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Extra 300L Information Manual

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TITLE PAGE
I N F O R M A T I O N M A N U A L
E X T R A 3 0 0 L
MANUFACTURER
EXTRA Flugzeugproduktions- und Vertriebs- GmbH
Flugplatz Dinslaken
46569 Hünxe, Federal Republic of Germany
W A R N I N G
This is an Information Manual and may be used for general purposes only.
This Information Manual is not kept current.
It must not be used as a substitute for the official FAA/EASA Approved Pilot's Operating
Handbook required for operation of the airplane.

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  • Page 1 I N F O R M A T I O N M A N U A L E X T R A 3 0 0 L MANUFACTURER EXTRA Flugzeugproduktions- und Vertriebs- GmbH Flugplatz Dinslaken 46569 Hünxe, Federal Republic of Germany W A R N I N G This is an Information Manual and may be used for general purposes only.
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  • Page 3 Pilot´s Operating Handbook EXTRA 300L LOG OF REVISIONS Dates of issue for original and revised pages: Date and sign of approval: Original ......9. September 1994 LBA approved ....31. January 1995 Revision No. 1 ....... 26. June 1997 LBA approved ....27. August 1997 Revision No.
  • Page 4 Pilot´s Operating Handbook EXTRA 300L LOG OF EFFECTIVE PAGES Page Date Page Date Title ........31. March 2009 6-9 thru 6-16 ..... 20. January 2016 i thru iii ......20. January 2016 7-1 ......20. September 2006 iv ........... 19. April 2012 7-2 ........
  • Page 5 Pilot´s Operating Handbook EXTRA 300L Page Date Page Date 927-1 ........ 31. October 2013 913-7 ........ 20. January 2016 927-2 ........19. April 2012 913-8 ......15. December 2005 927-3 ........ 31. October 2013 914-1 thru 914-2 ... 15. December 2005 927-4 thru 927-6 ....
  • Page 6 INTRODUCTION This handbook contains 9 sections, and includes the material required to be furnished to the pilot by FAR Part 23. It also contains supplementary data supplied by EXTRA Flugzeug- produktions- und Vertriebs- GmbH. THIS MANUAL IS FURNISHED TO THE CIVIL AVIATION AUTHORITIES AS A PART OF THE CERTIFICATION MATERIAL FOR THIS MODEL.
  • Page 7 Pilot´s Operating Handbook EXTRA 300L NOTES AND SAFETY NOTES Safety notes in this manual are marked by a boxed textmarker in the middle of the page and written in semi-bold characters. This manual distinguishes three warning levels: D A N G E R Indicates a hazardous situation which, if not avoided, will result in death or serious injury.
  • Page 8 Pilot´s Operating Handbook EXTRA 300L MAIN TABLE OF CONTENTS Section Page GENERAL LIMITATIONS EMERGENCY PROCEDURES NORMAL PROCEDURES PERFORMANCE WEIGHT & BALANCE/EQUIPMENT LIST AIRPLANE & SYSTEMS DESCRIPTIONS AIRPLANE HANDLING, SERVICE & MAINTENANCE SUPPLEMENTS Page Date: 31. March 2009...

  • Page 9: Table Of Contents

    Pilot´s Operating Handbook Section 1 EXTRA 300L General SECTION 1 GENERAL Table of Contents Paragraph Page SECTION 1 GENERAL DESCRIPTION ........................1-3 SPECIFICATION OF CLASS ....................1-3 MANUFACTURER ........................1-3 TECHNICAL DATA ......................... 1-3 1.3.1 3-View Drawing ........................1-3 1.3.2 Main Data ..........................
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  • Page 11: Description

    EXTRA 300L General DESCRIPTION The airframe of the EXTRA 300L is built of a tig-welded steel-tube construction. Wings, empennage and landing gear are manufactured of composite material. The aircraft is a two-seater with the rear seat instrumented for pilot in comand.

  • Page 12: Main Data

    Section 1 Pilot´s Operating Handbook General EXTRA 300L 1.3.2 MAIN DATA - Length 6,96 m (22,83 ft) - Height 2,62 m ( 8,60 ft) - Span 8,00 m (26,25 ft) - Wheel-base 5,07 m (16,63 ft) - Wheel-track 1,80 m ( 5,91 ft) 1.3.3...

  • Page 13: Engine

    Pilot´s Operating Handbook Section 1 EXTRA 300L General ENGINE Manufacturer: Textron-Lycoming Williamsport Plant PA 17701 USA. a) Type Lycoming AEIO-540-L1B5 b) Type Lycoming AEIO-540-L1B5D Rated power: 300 HP @ 2700 RPM; 270 HP @ 2400 RPM PROPELLER Manufacturer: MT-Propeller Entwicklung GmbH, Federal Republic of Germany.

  • Page 14: Loading

    Section 1 Pilot´s Operating Handbook General EXTRA 300L OIL (Cont.) Average ambient air Mil-L6082 Mil-22851 temperature grades ashless dispersant grades - 18°C til 21°C SAE 30 SAE 30,40 or 20W40 (0°F - 70°F) - 18°C til 32°C SAE 20W50 SAE 20W50 or 15W50 (0°F - 90°F)

  • Page 15: Secondary Terminology

    Pilot´s Operating Handbook Section 1 EXTRA 300L General Meteorological terminology International standard atmospheric condition Outside air temperature 1.10 SECONDARY TERMINOLOGY Feet/minute Feet = 0.3048 m inch = 2.54 cm Meter Litres US.gal US (liquid) gallon = 3.79 litres US.qt US (liquid) quart = 0.946 litres...

  • Page 16: Conversion Table

    Section 1 Pilot´s Operating Handbook General EXTRA 300L 1.11 CONVERSION TABLE 1 - 8 Page Date: 16. March 2009 Page Date: 20. April 2002...
  • Page 17 Pilot´s Operating Handbook Section 2 EXTRA 300L Limitations SECTION 2 LIMITATIONS Table of Contents Paragraph Page SECTION 2 LIMITATIONS GENERAL ........................... 2-3 AIR SPEED (IAS) ....................... 2-3 CROSS-WIND COMPONENT ..................... 2-3 ENGINE ..........................2-3 2.4.1 Fuel ............................. 2-4 2.4.2 Engine Limitations ....................... 2-4 PROPELLER ........................
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  • Page 19: General

    Pilot´s Operating Handbook Section 2 EXTRA 300L Limitations SECTION 2 LIMITATIONS GENERAL This section includes operating limitations, instrument markings, and basic placards necessary for the safe operation of the aircraft, its engine, standard systems, and standard equipment. The limitations included in this section have been approved by the EASA.

  • Page 20: Fuel

    Section 2 Pilot´s Operating Handbook Limitations EXTRA 300L 2.4.1 FUEL Minimum grade aviation gasoline: 100/100LL; for alternate fuelgrades see latest revision of Lyc. S.I. No. 1070 Total fuel capacity: 171 L (45.1 US.gal). Usable fuel capacity: 165.5 L (43.6 US.gal).

  • Page 21: Propeller

    Pilot´s Operating Handbook Section 2 EXTRA 300L Limitations f) Cylinder head temperature -Max 260°C 500°F PROPELLER MT-Propeller Entwicklung GmbH, Federal Republic of Germany a) Type MTV-14-B-C/C190-17 -Maximum Take-Off and Maximum Continuous 2700 rpm b) Type MTV-9-B-C/C200-15 -Maximum Take-Off (5 min)

  • Page 22: Acrobatic Flight (2 Seats)

    Section 2 Pilot´s Operating Handbook Limitations EXTRA 300L 2.7.3 ACROBATIC FLIGHT (2 SEATS) Max T/O Weight: forward C.G. rear C.G. 870 kg (1918 lbs) 67.1 cm (26.4") 84.1 cm (33.1") (and below) ACROBATIC MANEUVERS 2.8.1 NORMAL FLIGHT All acrobatic maneuvers are prohibited except stall, chandelle, lazy eight and turns up to 60 degrees bank angle.

  • Page 23: Load Factor

    Pilot´s Operating Handbook Section 2 EXTRA 300L Limitations Maneuvers Recommended entry speeds IAS Symbol Remarks min knots (km/h) max knots (km/h) Segment: horizontal Line 45°climbing 80 (148) 90° up 45° diving reduce throttle 90° diving reduce throttle 1/4 Loop climb.

  • Page 24: Acrobatic Flight

    Section 2 Pilot´s Operating Handbook Limitations EXTRA 300L 2.9.2 ACROBATIC FLIGHT + 10 g / - 10 g for 1 seat occupied (MTOW 820 kg / 1808 lbs) + 8 g / - 8 g for 2 seat occupied (MTOW 870 kg / 1918 lbs) 2.10...

  • Page 25: Operating Placards

    Pilot´s Operating Handbook Section 2 EXTRA 300L Limitations 2.14.2 OPERATING PLACARDS (near airspeed indicator) THE MARKINGS AND PLACARDS INSTALLED IN (in the rear cockpit) THIS AIRPLANE CONTAIN OPERATING LIMITATIONS WHICH MUST BE COMPLIED WITH WHEN OPERATING THIS AIRPLANE IN THE ACROBATIC CATEGORY.
  • Page 26 Section 2 Pilot´s Operating Handbook Limitations EXTRA 300L THE REMAINING FUEL IN LEVEL FLIGHT (on the rear instrument panel CANNOT BE USED SAFELY under the acro & center tank fuel WHEN INDICATOR READS "ZERO". capacity indicator) ACROBATIC: ± 10 G, 1 PILOT ±...
  • Page 27 Pilot´s Operating Handbook Section 2 EXTRA 300L Limitations Approved acrobatic maneuvers and recommended entry airspeeds Maneuvers Airspeeds Maneuvers Airspeeds min km/h km/h km/h km/h Segment: Horizontal Line Aileron roll 45°climbing Snap roll 90° up "Tail-slide" 45° diving Spin ---- 90° diving...

  • Page 28: Instrument Markings

    Section 2 Pilot´s Operating Handbook Limitations EXTRA 300L 2.14.3 INSTRUMENT MARKINGS AIRSPEED INDICATOR green arc 60 KIAS (111 km/h) - 158 KIAS (293 km/h) yellow arc 158 KIAS (293 km/h) - 220 KIAS (407 km/h) red line 220 KIAS (407 km/h) OIL PRESSURE INDICATOR Range markings are depending on instrument installed.

