Table of Contents
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Table of Contents
Related Manuals for Helio HT-295
Summary of Contents for Helio HT-295
- Page 2 PAGE Ailerons and Interce$tore- - - - - - - - - - - - - - - - - - - SECTION XI Flight And Operating xastructions Operating G e n e r a l Pilot Emergency Check S u m m a r y O p e r a t i o n a l Afrspeab- - - - - - - - - -‘- - - - - Take-Off, Cruise and Landing C r o s s - W i n d...
- Page 3 . SECTION I General Description of Airplane The W-295 is a high wing monoplane. The wing is fully cantilever and of all metal construction. The fuselage cabin section is a metal covered tubular structure and the aft section is all metal semi- monocoque.
- Page 4 The ailerons are the Frieze type, of 2024 alclad diagonal rib truss structure, fabric covered, They are hinged at both ends and operated by a push-pull tube at the ce&ex, The interceptors consist of heavy aluminum alloy curved plates (inboard) They emerge from the wings incon- and forward of each aileron).
- Page 5 SECTION II+F&IGHT,AND OPERATING INSTRUCTTONS The HT.295 incsrporates flight control devices to insure safe flight at slow air speeds without detriment to high-speed flight. however, The cockpit contmls, is the same as in any ather fixed-wing airplane. The exceptional degree of control is obtained by the use of reading edge slats, large flaps, interceptors and a fully movable horimntal tail surface with its anti-balance tab.
- Page 6 effective that through their normal use, it is possible to overcome the effects of both slats remaining closed on one side. All 1700 series aircraft have electric powered flaps as F L A P S standard with flap position Indicator on the instrument panel. Full flap can be used for landing under all normal wind conditions.
- Page 7 freedom af Check all controfs for cargo is secured and that the load is properly located, Check of electrical and ignition switches. Open cowl flaps. The following starting procedure is taken from the A copy of the Lycoming rfanual is furnished Lycoming Operator's Manual, with each airplane and is considered a part of this manual, Set the propeller control lever all the way forward in INCREASE RPM...
- Page 8 When it is suspected that a vapor lock exists, the follawfng procedures should be used: Fuel selector ON, electric fuel booster leave there until fuel pressure builds up and cavitating sound disappears, then return migture control ta idle cut-off and proceed with normal starting sequence.
- Page 9 reduce RPM t=o As SQQ~ as possible after take-off, the maximum Take-off continuous setting (3000 RPM) and retract the flaps. power may be used for 8 maximum of five (5) minutes, but it is advisable Best rate of obtained 65 MPH IAS flaps down, and at 90 MPH IAS climb is flaps up at MET0 A cylinder head temperature gauge is...
- Page 10 STALLS AKD SPINS, and the of the stabilator makes it impassible to fully stall the wing on is approached the HT-295. As the minimum speed obtainable with the yoke full back, a center section separation causes tail buffeting,...
- Page 11 Engine Nodel: Average An3iant Air Temperature Straight Qil Inlet For Starting Additive Temperature Desired Max. SAE 40 or 50 SAE 50 Above 60*F t o 7OoF SAE 30 a SAE 40 Below lOoF - SAE 20 ROTATING BEACON LIGHT beacon light is installed, this light should be turned off before entering overcast, as reflections from the rotating anti-collision light on clouds or dense haze can produce optical illusions and severe vertigo.
- Page 12 Throttle Propeller - FIsE;lL INcIbEASE Carburetor Heat - Cow) CHECK All Cfrcuit Breakera - IN 1 0 0 11 0 Fuel Ptupap - ON Propeller - CLEAR 13 0 Ignition Switch - TURH TO EXTREME RPG)IT AND P&H 15 a STARTS 16 8 (Simultaneously...
- Page 13 Flight Controls - FREE, FULLTRAWL Flight Instrtmmts = SET Trim Tab - SET wing Flaps DEGREES AS; DESIRED FULL IHXEASE RPM Mixture - RICH 10 0 11 4 2 I, R LIFT OFF FULL AIRSPEED 80 MPH MAXLMJM Cylinder Head 2750 RI= Propeller- 2600 RPM carburetor Heat - CfoLD (EXCEPT IN XCIms)
- Page 14 Abort if BEmRE Airborne Throttle - Control Wheel - Back Brakes - Apply Full aaicreaae RPM and Master Switch - Off Abort AFTER kcasrrfng If bchw 50 feet - Hold Yoke Back If above SO feet - Hose over artd attampt to pick up approximately 65 ME% to facilitate a normal with flaps...
