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51 Cards in this Set
- Front
- Back
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TGT Limits (DECU)
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TGT Limits (EDECU)
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Nr Limits
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Dual Engine Torque Limits (<80 KIAS)
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Single Engine Torque Limits
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Dual Engine Torque Limits (>80 KIAS)
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Ng Limits
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Transmission Temp Limits
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Transmission Press Limits
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Engine Oil Temp Limits
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Engine Oil Press Limits
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Engine Starter Limits
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Minimum Planned Fuel on Landing
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Minimum planned fuel on landing shall be no less than 225 pounds (approximately 20 minutes) of fuel per main tank. With fuel less than 300 pounds per main tank, maintain balanced flight at Angles Of Bank (AOBs) greater
than 30°. |
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Maximum wind velocity for rotor engagement or disengagement
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45 knots from any direction
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Max Airspeed: Autorotation
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100 KIAS.
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Max Airspeed: Sideward/rearward flight
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45 knots (35 knots with external load).
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Max Airspeed: Two SAS inoperative in IMC
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125 KIAS.
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Max Airspeed: SAS/BOOST OFF
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140 KIAS.
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Max Airspeed: Either PRI SERVO PRESS caution
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125 KIAS
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Max Airspeed: Cabin doors opening/closing
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100 KIAS
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Max Airspeed: Cabin doors open
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120 KIAS
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Max Airspeed: Gunner windows opening/closing
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170 KIAS
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Max Airspeed: Landing light in transition
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130 KIAS
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Max Airspeed: Searchlight in transition
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100 KIAS
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Max Airspeed: Aircraft gross weight >22,000 pounds with an external load
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120 KIAS
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Maximum rate of descent with recue hoist loads
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1,000 fpm.
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Max AOB: Normal operations
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45°.
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Max AOB: Operations above 10,000 feet DA
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30°.
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Max AOB: Either PRI SERVO PRESS caution ON
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30°.
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Max AOB: SAS/BOOST OFF flight
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30°.
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Maximum operating density altitude
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13,000 feet.
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Prohibited Maneuvers
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1. Aerobatic flight.
2. Hovering turns at a rate in excess of 30° per second. 3. Practice full-autorotation landings. 4. Intentional approaches into or inducement of retreating blade stall. |
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Maximum rotor speed for rotor brake application
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76 percent Nr.
Routine rotor stops shall be made between 30 and 50 percent Nr. Routine rotor brake stops should be limited to 180 psi to extend service life. |
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Maximum wind velocity for blade fold and spread
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45 knots from any direction.
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Required cooling period for blade fold.
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Following a complete blade fold and spread cycle, allow a 10-minute cooling period before commencing another blade fold and spread evolution.
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Maximum wind velocity for tail pylon or stabilator fold/spread operations
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45 knots from any direction
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Maximum rate of descent for level terrain
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540 fpm
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Maximum rate of descent for sloped terrain
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360 fpm
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Maximum touchdown and takeoff speed
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60 KGS with tailwheel locked and 20 KGS with tailwheel unlocked.
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Maximum braking speed
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35 KGS.
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Slope landing limitations:
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9° nose-up slope.
12° cross-slope. 6° nose-down slope. |
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Maximum operating gross weight
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23,500 pounds
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Maximum launch and recovery gross weight
for aviation ships |
23,500 pounds.
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Maximum launch and recovery gross weight for air-capable ships
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22,500 pounds.
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Maximum internal weight limits
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Cabin area aft of the cockpit (to include aircrew, passengers, and/or cargo)
is 5,500 pounds. The maximum total weight for palletized cargo is 4,733 pounds. The maximum weight for a single pallet of cargo is 3,000 pounds. |
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Maximum external load when employing the cargo hook
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8,000 pounds.
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Maximum external load when
employing the rescue hoist |
600 pounds.
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Operating Temp Limits
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Operations at temperatures below -40 °C (-40 °F) or above 60 °C (140 °F) are prohibited
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APU Limits (Rotors Static)
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APU may be operated continuously up to an ambient temperature limit of 51 °C.
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APU Limits (Rotors Engaged)
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APU may be operated continuously up to an ambient temperature limit of 43 °C. If operating the APU between 43° and 60 °C, operation is limited to 30 minutes.
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Backup Pump Limits
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