曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

March 2010
7-36 Information Manual
Section 7 Cirrus Design
Airplane Description SR20
Landing Gear
Main Gear
The main landing gear are bolted to composite wing structure between
the wing spar and shear web. The landing gear struts are constructed
of composite material for fatigue resistance. The composite
construction is both rugged and maintenance free. The main wheels
and wheel pants are bolted to the struts. Each main gear wheel has a
15 x 6.00 x 6 tire with inner-tube installed. Standard wheel pants are
easily removable to provide access to tires and brakes. Access plugs
in the wheel pants can be removed to allow tire inflation and pressure
checking. Each main gear wheel is equipped with an independent,
hydraulically operated, single-disc type brake.
Nose Gear
The nose gear strut is of tubular steel construction and is attached to
the steel engine mount structure. The nosewheel is free castering and
can turn through an arc of approximately 216 degrees (108 degrees
either side of center). Steering is accomplished by differential
application of individual main gear brakes. The tube-type nosewheel
tire is 5.00 x 5.
Airplane Cabin
Cabin Doors
• Caution •
Serials 1423 and subsequent: The seat back must be in the fully
upright or the fully reclined position before closing the cabin door. Seat
backs in the forward or break-over position can cause damage to the
door handle or interior panel.
Two large forward hinged doors allow crew and passengers to enter
and exit the cabin. The door handles engage latching pins in the door
frame receptacles at the upper aft and lower aft door perimeter. Gas
charged struts provide assistance in opening the doors and hold the
doors open against gusts. Front seat armrests are integrated with the
doors. A key lock in each door provides security. The cabin door keys
also fit the baggage compartment door lock. Separate keys are
provided for the fuel caps.
March 2010
Information Manual 7-37
Cirrus Design Section 7
SR20 Airplane Description
CABIN SPEAKER
EGRESS HAMMER
(IN ARMREST)
OVERHEAD LIGHT AND SWITCH
FIRE EXTINGUISHER
TIEDOWN LOOPS
(6 PLACES, AFT BULKHEAD)
TIEDOWN LOOPS
(4 PLACES, BAGGAGE FLOOR)
STALL WARNING HORN
DEFROST AIR OUTLETS
DOOR HANDLE
OVERHEAD LIGHT AND SWITCH
PASSENGER FRESH
AIR OUTLET
(UNDER PILOT'S SEAT)
SR20_FM07_1064
(OVERHEAD)
CAPS ACTIVATION T-HANDLE
DETAIL A
A
Figure 7-8
Cabin Arrangement
March 2010
7-38 Information Manual
Section 7 Cirrus Design
Airplane Description SR20
Baggage Compartment
The baggage compartment door, located on the left side of the
fuselage aft of the wing, allows entry to the baggage compartment.
The baggage door is hinged on the forward edge and latched on the
rear edge. The door is locked from the outside with a key lock. The
baggage compartment key will also open the cabin doors.
The baggage compartment extends from behind the rear passenger
seat to the aft cabin bulkhead. The rear seats can be folded forward to
provide additional baggage area for long or bulky items.
Four baggage tie-down straps are provided to secure baggage and
other items loaded in the baggage compartment. Each strap assembly
has a hook at each end and a cam-lock buckle in the middle. The hook
ends clip over loop fittings installed in the baggage floor and in the aft
bulkhead. The tie-down straps should be stowed attached and
tightened to the fittings. If not adequately restrained, baggage
compartment items may pose a projectile hazard to cabin occupants in
the event of rapid deceleration. Secure all baggage items with tiedown
straps.
To install tie-down strap:
1. Position straps over baggage. Thread straps through luggage
handles if possible.
2. Clip hook ends of straps over loop fittings.
3. Grasp the buckle and pull the loose strap end of each strap to
tighten straps over contents of baggage compartment.
To loosen tie-down straps:
1. Lift buckle release and pull on buckle to loosen strap.
2. Lift hook ends free of loop fittings.
Seats
The seating arrangement consists of two individually adjustable seats
for the pilot and front seat passenger and two individual seats with fold
down seat backs for the rear seat passengers.
The front seats are adjustable fore and aft and the seat backs can be
reclined for passenger comfort or folded forward for rear seat access.
Integral headrests are provided. The fore and aft travel path is
March 2010
Information Manual 7-39
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：西銳20飛機信息手冊CIRRUS DESIGN SR20 AIRPLANE INFORMATION MA(62)