CIRRUS DESIGN CAPS, Component Manual

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12128-001
95-01
Page 21 15 Sept 2002
(f) Install screws securing rocket cone to rocket motor igniter.
(4) Installation - CAPS Rocket Assembly
(a) Acquire necessary tools, equipment, and supplies.
(b) Ensure CAPS handle safety pin is installed.
(c) Record rocket serial number in airplane log book.
Note: To prevent rocket assembly from snagging on parachute, place cardboard
between rocket assembly and parachute during installation.
(d) Ensure firing pin actuator is rotated so threaded side of actuator is facing aft and screw
head attaching activation cable to firing pin actuator will be visible through rocket cone
inspection hole when installed.
(e) Insert cable loop into firing pin actuator slot on rocket motor igniter and using a magne-
tized screwdriver, install screw and washer to firing pin actuator slot.
WARNING: Activation of rocket igniter requires 25 lb (11.25 kg) pull force. The fol-
lowing verification is meant only to ensure firing pin capture. A very
slight pull force (0.25 lb (0.113 kg)) is all that is required to verify cap-
ture.
(f) Slightly pull cable projecting from rocket motor assembly base to verify firing pin capture.
(g) Screw cone adapter to rocket cone.
(h) Install access hole plug to rocket cone.
CAUTION: Do not overtighten nylon shear screws.
WARNING: Position rocket lanyard around top circumference of rocket motor
launch tube, NOT over top of launch tube. Failure to comply will abso-
lutely FAIL rocket deployment!
(i) Position rocket lanyard over rocket motor launch tube and install nylon shear screws.
(j) Position rocket motor assembly, shim, and backing plate to BH 222. Install bolts and wash-
ers.
(k) Verify activation cable is routed through shield slot and secured with cable grommet.
(l) Remove catch cloth from below rocket and parachute assembly.
(m) Install access panel CB7 to BH 222.
(n) Install BH 222 trim panel and carpet.
Description P/N or Spec. Supplier Purpose
CAPS Rocket Assembly Reference
Parts List Cirrus Design N/A
Cardboard 12” x 12” Any Source Facilitate Rocket
Removal