Page 1
THIS DOCUMENT MUST BE CARRIED IN THE AIRCRAFT AT ALL TIMES THIS AIRCRAFT MUST BE OPERATED IN ACCORDANCE WITH THE APPROVED DATA AND LIMITATIONS CONTAINED IN THIS MANUAL AT ALL TIMES. ANY PERSON FINDING THIS MANUAL IS REQUESTED TO RETURN IT TO JABIRU AIRCRAFT...
Page 2
Placards added, performance data altered. Layout revised per ASTM F2746 Review per ASTM F2746-12, US compliant placards, Weight and Balance and imperial units added for Jabiru USA Omissions and Errors corrected Minimum Take-off Oil temp corrected to be 40 C (104 Oil spec changed to SAE J-1899 (MIL-L-22851 obsolete) (section 8.6)
USE OF METRIC/IMPERIAL UNITS ................13 WARNINGS, CAUTIONS & NOTES ................13 GENERAL INFORMATION ..................... 14 LIGHT SPORT AIRCRAFT NOTIFICATION ..............14 ABOUT THE JABIRU J230-D ..................15 OWNER/OPERATOR RESPONSIBILITES ..............16 J230-D PERFORMANCE & SPECIFICATION SUMMARY ........... 17 LIMITATIONS ......................... 18 AIRSPEED LIMITS ......................
Page 4
Jabiru Aircraft Pilot Operating Handbook Model J230-D SPEEDS FOR NORMAL OPERATION ................. 36 BEST ANGLE OF CLIMB SPEED ................. 36 BEST RATE OF CLIMB SPEED ................... 36 PREFLIGHT INSPECTION ..................37 4.4.1 Remove Covers / Release Aircraft ................ 37 4.4.2 Pre-flight Inspections.....................
The basic POH provides all the information, procedures and limitations required to operate the aircraft as a Light Sport Aircraft. This basic POH is applicable to all Jabiru J230-D Aircraft. The operating procedures presented herein are the result of Jabiru Aircraft’s knowledge and experience gained up to the date of issue of this handbook.
Jabiru Aircraft Pilot Operating Handbook Model J230-D 0.1 SUPPORTING DOCUMENTATION The following manuals are required for correct operation & maintenance of the Jabiru J230-D. The current revisions are available free of charge from the Jabiru Aircraft website www.jabiru.net.au Pilot’s Operating Handbook...
Page 8
Jabiru Aircraft Pilot Operating Handbook Model J230-D JP-FM-09 Revision: 28/2/2020 Page 8...
Jabiru Aircraft Pilot Operating Handbook Model J230-D 0.4 SYMBOLS, ABBREVIATIONS AND TERMINOLOGY Ampere Above Ground Level AMSL Above Mean Sea Level AVGAS Aviation Gasoline Brake Horse Power CASA Civil Aviation Safety Authority (Australia) Civil Aviation Order (Australia) Civil Aviation Regulation (Australia) °C...
Page 10
Jabiru Aircraft Pilot Operating Handbook Model J230-D Outside Air Temperature Passenger Pilots Operating Handbook PROP Propeller Pounds per square inch Quantity Quarts Right Hand Right Hand Side Fuel Octane Rating Scale (Research Octane Number) Revolutions per minute Society of Automotive Engineers...
Page 11
Jabiru Aircraft Pilot Operating Handbook Model J230-D • Operating Manoeuvring Speed: the speed that an aircraft will stall in a nose- up pitching manoeuvre before exceeding structural limits. V cannot exceed √. • Never Exceed Speed: the limiting airspeed that may not be exceeded at any time.
Page 12
Jabiru Aircraft Pilot Operating Handbook Model J230-D Weight and Balance Terminology • Datum – An imaginary vertical plane from which all horizontal distances are measured for balance purposes. • Station – A location along the aircraft fuselage usually given in terms of distance from the reference datum.
Jabiru Aircraft Pilot Operating Handbook Model J230-D 0.5 USE OF METRIC/IMPERIAL UNITS This POH uses the metric system as the basic system of measurement. Where common usage or available instrumentation refer to the Imperial/US unit system, both units are quoted. The following conversion factors are presented as a ready reference to the conversion factors that have been used in this manual as well as supplying some others that may be found useful.
Jabiru Aircraft Pty Ltd has devoted significant resources and testing to develop the Jabiru J230-D aircraft. The Jabiru J230-D is designed to be operated and maintained only in strict accordance with its supporting documentation – consisting of Pilot’s Operating Handbook,...
