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[su_spoiler title=”Pilot Operating Handbook – POH” style=”fancy” center=”yes” icon=”arrow”]
دانلود POH ساوانا اس
[su_button url=”http://mahtabal.com/POH%20-%20Savannah.pdf” target=”blank” style=”flat” background=”#3650c1″ size=”10″ center=”yes” radius=”5″ icon=”icon: download” desc=”دانلود فایل”][/su_button][/su_spoiler]
[su_spoiler title=”عکس از سه نما ساوانا اس” style=”fancy” icon=”arrow”]
برای بزرگنمایی روی عکس کلیک نمایید
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[su_spoiler title=”ساختار ساوانا اس” style=”fancy” icon=”arrow”]
– The Savannah™ S is a monoplane type, with two side-by-side seats, fitted with a high wing supported by struts.
– The airframe structure is a full-metal one with load-resisting panels.
– The wing presents a “high lift” NACA 650-18 modified airfoil with Junkers type flaperon (aileron + flap) with manual or electrical (optional) control.
– Trim with electrical control on the elevator and with manual control on the rudder.
– It’s possible to install a parachute “Junkers 500” type.
– The tanks are installed into the wings and have 36 litres capacity each. They are communicating and flow into a collection sump, placed in the fuselage, provided with drain valve and with fuel reserve indicator connected to a push-to-test light.
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[su_spoiler title=”ساختار موتور و ملخ ساوانا اس” style=”fancy” icon=”arrow”]
– The engine cowling is completely removable to permit an easier engine van inspection.
– On the upper cowling has been inserted a little door that allows an easy inspection of the oil level.
– It’s possible to choose between two different engines:
Rotax 912 UL 2 – 80 Hp with two-blade prop “Duc” with adjustable pitch on the ground;
Rotax 912 ULS 2 – 100 Hp with three-blade prop “Duc” with adjustable pitch on the ground;
– The nose is completed with a glass fiber spinner 260 mm diameter.
– The new ring engine mount, that supports the engine by the rear, makes possible to have less vibrations.
– The fuel system is provided with an additional electric pump shielded anti-heat.
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[su_spoiler title=”IPC – Illustrated Part Catalog” style=”fancy” icon=”arrow”]
[su_button url=”http://mahtabal.com/wp-content/uploads/2022/07/2014.11.27-Spare-parts-catalogue-Savannah-S.pdf” target=”blank” style=”flat” background=”#3650c1″ size=”10″ center=”yes” radius=”5″ icon=”icon: download” desc=”دانلود فایل”][/su_button]
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[su_spoiler title=”مشخصات ساوانا اس” style=”fancy” icon=”arrow”]
برای بزرگنمایی روی عکس کلیک نمایید
[su_custom_gallery source=”media: 7134″ link=”image” target=”blank” width=”640″ height=”330″]
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[su_spoiler title=”کاتالوگ ساوانا اس” style=”fancy” icon=”arrow”]
[su_button url=”http://www.icpaviazione.it/wp-content/uploads/2015/04/Pieg_ENG.pdf” target=”blank” style=”flat” background=”#3650c1″ size=”10″ center=”yes” radius=”5″ icon=”icon: download” desc=”دانلود فایل”][/su_button]
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[su_spoiler title=”Savannah Service Bulletin” style=”fancy” icon=”arrow”]
SB 01-2001 Replacement of aileron and steering wheel control rods
SB 02-2001 Replacement of drums
SB 01-2002 Front wheel axle on Bingo
SB 02-2003 Introduction of a new silent-block for engine Rotax 912 ULS
SB 03-2003 Introduction of a new silent-block for engine Rotax 503 & 582
SB 05-2003 Installation kit of the retention bungee for spark plug for Bingo
SB 03-2004 Remove the spacer ring inside the rubber junction of carburetor
SB 04-2004 Mandatory change of throttle lever system
SB 05-2004 Break of spark plug for engine HKS 700 E
SB 06-2004 Supplementary oil radiator for engine HKS 700 E
SB 01-2005 Change of the coils support and doubling the ground cable
SB 02-2005 Mandatory check of the front strut attachment on the wing
SB 03-2005 Mandatory control of the front strut attachment on the wing
SB 04-2005 Change of place for airfilter on carburetors
SB 01-2007 Change of place for fuel pump
SB 02-2007 Safety screwing 4 wheel pin
SB 01-2009 Check of fixing plate of junkers rockets
SB 01-2011 Additional parachute bridles for savannah registered in germany
SB 024-2014 Junkers parachute bag additional support for Savannah S
SB 025-2016 Flap mixer assembly modification for Savannah S
SB026-10-2016 Verify rust (corrosion) presence inside aileron lever
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– The two large lateral doors allow an easy independent access to the cabin and they may be removed for flying in hot regions or to take pictures.
– The cockpit is completely sound insulated and covered with upholstery or fitted carpet.
– For a better visibility, the doors and the roof are fully transparent.
– The cabin arrangement features two canvas or upholstery covered side-by-side seats.
– The luggage van, situated behind the seats and accessible during the flight, may contain up to 45 lbs (20 kilograms)
– The cabin’s ventilation is provided by an opening between the doors and the upper part of the cabin door frame. A dynamic air scoop intended to extract the cabin air is fitted at the bottom of the baggage compartment. It’s possible to improve the cabin ventilation by using two rotating air scoops in the doors windows.
– Heating system can be orientated on feet or on windshield with control on the dashboard.
– Cabin light
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[su_spoiler title=”ابزارهای استاندارد ساوانا اس” style=”fancy” icon=”arrow”]
Anemometer D. 3 1/8” with coloured arcs
Altimeter D. 3 1/8” with setting window
Variometer D. 3 1/8”
Compass
Sljp and skid indicator
Tachometer
Fuel pressure
Oil pressure
Oil temperature
Hourmeter
Voltmeter
External temperature indicator + airbox (for Rotax 912 ULS only)
Water temperature in front left engine head
Water temperature in back right engine head
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