Foxcon Terrier T200 LSA Technical specifications

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: [phone] Mobile: [phone]
www.Foxcon.com
[e-mail]
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.

Terrier T200 LSA Flight Manual Rev No.: 1.0 15 April 2008 Page 2 of 31
Table of Contents
1.0 Introduction
2.0 Overall Dimensions
3.0 Specifications
4.0 Limitations
5.0 Normal Operations
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
Airplane Performance and Flight Planning Terminology
Weight and Balance Terminology
12.0 Abbreviations
13.0 Revision History
14.0 List of Valid Pages
15.0 Appendix
Weight & Balance

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1.0 Introduction
This is an Advanced Ultralight Aeroplane of composite construction.
The Foxcon LSA TERRIER T200 aircraft is a factory built aircraft. Each aircraft is subjected to factory flight test
program to determine that particular aircraft’s performance and characteristics complies with the design
standard.
The purpose of this manual is to provide guidance to owners and mechanics who wish to operate, undertake
maintenance, repairs, and alterations on the Terrier T200 LSA. If in any doubt, please contact the
manufacturer.
This Flight Manual applies only to the particular aircraft identified by the registration marking and serial number
on the Cover Page and contains the airworthiness limitations and essential operating data for this aircraft.
The Flight Manual shall be carried in the aircraft on all flights.
The pilot 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 be issued by Foxcon Aviation & Research Pty Ltd as necessary and will take the form of
replacement pages with the amendment date at the bottom of the page.
Interim / temporary amendments may be issued in the same manner and are to be inserted as directed. These
amendments will be issued on coloured pages and will take precedence over the stated affected page. It is the
owner’s responsibility to incorporate in this manual all such amendments, and to enter the date of incorporation
and his signature on the appropriate Amendment Record Sheet.
No entries or endorsements may be made to this Flight Manual except in the manner and by persons authorised
for the purpose.
It is the responsibility of the owner to maintain this Manual in a current status when it is being used for
operational purposes.
Owners should contact Foxcon Aviation & Research Pty Ltd whenever status of their Manual is in question.

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2.0 Overall Dimensions

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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 +6g/-4g)
+4g/-2g @ 600kg
Airfoil Section
Modified Chris Mk 4

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4.0 Limitations
4.1 Operating limitations, instrument markings and basic placards necessary for the safe operation of the
airplane, its engine, standard systems and standard equipment. Observance of these operating limitations is
required.
4.2 The aircraft shall be operated so that limitations and instructions included in this section are observed.
4.3 Type of Operation
VFR by Day
NO Aerobatics, including Spins.
Side Slips are not approved with flaps extended (flap MAY blank elevator)
4.4 Airspeed Limitations
Airspeed limitations and their operational significance are shown below.
Speed Knots Remarks
VNE Never exceed 125 Do not exceed this speed in any operation.
VNO Normal 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 Maximum flap extended speed 70 Do not exceed this speed with flaps down.
VSO 38 Full flaps 600 Kg MTOW
4.5 Airspeed Indicator Markings
Airspeed Indicator Markings and their operational significance are shown below.
Marking Knots Significance
White Arc 38 -70 Full-flap operating range. Lower limit is max. weight Vso in landing
configuration. Upper limit is max. speed permissible with flaps extended
Green Arc 38 -110 Normal operating range. Lower limit is Take-off Safety speed. Upper limit is
max. structural cruising speed
Yellow Arc 110 -120 Operations must be conducted with caution and only in still air
Red Line 125 VNE
4.6 Weights and Loading
Do not exceed under any circumstances.
MTOW Maximum Take Off Weight
600kg
Maximum Landing Weight 600kg

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4.7 Powerplant Limitations
Instrument Yellow Arc Green Arc Red Radial Line/Arc
Oil temp. 60° -90° C 90° -110° C 140° C
Oil Pressure 0,8 – 2,0 bar 2,0 – 5,0 bar 7 bar
Water Temperature 60° -120° C 130° C
Minimum Oil Temperature for
Take Off
50° C
Minimum Oil Pressure In Level Flight or climb 2 bar
In Descent 0.8 bar
Maximum Water
Temperature
130°C
Maximum RPM for all
operations
5000
Full Throttle Static RPM Not Above 4600
Not Under 4200
4.8 Other Limitations
4.9 Authorised Maneuvers and Associated Limitations
Aerobatic 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 weight.
4.13 Maximum Permissible Number of Occupants
Two (including Pilot).
4.14 Flights with Door(s) Open
Not permitted.
4.14a Flights with Door(s) Removed (before take-off)
Exercise caution and limited to 80 knots
4.15 Maximum Crosswind Velocity
20 knots (for experts only)
4.16 Maximum Baggage Weight
30 Kg provided rear Centre of Gravity is not exceeded.
4.17 Maximum G Factors
Limit +6g/-4g
4.18 Centre of Gravity
Forward Limit
2242mm aft of DATUM at 600kg
2227mm aft of DATUM at 440kg or less
Rear Limit
2404mm aft of DATUM at all weights
DATUM 2000mm forward of wing leading edge

