Cessna SkyHawk SP 172S NAV III 2005 Pilot Operating Handbook page 309

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AnlSafe, Inc.
Inflatable Restraints Division
1043 N. 47" Avenue
Phoenix,
AZ. 85043
Document
No.:
E508810
Revision: D
SECTION 3
EMERGENCY PROCEDURES
No Change
SECTION 4
NORMAL PROCEDURES
......
_-----_
....
_----_
....
_.
AFM Supplement for
AmSafe Aviation Inflatable Restraint
On
Cessna
172.182. and
206
STC SAOI700LA
To activate the system, Join (bUckle) the thrue-point restraint in the
same
manner
85
any other three-poinl
sealbell.
An
empty CO-pllot
or passenger seat restraint must not be buckled.
SECTION 5
PERFORMANCE
No Change
SECTION 6
WEIGHT AND BALANCE/EQUIPMENT UST
For complete information of the AA1R
V23
System effect on weighl and balance loading to the airplane, please
refer to AmSafe Aviation's, Weight and Balance Information Report. Document No. E508952.
In the summary that follows. Empty Weights and Moments are given for AAIR Systems with the current EMA,
PIN 508358-409 and the new, lighter-weight EMA, PIN 508358-421, useful for loading and Center of Gravity
caJculaUons. Those expressed in parentheses were calculated using the new, lighter EMA, PIN 508358-421.
Models 172R. 172S - with optional rear Hat bench AAIR System
Weioht-lbs
Arm-in
Moment-In Ibs
7.638
57.928
442.454
AA1R System Difference Added (EMA, PIN 508358-409)
(7.338)
(425.075)
AAlR System Difference Added (EMA, PIN 508358-421)
Models 172R. 172S - without optional [Jar Hat bench AAlR System
Welght-lbs
Arm-in
Moment-in. Ibs
3.848
45.397
174.686
AAlR System Difference Added (EMA, PIN 508358-409)
(3.698)
(167.871)
AAIR System Difference Added (EMA, PIN 508358-421)
Modols 1825, 18U l1eu - with rear seat bench AAtR System
Welght-!bs
Ann-In
Moment-In lbs
7.638
57.682
440.578
AAlR System Difference Added (EMA, PIN 508358-409)
(7.338)
(423.270)
AAlR System Difference Added (EMA, PIN 508358-421)
Models 1825, 1821.11821 - without rear Hat bench AAlR System
Weight-lbs
Arm-ln.
Moment"n lbs
3.848
41.798
160.838
AAlR System Difference Added (EMA, PIN 508358-409)
(3.698)
(154.569)
AAIR System Difference Added (EMA, PIN 508358-421)
Models 206" 1206" - with opttonal rear seat bench AAIB System
Welght-Ibs
Arm-In
Moment-In lbs
11.54
69.782
805.284
AAIR System Difference Added (EMA,
PIN
508358-409)
(11.090)
(773.882)
AAIR System Difference Added (EMA.
PIN
508358-421)
Models 208", 1208" - without optional
rear
seat bench AA1R System
Weioht-lbs
Arm-in.
Moment-in Ibs
7.75
53.852
417.350
AAlR System Difference Added (EMA, PIN 508358-409)
(7.450)
(401.197)
AAlR System Difference Added (EMA, PIN 508358-421)
FAA Approved 6-28-07
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