Cirrus SR22T Airplane Maintenance Manual

CIRRUS AIRPLANE MAINTENANCE MANUAL MODELS SR22 AND SR22T
22-11
Page 17
Serials 22-0435 thru 22-1306 after SB 2X-22-03, 1307
& subs, 22T-0001 & subs with optional installation
EFFECTIVITY:
G. Flight Director System - Serials 22-0435 thru 22-1306 after SB 2X-22-03, 1307 & subs, 22T-0001
& subs with optional installation (See Figure 22-116)
(1) Removal - Flight Director Switch Assembly
(a) Set BAT 1, BAT 2, and AVIONICS switches to OFF positions.
(b) Pull ESSENTIAL and NON-ESSENTIAL AVIONICS circuit breakers.
(c) Serials w/ Avidyne Avionics: Remove MFD. (Refer to 31-60)
(d) Serials w/ Perspective Avionics: Remove MFD. (Refer to 31-60)
(e) Remove glareshield. (Refer to 25-10)
(f) Serials w/ Avidyne Avionics: Serials 22-Remove PFD. (Refer to 31-60)
(g) Serials w/ Perspective Avionics: Serials 22-Remove PFD. (Refer to 31-60)
Note: To facilitate reinstallation, label wiring to ensure connectors are reattached
with the correct switches.
(h) Rotate locking screws on back of switch assembly counter-clockwise to disconnect switch
assembly from connector. Repeat for other switch assembly.
Note: To facilitate reinstallation, label push button to ensure switches are reas-
sembled with the correct push button.
(i) Remove push button from switch assembly. Repeat for other switch assembly.
(j) Rotate locking screws inside front of switch assembly counter-clockwise to disassemble
mounting sleeve, spacers, and seals from switch assembly. Repeat for other switch
assembly.
(2) Installation - Flight Director Switch Assembly
(a) Orient switch assembly so section labeled “TOP” is facing up and insert switch assembly
through lower section of instrument panel cut-out. Repeat for other switch assembly
through upper section of instrument panel cut-out.
Note: It may be necessary to discard one seal and spacer if attaching parts secur-
ing switch to instrument panel are too tight for cam engagement.
(b) Slide seals, spacers, and mounting sleeve onto switch assembly. Repeat for other switch
assembly.
(c) Position switches so that switch flanges are aligned with each other and installation area.
(d) Secure switch to instrument panel by rotating locking screws inside front of switch assem-
bly clockwise. Torque to 8 - 12 oz-in (576 - 864 gm-cm). Repeat on other switch assembly.
(e) Install push buttons to front of switch assemblies.
(f) Connect wiring harness connectors to switch assemblies.
(g) Secure switch to connector by rotating locking screws on back of connector assembly
clockwise. Torque to 8 - 12 oz-in (576 - 864 gm-cm). Repeat on other switch assembly.
(h) Serials w/ Avidyne Avionics: Install PFD. (Refer to 31-60)
(i) Serials w/ Perspective Avionics: Install PFD. (Refer to 31-60)
(j) Install glareshield. (Refer to 25-10)
(k) Serials w/ Avidyne Avionics: Install MFD. (Refer to 31-60)
(l) Serials w/ Perspective Avionics: Install MFD. (Refer to 31-60)
(m) Reset ESSENTIAL and NON-ESSENTIAL AVIONICS circuit breakers.
(n) Serials w/ Avidyne Avionics: Perform Operational Test - Flight Director (Avidyne). (Refer to
22-11)
(o) Serials w/ Perspective Avionics: Perform Operational Test - Flight Director (Perspective
Avionics and System 55X). (Refer to 22-11)
15 Jun 2010

Cirrus SR22T Specifications

General

Manufacturer	Cirrus Aircraft
Engine	Continental TSIO-550-K
Horsepower	315 hp
Max Takeoff Weight	3, 600 lbs
Service Ceiling	25, 000 ft
Cabin Width	49 in
Cabin Height	50 in
Seating Capacity	4
Avionics	Cirrus Perspective+ by Garmin
Category	Single-engine piston aircraft
Propeller	Hartzell 3-blade composite
Wingspan	38 ft 4 in
Length	26 ft
Height	8 ft 11 in
Maximum Cruise Speed	213 KTAS
Fuel Capacity	92 gallons
Stall Speed	64 knots
Safety Features	Cirrus Airframe Parachute System (CAPS)
Cruise Speed	183 knots