CESSNA MODEL 172 P
D r e a m f l e e t 2000
井盖为啥是圆的
P O H
THIS MANUAL IS INTENDED FOR FLIGHT SIMULATION USE ONLY. NO RESPONSIBILITY FOR TYPOGRAPHIC OR OTHER ERRORS IS TAKEN.
FOREWORD
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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, bad on the actual C-172P POH, for the DF2000 / FSD Cessna 172P.
It is an outstanding effort! This manual is intended for u along with the detailed documentation orig
inally 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
SECTION 1
TABLE OF CONTENTS
•Introduction
•Performance-Specifications •Dimensions
•Descriptive Data
-Engine -Propeller -Fuel -Oil
-Maximum Certificated Weight -Standard Airplane Weight
1123333344
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TOC
INTRODUCTION
This handbook includes the material required to be furnished
to the pilot by CAR Part 3.Section 1 provides basic data and至强e3
information of general interest.
PERFORMANCE-SPECIFICATIONS
SPEED:
Maximum at a level
Crui, 75% power at 8000 ft
CRUISE: Recommended lean mixture with fuel allowance for engine start, takeoff, climb and 45 minutes rerve
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
有关书籍的名言
Ground Roll
Total Distance Over 50-ft Obstacle
LANDING PERFORMANCE (KCAS)
Ground Roll
Total Distance Over 50-ft Obstacle
STALL SPEESDS (KCAS)泡姜
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
宁波罗蒙
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 13.815.043 GAL 54 GAL 68 GAL 75 IN
NOTE:
The performance figures are bad 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.
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DIMENSIONS
75‘‘ max
NOTES:
1. Wing span shown with strobe lights installed.
2. Maximum height shown with no gear depresd, all tires and no 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‘‘
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