  • Page 29: Kinds Of Operation Equipment List

    Pilot´s Operating Handbook Section 2 EXTRA 300L Limitations MANIFOLD PRESSURE INDICATOR green arc 10 " Hg - 25 " Hg yellow arc 25 " Hg - 29.5 " Hg red radial 29.5 " Hg 2.15 KINDS OF OPERATION EQUIPMENT LIST The aircraft may be operated in day VFR when the appropriate equipment is installed and operable.
  • Page 30 According FAR Part 91 „General Operating and Flight Rules" each occupant of an US registered airplane must wear an approved parachute when performing acrobatic maneuvers. Extra Flugzeugproduktions- und Vertriebs- GmbH considers acrobatics without wearing an approved parachute to be unsafe. 2 - 14 Page Date: 20.
  • Page 31 Pilot´s Operating Handbook Section 3 EXTRA 300L Emergency Procedures SECTION 3 EMERGENCY PROCEDURES Table of Contents Paragraph Page SECTION 3 EMERGENCY PROCEDURES INTRODUCTION ......................... 3-3 3.0.1 General ..........................3-3 3.0.2 General Behaviour in Emeregency Situations ..............3-3 AIRSPEEDS FOR EMERGENCY OPERATION ..............3-4 OPERATIONAL CHECKLIST .....................
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  • Page 33: Introduction

    Pilot´s Operating Handbook Section 3 EXTRA 300L Emergency Procedures SECTION 3 EMERGENCY PROCEDURES INTRODUCTION 3.0.1 GENERAL This section contains the checklist and procedures coping with emergencies that may occur. This checklist must be followed in various emergencies to ensure maximum safety for the crew and/or aircraft.

  • Page 34: Airspeeds For Emergency Operation

    Section 3 Pilot´s Operating Handbook Emergency Procedures EXTRA 300L AIRSPEEDS FOR EMERGENCY OPERATION Stall speed 60 KIAS (111 km/h) Engine failure after take-off 80 KIAS (148 km/h) Best recommended gliding speed ( glide angle 1 : 6,2 ) -Normal (950 kg)

  • Page 35: Oil System Malfunction

    Pilot´s Operating Handbook Section 3 EXTRA 300L Emergency Procedures 3.2.4 OIL SYSTEM MALFUNCTION If oil pressure indicates low: Apply positive "g" If oil pressure is not regained then: 1. Airspeed 80 KIAS (148 km/h) 2. Throttle REDUCE TO IDLE 3. Engine oil temperature OBSERVE INDICATION 4.

  • Page 36: Fires

    Section 3 Pilot´s Operating Handbook Emergency Procedures EXTRA 300L FIRES 3.4.1 DURING START ON GROUND 1. Cranking CONTINUE to get a start which would suck the flames and accumulated fuel through the air inlet and into the engine. 2. Fuel shutoff valve OFF (Pull &...

  • Page 37: Engine Fire In Flight

    Pilot´s Operating Handbook Section 3 EXTRA 300L Emergency Procedures 3.4.3 ENGINE FIRE IN FLIGHT 1. Mixture IDLE CUT OFF 2. Fuel shutoff valve OFF (Pull & Turn) 3. Master switch 4. Airspeed 100 KIAS (185 km/h), find your airspeed/attitude which will keep the fire away from the cockpit 5.

  • Page 38: Emergency Exit After Turn Over

    Section 3 Pilot´s Operating Handbook Emergency Procedures EXTRA 300L EMERGENCY EXIT AFTER TURN OVER 1. Master switch 2. Fuel shutoff valve OFF (Pull & Turn) 3. Seat belts OPEN 4. Parachute harnesses (if wearing a parachute) OPEN 5. Canopy handle...
  • Page 39 Pilot´s Operating Handbook Section 4 EXTRA 300L Normal Procedures SECTION 4 NORMAL PROCEDURES Table of Contents Paragraph Page SECTION 4 GENERAL ..........................4-3 4.0.1 Airspeeds for Normal Operation ................... 4-3 4.0.2 Checklist and Procedures ....................4-3 PREFLIGHT INSPECTION ....................4-4 4.1.1...
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  • Page 41: General

    Pilot´s Operating Handbook Section 4 EXTRA 300L Normal Procedures SECTION 4 NORMAL PROCEDURES GENERAL 4.0.1 AIRSPEEDS FOR NORMAL OPERATION CATEGORY ACRO NORMAL 1 seat 2 seats KIAS (km/h) KIAS (km/h) KIAS (km/h) Start: -Rotate Speed 60 (111) 62 (115) 65 (120)

  • Page 42: Preflight Inspection

    Section 4 Pilot´s Operating Handbook Normal Procedures EXTRA 300L PREFLIGHT INSPECTION 4.1.1 EXTERIOR INSPECTION ILLUSTRATION 4.1.2 GENERAL Visually check airplane for general condition during walk around inspection. Perform exterior check as outlined in the picture above in counterclockwise direction. CHECKLIST PROCEDURES 1) Cockpit 1.
  • Page 43 Pilot´s Operating Handbook Section 4 EXTRA 300L Normal Procedures 4) Nose 1. Engine oil dipstick CHECK 2. Propeller and spinner CHECK 3. Air inlet CHECK 4. Acro & center fuel tank drain DRAIN FOR AT LEAST 4 SECONDS TO CLEAR SUMP OF POSSIBLE WATER;...

  • Page 44: Starting Procedures

    Section 4 Pilot´s Operating Handbook Normal Procedures EXTRA 300L STARTING PROCEDURES 4.3.1 COLD ENGINES The following starting procedures are recommended, however, the starting conditions may necessitate some variation from these procedures. 1. Perform pre-flight inspection. 2. Set propeller governor control to "High RPM" position.

  • Page 45: Take-Off Procedure

    Pilot´s Operating Handbook Section 4 EXTRA 300L Normal Procedures TAKE-OFF PROCEDURE 4.5.1 BEFORE TAKE-OFF Before you line up at the runway for take-off: - Check oil pressure and oil temperature. N O T E The RPM Gauge is electronically operated. To check the magnetos the RPM source switch must be set to the same magento as the igintion switch.

  • Page 46: Landing Procedures

    Section 4 Pilot´s Operating Handbook Normal Procedures EXTRA 300L LANDING PROCEDURES 4.8.1 DESCENT 1. Throttle - Reduce 2. Mixture - "FULL RICH" 3. RPM Control - Set to 2400 RPM 4. Trim - Adjust 5. Fuel selector* - "ACRO & CENTER TANK"...

  • Page 47: Go-Around

    Pilot´s Operating Handbook Section 4 EXTRA 300L Normal Procedures N O T E The rudder is effective down to 30 KIAS (56 km/h) 3. Throttle - CLOSE / IDLE 4. Braking - Minimum required GO-AROUND Decide early in the approach if it is necessary to go around and then start go-around before too low altitude and airspeed are reached.

  • Page 48: Acrobatic Maneuvers

    Section 4 Pilot´s Operating Handbook Normal Procedures EXTRA 300L 4.12 ACROBATIC MANEUVERS 4.12.1 GENERAL N O T E Prior to executing these maneuvers tighten harnesses and check all loose items are stowed. Start the maneuvers at safe altitude and maximum continuous power setting if not otherwise noted.
  • Page 49 Pilot´s Operating Handbook Section 4 EXTRA 300L Normal Procedures - Segment line 45° climbing: The plane will follow the line at max. power. The speed will not decrease below 80 KIAS (148 km/h) - Segment line 90° up: Any entry speed may be used. Out of a horizontal pull-up at 200 KIAS (370 km/h) the vertical penetration will be 2.500 ft.

  • Page 50: Spin

    Section 4 Pilot´s Operating Handbook Normal Procedures EXTRA 300L 4.12.3 SPIN To enter a spin proceed as follows: - Reduce speed, power idle - When the plane stalls: - Kick rudder to desired spin direction - Hold ailerons neutral - Stick back (positive spinning), Stick forward (negative spinning) The plane will immediately enter a stable spin.
  • Page 51 Pilot´s Operating Handbook Section 5 EXTRA 300L Performance SECTION 5 PERFORMANCE Table of Contents Paragraph Page SECTION 5 PERFORMANCE GENERAL ........................... 5-3 5.1.1 Performance Charts ......................5-3 5.1.2 Definitions of Terms ......................5-3 5.1.3 Sample Problem ........................5-3 ISA CONVERSION ......................5-5 AIRSPEED CALIBRATION ....................
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  • Page 53: General

    Pilot´s Operating Handbook Section 5 EXTRA 300L Performance SECTION 5 PERFORMANCE GENERAL Performance data charts on the following pages are presented to facilitate the planning of flights in detail and with reasonable accuracy under various conditions. The data in the charts have been computed from actual flight tests with the aircraft and engine in good condition and using average piloting techniques.
  • Page 54 Section 5 Pilot´s Operating Handbook Performance EXTRA 300L TAKE-OFF Take-Off Distance is shown by Fig. 5.5 Example: -T/O Weight: 870 kg (1918 lbs) -Ground Roll: 112 m (367 ft) -Total Distance to clear a 50 ft obstacle: 248 m (813 ft) These distances are well within the available field length incl.

  • Page 55: Isa Conversion

    Pilot´s Operating Handbook Section 5 EXTRA 300L Performance ISA CONVERSION ISA Conversion of pressure altitude and outside air temperature Page Date: 20. April 2002 5 - 5...

  • Page 56: Airspeed Calibration

    Section 5 Pilot´s Operating Handbook Performance EXTRA 300L AIRSPEED CALIBRATION N O T E Indicated airspeed assumes zero instrument error 5 - 6 Page Date: 16. March 2009 Page Date: 20. April 2002...

  • Page 57: Stall Speed

    Pilot´s Operating Handbook Section 5 EXTRA 300L Performance STALL SPEED CONDITION: POWER IDLE FORWARD C/G STALL SPEEDS ANGLE OF BANK WEIGHT CATEGORY 0° 30° 45° 1,15 g 1,41 g kg (lbs) KIAS (km/h) KIAS (km/h) KIAS (km/h) Normal (2095) (111)

  • Page 58: Take-Off Performance

    Section 5 Pilot´s Operating Handbook Performance EXTRA 300L TAKE-OFF PERFORMANCE Power : T/O Power Runway: Concrete N O T E For every 5 kts (9 km/h) headwind, the T/O distance can be decreased by 4%. For every 3 kts (6 km/h) tailwind [up to 10 kts (19 km/h)], the T/O distance is increased by 10%.

  • Page 59: Rate Of Climb Performance

    Pilot´s Operating Handbook Section 5 EXTRA 300L Performance RATE OF CLIMB PERFORMANCE Page Date: 20. April 2002 Page Date: 16. March 2009 5 - 9...

  • Page 60: Time To Climb, Fuel To Climb

    Section 5 Pilot´s Operating Handbook Performance EXTRA 300L TIME TO CLIMB, FUEL TO CLIMB 5 - 10 Page Date: 20. April 2002...

  • Page 61: Range And Endurance

    Pilot´s Operating Handbook Section 5 EXTRA 300L Performance RANGE AND ENDURANCE Page Date: 20. April 2002 5 - 11...

