SECTION 1
PIPER AIRCRAFT CORPORATION
GENERAL
PA-28-236, DAKOTA
REPORT: VB-910
ISSUED: JUNE 1, 1978
1-4
REVISED: NOVEMBER 22, 1982
1.9 OIL
(a) Oil Capacity (U.S. qts.)
12
(b) Oil Specification
Refer to latest issue
of Lycoming Service
Instruction 1014.
(c) Oil Viscosity
Refer to Section 8 -
paragraph 8.19.
1.11 MAXIMUM WEIGHTS
(a) Maximum Ramp Weight (lbs.)
3011
(b) Maximum Takeoff Weight (lbs.)
3000
(c) Maximum Landing Weight (lbs.)
3000
(d) Maximum Weights in Baggage
Compartment (lbs.)
200
1.13 STANDARD AIRPLANE WEIGHTS *
Refer to Figure 6-5 for the Standard Empty Weight and the Useful Load.
1.15 BAGGAGE SPACE
(a) Compartment Volume (cu. ft.)
24
(b) Entry Width (in.)
22
(c) Entry Height (in.)
20
Summary of Contents for PA-28-236 DAKOTA
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