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Skyranger Operators Manual, Issue 3, Feb 2011 

13 

(LD) position should be selected. As flap is selected a gentle pull on the 
stick will be required to maintain constant airspeed. Therefore re 
trimming will be required.  

4.10.2 Roundout should be initiated around 15-20 ft and hold-off 2-3 ft 

above the runway.   

4.10.3 Pilots transitioning from more traditional lower performance 

microlight aircraft should be aware that if the airspeed is allowed to 
increase on the approach then the aircraft may exhibit considerable 
float during the hold off period and this may cause a tendency to 
‘balloon’ and will cause more runway than expected to be used. 

4.11  Short field landing 

 4.11.1 Select full flap (LD) position, and set up a powered approach at 

around 45 – 50 knots CAS[        IAS]. Use power adjustments to control 
the flight path and rate of descent whilst accurately maintaining 
airspeed with elevator. If tall obstacles are present on the approach, 
then transition into a glide approach once clear past them. Take care 
however to maintain airspeed during this phase. 50 knots CAS [        
IAS] is recommended as the minimum for a glide approach at max 
takeoff weight. 

4.11.2 When round out height is reached close the throttle fully and round 

out. Perform a brief hold off and land. Brakes can be used to shorten 
the landing roll if required. Take care not to brake too sharply on 
rough or soft surfaces. Braking efficiency is at its greatest if the 
elevator is applied fully up after touchdown and speed has decayed 
below flying speed. 

4.11.3 Accurate airspeed control is the key to short field performance and 

pilots new to the Skyranger must practice until this is achieved to be 
able to land in the published distance. 

4.12  Soft field landing 

4.12.1 Fly the approach as in 4.11.1 above. 

4.12.2 Fully hold off and try to touch down gently and as slow as possible. 

During the ground roll avoid braking and progressively apply full up 
elevator to keep the nose wheel up for as long as possible. Continue to 
hold up elevator when the nose wheel is on the ground. 

Содержание SkyRanger

Страница 1: ...by Aeros Ukraine Importer Aircraft Kits and Spares are imported by Skyranger UK Ltd This manual is a legal document which is approved for use with Skyranger microlight aircraft issued with a United K...

Страница 2: ...2 9 Maintenance 23 10 Repairs 37 11 Vital Statistics 38 Annex A The Microlight Airworthiness Approval Note recommending issue of a permit to fly Annex B Engine Manual Annex C Weight and balance report...

Страница 3: ...Skyranger Operators Manual Issue 3 Feb 2011 3 TABLE OF AMENDMENTS Amendment No Date incorporated Signed...

Страница 4: ...tor familiar with the type is strongly recommended and to carry out routine maintenance and minor repairs Manuals exist for this aircraft for use overseas which also include guidance on fitting modifi...

Страница 5: ...2 3 1 Pitch control is effected by fore aft movement of the central stick with movement transmitted to a conventional elevator through cables 2 3 2 Pitch trimming is effected by a hand operated lever...

Страница 6: ...nd CAS is basically the accuracy of your Pitot static system The IAS limits for your aircraft were determined when the aircraft was test flown and are shown in Annex A to this manual There will also b...

Страница 7: ...nded that the Skyranger is not flown where a crosswind component above 15 knots is predicted 3 3 6 Do not fly above 10 000ft standard pressure altitude without the use of personal oxygen 3 3 7 Do not...

Страница 8: ...engine ensure that the max takeoff weight will not be exceeded from fuel weight placard 4 2 2 The BMAA standard manual pre start checks STAIP are recommended The actual starting procedures for a parti...

Страница 9: ...ay from the wind and the elevator held down 4 3 4 Taxy checks When taxying check Brakes functioning Compass moving when aircraft turned Slip ball moving when aircraft turned Engine temps warming no li...

Страница 10: ...RPM F Fuel and Flaps Check fuel tap is ON Check contents sufficient for flight Cycle flaps and check symmetrical operation detent operation Set flap as required T Trim Check trim set for takeoff W Win...

Страница 11: ...he excellent climb rate especially with the 80hp and above engine options the nose is high and may obscure forwards view Therefore it is recommended to periodically weave or lower the nose to clear th...

Страница 12: ...ap 4 9 Crosswind takeoff 4 9 1 The maximum demonstrated takeoff crosswind limit of the Skyranger is a component of 15knots Pilots are advised to avoid crosswind components of greater than 10 knots unt...

Страница 13: ...on the approach then transition into a glide approach once clear past them Take care however to maintain airspeed during this phase 50 knots CAS IAS is recommended as the minimum for a glide approach...

Страница 14: ...ll touchdown into wind main wheel first Progressive aileron deflection should applied into wind as the speed decays during the ground roll to keep the aircraft on one wheel and gently lower the downwi...

Страница 15: ...e for strong gusts to overstress the aircraft 4 17 Stalling During test flying of the UK prototype G CBIV the following stalling speeds were recorded VS1 Stalling speed at max takeoff weight forward C...

Страница 16: ...re similar to the power off case An additional warning of the approaching stall is the attitude of the aircraft With full power set the aircraft stalls at a very high nose attitude 4 17 5 Because of t...

Страница 17: ...rtures Other departures from controlled flight are likely either to be due to damage to the aircraft or hazardous flying conditions In either case land as soon as possible and examine the aircraft par...

Страница 18: ...give the minimum descent rate min sink of around 550FPM 5 4 Cruise performance Because microlight aircraft are very strongly affected by weight engine condition propeller matching wind and air tempera...

