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ASTAR B3 EPS/LIMITS
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ENG P
- Reduce Power
- Check oil pressure
If Low or zero, shut down ENG
- AUTOROTATE
If pressure is correct:
- LAND AS SOON AS POSSIBLE
MGB TEMP
- Check MGB P Light
Not Illuminated:
- Reduce Power
- LAND AS SOON AS POSSIBLE
MGB P
- Reduce Power
- LAND AS SOON AS POSSIBLE
GOV
GOV Manual
- Avoid Abrupt PWR Changes
- Make small amplitude adjustments to Twist Grip
- Maintain NR in green range
- Fly approach at 40 KTS
- Land As Soon As Practical(After Landing Retard Throttleprior to Lowering Collective)
ENG FIRE
- AUTOROTATE
- Close Fuel Shut-off
- Gen
: Off- Electric Master All
- Off
: Off If you smell smoke
VEMD Failure Both Screens
- IAS 100 KTS @ 0 PA2 Kts per 1000 PA
- LASA PRACTICAL Without hovering
HYDR
- Set IAS 40 to 60 KTS(50 Kts Ideal)
- Collective HYD Switch - Off
- Make Shallow Approach
- Land with slight FWD A/S
- Land As Soon As POSSIBLE
Engine Oil Temp High
(Above 115C)
- Reduce A/S to 80 KTS
- Check for cooling
If Not Cooling
:
- Land As Soon As POSSIBLE
- Stop ENG Check Oil Cooler Fan for Operation
ENG CHIP
- Land As Soon As POSSIBLE
- Inspect chip plug
T/O Prohibited until specific maintenance checks complete
MGB CHIP
- Reduce ENG Power
- Monitor MGB P / MGB T Lights
- Land As Soon As PRACTICAL
TGB CHIP
- Continue Flight avoiding prolonged hovering
- Land As Soon As PRACTICAL
GENE
(DC Generator Failure)
- Test DC Voltage
- Reset Gen Switch
If Unsuccessful
:
- Shed unnecessary Circuits
BATT
(Battery no longer charging)
- Check Battery On
- Reset GEN
Keep Watch on Voltage
- Continue Flight Based on Situation
GOV
(Gov Function Degraded)
- Avoid abrupt power variations - LASA PRACTICAL
TWT GRIP
If necessary return twist grip to “Flight” VOL position
FUEL FILT
- Reduce ENG power
If light goes out:
- Continue at Reduced Power
If light remains on
:
- Land As Soon As POSSIBLE
FUEL P
(Fuel Pressure Drop Risk of Flame out)
- Reduce ENG power
- Boost Pump On
- Land As Soon As POSSIBLE
FUEL
(Fuel Quantity < 15.8 GAL)
- Avoid large attitude changes
- Boost Pump ON
Approximately 18 min. fuel remain at level flight
Tail Rotor Drive Failure
In FWD Flight:
- Reduce power to maintain Forward speed(Weathercock Effect)
- Set up Steep Approach
- On final 500’ – Shut Off Eng - AUTOROTATE
OR
- Shallow Approach Run-On Landing
Tail Rotor Control Failure
- Airspeed 70 KIAS
- Hyd. Accumulator Test - Push
- After 5 seconds - Reset
- Make shallow App to Run on Landing
(Best
: Rt Cross Wind w/speed < 20 Kts @ touchdown)
Author
navypilot29
ID
240901
Card Set
ASTAR B3 EPS/LIMITS
Description
ASTAR B3 EPS/LIMITS
Updated
2013-10-16T12:30:44Z
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