Fire - Kazan Helicopters Mi-17-1V Flight Manual

MI1-17-1B. Flight manual
6) After touchdown push the collective pitch control lever fully
down with simultaneous application of the control stick 1/3 to
1/4 full travel forward and apply the LG wheel brakes.
(d)
In case of failure of both engines at altitude below 100 m and air-
speed below 80 km/h proceed as follows:
1) Immediately push the collective pitch control lever fully down
and, if the altitude allows, accelerate up to a speed of 50 to 60
km/h.
2) Shut down the engines by closing the HP fuel shutoff valves,
give an order to the Flight Engineer to close the fuel fire shut-
off valves and switch off the fuel booster and transfer pumps.
3) At a height of 15 to 20m initiate reducing the vertical speed by
rapid and continuous increase of the collective pitch at the
maximum possible rate (10 to 12 deg/s).
4) After touchdown push the collective pitch control lever fully
down with simultaneous application of the control stick 1/3 to
1/4 full travel forward.
(e) When landing on wood, water or swamp, or if some other obstacles
are present, continue pre-landing deceleration at a pitch angle of 15
to 25° until slowing down of the vertical speed by increasing of the
main rotor collective pitch is initiated and, in case of necessity,
touch down at the pitch angle used for deceleration.
6.3. Fire
(1) Indications
(a) Illumination of the FIRE (nO>KAP) annunciator on the left instru-
ment panel and the red warning annunciator on the pilots' overhead
panel center subpanel (the fire protection system control panel) in-
dicating the area of fire: L ENG FIRE (nO>KAP nEB. ,[lB.). R ENG
FIRE (nO>KAP nPAB. ,[lB.), COMBUST HTR FIRE (nO>KAP KO-50),
APU GEAR FIRE (nO>KAP PE,[IYK. AVl-9).
(b) The PVl-65 information reporting system gives voice warning:
"Fire in ... compartment".
(c) Appearance of smoke, flame or burning smell in the flight compart-
ment.
When indications of fire appear recognize the fire zone by means of
the fire warning annunciator, voice warning of the PVl-65 informa-
tion reporting system or visually.
(2) Upon occurrence of fire in the left or right engine compartments the FIRE
(nO>KAP) master annunciator and red L ENG FIRE (nO>KAP nEB. ,[lB.)
or R ENG FIRE (nO>KAP nPAB. ,[lB.) annunciators come on. Simultane-
ously, the main discharge (1-st shot) fire extinguishers discharge auto-
matically fire extinguishant into the affected engine compartment, which
is indicated by illumination of the amber MAIN DISCH (1 04EPE,[Ib) an-
nunciator of the respective compartment.
(3) Crew's actions
(a) After the L ENG FIRE (nO>KAP nEB. ,[lB.) or R ENG FIRE (nO>KAP
np. ,[lB.) annunciator become illuminated on the fire protection sys-
tem control panel the Captain should proceed as follows:
1) Shut down the engine whose compartment Is on fire by the
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