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======Engine Values====== From the “Bf 109 E Flugzeughandbuch L.Dv.556/3 (Entwurf) - Teil 2 Betriebsanleitung” (December 1939) ====Engine Operation Data==== ^ Rating ^ Revolution ^ Manifold Pressure | | | U/min | ata | | 5' - full throttle | 2400 | 1,30 | | 30' - increased cont. | 2300 | 1,20 | | d - continuous | 2200 | 1,15 | | above 5 km full throttle | 2400 | | ====Engine Load At Barricade Flight==== ^ Height ^ Revolution ^ Manifold Pressure ^ Propeller Pitch | | km | U/min | ata | o'clock | | 1 | 1200 | 0,7 | 9<sup>20</sup> | | 1 | 1200 | 0,7 | 8<sup>30</sup> | | 1 | 1300 | 0,72 | 8<sup>00</sup> | | 1 | 1500 | 0,60 | 8<sup>45</sup> | ======Bf 109 E-1/E-3 Data Sheet====== From the "Bf 109 E Flugzeughandbuch L.Dv.556/3 (Entwurf) - Teil 9 Anlagen" (December 1939) {{ :bf109e-datasheet.jpg?nolink |}} {{ :bf109e-datasheet2.jpg?nolink |}} ^ Service ceiling | circa 10300 m | ^ Lift-off-speed at start | 140 km/h | ^ Start distance until 20 m height | 470 m | ^ Landing speed at touch-down | 135 km/h | ^ Landing distance from 20 m height until stop, braked normal | 530 m | {{ :bf109e-datasheet1.jpg?nolink |}} __Note:__ CINA-atmosphere.
