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Cessna 206H - WEIGHT LIMITS

Cessna 206H
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SOLOY TURBINE PAC SECTION 2
POHS CESSNA T206H/206H LIMITATIONS
2-8
F.A.A. Approved November 17, 2015
MISCELLANEOUS INSTRUMENT MARKINGS
INSTRUMEN
T LIMIT
BARBER
POLE*
RED LINE
GREEN ARC
YELLOW
ARC
RED LINE
RED DOT
RED
DIAMOND*
SUCTION
------
4.5-5.5
in. Hg.
------
-----
-
---
---
AMMETER
80-150
150
FUEL QTY.
E
Figure 2-5. Miscellaneous Instrument Markings.
NOTES: (1) N
1
and oil pressure limits are noted by a step in their respective
arcs.
N
1
Engine Oil Pressure
79% and below 50 130 psi
79% to 94% 90 130 psi
94% and above 115 130 psi
(2)* Minimum in flight torque is 14 psi.
(3) Not for intentional use.
(4) Limit - 60 seconds at torque settings greater than 20 psi.
(5) Aircraft incorporating an “enhanced” power turbine wheel per
Rolls-Royce CEB A-1365 must include the yellow arc extending
from 1358 rpm to 1630 rpm.
* These markings are depicted on the optional two inch engine
instruments.
WEIGHT LIMITS
Ramp Weight: 3617 lbs.
Maximum Takeoff Weight: 3600 lbs.
Maximum Landing Weight: 3600 lbs.
Maximum Weight in Baggage Compartment Station 109 to 145:
180 lbs. (See note below).
NOTE
Refer to Section 6 of this handbook for loading
arrangement with one or more seats for cargo
accommodation.
UNCONTROLLED
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