ICP Savannah Airplane Flight Manual Download | Manualshive

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Summary of Contents for Savannah

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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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