2 seat aircraft powered by a 2-stroke engine; it had limited range, basic equipment and little room to spare in the cabin. But this aircraft introduced the Jabiru ideal to the world – an aircraft which was light and efficient with good handling, good performance and excellent occupant protection.
Jabiru Aircraft Pilot Operating Handbook Model J230-D 1.2 OWNER/OPERATOR RESPONSIBILITES The following responsibilities for the owner/operator of a LSA listed are prescribed in the ASTM standard F2295: • Each owner/operator of a LSA shall read and comply with the maintenance and continued airworthiness information and instructions provided by the manufacturer.
Jabiru Aircraft Pilot Operating Handbook Model J230-D LIMITATIONS 2.0 AIRSPEED LIMITS SPEED KIAS ASI MARKING REMARKS Do not make full or abrupt Design Manoeuvring Speed (V control movements above this speed. Do not make full or abrupt Operating Manoeuvring Speed at...
Jabiru Aircraft Pilot Operating Handbook Model J230-D 2.2 LIMIT LOAD FACTORS Flap Position Speed Positive Negative + 4g + 4g -2-g DOWN + 2.0g 2.3 FLIGHT OPERATION LIMITATIONS Manoeuvres in the course of normal flying are approved. Stalls may be carried out at bank angles of up to 60°.
2.9.1 JABIRU USA ONLY The J230-D is equipped for Night VFR as standard and must carry the Jabiru J230-D Night VFR Operations Supplement (Document Number JP-MS-06). Note Carrying out Night VFR Operations without a valid, endorsed Pilot Licence, Night VFR Operations Supplement &...
To reduce the load on the alternator and maintain the battery at peak voltage, Jabiru Aircraft recommend only using the Landing Light for takeoff and landing – turning it off during normal cruise operations and wherever safe while taxiing.
Jabiru Aircraft Pilot Operating Handbook Model J230-D EMERGENCY PROCEDURES 3.0 GENERAL This section describes the procedures to be adopted in the event of an emergency or abnormal situation occurring in the J230-D aircraft. The procedures are arranged in the sequence considered to be the most desirable in the majority of cases.
Jabiru Aircraft Pilot Operating Handbook Model J230-D 3.2 CARBURETTOR ICING Carburettor icing occurs when moisture in the air forms ice within the carburettor – typically in the venturi throat and around the throttle butterfly. The ice restricts airflow and prevents the proper function of the carburettor.
The propeller may stop windmilling below 50 KIAS The Jabiru engine is a high compression engine & therefore airstarts when the propeller has stopped rotating, without the use of the starter, are unlikely before reaching V .
Jabiru Aircraft Pilot Operating Handbook Model J230-D 3.3.3 Forced Landings Emergency Landing Without Engine Power Airspeed ..............65 KIAS Ignition ..............OFF Fuel Shutoff Valve ..........OFF Fuel Pump ............. OFF Throttle ..............CLOSED Wing Flaps ............FULL PRIOR TO TOUCH DOWN Master Switch ............
Page 27
Jabiru Aircraft Pilot Operating Handbook Model J230-D Engine Fire In Flight Throttle .............. CLOSE Fuel Valve............OFF Fuel Pump ............OFF Ignition ............... OFF Master Switch ............ OFF AFTER FLAPS DEPLOYED Cabin Heat Vent ..........CLOSE Cabin Air Vent ........... OPEN BOTH Airspeed ............
Jabiru Aircraft Pilot Operating Handbook Model J230-D 3.3.5 Other Emergencies In some of the cases described below there is more than 1 potential cause for a given situation. For example, if the oil pressure gauge indicates zero, it may be due to a failure of the gauge or sender instead of an actual problem with the engine.
Page 29
Non-essential electrical equipment ....OFF Land ..............AT NEAREST AIRPORT NOTE The Jabiru Engine does not require external power to run: the engine will not stop if the aircraft battery runs flat. Overvoltage Electrical equipment........... ALL ON – MONITOR VOLTAGE RPM ..............
Page 30
Jabiru Aircraft Pilot Operating Handbook Model J230-D Flight into known icing conditions is prohibited. If icing is inadvertently encountered, change flight level or turn back to a region less conducive to icing. Monitor ice formation on the airframe and its effects on aircraft performance.
