Text in force at CAR3R-8: from CAR3R-0, effective 15 May 1956. OCR text
The structure shall be capable of supporting limit loads without suffering detrimental permanent deformations. At all loads up to limit loads, the deformation shall be such as not to interfere with safe operation of the airplane. The structure shall be capable of supporting ultimate loads without failure for at least 3 seconds, except that when proof of strength 13 demonstrated by dynamic tests simulating actual condiVe Vg SPEED Vmeu. LOADFACTOR,n+ oO— eocce- LIMIT MANEUVER ENVELOPES on weee- = LIMIT GUST ENVCLOPE LIMIT COMBINED ENVELOPE £ (nw) E(u,a) FIG. 3-1-—(V-n) DIAGRAM (FLIGHT ENVELOPE) tions of load application, the 3-second limit does not apply.