Question 1
Question
Single engine failure - flight
Procedure
1. OEI flight condition - [blank_start]Establish[blank_end]
2. Rotor speed - [blank_start]Trim to maximum[blank_end]
3. Affected engine - [blank_start]Identify[blank_end]
4. Single engine emergency shutdown - [blank_start]Perform[blank_end]
5. [blank_start]LAND AS SOON AS PRACTICABLE[blank_end]
Question 2
Question
Single engine failure - hover OGE Flight
Procedure
1. Collective lever – [blank_start]Adjust to maintain rotor RPM[blank_end]
2. Airspeed – [blank_start]Increase if possible[blank_end]
TRANSITION TO OEI - FLIGHT
3. Collective lever – [blank_start]Adjust to OEI-limits or below[blank_end]
4. Rotor speed – [blank_start]Trim to maximum[blank_end]
5. Airspeed – [blank_start]Gain[blank_end], [blank_start]65[blank_end] KIAS (VY)
After reaching safe altitude:
6. Collective lever – [blank_start]Reduce to OEI MCP or below[blank_end]
7. Affected engine – [blank_start]Identify[blank_end]
8. Single engine emergency shutdown – [blank_start]Perform[blank_end]
9. [blank_start]LAND AS SOON AS PRACTICABLE[blank_end]
Answer
-
Adjust to maintain rotor RPM
-
Increase if possible
-
Adjust to OEI-limits or below
-
Trim to maximum
-
Gain
-
65
-
Reduce to OEI MCP or below
-
Identify
-
Perform
-
LAND AS SOON AS PRACTICABLE
Question 3
Question
Single engine failure - hover OGE Landing
Procedure
1. Collective lever – [blank_start]Adjust to maintain rotor RPM[blank_end]
2. Airspeed – [blank_start]Increase if possible[blank_end]
FORCED LANDING
3. Landing attitude – [blank_start]Establish[blank_end]
4. Collective lever – [blank_start]Raise as necessary[blank_end] to [blank_start]stop descent and cushion landing[blank_end]
After landing:
5. Affected engine – [blank_start]Identify[blank_end]
6. Single engine emergency shutdown – [blank_start]Perform[blank_end]
Question 4
Question
Autorotation
Procedure
1. Collective lever – [blank_start]Reduce to maintain NRO within limits[blank_end]
2. Airspeed – [blank_start]75 KIAS recommended[blank_end]
3. Double engine emergency shutdown – [blank_start]Perform[blank_end]
8. BAT MSTR sw – [blank_start]OFF[blank_end]
Question 5
Question
Tail Rotor Drive Failure/Fixed-pitch Tail Rotor Control Failure - Forward Flight
Procedure
1. Collective lever – [blank_start]Reduce to obtain minimum sideslip angle[blank_end]
2. Airspeed – [blank_start]Maintain 70 KIAS or higher[blank_end]
3. Suitable landing area – [blank_start]Select[blank_end]
4. Shallow approach with nose left – [blank_start]Perform[blank_end]
5. Airspeed – [blank_start]Reduce close to the ground[blank_end] until [blank_start]nose is aligned[blank_end] with [blank_start]the flight direction[blank_end]
6. Landing – [blank_start]Perform[blank_end]
If the nose direction changes from left to right at airspeeds higher than 40 kts:
5. Airspeed – [blank_start]Increase[blank_end]
6. Approach – [blank_start]Abort[blank_end], [blank_start]climb to sufficient height[blank_end] for [blank_start]autorotation[blank_end]
7. Autorotation – [blank_start]Perform[blank_end]
Answer
-
Reduce to obtain minimum sideslip angle
-
Maintain 70 KIAS or higher
-
Perform
-
Select
-
Reduce close to the ground
-
nose is aligned
-
the flight direction
-
Perform
-
Increase
-
Abort
-
climb to sufficient height
-
autorotation
-
Perform
Question 6
Question
Engine underspeed – governor failure
Procedure
1. OEI flight condition – [blank_start]Establish[blank_end]
2. Bleed air consumers – [blank_start]Off[blank_end]
3. VAR NR system NORM/MAN pb – [blank_start]Check MAN[blank_end]
4. Affected engine – [blank_start]Identify[blank_end]
5. N2 TRIM sw – [blank_start]Compensate N2/NRO drop[blank_end] and [blank_start]try to match torque[blank_end]
If torque match is not possible:
6. Twist grip (affected engine) – [blank_start]Release stop plate[blank_end] and [blank_start]rotate towards FLIGHT[blank_end] until [blank_start]N2 and NRO stabilize in normal range[blank_end] and [blank_start]FLI needles match[blank_end]
7. [blank_start]LAND AS SOON AS PRACTICABLE[blank_end]
If no residual torque (affected engine) is available:
8. Single engine emergency shutdown – [blank_start]Perform[blank_end]
Question 7
Question
WARNING LIGHT INDICATIONS - FIRE (ENGINE 1 or ENGINE 2) - On Ground
Procedure
1. [blank_start]FIRE sw (affected engine)[blank_end] – [blank_start]Raise guard[blank_end], [blank_start]press[blank_end]
NOTE Affected engine will shut down automatically, ACTIVE indicatior light, BOT 1
legend (both EMER OFF SW pnl), and F VALVE CL caution indication (CAD)
come on. FIRE legend remains on as long as overheat condition exists.
2. [blank_start]Both FUEL PRIME PUMPS[blank_end] – [blank_start]Check OFF[blank_end]
3. [blank_start]BOT 1/BOT 2 pb[blank_end] – [blank_start]Press[blank_end]; [blank_start]bottle 1 activated[blank_end]; – [blank_start]EXT indicator light comes on[blank_end] ([blank_start]EMER OFF SW pnl[blank_end])
NOTE Extinguisher bottle will begin discharging when N1t 50%. After discharge of
bottle contents, BOT 1 legend and EXT indicatior light go off; BOT 2pb legend
comes on.
