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MD 530F

PERFORMANCE SPECIFICATIONS

7.0 Performance Specifications
Characteristics at
Design Gross Weight
Metric
1406 kg
Imperial
3,100 lb
Maximum Cruise Speed Sea Level
1524 m (5,000 ft)
248 km/hr
249 km/hr
134 kt (154 mph)
135 kt (155 mph)
Speed for Best Range 1524 m (5,000 ft) 243 km/hr 118 kt (219 mph)
Maximum Permitted
Speed
VNE at sea level 282 km/hr 152 kt (175 mph)
Maximum Range Sea Level
1524 m (5,000 ft)
381 km
430 km
206 nm (237 m)
232 nm (267 m)
Maximum Endurance Sea Level 381 km 206 nm (237 m)
Maximum Rate of Climb Sea Level, Standard
Day
ISA +20° C Day
10.5 m/sec
105 m/sec
2069 fpm
2061 fpm
Maximum Operating
Altitude
Density Altitude 6096 m 20,000 ft
Service Ceiling ISA 5700 m 18,700 ft
Maximum Hook
Capacity
907 kg 2,000 lb
Hovering Performance (No wind)
In-ground effect Standard Day
ISA +20° C Day
4877 m
4359 m
16,000 ft
14,300 ft
Out-of-ground effect Standard Day
ISA +20° C Day
4389 m
3536 m
14,400 ft
11,600 ft
WEIGHTS
Characteristics Metric Imperial
Maximum Gross Weight Normal Capacity
External Load
Operations
1406 kg
1701 kg
3,100 lb
3,750 lb
Empty Weight Standard Configuration 722 kg 1,591 lb
Useful Load Normal Capacity 684 kg 1,509 lb
External Load
Operations
979 kg 2,159 lb
Usable Fuel Capacity 242 l (64 gal) 183 kg 403 lb
POWER PLANT
Characteristics Metric Imperial
Rolls-Royce 250-C30
gas turbine
Rated Power 485 kw 650 shp
Derated for reliability
and safety to
Takeoff Power
Max Continuous Power
317 kw
280 kw
425 shp
375 shp

- 31 -
MD 530F


PERFORMANCE SPECIFICATIONS

7.1 Hover-In-Ground-Effect
- 32 -
MD 530F


PERFORMANCE SPECIFICATIONS

7.2 Hover-Out of-Ground-Effect
- 33 -
MD 530F

PERFORMANCE SPECIFICATIONS

7.3 Takeoff Gross Weight Worksheet
Example Mission #1 Mission #2
Empty Weight 1,591 lb
(722 kg)
Pilot 170 lb
(77 kg)
Fuel 403 lb
(183 kg)
Payload 936 lb
(424 kg)
Takeoff GW 3,100 lb
(1406 kg)

- 34 -
MD 530F


PERFORMANCE SPECIFICATIONS

7.4 Payload vs Range (5000’, ISA)
- 35 -
MD 530F


PERFORMANCE SPECIFICATIONS

7.5 Speed for Best Range
- 36 -
MD 530F


PERFORMANCE SPECIFICATIONS

7.6 Speed for Best Endurance
- 37 -
MD 530F

PERFORMANCE SPECIFICATIONS

7.7 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 10 ampere electrical load.

- 38 -
MD 530F

PERFORMANCE SPECIFICATIONS

7.8 Fuel Flow, Sea Level, ISA +20°C (35°C)
Note: Use for Estimates Only. Not FAA Approved. Based on clean aircraft, level
flight performance, minimum specification engine,
particle separator and 10 ampere electrical load.

- 39 -
MD 530F

PERFORMANCE SPECIFICATIONS

7.9 Fuel Flow, 4,000 feet, ISA (7°C)
Note: Use for Estimates Only. Not FAA Approved. Based on clean aircraft, level
flight performance, minimum specification engine,
particle separator and 10 ampere electrical load.

- 40 -
MD 530F

PERFORMANCE SPECIFICATIONS

7.10 Fuel Flow, 4,000 feet, ISA +20°C (27°C)
Note: Use for Estimates Only. Not FAA Approved. Based on clean aircraft, level
flight performance, minimum specification engine,
particle separator and 10 ampere electrical load.

