background image

 

 

 

 

 

A slight tendency to swing to port can be held easily with the rudder. 

 
 

The aircraft should be flown off at approx 40 knots IAS, Before climbing 

 

increase speed to 46 knots IAS (20º Flap) or 50 knots with no flap. 

 
 

After retracting the flap at a safe height a speed of 55 knots IAS and full throttle 

 

will satisfy normal climb requirements. 

 
 

Short take off 

 
 

Minimum ground run and best obstacle clearance is obtained using the 20º flap 

 

setting and a climb speed of 46 knots IAS. 

 
 

Apply full throttle while holding the aircraft on the brakes. 

 
 

Release the brakes when the aircraft starts to move forward or when at full 

 

throttle and accelerate to the minimum possible unstick speed maintaining a 

 

slightly lower than normal tail low attitude. 

 
 

Allow the aircraft to accelerate to 46 knots IAS, then climb steadily at this speed 

 

until clear of all obstacles. 

 
 

When clear, increase speed to 50 knots IAS, raise the flaps, increase speed to 55 

 

knots IAS and continue the climb, using full throttle. 

 

 Cross-Wind 

Take-Off 

 
 Flaps 

retracted. 

          

                           Pilot’s Operating Handbook VH-SJH                   Chapter 5 

 

                                               

Handling 

 
Apply full throttle using sufficient aileron into wind to keep the wings level. 

 

Hold the aircraft on the ground until speed is about 5 knots above the normal 

 

unstick speed, then effect a clean, quick take-off with a positive backwards 

 

movement of the control column. 

 
 

Climb at full throttle increasing airspeed as for a normal take-off at the same time

 

 laying off the effect of drift by turning slightly into wind as required. 

 

 

 

NOTE.  All airspeed quoted apply to a maximum AUW of 658kgs (1450lbs), 
therefore, slightly better performance at lower weights can be obtained by 
reducing the speeds quoted but this practice is not recommended for normal 
operations. 

 

8 Climbing 

 
 

Maximum rate and angle of climb at 658kgs (1450lbs) maximum AUW and full 

 

throttle is obtainable at the following speeds:- 

 
 

 

Flaps 20º - 46 knots IAS 

 

 

Flaps up  -  50 knots IAS 

 
 

For all other requirements the recommended climbing speed is 55 knots IAS 

 

(flaps up).  The engine manufacturers recommend full throttle for all climbs but 

 

power may be reduced if desired for “cruising” climbs. 

 
 

Full rich mixture should be used unless leaning is necessary to eliminate rough 

 

running due to over-rich mixture at altitude or use of carburettor heat, (refer to 11 

 

and 12, this Chapter). 

 

9 General Flying 
 
 Flying 

Controls 

 
 

Flying the “Emeraude” is a pleasant experience.  Stick forces are exceptionally 

 

light, the controls are well harmonised and effective throughout the speed range. 

 
 

Little, if any rudder is required to assist turning.  In calm conditions the aircraft 

 

may be flown feet off for long periods. 

 
 

 

 

          

                             Pilot’s Operating Handbook VH-SJH                   Chapter 5 

 

                                                

Handling 

 
The maximum rate of roll is approximately 80º per second. 

 

Change of Trim 

 
 

There is no change of trim when the flaps are operated due to the action of the 

 

automatic trim tab on the starboard elevator operated from the flap cables. 

 

Содержание EMERAUDE CP301 VH-SJH

Страница 1: ...VH SJH FLIGHT MANUAL Nationality and Registration Marks VH SJH Aeroplane Serial Number 357 N10 Manufacturer Schenk Jenatsch Hodges Designation of Aeroplane Piel Emeraude CP301 Series 100 Certificatio...

Страница 2: ...adequate control will exist under all conditions including turbulence and sudden and complete engine failure during the climb after take off Approach Speed The approach speed is a speed chosen to ens...

Страница 3: ...t NOTE This provides special information to make maintenance easier or important instructions clearer Pilot s Operating Handbook VH SJH Chapter 1 DESCRIPTION Type The Piel Emeraude is a low wing monop...

