曝光台 注意防骗
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and retain until further notice.
Purpose: This POH Temporary Revision adds Limitations
associated with the Garmin GTS 800 Series Traffic
Advisory System to the basic AFM/POH.
May 04, 2010
2 of 2 TPOH 10-03
TPOH Cirrus Design
POH Temporary Change SR22 / SR22T
Systems and Equipment Limits
Cirrus Perspective Integrated Avionics System
11. Use of the GTS 800 Series TRAFFIC ADVISORY SYSTEM (TAS)
to maneuver the airplane to avoid traffic is prohibited. The TAS is
intended for advisory use only. TAS is intended only to help the
pilot to visually locate traffic. It is the responsibility of the pilot to
see and maneuver to avoid traffic.
May 04, 2010
TPOH 10-05 1 of 2
Cirrus Design TPOH
SR20 POH Temporary Change
SR20 Airplane Flight Manual (AFM)
Temporary Change
Section 7 - Airplane and Systems Description
Nose Landing Gear
- See following page -
Affected Publication: SR20 POH 11934-003 thru Revision A9
SR20 POH 11934-004 thru Revision 1
Filing Instructions: Insert this temporary change in Section 7 - System
Description adjacent to the Landing Gear Section
and retain until further notice.
Purpose: This POH Temporary Revision adds system
description changes associated with Landing Gear
System to the basic AFM/POH.
Original Issue: 10-04-2010
2 of 2 TPOH 10-05
TPOH Cirrus Design
POH Temporary Change SR20
Landing Gear
Nose Gear
Serials 1005 thru 2064, 2065 & subs w/o Perspective Avionics:
The nose gear strut is of tubular steel construction and is attached to
the steel engine mount structure. The nose wheel is free castering and
can turn through an arc of approximately, Serials 1005 thru 1885, 216
degrees (108 degrees either side of center) or, Serials 1886 thru 2064,
170 degrees (85 degrees either side of center). Nose gear shock
absorption is provided by polymer shock absorbing pucks. Steering is
accomplished by differential application of individual main gear brakes.
The tube-type nosewheel tire measures 5.00 x 5.
Serials 2065 & subs w/ Perspective Avionics:
The nose gear strut is of tubular steel construction and is attached to
the steel engine mount structure. The nose wheel is free castering and
can turn through an arc of approximately 170 degrees (85 degrees
either side of center). Nose gear shock absorption is accomplished by
an oleo strut. Steering is accomplished by differential application of
individual main gear brakes. The tube-type nosewheel tire measures
5.00 x 5.
Original Issue: 10-04-2010
McCauley Propeller Systems
Warranty Policy Information And Procedures
Propellers, Governors & Components
McCauley Propeller Systems Standard Limited Warranty
McCauley Propeller Systems, a Division of Cessna Aircraft Company, Wichita, Kansas,
U.S.A., expressly warrants new products produced and sold by McCauley to be free from
defects in material and workmanship under normal use and service for a period of thirtysix
(36) months after delivery to the original retail purchaser or until the expiration of the
maximum hours of use or calendar limits for overhaul published by McCauley for the
subject product, whichever occurs first.
McCauley's obligation under this limited warranty is limited to repairing or replacing, at
its sole option, any propeller, propeller parts, governor or governor parts determined by
McCauley to have been defective. The repair or replacement of defective parts will be
made without charge to the owner for parts, or labor for removal and installation, except
export/import duties, and/or sales or use taxes, if any, which are solely the owner's
responsibility. McCauley will warrant a part replaced pursuant to this limited warranty
under the same terms as the original part for the remainder of the applicable warranty
period
of the original part. This limited warranty is not intended to and does not cover the costs
of normal maintenance or overhaul. In addition, McCauley will repair or replace, at its
option, any propeller, propeller parts, governor, or governor parts requiring replacement
due to manufacturing defect if found at or before the first recommended overhaul interval
as described in McCauley published service information. This first overhaul coverage
does not include labor, standard overhaul replacement parts, parts repairable via
published service information (re -plating, painting, etc.), other costs associated with the
propeller or governor overhaul, or export/import duties, and/or sales or use taxes, nor
does it apply to defects found after McCauley published overhaul hour or calendar limits.
The provisions of this limited warranty do not apply to: any McCauley parts which have
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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(139)
