TD 19

Question 1

The first limit indicator (FLI) gives an analogue indication of the limiting parameter associated with the helicopter engine primary limitations for: _______. This indication is completed by the display of digital data for the three parameters. The dial scale of the _______ and does ___ represent a ____ value.

NOTE Even though the rotor is stopped it is possible that due to torque calibration tolerance, a digital torque value of up to ___ is indicated and the needle of first limit indicator is in “0” position. In that case __ corrective action is necessary.

Answer 1

N1 TOT and Torque, analogue display is arbitrary, not, percent,

3%, no

Question 2

The airspeed tendency indicator gives the predicted airspeed after ____ if the acceleration remains constant.
NOTE As airspeed values below ____ are ____, no precise graduations are
shown below this figure.

Answer 2

5 secs, 20 KIAS, unreliable

Question 3

Compressor stall
Conditions/Indications
– Popping \_\_\_\_
– Torque and N1 indications may \_\_\_\_
– TOT may \_\_\_\_
– Slight yaw \_\_\_\_
Procedure
1. Collective lever – 
2. Engine instruments – 
3. Collective lever – 
If compressor stall returns:
4. Affected engine – 
5. Single engine emergency shutdown – 
6. LAND AS SOON AS

Answer 3

Compressor stall
Conditions/Indications
– Popping sounds
– Torque and N1 indications may decrease
– TOT may increase
– Slight yaw jerk
Procedure
1. Collective lever – Lower
2. Engine instruments – Monitor
3. Collective lever – Raise slowly
If compressor stall returns:
4. Affected engine – Identify (TOT)
5. Single engine emergency shutdown – Perform
6. LAND AS SOON AS PRACTICABLE

Question 4

LAND IMMEDIATELY

Answer 4

The urgency of landing is paramount. Primary considerations is to assure survival of the occupants. Landing in water, trees, or other area should be considered only as a last resort

Question 5

LAND AS SOON AS POSSIBLE

Answer 5

Land without delay at the nearest adequate site (i .e. open field) at which a safe approach and landing can be made

Question 6

LAND AS SOON AS PRACTICABLE

Answer 6

The landing site and duration of flight are at the discretion of the pilot. Extended flight beyond the nearest landing area where appropriate assistance can be expected is not recommended

Question 7

SINGLE ENGINE EMERGENCY SHUTDOWN

Answer 7

1. Twist grip (affected engine) - rotate slowly to idle, check indications, then to OFF
2. Rotor speed - trim to maximum
   Bleed air heating (if installed) will be shutdown automatically, however, depending on power margin of remaining engine, may be re-engaged as follows:
3. BLD HTG EMER/NORM SW - EMER
4. BLD HTG Rheostat - ON

Question 8

DOUBLE ENGINE EMERGENCY SHUTDOWN

Answer 8

ON GROUND

1. Both twist grips - OFF
2. Both FUEL PRIME PUMP sw - OFF
3. BAT MSTR sw - OFF

IN FLIGHT
1. Both twist grips - OFF
If there is an indication that the engines are still running
2. Both EMER OFF sw - Press