n374ma c-172s cessna weight & balance - ram aviation

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N374MA C-172S CESSNA WEIGHT & BALANCE RAM Tomahawk Weight and Balance Rev. 009 Effective: 01.05.17 1 Max Gross Weight: 2550.00 LBS Useful Load: 856.34 LBS Basic Empty Weight (N374MA 01/05/17): 1693.66 LBS Useable Fuel: 53 GAL (318 LBS) Total Fuel: 56 GAL Weight x Arm = Moment (divide by 1000 for smaller numbers) Moment divided by Weight = Center of Gravity x 1000 = C.G. Weight and Balance Example: WEIGHT X ARM = MOMENT/1000 1693.66 360 170 5 Basic Empty Weight Pilot and Passenger Rear Passengers Baggage Area Fuel 318 X X X X X 39.58 37.0 73.0 95.0 48.0 = = = = = 67.04 13.32 12.41 .48 15.26 Ramp Weight/Mom 2546.66 108.51 Taxi/Run-Up Takeoff Weight En-route Fuel Burn Takeoff C.G. Landing Weight Landing C.G. -1.5 2545.16 42.61 -96.0 2449.16 42.39 X 48.0 = -0.072 108.44 Refer to Section 6 of the POH X 48.0 = -4.61 103.83 Refer to Section 6 of the POH

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Page 1: N374MA C-172S CESSNA WEIGHT & BALANCE - RAM Aviation

N374MA C-172S CESSNA

WEIGHT & BALANCE

RAM Tomahawk Weight and Balance Rev. 009 Effective: 01.05.17 1

Max Gross Weight: 2550.00 LBS

Useful Load: 856.34 LBS

Basic Empty Weight (N374MA 01/05/17): 1693.66 LBS

Useable Fuel: 53 GAL (318 LBS) Total Fuel: 56 GAL

Weight x Arm = Moment (divide by 1000 for smaller numbers)

Moment divided by Weight = Center of Gravity x 1000 = C.G.

Weight and Balance Example:

WEIGHT X ARM = MOMENT/1000

1693.66

360

170

5

Basic Empty Weight

Pilot and Passenger

Rear Passengers

Baggage Area

Fuel 318

X

X

X

X

X

39.58

37.0

73.0

95.0

48.0

=

=

=

=

=

67.04

13.32

12.41

.48

15.26

Ramp Weight/Mom 2546.66 108.51

Taxi/Run-Up

Takeoff Weight

En-route Fuel Burn

Takeoff C.G.

Landing Weight

Landing C.G.

-1.5

2545.16

42.61

-96.0

2449.16

42.39

X 48.0 = -0.072

108.44

Refer to Section 6 of the POH

X 48.0 = -4.61

103.83

Refer to Section 6 of the POH

Page 2: N374MA C-172S CESSNA WEIGHT & BALANCE - RAM Aviation

N374MA C-172S CESSNA

WEIGHT & BALANCE

RAM Tomahawk Weight and Balance Rev. 009 Effective: 01.05.17 2

AT Sea Level, 10kts Headwind: Ground Run – 995’ Over 50’ Obstacle – 1690’

Take Off Distance (Ground Run): ________________________

Take Off Distance (Over 50’ Obstacle): ___________________

Vy: 74 KIAS Vx: 62 KIAS

Landing Distance (Normal): ____________________________

Landing Distance (Over 50’ Obstacle): ___________________

AT Sea Level, 10kts Headwind: Landing Distance – 585’ Over 50 Obstacle – 1350’

WEIGHT X ARM = MOMENT/1000

1693.66

Basic Empty Weight

Pilot and Passenger

Rear Passengers

Baggage Area

Fuel

X

X

X

X

X

39.58

37.0

73.0

95.0

48.0

=

=

=

=

=

67.04

Ramp Weight/Mom

Taxi/Run-Up

Takeoff Weight

En-route Fuel Burn

Takeoff C.G.

Landing Weight

Landing C.G.

-1.5

-

X 48.0 = -4.61

Refer to Section 6 of the POH

X 48.0 = -

Refer to Section 6 of the POH

Page 3: N374MA C-172S CESSNA WEIGHT & BALANCE - RAM Aviation

N374MA C-172S CESSNA

WEIGHT & BALANCE

RAM Tomahawk Weight and Balance Rev. 009 Effective: 01.05.17 3

C.G. Envelope: Range – 35.0 Fwd to 47.3 Aft

Page 4: N374MA C-172S CESSNA WEIGHT & BALANCE - RAM Aviation

N374MA C-172S CESSNA

WEIGHT & BALANCE

RAM Tomahawk Weight and Balance Rev. 009 Effective: 01.05.17 4

Cessna 172SP Profile (KTS):

Compass Card:

SPEED GAL/Hr LBS/Hr RATE

74

120

125

CLIMB

CRUISE

DESCENT

15.0

10.0

8.0

90.0

60.0

48.0

500 FPM

0

500 FPM

CLIMB After 1000’ 85 13.0 78.0 500 FPM