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Jabiru Aircraft

Model

J170-C

PILOT'S OPERATING HANDBOOK

Revision 0

THIS DOCUMENT MUST BE CARRIED IN THE AIRCRAFT AT ALL TIMES

Содержание J170-C

Страница 1: ...Jabiru Aircraft Model J170 C PILOT S OPERATING HANDBOOK Revision 0 THIS DOCUMENT MUST BE CARRIED IN THE AIRCRAFT AT ALL TIMES...

Страница 2: ...AIRCRAFT MUST BE OPERATED IN ACCORDANCE WITH THE APPROVED DATA AND LIMITATIONS CONTAINED IN THIS MANUAL AT ALL TIMES Registration Marks Manufacturer Jabiru Aircraft Pty Ltd Aircraft Serial Number Cer...

Страница 3: ...Jabiru Aircraft Pilot Operating Handbook Model J170 C JP FM 08 Revision 0 3 April 2007 Page 3 AMENDMENT RECORD SHEET Amendment Date Affected Sections Affected Pages Date Inserted Signature...

Страница 4: ...the contents of this handbook before initial operation Thereafter the handbook should be reviewed periodically to enable the operator to maintain the highest level of familiarity with the aircraft it...

Страница 5: ...employed in the following context WARNING Operating procedures techniques etc which if not followed correctly may result in personal injury or death CAUTION Operating procedures techniques etc which...

Страница 6: ...Jabiru Aircraft Pilot Operating Handbook Model J170 C JP FM 08 Revision 0 3 April 2007 Page 6 THREE VIEW DRAWING Figure 1 1 Three View Drawing of the J170 C Note All dimensions in millimetres...

Страница 7: ...tration USA F Degrees Fahrenheit FAR Federal Aviation Regulation USA ft Foot feet ft min Feet per minute g Acceleration due to gravity Gal Gallon hPa Hectopascal hectopascals HF High Frequency ICAO In...

Страница 8: ...AS Calibrated Airspeed the indicated speed of an aircraft corrected for position and instrument error Calibrated airspeed is equal to true airspeed in standard atmosphere at sea level KCAS Calibrated...

Страница 9: ...air static temperature Airfield Pressure Height The height registered at the surface of an aerodrome by an altimeter with the pressure sub scale set to 1013 hPa 29 92 inches Hg Pressure Altitude Alti...

Страница 10: ...ce from the C of G to the reference datum can be found by dividing the total moment by the total weight of the aircraft C of G Arm The arm obtained by adding the aircraft s individual moments and divi...

Страница 11: ...n used in this manual as well as supplying some others that may be found useful 1 Pound lb 0 4536 Kilogram kg 1 Pound per sq in psi 6 895 Kilopascal kPa 1 Inch in 25 4 Millimetres mm 1 Foot ft 0 3048...

Страница 12: ...RPLANT LIMITATIONS 20 3 7 1 Fuel Grade 20 3 7 2 Lubricating Oil 21 3 8 POWERPLANT INSTRUMENT MARKINGS 21 3 9 EFIS EMS LIMITATIONS DISPLAY 21 3 9 1 Required EFIS limitation displays 21 3 9 2 Required E...

Страница 13: ...F CLIMB SPEED 44 7 4 BEST RATE OF CLIMB SPEED 44 7 5 PREFLIGHT INSPECTION 45 7 6 NORMAL PROCEDURES CHECK LISTS 48 7 6 1 Before Starting Engine 48 7 6 2 Starting Engine Cold 48 7 6 3 Before Take Off 48...

Страница 14: ...Aircraft Pilot Operating Handbook Model J170 C JP FM 08 Revision 0 3 April 2007 Page 14 1 GENERAL INFORMATION 1 1 MANUFACTURERS STATEMENT OF COMPLIANCE INSERT COPY OF MANUFACTURERS STATEMENT OF COMPL...

Страница 15: ...ilots and passengers have a duty to exercise good judgment and act in a responsible manner while using the aircraft and to obey all oral or written warnings or both prior to or during use of the aircr...

Страница 16: ...to Section 3 for additional details 2 4 ENGINE OIL Jabiru Aircraft approves lubricating oils of any brand name conforming to specifications MIL L 6082 for straight mineral oil and MIL L 22851 for ash...

Страница 17: ...of datum Fuel Station 451 mm aft of datum Refer to Section 4 for additional details 2 6 MINIMUM EQUIPMENT LIST System Instruments and or Equipment VFR Day Remarks Communications VHF Comm A R As requi...