  • Page 62: Fuel Consumption

    Section 5 Pilot´s Operating Handbook Performance EXTRA 300L FUEL CONSUMPTION (23.8) (21.1) (18.5) (15.9) (13.2) (10.6) (7.9) (5.3) (2.6) HOUR EXAMPLE: PA = 8000 ft (ISA); POWER SETTING 65% FUEL CONSUMPTION: => 52 LTR/HRS (13.7 GAL/HRS) => 3.25 NM/LTR (12.3 NM/GAL) (15.1)

  • Page 63: Cruise Performance

    Pilot´s Operating Handbook Section 5 EXTRA 300L Performance 5.10 CRUISE PERFORMANCE Range and Endurance values for a T/O Weight of 950 kg (2095 lb) including fuel for warm-up and Take-Off from SL, max. cont. Power climb to cruising altitude, and a reserve of 21 L (5.55 US.gal) for 45 minutes with 45% Power.

  • Page 64: Landing Performance

    Section 5 Pilot´s Operating Handbook Performance EXTRA 300L 5.11 LANDING PERFORMANCE Power : Idle Runway: Concrete Brakes: maximum N O T E For every knot (1.852 km/h) headwind, the landing distance can be decreased by 3%. On a solid, dry and plain grass runway, the landing is increased by 15%.
  • Page 65 Pilot´s Operating Handbook Section 6 EXTRA 300L Weight and Balance and Equipment List SECTION 6 WEIGHT AND BALANCE AND EQUIPMENT LIST Table of Contents Paragraph Page SECTION 6 WEIGHT AND BALANCE AND EQUIPMENT LIST GENERAL ..........................6-3 AIRCRAFT WEIGHING PROCEDURE ................. 6-3 6.2.1...
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  • Page 67: General

    Pilot´s Operating Handbook Section 6 EXTRA 300L Weight and Balance and Equipment List GENERAL This section describes the procedure for establishing the basic weight and moment of the aircraft. Sample forms are provided for reference. Procedures for calculating the weight and movement for various operations are also provided.

  • Page 68: Owners Weight And Balance Record

    Section 6 Pilot´s Operating Handbook Weight and Balance and Equipment List EXTRA 300L If a new weight is added to the known old weight and CG position the resulting new weight and CG can be obtained by a simple calculation:...

  • Page 69: Center Of Gravity Calculation (Sample Problem)

    Pilot´s Operating Handbook Section 6 EXTRA 300L Weight and Balance and Equipment List CENTER OF GRAVITY CALCULATION (SAMPLE PROBLEM) PILOT ACRO-TANK COPILOT WING-TANK Rear Seat Fuel Front Seat Fuel Position 51 LTR 120 LTR (13.4 US GAL) (31,7 US GAL)
  • Page 70 Section 6 Pilot´s Operating Handbook Weight and Balance and Equipment List EXTRA 300L 6 - 6 Page Date: 20. April 2002...

  • Page 71: Sample

    Pilot´s Operating Handbook Section 6 EXTRA 300L Weight and Balance and Equipment List 6.3.1 Sample Take-off Condition: Pilot On Rear Seat 90.0 kg ( 198.5 lbs) Copilot On Front Seat 90.0 kg ( 198.5 lbs) Acro Fuel 51 L 37.0 kg ( 81.5 lbs)

  • Page 72: Loading Weights And Moments

    Section 6 Pilot´s Operating Handbook Weight and Balance and Equipment List EXTRA 300L LOADING WEIGHTS AND MOMENTS OCCUPANTS : max. 2 PILOT COPILOT WEIGHT REAR SEAT FRONT SEAT Pilot + Parachute Arm = 207cm (81.5 inch) Arm = 98 cm (38.4 inch)

  • Page 73: Weights And Moments Limits

    Pilot´s Operating Handbook Section 6 EXTRA 300L Weight and Balance and Equipment List WEIGHTS AND MOMENTS LIMITS EXAMPLE: At 790 KG (1741 LBS) and 64000 kgcm the C/G location is 81.0 cm (31.9") aft of ref datum Page Date: 20. April 2002 Page Date: 20.

  • Page 74: Equipment List

    Section 6 Pilot´s Operating Handbook Weight and Balance and Equipment List EXTRA 300L EQUIPMENT LIST EXTRA 300L S/N: ITEM MANUFACT. PART OR P/N WEIGHT MARK IF REQUIRED (R) (kg) INSTALLED OPTIONAL (O) ALTERNAT. (A) Engine Textron Lycoming AEIO-540-L1B5 194.90 -0.72...
  • Page 75 Pilot´s Operating Handbook Section 6 EXTRA 300L Weight and Balance and Equipment List ITEM MANUFACT. PART OR P/N WEIGHT MARK IF REQUIRED (R) (kg) INSTALLED OPTIONAL (O) ALTERNAT. (A) Throttle Control Teleflex F303 03250 0.56 0.60 or CC330 10' Throttle Control Cable Cablecraft 580-540-501 0.63...
  • Page 76 Section 6 Pilot´s Operating Handbook Weight and Balance and Equipment List EXTRA 300L ITEM MANUFACT. PART OR P/N WEIGHT MARK IF REQUIRED (R) (kg) INSTALLED OPTIONAL (O) ALTERNAT. (A) RPM Indicator digital Horizon P100-230-635-00 0.68 1.60 (2600RPM) Magnetic Compass Airpath C 2300 0.25...
  • Page 77 Pilot´s Operating Handbook Section 6 EXTRA 300L Weight and Balance and Equipment List ITEM MANUFACT. PART OR P/N WEIGHT MARK IF REQUIRED (R) (kg) INSTALLED OPTIONAL (O) ALTERNAT. (A) Radar Altimeter Anten. FreeFlight TRA 3000 0.68 2.33 incl. Digital Indicator TRI 20 0.34...
  • Page 78 Section 6 Pilot´s Operating Handbook Weight and Balance and Equipment List EXTRA 300L ITEM MANUFACT. PART OR P/N WEIGHT MARK IF REQUIRED (R) (kg) INSTALLED OPTIONAL (O) ALTERNAT. (A) Manifold Press. / United Instruments UI6331-H.186 0.49 1.60 Fuel Flow Ind.
  • Page 79 0.55 0.15 Brake Cyl., rear Cleveland 10-20 or 10-20E 0.55 1.15 Brake Cyl., rear Matco MC-4E 0.55 1.15 Brake Fluid Reservoir EXTRA 53301.1 0.20 0.03 Brake Fluid Reservoir ACS A-315 0.20 0.04 Safety Belt Assy Hooker FK0002 or FK0019 3.30 2.12...
  • Page 80 Sighting Dev. LH/RH EXTRA 83801.10 0.54 1.59 each Aresti-Card Holder EXTRA Assy 0.09 1.66 Wing Tie Down Rings EXTRA 83801.2-01 0.04 1.08 Remote Mounted Airwolf Filter Corp. AFC-K007 -0.09 Oil Filter Kit 6 - 16 Page Date: 20. January 2016...
  • Page 81 Pilot´s Operating Handbook Section 7 EXTRA 300L Description and Operation of Aircraft and Systems SECTION 7 DESCPRIPTION AND OPERATION OF AIRCRAFT AND SYSTEMS Table of Contents Paragraph Page SECTION 7 DESCPRIPTION AND OPERATION OF AIRCRAFT AND SYSTEMS THE AIRCRAFT ........................7-3 FUSELAGE .........................
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  • Page 83: The Aircraft

    OF AIRCRAFT AND SYSTEMS THE AIRCRAFT The aircraft EXTRA 300L is designed and developed by EXTRA Flugzeugproduktions- und Vertriebs- GmbH, Flugplatz Dinslaken, 46569 Hünxe, Federal Republic of Germany, in accordance with the U.S. Federal Aviation Regulations, part 23, categories normal and acrobatic to fullfill the primary flight training, normal operation rules and acrobatic training up to the unlimited acrobatic level.

  • Page 84: Wings

    EMPENNAGE The EXTRA 300/L possesses a cruziform empennage with stabilizers and moveable control surfaces. The rudder is balanced aerodynamically at the tip. Spars consist of PVC foam cores, CRP caps and GRP laminates. The shell is built using honeycomb sandwich with GRP laminates.

  • Page 85: Flight Control System

    FLIGHT CONTROL SYSTEM 7.5.1 PRIMARY CONTROL SYSTEM The EXTRA 300/L is standard equipped with full dual primary flight controls including conventional stick-type control columns and adjustable rudder pedals. The primary control surfaces are operated through a direct mechanical linkage. 7.5.2 LONGITUDINAL FLIGHT CONTROL SYSTEM The two control columns are interconnected by a torque tube.

  • Page 86: Instrumentation

    EXTRA 300L INSTRUMENTATION The Extra 300/L is equipped with flight instruments in both cockpits. Instruments and placards can be provided with markings in either metric or English units. The colour markings in instruments follow US-FAR, part 23 recommendation ( see section 2 ).
  • Page 87 Pilot´s Operating Handbook Section 7 EXTRA 300L Description and Operation of Aircraft and Systems Standard Optional Position Item Magneto Selector switch & starter Amperemeter Airspeed indicator Magn. Direction indicator Oil pressure / Oil temperature EGT / CHT RPM indicator Circuit breaker...

  • Page 88: Instrument Panel (Front Cockpit)

    Section 7 Pilot´s Operating Handbook Description and Operation of Aircraft and Systems EXTRA 300L 7.6.2 INSTRUMENT PANEL (FRONT COCKPIT) Normally the instument panel in the front cockpit is only equipped with the following positions. Airspeed indicator Altimeter indicator Intercom button...

  • Page 89: Seats, Seat Belts

    Pilot´s Operating Handbook Section 7 EXTRA 300L Description and Operation of Aircraft and Systems SEATS, SEAT BELTS The seats are ergonomically shaped composite designs. The rear seat angle can be adjusted on the ground with 2 quickpins, there are different seat angle possibilities. The back rest is also adjustable on the ground in different positions and angle.

  • Page 90: Power Plant

    Section 7 Pilot´s Operating Handbook Description and Operation of Aircraft and Systems EXTRA 300L 7.10 POWER PLANT 7.10.1 ENGINE The power plant consists of one Textron-Lycoming six-cylinder, horizontally opposed, aircooled, direct drive, fuel injection engine type with inverted oil system.

  • Page 91: Oil System

    Pilot´s Operating Handbook Section 7 EXTRA 300L Description and Operation of Aircraft and Systems 7.10.2 OIL SYSTEM The oil is cooled by a Two Cooler System mounted on the left hand side in the engine compartment. Alternatively a Single Cooler System is available. In this case the oil is cooled by one oil cooler mounted on the aft, right hand side of the engine.

