Piper PA-28-236 DAKOTA, Pilot Operating Handbook

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PIPER AIRCRAFT CORPORATION
PA-28-236, DAKOTA
REPORT: VB-910 ISSUED: JUNE 1, 1978
2-4
2.13 CENTER OF GRAVITY LImITS
Weight Forward Limit Rearward Limit
Pounds Inches Aft of Datum Inches Aft of Datum
3000 88.5 92.0
2500 82.5 92.0
1900 79.8 92.0
NOTES
Straight line variation between points given.
The datum used is 78.4 inches ahead of the wing
leading edge.
It is the responsibility of the airplane owner and
the pilot to insure that the airplane is properly
loaded. See Section 6 (Weight and Balance) for
proper loading instructions.
2.15 mANEUVER LImITS
No acrobatic maneuvers, including spins, approved.
2.17 FLIGHT mANEUVERING LOAD FACTORS
(a) Positive Load Factor (Maximum) 3.8 G
(b) Negative Load Factor (Maximum) No inverted maneuvers
approved
2.19 TYPES OF OPERATIONS
The airplane is approved for the following operations when equipped in
accordance with FAR 91 or FAR 135.
(a) Day V.F.R.
(b) Night V.F.R.
(c) Day I.F.R.
(d) Night I.F.R.
(e) Non Icing