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Piper Dakota - Leading Particulars and Principal Dimensions

Piper Dakota
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DIMENSIONS
Airplane dimensions and specifications are shown in figure 6-1 and listed in chart 601.
CHART 601. LEADING PARTICULARS AND PRINCIPAL DIMENSIONS
MODEL PA-28-236
ENGINE
Manufacturer Avco-Lycoming
Model 0-540-J3A5D
Rated horsepower at propeller rpm 235 hp/2400 rpm
Oil sump capacity l2 U.S. qts.
Fuel, aviation grade, minimum l00/ 130
Magneto, Bendix D6LN-203l, 303l, 3000
Magneto timing 23° btc
Approved spark plugs Refer to the latest issue of Avco
Lycoming Service Instructions
No. 1042
Spark plug gap 0.017 to 0.021
Firing order 1-4-5-2-3-6
Carburetor, Marvel-Schebler MA4-5
Starter, Prestolite, l2 Volt MZ4206
Alternator, Prestolite (60 Amp) ALY-6422
1
Alternator, Chrysler (60 Amp) 3656624
2
Alternator, Chrysler (60 Amp) 4111810
3
PROPELLER (CONSTANT SPEED)
Manufacturer Hartzell
Hub, model HC-F2YR-l( )
Blade, model F8468A-4R
Diameter max./min. 80.0 In.
Governor control Hartzell
Governor model F-4-2l( )
1
Airconditioned aircraft
2
Non-Airconditioned aircraft s/n: 28-7911001 to 28-7911087
3
Non-Airconditioned aircraft s/n: 28-7911088 and up
6 - 10 - 00
Page - 6 - 01
Reissued: August 1, 1986
1B15
PIPER AIRCRAFT
PA-28-236
MAINTENANCE MANUAL

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