10.06 meter
11,66 meter
Lycoming 0-540-F1B5, sex cylindrig, horizontal opposed, direct drive, aircooled, carburetted, normally aspirated
speed for best rate of climb
stabilized level flight speed at maximum continus power
indikerad höjd när altimetern är satt på 1013
indikerad höjd när altimetern är satt till rådande QNH
100 inches framför rotor shaft centerline
general
Limitations
Power off Vne
100 KIAS
100 KIAS
120 KIAS
130 KIAS
100 KIAS
7 qt
2400 lb (1089 kg)
1550lb (703 kg)
136 kg
23 kg
68 kg
bak med cyclic för att belasta rotorn innan man häver rollen
14000 feet
9000 fot pga möjlighet att landa vid brand inom 5 min
alternator
RPM govenor
low roror rpm warning system
OAT gage
hydraulic control system
landing lights
navigation lights
instrument light
anti collision lights
112 liter
64 liter
176 liter
25 psi
+1,6 in
Emergency procedures
Land on nearest clear area where safe normal landing can be performed. be prepared to enter autorotation during approach, if required.
Landing site is at pilots discreriin based on nature of problem and availible landing areas. Flight beond nearest airport is not recommended.
Low RPM horn
change in noise level
nose left yaw
oil pressure light
decreasing engine PRM
unusual noise or vibration
nose right or left yaw
decreasing rotor PPM while engine RPM is increasing
90 KIAS, Rotor rpm 90%
55 KIAS, Rotor RPM approximatley 90%
97%
lateral cyclic
nose right yaw which cannot be corrected by applying left pedal
Immediatly ener autorotation
Maintain 70 KIAS if practical (hjälper till att hålla nosen rak)
select landing site
roll thottle into overtravel spring, and perform autorotation landing
lnd as soom as practical, pilot will not hear liw RPM horn with failed headset.
fuel mixure off
fuel valve off
battery swich off
rotor brake, if time permits
exit helicopter
enter autorotation
cabin heat-OFF
cabin vent -ON
ENGINE RUNNING
- perform normal landing, then fuel valve/mixure OFF
ENGINE STOPS
-fuel valve OFF and complete autorotation landing
battery swich -OFF
rotorbrake
exit helicopter
Battery and Alternator -OFF
open cabin vents
land immediatley
fuel mixure OFF and fuel valve OFF
if time permits apply rortobrake
exit helicopter
Low PPM system
Governor
allow govenor to control rpm,
Land as soon as practical
samtliga har separata power circuits.
en special citcuit gör så att batteriet kan förse tachs med ström även fastän BATT/ALT är OFF.
-är dock batteriet slut, fungerar inte tachs!!
tillfällig eller konstant vibrationer i controls
Verify HYD- ON
If hyd not restored- HYD-OFF
adjust airspeed and flight vondirion as desired for comfortable control.
Land as soon as practical
Grip throttle firmly to override govenor,
switch hovenor off
complete flight using manual throttle control
Lampan indikerar loss of engine power or oil pressure.
kolla tach för powerloss.
kolla oil pressure gage- om trycket är lågt - landa direkt!
om lampan tänd och noise,vibration, temp raise occurs- Land immediatly
om ingen annan indikation, land as soom as practical.
3 gallons( 11 Liter), max 10 min i cruise power
låt ej lysa mer än 10 sek, dra cuircut breaker vid 9
indicates low voltage and possible alternator failure.
turn off all non essential electroc equioment and switch ALT OFF and back ON to reset alternator control unit.
it lightstays on, land as soon as practical.
-fortsatt föygning utan alternator kan resultera i att batteriet dras ur och tachometerna slutar fungera som kan ge farliga flygsituationer.
indikerar att startmotorn jobbar.
if light not go out after ignition swich is relesed from start position, immediatly pull mixture off and tyrn off battery swich off. Have starter motor serviced.
indikerar rotorvarv under 97%
sänk omedelbart collective, apoly aft cyclic.
Light is disabled when collective is full down.
shut of heater
open nose and side vent doors
om huvudvärk, ysel i samband med light, land immediatly.
indicates engine near full throttle. Govenor will br inefective beacuse can not increase throttle to maintain RPM.
Lower collective as required to extringuish light.
60 KIAS
60 KIAS
55 KIAS
100 KIAS
60-70 KIAS
110 KIAS
60 KIAS
60-70 KIAS
fine blackish powder
engine RPM below 80%
OAT -4c och +30c och skillnad mellan dewpoint och OAT med än 15 grader
fenerally occurs when airspeed is below 100 KIAS. Use fairly sterp approach until saitspeed is below 65KIAS
notmal procedures
performance
weight and balance
system descriotion