MAXIMUM GROSS WEIGHT | 1370 lbs. |

MINIMUM GROSS WEIGHT | 920 lbs. |

MAXIMUM PER SEAT INCLUDING BAGS | 240 lbs. |

MAXIMUM IN EITHER BAGGAGE COMPARTMENT | 50 lbs. |

MINIMUM SOLO PILOT WEIGHT | 135 lbs. |

R22

1. Find Basic Empty Weight from A/C data

2. Fill in weight of passengers and baggage

3. Total weight

4. Figure weight of fuel in each tank / ONE GALLON OF FUEL WEIGHS
6 LBS.

5. Total weight with fuel

6. Find arm of helicopter in A/C date (longitudinal CG)

7. Multiply Weight x Arm to find A/C moment (longitudinal moment in
A/C data)

8. Find arm of passengers and baggage in POH p. 6-6 (see note and compare
serial number in A/C data)

9. Multiply Weight x Arm to find moment of passengers and baggage

10. Total moments

11. Divide moment by weight to find CG zero fuel

12. Find arms of fuels in POH p. 6-6

13. Multiply Weights x Arms to find moment in fuels

14. Total moments

15. Divide total moment by total weight to find A/C CG full fuel

Lateral

16. Find lateral arm of helicopter from A/C data (lateral CG)

17. Multiply Weight x Arm to find A/C moment (lateral moment in A/C
data)

18. Find arms of right and left seats from POH p. 6-6

19. Multiply Weights x Arms to find moments of right and left seats

20. Total moments

21. Divide total moments by total weight to find A/C CG zero fuel

22. Find arms of fuels from POH p. 6-6

23. Multiply Weights x Arms to find moments of fuels

24. Total moments

25. Divide total moment by total weight to find A/C CG full fuel

26. Graph in POH p. 2-6.1

A/C = Aircraft

POH = Pilot's Operating Handbook

CG = Center of Gravity

Weight x Arm = Moment

Moment / Weight = CG

Basic Empty Weight includes oil and unusable fuel