FAA Approved Airplane Flight Manual Supplement

190-00716-02 Rev. 3 Hawker Beechcraft King Air 300/300LW
FAA APPROVED Page 111 of 167
A
LTIMETER CORRECTION - NORMAL SYSTEM
FLAPS UP
NOTE Above 18,000 ft, Corrected Altitude = Indicated Altitude
-150 -140 -130 -120 -110 -100
-90 -80 -70 -60 -50 -40 -30 -20 -10
0
10 20 30 40 50
80 90 100 110 120 130 140 150 160 170 180 190 200 210 220 230 240 250 260 270
Indicated Airspeed - Kt
Altimeter Correction - Ft
(Add to Indicated Altitude)
Vali d fo r Altitud es Below 18,000 ft
Section 5 – Performance