- 41 -
530performance specif3

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530performance specif3

  • 1. MD 530F PERFORMANCE SPECIFICATIONS 7.0 Performance Specifications Characteristics at Design Gross Weight Metric 1406 kg Imperial 3,100 lb Maximum Cruise Speed Sea Level 1524 m (5,000 ft) 248 km/hr 249 km/hr 134 kt (154 mph) 135 kt (155 mph) Speed for Best Range 1524 m (5,000 ft) 243 km/hr 118 kt (219 mph) Maximum Permitted Speed VNE at sea level 282 km/hr 152 kt (175 mph) Maximum Range Sea Level 1524 m (5,000 ft) 381 km 430 km 206 nm (237 m) 232 nm (267 m) Maximum Endurance Sea Level 381 km 206 nm (237 m) Maximum Rate of Climb Sea Level, Standard Day ISA +20° C Day 10.5 m/sec 105 m/sec 2069 fpm 2061 fpm Maximum Operating Altitude Density Altitude 6096 m 20,000 ft Service Ceiling ISA 5700 m 18,700 ft Maximum Hook Capacity 907 kg 2,000 lb Hovering Performance (No wind) In-ground effect Standard Day ISA +20° C Day 4877 m 4359 m 16,000 ft 14,300 ft Out-of-ground effect Standard Day ISA +20° C Day 4389 m 3536 m 14,400 ft 11,600 ft WEIGHTS Characteristics Metric Imperial Maximum Gross Weight Normal Capacity External Load Operations 1406 kg 1701 kg 3,100 lb 3,750 lb
  • 2. Empty Weight Standard Configuration 722 kg 1,591 lb Useful Load Normal Capacity 684 kg 1,509 lb External Load Operations 979 kg 2,159 lb Usable Fuel Capacity 242 l (64 gal) 183 kg 403 lb POWER PLANT Characteristics Metric Imperial Rolls-Royce 250-C30 gas turbine Rated Power 485 kw 650 shp Derated for reliability and safety to Takeoff Power Max Continuous Power 317 kw 280 kw 425 shp 375 shp - 31 -
  • 3. MD 530F PERFORMANCE SPECIFICATIONS 7.1 Hover-In-Ground-Effect - 32 -
  • 4. MD 530F PERFORMANCE SPECIFICATIONS 7.2 Hover-Out of-Ground-Effect - 33 -
  • 5. MD 530F PERFORMANCE SPECIFICATIONS 7.3 Takeoff Gross Weight Worksheet Example Mission #1 Mission #2 Empty Weight 1,591 lb (722 kg) Pilot 170 lb (77 kg) Fuel 403 lb (183 kg) Payload 936 lb (424 kg) Takeoff GW 3,100 lb (1406 kg) - 34 -
  • 6. MD 530F PERFORMANCE SPECIFICATIONS 7.4 Payload vs Range (5000’, ISA) - 35 -
  • 7. MD 530F PERFORMANCE SPECIFICATIONS 7.5 Speed for Best Range - 36 -
  • 8. MD 530F PERFORMANCE SPECIFICATIONS 7.6 Speed for Best Endurance - 37 -
  • 9. MD 530F PERFORMANCE SPECIFICATIONS 7.7 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 10 ampere electrical load. - 38 -
  • 10. MD 530F PERFORMANCE SPECIFICATIONS 7.8 Fuel Flow, Sea Level, ISA +20°C (35°C) Note: Use for Estimates Only. Not FAA Approved. Based on clean aircraft, level flight performance, minimum specification engine, particle separator and 10 ampere electrical load. - 39 -
  • 11. MD 530F PERFORMANCE SPECIFICATIONS 7.9 Fuel Flow, 4,000 feet, ISA (7°C) Note: Use for Estimates Only. Not FAA Approved. Based on clean aircraft, level flight performance, minimum specification engine, particle separator and 10 ampere electrical load. - 40 -
  • 12. MD 530F PERFORMANCE SPECIFICATIONS 7.10 Fuel Flow, 4,000 feet, ISA +20°C (27°C) Note: Use for Estimates Only. Not FAA Approved. Based on clean aircraft, level flight performance, minimum specification engine, particle separator and 10 ampere electrical load. - 41 -