IP__\'S[2].txt

• 1. Fuel systems(fuel boost pump, transfer pump, external fuel tanks
• 2. Utility receptacle(ext tools etc)
• 3. NIU(remove 70% O2 from air in fuel cells)
• 4. Ice detector probe(pushes air out of the back of the probe creating low pressure suction in front, active in auto mode <5 degress C turns back off > 7 degrees C)
• 5. Window defog
• 6. Hydraulic resevoir(creates backpressure to prevent cavitation and foaming of fluid)
• 7. ATS
• 8. Louver doors(internal on catwalk)
• 9. ECS(only provided in heating mode)
• FUNIWHALE

375 gal.

156 gal

220 gal

100 or 130 gal

1295 gal

• when tank is < 800lbs
• if fwd fuel is >280lbs or if aft is >240lbs
• if >500lbs there is >100lb split
• if <500lbs there is >50lb split
• halts when split is <20lbs

• 1. arm fire extinguisher system
• 2. shuts off fuel flow to indicated engine or APU
• 3. shuts off bleed air from souce
• 4. turns off air partical separator
• 5. closes cooling louvers to affected engine
• 6. turns off voice warning message
• 7. turns off master warning light

4 flight control servoactuators

• 1. utility side 4 flight control servoactuators
• 2. rotor brake
• 3. AWS turret
• 4. tail wheel unlock actuator
• 5. APU start motor
• 6. pylon articulation
• 7. emergency hydraulics

• provide damping for fluid pressure changes, and power:
• 1. rotor brake
• 2. APU start motor
• 3. emergency flight control operation

T/R HYD fail

FMC and BUCS (need electricity AND hydraulics to operate)

• 1. Comparing hover TQ OGE to max TQ DE
• 2. Comparing max GWT OGE to current GWT
• 3. noting the color of hover TQ OGE or MAX GWT OGE

• 1. VMC takeoff (confined area alt over airspeed)
• 2. VMC approach (to an OGE hover)
• 3. Engine failure OGE hover
• 4. Terrain flight (NOE)
• 5. Terrain flight decel
• 6. ITO
• 7. Mask and unmask (unmask at a hover vertically)

• 1. IGE power limited/unavailable takeoff/landing
• 2. Max A/S w/one eng inop

Optional: Height/velocity avoid region

• 1. Major overhaul/repairs
• 2. modifications of 1% or greater of A/C gwt are applied
• 3. modifications (painting) for which weight and CG cannot be accurately computed
• 4. weight/CG data records are suspected to be in error

or if has been 24 months since last weighed

• DECU has/can:
• 1. powered by alternator or A/C power
• 2. MTRA - reduces the risk of exceeding DE TQ limits during uncompensated manuevers
• 3. Hot start prevention - 900 degrees C
• 4. TQ spike suppresion algorithm - locks out TQ signal below 35% NP
• 5. Signal validation for selected input signals w/in electrical system

• 1. ignition exciter
• 2. ECU/DECU power
• 3. NG speed signal

the HMU provides mechanical overspeed protection by the use of flyweights that cut off the fuel flow and occurs at 110% +- 2 NG

the ECU/DECU electronically close a solenoid on the overspeed drain valve cutting off the fuel flow @ 119.6% +- 1 NP

4th stage bleed air pushes oil out of A and B sumps to spray oil mist on the bearings providing 30 seconds of emergency lubrication @ 75% NG

ENG# OIL PSI

• Loss of oil pressure
• Overspeed
• Loss of NG speed
• Overtemp
• Loss of thermocouple
• Overcurrent

• 1. absorbs torque reaction during rotor brake
• 2. prevents shimmy during rolling takeoff/landings
• 3. prevents swivel during slope ops

auxillary isolation valve - closes and denys hydraulics to AWS turret, pylon articulation, and ammo carrier drive

shutoff valve - prevents hydraulic fluid to utility side of directional servoactuators, and tail wheel unlock (aft of tailboom)

• announce IIMC
• transition to instruments bring up flt page
• attitude
• heading
• torque
• airspeed
• trim
• climb to 3500
• contact cairns PAR RWY 6

• yellow = power and control system trim signals
• blue = overspeed and torque signals
• green = engine condition monitoring
• black = ignition exciter