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5.0 Normal Operations
Speeds for Normal Operation
The following speeds are based on a maximum weight 600 Kg and may be used for any lesser weight.
Takeoff: Knots
Take off, 1st Stage Flap 42
Short Field Take off, 1st Stage Flap 40
When Clear obstacles retract flaps and climb at 60-75
Climb, Flaps Up: Knots
Normal 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 engine temperatures
Landing Approach: (MTOW) Knots
Normal Approach, Flaps Full 45
Short Field Approach, Flaps Full. 42
Missing Approach (go around) Knots
Apply full power; allow speed to increase to 42
Retract Flap to 1st Stage
Then retract flap fully and continue to climb at or above 60
Maximum Recommended Turbulent Air Penetration Speed 90
Maximum Demonstrated Crosswind Velocity 20

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6.0 Checklist & Procedures
Pre-flight Inspection
Prior to flight, the aircraft should be inspected in accordance with the following checklists.
NOTE
Visually check airplane for general condition during walk-around inspection. In cold weather, remove even small
accumulations of frost, ice or snow from wing, tail and control surfaces. Also, make sure that control rods and
cables are free of ice and move freely.
6.1 Pre-flight Inspection Checklists
1 Fuel
1 Fuel Quantity Check level in tank through visual
2
Water Check
Before first flight of the day & after each refuelling, drain
small quantity of fuel from fuel drain valve & check for
water & sediment.
3 Fuel Filler Cap Check secure on each wing
2 Empennage
2 Control Surfaces Check freedom of movement & security
3
Check freedom of movement & security
3 Right Wing – Trailing Edge
1
Aileron
Check freedom of movement & security
2 Flap Check security
3
Control Rods
Check 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 Wing
1 Wing Control for damages
2 Main Wheel & Tyres Check for security. Proper tyre inflation & wear or damage
3
Wing Mount Bolts and Struts
Check for security
6 Nose
1 Propeller & Spinner Check for nicks & security
2 Cowling Remove and check security of engine components &
systems, particularly mounts, spark plugs, wiring, fuel
lines, baffles, check for oil leaks.
3
Engine Oil & Cooling Liquid
Level
Check & top up if necessary. Clean up any spilt oil.
4 Cowling Replace and check clips fastened & secure
7 Left Wing
1
Main Wheel & Tyre
Check for security. Proper tyre inflation or damage
2
Wing Mount Bolts and Struts
Check for security
3 Wing Control for damages
8 Left Wing – Trailing Edge
1 Aileron Check freedom of movement & security
2 Flap Check security
3
Control Rods
Check aileron & flap control bolts & nuts & flap control rod
for security. Check rod ends for freedom of rotation &
excessive movement
9 -Cabin
1 Flight manual Available in the aircraft
2 Ignition Switches OFF
3 Master Switch OFF

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4 Fuel Shutoff Valve ON
5
Seatbelts and Shoulder
Harnesses
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 Check for free movement & bolts secure.
10 Throttle controls Check for full & free travel
11 Brake lever Check for free travel & pressure.

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6.2 Before Starting Engine
1 Pre-flight Inspection COMPLETE
2 Seatbelts & Harness ADJUST & LOCK
3 Fuel Shutoff Valve Both ON
4 Radio/Intercom OFF
5 Brakes TEST & SET
6 Set Instruments Instruments SET
6.3 Starting Engine – Cold Engine
1 Carburettor Heat OFF
2 Choke ON
3 Throttle 25%
4 Fuel Boost Pump ON
5 Propeller Area CLEAR
6 Master Switch ON
7 lgnition Switches ON
8 Joystick FULL BACK
9 Start Button PRESS
10 Check all engine instruments for function
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 Starting Engine -Hot Engine
Proceed as for cold engine above, but choke to be closed
6.5 Warm-Up and Functional Check
Warm-up the engine with a fast idle of 1500 -2000 RPM until the oil temperature reaches 50 degrees C.
During this phase, the cooling is insufficient due to reduced airflow. It is therefore advisable not to shorten
the warm-up time by running the engine at higher RPM. The aircraft should be pointed into wind to allow
additional cooling air. As soon as the oil reaches 50° C, it is possible to do the run-up.

