FAA-H-8083-25C · Source PDF page 252

Weight and Balance

Determining Loaded Weight and CG · PHAK page 10-8

Original FAA PHAK page 10-8
Faithful view of source page 10-8. Select it to enlarge.

Searchable transcription

Load Moment/1,000 (kilogram-millimeters) 0 50 100 150 200 250 300 350 400 200 400 175 350 340 150 300 125 250 100 200 75 150 50 100 50 25 0 0 5 10 12.7 15 20 25 30 10-8 )smargolik( thgieW daoL Load Moment/1,000 (inch-pounds) )sdnuop( thgieW daoL g/lit er) 60 g 6 a 2 l ( g 2 a 2 l 7 ** .1 *( 2 lit 3 e 4 r . s 7 ) lit R e e rs a ) r passengers 2 k n g er al; 0. 7 50 gal**(189.3 liters) e g & fr o nt p a s s F u el ( 6 l b/ 40 4 g 2 a g l* a (1 l 8 re 9 d .3 u c li e te d r * s * ) *(159 liters) ot Pil 30 gal (113.6 liters) 20 gal (75.7 liters) Baggage area 1 or Maximum Usable Fuel passenger on child’s seat * Standard tanks 10 gal (37.9 liters) ** Long range tanks *** Internal tanks Baggage area 2 Loaded Aircraft Moment/1,000 (kilogram-millimeters) 1,100 2,400 2,367 1,050 2,300 2,200 1,000 2,100 950 2,000 900 1,900 850 1,800 800 1,700 750 1,600 700 1,500 45 50 55 60 65 70 75 80 85 90 95 100 105 110 105.2 )smargolik( thgieW enalpriA dedaoL Loaded Aircraft Moment/1,000 (inch-pounds) )sdnuop( thgieW tfarcriA dedaoL Figure 10-7. Loading graph. 600 700 800 900 1,000 1,100 1,200 1,300 Normal category y or g e at c y Utilit Figure 10-8. CG moment envelope.