Cessna 172R User Manual

GARMIN
Ltd.
or
its subsidiaries
c/o
Garmin
International
1
200
E.
1
5
1
“
Street,
Olathe,
KS
66062
USA
AIRPLANE
FLIGHT
MANUAL SUPPLEMENT
or
SUPPLEMENTAL
AIRPLANE
FLIGHT
MANUAL
for
a
Garmin
400W
Series
Navigation
System
TabJcofCon
tents
SECTION
PAGE
Section
I.
GENERAL
4
1
.
1
Garmin
400W
Series GPS/WAAS
Nav
Com
4
1
.2
Operation
5
1
.3
Class
II
Oceanic,
Remote,
and other
Operations:
5
Section
2.
LIMITATIONS
6
2.1
Pilot's
Guide
6
2.2
System
Software:
6
2.3
Navigation
Database
7
2.4
Terrain Database
7
2.5
Navigation
8
2.6
Approaches
8
2.7
Autopilot
Coupling
9
2.8
Terrain
Display
9
2.9
VNAV
9
2.10
Weather
Display
9
2.11
Traffic
Display
10
Section
3.
EMERGENCY
PROCEDURES
1 1
3.
1
Emergency
Procedures
1
1
3.2
Abnormal
Procedures
1
1
Section
4.
NORMAL
PROCEDURES
13
4.1
Approaches
with
Vertical
Guidance
13
4.2
Approaches
without
Vertical
Guidance
14
For
additional information
on
LP
approaches
refer
to
the
400W
Series
unit
Pilot's
Guide.
14
4.3
Autopilot Operation
14
4.4
Coupling
the
Autopilot
during
approaches
14
4.5
WFDE
Prediction
Program
16
Section
5.
PERFORMANCE
16
Section
6.
WEIGHT
AND
BALANCE
16
Section
7.
SYSTEM DESCRIPTIONS
16
190-00356-03
Rev.
B
Page
3
of
16

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