  • Page 92: Mixture

    Section 7 Pilot´s Operating Handbook Description and Operation of Aircraft and Systems EXTRA 300L 7.10.6 MIXTURE Vernier-control located at the left side of the rear cockpit (red knob). 7.10.7 RPM-CONTROL Vernier-control on the left side of the rear cockpit. Preselection of RPM possible due to constant speed governor (blue knob).

  • Page 93: Electrical System

    Pilot´s Operating Handbook Section 7 EXTRA 300L Description and Operation of Aircraft and Systems A fuel filter with drain is installed between the fuel selector valve and the boost pump. Separate drains are located at the lowest point of each tank system.
  • Page 94 Section 7 Pilot´s Operating Handbook Description and Operation of Aircraft and Systems EXTRA 300L 7 - 14 Page Date: 08. October 2009 Page Date: 20. April 2002...

  • Page 95: Cabin Environment Control

    Pilot´s Operating Handbook Section 7 EXTRA 300L Description and Operation of Aircraft and Systems 7.13 CABIN ENVIRONMENT CONTROL A ventilation system in the canopy on the left side is provided for the supply of fresh air to the cabin. Left and right at the rear seat are eyeball-type adjustable vents.
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  • Page 97 Pilot´s Operating Handbook Section 8 EXTRA 300L Handling, Servicing and Maintenance SECTION 8 HANDLING, SERVICING AND MAINTENANCE TABLE OF CONTENTS Paragraph Page SECTION 8 HANDLING, SERVICING AND MAINTENANCE INTRODUCTION ......................... 8-3 AIRPLANE INSPECTION PERIODS ................... 8-3 PILOT CONDUCTED PREVENTIVE MAINTENANCE ............8-3 ALTERATIONS OR REPAIR ....................
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  • Page 99: Introduction

    Pilot´s Operating Handbook Section 8 EXTRA 300L Handling, Servicing and Maintenance SECTION 8 HANDLING, SERVICING AND MAINTENANCE INTRODUCTION a) The airplane owner should establish contact with the dealer or certified service station for service and information. b) All correspondence regarding the airplane must include its serial number which is stamped on a plate on the L/H rear part of the fuselage.

  • Page 100: Servicing

    Section 8 Pilot´s Operating Handbook Handling, Servicing and Maintenance EXTRA 300L SERVICING In addition to the airplane inspection periods (8.2) information for servicing the aircraft with proper oil and fuel is covered in Section 2 (Limitations) and Section 7 (Description and Operation).
  • Page 101 Pilot´s Operating Handbook Section 9 EXTRA 300L Supplements SECTION 9 SUPPLEMENTS SECTION 9 SUPPLEMENTS Doc-No. EA-06701.1 SUPPLEMENTS ........................3 Table of Contents Section Pages Supplements ......................4 p.  Steerable Tail Wheel ....................4 p.  Electric Pedal Adjustment ..................4 p.
  • Page 102 Section 9 Pilot´s Operating Handbook Supplements EXTRA 300L  ASPEN EFD1000 PILOT PFD ................... 12 p.  GARMIN GNC 420W ....................8 p.  ARTEX ME-406 ELT ....................8 p.  AIRPLANES REGISTERED IN BRAZIL AND OPERATING UNDER THE AGÊNCIA NACIONAL DE AVIAÇÃO CIVIL REQUIREMENTS ......... 6 p.
  • Page 103 Notes The described systems and equipment are certified by the EASA for the EXTRA 300/L. Pages and contents of this section must not be exchanged and alterations of or additions to the approved contents must not be made without the EXTRA Flugzeugproduktions- und Vertriebs- GmbH/EASA approval.
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  • Page 105 Section 901 Pilot´s Operating Handbook Steerable Tail Wheel EXTRA 300L SECTION 901 STEERABLE TAIL WHEEL Table of Contents Paragraph Page SECTION 901 STEERABLE TAIL WHEEL 901.1 GENERAL ........................901-3 901.2 LIMITATION ........................901-3 901.3 EMERGENCY PROCEDURES ..................901-3 901.4 NORMAL PROCEDURES ....................901-3 901.5...
  • Page 106 Section 901 Pilot´s Operating Handbook Steerable Tail Wheel EXTRA 300L Left blank intentionally 901 - 2 Page Date: 20. April 2002...
  • Page 107 901.1 GENERAL To improve taxi and handling quality, the EXTRA 300/L can be equipped with an optional steerable tailwheel. The deflection angle of this tailwheel is arranged by the rudder control up to plus/minus 30°. Exceeding this deflection the tailwheel has a full-swivel capability by a release mechanism.
  • Page 108 Section 901 Pilot´s Operating Handbook Steerable Tail Wheel EXTRA 300L 901.8 HANDLING, SERVICING AND MAINTENANCE During 50 hour inspection, the bearing steelsleeve has to be lubricated on the point of lubricating. Additionally all parts of the tailwheel have to be inspected visually for deforma- tions, cracks and corrosion.
  • Page 109 Pilot´s Operating Handbook Section 902 EXTRA 300L Electric Pedal Adjustment SECTION 902 ELECTRIC PEDAL ADJUSTMENT Table of Contents Paragraph Page SECTION 902 ELECTRIC PEDAL ADJUSTMENT 902.1 GENERAL ........................902-3 902.2 LIMITATIONS ........................902-3 902.3 EMERGENCY PROCEDURES ..................902-3 902.4 NORMAL PROCEDURES ....................902-3 902.5...
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  • Page 111 902.1 GENERAL To improve seat and control convenience, the EXTRA 300/L can be equipped with an optional elect. pedal adjustment system. The pedal adjustment system provides an in-flight capability to adjust the pedals according the pilots size and operation. For example a more relaxed, stretched seating position for long cross-country flights is possible.
  • Page 112 Section 902 Pilot´s Operating Handbook Electric Pedal Adjustment EXTRA 300L attachment. A full travel from the most rearward to the most forward position takes approxi- mately 15sec. FORWARD CONTROL-SWITCHES BACK LH --------- RH PEDALADJUST PEDAL- ADJUST. CIRCUIT BREAKER 7.5A 902.8 HANDLING, SERVICING AND MAINTENANCE Not affected.
  • Page 113 Pilot´s Operating Handbook Section 903 EXTRA 300L Electronic Accelerometer SECTION 903 ELECTRONIC ACCELEROMETER Table of Contents Paragraph Page SECTION 903 ELECTRONIC ACCELEROMETER 903.1 GENERAL ........................903-3 903.2 LIMITATIONS ........................903-3 903.3 EMERGENCY PROCEDURES ..................903-3 903.4 NORMAL PROCEDURES ....................903-3 903.5...
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  • Page 115: General

    Pilot´s Operating Handbook Section 903 EXTRA 300L Electronic Accelerometer ELECTRONIC ACCELEROMETER 903.1 GENERAL The standard equipped accelerometer typ AN 5745 can be replaced by an optional "Digital Solid State Accelerometer DSA 12". 903.2 LIMITATIONS The instrument markings and placards are provided for the acrobatic category (1 seat) only;...
  • Page 116 Section 903 Pilot´s Operating Handbook Electronic Accelerometer EXTRA 300L The other output-display are twentyfive LEDs which are arranged in a semicircle. The upper twelve LEDs show positive acceleration, the lower twelve LEDs show negative acceleration. The middle LED is on line all time long.
  • Page 117 Pilot´s Operating Handbook Section 903 EXTRA 300L Electronic Accelerometer After resetting the “Current Extreme Values”, the LC-Display shows + 3.0 g - 0.0 g and only the middle LED and three LEDs in the positive range of the LED-Display are shining.
  • Page 118 Section 903 Pilot´s Operating Handbook Electronic Accelerometer EXTRA 300L OPERATING INSTRUCTIONS The left button of the instrument will be called S1 and the right button will be called S2 during the following text. If the LC-Display shows acceleration values, then the upper line exhibits the positive acceleration, and the lower line shows the negative acceleration.
  • Page 119 Pilot´s Operating Handbook Section 903 EXTRA 300L Electronic Accelerometer 3) RESET OF THE “CURRENT EXTREME VALUES” Push button: once S1 If you want to reset the “Current Extreme Value” to 0g (for example you want to measure the extreme values of the next flight figure), you have to push S1 once. In this case, all LEDs are lighting up for two seconds, the LC-Display is showing: + 0.0 g...
  • Page 120 Section 903 Pilot´s Operating Handbook Electronic Accelerometer EXTRA 300L Additionally the long-term memory stores the times and dates when new “Absolute Extreme Values” occur. They are shown if you push S2 next. In this case during the next twelve seconds the LC-Display shows under the title “MAX-DATE” the time and date of the positi ve “Absolute Extreme Value”...

  • Page 121: Handling, Servicing And Maintenance

    Pilot´s Operating Handbook Section 903 EXTRA 300L Electronic Accelerometer into the “Normal Operating Mode” and the clock will be programmed with the correct changed numbers. The wrongly changed number is exchanged by its old value. 903.8 HANDLING, SERVICING AND MAINTENANCE If the absolute extreme value "C"...
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  • Page 123 Pilot´s Operating Handbook Section 904 EXTRA 300L Emergency Locator Transmitter SECTION 904 EMERGENCY LOCATOR TRANSMITTER Table of Contents Paragraph Page SECTION 904 EMERGENCY LOCATOR TRANSMITTER 904.1 GENERAL ........................904-3 904.2 LIMITATIONS ........................904-3 904.3 EMERGENCY PROCEDURES ..................904-4 904.4 NORMAL PROCEDURES ....................904-6 904.5...
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  • Page 125: General

    904.1 GENERAL To improve the passive security, the EXTRA 300/L can be equipped with an optional Emergency Locator Transmitter POINTER 3000 ELT. This POINTER 3000 ELT transmit s automatically after a crash or manual activity on the emergency frequencies of 121.5 MHz (civilian) and 243.0 MHz (military).

  • Page 126: Emergency Procedures

    Section 904 Pilot´s Operating Handbook Emergency Locator Transmitter EXTRA 300L 904.3 EMERGENCY PROCEDURES Aircraft accident or forced landing Manual activation Warbling tone on headset 121.5 MHz - Broken or disabled antenna? - Severed whip antenna cable? - Danger of fire in aircraft?
  • Page 127 Pilot´s Operating Handbook Section 904 EXTRA 300L Emergency Locator Transmitter C ) Operating of the ELT in the portable mode After forced landing or aircraft accident it may be desirable to use the transmitter in the portable mode. Various reasons may necessitate this, such as: ⇒...

  • Page 128: Normal Procedures

    Section 904 Pilot´s Operating Handbook Emergency Locator Transmitter EXTRA 300L 904.4 NORMAL PROCEDURES There is no change of basic normal procedures with the installation of the POINTER 3000 ELT. In addition to the existing normal procedures the "AUTO" position of the unit master switch or the remote switch has to be checked during the preflight check.

