...symmetrical power conditions, and for all speeds from 1.2 V81 up to the maximum permissible speed. The static lateral stability, as shown by the tendency to raise the low wing in a side-slip, shall be positive within the same limits. 2.134 Stalling. In the two cases of : (1) With power off,...

...symmetrical power conditions, and for all speeds from 1.2 V81 up to the maximum permissible speed. The static lateral stability, as shown by the tendency to raise, the low wing in a side-slip, shall be positive within the same limits. 2.134 Stalling. In. the two cases of: (1) With power off,...

...symmetrical power conditions, and for all speeds from 1.2 V§1 up to the maximum permissible speed. The static lateral stability, as shown by the tendency to raise the low wing in a side-slip, shah" be positive within the same limits. Stalling. In the two cases of: (1) With power off, and (2)...

...with all landing gear and flap positions and symmetrical power conditions, at all speeds from 1.2 Vt up to the operating limit speed. (b) The static lateral...speed, (2) Not be negative at a speed equal to 1.2 Vij. (c) In straight steady sideslips (unaccelerated forward slips) the aileron and rudder control...

...speeds from 1.2 V>: up to VFS, VLB, or VFC/MFC, whichever is appropriate to the airplane configuration. (b) The static lateral stability, as shown by the...symmetrical power conditions, shall: (1) Be positive at VFS, VLE, or VFC/ MFC, whichever is appropriate to the airplane configuration. (2) Not be negative...

...and symmetrical power condition, at speeds from 1.2 Vsi up to VFK, VLS, or Vrc/Mrc (as appropriate). (b) The static lateral stability (as shown by the...wing in a sideslip with the aileron controls free and for any landing gear and flap position and symmetrical power condition) may not be negative at any...

...and symmetrical power condition, at speeds from 1.2 Vsi up to VFE, VLE, or VFC/MFC (as appropriate). (b) The static lateral stability (as shown by the...wing in a sideslip with the aileron controls free and for any landing gear and flap position and symmetrical power condition) may not be negative at any...

...whichever occurs first, and at speeds from 1.2 vs, to V0, the rudder pedal force must not reverse. (b) The static lateral stability, as shown by the tendency to raise the low wing in a sideslip, must be positive for all landing gear and Пар positions. This must be shown with symmetrical power...

...whichever occurs first, and at speeds from 1.2 VSi to V0, the rudder pedal force must not reverse. (b) The static lateral stability, as shown by the tendency to raise the low wing in a sideslip, must be positive for all landing gear and Пар positions. This must be shown with symmetrical power...

...symmetrical power conditions, and for all speeds from 1.2 V,, up to the maximum permissible speed. The static lateral stability as shown by the tendency to raise the low wing in a sideslip shall be positive within the same limits. [Amdt. 04-8, 7 FR 987. Feb. 14, 1942] § 4a.759-T Stalling....