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6.6 Before Take Off
1 Brakes CHECK
2 Cabin Doors CLOSED & LATCHED
3 Flight Controls FREE & CORRECT
4 Flight instruments SET
5 Fuel Shutoff Valve Both ON
6 Elevator Trim NEUTRAL (if present)
7 Flaps SET FOR TAKEOFF
8
Ignition Check
Throttle to 2000 RPM
Switch OFF No. 1 Ignition (key switch) and check if engine
still running.
Switch ON the No. 1 Ignition & switch OFF the No. 2 Ignition
and check if engine still running
Switch No. 2 Ignition ON.
9
Power Check
Throttle to 4500 RPM Open the throttle fully & slowly to
check the maximum RPM being produced. Wind conditions
may effect, but as an average 4300 RPM should be seen.
NOTE If the RPM is found to be more than 300 RPM lower than normal, the engine should be
examined to determine the reason.
10
Idle Check
Throttle to idle position & check that the engine runs
smoothly. With too low an idle speed, or rough running, the
cause must be located & corrected 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 position.
6.7 Taxi Instructions
Normal taxi is provided with throttle, nose wheel and brakes. The right application and coordination makes
taxying easy. Let the speed of the airplane increase slowly and check the brakes operation and direction of
operation. The front wheel is used to control normal operations on the ground. All taxi operations must be
carried out under the lowest speed to ensure non-overloading of the landing gear. Be sure, that along the
landing field are no obstacles during the taxi operation.
6.8 Taxi with headwind
Keep the joystick slightly forward to ensure that the nose wheel will be firmly on the ground and allow for
easier operating.
6.9 Taxi with tail wind
Keep the joystick in the neutral position to avoid the wind making the aircraft “nose dive" flight due the wind
lifting the tail.
6.10 Taxi with cross wind
Keep the joystick "into the wind" to hold balanced wings. The directions will be held by correctly use of
vertical rudder.

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6.11 Take Off
The take off methods depend on various coefficients: height and distance of the next obstacle, kind of the
wind, surface, outside temperature, maximal weight at take off. In addition it’s necessary to note, that under
the speed of 30 knots it is not possible to read airspeed indicator correctly.
6.12 Normal takes off (fully loaded)
Check for airplanes in the area and on final approach and taxi to the middle of the runway, put flaps into
take-off position, slowly introduce the throttle to maximum.. As the take off speed is reached, let the airplane
take off and help with a gentle pull backwards on the joystick normally at about 40-45 knots.
6.13 Short Take Off
Set one notch of flaps, this gives the best gain in lift with the lowest increase in drag. Apply full brake, feed full
throttle, release brakes at full RPM and as the airspeed hits 40 Kts, pull the stick back. As soon as the wheels
leave the ground, relax the back pressure slightly until the airspeed reads 60 Kts, (the increase in speed will
generate more lift). Once past the obstacle, relax the back pressure gradually until airspeed gets to 75 Kts,
then slowly retract the flaps. Continue 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 knots, be sure that you will miss the obstacle.
6.15 Take Off with Cross Wind
Keep the flaps in the neutral position and follow the instructions for a normal takeoff (except for flaps) keep
the runway direction with the rudder pedals. Rise the nose up gently, as usual and operate the joystick and
rudder pedals in accordance with the wind direction, keeping the windward wing down.
6.16 After Take Off
At a safe altitude, decrease the engine RPM and monitor the speed. Operate the airplane as necessary,
retract the flaps (recommended height 500 ft) and trim the plane.
6.17 Climb
The best climb will be reached at the speed of 75 knots, obtained under full engine speed. This will provide
the greatest altitude gain in the shortest time.
6.18 Cruising Flight
4500 RPM (75 % power) speed 110 knots
6.19 Take Off
Normal Take Off
1 Wing Flaps 1st Stage
2 Carburettor Heat COLD – if present
3 Throttle FULL.....OPEN
4 Elevator Control Raise the nose
5 Climb Speed 50 knots until flaps retracted, then 70 knots.
6
At top of Climb, Fuel Boost
Pump
OFF – if fitted
Short Field Take Off
1 Wing Flaps 1st Stage
2
Carburettor Heat
COLD – if present
3
Brakes
APPLY
4
Throttle
FULL OPEN
5
Brakes
RELEASE
6
Elevator Control
Raise the nose
7
Take off Speed
40 knots

