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Skyranger Operators Manual, Issue 3, Feb 2011 

27 

 

Rudder and hinges, horns and cables 

 

Condition of tail surface coverings 

 

General alignment of vertical and horizontal tail surfaces 

 

Condition of bracing wires and their terminations 

Moving forwards to the port wing, inspect 

 

Port 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 strut lower attachment bolt 

 

Jury strut brackets 

 

Wing struts and jury struts straight 

 

Condition of wing covering and security of battens 

 

Flap, hinges, 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 wing strut attachments 

 

Through the inspection panel in the lower surface, check condition of 
the aileron pulleys and cables and internal wing structure. 

 

Condition of door, hinges and latches  

 

Static vent is clear of obstructions 

 

Finally  stand  back  and  take  an  overall  view  looking  for  general 
symmetry. 

9.8   Check B, C and Annual   

 

 

Check  B 

(25hrs/3 
months)

 

Check  C 

(50hrs/6 
months)

 

Annual  

(or 150 hrs)

 

Fuselage 

 

 

 

Check  all  pressure  instruments  for  cracks,  leaks  and 
stiction 

Check all fuselage tubes for cracks, dents, corrosion or 
deformation 

Check all fasteners for security, condition and fretting 

Summary of Contents for SkyRanger

Page 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...

Page 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...

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

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

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

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