SECTION 2 CESSNA
LIMITATIONS MODEL
2088 (675 SHP)
POWER PLANT LIMITATIONS
(Continued)
SHP
(9)
675
675
675
I
(Continued Next Page)
1
1
2-8
U.S.
OIL
PSlG
(9)
6510105
6510 105
6510 105
1
1
1
Idle
Maximum
Reverse
(5)
Translent
FAA APPROVED
Revision 23
OIL
TEMPT
(7)
101099
0 to 99
0
to 99
GASGEN
RPM%Ng
(2)
101.6
101.6
101.6
Figure 2-3. Engine Operating Limits
1
1. Per the Maximum Engine Torque For Takeoff figure of Section
5.
2. For every 10°C (18°F) below -30°C (-22°F) ambient temperature,
reduce maximum allowable
Ng by 2.2%.
3. Normal oil pressure is
85
to 105 PSI at gas generator speeds
above 72% with oil temperature between 60" and 70°C (140" and
158°F). Oil pressures below
85
PSI are undesirable and should
be tolerated only for the completion of the flight, preferably at a
reduced power setting. Oil pressures below normal should be
reported as an engine discrepancy and should be corrected
before the next flight. Oil pressures below 40 PSI are unsafe and
require that either the engine be shut down or a landing be made
as soon as possible using the minimum power required to sustain
flight.
Stnrtlng
Maxlmum
Rated
(8)
PROP
RPM
1900
1900
------
1900
POWER
SETTING
Takeoff
Maxlmum
Cllmb
-
Maxlmum
Crulse
.-
1865
2400 (6)
---
1665
TORQUE
FT-LBS
(I), (4)
(4), (13)
(4). (14)
665
(15)
805
650 (11)
MAXIMUM
ITT
('CI
605 (10)
765
740
1090
(11)
805
52
Minimum
101.6
102.6 (11)
...
101 6
---
1625
2090
-.
1900
40
Minimum
65
to
105
...
40
lo
99
0
to 99
0
to 99
010104
1121
---
675
.-
.-
65
to
105
. .
40
Minmurn
10 to99
...
675
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