Pilots Operating Handbook Cessna 172.pdf

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P O H
THIS MANUAL IS INTENDED FOR
FLIGHT SIMULATION USE ONLY. NO
RESPONSIBILITY FOR TYPOGRAPHIC
OR OTHER ERRORS IS TAKEN.
CESSNA MODEL 172 P
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FOREWORD
FOREWORD
I would like to extend my compliments and thanks to Alex
Franzen, who expended a great deal of time and talent to
produce this manual, based on the actual C-172P POH, for
the DF2000 / FSD Cessna 172P.
It is an outstanding effort! This manual is intended for use
along with the detailed documentation originally provided
with our C-172P panel, and also makes reference to certain
features of our panel.
It is people such as Alex who make this hobby the great one
that it is, and we all hope you enjoy many happy hours
flying the 172, with this manual as your guide.
Happy Flying!
Louis J Betti
Executive Director - DreamFleet 2000
FLIGHT SIMULATION USE ONLY
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GENERAL INFORMATION
TOC
SECTION 1
TABLE OF CONTENTS
•Introduction
•Performance-Specifications
•Dimensions
•Descriptive Data
-Engine
-Propeller
-Fuel
-Oil
-Maximum Certificated Weight
-Standard Airplane Weight
1
1
2
3
3
3
3
3
4
4
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GENERAL INFORMATION
PAGE 1
INTRODUCTION
This handbook includes the
material required to be furnished
to the pilot by CAR Part 3.
Section 1 provides basic data and
information of general interest.
PERFORMANCE-SPECIFICATIONS
SPEED:
Maximum at sea level
Cruise, 75% power at 8000 ft
CRUISE: Recommended lean mixture with fuel allowance
for engine start, takeoff, climb and 45 minutes reserve
75% power at 8000 ft
40 gallons usable fuel
75% power at 8000 ft
50 gallons usable fuel
75% power at 8000 ft
62 gallons usable fuel
Maximum Range at 10000 ft
40 gallons usable fuel
Maximum Range at 10000 ft
50 gallons usable fuel
Maximum Range at 10000 ft
62 gallons usable fuel
RATE OF CLIMB AT SEA LEVEL
SERVICE CEILING
TAKEOFF PERFORMANCE
Ground Roll
Total Distance Over 50-ft Obstacle
LANDING PERFORMANCE (KCAS)
Ground Roll
Total Distance Over 50-ft Obstacle
STALL SPEESDS (KCAS)
Flaps Up, Power Off
Flaps Down, Power Off
MAXIMUM WEIGHT
Ramp
Takeoff or Landing
STANDARD EMPTY WEIGHT
Skyhawk
Skyhawk II
MAXIMUM USEFUL LOAD
Skyhawk
Skyhawk II
BAGGAGE ALLOWANCE
WING LOADING: Pounds/Sq Ft
POWER LOADING: Pounds/HP
FUEL CAPACITY
Standard Tanks
Long Range Tanks
Integral Tanks
PROPELLER: Fixed Pitch, Diameter
123 Knots
120 Knots
NOTE:
The performance figures are
based on the indicated weights,
standard atmospheric conditions,
level, hard-surface, dry runways
and no wind. They are calculated
values derived from flight tests
conducted by the Cessna Aircraft
Company under carefully
documented conditions and will
vary with individual airplanes
and numerous factors affecting
flight performance.
440 NM
3.8 HRS
585 NM
5.0 HRS
755 NM
6.4 HRS
520 NM
5.6 HRS
680 NM
7.4 HRS
875 NM
9.4 HRS
700 FPM
13000 FT
890 FT
1625 FT
540 FT
1280 FT
51 Knots
46 Knots
2407 LBS
2400 LBS
1414 LBS
1440 LBS
993 LBS
967 LBS
120 LBS
13.8
15.0
43 GAL
54 GAL
68 GAL
75 IN
FLIGHT SIMULATION USE ONLY
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GENERAL INFORMATION
PAGE 2
DIMENSIONS
5‘-4.15‘‘
26‘-11‘‘
NOTES:
1. Wing span shown with strobe
lights installed.
2. Maximum height shown with
nose gear depressed, all tires
and nose strut properly
inflated and flashing beacon
installed
3. Proper ground clearance is
11 3/4‘‘
4. Wing area is 174 square feet
5. Minimum turning radius is
25‘-5 1/2‘‘
11‘-4‘‘
FLIGHT SIMULATION USE ONLY
36‘-0‘‘
75‘‘ max
8‘-4 1/2‘‘
8‘-9 1/2‘‘

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