Mooney M20TN S type, Руководство по эксплуатации для пилотов

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MOONEY
M20TN - MODEL TYPE-S
SECTION III
EMERGENCY PROCEDURES
3 -- 11
AIRPLANE FLIGHT MANUAL
ORIGINAL ISSUE -- 04-02-2008
be less for a given propeller RPM compared to the primary induction air system. This is due to
loss of ram effect and induction of warmer inlet air.
The following check list should be used if a partial power loss due to primary induction air sys-
tem blockage is experienced:
Alternate Air Verify OPEN (annunciator light ON) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Manifold Pressure 1 -- 2 inches less than normal, due to warm induction air . . . . . . . . . . . . . . .
NOTE:
The alternate air door should open automatically when primary induction system
is restricted. If alternate air door has not opened (Annunciator light--OFF) it can
be opened manually by pulling alternate air control.
Throttle INCREASE as desired . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Propeller INCREASE as required . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
to maintain desired cruise power setting (Ref. SECTION V) . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Mixture RELEAN to desired EGT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Flight CONTINUE -- request altitude with warmer air, if able . . . . . . . . . . . . . . . . . . . . . . . . . . . .
In the unlikely event that a total power loss , due to primary engine induction air blockage, is
experienced, the following checklist should be used:
Airspeed BEST GLIDE SPEED . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
3368 lb./1528 kg 91.5 KIAS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
3200 lb./1452 kg 89.0 KIAS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
2900 lb./1315 kg 84.5 KIAS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
2600 lb./1179 kg 80.0 KIAS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Alternate Air Manually OPEN . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
LOW Boost Pump ON . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Throttle SET TO HALF OPEN . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Propeller FULL FORWARD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Mixture PULL TO CUTOFF, THEN GRADUALLY RICHEN UNTIL ENGINE STARTS . . . . . .
Magneto/Starter Switch Verify on BOTH . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
After engine re--start:
Throttle
ADJUST as required . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Propeller ADJUST as required . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Mixture RELEAN as required for power setting . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
(Refer to power charts -- SECTION V) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
LOW Boost Pump
OFF . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
If engine does not re--start after several attempts, maintain best glide speed & proceed to
FORCED LANDING EMERGENCY .
TURBOCHARGER FAILURE
--WARNING--
If turbocharger failure is a result of a loose, disconnected or burned through ex-
haust, than a serious fire hazard exists. If a failure in the exhaust system is sus-
pected in flight, shut down the engine and LAND AS SOON AS POSSIBLE. If a
suspected exhaust system failure occurs before takeoff, DO NOT FLY THE AIR-
CRAFT.
Turbocharger failure may be evidenced by the inability of the engine to develop manifold air
pressure above the ambient pressure. The engine will revert to “normally aspirated” mode and
can be operated but will produce less than rated horsepower. If turbocharger failure occurs be-
fore takeoff, do not fly the aircraft. If a failure occurs in flight, readjust mixture as necessary to
obtain fuel flow appropriate to manifold air pressure and RPM.