SOLOY TURBINE PAC
SECTION 2
POHS CESSNA T206H/206H
LIMITATIONS
2-8
F.A.A. Approved
November 17, 2015
MISCELLANEOUS INSTRUMENT MARKINGS
IN
S
TR
U
M
E
N
T
L
IMI
T
B
A
R
B
E
R
P
OLE
*
R
E
D
LI
N
E
GR
E
E
N
A
R
C
Y
E
L
LOW
ARC
R
E
D
LI
N
E
R
E
D
D
OT
R
E
D
D
IA
MON
D
*
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
COPY
