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Publication

JP OM15

Jabiru J400

Owners Manual

Section: 0

REVISION

0

Dated: SEPT 00

Page 0-9 of 9

AIRPLANE PERFORMANCE AND FLIGHT PLANNING

TERMINOLOGY

MAXIMUM CROSSWIND
VELOCITY

The velocity of the crosswind component for which
adequate control of the airplane during takeoff and
landing was actually demonstrated during the
certification tests. The value shown is limiting.

USEABLE FUEL

The fuel available for flight planning

UNUSABLE FUEL

The quantity of fuel that cannot be safely used in flight

LPH LITRES PER
HOUR

The amount of fuel ( in litres ) consumed per hour

NMPL NAUTICAL
MILES PER LITRE

The distance ( in nautical miles ) which can be
expected per litre of fuel consumed at a specific engine
power setting and/or flight configuration.

g

The acceleration due to gravity.

WEIGHT AND BALANCE TERMINOLOGY

STATION

Only two load stations are specified: ie Seat Station
which is the centre of the fixed seats and Fuel Station
which is the centre of the fixed fuel tank.

C.G. CENTRE OF
GRAVITY

The point at which an airplane, or equipment, would
balance if suspended.

C.G. LIMITS

The extreme centre of gravity locations within which the
airplane must be operated at a given weight.

STANDARD EMPTY
WEIGHT

The weight of a standard airplane, including unusable
fuel, full operating fluids and full engine oil.

BASIC EMPTY WEIGHT

The standard empty weight plus the weight of optional
equipment.

USEFUL LOAD -

The difference between ramp weight and the basic
empty weight.

MTOW MAXIMUM
TAKEOFF WEIGHT

The maximum weight approved for the start of the
takeoff run.

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Содержание J400

Страница 1: ...URER Jabiru Aircraft Pty Ltd Airport Drive Bundaberg Queensland 4670 Australia Postal Address P O Box 5186 Bundaberg West Queensland 4670 Australia Telephone 07 4155 1778 int 61 7 4155 1778 Email Info...

Страница 2: ...Owners Manual Section 0 APPROVAL PAGE Nationality and Registration Marks Australia Manufacturer Jabiru Aircraft Pty Ltd Designation of Aircraft J400 Registration Number Aircraft Serial Number REVISIO...

Страница 3: ...iru J400 Owners Manual Section 0 TABLE OF CONTENTS SECTION General 1 Limitations 2 Emergency Procedures 3 Normal Procedures 4 Performance 5 Weight and Balance Statement 6 Supplements 7 REVISION 0 Date...

Страница 4: ...ndment No Paragraph s Affected Signature Date of Incorporation Incorporation of a General Amendment should be certified by inserting the date of incorporation signature in the appropriate columns All...

Страница 5: ...dditional limitations and instructions are listed in the Supplements Section and this section shall be consulted before undertaking any such operations For operating information not included in this m...

Страница 6: ...this Manual in a current status when it is being used for operational purposes Owners should contact JABIRU AIRCRAFT PTY LTD whenever the revision status of their Manual is in question A revision bar...

Страница 7: ...normally be exceeded Operations above the Normal Operating Speed shall be conducted with caution and only in smooth air Va MANOEUVRING SPEED Maximum for manoeuvres involving an approach to stall cond...

Страница 8: ...atest gain in altitude in a given time METEOROLOGICAL TERMINOLOGY OAT OUTSIDE AIR TEMPERATURE The free static air temperature It is expressed in either degrees Celsius or degrees Fahrenheit STANDARD T...

Страница 9: ...umed at a specific engine power setting and or flight configuration g The acceleration due to gravity WEIGHT AND BALANCE TERMINOLOGY STATION Only two load stations are specified ie Seat Station which...

Страница 10: ...______________________________ 3 1 2 2 PROPELLER __________________________________________________________ 3 1 2 3 APPROVED FUEL TYPES AND GRADES_________________________________ 3 1 2 4 FUEL CAPACIT...

Страница 11: ...Publication JP OM15 Jabiru J400 Owners Manual Section 1 REVISION 0 Dated SEPT 00 Page 1 2 of 4 1 1 THREE VIEW DRAWING Ground Turning Radius 6 4 metres Section 1 GENERAL GENERAL GENERAL GENERAL...

