If con di tions per mit, place the twistgrip in the IDLE po si tion once
a land ing area is se lected, and per form a nor mal auto ro ta tion. Plan
to touch down with lit tle or no for ward speed.
WARNING
WHEN HOVERING AT AL TI TUDES WITHIN OR
ABOVE THE CROSS-HATCHED AREAS DE PICTED
ON THE HEIGHT VE LOC ITY DI A GRAM (FIG. 5-2), IT
IS NEC ES SARY TO RE DUCE AL TI TUDE TO 7 FEET
OR LESS PRIOR TO PLACING THE TWISTGRIP IN
THE GROUND IDLE PO SI TION AND PER FORMING
A HOVERING AUTO RO TA TION.
While at a hover: Place the twistgrip in the IDLE po si tion and per form
a hov er ing auto ro ta tion.
Tail Ro tor Con trol Fail ure - Fixed Pitch Set ting:
Ad just power to main tain 50 to 60 knots air speed.
Per form a shal low ap proach and run ning land ing to a suit able area,
touch ing down into wind at a speed be tween ef fec tive translational
lift and 30 knots. Di rec tional con trol may be ac com plished by
small ad just ments in throt tle and/or col lec tive con trol.
3-10. ENGINE IDLE AT AL TI TUDE
En gine idle speeds at high den sity al ti tudes may be less than those set at
sea level con di tions. Do not rap idly re duce throt tle to idle stop in flight.
Emergency Procedures
SCHWEIZER
Model 269C Helicopter
Pilot's Flight Manual
Reissued:
16 Jan 2019
3-7
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This Document contains technical data subject to EAR. See WARNING and classifications on first page.
FAA Approved
CSP Book 1 CSP-C-1.indd 77
8/4/19 12:45 PM
Содержание S300C 269C
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