Robinson R44 - General Weight and Balance

REVISED: 21 FEB 2014 6-1
ROBINSON
MODEL R44
SECTION 6
WEIGHT AND BALANCE
SECTION 6
WEIGHT AND BALANCE
GENERAL
The helicopter must be flown only within weight and
balance limits specified in Section 2. Loadings outside
these limits can result in insufficient control travel for safe
operation.
The center of gravity may be adjusted by adding removable
ballast (any appropriate item of mass) to any under-seat
baggage compartment. Recalculate weight and balance
after adding ballast, and verify ballast meets baggage
compartment limits given in Section 2.
Loaded helicopter weight and balance can be determined
using the method given under LOADING INSTRUCTIONS.
In accordance with FAA procedures, the detail weight
and balance data of this section are not subject to
FAA approval. The loading instructions of this section,
however, have been approved by the FAA as satisfying all
requirements for instructions on loading of the rotorcraft
within approved limits of weight and center of gravity and
on maintaining the loading within such limits.
CAUTION
Fuel burn causes CG to move forward during
flight. Always determine safe loading with empty
fuel as well as with takeoff fuel. Payload may be
limited by forward CG as fuel is burned.