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Empty-Weight CG Range................................................5-4
Adverse-Loaded CG Checks............................................5-4
Forward Adverse-Loaded CG Check..........................5-5
Aft Adverse-Loaded CG Check...................................5-6
Ballast.........................................................................5-6
Temporary Ballast.......................................................5-6
Temporary Ballast Formula........................................5-6
Permanent Ballast.......................................................5-6
Chapter 6
Weight and Balance Control—Helicopters ................6-1
Determining the Loaded CG of a Helicopter...................6-2
Effects of Offloading Passengers and Using Fuel.......6-3
Chapter 7
Large Aircraft
Weight and Balance ......................................................7-1
Weighing Procedures.......................................................7-1
Determining the Empty Weight and EWCG....................7-1
Determining the Loaded CG of the Airplane
in Percent MAC...........................................................7-2
On Board Aircraft Weighing System...........................7-2
Determining the Correct Stabilizer Trim Setting.............7-4
Stabilizer Trim Setting in % MAC...............................7-4
Stabilizer Trim Setting in Units ANU
(Airplane Nose Up).....................................................7-4
Determining CG Changes Caused by
Modifying the Cargo........................................................7-4
Effects of Loading or Offloading Cargo.....................7-4
Effects of Onloading Cargo.............................................7-5
Effects of Shifting Cargo from
One Hold to Another...................................................7-6
Determining Cargo Pallet Loads with
Regard to Floor Loading Limits......................................7-7
Determining the Maximum Amount of Payload
That Can Be Carried........................................................7-8
Determining the Landing Weight.....................................7-8
Determining the Minutes of Fuel Dump Time...............7-10
Weight and Balance of Commuter
Category Airplanes........................................................7-11
Determining the Loaded Weight and CG..................7-15
Determining the Changes in CG When
Passengers are Shifted..............................................7-15
Determining Changes in Weight and CG
When the Airplane is Operated in
its Cargo Configuration............................................7-16
Determining the CG Shift When Cargo is Moved
From One Section to Another...................................7-16
Determining the CG Shift When Cargo is
Added or Removed....................................................7-17
Determining Which Limits are Exceeded.................7-17
Chapter 8
Use of Computers for Weight
and Balance Computations...........................................8-1
Using an Electronic Calculator to Solve
Weight and Balance Problems....................................8-1
Using an E6-B Flight Computer to Solve
Weight and Balance Problems....................................8-1
ix
Using a Dedicated Electronic Flight Computer to
Solve Weight and Balance Problems...............................8-3
Typical Weight and Balance Problems.......................8-3
Determining CG in Inches From the Datum....................8-3
Nose Wheel Airplane with Datum
Ahead of the Main Wheels..........................................8-3
Nose Wheel Airplane with Datum
Behind the Main Wheels.............................................8-4
Tail Wheel Airplane with Datum
Ahead of the Main Wheels..........................................8-4
Tail Wheel Airplane with Datum
Behind the Main Wheels.............................................8-4
Determining CG, Given
Weights and Arms............................................................8-4
Determining CG, given Weights
and Moment Indexes...................................................8-5
Determining CG in Percent of
Mean Aerodynamic Chord..........................................8-5
Determining Later CG
of a Helicopter............................................................8-5
Determining ΔCG caused by
Shifting Weights..........................................................8-6
Determining Weight Shifted to Cause
Specified ΔCG.............................................................8-6
Determining Distance Weight is Shifted to
Move CG a Specific Distance.....................................8-6
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Aircraft Weight and Balance Handbook(3)