Страница 19: ...ately provided hedge at the far end of the runway For every 1000ft you are above sea level multiply by 1 05 For every 100C above 150C air temperature multiply by 1 05 For every 2 of downslope multiply...

Страница 20: ...n the cockpit Switch off all electrical devices not the ignition unless there is an engine fire also close heater vent open fresh air vents land immediately and vacate the aircraft 6 6 Emergency Landi...

Страница 21: ...as per placard in cockpit on central upright Final inspection of all nuts and bolts cable routing and attachments 7 2 To remove the wings from the Skyranger Disconnect aileron cables Disconnect pitot...

Страница 22: ...n hunting in speed and height when disturbed which will be most noticeable in turbulent conditions Flying outside of the permitted CG limits at either extreme is potentially dangerous and should not b...

Страница 23: ...y should limit themselves to the simple maintenance actions and engage suitably skilled persons to undertake the more complex tasks No specific qualifications are legally required for persons carrying...

Страница 24: ...nique airframe parts must be purchased from the manufacturer or another organization approved by the BMAA for manufacturing such parts usually if the manufacturer has ceased trading Some parts may be...

Страница 25: ...9 7 2 Aircraft The following is a brief summary of the minimum pre flight inspection If you are unsure it does no harm to increase the number of items on your inspection Inside the Cockpit Ignition sw...

Страница 26: ...and latches Starboard undercarriage leg undistorted Undercarriage drag strut and shoes secure Tyre condition and pressure Security of wheel spat Check for evidence of hydraulic leaks Security of wing...

Страница 27: ...es and security of actuating rod attachment Aileron movement and hinges attachment of cables and control horn condition General condition of leading edge wing tip area and covering Security of upper w...

Страница 28: ...peration of latches x x x Check windscreen for security and condition cracks in lexan x x x Undercarriage Check main gear legs for distortion security and condition x x x Check noseleg for distortion...

Страница 29: ...k electrolyte level of battery if applicable x x x Check security of battery mounting leaks connections security x x x Check all wiring for condition and security x x x Check condition of all switches...

Страница 30: ...tion there should be no movement x x x Check operation of elevator x x x Check hinges condition and security x x x Lubricate hinges x x x Check fabric and stitching condition x x x Check condition and...

Страница 31: ...tor header tank overflow bottle level and leaks Water carb heat if fitted x x x Check exhaust system security springs check for cracks dents blowing Proximity to cowlings fluid pipes x x x Lubricate e...

Страница 32: ...an Xlam when exposed to UV light and therefore requires more care to ensure a long service life 9 10 2 Prolonged outside uncovered storage is not recommended 9 10 3 Covering fabric and its stitching c...

Страница 33: ...ep the aircraft clean It pays to clean the aircraft after use before storage But avoid putting the aircraft away wet in a closed hangar with reduced ventilation 9 12 3 Proprietary car wash wax cleanin...

Страница 34: ...ear movement of the whole rubber parts relative to the hole in the mounting structure indicates that the rubber should be replaced 9 14 Fuel tanks 9 14 1 The fuel tanks are clear polyethylene Taking o...

Страница 35: ...rudder side to side If increased friction is found this indicates a bent noseleg Removing the noseleg will confirm this It may also be possible if overloaded to bend the large washer under the suspens...

Страница 36: ...our local inspector maintenance professional the importer 9 16 3 Such a strip down will involve removal of fabric coverings and fuselage fairings This permits full detailed inspection of airframe comp...

Страница 37: ...aircraft like the Nynja it is normally far simpler and cheaper to replace the damaged component 10 5 Repairs to the Engine These should be carried out in accordance with the maintenance manual for th...

Страница 38: ...eplaced 11 Vital Statistics Weight values for this Skyranger are at Annex C and a description of the aircraft is at section 2 However the following describes the basic dimensions of the aircraft Lengt...

Страница 39: ...Skyranger Operators Manual Issue 3 Feb 2011 39 ANNEX A MAAN RECOMMENDING ISSUE OF A PERMIT TO FLY The approval MAAN for this aircraft is to follow this page...

Страница 40: ...Skyranger Operators Manual Issue 3 Feb 2011 40 ANNEX B ENGINE MANUAL The operators and maintenance manual for the engine fitted to this aircraft is to follow this page...

Страница 41: ...Skyranger Operators Manual Issue 3 Feb 2011 41 ANNEX C WEIGHT AND BALANCE REPORT Forms BMAA AW 028 completed for this aircraft are to follow this page...

Страница 42: ...rs Manual Issue 3 Feb 2011 42 ANNEX D MINOR MODIFICATIONS FITTED TO THIS AIRCRAFT SINCE INITIAL PERMIT ISSUE Minor modification approval sheets are to follow this page Minmod No Description Sign and d...

Страница 43: ...Feb 2011 43 ANNEX E MAJOR MODIFICATIONS FITTED TO THIS AIRCRAFT SINCE INITIAL PERMIT ISSUE BMAA MAANs and CAA AANs other than the original approval MAAN are to follow this page MAAN AAN No Issue Desc...

Страница 44: ...Skyranger Operators Manual Issue 3 Feb 2011 44 ANNEX F INSTRUCTIONS AND MANUALS FOR OTHER DEVICES FITTED TO THIS AIRCRAFT No Description Issue or date Approval Mod No or original equipment...

Страница 45: ...Skyranger Operators Manual Issue 3 Feb 2011 45...

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