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1400 4593
1600 5249
1800 5906
2000 6562
2200 7218
2400 7874
2600 8530
2800 9186
3000 9843
3200 10499
3400 11155
3600 11811
3800 12467
4000 13123
4200 13780
Original Issue: 01-20-09
P/N 13772-142 13 of 14
Cirrus Design Section 9
SR22 Supplements
Section 6 – Weight and Balance
No Change.
Section 7 – Airplane and Systems Description
No Change.
Section 8 – Handling, Service, & Maintenance
No Change.
Section 9 – Supplements
No Change.
Section 10 – Safety Information
No Change.
Original Issue: 01-20-09
14 of 14 P/N 13772-142
Section 9 Cirrus Design
Supplements SR22
Original Issue: 01-20-09
Intentionally Left Blank
P/N 28730-001 1 of 12
Cirrus Design Section 9
SR2X Supplements
System Description Supplement
for the
Cirrus Landing Gear Simulator System
Information in this System Description Supplement is Advisory Only,
and does not contain information prescribed in 14 Code of Federal
Regulations (CFR) Part 23.1581 through 23.1589. Therefore, this
supplement is not part of the FAA Approved Airplane Flight Manual.
Original Issue: 08-26-09
Cirrus Design Corporation
4515 Taylor Circle
Duluth, MN 55811
USA
2 of 12 P/N 28730-001
Section 9 Cirrus Design
Supplements SR2X
Section 1 - General
This document discusses system and operating information for the
Cirrus Landing Gear Simulator (CLGS). The simulator is designed to
be used in flight to facilitate training on the operation of retractable
landing gear systems. The intent of the system is to replicate the
appearance, style, and general function of a typical retractable landing
gear system. The CLGS can be manipulated in flight to simulate a
variety of possible system failures including incomplete gear
extension/retraction, indicator and control system failures, and the use
of emergency gear extension.
Section 2 - Limitations
Not Applicable.
Section 3 - Emergency Procedures
Not Applicable.
Section 3A - Abnormal Procedures
Not Applicable.
Section 4 - Normal Procedures
Not Applicable.
Section 5 - Performance
Not Applicable.
Section 6 - Weight and Balance
Not Applicable.
Original Issue: 08-26-09
P/N 28730-001 3 of 12
Cirrus Design Section 9
SR2X Supplements
Section 7 - System Description
This airplane is equipped with a Cirrus Landing Gear Simulator
designed to be used in flight to facilitate training on the operation of
typical retractable landing gear systems. The system consists of the
Pilot Interface Panel, Instructor Fault Select Panel, Warning Horn Push
Button, Logic Unit, Warning Horn, Circuit Breaker, and the necessary
Wiring and Connectors.
28 VDC for CLGS System operation is supplied through 2-amp circuit
breaker on MAIN BUS 3.
Pilot Interface Panel
The Pilot Interface Panel, located at the bottom of the center console
opposite to the Flap Control Switch, provides the pilot with the ability to
simulate operation of a retractable landing gear system. The panel is
backlit for night operations and contains a GEAR UP/DOWN Locking
Toggle Switch, three dimmable Light Emitting Diodes (LED), an
Emergency Extension push-button and a Lamp Test push-button.
To simulate prevention of accidental gear retraction, the GEAR UP/
DOWN Toggle Switch must be slightly pulled to release a lock prior to
pivoting the lever up or down to simulate gear operation. To facilitate
system identification the Toggle Switch knob is in the shape of a
wheel.
Three LEDs, labeled NOSE, LH, and RH, indicate gear position and
security. Red indicates the gear is in-transit. Green indicates the gear
is down and locked. No lights indicate the gear is up and locked.
The Emergency Extension push-button simulates a secondary method
of extending the landing gear. Pressing and holding the EMER EXT
push-button will turn all of the LED's Red until the EMER EXT pushbutton
has been held for a cumulative total of 5 seconds, at which time
the LED's illuminate Green.
The Lamp Test push-button provides for LED continuity testing. When
the LAMP TEST push-button is pressed and held, the LED's will
illuminate Red for 2±1 seconds and then illuminate Green until the
push-button is released.
Original Issue: 08-26-09
4 of 12 P/N 28730-001
Section 9 Cirrus Design
Supplements SR2X
Instructor Fault Selection Panel
The Instructor Fault Selection Panel, located out of the pilot’s view on
the RH mid-console trim panel, provides the instructor with the ability
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Cirrus Design SR20西锐20飞行员操作手册和飞机飞行手册附录(81)