  • Page 129: Handling, Servicing And Maintenance

    Pilot´s Operating Handbook Section 904 EXTRA 300L Emergency Locator Transmitter OPERATING INSTRUCTION OF THE TRANSMITTER The operation of the ELT is possible over the master unit switch or over the remote switch (optional) in the panel. UNIT MASTER SWITCH used to activate the transmitter for test or emergency situations...
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  • Page 131 Pilot´s Operating Handbook Section 905 EXTRA 300L External Power SECTION 905 EXTERNAL POWER Table of Contents Paragraph Page SECTION 905 EXTERNAL POWER 905.1 GENERAL ........................905-3 905.2 LIMITATIONS ........................905-3 905.3 EMERGENCY PROCEDURES ..................905-3 905.4 NORMAL PROCEDURES ....................905-3 905.5...
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  • Page 133: General

    905.1 GENERAL The EXTRA 300/L can be equipped with two versions of an optional external power receptacle system. The "normal" system (PN 93102.16-01) provides the capability to start the engine independent of the board battery and is limited to this use. The "continuous operation"...

  • Page 134: Performance

    Section 905 Pilot´s Operating Handbook External Power EXTRA 300L D A N G E R Propeller strike possible. Do not allow any person to stay close to the propeller area! N O T I C E Risk of damage due to propeller strike or air stream.

  • Page 135: Description Of The System

    Pilot´s Operating Handbook Section 905 EXTRA 300L External Power 905.7 DESCRIPTION OF THE SYSTEM The external power receptacle is attached left under the rear seat. The main-relais is located at the left side of the firewall, above the starter-relais. For the avoidance of sparks, this relais does not switch before a safe contact from plug to receptacle will be ensured.
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  • Page 137 Pilot´s Operating Handbook Section 906 EXTRA 300L Digital RPM Indicator SECTION 906 DIGITAL RPM INDICATOR Table of Contents Paragraph Page SECTION 906 DIGITAL RPM INDICATOR 906.1 GENERAL ......................... 906-3 906.2 LIMITATIONS ........................906-3 906.3 EMERGENCY PROCEDURES ................... 906-3 906.4 NORMAL PROCEDURES ....................906-3 906.5...
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  • Page 139: General

    DIGITAL RPM INDICATOR 906.1 GENERAL The EXTRA 300/L can be equipped with the optional "P-1000" Digital RPM indicator as an alternative to the mechanical VDO RPM indicator. One of the following models is used: P100-230-635-00 (max. 2600RPM) P100-230-643-00 (max. 2700RPM) 906.2...

  • Page 140: Performance

    Section 906 Pilot´s Operating Handbook Digital RPM Indicator EXTRA 300L Ignition switch position: RIGHT Status area: Left red LED illuminates Display: shows RPM drop Ignition switch position: BOTH Status area: Right and left red LED OFF The middle LED should be OFF, otherwise the difference is more than permissible.
  • Page 141 Pilot´s Operating Handbook Section 906 EXTRA 300L Digital RPM Indicator RPM RANGES Engine operating ranges are indicated by the large green, yellow, and red LEDs. These LEDs are located on the upper right corner of the indicator face. MAGNETO-CHECK Three small LED magneto system alert indicator lights are located within the "Status" aera on the upper left corner of the indicator face.

  • Page 142: Handling, Servicing And Maintenance

    Section 906 Pilot´s Operating Handbook Digital RPM Indicator EXTRA 300L PRESS-AND-RELEASE operation mode (press and release in less than 2/3 of a second) This operation mode is placarded below each button.( L , DIM , R ) Masks ( L , R ) During normal operation, the tachometer presents the average of the left and right internal tachometers on the display.
  • Page 143 Pilot´s Operating Handbook Section 907 EXTRA 300L Long Range Wing Tank Capacity SECTION 907 LONG RANGE WING TANK CAPACITY Table of Contents Paragraph Page SECTION 907 LONG RANGE WING TANK CAPACITY 907.1 GENERAL ......................... 907-3 907.2 LIMITATIONS ........................907-3 907.3 EMERGENCY PROCEDURES ...................
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  • Page 145: General

    Pilot´s Operating Handbook Section 907 EXTRA 300L Long Range Wing Tank Capacity LONG RANGE WING TANK CAPACITY 907.1 GENERAL The leading edge wing tank on the EA 300/L equipped with the long range tank capacity features two tank compartments on either wing side. The compartments are separated by a slosh rib.

  • Page 146: Performance

    Section 907 Pilot´s Operating Handbook Long Range Wing Tank Capacity EXTRA 300L 907.5 PERFORMANCE RANGE AND ENDURACE Range and Endurance values for a T/O Weight of 950 kg (2095 lbs) including fuel for warm up and Take-Off from SL, max. continuous Power climb to cruising altitude, and a reserve of 21 litre (5.5 US Gal.) for 45 minutes with 45% Power.

  • Page 147: Weight And Balance

    Pilot´s Operating Handbook Section 907 EXTRA 300L Long Range Wing Tank Capacity W A R N I N G Risk of engine overheating. Always return the mixture to full rich before increasing power settings. 907.6 WEIGHT AND BALANCE LOADING WEIGHTS AND MOMENTS TOTAL FUEL CAPACITY: 205 Litre (54.1 US GAL.)

  • Page 148: Description Of The System

    Section 907 Pilot´s Operating Handbook Long Range Wing Tank Capacity EXTRA 300L 907.7 DESCRIPTION OF THE SYSTEM Wing tank: The leading edge section of each wing in front of main spars forms an integral fuel tank providing two interconnected tanks with 154 litres (40.7 US GAL.) total capacity. Each side of the wing has a 2"...
  • Page 149 Pilot´s Operating Handbook Section 908 EXTRA 300L Airtow Hook SECTION 908 AIRTOW HOOK Table of Contents Paragraph Page SECTION 908 AIRTOW HOOK 908.1 GENERAL ........................908-3 908.2 LIMITATIONS ........................908-3 908.3 EMERGENCY PROCEDURES ..................908-4 908.4 NORMAL PROCEDURES ....................908-4 908.5...
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  • Page 151: General

    Airtow Hook 908.1 GENERAL The EXTRA 300/L can optionally be equipped with a "TOST" glider air-tow release Typ E 85. The release mechanism is mounted at the tail spring end and actuated from the cockpit by a yellow knob. 908.2...

  • Page 152: Emergency Procedures

    Section 908 Pilot´s Operating Handbook Airtow Hook EXTRA 300L 908.3 EMERGENCY PROCEDURES A) ABORTED TAKE OFF 1. Pilot of the glider INFORM 2. Throttle IDLE 3. Mixture IDLE CUT OF 4. Brakes APPLY AS PRACTICAL B) ENGINE FAILURE IMMEDIATELY AFTER TAKEOFF Stall speed: 60 KIAS (111 km/h) 1.

  • Page 153: Performance

    Pilot´s Operating Handbook Section 908 EXTRA 300L Airtow Hook E) DESCENT AND LANDING While descending the engine temperatures shall be observed (Avoid overcooling). Final approach should account for the air-tow hanging below the aircraft flight path. 908.5 PERFORMANCE The existing POH-Data remain valid with the exception of:...
  • Page 154 Section 908 Pilot´s Operating Handbook Airtow Hook EXTRA 300L 908 - 6 Page Date: 16. March 2009 Page Date: 20. April 2002...
  • Page 155 Pilot´s Operating Handbook Section 908 EXTRA 300L Airtow Hook CLIMBRATE Conditions: Power: 2500 Rpm and full throttle, mixture rich, Speed of the aircraft tow: 76 KIAS = 140 Km/h, Weight of the towing aircraft: m = 820 Kg (1808 lb), (1 Pilot = 86 kg, Acro & Center Tank...

  • Page 156: Weight And Balance

    Section 908 Pilot´s Operating Handbook Airtow Hook EXTRA 300L 908.6 WEIGHT AND BALANCE Not affected. 908.7 DESCRIPTION OF THE SYSTEM The release mechanism is a typ "E 85" of the "TOST" company, Munich. It is mounted at the tail spring rear end aft the tail wheel and activated with a yellow handle located at the rear seat cockpit via a bowden cable.
  • Page 157 Pilot´s Operating Handbook Section 909 EXTRA 300L Smoke System SECTION 909 SMOKE SYSTEM Table of Contents Paragraph Page SECTION 909 SMOKE SYSTEM 909.1 GENERAL ......................... 909.3 909.2 LIMITATIONS ........................909.3 909.3 EMERGENCY PROCEDURES ................... 909.4 909.4 NORMAL PROCEDURES ....................909.4 909.5...
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  • Page 159: General

    EXTRA 300L Smoke System SMOKE SYSTEM 909.1 GENERAL For performing at airshows, the EXTRA 300L may optionally be equipped with a smoke system. 909.2 LIMITATIONS For safe operation of the smoke system the following limitations have to be considered: 1) The load factor and "MTOW" are limited to:...

  • Page 160: Emergency Procedures

    Section 909 Pilot´s Operating Handbook Smoke System EXTRA 300L 909.3 EMERGENCY PROCEDURES FAILURE OF THE SMOKE-SYSTEM 1. Switch "SMOKE ARM" and "SMOKE REFILL": OFF 2. Circuit breaker PULL FIRE IN FLIGHT 1. Switch "SMOKE ARM" If the fire (after the smoke system is shut off) will not extinguish proceed as follows: 2.

  • Page 161: Performance

    Pilot´s Operating Handbook Section 909 EXTRA 300L Smoke System After automatic refill shut-off : 3. Switch "SMOKE REFILL" 4. Refill hose DISCONNECT N O T E A shut-off failure of the refill process can be recognized by smoke oil spilling out of the vent line.

  • Page 162: Description Of The System

    Section 909 Pilot´s Operating Handbook Smoke System EXTRA 300L 909.7 DESCRIPTION OF THE SYSTEM On pilot's demand the smoke system produces a trail of smoke by injection of smoke oil (straight paraffin oil) into the engine exhaust. The smoke oil is vaporised by the exhaust gas heat and is visible as dense smoke after leaving the exhaust.

  • Page 163: Handling, Servicing And Maintenance

    Pilot´s Operating Handbook Section 909 EXTRA 300L Smoke System the pump off. The same pump (normal polarity) injects the smoke oil from the floptube smoke oil tank through an overpressure/check valve and the injector nozzle into the hot exhaust gas to generate smoke.
  • Page 164 Section 909 Pilot´s Operating Handbook Smoke System EXTRA 300L After each flight with activated Smoke System - Clean the aircraft belly fairing and the rudder cable from smoke oil contamination N O T E The rudder cables might suffer from increased wear, when they are covered with smoke oil and dust.
  • Page 165 Pilot´s Operating Handbook Section 910 EXTRA 300L Acro III Category SECTION 910 ACRO III CATEGORY Table of Contents Paragraph Page SECTION 910 ACRO III CATEGORY 910.1 GENERAL ........................910-3 910.2 LIMITATIONS ........................910-3 910.3 EMERGENCY PROCEDURES ..................910-4 910.4 NORMAL PROCEDURES ....................910-4 910.5...
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  • Page 167: General

    910.1 GENERAL The EXTRA 300/L can be operated in an additional two seat Acro III category. This category is defined by a MTOW of 950 kg (2095 lbs), a max. load factor of +6g/-6g, and a V of 158 KIAS (293 km/h).