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6.20 Landing
Warning: In case of protracted descent with minimal engine speed, the engine can sometimes rapidly cool
and ice can be formed in the carburettor. Therefore we remind you to be aware of carburetor icing.
6.21 Normal Landing (at MTOW)
Fly the descent with power off and with flaps on the second position. During this phase keep the speed at
55-60 knots. After landing (which will be reached in approx. 40 knots), brake carefully with brakes. After the
landing retract the flaps.
Note: Remember, that the landing is not finished after the landing, but after the engine is off. Be careful in
this phase.
6.22 Short Landing
In the final landing phase use full flaps, decrease the descending speed to 40 knots and start to "flare" at
about 2 ft. Remember that the stalling speed with full loading is in this case 38 knots. Land on main wheels.
6.23 Landing with Cross Wind
Use the wing method into the wind (joystick is in the wind direction) and apply opposite pedal to keep the
runway direction.
Shortly before the landing, which should be done only on one main wheel, put the joystick in the middle and
land on all 3 wheels under the gentle wind and on the main landing gear in a strong wind. In case of the
strong wind keep the nose lowered and let 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.
Note: As the airplane will be affected with the cross wind, it leads to rotation around its vertical axis with the
wind direction. The application of flaps increases this tendency. For this reason the application of flaps in
cross wind landings should be limited to prevent ground loops.
6.24 Aborted Landing
If it is necessary to abort the landing use full power. At the moment when sufficient speed or height is
reached retract the flaps.
6.25 Stall
This airplane has good stability and flight features. The features of the stall of this airplane are normal and
gentle. It will be possible to notice the stall coming on by the pull of the joystick.
6.26 Balancing the Stall
The construction philosophy of this plane is to climb at speeds just above the stall. For this reason the
recovery from stall will be with minimal height loss. The airplane could be recovered from the stall very
quickly by reducing pressure of the joystick, but absolutely avoid too sudden a manoeuvre to avoid unwanted
tilt, and at the same time apply full throttle.
6.27 After Landing
Leave the runway and park the airplane.
Switch off the second ignition switch and stop the engine with keyed switch. Turn off all switches and fuel
taps. Pull out the starter key and chock the wheels. Cover the pitot tube. Secure the airplane. Tie as
required.

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6.28 Enroute Climb
1 Airspeed 75 knots
2 Throttle FULL OPEN
NOTE: During climb, monitor the water & oil temperatures to avoid exceeding their limits.
The aircraft has been tested to ensure adequate cooling in climb, therefore any excessive
readings may indicate a malfunction. Should this occur, decrease the rate of climb in order
to increase the airspeed for improved cooling.
6.29 Cruise
1 Power 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 ON
6.31 Landing
Normal Landing
1 Airspeed 50 knots
2 Wing flaps 1 stage
3 Touchdown Main wheels first
4 Braking Minimum required
Short Field Landing
1 Airspeed 45 knots
2 Wing Flaps 2 stage
3 Power REDUCE to idle as obstacle is cleared
4 Touchdown Main wheels first
5 Brakes APPLY AS REQUIRED
6 Wing Flaps RETRACT AFTER THE STOP
6.32 Missed Approach
1 Throttle FULL OPEN
2 Carburettor Heat OFF
3 Airspeed 60 knots until clear of obstacles
4 Wing Flaps Retract

