Here's the 'shoulds' for the UH:
1. The engines should be of modular design and should have full authority digital control (FADEC) with training modes.
2. The helicopter’s fuel system should have:
a. Pressure and gravity re-fuelling capability.
b. Fuel Cells with crashworthy properties. Tenderers should state the crashworthiness standard.
c. Fuel flow meter, or equivalent provisions.
d. Fuel Jettison capability.
e. In flight inter tank fuel transfer.
3. Defect and flaw tolerance in the rotor should be in accordance with FAR/JAR requirements. The rotor system should have a demonstrated ballistic tolerance.
4. There should be an ability to generate hydraulic power independently on the ground or if not, it must have capability of accepting a standard hydraulic ground rig.
5. The cockpit should be ergonomic and provide the pilot with a high degree of external visibility. There should be adequate secure stowage for flight documents and chart, including an illuminated, NVE compatible, IFR approach chart holder.
6. The cockpit displays should be based on the use of modern flat screen units, with adequate redundancy and flexibility to transfer display page formats from one display unit to any other.
7. The helicopter should be equipped with emergency egress lighting.
8. The tenderer should provide a mounting for a General Purpose Machine Gun of 7.62mm calibre on both sides of the fuselage. The mounting should be a removable part. Restrictions imposed on the operation of the sliding doors when the weapon is mounted and deployed, should be stated.
9. The helicopter should be equipped with weather radar.
10. The helicopter should be equipped with a wire strike protection system.
11. Tenderers should provide options on the capability of the helicopters to provide limited fire support, which should cover a broad spectrum of basic weapons.
1. The engines should be of modular design and should have full authority digital control (FADEC) with training modes.
2. The helicopter’s fuel system should have:
a. Pressure and gravity re-fuelling capability.
b. Fuel Cells with crashworthy properties. Tenderers should state the crashworthiness standard.
c. Fuel flow meter, or equivalent provisions.
d. Fuel Jettison capability.
e. In flight inter tank fuel transfer.
3. Defect and flaw tolerance in the rotor should be in accordance with FAR/JAR requirements. The rotor system should have a demonstrated ballistic tolerance.
4. There should be an ability to generate hydraulic power independently on the ground or if not, it must have capability of accepting a standard hydraulic ground rig.
5. The cockpit should be ergonomic and provide the pilot with a high degree of external visibility. There should be adequate secure stowage for flight documents and chart, including an illuminated, NVE compatible, IFR approach chart holder.
6. The cockpit displays should be based on the use of modern flat screen units, with adequate redundancy and flexibility to transfer display page formats from one display unit to any other.
7. The helicopter should be equipped with emergency egress lighting.
8. The tenderer should provide a mounting for a General Purpose Machine Gun of 7.62mm calibre on both sides of the fuselage. The mounting should be a removable part. Restrictions imposed on the operation of the sliding doors when the weapon is mounted and deployed, should be stated.
9. The helicopter should be equipped with weather radar.
10. The helicopter should be equipped with a wire strike protection system.
11. Tenderers should provide options on the capability of the helicopters to provide limited fire support, which should cover a broad spectrum of basic weapons.
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