  • Page 168: Emergency Procedures

    Section 910 Pilot´s Operating Handbook Acro III Category EXTRA 300L 910.3 EMERGENCY PROCEDURES Not affected 910.4 NORMAL PROCEDURES AIRSPEEDS FOR NORMAL OPERATION CATEGORY ACRO I ACRO II ACRO III NORMAL 1 seat 2 seats 2 seats KIAS (km/h) KIAS (km/h) KIAS (km/h) KIAS (km/h)

  • Page 169: Performance

    Pilot´s Operating Handbook Section 910 EXTRA 300L Acro III Category 910.5 PERFORMANCE STALL SPEEDS CONDITION: POWER IDLE FORWARD C/G ANGLE OF BANK / STALL SPEEDS WEIGHT CATEGORY 0° 30° 45° 1,15 g 1,41 g KIAS (km/h) KIAS (km/h) KIAS (km/h)

  • Page 170: Weight And Balance

    Section 910 Pilot´s Operating Handbook Acro III Category EXTRA 300L 910.6 WEIGHT AND BALANCE 910 - 6 Page Date: 20. April 2002...
  • Page 171 Pilot´s Operating Handbook Section 910 EXTRA 300L Acro III Category WEIGHT AND MOMENT LIMITS EXAMPLE: At 790 KG (1741 LBS) and 640000 kgcm the C/G location is 80,0 cm (31,4") aft of ref datum Page Date: 20. April 2002 910 - 7...

  • Page 172: Description And Operation Of Aircraft And Its Systems

    Section 910 Pilot´s Operating Handbook Acro III Category EXTRA 300L 910.7 DESCRIPTION AND OPERATION OF AIRCRAFT AND ITS SYSTEMS Not affected. 910.8 HANDLING, SERVICING AND MAINTENANCE Not affected. 910 - 8 Page Date: 20. April 2002...
  • Page 173 Pilot´s Operating Handbook Section 911 EXTRA 300L Single Seat Canopy SECTION 911 SINGLE SEAT CANOPY Table of Contents Paragraph Page SECTION 911 SINGLE SEAT CANOPY 911.1 GENERAL ........................911-3 911.2 LIMITATIONS ........................911-3 911.3 EMERGENCY PROCEDURES ..................911-3 911.4 NORMAL PROCEDURES ....................911-3 911.5...
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  • Page 175 Pilot´s Operating Handbook Section 911 EXTRA 300L Single Seat Canopy SINGLE SEAT CANOPY 911.1 GENERAL For airshow performances the standard canopy can be replaced by a single seat canopy, which gives a gorgeous appearance. 911.2 LIMITATIONS With the single seat canopy installed the aircraft is limited to the categories NORMAL and ACRO I.
  • Page 176 Section 911 Pilot´s Operating Handbook Single Seat Canopy EXTRA 300L Left blank intentionally 911 - 4 Page Date: 20. April 2002...
  • Page 177 Pilot´s Operating Handbook Section 912 EXTRA 300L FILSER TRT 600 Transponder SECTION 912 FILSER TRT 600 TRANSPONDER Table of Contents Paragraph Page SECTION 912 FILSER TRT 600 TRANSPONDER 912.1 GENERAL ........................912-3 912.1.1 Front Panel Operation ..................... 912-3 912.1.2 System Operation ......................912-5 912.1.3...
  • Page 178 Section 912 Pilot´s Operating Handbook FILSER TRT 600 Transponder EXTRA 300L Left blank intentionally 912 - 2 Page Date: 15. December 2005...

  • Page 179: General

    Pilot´s Operating Handbook Section 912 EXTRA 300L FILSER TRT 600 Transponder 912.1 GENERAL The TRT 600 is Level 2es Class2 (SSR Mode S Elementary Surveillance) Transponder. It has Mode A, Mode A/C and Mode S capability. In Mode S the transponder provides acquisition capability.
  • Page 180 Section 912 Pilot´s Operating Handbook FILSER TRT 600 Transponder EXTRA 300L ROTATING KNOBS Four rotating knobs are used to select the IDENT CODE. The assignments X… , .X.. , ..X. , …X indicate the position of the code number set by each knob.
  • Page 181 Pilot´s Operating Handbook Section 912 EXTRA 300L FILSER TRT 600 Transponder In-Flight Flag When there is an undercarriage switch installed, the display can toggle between the letters 'F' whether the aircraft is in flight condition or the letter 'G' whether the aircraft is in „on-ground“...
  • Page 182 Section 912 Pilot´s Operating Handbook FILSER TRT 600 Transponder EXTRA 300L 7777 Military interceptor operations (Never squawk this code) 0000 Military use (Not enterable) Care should be taken not to select the code 7500 and all codes in the 7600-7777 range, which trigger special indicators in automated facilities.
  • Page 183 Pilot´s Operating Handbook Section 912 EXTRA 300L FILSER TRT 600 Transponder The Aircraft Identification (FID) code is displayed on the right bottom line and consists of seven alphanumerical characters. N O T E The ICAO Flight Plan specifies only 7 characters as Flight Identification. Filser reserves 8 characters as stated in ED- 73B for further expansion of the flight plan.
  • Page 184 Pilot´s Operating Handbook FILSER TRT 600 Transponder EXTRA 300L To meet ICAO specifications the TRT 600 uses an external memory inside the aircraft connector housing of the cable set, which is a part of the aircraft. Because this cable is installed permanent into the aircraft, a change of the transponder will not affect the aircraft address and the Flight ID.
  • Page 185 Pilot´s Operating Handbook Section 913 EXTRA 300L FILSER TRT 800 Transponder SECTION 913 FILSER TRT 800 TRANSPONDER Table of Contents Paragraph Page SECTION 913 FILSER TRT 800 TRANSPONDER 913.1 GENERAL ......................... 913-3 913.1.1 Front Panel Operation ....................... 913-3 913.1.2 System Operation ......................913-5 913.1.3...
  • Page 186 Section 913 Pilot´s Operating Handbook FILSER TRT 800 Transponder EXTRA 300L Left blank intentionally 913 - 2 Page Date: 15. December 2005...
  • Page 187 Pilot´s Operating Handbook Section 913 EXTRA 300L FILSER TRT 800 Transponder 913.1 GENERAL The TRT 800 is Level 2es Class2 (SSR Mode S Elementary and Enhanced Surveillance) Transponder. It has Mode A, Mode A/C and Mode S capability. In Mode S the transponder provides acquisition and extended squitter capability.
  • Page 188 Section 913 Pilot´s Operating Handbook FILSER TRT 800 Transponder EXTRA 300L ROTATING KNOBS Four rotating knobs are used to select the IDENT CODE. The assignments X… , .X.. , ..X. , …X indicate the position of the code number set by each knob.

  • Page 189: System Operation

    Pilot´s Operating Handbook Section 913 EXTRA 300L FILSER TRT 800 Transponder IN-FLIGHT FLAG When there is an undercarriage switch installed, the display can toggle between the letters 'F' whether the aircraft is in flight condition or the letter 'G' whether the aircraft is in „on-ground“...
  • Page 190 Section 913 Pilot´s Operating Handbook FILSER TRT 800 Transponder EXTRA 300L 7700 Emergency 7777 Military interceptor operations (Never squawk this code) 0000 Military use (Not enterable) Care should be taken not to select the code 7500 and all codes in the 7600-7777 range, which trigger special indicators in automated facilities.

  • Page 191: Error Reporting / Fault Codes

    Pilot´s Operating Handbook Section 913 EXTRA 300L FILSER TRT 800 Transponder The Aircraft Identification (FID) code is displayed on the right bottom line and consists of seven alphanumerical characters. N O T E The ICAO Flight Plan specifies only 7 characters as Flight Identification. Filser reserves 8 characters as stated in ED- 73B for further expansion of the flight plan.

  • Page 192: Limitations

    Pilot´s Operating Handbook FILSER TRT 800 Transponder EXTRA 300L To meet ICAO specifications the TRT 800 uses an external memory inside the aircraft connector housing of the cable set, which is a part of the aircraft. Because this cable is installed permanent into the aircraft, a change of the transponder will not affect the aircraft address and the Flight ID.
  • Page 193 Pilot´s Operating Handbook Section 914 EXTRA 300L GARMIN GTX 327 Transponder SECTION 914 GARMIN GTX 327 TRANSPONDER Table of Contents Paragraph Page SECTION 914 GARMIN GTX 327 TRANSPONDER 914.1 GENERAL ........................914-3 914.1.1 Mode Selection Keys ....................... 914-3 914.1.2 Code Selection ........................ 914-4 914.1.3...
  • Page 194 Section 914 Pilot´s Operating Handbook GARMIN GTX 327Transponder EXTRA 300L Left blank intentionally 914 - 2 Page Date: 15. December 2005...

  • Page 195: General

    Pilot´s Operating Handbook Section 914 EXTRA 300L GARMIN GTX 327 Transponder 914.1 GENERAL The GARMIN GTX 327 is a panel-mounted TSO.d transponder with the addition of timing functions. The transponder is a radio transmitter and receiver that operates on radar frequencies, receiving ground radar interrogations at 1030 MHz and transmitting a coded response of pulses to ground- based radar on a frequency of 1090 MHz.

  • Page 196: Code Selection

    Section 914 Pilot´s Operating Handbook GARMIN GTX 327Transponder EXTRA 300L 914.1.2 CODE SELECTION Code selection is done with eight keys (0 - 7) that provide 4,096 active identification codes. Pushing one of these keys begins the code selection sequence. The new code will not be activated until the fourth digit is entered.

  • Page 197: Limitations

    Pilot´s Operating Handbook Section 914 EXTRA 300L GARMIN GTX 327 Transponder Resets the Count Up and Count Down timers and cancels the previous keypress during code selection. Reduces Contrast and Display Brightness when the respective pages are displayed. Also enters the number eight into the Count Down timer.