Page 31
Jabiru Aircraft Pilot Operating Handbook Model J230-D Inadvertent Operation in Light Rain RPM ..............REDUCE: 2200 – 2400 RPM Flaps..............TAKE-OFF (first stage) Carburettor heat ..........ON Aircraft Position / heading ........AWAY FROM RAIN WARNING The J230-D is not designed or approved to fly in heavy rain. The above is included for inadvertent operation in light rain only.
Page 32
Jabiru Aircraft Pilot Operating Handbook Model J230-D Loss of Flight Controls It is a requirement of the design standard that the following section be included in this manual, however such failures are extremely rare. As always, the 3 key rules apply: Maintain Aircraft Control.
Jabiru Aircraft Pilot Operating Handbook Model J230-D 3.4 AMPLIFIED EMERGENCY PROCEDURES This section is provided to supply the pilot with additional information concerning emergency procedures in general. Elaboration of the procedures specified in the EMERGENCY PROCEDURES CHECK LISTS as well as the inclusion of some more generalised emergency procedures that can be better covered by a general descriptive procedure rather than a formal check list are included in this section.
Jabiru Aircraft Pilot Operating Handbook Model J230-D 3.4.4 Ditching The aircraft has not been flight tested in actual ditchings, therefore the recommended procedure is based entirely on the best judgement of the manufacturer. If available, life jackets should be donned but not inflated until after evacuating the aircraft.
If the battery charge drops sufficiently electrical systems will fail. While the Jabiru engine does not require external power while running, devices such as radios, transponders, GPS units, and intercoms will eventually drain the battery.
Jabiru Aircraft Pilot Operating Handbook Model J230-D NORMAL PROCEDURES GENERAL This section describes the procedures to be adopted for normal operations of the J230-D aircraft. The procedures are arranged in the sequence considered to be the most desirable and therefore steps should be performed in the order listed unless good reasons for a deviation exist.
Jabiru Aircraft Pilot Operating Handbook Model J230-D 4.4 PREFLIGHT INSPECTION Before flight, a careful visual inspection is to be carried out to ensure that the aircraft and its systems are serviceable. Aircraft must be placed in a clear area of level ground to carry out the inspection.
A hot engine may fire with the ignition/s switched OFF. DO NOT pull through a hot engine. CAUTION Several causes of irregular compression – such as leaking valves – can lead to extensive engine damage if not addressed. The Jabiru Engine Maintenance Manual provides additional details. Propeller Propeller ...........CHECK for damage & security Spinner .............CHECK for damage, wear, hardware.
Jabiru Aircraft Pilot Operating Handbook Model J230-D Control rods & cables ....... CHECK Security. Check rod ends for freedom of rotation & excess movement. * - Holding the wingtip, push the tip up & down, forwards & backwards. If a wing / strut attachment is degrading, free-play will be felt.
Jabiru Aircraft Pilot Operating Handbook Model J230-D 10. Fuel Quick Drains Test fuel at each drain ......CHECK for contamination 11. Stand Back Inspection Stand back from the aircraft & check for anything “out of place”. i.e: assuming the aircraft is on flat ground if the wingtips are not level it can indicate damage to the undercarriage.
Jabiru Aircraft Pilot Operating Handbook Model J230-D 4.6 Before Take-Off 4.6.1 Ground Check & Run Up Warm Up ..........1000-1200 RPM avoid prolonged idle at low RPM Ignition Check ..........2000 RPM Both-L-Both-R-Both. Max drop 100RPM Carburettor heat ........2000 RPM – ON – slight drop in RPM Carburettor heat ........2000 RPM –...
4.9.3 Starting Engine The Jabiru 3300 engine is fitted with a dual electronic ignition system. The engine will not start below 300 RPM, which precludes the option of hand swinging or "propping" an engine when there is insufficient charge available in the aircraft battery for a normal start. Starting using an external...
Flight should not be undertaken with a faulty battery. It could cause failure of the electrical system. The charging system in the Jabiru is not designed to be flown with a flat or faulty battery. If external power is required to start the engine the batteries condition should be verified.
Jabiru Aircraft Pilot Operating Handbook Model J230-D Most of the warm up will have occurred during taxiing and whilst conducting the Before Take-Off checks. The engine is warm enough for take-off when the cylinder head and oil temperatures are in the green arcs.
