Harbin Aircraft Manufacturing Corporation / AVICopter - China
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(OPERATORS list includes past, present, and future operators when applicable)
(Showcased structural values pertain to the Harbin Z-19 production variant)
2 x WZ8A turboshaft engines developing 848 horsepower to four-bladed main rotor system and fenestron tail rotor.
(245 kph | 132 kts)
(700 km | 1,296 nm)
♦ MACH Regime (Sonic)
RANGES (MPH) Subsonic: <614mph | Transonic: 614-921 | Supersonic: 921-3836 | Hypersonic: 3836-7673 | Hi-Hypersonic: 7673-19180 | Reentry: >19030
Variable based on mission parameters and set about conventional wing stub pylons:
"Blue Arrow-9" Anti-Tank Guided-Missiles (ATGMs), TY-90 Air-to-Air Missiles (AAMs), HJ-8 ATGMs, rocket pods (unguided), cannon pods and gun pods supported.
(Not all ordnance types may be represented in the showcase above)
Values are derrived from a variety of categories related to the design, overall function, and historical influence of this aircraft in aviation history.
The overall rating takes into account over 60 individual factors related to this aircraft entry.
Rating is out of a possible 100 points.
This entry's maximum listed speed (152mph).
Graph average of 150 miles-per-hour.
Harbin Z-19 operational range when compared to distances between major cities (in KM).
Showcasing era cross-over of this aircraft design.
Compared against Ilyushin IL-2 (military) and Cessna 172 (civilian).
Ribbon graphics not necessarily indicative of actual historical campaign ribbons. Ribbons are clickable to their respective aerial campaigns / operations / aviation periods.