See the type certificate data http://www.airweb.faa.gov/Regulatory_and_Guidance_Library/rgMakeModel.nsf/0/5C679681565DE939852567390045D9B1/$FILE/a-691.pdf
VI - Model PA-11, 2 PCLM, Approved April 30, 1947. See NOTE 7 regarding conversion to 2 POLM.
Model PA-11 is generally similar to the J3C-65 except vertical location of engine mount, cowling, forward fuselage structure,
types of seats, fuel system (including gas tank location), lift struts, required equipment, and eligibility of certain equipment items,
as listed. Elevator bungee (Piper Drawing number 80352) must be installed in order that the aircraft conform to the pertinent
flight requirements.
Engine Continental A-65-8F (See Item 311D for optional engines)
Engines and Engine Accessories - Fuel and Oil System (cont.)
311. D.
(6) Lycoming O-235-C Use actual weight and arm
Eligible on landplane only and when installed in accordance with Piper Dwg. No 12447.
Engine Limits: All operations, 2600 r.p.m. (100 hp)
Fuel: 80 minimum octane aviation gasoline.
Oil Capacity: 6 qts. (-31)
Propeller Limits: (with propeller, Item 10 or 11 only)
Static r.p.m. at maximum permissible throttle setting:
Not over 2450, not under 2250.
No additional tolerance permitted.
C. G. Range: (+12.9) to (+17.3)
Aircraft weight and balance should be checked to determine need for
11¼ lb. ballast at (+179) or limitation to solo from rear seat only.
Placard required in full view of pilot: "All acrobatics, including spins, prohibited."