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Maximum Number of Occupants
11, including the flight crew
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Minimum Flight Crew
Pilot in the right seat
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Maximum Gross Weight
3525 KG (7903 lbs)
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Maximum Allowable Floor Loading
600 KG/m2 (1231 lb)
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Maximum weight per tie-down ring
70 KG (154 lbs)
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Vne for OEI operation under all conditions
110 KIAS
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Vne for Steady-State Autorotation
90 KIAS
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Maximum Operating Altitude
18,000' PA
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Maximum operating altitude for hover (IGE) or takeoff/landing
18,000' PA or 18,000' DA, whichever is less
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Flights with NACA inlets closed (PUSH FOR AIR knob pulled)
Limited to 30 minutes to prevent avionics overheating
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Minimum air temperature without cold weather kit
-30 C
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Maximum Air Temperature
50 C
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For engine startup at OAT below _____ using the aircraft battery, the aircraft battery shall be preheated to at least _____.
-20 C
-20 C
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ROTOR LIMITATIONS
- POWER ON POWER OFF
- Transient (12 seconds) 85%
- Minimum Continuous
- GM =< 2000 Kg 96% 80%
- GM > 2000 Kg 96% 85%
- MAX Continuous 104% 104%
- Partial Power (TQ =< 2X30%) 106% -----
- MAX Transient 106% 110%
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Engine Oil Pressure
- Minimum 1.3 bar
- Caution Range 1.3-1.5 bar
- Continuous 1.5-5.0 bar
- MAX Continuous 5.0 bar
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Engine Oil Temperature
- MIN for starting (oil vis. 3 cSt) -45 C
- MIN for power application (oil vis 3 cSt) -10 C
- Maximum Operating Temperature 115 C
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Ventilation Limits (Starter time limits)
- EXT PWR Onboard BATT
- 15 SECONDS ON 20
- 60 SECONDS OFF 60
- 15 SECONDS ON 20
- 23 MINUTES OFF 23
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Maximum Continuous Load Per Generator
Total Maximum Continuous Generator Load
200 A
360 A
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Main Transmission Oil Pressure
- Minimum 1.0 bar
- Caution Range 1.0-1.5 bar
- Continuous 1.5--5.0 bar
- Maximum 5.0 bar
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Main Transmission Oil Temperature
- Continuous Operation -10 to 105 C
- Maximum 105 C
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Fuel Quantity (Usable Fuel)
1530 lbs
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Hydraulic System Quantity
System 1: 1.0 liters
System 2: 1.2 liters (because system 2 is the only one to pressurize the pedals)
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PROHIBITED MANEUVERS
- Full intentional touchdown autorotations
- Flight into icing
- Aerobatic maneuvers
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Rotor Starting and Stopping in High Wind
Up to maximum of 50 knot winds from all horizontal directions
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Hover Turns
- Up to 3200Kg: maximum 45 degrees per second
- Above 3200 Kg: maximum 30 degrees per second
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Main Rotor Mast Moment Limits
- Maximum: RED bar
- Caution: YELLOW region
- Normal: Area LEFT of the Yellow region
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SLOPE LIMITS
- Left Slope: 11 degrees maximum
- Right Slope: 6 degrees maximum (due to mast moment issues)
- Up or Down Slope: 8 degrees maximum
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Operation with open doors (9.1-2)
For operation with opened doors, a certified locking device for the hinged doors and/or the sliding doors must be installed. During single-pilot night flight is is NOT allowed to open or close the pilot's door in flight.
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AFCS (9.2-1)
Maximum airspeed for hands-on operation in CRUISE following an AFCS failure
Maximum airspeed for hands-on operation during ILS APPROACH following an AFCS failure
Glide Slope Mode (GS) shall not be engaged...
120 Knots
100 Knots
Above the Glide Slope
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SPIFR KIT (9.2-8)
Minimum height for hands-off and feet-off operation during takeoff and approach
Minimum height for hands-off and feet-off operation in cases other than takeoff and approach
200 ft AGL
500 ft AGL
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SPIFR KIT (9.2-8)
Minimum Airspeed (Vminl)
Minimum airspeed for Instrument Approach (Vminl, app)
60 KIAS
70 KIAS
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ROTOR BRAKE
The rotor brake shall not be applied until BOTH engines are SHUT DOWN and ROTOR RPM has dropped below 50%.
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Garmin GNS 430 (9.2-43)
Wearing of glasses having POLARIZED lenses could jeopardize the readability of the GNS 430 display.
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MAX TOT for Starting
MAX TOT Transient
785 C, FLI 8.5, Red Outlined Triangle on FLI
865 C, FLI 11.0, Red Triangle on FLI
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AEO (All Engines Operating) Takeoff Power Range
AEO Max TOT
FLI 8.5 to 10.0, 5 minute limit, 71-88% TQ, 845 C.
FLI 10.0, 5 minute limit, 88 %TQ, 845 C.
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OEI (One Engine Inoperative) MAX CONTINUOUS
OEI 2.5 Minute Power
FLI 11.0, 91.5% TQ, 845 C
FLI 12.0, 2.5 minute limit, 125% TQ, 885 C
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AEO MAX TRANSIENT
OEI MAX TRANSIENT
FLI 10.5, 12 second limit, 97% TQ
FLI 14.0, 12 second limit, 140% TQ
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Airspeed limits for Sliding Doors Closed (with various hinged door configurations)
Hinged Doors CLOSED
Spoiler Position Opening/Closing
Spoiler Position Open
Extension Position Opening/Closing
Extension Position Open
Hinged Doors Removed
- Hinged Doors CLOSED Vne
- Spoiler Position Opening/Closing 30 KIAS or Vne
- Spoiler Position Open 100 KIAS or Vne, Rearward Flight 15 kts
- Extension Position Opening/Closing 30
- Extension Position Open 30 kts, Rearward Flight also 30 kts
- Hinged Doors Removed 30 kts
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Airspeed limits for Sliding Doors Opening or Closing
Hinged Doors CLOSED
Spoiler Position Opening/Closing
Spoiler Position Open
Extension Position Opening/Closing
Extension Position Open
Hinged Doors Removed
- Hinged Doors CLOSED 60 kts
- Spoiler Position Opening/Closing 30-60 kts
- Spoiler Position Open 80 kts or Vne
- Extension Position Opening/Closing 30kts
- Extension Position Open 30 kts, Rearward flight also 30 kts
- Hinged Doors Removed 30 kts
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Airspeed limits for Sliding Doors OPEN
Hinged Doors CLOSED
Spoiler Position Opening/Closing
Spoiler Position Open
Extension Position Opening/Closing
Extension Position Open
Hinged Doors Removed
- Hinged Doors CLOSED 60 kts
- Spoiler Position Opening/Closing 30-60 kts
- Spoiler Position Open 100kts or Vne
- Extension Position Opening/Closing 30kts
- Extension Position Open 30 kts, Rearward Flight also 30 kts
- Hinged Doors Removed 30 kts
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Airspeed limits for Sliding Doors REMOVED
HingedDoors CLOSED
Spoiler Position Opening/Closing
Spoiler Position Open
Extension Position Opening/Closing
Extension Position Open
Hinged Doors Removed
- HingedDoors CLOSED 60kts
- Spoiler Position Opening/Closing 30-60 kts
- Spoiler Position Open 100 kts or Vne
- Extension Position Opening/Closing 30kts
- Extension Position Open 30 kts, Rearward Flight also 30kts
- Hinged Doors Removed 30 kts
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