Engine failure in HIGE
Eng Fail in take off
Eng Fail in HOGE
Eng Fail in Cruise
Engine Restart in Flight
Autorotative Landing
At approximately 150’
1. Cyclic - Flare to reduce forward speed
At approximately 20-30’ AGL
2. Collective increase to reduce rate of descent
3. Cyclic - forward to obtain skid level attitude
4. Collective - Continue application to cushion the touchdown
5. Pedals - maintain direction
6. Emergency shutdown - complete
Caut: if you contact on aft skid don’t counteract the pitch down with cyclic
Eng Oil Px Low
Eng oil px below 40 psi or 40-80 psi and decreasing
1. Reduce power
2. Monitor engine parameters
3. Land as soon as possible
warning: may result in eng fail
note: eng oil px may enter cautionary range during practice autos
Eng Oil Temp Hi
Abort Start
Eng Compressor Stall
warning: may result in eng fail
note: if you have power but can’t maintain level flight, use the power you have to get to a good landing site or land well
Overspeed
Malfunction of FCU
if fuel control system malfunction causes an increase in power (overspeed)
1. Twist Grip - Reduced until Nr/N2 are in normal range
2. Collective/Twist Grip - coordinate
3. Land as soon as possible
Warn: N1 decreasing below 51% will cause flameout
Note: overspeed may result in EEC fail
Underspeed
Malfunction of FCU
if fuel control sys causes decrease in power (underspeed)
1. Collective - lower to maintain Nr
2. Man/Nor selector - man
3. Twist Grip - slowly rotate toward max, as required
4. Collective/Twist Grip - coordinate
5. Land as soon as possible
Warn: rapid twist grip movement may result in exceedance
N1 below 51% will cause flameout
Eng RGB chip
Eng AGB Chip
XMSN Malfunction
if failure is imminent
1. land immediately
if failure is not imminent
2. reduce power
3. monitor transmission parameters
4. land as soon as possible
warn: Possible indications of imminent transmission failure may include: yaw attitude excursions with no control input, an increase in power required for a fixed collective setting, increased noise,
increased vibrations, or abnormal fumes.
note: transit min power required airspeed at low alt to effect a quick flare and immediate landing in event of imminent failure
XMSN Chip
If xmsn chip message illuminated
1. Check for secondary indications
if secondary indications exist
2. Transmission malf EP - perform
If no secondary indications:
3. Chip burner sw- activate and release
4. Transmission malfunction EP - perform
use of chip burner sw when relative oil px is below limits is prohibited
note: no chip burner on ground, chip burner only 3x per flight
Loss of T/R thrust in a hover
Loss of T/R thrust in cruise flight
Tail Rotor Chip
Hyd Sys #1 or #2 px loss
Batt Temp Hi
Emergency DC bus fail
Fuel Pump 1 and/or fuel pump 2 fail
if both pumps fail with 0 psi:
1. land as soon as possible
Eng Fire in flight