CIRRUS DESIGN CAPS, Руководство по компонентам

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12128-001
95-01
Page 15 15 Sept 2002
B. CAPS Cover (See Figure 95-016)
(1) Removal - CAPS Cover
(a) Acquire necessary tools, equipment, and supplies.
(b) Remove CAPS handle access cover and install CAPS handle safety pin.
(c) From aft edge of rear window and along airplane center line, measure 6.0 inches (15.2
cm) aft and mark the CAPS cover edge-seam location.
CAUTION: Exercise caution when sanding composite surface to prevent sanding into
laminate. Control dust migration.
(d) Using die grinder and disc, at CAPS cover edge-seam reference mark, sand in a 0.5 inch
(1.3 cm) area, and locate CAPS cover seam line. Sand around cover circumference follow-
ing seam line to reveal entire perimeter of cover.
WARNING: Use utmost care when working around embedded forward harness
straps and lightening protection mesh with sharp tools. Failure to fol-
low this WARNING could result in damage to CAPS system and failure
upon deployment.
Note: CAPS cover remnant may be used as an outline template to facilitate cover
installation. Avoid unnecessary damage to remnant cover during removal.
(e) Beginning at the aft, RH edge of cover seam line, carefully pry cover away from adhesive
using a small chisel. Avoid scratching or denting fuselage with chisel. Work edge back
until it is possible to slowly peel cover away from fuselage flange.
(f) Remove cover remnant from airplane.
(2) Installation - CAPS Cover (See Figure 95-015)
(a) Acquire necessary tools, equipment, and supplies.
Description P/N or Spec. Supplier Purpose
ScotchBrite Conditioning
Disc 840332 Standard Abrasives
Simi Valley, CA
(805) 520-5800 Composite
Removal.
Description P/N or Spec. Supplier Purpose
CAPS Cover Reference
Parts List Cirrus Design N/A
ScotchBrite Conditioning
Disc 840332 Standard Abrasives
Simi Valley, CA
(805) 520-5800 Composite
Removal
Foam Tape
1/8” x 1/4” 93675K11 McMaster-Carr
Atlanta, GA
(404) 346-7000 Cover Installation
Plastic Sheet - Any Source Cover Installation