  • Page 198: Emergency Procedures

    Section 914 Pilot´s Operating Handbook GARMIN GTX 327Transponder EXTRA 300L 914.3 EMERGENCY PROCEDURES 914.3.1 IMPORTANT CODES 7600 Loss of communications. 7500 Hijacking. 7700 Emergency (All secondary surveillance radar sites are ready to receive this code at all times). See the Airman’s Information Manual (AIM) for a detailed explanation of identification codes.
  • Page 199 Pilot´s Operating Handbook Section 915 EXTRA 300L GARMIN GTX 330 Transponder SECTION 915 GARMIN GTX 330 TRANSPONDER Table of Contents Paragraph Page SECTION 915 GARMIN GTX 330 TRANSPONDER 915.1 GENERAL ........................915-3 915.1.1 Mode Selection Keys ....................... 915-4 915.1.2 Code Selection ........................ 915-4 915.1.3...
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  • Page 201: General

    Pilot´s Operating Handbook Section 915 EXTRA 300L GARMIN GTX 330 Transponder 915.1 GENERAL The Garmin GTX 330 panel mounted Mode S Transponder is a radio transmitter and receiver that fulfills the role of the airborne beacon equipment according to the requirements of the Air Traffic Radar Beacon System (ATCRBS).

  • Page 202: Mode Selection Keys

    Section 915 Pilot´s Operating Handbook GARMIN GTX 330 Transponder EXTRA 300L 915.1.1 MODE SELECTION KEYS Powers off the GTX 330. STBY Selects the standby mode displaying the last active identification code. When in standby mode, the transponder will not reply to any interrogations.

  • Page 203: Keys For Other Gtx 330 Functions

    Pilot´s Operating Handbook Section 915 EXTRA 300L GARMIN GTX 330 Transponder Avoid selecting code 7500 and all codes in the 7600-7777 range. These trigger special indicators in automated facilities. Only the code 7500 will be decoded as the hijack code. An aircraft’s transponder code (if available) is utilized to enhance the tracking capabilities of the ATC facility, therefore care should be taken when making routine code changes.

  • Page 204: Configuration Mode

    Section 915 Pilot´s Operating Handbook GARMIN GTX 330 Transponder EXTRA 300L 'FLIGHT TIME' Displays the Flight Time controlled by the START/STOP and CLR keys when Automated Airborne Determination is configured as normal. 'ALTITUDE MONITOR' The ALTITUDE MONITOR function is not available in this installation.

  • Page 205: Limitations

    Pilot´s Operating Handbook Section 915 EXTRA 300L GARMIN GTX 330 Transponder 915.2 LIMITATIONS Not applicable. 915.3 EMERGENCY PROCEDURES 915.3.1 IMPORTANT CODES 7600 Loss of communications. 7500 Hijacking. 7700 Emergency (All secondary surveillance radar sites are ready to receive this code at all times).
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  • Page 207 Pilot´s Operating Handbook Section 916 EXTRA 300L BENDIX/KING KT 76A Transponder SECTION 916 BENDIX/KING KT 76A TRANSPONDER Table of Contents Paragraph Page SECTION 916 BENDIX/KING KT 76A TRANSPONDER 916.1 GENERAL ........................916-3 916.1.1 Code Selection ......................... 916-3 916.1.2 Reply Light ........................916-4 916.1.3...
  • Page 208 Section 916 Pilot´s Operating Handbook BENDIX/KING KT 76A Transponder EXTRA 300L Left blank intentionally 916 - 2 Page Date: 15. December 2005...

  • Page 209: General

    Pilot´s Operating Handbook Section 916 EXTRA 300L BENDIX/KING KT 76A Transponder 916.1 GENERAL The BENDIX/KING KT 76A panel mounted transponder receives interrogations at 1030 MHz, and these trigger a coded response of radar pulses, which are transmitted back to ATC at 1090 MHz.

  • Page 210: Reply Light

    Section 916 Pilot´s Operating Handbook BENDIX/KING KT 76A Transponder EXTRA 300L 7600 Loss of communications 7700 Emergency 7777 Military interceptor operations (Never squawk this code) 0000 Military use (Not enterable) Avoid selecting code 7500 and all codes in the 7600-7777 range. These trigger special indicators in automated facilities.

  • Page 211: Normal Procedure

    Pilot´s Operating Handbook Section 916 EXTRA 300L BENDIX/KING KT 76A Transponder 916.4 NORMAL PROCEDURE After engine start-up, turn the function selector to the Standby (SBY) position. Then select the proper reply code by rotating the code select knobs. As soon as aircraft is airborne, switch the function selector to ON. Your KT 76A is now operating in „Mode A“, or normal mode.
  • Page 212 Section 916 Pilot´s Operating Handbook BENDIX/KING KT 76A Transponder EXTRA 300L Left blank intentionally 916 - 6 Page Date: 15. December 2005...
  • Page 213 Pilot´s Operating Handbook Section 917 EXTRA 300L BENDIX/KING KT 73 Transponder SECTION 917 BENDIX/KING KT 73 TRANSPONDER Table of Contents Paragraph Page SECTION 917 BENDIX/KING KT 73 TRANSPONDER 917.1 GENERAL ......................... 917-3 917.1.1 Function Selector Knob ....................917-4 917.1.2 Code Selection ......................... 917-4 917.1.3...
  • Page 214 Section 917 Pilot´s Operating Handbook BENDIX/KING KT 73 Transponder EXTRA 300L Left blank intentionally 917 - 2 Page Date: 31. March 2009...

  • Page 215: General

    Pilot´s Operating Handbook Section 917 EXTRA 300L BENDIX/KING KT 73 Transponder 917.1 GENERAL The BENDIX/KING KT 73 panel mounted Mode S Transponder is a radio transmitter and receiver that fulfills the role of the airborne beacon equipment according to the requirements of the Air Traffic Radar Beacon System (ATCRBS).

  • Page 216: Function Selector Knob

    Section 917 Pilot´s Operating Handbook BENDIX/KING KT 73 Transponder EXTRA 300L 917.1.1 FUNCTION SELECTOR KNOB The following operating modes can be chosen by the Function Selector Knob: Powers off the KT 73. When the unit is turned to another mode, it will reply or squitter within two seconds, according to the selected mode.

  • Page 217: Buttons/Selectors For Other Kt 73 Functions

    Pilot´s Operating Handbook Section 917 EXTRA 300L BENDIX/KING KT 73 Transponder 0021 The VFR code commonly used in Germany (default is set to 0021 at time of installation) 7500 Hijack code (Aircraft is subject to unlawful interference) 7600 Loss of communications...

  • Page 218: Function Display

    Section 917 Pilot´s Operating Handbook BENDIX/KING KT 73 Transponder EXTRA 300L When in TST mode, rotating the BRT knob (= 4th ATCRBS Code Selector Knob) will manually adjust the display brightness. Clockwise rotating will increase display brightness and counterclockwise will decrease display brightness. The brightness of the display is determined by a photocell relative to the programmed or manual adjusted brightness level.

  • Page 219: Failure Annunciation

    Pilot´s Operating Handbook Section 917 EXTRA 300L BENDIX/KING KT 73 Transponder 917.1.7 FAILURE ANNUNCIATION If the unit detects an internal failure, FAIL annunciation light on the left side of the displays will illuminate. 917.2 LIMITATIONS Not applicable. 917.3 EMERGENCY PROCEDURES IMPORTANT CODES 7600 Loss of communications.
  • Page 220 Section 917 Pilot´s Operating Handbook BENDIX/KING KT 73 Transponder EXTRA 300L Left blank intentionally 917 - 8 Page Date: 31. March 2009...
  • Page 221 Pilot´s Operating Handbook Section 918 EXTRA 300L BECKER ATC 2000 Transponder SECTION 918 BECKER ATC 2000 TRANSPONDER Table of Contents Paragraph Page SECTION 918 BECKER ATC 2000 TRANSPONDER 918.1 GENERAL ........................918-3 918.1.1 Built-in Test ........................918-4 918.1.2 Squawk selection ......................918-4 918.1.3...
  • Page 222 Section 918 Pilot´s Operating Handbook BECKER ATC 2000 Transponder EXTRA 300L Left blank intentionally 918 - 2 Page Date: 15. December 2005...

  • Page 223: General

    Pilot´s Operating Handbook Section 918 EXTRA 300L BECKER ATC 2000 Transponder 918.1 GENERAL The Becker panel mounted ATC 2000 Transponder is a radio transmitter and receiver that fulfills the role of the airborne beacon equipment according to the requirements of the Air Traffic Radar Beacon System (ATCRBS).

  • Page 224: Built-In Test

    Section 918 Pilot´s Operating Handbook BECKER ATC 2000 Transponder EXTRA 300L N O T E The ATC 2000 owner accepts all responsibility for obtaining the proper license before using the transponder. N O T I C E Damage possible due to current peaks.

  • Page 225: Mode A Operation

    Pilot´s Operating Handbook Section 918 EXTRA 300L BECKER ATC 2000 Transponder 918.1.3 MODE A OPERATION Activate the transponder on ATC request only. To enshure instant readiness, position the mode switch to SBY (standby) during the flight. Set the code requested by ATC using the four coding switches. Set two-digit code numbers in the first two windows of the readout.

  • Page 226: Normal Procedures

    Section 918 Pilot´s Operating Handbook BECKER ATC 2000 Transponder EXTRA 300L 918.4 NORMAL PROCEDURES Not applicable 918.5 PERFORMANCE Not applicable 918 - 6 Page Date: 15. December 2005...
  • Page 227 Section 919 Pilot´s Operating Handbook BECKER ATC 4401 Transponder EXTRA 300L SECTION 919 BECKER ATC 4401 TRANSPONDER Table of Contents Paragraph Page SECTION 919 BECKER ATC 4401 TRANSPONDER 919.1 GENERAL ........................919-3 919.1.1 Controls and indicators ....................919-4 919.1.2 Switching on the unit (pre-flight check) ................919-4 919.1.3...
  • Page 228 Section 919 Pilot´s Operating Handbook BECKER ATC 4401 Transponder EXTRA 300L Left blank intentionally 919 - 2 Page Date: 15. December 2005...

  • Page 229: General

    Section 919 Pilot´s Operating Handbook BECKER ATC 4401 Transponder EXTRA 300L 919.1 GENERAL The Becker panel mounted ATC 4401 Transponder is a radio transmitter and receiver that fulfills the role of the airborne beacon equipment according to the requirements of the Air Traffic Radar Beacon System (ATCRBS).

  • Page 230: Controls And Indicators

    Section 919 Pilot´s Operating Handbook BECKER ATC 4401 Transponder EXTRA 300L 919.1.1 CONTROLS AND INDICATORS o i t c t i f f o g i l i t h h t i o i t o i t c t i...

  • Page 231: Squawk Selection

    Section 919 Pilot´s Operating Handbook BECKER ATC 4401 Transponder EXTRA 300L 3 After the switch-on test has elapsed and no error-message is written in the display, the transponder switches to the mode set on the mode switch (A). N O T E The blind encoder is only powered if the transponder is not switched OFF (at least SBY).
  • Page 232 Section 919 Pilot´s Operating Handbook BECKER ATC 4401 Transponder EXTRA 300L b Press store push-button STO (J), the set code then flashes. c Press the VFR1 push-button (F) or the VFR2 push-button (G) wit-hin 3 seconds to store the code under the corresponding button.

