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Terrier T200 LSA Flight Manual Rev No.: 1.0  15 April 2008  

 

Page 1 of 31 

 

FOXCON 

Aviation & Research Pty Ltd 

 

291 Gormley’s Road Seaforth Mackay QLD 4741 

Ph/Fax: 07 4959 0252 Mobile: 0418 747 751 

www.Foxcon.com

 

[email protected]  

 

            

 

 

Flight Manual 

Terrier T200 LSA 

Aircraft Registration 
Number: 

21-5161 

Aircraft Serial Number: 

#040701 

Power plant: 

Subaru EA-81 

Power plant Serial No: 

544848 

Propeller: 

Bolly BOS3 

Date of First Flight: 

05.03.08 

Current Owner: 

 

Address: 

 

 

 

Empty Weight

 

Moment

 

Date Weighed

 

323kg 

698.26 

25.02.08 

 

NOTE: Please keep all the above information current, and notify Foxcon Aviation & 

Research Pty Ltd  of any changes in ownership, address, or aircraft equipment and/or 

modifications. 

 

You are reminded that as part of the LSA certification, any modifications to the aircraft, 

including any change in the instrument or engine package supplied from the factory, 

has to be approved by Foxcon Aviation & Research Pty Ltd. 

Summary of Contents for Terrier T200 LSA

Page 1: ...lant Serial No 544848 Propeller Bolly BOS3 Date of First Flight 05 03 08 Current Owner Address Empty Weight Moment Date Weighed 323kg 698 26 25 02 08 NOTE Please keep all the above information current...

Page 2: ...ations 6 0 Checklist Procedures 7 0 Emergency Procedures 8 0 Operational Checklists 9 0 Other Procedures 10 0 Performance 11 0 Definitions Speeds Meteorological Terminology Engine Power Terminology Ai...

Page 3: ...t in command of the aircraft shall comply with all requirements procedures and limitations with respect to the operation of the aircraft set out in the Flight Manual for the aircraft Amendments shall...

Page 4: ...Terrier T200 LSA Flight Manual Rev No 1 0 15 April 2008 Page 4 of 31 2 0 Overall Dimensions...

Page 5: ...08 Page 5 of 31 3 0 Specifications Engine Subaru EA 81 Wing Span 8 70m Length 6 10m Empty Weight 334kg Gross Weight 600kg Fuel Capacity 88L Landing Gear Track 2 12m Baggage 30kg Design Load Ultimate 6...

Page 6: ...mal Operations Speed 38 110 Caution Range 110 120 Only fly at these speeds in smooth air VA Maneuvering speed at Gross Weight 85 Do not make full or abrupt control movements above this speed VFE Maxim...

Page 7: ...ic maneuvers including spins are not permitted 4 10 Engine Start Operating Temperature MAX 50 C MIN 20 C 4 11 Smoking Prohibited 4 12 Maximum Air Temperature for Operations 50 C for take off at gross...

Page 8: ...mal 75 Best Rate of Climb at low altitude 75 Note Best Obstacle clearance gradient is with 1st Stage Flaps but do not maintain this condition for longer than necessary as this may cause excessive engi...

Page 9: ...ck aileron flap control bolts nuts flap control rod for security Check rod ends for freedom of rotation excessive movement 4 Pitot Tubes 1 Static Dynamic Source Remove cup check for blockage 5 Right W...

Page 10: ...s Check condition and security 6 Ailerons Check for free rotation excessive movement 7 Elevator Check for free rotation excessive movement 8 Rudder Check free security free movement 9 Flap Control Che...

Page 11: ...unction 11 Choke CLOSED after warm up completed IMPORTANT Check the engine oil pressure If you do not see oil pressure within 10 seconds shut down the engine immediately and check the cause 6 4 Starti...

Page 12: ...d to avoid the potential for an in flight stoppage 11 Carburettor Heat Check Throttle up to 4000 RPM Pull out the Carburettor Heat Control Return the Carburettor Heat Control to the Full IN or cold po...