4. [blank_start]Clock stop watch[blank_end] – [blank_start]Start[blank_end] ([blank_start]after BOT 1 legend[blank_end] and [blank_start]EXT indicator light go off[blank_end]
([blank_start]EMER OFF SW pnl[blank_end])
5. [blank_start]Double engine emergency shutdown[blank_end] – [blank_start]Perform[blank_end]
6. Passengers – Alert/Evacuate
If situation permits and FIRE warning is still on after 1 minute:
7. [blank_start]BOT 1/BOT 2 pb[blank_end] – [blank_start]Press[blank_end]; [blank_start]bottle 2 activated[blank_end]; – [blank_start]EXT indicator light comes on[blank_end] ([blank_start]EMER OFF SW pnl[blank_end])
8. BAT MSTR sw – OFF
Answer
-
Raise guard
-
press
-
Check OFF
-
Press
-
bottle 1 activated
-
EXT indicator light comes on
-
EMER OFF SW pnl
-
Start
-
after BOT 1 legend
-
EXT indicator light go off
-
EMER OFF SW pnl
-
Perform
-
Press
-
bottle 2 activated
-
EXT indicator light comes on
-
EMER OFF SW pnl
-
FIRE sw (affected engine)
-
Both FUEL PRIME PUMPS
-
BOT 1/BOT 2 pb
-
Clock stop watch
-
Double engine emergency shutdown
-
BOT 1/BOT 2 pb
Question 8
Question
WARNING LIGHT INDICATIONS - FIRE (ENGINE 1 or ENGINE 2) - In Flight
Procedure
1. [blank_start]OEI flight condition[blank_end] – [blank_start]Establish[blank_end]
2. [blank_start]Airspeed[blank_end] – [blank_start]Reduce if IAS is exceeding 100 kts[blank_end]
3. [blank_start]FIRE sw (affected engine)[blank_end] – [blank_start]Raise guard[blank_end], [blank_start]press[blank_end]
NOTE Affected engine will shut down automatically, ACTIVE indicatior light, BOT 1
legend (both EMER OFF SW pnl), and F VALVE CL caution indication (CAD)
come on. FIRE legend remains on as long as overheat condition exists.
4. [blank_start]BOT 1/BOT 2 pb[blank_end] – [blank_start]Press[blank_end]; [blank_start]bottle 1 activated[blank_end]; – [blank_start]EXT indicator light comes on[blank_end] ([blank_start]EMER OFF SW pnl[blank_end])
NOTE Extinguisher bottle will begin discharging when N1t 50%. After discharge of
bottle contents, BOT 1 legend and EXT indicatior light go off; BOT 2pb legend
comes on.
5. [blank_start]Clock stop watch[blank_end] – [blank_start]Start[blank_end] ([blank_start]after BOT 1 legend[blank_end] and [blank_start]EXT indicator light go off[blank_end]) ([blank_start]EMER OFF SW pnl[blank_end])
6. [blank_start]Affected engine[blank_end] – [blank_start]Identify[blank_end]
7. Single engine emergency shutdown – [blank_start]Perform[blank_end]
8. Passengers – Alert
9. [blank_start]LAND AS SOON AS POSSIBLE[blank_end]
If FIRE warning is still on after 1 minute:
10. [blank_start]BOT 1/BOT 2 pb[blank_end] – [blank_start]Press[blank_end]; [blank_start]bottle 2 activated[blank_end]; – [blank_start]EXT indicator light comes on[blank_end] ([blank_start]EMER OFF SW pnl[blank_end])
If FIRE warning remains on:
11. [blank_start]LAND IMMEDIATELY[blank_end]
Answer
-
Establish
-
Reduce if IAS is exceeding 100 kts
-
Raise guard
-
press
-
Press
-
bottle 1 activated
-
EXT indicator light comes on
-
EMER OFF SW pnl
-
Start
-
after BOT 1 legend
-
EXT indicator light go off
-
EMER OFF SW pnl
-
Identify
-
Perform
-
LAND AS SOON AS POSSIBLE
-
Press
-
bottle 2 activated
-
EXT indicator light comes on
-
EMER OFF SW pnl
-
LAND IMMEDIATELY
-
OEI flight condition
-
Airspeed
-
FIRE sw (affected engine)
-
BOT 1/BOT 2 pb
-
Clock stop watch
-
Affected engine
-
BOT 1/BOT 2 pb
Question 9
Question
Engine overspeed – governor failure
Procedure
1. Collective lever – [blank_start]Raise as necessary[blank_end] to [blank_start]maintain N2 and NRO within limits[blank_end]
2. VAR NR system NORM/MAN sw – [blank_start]Check MAN[blank_end]
3. N2 TRIM sw – [blank_start]Try to trim NRO[blank_end] to [blank_start]101[blank_end]% [blank_start]with matched torque[blank_end]
If step 3. is not possible:
4. Affected engine – [blank_start]Identify[blank_end]
5. Twist grip (affected engine) – [blank_start]Rotate towards IDLE[blank_end] until [blank_start]N2 and NRO stabilize in normal range[blank_end] and [blank_start]FLI needles match[blank_end]
6. [blank_start]LAND AS SOON AS PRACTICABLE[blank_end]
Answer
-
Raise as necessary
-
maintain N2 and NRO within limits
-
Check MAN
-
101
-
Try to trim NRO
-
with matched torque
-
Identify
-
Rotate towards IDLE
-
N2 and NRO stabilize in normal range
-
FLI needles match
-
LAND AS SOON AS PRACTICABLE