Страница 4: ...spring and is connected by springs to the rudder to eliminate shimmy and to assist in turning External disc type hydraulic brakes are fitted Empennage A single fin and rudder streamlined with the bott...

Страница 5: ...system Rubber blocks in compression springs for rebound Wheels Dunlop Tyers 500x4in Tyre Pressure 25 lb Brakes Hydraulic external disc Pilot s Operating Handbook VH SJH Chapter 2 LEADING PARTICULARS T...

Страница 6: ...oned on the right side of the instrument panel adjacent to the master and generator isolation switches An ammeter placed to the left of the master switch shows the rate of charge to the battery Any ex...

Страница 7: ...ttor Air Temperature Control A push pull type control is fitted to the left of the throttle Carburettor air temperature is controlled by a lever operated plate valve in the intake housing which opens...

Страница 8: ...elevator trim tab fitted to the port elevator is controlled by a lever mounted centrally in a box between the two seats Settings designated NOSE UP and NOSE DOWN are clearly marked on the box at each...

Страница 9: ...ic head carried on the underside of the port wing outer section The Turn and Balance Indicator is electrically driven All the instruments including the Magnetic Compass are grouped in front of the pil...

Страница 10: ...m system is mounted above the radio in the instrument panel Protection for the radio is provided by a separate press to reset circuit breaker positioned next to the master switch on the instrument pan...

Страница 11: ...ing intentional spinning in accordance with the C of A for individual aircraft See DCA Aeronautical Report 61 3 Inverted Flight Prohibited Pilot in Command Solo flying permitted only from the left sea...

Страница 12: ...ndition all inspection panels secure Port Undercarriage Wheel Fairing Condition and secure Leg Condition extension approx 120mm Torque Link secure Brake Unit Secure no leaks Tyre No cuts or creep pres...

Страница 13: ...n check Flaps UP Canopy Closed and latched Master switch ON Fuel Pump ON Instrument Switch ON Generator ON Fuel Selector ON Fuel Gauge Check Contents Mixture Full rich Carburettor air temp cold Radio...

Страница 14: ...been demonstrated as safe to taxi in winds up to 25 knots There is no tendency for the aircraft to tip onto its nose if the brakes are used harshly As always however care should be taken to avoid har...

Страница 15: ...full throttle increasing airspeed as for a normal take off at the same time laying off the effect of drift by turning slightly into wind as required NOTE All airspeed quoted apply to a maximum AUW of...

Страница 16: ...g on the ground has been dealt with earlier in this Chapter Carburettor heat should be used in flight at the first indications engine roughness or loss of rpm that ice may be forming To remove carbure...

Страница 17: ...or no delay prior to the spin proper To the right the aircraft has a definite tendency to spiral and in some cases will not enter the spin proper unless opposite aileron is applied This is not recomm...

Страница 18: ...ent at cruising speed or for en route let down by gliding with the throttle closed Before descending check mixture is fully RICH unless carburettor heat is required in which case adjust accordingly Op...

Страница 19: ...here is a tendency to weathercock when landing in strong cross winds Use of differential brake will help prevent this Flapless Landing Little difference exists between the flapped and un flapped landi...

Страница 20: ...Section AGA 4 and the LAH Section GEN which specifies a minimum strip length at sea level of 2000 feet plus 200 feet increase for every 1000 feet the landing area is above sea level 3 Climb Maximum r...

Страница 21: ...ches Magnetos on BOTH T Throttle Linkages Pilot s Operating Handbook VH SJH Chapter 7 Performance Assuming the failure cannot be rectified pass the appropriate Radio distress message and check Canopy...

Страница 22: ...ding in plenty of time to ensure its successful completion Dive Start Height at least 3000 ft AGL Establish the glide trim and conduct cockpit check as above but open the throttle half way Check all c...

Страница 23: ...Pilot s Operating Handbook VH SJH Chapter 8 AMENDMENT RECORD SHEET Amendment Number Paragraph s Affected Signature Date of Incorporation...

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