Page 13: ...normal climb out NEVER use full flap for take off 6 14 Take Off with Obstacles Follow instructions as by the short take off after the T O rise up and increase the speed in ground effect to 56 60 knot...

Page 14: ...the airplane slow down don t brake Provide the direction of the airplane by operation of vertical rudder The landing speed with cross wind should be increased Maximum cross wind limit is 20 knots Not...

Page 15: ...Not above maximum continuous power of 4800 RPM 4200 4500 Normal 2 Elevator Trim ADJUST if fitted 6 30 Before Landing 1 Seatbelts Harnesses ADJUST LOCK 2 Carburettor Head As required 3 Fuel Boost Pump...

Page 16: ...ft the nozzle out slightly for the last four litres and slow the speed down as you can create a siphon motion that will dump the last four litres out until the vent is above the fuel level If this hap...

Page 17: ...ly with window cleaner and a clean chamois To prevent scratching move the chamois up and down not in a circular movement In this case we do not take any responsibility for damages 6 38 Stopping the En...

Page 18: ...emergency arise the basic guidelines outlined in this section should be considered and applied as necessary to correct the problem 7 1 Airspeeds for Emergency Operation Engine Failure After Takeoff 50...

Page 19: ...Airspeed 45 knots at least 2 Fuel Shutoff Valves Both OFF 3 Ignition Switches OFF 4 Wing Flaps as required 5 Master Switch OFF Note A slightly higher speed may give better distance over the ground if...

Page 20: ...wiring before conducting another flight 8 7 Engine Fire in Flight 1 Throttle CLOSED 2 Fuel Shutoff Valves Both OFF 3 Ignition Switches OFF 4 Master Switch OFF 5 Cabin Air CLOSE 6 Airspeed 75 knots if...

Page 21: ...y giving location and intentions 2 Heavy Objects Secure 3 Approach High winds heavy seas INTO wind Light winds heavy swells parallel to swells 4 Wing Flaps Full Flap 5 Touchdown Near Stall Speed Ditch...

Page 22: ...earing on airframe reduce power to minimum to sustain level flight and proceed to nearest landing area Be prepared to make an emergency landing enroute should the engine fail 2 Gradual reduction in oi...

Page 23: ...ne end then you would have to move your finger airplane wings to make it balance again or get a SAME weight lump on the other end if they were HEAVY lumps of putty your finger wings may now bend Same...

Page 24: ...4 mm At weights below 440 Kg fwd limit 2227 mm EXAMPLE Item Wt Kg Arm Moment Basic Empty Wt 345 787910 Front seat occupant 1 80 x 2390 191200 Front seat occupant 2 65 x 2390 155350 Baggage 10 x 3100 3...

Page 25: ...ff Safety Speed is a speed chosen to ensure that adequate control will exist under all conditions including turbulence and sudden and complete engine failure during the climb after takeoff 11 3 4 Land...

Page 26: ...ff and landing was actually demonstrated during the certification tests 11 6 2 Useable Fuel The fuel available for flight planning 11 6 3 Unusable Fuel The quantity of fuel that cannot be safely used...

Page 27: ...t Manual Rev No 1 0 15 April 2008 Page 27 of 31 11 7 6 Useful Load The difference between the MTOW and the basic empty weight 11 7 7 MTOW Maximum Take Off Weight The maximum weight approved for the st...

Page 28: ...y Authority CASR Civil Aviation Safety Regulation FAA Federal Aviation Administration of the USA FAR Federal Aviation Regulations of the USA FM Flight Manual GIR Ground Inspection Report IAS Indicated...

Page 29: ...age also any changes in page content should be clearly visible e g marked with a bold vertical line Revision Number Name of Revision Date Description Signature Date 1 0 Spelling corrections 15 Apr 08...

Page 30: ...ations 8 Original Checklist Procedures 9 17 Original Emergency Procedures 18 Original Operational Checklists 19 21 Original Other Procedures 22 Original Performance 23 24 Original Definitions 25 27 Or...

Page 31: ...Terrier T200 LSA Flight Manual Rev No 1 0 15 April 2008 Page 31 of 31 15 0 Appendix 15 1 Weight and Balance Worksheet...

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