Jabiru Aircraft Pilot Operating Handbook Model J230-D 4.9.10 Stalls In any attitude or under any loading condition there is no natural stall warning. An artificial stall warning horn is set to activate 5 to 10 KIAS above the stall speed in any configuration. All controls are effective up to and completely through the stall and there is no noticeable tendency to enter a spin after the stall.
Jabiru Aircraft Pilot Operating Handbook Model J230-D 4.10 Advanced Procedures The following procedures are advanced techniques designed for special circumstances. To carry them out successfully the pilot must be well trained and experienced in the particular aircraft being used. Before attempting them the pilot must realistically assess the circumstances and their skills.
Jabiru Aircraft Pilot Operating Handbook Model J230-D 4.10.2 Short Field Landing Approach ..........FLAT. Aim for wheels to touch as near to the target point as possible. Approach under power. Power ............APPROX 1500 RPM Airspeed ..........55 KIAS Touch-down..........AT TARGET POINT. Wheel brakes are the best way to slow the aircraft.
Jabiru Aircraft Pilot Operating Handbook Model J230-D NOTE Soft field take-offs are potentially high risk manoeuvres with reduced safety margins, especially in a cross wind, wind gust or if the engine fails. Where possible, they should only be attempted in good conditions.
Crosswind Landing – “Wing Low” Method 4.10.6 Jabiru Aircraft recommend using the “wing low” method of landing in crosswinds as it allows the strength of the crosswind to be continually assessed during the final approach and is less likely to cause directional control issues on touch-down.
Jabiru Aircraft Pilot Operating Handbook Model J230-D directional control. Power ............IDLE Brakes ............AS NEEDED. DO NOT LOCK WHEELS. Aileron / Elevator Deflection .....MAINTAIN: in strong wind the aircraft must be “flown” during ground operations to minimise the risk of being flipped.
Jabiru Aircraft Pilot Operating Handbook Model J230-D 4.10.8 S-Turns S-turns are a means of losing excess height during the landing approach to position the aircraft correctly for touch-down. Essentially the pilot flies the aircraft through a sequence of left and right turns within an arc of 90°...
Jabiru Aircraft Pilot Operating Handbook Model J230-D PERFORMANCE 5.0 TAKE OFF AND LANDING DISTANCES Take-Off Distance to 50’ (Factored) 392 m (1286 ft) Take-Off Ground Roll (Factored) 249 m (817 ft) Landing Distance from 50’ (Factored) 588 m (1929 ft)
Jabiru Aircraft Pilot Operating Handbook Model J230-D 5.2 CRUISE SPEEDS / RPM / FUEL CONSUMPTION • Cruise speed values given are based on tests carried out at gross aircraft weight, at sea level and 28°C (82°F). Values are averaged. Actual values will vary slightly from one aircraft to the next.
Jabiru Aircraft Pilot Operating Handbook Model J230-D WEIGHT AND BALANCE INFORMATION 6.0 CG RANGE 99-mm (3.9”, 10%MAC) aft of datum up to & including 600 Forward Limit: kg (1320lb) 277-mm (10.9”, 28 %) aft of datum at all weights Aft Limit...
Jabiru Aircraft Pilot Operating Handbook Model J230-D 6.1 BAGGAGE ZONES The cabin has two baggage zones: Figure 6.1 – Baggage Zones Baggage is restrained using the straps fitted in the baggage areas. JP-FM-09 Revision: 28/2/2020 Page 58...
Jabiru Aircraft Pilot Operating Handbook Model J230-D 6.2 MINIMUM EQUIPMENT LIST System Instruments and/or Remarks Equipment Communications As required per local VHF Comm operating regulations Electrical Power Alternator Battery Voltage Indicator Fire Protection As required per local Portable Fire Extinguisher...
Page 60
Jabiru Aircraft Pilot Operating Handbook Model J230-D System Instruments and/or Remarks Equipment Altimeter Airspeed Indicator Magnetic Compass May be carried on the Time Piece pilot As required per local Turn Co-ordinator operating regulations Pitot/Static System As required per local Transponder...
Jabiru Aircraft Pilot Operating Handbook Model J230-D 6.4 TRIM SHEETS (USING METRIC UNITS) The trim sheets included below, when used correctly, provide a means of calculating the aircraft weight and CG position without manual calculations. An example of using the sheet is included for reference.
Jabiru Aircraft Pilot Operating Handbook Model J230-D 6.4.3 Calculating the Operating CG Locations Take the calculated Empty Weight Trim Index and mark it’s position on the Aircraft 2-1. Index Units Ladder at the top of the sheet. Draw a vertical line down from the point marked above to intersect with a sloping line in the “Baggage Zone A”...
