GROUNDS AND BOTH POWER LEADS
REQUIRED.
2. INVERTER 1 ONLY REQUIRED IF XYZ GYRO OR XYZ ADF ARE
CONNECTED TO P1, OR IF BOOTSTRAP SYNCHRO OUTPUT IS
CONNECTED, OR IF AUTOPILOT USES AC COURSE AND HEADING
DATUM AND CRS/HDG EXTERNAL EXCITATION (P2-10) IS NOT USED.
3. INVERTER 2 ONLY REQUIRED IF XYZ ADF IS USED CONNECTED
TO P2.
4. INSTALLATIONS IN 14 VOLT AIRCRAFT REQUIRE SN3500 SERIAL
NUMBER 5-2500 OR HIGHER. SN3500 SERIAL NUMBERS LOWER
THAN 5-2500 AND INSTALLED IN 14 VOLT AIRCRAFT REQUIRE A 14V
TO 28V CONVERTER. CONTACT SANDEL FOR COMPATABLE
MODELS.
C
A/R 806 NEW PAGE NUMBER. ADDED INVERTER 2.
CORRECTED NOTE 2.
COMPUTER CONTROLLED DRAWING
DO NOT REVISE MANUALLY
SN3500 input power requires 11 to 33 VDC.
See Note 4.
C1
A/R 824 ADDED ADDITIONAL TEXT TO EMPHASIZE
POWER REQUIREMENTS.
MODIFIED NOTE 2 TO INCLUDE CLARIFICATION
FOR AUTOPILOT CONNECTION.
JAN 12, 2006
D
JUL 18, 2008
UPDATED FOR 14 VOLT AIRCRAFT AND
NOTE 4. AR 1023
Summary of Contents for SN3500
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