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84 Air Regulations, 1938 23. HORIZONTAL TAIL PLANE (a) Area........ (b) Span........ (c) Max chord ........ (d) Shape............... (e) Range in degrees............. (f) Angle between neutral position of Tail Plane and the Upper Wing Chord at centre [[center]] section................................................... .......................................................... 24. ELEVATORS (a) Span........ (b) Chord........ (c) Total area........ (d) Balance area................... Span ................ (e) Distance from elevator hinge to leading edge of lower wing..................................................... 25. VERTICAL FIN (a) Area.............. (b) Shape ........................ 26. RUDDER (a) Height ........... (b) Chord (not including (c) Total area........ balance)............... (d) Balance area...... (e) Distance from rudder hinge to leading edge of lower wing ............................................................ 27. FUSELAGE OR HULL (a) Maximum cross section area.............................. (b) Width at main planes.................................... 28. LANDING GEAR OR FLOATS (a) Type.................................................... If of foreign manufacture submit proof of type approval from country of origin. (If products from U.S.A. insert A.T.C. number.) (b) Shock absorbing system (c) No. of wheels............. .......................... Size of tires............. (d) Track ................ (e) Braking device............ (f) Number of floats...... Track ......................... (g) Number of skis........ Track ......................... (h) Horizontal distance from leading edge of lower wing to C/L of axle (in flying position).......................... .......................................................... 29. AIRSCREWS (a) Number of airscrews.......... Type.................... If of foreign manufacture submit proof of type approval from country of origin. (If products from U.S.A. insert A.T.C. number.) (b) Make................. (c) Drawing number.............. (d) Diameter ............ (e) Pitch ...................... (f) Clearance (flying position)........................... 30. POWER PLANT (a) Manufacturer of engine................................ (b) Manufacturer's Serial Number ........ (c) Type........ If of foreign manufacture submit proof of type approval from country of origin. (If products from U.S.A. insert A.T.C. number.) (d) Location.............................................. (e) International rating: ......................H.P. at...................... R.P.M ......................H.P. at...................... R.P.M (f) Compression ratio.....................................