- Page 15 Propeller Underrpeeding and proceed to nesrest airport, If this is not pcralrfble mka Use excem altitude otnd power available to emergency landin& Propeller - Full Iacrease RPM Airspeed - Maintain Maximum of 4 & touch-down, safe-epaed tire in the direction of the flat with the rudder and brakes, LANDING ON U#P&EPARAED TERRAIN On soft or rough ground, use caution in .-lying brakes.
- Page 16 When an atirapetsd of approxiwaely 40 MFH has been reached the awe and the aircraft will bet- aPrborne. climb 64 XI?‘& reduca 3000 RPM and mahmia full throttlr! (5 slim&es at t&x!-off WM of Flaps may at 3Q” and an when opmIRting fmm 8 of climb, or until...
- Page 17 For half-flap landings, an approach speed of 65 to 70 miles an when irastrectiag a pilot new tu the the pilot’s profSciency the pilot should be rmitided that the darts will speed, that flare-out just 8s ha begins his they will have nc) With effect has little @@floatVQ...
- Page 18 poke ahuuld be hald full beck. approach is eae,se of glide path in this to make amooth landings, of landing is laeceasary, order type For ful,I-flap, no-pop~rer Landingr, it advisable that the pflot keep the aipproach *peed st 60 to 65 MPH, but not below 60 WEi.
- Page 19 Experience galned En th%s type sf take-off w%ll ermbh the pilot aunt of yoke mcw~mernt and/or rapidity of action to determine tha run. This type .of s~inimum run take-off is most useful when ground is rough, bumpy, muddy Muddy Terrain Take-Off The Helllo Courier is an unusua1lp good “Blludder”.
- Page 20 the Helis Cmrier, there too low u. apeed with a s p i n . flaps dm, altitude The asost emoa cause of HeIia crsahe~ and major daarage -- though off the ground prematurely at toa law B speed pull aircraft the propeller a;t km fmrvmrd Thus, with...
- Page 21 CAUTION attain sh.ort field proficiency is therefare after the amme pawet c)r diminish pcrsrer a hard lamding. Centrally, mast of the originally selected barrier CrQssiag pcwet rcmafn# on, and, at the ftnal rotmd-uut high rate-of-desseat, but stopping short of the point If ‘khatter”...
- Page 22 (2)In that most radvimble tcchniquct, the aimraft approach pattern any fntantional devfstfon fram a straight line appralech cwer then by power adjustment8. of the The me and only sotatian 5s entire a;pprosch. the lasr abrupt xaund-out just p&w to touch-dawn. the S,ToL pflot to In the this awarene~a, STOL.technfques differ mmte-...
- Page 23 T h e During greater take-offs, attention ts’dfrcctianal cxmtrol. is required when the cram- left Cross-wfnd amplifies the *tprq wind ia factor of the propelIxr, aad tendency of the wtnd. The sburt be used may take-off ground run can times to When pasrrible, the take-off psth pslipsy be at a slight...
- Page 24 below the rilpht fonaard off the fuel frm the tanka when f i l t e r is T h i s t h e be aafetted, volt supply battery s;nd an ongtne driven afternator for tAe the 1700 series aircraft the battery ka fcxxted on the engine rccesaory mction, electrical system through a voltage 50 asaperas.
- Page 25 Hut or cold air anterr ths ca;bia through ~taiwPsss steel regulation is abraimed by tme af the eontral knob on the inatrtmrrrent, Hot air is abtsfaad by paesiag cold outside air rrrmnd one of the exhatmt The txhmat ats~k stocks hours.
- Page 26 the tzoatrof lock is wed utt the contra1 wheel, bs sure that is conspicuons to thcsr pilot on his gromd ehtck, The parking brake control fs sperated in eonjunctfon wllth the tot brakes, the desired brakes ta control lcwated brake ON THE Avoid heavy...