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ISA +20°C Day
2,100 1,900
1,700 1,500
1,350 ft/min 1,150 ft./min
Maximum Operating Altitude
Density Altitude
20,000
20,000
20,000
Service Ceiling
ISA @ 100 ft/min
20,000+
20,000+
13,500
HIGE (Hover-in-Ground Effect)
Standard Day ISA +20°C Day
14,500+ 12,200+
14,500+ 11,600
11,100 ft 7,000 FT
HOGE (Hover Out-of-Ground Effect)
Standard Day ISA +20°C Day
14,500+ 12,200+
11,700 8,000
6,000 ft 3,200 ft
Certification Limits:
Standard Weight
Normal Category Maximum Internal
4,100 lb 4,500 lb*
Empty Weight
Standard Configuration Industrial Configuration
2,100 lb 2,036 lb
Useful Load
Internal External
2,000 lb 2,400 lb**
Cargo Hook Structural Rating
3,000 lb
Fuel Capacity
115 gal
Powerplant: Rolls-Royce Engine Company Model 250-C47M gas turbine, rated at 603 kw (808 shp), derated for reliability and safety to: Takeoff 447 kw (600 shp) Max Continuous Power 395 kw (530 shp)
PERFORMANCE SPECIFICATIONS
23
1406 kg
1633 kg
1860 kg
Maximum Cruise Speed
KTAS Sea Level ISA KTSA 1524 m, ISA
267 274
257 255
248 kph 248 kph
Maximum Permitted Speed
Vne (KCAS) at Sea Level
282
282
250 kph
Maximum Range
Sea Level ISA
1524 m, ISA
693 783
661 743
633 km 704 km
Maximum Endurance
Sea Level ISA
1524 m, ISA
3.9 4.4
3.8 4.1
3.6 hr 3.9 hr
Maximum Rate-of-Climb (AEO)
Sea Level Standard ISA
ISA +20°C Day
10.7 9.6
8.6 7.6
6.9 m/s 5.8 m/s
Maximum Operating Altitude
Density Altitude
6096
6096
6096 m
Service Ceiling
ISA @ 30.5 m/min
6096+
5639
4115m
HIGE (Hover-in-Ground Effect)
Standard Day ISA +20°C Day
4420+ 3719+
4420+ 3536
3383 m 2134 m
HOGE (Hover Out-of-Ground Effect)
Standard Day ISA +20°C Day
4420+ 3719+
3566 2438
1829 m 975 m
Certification Limits
Standard Weight
Normal Category External Load
1859 kg 2131 kg*
Empty Weight
Standard Configuration Industrial Configuration
962 kg 923 kg
Useful Load
Internal External
907 kg 1179 kg**
Cargo Hook Structural Rating
1360 kg
Fuel Capacity
4351
Powerplant: Rolls-Royce Engine Company Model 250-C47M gas turbine, rated at 603 kw (808 shp), derated for reliability and safety to: Takeoff 447 kw (600 shp) Max Continuous Power 395 kw (530 shp)
PERFORMANCE SPECIFICATIONS
24
5.1. Hover-In-Ground-Effect.
PERFORMANCE SPECIFICATIONS
25
5.2. Hover-Out of-Ground-Effect.
PERFORMANCE SPECIFICATIONS
26
5.3. Gross Weight Worksheet
Example
Mission #1
Mission #2
Empty Weight
2,100 lb (952 kg)
Pilot
170 lb (77 kg)
Fuel
782 lb (355 kg)
Payload
1,048 lb (476 kg)
Takeoff GW
4,100 lb (1860 kg)
PERFORMANCE SPECIFICATIONS
27
5.4. Payload vs Range.
PERFORMANCE SPECIFICATIONS
28
5.5. Speed for Best Range.
Note: Use for Estimates Only. Not FAA Approved. Based on clean aircraft, level flight performance, minimum specification engine, particle separator and 40 ampere electrical load.
PERFORMANCE SPECIFICATIONS
29
5.6. Speed for Best Endurance.
Note: Use for Estimates Only. Not FAA Approved. Based on clean aircraft, level flight performance, minimum specification engine, particle separator and 40 ampere electrical load.
PERFORMANCE SPECIFICATIONS
30
5.7. Fuel Consumption
5.7.1. Fuel Flow, Sea Level, ISA (15°C).
Note: Use for Estimates Only. Not FAA Approved. Based on clean aircraft, level flight performance, minimum specification engine, particle separator and 40 ampere electrical load.
PERFORMANCE SPECIFICATIONS
31
5.7.2. Fuel Flow, 4000 ft, ISA (7°C).
Note: Use for Estimates Only. Not FAA Approved. Based on clean aircraft, level flight performance, minimum specification engine, particle separator and 40 ampere electrical load.
PERFORMANCE SPECIFICATIONS
32
5.7.3. Fuel Flow, Sea Level, ISA +20 (35°C).
Note: Use for Estimates Only. Not FAA Approved. Based on clean aircraft, level flight performance, minimum specification engine, particle separator and 40 ampere electrical load.
PERFORMANCE SPECIFICATIONS
33
5.7.4. Fuel Flow, 4000 ft, ISA +20 (27°C).
Note: Use for Estimates Only. Not FAA Approved. Based on clean aircraft, level flight performance, minimum specification engine, particle separator and 40 ampere electrical load.
DIRECT OPERATING COST
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MD600 TechDescription Feb09(9)
