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Rolls-Royce Turbomeca RTM322-01/9

RTM322-01/9 exact certified turboshaft variant in the Safran RTM322 family, documented for NH90 and other ten-to-fifteen-ton helicopter applications. EASA records a two-spool modular turboshaft with 1,566 kW normal takeoff, 30-minute AEO, and maximum-continuous power for the baseline configuration, with a 1,611 kW rating when the specified C3028/NFHDIS configuration is active; the typed power field uses the conservative 1,566 kW baseline. The type certificate records 1,181 mm overall length, 232.15 kg dry mass including EECU, and 20,841 rpm nominal output-shaft speed. Safran currently supports the RTM322 program and reports more than two million flight hours.

Identity

Aliases
RTM322-01/9Rolls-Royce Turbomeca RTM322-01/9Safran RTM322-01/9
Domains
aviation
Identity Level
variant
Kind
turboshaft
Name
Rolls-Royce Turbomeca RTM322-01/9
Status
active

Details

Air Breathing Specs
Shaft Power
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Description
RTM322-01/9 exact certified turboshaft variant in the Safran RTM322 family, documented for NH90 and other ten-to-fifteen-ton helicopter applications. EASA records a two-spool modular turboshaft with 1,566 kW normal takeoff, 30-minute AEO, and maximum-continuous power for the baseline configuration, with a 1,611 kW rating when the specified C3028/NFHDIS configuration is active; the typed power field uses the conservative 1,566 kW baseline. The type certificate records 1,181 mm overall length, 232.15 kg dry mass including EECU, and 20,841 rpm nominal output-shaft speed. Safran currently supports the RTM322 program and reports more than two million flight hours.
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Dry Mass
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Creation Time
August 13, 2026 at 18:11:38 UTC
Updated Time
August 21, 2026 at 07:07:16 UTC

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