Protection of other airplane components against fire.

29. Protection of other airplane components against fire. To meet the requirements of 121.277, C-46 airplanes must -
(a) Conform to the type design and all applicable airworthiness directives; and
(b) Be modified or have operational procedures established to provide additional fire protection for the wheel well door aft of each engine compartment. Modifications may consist of improvements in sealing of the main landing gear wheel well doors. An operational procedure which is acceptable to the Agency is one requiring the landing gear control to be placed in the up position in case of in-flight engine fire. In accordance with ยง 121.315, such procedure must be set forth in the emergency portion of the operator's emergency checklist pertaining to in-flight engine fire.

Source

14 CFR § C_to_part_121


Scoping language

None
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