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Содержание Savannah

Страница 1: ...lI C P Sri j Savannah FLIGHT MANUAL Pag 11 AIRPLANE FLIGHT MANUAL Issue l Revision l Apr Ol Savannah l l ICP Sri Via Torino 12 14020 PIOVA MASSAIA AT Italy Phone 39 0141 996503 Fax 39 0141 996506...

Страница 2: ...Original l 2 Ott 02 Original l l Apr Ol Original l l Apr Ol Original l 4 July 03 Original l l Apr Ol Original l l Apr Ol Original l l Apr Ol Original l 2 Ott 02 Original l l Apr Ol Original l l Apr O...

Страница 3: ...ll Ol All 02 6 to11 18 21 24 28 32 34 03 2 3 14 04 2 3 14 05 2 3 5 8 9 10 06 2 3 6 Issue l Revision 6 July 04 New emission 03 01 Cerreetions 04 01 Cerreetions 10 02 Cerreetion 10 02 Note on Instrument...

Страница 4: ...ECTION 4 SECTIONS SECTION 6 Issue l Revision l Apr Ol TABLE OF CONTENTS AIRPLANE TECHNICAL DESCRIPTION LIMITATIONS EMERGENCYPROCEDURES NORMALPROCEDURES PERFORMANCE WEIGHT AND BALANCE ICP Sri Via Torin...

Страница 5: ...specifications Structure Landing gear Engine Engine controls Propeller Fuel system Electrical system Cabin Cabin features and upholstery Ventilation Cabin heating Instrument panel Flight controls Fla...

Страница 6: ...lI C P Sri l Savannah FLIGHT MANUAL Pag 61 AIRPLANE THREE VIEW 2580 Issue l Revision 6 july 04 ICP Sri Via Torino 12 14020 PlOVA MASSAIA AT Ita1y Phone 39 0141 996503 Fax 39 0141 996506...

Страница 7: ...nt instalied as per the customer requirements p l owerp ant Engine Take off performance Dispiacement Compression ratio Fuei consumption 75 power Fuel and oil Fuel capacity Fuel grade Oil capacity L d...

Страница 8: ...YLIGHT VFR conditions The instalied engine is not a certificated aircraft engine It has not received any safety or durability testing and conforms to no aircraft standards This is for use in experimen...

Страница 9: ...nt hole The reservoirs features an overcapacity fuel pipe ending below the wing The left fuel tank is with a visual fuel level indicator located on left wing first rib The drain valve 5 is located in...

Страница 10: ...er relais B regulator C electric fuel pump D master switch E power supply F elevator trim motor G battery 4 revolution counter supply 5 hourmeter 6 voltmeter 7 left head temperature 8 right head tempe...

Страница 11: ...the cabin ventilation by using two rotating air scoops in the doors windows lt s important to get an efficient cabin ventilation to avoid the windshield frosting in high humidity low temperature and...

Страница 12: ...STEM Issue l Revision l Apr Ol Savannah FLIGHT MANUAL lPag 12j Pigure nr l l l l l l l l l l l l l l l Hl l l IIII l l l ____ J ICP Sri Via Torino 12 14020 PlOVA MASSAIA AT ltaly Phone 39 0141 996503...

Страница 13: ...FLIGHTMANUAL ELECTRIC SYSTEM il o 3 1 H t w K1 r pp 1 _j r r l l w z l L J z w r _j Figure nr 2 l Pag 13j Issue l Revision l Apr Ol ICP Sri Via Torino 12 14020 PlOVA MASSAIA AT Italy Phone 39 0141 996...

Страница 14: ...ol 13 Revolution co nter 14 Fuel preSSl lr E indicotor 15 Slip inclico tor 16o Left cylinder head t eMpera t ure l6b Right c ylinder head teMpera t ure 17 Externol ter pe ro t ur e 912 UU A1r oox teM...

Страница 15: ...ull backward the flap results 36 3 lowered with flaps fully extended and stick completely pushed to the right position the left flap results extended of 40 3 the right flaperon results extended of32 3...

Страница 16: ...IGHT CONTROLS Issue l Revision l Apr Ol Savannah FLIGHTMANUAL 1 1 J l 1 f l l CL l l l l l Figure nr 3 z o C w J 4 l Pag 16j ICP Sri Via Torino 12 14020 PlOVA MASSAIA AT Italy Phone 39 0141 996503 Fax...

Страница 17: ...ting limits Weight imitations C of G imitations Kind of operations Kind of maneuverings TABLE OF CONTENTS SECTION2 LIMITATIONS Max crosswind for T 0 and landing lPag 171 Page 18 18 18 19 19 19 19 19 I...

