§3.266 Design weight.

CAR 3 · Design Weight · Strength Requirements · at CAR3-14 (current)

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

The design weight used in the water landing conditions shall not be less than the maximum weight for which certification is desired for any operation. BOAT SEAPLANES

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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