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NOTICE
AT THE TIME OF ISSUANCE, THIS
INFORMATION MANUAL WAS AN EXACT
DUPLICATE OF THE OFFICIAL PILOT'S
OPERATING HANDBOOK AND FAA
APPROVED AIRPLANE FLIGHT MANUAL
AND IS TO BE USED FOR GENERAL
PURPOSES ONLY.
IT WILL NOT BE KEPT CURRENT AND,
THEREFORE, CANNOT BE USED AS A
SUBSTITUTE FOR THE OFFICIAL PILOT'S
OPERATING HANDBOOK AND FAA
APPROVED AIRPLANE FLIGHT MANUAL
INTENDED FOR OPERATION OF THE
AIRPLANE.
CESSNA AIRCRAFT COMPANY
ORIGINAL ISSUE - 2 DECEMBER 1996
Dec 2/96
i
PERFORMANCESPECIFICATIONS
CESSNA
MODEL 172R
PERFORMANCE - SPECIFICATIONS
* SPEED:
Maximum at Sea Level . . . . . . . . . . . . . . . . . . .
123 KNOTS
Cruise, 80% Power at 8000 FT
............
122 KNOTS
CRUISE:
Recommended lean mixture with fuel allowance for
engine start, taxi, takeoff, climb and 45 minutes
reserve.
80% Power at 8000 FT . . . . . . . . . . . . Range
580 NM
53 Gallons Usable Fuel
Time
4.8 HRS
Range at 10,000 FT, 60% power . . . . . Range
687 NM
53 Gallons Usable Fuel
Time
6.6 HRS
RATE OF CLIMB AT SEA LEVEL . . . . . . . . . . . . . . . . . 720 FPM
SERVICE CEILING . . . . . . . . . . . . . . . . . . . . . . . . . . .
13,500 FT
TAKEOFF PERFORMANCE:
Ground Roll . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
945 FT
Total Distance Over 50 FT Obstacle . . . . . . . . . . . . 1685 FT
LANDING PERFORMANCE:
Ground Roll . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
550 FT
Total Distance Over 50 FT Obstacle . . . . . . . . . . . . 1295 FT
STALL SPEED:
Flaps Up, Power Off . . . . . . . . . . . . . . . . . . . . . . .
51 KCAS
Flaps Down, Power Off . . . . . . . . . . . . . . . . . . . . .
47 KCAS
MAXIMUM WEIGHT:
Ramp . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
2457 LBS
Takeoff . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
2450 LBS
Landing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
2450 LBS
STANDARD EMPTY WEIGHT . . . . . . . . . . . . . . . . . . .
1639 LBS
MAXIMUM USEFUL LOAD . . . . . . . . . . . . . . . . . . . . . .
818 LBS
BAGGAGE ALLOWANCE . . . . . . . . . . . . . . . . . . . . . . .
120 LBS
ii
Feb 28/00
CESSNA
MODEL 172R
SECTION 1
GENERAL
PERFORMANCE-SPECIFICATIONS
(Continued)
WING LOADING: Lbs/Sq Ft . . . . . . . . . . . . . . . . . . . . . . . . .
14.1
POWER LOADING: Lbs/HP . . . . . . . . . . . . . . . . . . . . . . . . .
15.3
FUEL CAPACITY . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
56 GAL
OIL CAPACITY . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
8 QTS
ENGINE: Textron Lycoming . . . . . . . . . . . . . . . . . . . .
IO-360-L2A
160 BHP at 2400 RPM
PROPELLER: Fixed Pitch, Diameter . . . . . . . . . . . . . . . . .
75 IN.
* NOTE
Speed performance is shown for an airplane equipped with
optional speed fairings which increase the speeds by
approximately 2 knots. There is a corresponding difference
in range, while all other performance figures are unchanged
when speed fairings are installed.
The above performance figures are based on the indicated