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6.33 Fuelling
SAFETY WARNINGS
Never prepare fuel in an area that is enclosed or where fumes could reach ignition point. DO NOT SMOKE
or allow open flames or sparks in the vicinity. Never add fuel while the engine is running.
Use only approved fuel containers. Never transport fuel in an unsafe manner.
Always check for fuel contamination. Contamination is a major cause of engine failure. The best place to
avoid contamination is at the source. Once your fuel is in the container a very hazardous potential exists.
Use a clean safety approved storage container. Do not overfill the container -allow for expansion.
We recommend the use of a funnel filter.
The engine is designed for use with unleaded MOGAS and AVGAS.
Always earth the aircraft through the Earthing Point provided at the engine muffler.
Before first flight of the day, and after each refuelling, use a sampler cup and drain a small quantity of fuel
from the fuel drain valve -check for water, sediment and contamination.
6.34 Filling the Tank
When fuelling from a pump to a full tank condition lift 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 happens quickly remove the fuel cap to break the siphon. (TAKE CARE OF
WINDOWS!)
6.35 Propeller Care
Full throttle run up over loose gravel is especially harmful to propeller tips. When takeoffs must be made over
a gravel surface, it is very important that the throttle is advanced slowly. This allows the airplane to start
rolling before high RPM is developed, and the gravel will be blown behind the propeller rather than pulled
into it. When unavoidable small nicks appear in the propeller, they should be immediately fixed.
6.36 Noise Abatement
Increased emphasis on improving the quality of our environment requires renewed effort on the part of all
pilots to minimize the effect of airplane noise on the public.
As pilots, we can demonstrate our concern for environmental improvement by application of the following
procedures:
1 At altitudes under 2000 feet, avoid flying in close proximity to houses or over parks and recreational areas
2 During approach to or departure from an airport, climb after takeoff and descent for landing should be
made so as to avoid prolonged flight at low altitude near noise sensitive areas.

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6.37 Cleaning Of Windows
Cleaning only 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 Engine
To stop the engine, turn OFF the second ignition switch and turn OFF the keyed switch or master switch.

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7.0 Emergency Procedures
Emergencies caused by aeroplane malfunctions are rare if proper pre-flight inspections and maintenance are
practiced. En route weather emergencies can be minimised or eliminated by careful flight planning and good
judgement when unexpected weather is encountered. However, should an 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 knots
Manoeuvring Speed (at all weights)
75 knots
Maximum Glide Distance, Still Air
75 knots
Precautionary Landing Approach with Engine Power 45 knots
Landing Approach Without Engine Power
Landing Flaps Up
Landing Flaps Down
50 knots
45 knots
Note: A slightly higher speed may give better distance over the ground if gliding into wind; a slightly lower
speed if gliding downwind.

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8.0 Operational Checklists
8.1 Engine Failures
8.2 Engine Failure during Takeoff Run
1 Throttle ldle
2 Brakes Apply
3 Ignition Switches OFF
4 Master Switch OFF
8.3 Engine Failure Immediately After Takeoff
1 Move the control stick FORWARD to maintain 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 gliding into wind; a slightly lower
speed if gliding downwind
8.4 Airstart & Limitations
In the event that the engine is stopped during flight, it may be restarted by application of fuel & ignition.
Note : The engine cools quickly with the Propeller stopped. Choke may need to be used to start if
time between restart is longer.

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8.5 Fire
8.6 Fire during Start on Ground
1
Cranking
CONTINUE to get a start that would suck the flames and
accumulated fuel through the carburettor and into the engine.
If engine starts,
2 Power 2500 RPM
3
Fuel OFF & allow engine to empty carburettor
4
Engine Inspect for damage
If engine fails to start,
5
Cranking
CONTINUE in an effort to obtain a start. If no start in 15 seconds :
Shut off fuel & continue to crank for another 15 seconds.
6
Engine SECURE.
A Second Ignition Switch OFF
B Master Switch OFF
C Fuel Shutoff Valves Both OFF
7
Fire Extinguish using fire extinguisher, wool blanket, or dirt.
8
Fire Damage
Have authorised people inspect, repair damage or replace
damaged components or 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 fire is not extinguished, increase glide speed to find an
airspeed which will provide an incombustible mixture).
7
Forced Landing
Execute (as described in Emergency Landing Without Engine
Power).
8.8 Electrical Fire in Flight
1 Master Switch OFF
2 All Other Switches OFF
3 Vents/cabin air (*) OPEN THE CABIN DOOR
If fire appears out and electrical power is necessary for continuance of flight:
4 Master Switch ON
5
Second Ignition Switch
ON
6
Fuses
CHECK for faulty circuit, DO NOT reset or replace.
7
Radio/Electrical Switches
ON one at a time, with delay after each switch until short
circuit is localised.
8
Land as soon as possible to inspect for damage
8.9 Cabin Fire
1 Master Switch OFF
2 Vents/Cabin Air (*) / Door OFF
3 Land as soon as possible to inspect for damage.