Страница 12: ...ameter 60 inches 1524 mm Pitch 53 inches 1346 mm 1 2 3 APPROVED FUEL TYPES AND GRADES 100 LL or 100 130 grade aviation gasoline 1 2 4 FUEL CAPACITY Total 140 0 litres Useable 138 0 litres 1 2 5 APPROV...

Страница 13: ...Publication JP OM15 Jabiru J400 Owners Manual Section 1 REVISION 0 Dated SEPT 00 Page 1 4 of 4 1 2 7 TYRE INFLATION PRESSURES Standard Mains 168 kpa 24 psi Nose 84 105 kpa 12 15 psi...

Страница 14: ...____________________3 2 6 POWERPLANT LIMITATIONS ___________________________________________4 2 7 OTHER LIMITATIONS__________________________________________________4 2 7 1 AUTHORISED MANOEUVRES AND A...

Страница 15: ...cluded in this section are observed 2 2 TYPE OF OPERATION VFR by Day No aerobatics including Spins 2 3 AIRSPEED LIMITATIONS Airspeed limitations and their operational significance are shown below SPEE...

Страница 16: ...imit is max structural cruising speed Yellow Arc 91 138 Operations must be conducted with caution and only in still air Red Line 138 Vne 2 4 WEIGHTS and LOADING Maximum takeoff weight 700 kg Maximum l...

Страница 17: ...f Needle must be seen to move off the stop before Takeoff Minimum Oil Pressure in Level Flight or climb 220 kPa In Descent 80 kPa Maximum Cylinder Head Temperature 175oC 347oF Maximum RPM for all oper...

Страница 18: ...nual Section 2 40oc for takeoff at gross weight 2 7 4 FLIGHTS WITH DOORS REMOVED Prohibited 2 7 5 MAXIMUM PERMISSIBLE NUMBER OF OCCUPANTS Four including Pilot 2 7 6 MAXIMUM CROSSWIND VELOCITY 14 knots...

Страница 19: ...Wing Spar Carry through Beam in the Cabin Ceiling Owners Manual P No 5036194 FLIGHT OWNERS MANUAL Fitted to Inside of RH Door above the Door Pocket Door Open LHS P No5027094 OPEN Fitted to the Outside...

Страница 20: ...elage of RHS of cabin between Door and Rear Window P No5098694 1 Cockpit Controls Trim Position P No5024094 NOSE DOWN NEUTRAL TRIM NOSE UP BRAKE ON Fitted on the Top of the Main Beam Beside the trim c...

Страница 21: ...c Tube Electrical Earthing P No 5078064 EARTH ON NOSE LEG Attach above the Earthing Pole adjacent to the Fuel Filler Cap Fuel Grade P No 5091064 2 OFF FUEL AVGAS 100LL 70 Litre Capacity Earth on Post...

Страница 22: ..._____________________6 ELECTRICAL FIRE IN FLIGHT_____________________________________________________6 CABIN FIRE_____________________________________________________________________7 3 3 3 FORCED LAN...

Страница 23: ...ountered However should an emergency arise the basic guidelines outlined in this section should be considered and applied as necessary to correct the problem 3 2 AIRSPEEDS FOR EMERGENCY OPERATION Engi...

Страница 24: ...Airspeed 80 KIAS 2 Fuel Shutoff Valve OFF 3 Ignition Switches OFF 4 Wing Flaps as required 5 Master Switch OFF ENGINE FAILURE DURING FLIGHT 1 Airspeed Best Glide Angle 80 KIAS 1 2 Carburetor Heat ON...

Страница 25: ...herefore the following procedure addresses only airstarts by use of the Starter Motor IMPORTANT DO NOT depress starter button while propeller is rotating 1 Ignition Switches OFF 2 Cabin Clear 3 Increa...

Страница 26: ...tart 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 Fire Extinguisher Obtain have ground attendants obtain if not...

Страница 27: ...ixture 8 Forced Landing Execute as described in Emergency Landing Without Engine Power ELECTRICAL FIRE IN FLIGHT 1 Master Switch OFF 2 All Other Switches OFF 3 Vents cabin air OPEN If fire appears out...