Страница 18: ...LOAD FACTORS Fia s retracted 4 Fia s full extended 2 NOTE the maximum load factors limit load factors are obtained multiplying theabove indicated values by the coefficient 1 5 2 3 ENGINE OPERATING LIM...

Страница 19: ...D OF OPERATIONS 30 MAC 38 5 MAC The airplane can be operated only in day VFR conditions 2 7 KIND OF MANEUVERINGS The airplane is intended for non aerobatic operations only 2 8 MAX CROSSWIND FOR T 0 AN...

Страница 20: ...ROCEDURES Fire on the ground engine operating In flight fire Cabin fire Unintentional spins Engine failure during T 0 on the ground or immediately after T 0 low altitude Engine start during flight lPa...

Страница 21: ...TING Fuel valve Throttle 3 4 IN FLIGHT FIRE Fuel valve Engine Electrical system Landing 3 5 CABIN FIRE Electrical system Fire extinguisher 3 6 UNINTENTIONAL SPINS Rotation Control stick Upon taking ai...

Страница 22: ...d 30 right Throttle 50 fuel pump ON and_ y to restart the engine lfprevious point fails Before touching the ground magnetces OFF master switch OFF throttle idle fuel valve shut off Flaps Fully deflect...

Страница 23: ...start up 24 4 4 Taxying 26 4 5 Before to take off 26 4 6 Take off and climb 27 4 7 Cruise 28 4 8 Descent 28 4 9 Approach and landing 28 4 10 Cross wind landing 29 4 11 Aborted landing Go around 29 4 1...

Страница 24: ...Visual check of connection pionts Main landing gear and strut attachments Visual check to bolts and nuts Slat Ailerons Horizontal and vertical tail Coolant radiator 4 3 ENGINE START UP COLDENGINE Mast...

Страница 25: ...arter call with loud vmce BEWARE OF PROPELLER Then upon making sure himself none is close to the propeller he can start the engine If someone is standing close to the aircraft it would be his responsi...

Страница 26: ...DJUST Trim ADJUST to neutral position Flaps retracted CHECK Flight controls freedom of movement and correct CHECK movement of surfaces Doors closed and locked CHECK Safety helts fastened CHECK Fuellev...

Страница 27: ...45 mph until the 50 ft obstacle SET clearing Flaps upon reaching a safe altitude and airspeed FULLY RETRACTED NOTES the hest rate of climb makes the aircraft climb to the required altitude in the sho...

Страница 28: ...flight attitude the engirre power output will decrease as well as the propeller s thrust to compensate it it s required to increase the engine s RPM The normal engirre running speed is 4 000 to 5 400...

Страница 29: ...NUTES Throttle IDLE Magnetos OFF Master switch OFF It s recommended to keep the engine running at low RPM for as long as two minutes in order to avoid a thermal shock and to achieve a thermal balance...

Страница 30: ...ll speed Take offrun TABLE OF CONTENTS SECTION 5 PERFORMANCE Landing distances from 15 m and landing run Rate of climb j Pag 30 l Page 31 31 31 32 Issue l Revision l Apr Ol ICP Sri Via Torino 12 14020...

Страница 31: ...rease until the stall occurs followed by a quick nose lowering NOTE the maximum flaps extended airspeed is 60 96 mph km h 5 2 TAKE OFF RUN Take off run Maximum weight l000 454 l hard surface flaps 20...

Страница 32: ...5 m s 37 mph 60 km h The maximum ceiling is 14 000 ft 4200 m pressure attitude at the maximum weight The hest rate of climb speed is 48177 mph kmlh The hest angle of climb speed is 45172 mphlkm h The...

Страница 33: ...ION 6 WEIGHT AND BALANCE General Weight and balance report Weight and balance drawings Weight and balance pilot s computing table and graph l Pag 331 Page 34 35 36 37 Issue l Revision l Apr Ol ICP Sri...

Страница 34: ...refer to the attached table Compute the total weight and the total moment given by adding all the single moments To be acceptable the found point MUST be located into the WHITE area between the two l...

Страница 35: ...t P3 By using a plumbing wire fixed to the leading edge measure the distance Dl between the projection on the floor of the leading edge and the nose wheel axle and the distance D2 between the same pro...

Страница 36: ...e D1 700mm D2 700mm Pl weight on forward gear P2 total weight on principal gear X P2 D Pl P2 Dl X ff J Z f l J Ttt loo M 1 L f f foD l i i o N Q_ lPag 361 Issue l Revision l Apr Ol ICP Sri Via Torino...

Страница 37: ...l max 11Olb max 0 i 0 595 Baggage 45 lb max 7 c l o c 1 42 TOTALS l i cf cl l 075 r _ GRAPH f orward limit 30 MAC X 0 429 m Total weight Ib 1100 T 900 800 500 100 Forward C of G limit Rear C of G limi...

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