A~rcraR Publications
Piper Comanche
250
(Early Model)
Section
-
2
Limitations
POWER PLANT LINIITATIONS
i
1.)
Engine Operating Limits:
One Lycoming Model: 0-540-AlA5, AlB5, AlC5, or AID5
..........................................
Takeoff Power and MCP
......................
...
2575 rpd250 bhp
2.)
Propeller Limitations:
One Hartzell
Hub Model:
HC-A2XK-1
or HC-82XK-ID
Blade Model: 8433-7
Diameter
......................................................................
Maximum 77 in
*
Minimum
76
in
Pitch (30 in Station)
..........................
Low 14.5 to 15.0 Degrees
*
High 31.0 to 33.0 Degrees
One McCauley Hub Model: 2D36C28180MM-6
Blade Model: D-2286/80MM-6
Diameter
.......................................................................
Maximum 74
in
*
Minimum 73 in
...................................
Pitch (30 in Station)
Low 15.5 to 15.9 Degrees
*
High 32.0 Degrees
~.
WEIGHT LIMITS
(
.i
....................................
Maximum Takeoff Weight 2,800 1b
............
.............................
Maximum Landing Weight
..
2,800 lb
...........................................................
........................
Maximum Baggage Weight
.......
200 lb
CENTER OF GRAVITY LJMITS
Weight
Arm
Forward Limit
Arm
Rearward Limit
Pounds Inches
Afl
of Datum Inches
Aft
of Datum
2,800 87.7
2,400 82.5
1,900 or Less 80.5
**
NOTE
**
Straight line variation exists between the points given.
STRUCTURAL
LOAD
FACTORS
.
.
........................................................................................
Posltive
Normal Category
+
3.80 g
......................................................................................
Negative
Normal Category
-
1.52 g
**
NOTE
**
No inverted maneuvers are approved
FAA
APPROVED
(November 10,1993)
Copyright: 1993
ALRPLANE FLIGHT
MANUAL
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