Страница 28: ...to inspect for damage 3 3 3 FORCED LANDING EMERGENCY LANDING WITHOUT ENGINE POWER 1 Airspeed 80 KIAS flaps UP Approach 65 KIAS flaps DOWN 2 Fuel Shutoff Valve OFF 3 Fuel Pump OFF 4 Ignition Switches O...

Страница 29: ...75 KIAS 2 Wing Flaps 1st Stage 3 Fuel Pump ON 4 Selected Field FLY OVER Note terrain and obstructions 5 Radio and Electrical Switches ON 6 Wing Flaps FULL on final approach 7 Airspeed 65 KIAS 8 Touch...

Страница 30: ...tablish 50 ft min descent at 65 KIAS 6 Touchdown level attitude 7 Face Cushion at touchdown with folded coat or cushion 8 Aeroplane Evacuate through cabin doors If necessary breakout windows and flood...

Страница 31: ...ermits by stopping propeller windmilling This can be achieved by slowing below 50 knots 3 3 6 RECOVERY FROM AN INADVERTENT SPIN Aerobatic manoeuvres including spins are prohibited While inadvertent sp...

Страница 32: ...arburettor heat is not to be used during takeoff or climb also because it creates a small power loss IMPORTANT During descent approach the carburettor heat should be used because low power settings cr...

Страница 33: ...enroute should the engine fail 2 Gradual reduction in oil pressure below observed normal position Action Observe oil temperature indications If oil temperature is higher than normal indications and a...

Страница 34: ..._______________________________________ 11 4 3 11 LANDING _____________________________________________________________ 12 4 3 12 AFTER LANDING______________________________________________________ 12...

Страница 35: ...Flap 75 KIAS Short Field Takeoff 1st Stage Flap Speed at 50 Feet 71 KIAS When Clear of obstacles retract flaps and climb at 85 KIAS Climb Flaps Up Normal 85 KIAS Best Rate of Climb at low altitude 85...

Страница 36: ...ers Manual Section 4 Then retract flap fully and continue to climb at or above 85 KIAS Maximum Recommended Turbulent Air Penetration Speed 91 KIAS Maximum Demonstrated Crosswind Velocity 14 Knots REVI...

Страница 37: ...the following checklists and in the sequence shown in the following diagram NOTE Visually check airplane for general condition during walk around inspection In cold weather remove even small accumulat...

Страница 38: ...elt Fastening 3 Ignition Switches OFF 4 Master Switch OFF 5 Fuel Shutoff Valve ON 6 Seatbelts and Shoulder Harnesses CHECK condition and security 7 Aileron Cable Mountings Rod Ends CHECK for free rota...

Страница 39: ...of movement security 2 Flap CHECK security 3 Control Rods Cables CHECK aileron flap control bolts nuts flap control rod for security CHECK rod ends for freedom of rotation excessive movement 7 RIGHT W...

Страница 40: ...inflation wear or damage 9 LEFT WING 1 Main Wheel Tyre CHECK for proper inflation wear or damage 2 Wing Strut Mount Bolts CHECK for security CAUTION Wing Strut attachment bolts must be free to rotate...

Страница 41: ...ON 7 Ignition Switches ON 8 Start Button PRESS 9 Note If the engine is cranking below 300 RPM it will not start As soon as engine is running throttle back to an idle speed of 900 1000 RPM 10 Check all...

Страница 42: ...rs CLOSED LATCHED 3 Flight Controls FREE CORRECT 4 Flight Instruments SET 5 Fuel Shutoff Valve ON 6 Elevator Trim NEUTRAL 7 Flaps SET FOR TAKEOFF 8 Ignition Check Throttle to 2000 RPM Hold this engine...

Страница 43: ...g the cause must be located corrected to avoid the potential for an in flight stoppage 11 Carburettor Heat Check Throttle up to 2000 RPM Pull out the Carburettor Heat Control look for an RPM drop Retu...

Страница 44: ...PEN NOTE During climb monitor the cylinder head oil temperatures to avoid exceeding their limits The aircraft has been tested to ensure adequate cooling in climb therefore any excessive readings may i...

