§3.281 Wing structure.

CAR 3 · Wing-tip Float and Sea Wing Loads · Strength Requirements · at CAR3-14 (current)

Text in force at CAR3-14: from CAR3-0, effective 1 Nov 1949. OCR text

The primary wing structure shall incorporate sufficient extra strength to insure that failure of wing-tip float attachment members occurs before the wing structure is damaged.

Version history

Version	Effective	Published
CAR3-0	1 Nov 1949

Aircraft using this section

Textron Aviation Inc. 172 entry 1 at CAR3-0
Textron Aviation Inc. 172A entry 1 at CAR3-0
Textron Aviation Inc. 172B entry 1 at CAR3-0
Textron Aviation Inc. 172C entry 1 at CAR3-0
Textron Aviation Inc. 172D entry 1 at CAR3-0
Textron Aviation Inc. 172E entry 1 at CAR3-0
Textron Aviation Inc. 172F entry 1 at CAR3-0
Textron Aviation Inc. 172G entry 1 at CAR3-0
Textron Aviation Inc. 172H entry 1 at CAR3-0
Textron Aviation Inc. 172I entry 1 at CAR3-0
Textron Aviation Inc. 172K entry 1 at CAR3-0
Textron Aviation Inc. 172L entry 1 at CAR3-0
Textron Aviation Inc. 172M entry 1 at CAR3-0
Textron Aviation Inc. 172N entry 1 at CAR3-0
Textron Aviation Inc. 172P entry 1 at CAR3-0
Textron Aviation Inc. 172Q entry 1 at CAR3-0

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