Cessna 172R User Manual

SECTION
9
-
SUPPLEMENTS
SUPPLEMENT
19
-
FAA
APPROVED
CESSNA
MODEL
172R
SUPPLEMENT
19
BENDIX/KING
KLN
94
GLOBAL
POSITIONING SYSTEM
(IFR)
The
following
Log
of Effective
Pages
provides
the
date
of
issue
for
original
and
revised
pages,
as
well
as
a
listing
of
all
pages
in
the
Supplement.
Pages
which
are
affected
by
the
current
revision
will
carry
the date
of
that
revision
Revision Level
Date
of
Issue
0
(Original)
1
2
3
November
6,
2000
December
18,
2000
December
30,
2000
January
22,
2001
LOG
OF EFFECTIVITY
PAGES
PAGE
DATE
PAGE
DATE
Title
(S19-1)
Jan
22/01
S19-11
Dec
30/00
S19-2
Jan
22/01
S19-12
Jan
22/01
S19-3
Nov
6/00
S19-13
Jan
22/01
S19-4
Dec
30/00
S19-14
Jan
22/01
S19-5
Dec
30/00
S19-15
Dec
30/00
S19-6
Nov
6/00
S19-16
Dec
30/00
S19-7
Jan
22/01
S19-17
Dec
30/00
S19-8
Jan.
22/01
S19-18
Dec
30/00
S19-9
Jan
22/01
S19-19
Dec
30/00
S19-10
Dec
30/00
S19-20
Dec
30/00
FAA
APPROVAL
FAA
APPROVE)
UNOCR
FAR
21
5UOWTJ
___
VwOtrnm
Aimft
Co.
OatqafenOpaonAuftortaaonDOMOOt&ce
Date:
January
23,
2001
S19-2
Jan
22/01

Cessna 172R Specifications

General

Manufacturer	Cessna
Model	172R
Engine	Lycoming IO-360-L2A
Horsepower	160 hp
Cruise Speed	124 knots (143 mph, 230 km/h)
Service Ceiling	13, 500 ft (4, 100 m)
Wingspan	36 ft 1 in (11.0 m)
Empty Weight	1, 691 lb (767 kg)
Max Takeoff Weight	2, 450 lb (1, 111 kg)
Seating Capacity	4
Takeoff Distance	1, 630 ft (497 m)
Type	Single-engine, high-wing
Range	696 nm (801 mi, 1, 289 km)
Rate of Climb	720 ft/min (3.7 m/s)
Length	27 ft 2 in (8.28 m)
Height	8 ft 11 in (2.72 m)
Fuel Capacity	56 US gal (212 L)
Stall Speed (Flaps Down)	47 knots
Landing Distance	1, 335 feet