C I R R U S
C O M P O N E N T M A I N T E N A N C E M A N U A L - C A P S
M O D E L S R 2 0
95-01-01
Page 57
Serials 2228 & subs
EFFECTIVITY:
Figure 95-01-0112
Rocket Assembly Wiring - Serials 2228 & subs (3 of 4)
LEGEND
1. Wiring Harness
2. Cable Tie
3. Cable Anchor
4. Igniter Switch
5. Rocket Shield
6. Standoff
7. Sleeving
8. Heatshrink
TR1456
(NEGATIVE)
1.0 ±0.5 inch
(2.54 ±1.27 mm)
TR1454
(POSITIVE)
NOTE
TR2705
TR2706
R2700
5
7
2
LH-SIDE VIEW
LOOKING RIGHT
P2701
2
3
2 PLC'S
2
7
6
7
2
3
6
1
5
A
4
TR2706
R2700
TR2705
FORWARD-SIDE VIEW
LOOKING AFT
1
P2701
2
3
2
3
2
3
8
2
7
3
A2
A2
A1
A1
Serials 2228 & subs.
SR20_CM95_3579A
Install anchors and cable ties to prepared surface on side of launch tube using adhesive.
Wrap wires with tape as required to ensure security hold under cable ties.
Secure R2700 and wires to anchor at back of rocket shield with cable tie.
Install TR2705 as shown with hardware provided. Orient linkage as shown and position
ring lug downward and towards front of aircraft.
At upper rocket shield, place one 3 inch section of sleeving over both wires and secure to inside of
rocket shield using cable tie and holes in shield. Ensure sleeving extends above rocket shield edge
1.0 ±0.5 inch (2.54 ±1.27 mm). Secure sleeving at ends with cable ties to prevent fraying.
Place 3 inch sections of sleeving on each wire. Position sleeving as shown and secure
both to standoff using cable tie. Secure sleeving at ends with cable ties to prevent fraying.
Cover terminal ring (TR2706) with heatshrink and stow.
6
7
5
3
2
1
4 May 2015