Страница 18: ...ic Altimeter 1 Airspeed Indicator 1 Magnetic Compass 1 Time Piece 1 May be carried on the pilot Turn Co ordinator A R As required per local operating regulations Pitot Static System 1 Transponder A R...

Страница 19: ...nsure the aircraft is appropriate for the intended operations 3 2 AIRSPEED LIMITS SPEED KCAS REMARKS Max Manoeuvring Speed VA 90 Do not make full or abrupt control movements above this speed Never Exc...

Страница 20: ...75psi 20 kPa 3psi 80 kPa 11 psi 525 kPa 76 psi Note 1 Time with CHT at between 180 C and 200 C is not to exceed 5 Minutes Note 2 If temperature limits are reached shut the engine down or cool it by po...

Страница 21: ...fication basis If adjustments are required to the displays the work must be carried out before further flight by an authorised person with reference to the user manuals for the instruments and the fol...

Страница 22: ...rical systems are running To reduce the load on the alternator Jabiru Aircraft recommend only using the Landing Light for takeoff and landing turning it off during normal cruise operations and whereve...

Страница 23: ...acard P No 5026094 PULL TO OPEN Fitted on Inside of both Doors Above Door Handle Fuel Gauge P No 5A050A0D Where Equipped Fitted on the instrument panel immediately below fuel gauges Electric Fuel Gaug...

Страница 24: ...No 5A074A0D Fit to inside of fuselage on right side just below rear quarter window Locate vertical line in line with rear of baggage shelf Loading Limitations P No 5A073A0D Fitted on inside of fuselag...

Страница 25: ...lve Carby Heat P No 5A030A0D Fitted to lower central section of instrument panel Table 2 15 2 3 12 3 External Fuselage Static Port P No 5043094 STATIC VENT KEEP CLEAR Attach to LHS of Vertical Fin in...

Страница 26: ...o 5A013A0D Fit to top of doors Wing Bolt Tightening P No 5039094 Qty 8 Required DANGER DO NOT TIGHTEN Attach to the fuselage and wings beside each wing and lift strut attachment fitting Earth on Post...

Страница 27: ...0kg 1323lb Linear variation between points Aft Limit 287 mm 11 3 29 0 aft of datum at all weights Datum Wing Leading Edge Levelling Means Longitudinal Spirit Level placed on the lower section of the d...

Страница 28: ...0 400 450 500 550 600 650 150 175 200 225 250 275 300 325 CG Position mm Weight kg 4 2 Baggage Zones The cabin has one baggage zone Figure 6 3 1 Baggage Zones Baggage is restrained using the straps fi...

Страница 29: ...Jabiru Aircraft Pilot Operating Handbook Model J170 C JP FM 08 Revision 0 3 April 2007 Page 29 4 3 AIRCRAFT WEIGHT DATA Insert Page 6 2 here...

Страница 30: ...Jabiru Aircraft Pilot Operating Handbook Model J170 C JP FM 08 Revision 0 3 April 2007 Page 30 Insert Page 6 3 here...

Страница 31: ...Jabiru Aircraft Pilot Operating Handbook Model J170 C JP FM 08 Revision 0 3 April 2007 Page 31 Insert Equipment List here...

Страница 32: ...a point 1 4 Move horizontally to the left from the point made in Step 1 3 to enter the next scale which is the Baggage Weight Scale 1 5 Move vertically downward one line on this scale for each 5 kg of...

Страница 33: ...from the point marked in Step 2 5 one line for each 5 kg of load calculated i e 20 kg 4 lines and mark a point at this location 2 8 Drop a vertical line down from the point marked in Step 2 10 to inte...

Страница 34: ...Jabiru Aircraft Pilot Operating Handbook Model J170 C...

Страница 35: ...Jabiru Aircraft Pilot Operating Handbook Model J170 C...

Страница 36: ...phere 5 3 CRUISE SPEEDS RPM FUEL CONSUMPTION Cruise speed values given are based on tests carried out at gross aircraft weight at sea level and around 28 C Values are averaged Actual values will vary...

Страница 37: ...Conditions Power As required for level flight or maximum rated RPM as appropriate KCAS KIAS Flaps UP Flaps Take off Flaps Landing 42 40 45 43 43 47 45 45 45 50 48 48 48 56 53 54 54 57 54 55 55 63 60 6...

