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TAKE-OFF DATATA K E-O FF DISTANCE FR OM HA RD SURFA CE RU NW A Y W ITH FL A PS U P

AT SEA LEVEL & 59'F AT 2500 FT. & 50'F AT 5000 FT. & 41F AT 7500 FT. & 32'F

GROSS lAS HEAD TOTAL TOTAL TOTAL TOTALWEIGHT AT 50' WIND GROUND TO CLEAR GROUND TO CLEAR GROUND TO CLEAR GROUND TO CLEARPOUNDS MPH KNOTS RUN 50 FT OBS RUN 50 FT OBS RUN 50 FT OBS RUN 50 FT OBS

0 865 1525 1040 1910 1255 2480 1565 3855!'2300 68 10 615 1170 '750 .1485 920 1955 1160 3110

20 405 850 505 1100 630 1480 810 2425

0 630 1095 755 1325 905 1625 1120 21552000 63 10 435 820 530 1005 645 1250 810 1685

20 275 580 340 720 425 910 595 1255

0 435 780 520 920 625 1095 765 1370

1700 58 10 290 570 355 680 430 820 535 1040

20 175 385 215 470 270 575 345 745

NOTES: 1. Increase distance 10% for each 25'F above standard temperature for particular altitude.

2. 'For operation ona dry, grass runway, increase distances (both "ground run" and "total to clear

50 ft. obstacle") by 7% of the "total to clear 50 ft. obstacle" figure.

MAXIMUM RATE-OF-CLIMB DATA

AT SEA LEVEL & 59'F AT 5000 FT. & 41F AT 10,000 FT. & 23F AT 15,000 FT. & 5F

GROSS RATE OF GAL. RATE OF FROM RATE OF FROM RATE OF FROM

WEIGHT !AS CLIMB OF EUEL lAS CLIMB S.L.

lAS CLIMB S.L.

IAS CLIMB S.L.

FUEL FUEL FUELPOUNDS MPH FT/MIN USED MPH FT/MIN USED MPH FT/MIN USED MPH FT/MIN USED

2300 91 645 1.0 85 435 2.6 80 230 4.8 73 20 11.5

2000 88 840 1.0 81 610 2.2 75 380 3.6 68 155 6.3

1700 83 1085 1.0 77 825 1.9 70 570 2.9 64 315 4.4

NOTES: 1. Flaps up, full throttle, mixture leaned for smooth operation above 3000 ft./ 2. Fuel used includes warm up and take-off allowance.

3. For hot weather, decrease rate of climb 20 ft./min. for each 10F above standard daytemperature for particular altitude.

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CRUISE Gross Weight- 2300 Lbs.

PERFORMANCE Standard Conditions

Zero Wind Lean Mixture

SKYHAWK

NOTE: Maximum cruise is normally limited to 75% power. Cruise speeds lor the

standard Model 172 are 1 to 3 MPH lower than shown with the maximumdifference occurring at higher powers.

38 GAL (NO RESERVE) 48 GAL (NO RESERVE)

TAS GALl ENDR. RANGE ENDR. RANGE

ALTITUDE RPM % BHP MPH HOUR HOURS MILES HOURS MILES

2500 2700 8 7 139 9.6 3.9 545 5.0 69 02600 78 133 8. 6 4. 4 59 0 5.6 74 52500 70 12 8 7.7 4. 9 63 0 6. 2 79 52400 63 12 2 7.1 5.3 655 6. 7 82 52300 57 11 6 6.6 5. 7 66 5 7.2 84 0

2200 51 10 9 6.2 6. 1 66 5 7.7 84 0

5000 2700 81 13 8 8.9 4. 3 585 5. 4 740

2600 7 3 133 8.1 4. 7 630 6.0 79 5

2500 66 128 7. 4 5. 1 65 5 6.5 83 0

2400 60 12 1 6.8 5. 6 675 7.0 85 0

2300 54 11 4 6. 4 5.9 675 7. 5 85 5

2200 48 107 6.0 6.3 675 8. 0 85 0

7500 2700 76 13 8 8. 4 4. 5 63 0 5. 7 79 5

2600 69 133 7. 6 5. 0 66 0 6.3 8352500 63 126 7.1 5. 4 67 5 6. 8 8552400 57 11 9 6. 6 5.8 685 7.3 86 5