Page 66
Jabiru Aircraft Pilot Operating Handbook Model J230-D ORIGINAL (METRIC UNITS) Aircraft Index Units Baggage Zone A Index Units - Come right 1 line per 5kg added in zone A Baggage Zone B Index Units - Come right 1 line per 5kg added in zone B Fuel Index Units - Come right 1 line per 10L fuel added.
Page 67
Jabiru Aircraft Pilot Operating Handbook Model J230-D EXAMPLE (METRIC UNITS) Aircraft Index Units STEP 1: Start at the empty aircraf t's index STEP 3: Draw a line down f rom the Aircraf t Index STEP 3 to the Baggage Zone A Index ladder. Move 1 line right f or every 10kg of crew, every 5kg in Baggage Zone A.
Jabiru Aircraft Pilot Operating Handbook Model J230-D 6.5 TRIM SHEETS (USING IMPERIAL UNITS) The trim sheets included below, when used correctly, provide a means of calculating the aircraft weight and CG position without manual calculations. An example of using the sheet is included for reference.
Jabiru Aircraft Pilot Operating Handbook Model J230-D 6.5.3 Calculating the Operating CG Locations Take the calculated “Empty Weight Trim Index” and mark this value on the “Aircraft 2-1. Index Units” Ladder at the top of the sheet. Draw a vertical line down from the point marked above to intersect with a sloping line in the “Baggage Zone A”...
Page 70
Jabiru Aircraft Pilot Operating Handbook Model J230-D ORIGINAL (IMPERIAL UNITS) 10.5 11.5 12.5 13.5 Aircraft Index Units Baggage Zone A Index Units - Come right 1 line per 10lbs baggage Baggage Zone B Index Units - Come right 1 line per 10lbs baggage Fuel Index Units - Come right 1 line per 3 US Gallons fuel added.
Page 71
Jabiru Aircraft Pilot Operating Handbook Model J230-D EXAMPLE (IMPERIAL UNITS) STEP 1: Start at the empty aircraf t's index 10.5 11.5 12.5 13.5 Aircraft Index Units STEP 3A STEP 3: Draw a line down f rom the Aircraf t Index to the Baggage Zone A Index Units - Come right 1 line per 10lbs baggage Baggage Zone A.
Model J230-D DESCRIPTION of AIRPLANE & SYSTEMS 7.0 GENERAL The Jabiru J230-D is a high wing strut braced monoplane. The aircraft layout is shown below. Figure 7-1 Three View Drawing of the J230-D Figure 7-2 Three View Drawing of the J230-D...
Jabiru Aircraft Pilot Operating Handbook Model J230-D 7.1 AIRFRAME The fuselage, engine cowlings, wings, empennage, main undercarriage legs and all control surfaces are constructed of fibreglass-epoxy resin composite. The nose leg, engine mount and wing struts are the only large structural elements made from metal. The aircraft uses a tricycle, nose-wheel undercarriage layout and is equipped with wheel spats (fairings) as standard equipment.
Minimum System Voltage (Bottom of green arc) • Maximum System Voltage (top of green arc) Note (applicable to Jabiru USA aircraft only): In the absence of a Fuel Pressure display, a Fuel flow rate display may substitute Note The display of these limitations are required for the aircraft’s certification. It does not comply with the certification basis if these limits are missing or modified.
Jabiru Aircraft Pilot Operating Handbook Model J230-D 7.7 PLACARDS The following placards are required, and are to be located in the proximity indicated. 7.7.1 Cockpit Placards General Warning Placard P/No. 5A076A0D Fitted On The Cabin Roof Forward Of The Front Wing Spar Carry- Through Beam.
Page 78
Jabiru Aircraft Pilot Operating Handbook Model J230-D Engine Limits P/No. 5A079B0D Fit to instrument panel. (Not required if EMS / EFIS clearly display/ indicate these limits) No Smoking P/No. 5A035A0D Fit to instrument panel. No Intentional Spins. P/No. 5A072A0D Fit to Instrument Panel No Aerobatics, No Operations in IMC.
Page 79
Jabiru Aircraft Pilot Operating Handbook Model J230-D Electric Fuel Gauge Quantities. P/No. 5A053A1D P/No. 5A053A2D (Metric Litres) P/No. 5A053A3D P/No. 5A053A2D (US gallons) (Metric Litres) (US gallons) Where Equipped. Fit inside wing root immediately aft of windows through to electric fuel...
