Indonesian Aerospace (IAe) - Indonesia
Manufacturer(s)
Indonesia (planned)
Operators
2019
Service Year
Indonesia
National Origin
In-Development
Project Status
2
Crew
2
Units
SPECIAL-MISSION: MECICAL EVACUATION
Extraction of wounded combat or civilian elements by way of specialized onboard equipment and available internal volume or external carrying capability.
SPECIAL-MISSION: SEARCH & RESCUE
Ability to locate and extract personnel from areas of potential harm or peril (i.e. downed airmen in the sea).
TRANSPORT
General transport functionality to move supplies/cargo or personnel (including wounded and VIP) over range.
COMMERCIAL AVIATION
Used in roles serving the commercial aviation market, ferrying both passengers and goods over range.
VIP SERVICE
Used in the Very-Important-Person (VIP) passenger transport role, typically with above-average amenities and luxuries as standard.
INTELLIGENCE-SURVEILLANCE-RECONNAISSANCE
Surveil ground targets / target areas to assess environmental threat levels, enemy strength, or enemy movement.
SPECOPS
Serving Special Forces / Special Operations elements and missions.
MULTI-ENGINE
Incorporates two or more engines, enhancing survivability and / or performance.
RUGGED AIRFRAME
Inherent ability of airframe to take considerable damage.
EXTENDED RANGE PERFORMANCE
Capability to travel considerable distances through onboard fuel stores.
MARITIME OPERATION
Ability to operate over ocean in addition to surviving the special rigors of the maritime environment.
CREW-MANAGED
Beyond a pilot, the aircraft takes advantage of additional crew specialized in specific functions aboard the aircraft.
ENCLOSED CREWSPACE(S)
Features partially- or wholly-enclosed crew workspaces.
ENHANCED ACCESS
Design incorporates feature(s) that facilitates loading / unloading of cargo / personnel from the aircraft.
54.1 ft
(16.50 meters)
Length
64.0 ft
(19.50 meters)
Width/Span
20.3 ft
(6.18 meters)
Height
9,502 lb
(4,310 kilograms)
Empty Weight
15,498 lb
(7,030 kilograms)
Maximum Take-Off Weight
+5,997 lb
(+2,720 kg)
Weight Difference
monoplane / shoulder-mounted / straight
Mainplane Arrangement
Monoplane
Design utilizes a single primary wing mainplane; this represents the most popular modern mainplane arrangement.
Shoulder-Mounted
Mainplanes are mounted at the upper section of the fuselage, generally at the imaginary line intersecting the pilot's shoulders.
Straight
The planform involves use of basic, straight mainplane members.
2 x Pratt & Whitney Canada PT6A-42 turboprop engines developing 850 horsepower and driving four-bladed propeller units.
Propulsion
249 mph
(400 kph | 216 knots)
Max Speed
9,843 ft
(3,000 m | 2 miles)
Ceiling
966 miles
(1,555 km | 840 nm)
Range
2,000 ft/min
(610 m/min)
Rate-of-Climb
MACH Regime (Sonic)
Sub
Trans
Super
Hyper
HiHyper
ReEntry
RANGES (MPH) Subsonic: <614mph | Transonic: 614-921 | Supersonic: 921-3836 | Hypersonic: 3836-7673 | Hi-Hypersonic: 7673-19180 | Reentry: >19030
