§3.609 Carburetor fluid de-icing system detail design.

CAR 3 (Reissue) · Induction System · Powerplant Installations – Reciprocating Engines · at CAR3R-8 (current)

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

Carburetor fluid deicing systems shall comply with provisions for the design of fuel systems, except as specified in §§ 3.607 and 3.608, unless such provisions aré manifestly inapplicable.

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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