Jabiru Aircraft Pilot Operating Handbook Model J230-D Loading Limitations P/No 5A073A0D Fitted on inside of fuselage of RHS of cabin below rear quarter window. Table 2.15.1 7.7.2 Cockpit Controls Trim Position P/No. 5A031A0D (1 OFF) Fit to centre console beside of elevator fwd stop, between trim levers.
Jabiru Aircraft Pilot Operating Handbook Model J230-D 7.7.3 External Fuselage Static Port STATIC VENT KEEP CLEAR P/No 5043094 Attach to LHS of Vertical Fin in line with Static Tube Fuel Grade- Wing Tanks P/No 5091344 2 OFF Attach to top skin of wing adjacent to Fuel Filler Cap.
Page 82
Jabiru Aircraft Pilot Operating Handbook Model J230-D Earth on Post P/No. 5A066A0D Attach to upper wing skin beside fuel filler earth post. No Step P/No. 5A006A0D Qty 2 required. Fit to top of main wheel spats Earth on Exhaust P/No. 5029094 Attach to the lower fuselage on the pilot’s side immediately above the...
HANDLING & SERVICING 8.0 INTRODUCTION This section of the manual provides information on how to handle and service the Jabiru J230-D. 8.1 GROUND HANDLING – TAXIING When taxiing, it is important that speed and use of brakes be kept to a minimum. All controls must be utilized (see Figure below) to maintain directional control and balance;...
Model J230-D 8.2 TOWING INSTRUCTIONS The Jabiru J230-D is a relatively small and light aircraft and should be towed by hand only. The recommended method is to grasp the propeller immediately beside the spinner and tow the aircraft forwards from there. Alternatively the aircraft may be pushed backwards by pressing against the front of the horizontal tail close beside the fuselage.
Jabiru Aircraft Pilot Operating Handbook Model J230-D 8.4 SERVICING 8.4.1 Fuelling Ensure the aircraft is parked on level ground with the handbrake OFF – to enable it to quickly be pushed clear in an emergency. Connect the main bowser earth wire to the tip of the engine exhaust Stand on a small ladder or similar so that the fuel level is clearly visible through the filler.
If the level of “water” increases, alcohol is present in the fuel. At the time of writing Jabiru Aircraft are delivered with an OEM fuel tester marked with graduations for use in assessing alcohol content.
QA standards, even following best practice it is still possible for a particular tank-full of MOGAS to be unsuitable or unsafe for use. Jabiru Aircraft may choose to void any warranty for engines...
Fuels containing alcohol are inherently unsuitable for use in aircraft due to the way they absorb moisture from the air and change over time. d. Further information on fuels – including Ethanol content – is given in Jabiru Service Letter JSL007.
The brakes of the J230-D use automotive brake fluid. Refer to the aircraft Technical manual for details of appropriate brake fluid specifications. WARNING: The JABIRU uses automotive brake fluid (DOT 3 or DOT 4). DO NOT use Aircraft hydraulic fluid (mineral based) or damage to the brake system will result. 8.8 CLEANING & CARE Keeping the aircraft clean is important.
Page 90
Model J230-D CAUTION JABIRU aircraft are designed for minimum maintenance. However, special attention should be applied when the aircraft has been used in extremely corrosive conditions, e.g. beach landings with sand and salt. Always ensure the aircraft is thoroughly hosed and washed immediately after such use.
However, the final decision on their adoption or otherwise rests with JABIRU AIRCRAFT Pty Ltd. Any issues or corrections required of Jabiru publications are requested to be passed on to Jabiru in writing to incorporation in subsequent revisions. Emails to info@jabiru.net.au...
Each owner/operator of a LSA is responsible for providing the manufacturer with current contact information where the manufacturer may send the owner/operator supplemental notification bulletins. The following proforma may be used & sent to Jabiru Aircraft at info@jabiru.net.au the contact details given in Section 0.2.
POH are recorded on the Log of Supplements page. In the event that the aircraft is modified at a non Jabiru Aircraft facility through an STC or other approval method, it is the owner’s responsibility to ensure that the proper supplement, if applicable, is installed in the handbook and the supplement is properly recorded on the Log of Supplements page as amended from time to time.
Need help?
Do you have a question about the J230-D 2020 and is the answer not in the manual?
Questions and answers