ECCN 9A101
MTATTurbojet and turbofan engines, other than those controlled by 9A001, as follows .
Items Covered
- a.Engines having all of the following characteristics:
- 1. 'Maximum thrust value' greater than 400 N (achieved un-installed) excluding civil certified engines with a maximum thrust value greater than 8,890 N (achieved un-installed);
- 2. Specific fuel consumption of 0.15 kg N−1 h−1 or less;
- 3. 'Dry weight' less than 750 kg; and
- 4. 'First-stage rotor diameter' less than 1 m; or
- b.Engines designed or modified for use in "missiles" or UAVs with a range equal to or greater than 300 km, regardless of thrust, specific fuel consumption, 'dry weight' or 'first-stage rotor diameter'.
Control Reasons
MTMissile Technology
Items controlled under the Missile Technology Control Regime (MTCR).
Column 1: YesColumn 2: No
ATAnti-Terrorism
Items controlled for anti-terrorism reasons. Most items on the CCL have AT controls.
Column 1: YesColumn 2: No
Disclaimer
This information is for reference only. For official classifications, consult BIS or a qualified export control professional.