Cessna skylance tc T182T, Information Manual

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SECTION 5 CESSNA
PERFORMANCE MODEL T182T NAV III
GFC 700 AFCS
U.S.
ALTIMETER CORRECTION
ALTERNATE STATIC SOURCE
CONDITIONS:
Power required for level flight or maximum power descent cruise
configuration. Altimeter corrections for the takeoff configuration are less
than 50 feet.
NOTE
Add correction to desired altitude to obtain indicated
altitude to fly. Windows and ventilators closed, cabin heater,
cabin air, and defroster on maximum.
Figure 5-2
CONDITION
Flaps UP
CORRECTION TO BE ADDED - FEET
KIAS - Alternate Static Source ON
60 80 100 120 140 160
Sea Level 30 10 -20 -20 -10 40
2000 Feet 30 10 -20 -30 -10 40
4000 Feet 30 10 -20 -30 -10 40
6000 Feet 40 10 -20 -30 -10 40
8000 Feet 40 10 -20 -30 -10 50
10,000 Feet 40 10 -20 -30 -10 50
12,000 Feet 40 10 -20 -30 -10 50
14,000 Feet 40 10 -30 -40 -10 50
T182TPHBUS-00
5-12