Contact|RisingUp Home


Federal Aviation Regulations

Sec. 23.1041 — General.

The powerplant and auxiliary power unit cooling provisions must maintain the temperatures of powerplant components and engine fluids, and auxiliary power unit components and fluids within the limits established for those components and fluids under the most adverse ground, water, and flight operations to the maximum altitude and maximum ambient atmospheric temperature conditions for which approval is requested, and after normal engine and auxiliary power unit shutdown.

[Doc. No. 26344, 58 FR 18973, Apr. 9, 1993, as amended by Amdt. 23–51, 61 FR 5137, Feb. 9, 1996]

NEXT: Sec. 23.1043 - Cooling tests.
PREVIOUS: Sec. 23.1027 - Propeller feathering system.

Search the FARS for