12128-001
95-01
Page 11
15 Sept 2002
MAINTENANCE GUIDE
1.
GENERAL
Procedures and parts listed in this manual are reflective of Cirrus Design SR20 airplanes serial numbers
1195 and subsequent, SR22 airplanes serial numbers 0210 and subsequent, and all prior airplanes incor-
porating Service Bulletin SB 20-95-05 or SB 22-95-05 respectively.
WARNING:
CAPS must be serviced and maintained by Cirrus Design trained and authorized para-
chute system technicians only. Airframe and Powerplant license is not sufficient cre-
dentials for performing maintenance on CAPS.
Never activate CAPS on the ground. The rocket exits the fuselage with a velocity of
150 mph in the first tenth of a second and reaches full extension in 2.5 seconds. Peo-
ple near the airplane may be injured and extensive damage to the airframe will occur.
Ground activation will cause the airplane to be out of service until CAPS is replaced
and the airframe repaired and inspected.
Rocket ignition will occur at temperature above 500° F (260° C). In the event of ground
fire, use necessary precautions to avoid CAPS deployment.
FAA Type Certification for the airplane is contingent on a functional Cirrus Airframe
Parachute System (CAPS). The airplane may not be flown when CAPS is rendered
inoperative.
Note:
CAPS part identification and descriptions can be found in the Illustrated Parts List section of
this manual.
A. Servicing - Cirrus Airframe Parachute System (See Figure 95-015)
(1)
Removal - Pyrotechnic Line Cutters Replacement
(a)
Acquire necessary tools, equipment, and supplies.
(b)
Remove CAPS handle access cover and install CAPS handle safety pin
(c)
Remove bulkhead 222 (BH 222) trim panel and carpet.
(d)
Remove access panel CB7 from BH 222. (Refer to AMM 6-00)
(e)
To prevent debris and components from falling into bottom of empennage, place catch
cloth below rocket and parachute assembly.
(f)
Pull open flaps secured with hook and loop to gain access to line cutters.
(g)
Remove line cutter lanyard from D-ring and un-thread lanyard routed through line cutter’s
ignition loops.
WARNING:
When cutting nylon cord, ensure three-ring assembly stackup is not
altered.
(h)
Cut and remove nylon cord securing line cutters to link assembly.
(i)
Remove line cutters from airplane and safely discard.
Description
P/N or Spec.
Supplier
Purpose
Pyrotechnic Line Cutter
Replacement Kit
TBD
Cirrus Design
Replacment.
Summary of Contents for CAPS
Page 2: ......
Page 4: ......
Page 11: ...12128 001 95 01 Page 3 Figure 95 011 CAPS System and Deployment 15 Sept 2002 ...
Page 13: ...12128 001 95 01 Page 5 Figure 95 012 CAPS Handle and Ignition System 15 Sept 2002 ...
Page 15: ...12128 001 95 01 Page 7 Figure 95 013 Incremental Bridle and Deployment Bag 15 Sept 2002 ...
Page 17: ...12128 001 95 01 Page 9 Figure 95 014 Parachute Assembly and Line Cutters 15 Sept 2002 ...
Page 18: ...THIS PAGE INTENTIONALLY LEFT BLANK ...
Page 27: ...12128 001 95 01 Page 19 Figure 95 016 CAPS Cover Installation 15 Sept 2002 ...
Page 30: ...12128 001 95 01 Page 22 Figure 95 017 CAPS Rocket Assembly Sheet 1 of 2 15 Sept 2002 ...
Page 31: ...12128 001 95 01 Page 23 Figure 95 017 CAPS Rocket Assembly Sheet 2 of 2 15 Sept 2002 ...
Page 37: ...12128 001 95 01 Page 29 Figure 95 018 CAPS Activation System 15 Sept 2002 ...
Page 38: ...12128 001 95 01 Page 30 Figure 95 019 Sheet 1 of 2 CAPS Test Fixture 15 Sept 2002 ...
Page 39: ...12128 001 95 01 Page 31 Figure 95 019 Sheet 2 of 2 CAPS Test Fixture 15 Sept 2002 ...