Ppl - Eqc C172m
.
- 1.Maximum gross weight
- A.
2350 lbs
- B.
2300 lbs
- C.
2400 lbs
- 2.Maximum useful weight
- A.
995 lbs
- B.
965 lbs
- C.
950 lbs
- D.
925 lbs
- 3.Standard empty weight
- A.
1375 lbs
- B.
1335 lbs
- C.
1350 lbs
- D.
1305 lbs
- 4.Maximum baggage capacity
- A.
120 lbs
- B.
132 lbs
- C.
155 lbs
- 5.Propeller diameter
- A.
65 inches (maximum)
- B.
75 inches (maximum)
- C.
85 inches (maximum)
- 6.Take off performance - Ground roll
- A.
965 ft
- B.
865 ft
- C.
895 ft
- 7.Take off performance - Ground roll to clear 50 ft obstacle
- A.
1525 ft
- B.
1635 ft
- C.
1725 ft
- 8.Landing Performance - Ground Roll
- A.
420 ft
- B.
380 ft
- C.
520 ft
- 9.Landing Performance - Total distance to clear 50 ft obstacle
- A.
1250 ft
- B.
1350 ft
- C.
1450 ft
- 10.Fuel capacity - Standard Tanks
- A.
40 gal
- B.
42 gal
- C.
45 gal
- 11.Fuel Capacity - Optional Longrange tanks
- A.
50 gal
- B.
52 gal
- C.
55 gal
- 12.Standard total usable fuel
- A.
38 gal
- B.
35 gal
- C.
42 gal
- 13.Maximum distance with 38 gallons - At 8000 ft altitude
- A.
835 statute miles
- B.
735 statute miles
- C.
635 statute miles
- 14.Maximum distance with 38 gallons - At 10,000 ft altitude
- A.
695 statute miles
- B.
595 statute miles
- C.
795 statute miles
- 15.Wing load
- A.
13.2 lbs/sq.ft
- B.
15.2 lbs/sq.ft
- C.
17.2 lbs/sq.ft
- 16.Wing span
- A.
38 ft
- B.
33 ft
- C.
36 ft
- 17.Rate of climb at sea level
- A.
645 ft/min
- B.
605 ft/min
- C.
675 ft/min
- 18.Service ceiling of C172M
- A.
13,100 ft
- B.
13,000 ft
- C.
13,300 ft
- 19.Maximum engine speed
- A.
2700 RPM
- B.
3700 RPM
- C.
2500 RPM
- 20.Stall speed, flaps up, power off
- A.
47 kts
- B.
57 kts
- C.
67 kts
- 21.Normal operating range at 5000 ft
- A.
3200 to 3600 RPM
- B.
1200 to 2600 RPM
- C.
2200 to 2600 RPM
- 22.Use of flaps 10
- A.
Shorten ground run by 10%
- B.
Shorten ground run by 15%
- C.
Shorten ground run by 20%
- 23.Steep climb angle
- A.
48 kts, flaps retracted (takeoff obstacle)
- B.
68 kts, flaps retracted (takeoff obstacle)
- C.
58 kts, flaps retracted (takeoff obstacle)
- 24.Short field landing
- A.
69 kts, flaps 20
- B.
59 kts, flaps 40
- C.
79 kts, flaps 10
- 25.Emergency landing without engine power
- A.
60-70 kts (flaps up), 55-65 kts (flaps down)
- B.
50-60 kts (flaps up), 55-65 kts (flaps down)
- C.
70-80 kts (flaps up), 65-75 kts (flaps down)
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