§3.317 Proof of strength.

CAR 3 (Reissue) · Wings · Design and Construction · at CAR3R-8 (current)

Text in force at CAR3R-8: from CAR3R-0, effective 15 May 1956. OCR text

The strength of stressed-skin wings shail be substantiated by load tests or by combined structural analysis and tests.

Version history

Version	Effective	Published
CAR3R-0	15 May 1956

Aircraft using this section

Textron Aviation Inc. 206 entry 1 at CAR3R-0
Textron Aviation Inc. P206 entry 1 at CAR3R-0
Textron Aviation Inc. P206A entry 1 at CAR3R-0
Textron Aviation Inc. P206B entry 1 at CAR3R-0
Textron Aviation Inc. P206C entry 1 at CAR3R-0
Textron Aviation Inc. P206D entry 1 at CAR3R-0
Textron Aviation Inc. P206E entry 1 at CAR3R-0
Textron Aviation Inc. TP206A entry 1 at CAR3R-0
Textron Aviation Inc. TP206B entry 1 at CAR3R-0
Textron Aviation Inc. TP206C entry 1 at CAR3R-0
Textron Aviation Inc. TP206D entry 1 at CAR3R-0
Textron Aviation Inc. TP206E entry 1 at CAR3R-0
Textron Aviation Inc. TU206A entry 1 at CAR3R-0
Textron Aviation Inc. TU206B entry 1 at CAR3R-0
Textron Aviation Inc. TU206C entry 1 at CAR3R-0
Textron Aviation Inc. TU206D entry 1 at CAR3R-0
Textron Aviation Inc. TU206E entry 1 at CAR3R-0
Textron Aviation Inc. TU206F entry 1 at CAR3R-0
Textron Aviation Inc. TU206G entry 1 at CAR3R-0
Textron Aviation Inc. U206 entry 1 at CAR3R-0
Textron Aviation Inc. U206A entry 1 at CAR3R-0
Textron Aviation Inc. U206B entry 1 at CAR3R-0
Textron Aviation Inc. U206C entry 1 at CAR3R-0
Textron Aviation Inc. U206D entry 1 at CAR3R-0
Textron Aviation Inc. U206E entry 1 at CAR3R-0
Textron Aviation Inc. U206F entry 1 at CAR3R-0
Textron Aviation Inc. U206G entry 1 at CAR3R-0

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