Text in force at CAR3R-8: from CAR3R-5, effective 1 Oct 1959. OCR text
bal 2 o * * {c) The wing flap and landing gear controls shall comply with the following: | (L) The wing flap or auxiliary lift device control shall be located centrally or to the right of the pedestal centerline or of the powerplant throttle control center~ line and shall be sufficiently displaced from the landing gear control to avoid confusion.
(2) The landing gear control shall located to the left of the throttle cent line or of the pedestal centerline, (3) The control knobs shall be shaped in accordance with figure 3-13. Nore: Figure 3-13 is not intended to indicate the exact size or proportion of the control knobs. 9. By adding a new figure 3-13 as follows: FLAP CONTROL KNOB LANDING GEAR CONTROL KNOB Ficurs 3-13.—Controt KNos SHAPES, 10. By amending § 3.416 by adding a new paragraph (c) to read as follows:
(Secs. 313(a), 601, 608, 72 Stat. 752, 775, 776; 49 U.S.C. 1354(a), 1421, 1423) ·