Страница 45: ...dle as obstacle is cleared 4 Touchdown MAIN WHEELS FIRST 5 Brakes APPLY AS REQUIRED 6 Wing Flaps RETRACT when convenient for better braking Baulked Landing 1 Throttle FULL OPEN 2 Carburettor Heat COLD...

Страница 46: ...ed fuel containers and 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 sou...

Страница 47: ...in directional control and balance The carburettor heat control knob should be pushed full IN that is NOT selected during all ground operations unless heat is absolutely necessary Taxiing over loose g...

Страница 48: ...Publication JP OM15 Jabiru J400 Owners Manual Section 4 Figure 4 1 Taxiing Diagram REVISION 0 Dated SEPT 00 Page 4 15 of 15...

Страница 49: ...ted into the wind the airplane is accelerated to a speed slightly higher than normal and then pulled off positively and smoothly to prevent possible settling back to the runway while drifting When cle...

Страница 50: ...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 an...

Страница 51: ...ine from an external power source Remove Top cowl Place jumper leads directly on battery terminals ensuring positive to positive and negative to negative Start as for normal operation Stop engine remo...

Страница 52: ...___________________________________________________________2 5 1 1 STALL SPEEDS __________________________________________________________ 2 5 1 2 NATURE OF STALL WARNING _____________________________...

Страница 53: ...ing Zero Stage 1 Takeoff Stage 2 Landing Maximum Takeoff Landing Weight 60 54 50 5 1 2 NATURE OF STALL WARNING Configuration Stall Warning Power Off Clean Flap Stage 1 Flap Stage 2 Audible Warning hor...

Страница 54: ...wind or slope on a short dry grass surface is 400 metres The sea level take off strip length exceeds the landing strip length Takeoff and Landing Distance is therefore 400 metres times 1 3 520 metres...

Страница 55: ..._________ 4 6 3 3 Calculating the Operating CG Locations __________________________________ 4 6 3 3 1 Allowable Trim Conditions____________________________________________________6 6 4 Weight Limits _...

Страница 56: ...Empty Weight Record Registration No Aircraft Model Serial Number Date of Weighing Empty Aircraft Weight kg Empty Aircraft Arm mm aft of datum Aircraft Moment kg mm Trim Sheet IndexUnits Fixed Ballast...

Страница 57: ...en in Figure 6 1 The chart is based on an aircraft EMPTY WEIGHT TRIM INDEX which is calculated using the following formula Aircraft Empty Weight Empty Weight Arm Empty Weight Trim Index 1000 Example T...

Страница 58: ...he point made in Step 7 to enter the Take Off Fuel Quantity Scale and mark a point This point is the Zero Fuel Weight Reference Point 1 9 Move Horizontally to the left of the Zero Fuel Reference Point...

Страница 59: ...ep 2 4 to intersect a sloping purple line in the Blue Baggage Calculation Box and mark a point at this location 2 6 Estimate the weight of baggage stowed in the baggage compartment behind the rear sea...

Страница 60: ...en both the Zero Fuel Condition and the Take Off Condition fall with the area bounded by the Line in the Aircraft Trim Conditions Graph REVISIO N 0 1 2 Dated July 02 Page 6 C Documents and Settings Ad...

Страница 61: ...o Fuel Condition and Take Off Condition Must Lie Within Blue Boundary Aircraft Weight kg Aircraft Weight kg 200 220 240 260 280 300 320 340 360 380 400 420 440 460 480 500 520 540 560 580 600 620 640...

Страница 62: ...craft Trim Conditions For Correct Balance Zero Fuel Condition and Take Off Condition Must Lie Within Blue Boundary Aircraft Weight kg Aircraft Weight kg 200 220 240 260 280 300 320 340 360 380 400 420...

Страница 63: ...0 mm aft of datum at all weights Datum Wing Leading Edge Leveling Means Longitudinal Spirit Level placed on the trim control lever decal Lateral Spirit Level placed across the fuselage forward of the...

Страница 64: ...rcraft at manufacture and were included in the aircraft basic weight Generic Item Specific Item Description Engine Jabiru 3300 Propeller Jabiru Fixed Pitch Wooden P No C000262 D60P43 Flight Instrument...

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