2300 5 1 112 6. 2 6. 1 68 5 7. 8 865

10 ,0 00 2700 72 138 7.9 4. 8 66 5 6.1 8402600 66 13 1 7.3 5.2 685 6.6 86 02500 59 124 6.8 5.6 69 5 7. 1 87 52400 54 11 7 6.4 6. 0 700 7.5 88 02300 48 110 6.0 6. 3 700 8. 0 88 0

12 ,5 00 2650 65 132 7.2 5.3 695 6. 6 88 02500 56 122 6.5 5.8 710 7. 3 89 52400 51 115 6.2 6. 2 710 7. 8 89 5

. ,

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LANDING DATALANDING DISTANCE ON HARD SURFACE RUNWAY

NO WIND - 40 FLAPS - POWER OFF

GROSS AP PROA CHAT SEA LEVEl & 59F AT 2500 FT. & 50F AT 5000 FT. & 41F AT 7500 FT. & 32F

WEIGHT JASGROUND T OTAL GROUND TOTAL GROUND TOTAL GROUND TOTAL

LBS. MPH

ROLL TO CLEAR ROll TO CLEAR ROll TO CLEAR ROll TO CLEAR50' OBS. 50' OBS. 50' 085. 50' OBS.

2300 70 520 1250 560 1310 605 1385 650 1455

NOTES: l. Reduce landing distance 10%for each 5knotheadwind.2. For operationon adry, grass runway, increase distances (both"ground roll" and "total to clear 50ft.

."" ' " obstacle") by 20%ofthe "total to clear 50 ft. obstacle" figure.

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SPEED 80 MPH (IAS)

PROPELLER WINDMILLING

FL APS UP ZERO WIND

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Cruise, 75%Power at 8000 it

48 Gallons, No Reserve

M odel 172* S kyhawk *

2300 lbs 2300 lbs

140 mph 144 mph

135 mph 138 mph

635 mi 650 mi

4.7 hrs 4.7 hrs

135 mph 138 mph

.795 mi 815 mi

5.9 hrs 5.9 hrs

135 mph 138 mph

.695 mi 700 mi

6.0 hrs 6.0 hrs

116 mph 117 mph

870 mi 875 mi

7.5 hrs 7.5 hrs116 mph 117 mph

645 fpm 645 fpm

13,100 ft 13, 100 it

865 it 865 ft

1525 ft 1525 ft

520 ft 520ft

1250 ft 1250 ft

57 mph 57 mph.49 mph 49 mph

1300 Ibs 1345 lbs

1000lbs 955 1bs

120 lbs 120Ibs

13.2 13.2

15.3 15.3

42 gal. 42 gal.

52gal. 52 gal.

8 qts 8 qts

75 inches 75 inches

.O-320-E2D 0-320-E2D

GROSS WEIGHT

SPEED:

Top Speed at Sea Level .

Cruise, 75%Power at 8000 ftRANGE:

Cruise, 75%Power at 8000 ft

38 Gallons, No Reserve

Maximum Range at 10,000 ft

38 Gallons, No Reserve

Maximum Range at 10,000 ft

48 Gallons, No Reserve

RATE OF CLIMB AT SEA LEVEL

SERVICE CEILING. .....

TAKE-OFF:

Ground Run . .

Total Distance Over 50-Foot Obstacle

LANDING:

Ground Roll . . . . . . . . . . . .

Total Distance Over 50-Foot Obstacle

STALL SPEED:

Flaps Up, Power Off . . .Flaps Down, Power Off . .

EMPTY WEIGHT (Approximate)

USEFUL LOAD (Approximate) .

BAGGAGE. . . . . . . . . .

WING LOADING: Pounds/Sq Foot

POWER LOADING: Pounds/HP

FUEL CAPACITY: Total

Standard Tanks. . . . . .

Optional Long Range Tanks

OIL CAPACITY: Total . . . .

PROPELLER: Fixed Pitch, Diameter.

ENGINE:

Lycoming Engine. . . . . .

150rated HP at 2700 RPM

tl -T h is m anua l covers opera tion o f th e M ode l 172/S kyhaw k w h ich is cer!ifica ted

as M ode l 172M under FA A Type C ertifi ca te N o.3A 12. The m anua l a lso covers

opera tion o f the R e im s/C essna F172 S kyhaw k w h ich is cert ifi ca ted as M ode l

F 1 72M under F rench Type C erti fi ca te N o. 25 and FA A T yp e C ertific ate N o. A 4E U .COPYRIGHT 1985

Cessna Aircraft Company

Wichita, Kansas USA