Страница 38: ...essential to analyse the situation correctly and determine the best course of action in any particular circumstance The following basic rules apply to all aircraft emergencies 1 Maintain Aircraft Cont...

Страница 39: ...ts when the propeller has stopped rotating without the use of the starter are unlikely before reaching VNE Therefore the following procedure addresses only airstarts by use of the starter motor IMPORT...

Страница 40: ...RFLY INSPECT 5 Wing Flaps FULL ON FINAL APPROACH 6 Airspeed 65 KIAS 7 Braking HEAVY AFTER TOUCH DOWN 8 Ignition OFF 9 Fuel Shutoff Valve OFF 10 Master Switch OFF Ditching 1 Airspeed 65 KIAS 2 Power if...

Страница 41: ...ATE If fire goes out 5 Smoke VENTILATE CABIN DOORS MAY BE OPENED SLIGHTLY 6 Precautionary Landing AS SOON AS PRACTICAL If fire does not go out 4 Land EXECUTE IMMEDIATELY WARNING With the Master Switch...

Страница 42: ...l gauges Check level Fly aircraft with the wing with the most fuel above the other 3 Precautionary Landing As soon as safe NOTE Due to the types of fuel pumps used it is normal for the fuel pressure w...

Страница 43: ...spins are prohibited in this aircraft Should an inadvertent spin occur the following recovery procedure should be used 1 Retard the throttle to idle 2 Centralise ailerons 3 Apply and hold full rudder...

Страница 44: ...optional equipment so checks that do not apply to this aircraft may be skipped 7 2 SPEEDS FOR NORMAL OPERATION Unless otherwise noted the following speeds are based on a maximum weight of 600 kg 1323l...

Страница 45: ...ight inspection checklist Figure 4 1 Pre flight Inspection 1 Fuel Quantity in both tanks Check Fuel caps Secure Water Check Both wing tanks and header tank 2 AOA Pitot Head All openings open unobstruc...

Страница 46: ...rmal but there should be no movement of the top of the leg relative to the fuselage 5 Static Source Static Source CHECK FOR BLOCKAGE 6 Empennage Tail tie down DISCONNECT Control surfaces CHECK Securit...

Страница 47: ...ck for regular compression CAUTION Prior to pulling through the propeller by hand the engine must be cold both ignition circuits the Master Switch must be switched OFF the brakes applied throttle clos...

Страница 48: ...cated within 10 secs Choke Closed Throttle 900 1000 RPM Alternator Warning Light CHECK OFF Avionics ON If the engine is hot proceed as for cold engine but do not use choke If the engine is turning at...

Страница 49: ...l clear of ground Take Off Safety Speed 65 KIAS Accelerate to Climb Speed 70 KIAS Flaps UP Fuel Pump OFF at top of climb Power SET as required 7 6 5 Initial Climb Throttle FULL OPEN Airspeed 70 KIAS 7...

Страница 50: ...im 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...

Страница 51: ...ry out engine run up tests with the aircraft pointing into wind In hot weather after performing run up checks leave the aircraft pointing into wind and idling at 1200rpm for 30 seconds to aid cooling...

Страница 52: ...ol 8 2 OIL 8 2 1 Engine Oil Specification Jabiru Aircraft approves lubricating oils of any brand name conforming to specifications MIL L 6082 for straight mineral oil and MIL L 22851 for ashless dispe...

Страница 53: ...ES The brakes of the J170 C use automotive brake fluid Refer to the J160 J170 Technical manual for details of appropriate brake fluid specifications WARNING The JABIRU uses automotive brake fluid DOT...

Страница 54: ...ru Aircraft Pilot Operating Handbook Model J170 C JP FM 08 Revision 0 3 April 2007 Page 54 9 CLIMATIC RESTRICTIONS Maximum Ambient Operating Temperature 38 C Flight into known icing conditions Prohibi...

Страница 55: ...he Log of Supplements shows the CASA Approved Jabiru Aircraft Supplements available for the J170 C at the date of publication of this POH The Log of Supplements page can be utilised as a Table of Cont...

Страница 56: ...Pilot Operating Handbook Model J170 C JP FM 08 Revision 0 3 April 2007 Page 56 10 1 LOG OF SUPPLEMENTS JABIRU AIRCRAFT SUPPLEMENTS Applicable to aircraft serial number J170 C ______________ Install Do...

Страница 57: ...Jabiru Aircraft Pilot Operating Handbook Model J170 C JP FM 08 Revision 0 3 April 2007 Page 57 This Page Intentionally Left Blank...

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