  • Page 233: Flight Operation In Mode A (Transponder Reply Code Only)

    Section 919 Pilot´s Operating Handbook BECKER ATC 4401 Transponder EXTRA 300L N O T E Unintentional transmission of an emergency code is prevented in that the transponder replies are inhibited whilst the code is being set. This applies particularly where the new code is being set in the ON or ALT modes.

  • Page 234: Configuration Mode

    Pilot´s Operating Handbook BECKER ATC 4401 Transponder EXTRA 300L 3 A further test of the unit is triggered, if the VFR1 button (F) and VFR2 button (G) are pressed simultaneously. At this test all segments must flash into display (E) as long as the buttons are pushed.
  • Page 235 Pilot´s Operating Handbook Section 920 EXTRA 300L BECKER BXP 6401 Transponder SECTION 920 BECKER BXP 6401 TRANSPONDER Table of Contents Paragraph Page SECTION 920 BECKER ATC 6401 TRANSPONDER 920.1 GENERAL ........................920-3 920.1.1 Controls and Indicators ....................920-4 920.1.2 Switching on the Unit (pre-flight check) ................920-4 920.1.3...
  • Page 236 Section 920 Pilot´s Operating Handbook BECKER BXP 6401 Transponder EXTRA 300L Left blank intentionally 920 - 2 Page Date: 31. March 2009...

  • Page 237: General

    Pilot´s Operating Handbook Section 920 EXTRA 300L BECKER BXP 6401 Transponder 920.1 GENERAL The Becker panel mounted BXP 6401 Transponder is a radio transmitter and receiver that fulfills the role of the airborne beacon equipment according to the requirements of the Air Traffic Radar Beacon System (ATCRBS).

  • Page 238: Controls And Indicators

    Section 920 Pilot´s Operating Handbook BECKER BXP 6401 Transponder EXTRA 300L 920.1.1 CONTROLS AND INDICATORS h t i o i t c t i o i t o i t c t i o i t c t i t i t l...

  • Page 239: Squawk Selection

    Pilot´s Operating Handbook Section 920 EXTRA 300L BECKER BXP 6401 Transponder N O T E The blind encoder is only powered if the transponder is not switched OFF (at least SBY). A blind encoder needs a warm-up time (sometimes a several minutes). Therefore although the solid state transponder needs no warm-up time, turn the transponder to SBY immediately after starting the engine.

  • Page 240: Squawk Ident

    Section 920 Pilot´s Operating Handbook BECKER BXP 6401 Transponder EXTRA 300L 7777 Military interceptor operations (Never squawk this code) 0000 Military use (Not enterable) Avoid selecting code 7500 and all codes in the 7600-7777 range. These trigger special indicators in automated facilities. Only the code 7500 will be decoded as the hijack code. An aircraft’s transponder code (if available) is utilized to enhance the tracking capabilities of the ATC facility, therefore care should be taken when making routine code changes.

  • Page 241: Selection Mode

    Pilot´s Operating Handbook Section 920 EXTRA 300L BECKER BXP 6401 Transponder During the PBIT the XPDR is in the SBY mode but this is not indicated on the display. The operating mode indication on the display starts immediately after finalisation of the PBIT.
  • Page 242 Section 920 Pilot´s Operating Handbook BECKER BXP 6401 Transponder EXTRA 300L SETTING THE FLIGHT NUMBER: 1 Press SEL button (G) to enter the select mode. 2 Rotate (B) until 'AI' is displayed. 3 Push (C) to switch to 'FN'. The cursor is set on the first character.

  • Page 243: Flight Operation In Mode A/C/S (Reply Code And Altitude Code)

    Pilot´s Operating Handbook Section 920 EXTRA 300L BECKER BXP 6401 Transponder VFR CODE PRESETTING Press the SEL button (G) to get into configuration mode (selection is indicated in the left bottom corner of the display under the operating mode indication).

  • Page 244: Vfr Code Activation

    Section 920 Pilot´s Operating Handbook BECKER BXP 6401 Transponder EXTRA 300L 920.1.9 VFR CODE ACTIVATION 1 Press the VFR push-button (J). The preselected code is then displayed. After 3 seconds, the displayed code gets active and overwrites the previously-set reply code.
  • Page 245 Pilot´s Operating Handbook Section 921 EXTRA 300L Lycoming AEIO-580-B1A Engine SECTION 921 LYCOMING AEIO-580-B1A ENGINE Table of Contents Paragraph Page SECTION 921 921.1 GENERAL ......................... 921-3 921.2 LIMITATIONS ........................921-3 921.2.1 Engine Limitations ......................921-3 921.2.2 Weight Limits ........................921-4 921.2.3...
  • Page 246 Section 921 Pilot´s Operating Handbook Lycoming AEIO-580-B1A Engine EXTRA 300L Left blank intentionally 921 - 2 Page Date: 5. December 2008...

  • Page 247: General

    Lycoming AEIO-580-B1A Engine 921.1 GENERAL As an alternative to the Lycoming AEIO-540-L1B5 engine the EXTRA 300L can be equipped with an AEIO-580-B1A engine. It is a six-cylinder, horizontally opposed, aircooled, direct drive, fuel injection engine with inverted oil system. The EXTRA 300L with AEIO-580-B1A engine is available in one of the following fuel tank configurations ex factory, both combined with a wing tank of 120 L (31.7 US gal) capacity:...

  • Page 248: Weight Limits

    Section 921 Pilot´s Operating Handbook Lycoming AEIO-580-B1A Engine EXTRA 300L 921.2.2 Weight Limits Max allowed empty weight: -Normal category configuration 1 742 kg (1636 lb) configuration 2 729 kg (1607 lb) -Acrobatic category single seat operation / ACRO I configuration 1...

  • Page 249: Instrument Markings

    Pilot´s Operating Handbook Section 921 EXTRA 300L Lycoming AEIO-580-B1A Engine (On the rear instrument panel CENTER TANK INDICATION next to the fuel quantity indicator) SHOWS "ZERO" IN LEVEL FLIGHT BELOW 9 L (2.4 US GAL). UNUSABLE FUEL 2 L (0.5 US GAL) 921.2.5 Instrument Markings...

  • Page 250: Performance

    Section 921 Pilot´s Operating Handbook Lycoming AEIO-580-B1A Engine EXTRA 300L 921.5 PERFORMANCE Due to the slightly increased power as well as the similar brake specific fuel consumption of the AEIO-580-B1A engine compared to the AEIO-540-L1B5 engine, the performance data given in Section 5 of this handbook are considered to be conservative thus can be applied in general.
  • Page 251 Pilot´s Operating Handbook Section 921 EXTRA 300L Lycoming AEIO-580-B1A Engine Eng. Manif. Power Setting Fuel Endur. Range Mixture Press. Consumption [ft] (m) [rpm] [inHg] [hp] [L/h] (gal/h) [kts] (km/h) [kts] (km/h) [h] [nm] (km) Best ... 2000 2700* 26.5 88.2 (23.3) 182.6 (338) 173 (320) 1.49...

  • Page 252: Range Configuration 1

    Section 921 Pilot´s Operating Handbook Lycoming AEIO-580-B1A Engine EXTRA 300L 921.5.2 Range Configuration 1 921 - 8 Page Date: 5. December 2008 Page Date: 19. April 2012...

  • Page 253: Endurance Configuration 1

    Pilot´s Operating Handbook Section 921 EXTRA 300L Lycoming AEIO-580-B1A Engine 921.5.3 Endurance Configuration 1 Page Date: 5. December 2008 Page Date: 19. April 2012 921 - 9...

  • Page 254: Cruise Performance Chart Configuration 2

    Section 921 Pilot´s Operating Handbook Lycoming AEIO-580-B1A Engine EXTRA 300L 921.5.4 Cruise Performance Chart Configuration 2 Configuration: T/O Weight 950 kg (2095 lb) Acro & Center Tank Fuel Capacity 69 L (18.2 US gal) Total Fuel Capacity 189 L (49.9 US gal) Range and Endurance values include fuel for warm-up and Take-Off from SL, max.

  • Page 255: Range Configuration 2

    Pilot´s Operating Handbook Section 921 EXTRA 300L Lycoming AEIO-580-B1A Engine 921.5.5 Range Configuration 2 Page Date: 5. December 2008 Page Date: 19. April 2012 921 - 11...

  • Page 256: Endurance Configuration 2

    Section 921 Pilot´s Operating Handbook Lycoming AEIO-580-B1A Engine EXTRA 300L 921.5.6 Endurance Configuration 2 921 - 12 Page Date: 5. December 2008 Page Date: 19. April 2012...

  • Page 257: Weight And Balance

    Pilot´s Operating Handbook Section 921 EXTRA 300L Lycoming AEIO-580-B1A Engine 921.6 WEIGHT AND BALANCE LOADING WEIGHTS AND MOMENTS FUEL ACRO & CENTER TANK WING TANK kg x cm kg x cm (US gal) (lb) (lb x in) (US gal) (lb) (lb x in) (2.4)
  • Page 258 Section 921 Pilot´s Operating Handbook Lycoming AEIO-580-B1A Engine EXTRA 300L Figure 921-1, Center Tank Versions 921 - 14 Page Date: 5. December 2008 Page Date: 19. April 2012...
  • Page 259 EXTRA 300L Lycoming AEIO-580-B1A Engine Figure 921-1 shows both fuselage fuel tank configurations which are available for the EXTRA 300L ex factory. Item 6 shows the contour of the center tank with 42 L (11.1 US gal) capacity (configuration 1). Item 7 shows the contour of the center tank with 60 L (15.9 US gal) capacity (configuration 2).
  • Page 260 Section 921 Pilot´s Operating Handbook Lycoming AEIO-580-B1A Engine EXTRA 300L Left blank intentionally 921 - 16 Page Date: 5. December 2008 Page Date: 19. April 2012...
  • Page 261 Pilot´s Operating Handbook Section 922 EXTRA 300L Center Tank Increased Capacity SECTION 922 CENTER TANK INCREASED CAPACITY Table of Contents Paragraph Page SECTION 922 922.1 GENERAL ......................... 922-3 922.2 LIMITATIONS ........................922-3 922.2.1 Fuel ..........................922-3 922.2.2 Weight Limits ........................922-3 922.2.3...
  • Page 262 Section 922 Pilot´s Operating Handbook Center Tank Increased Capacity EXTRA 300L Left blank intentionally 922 - 2 Page Date: 5. December 2008...

  • Page 263: General

    922.1 GENERAL The center fuel tank with an increased fuel capacity from 42 to 60 L is available ex factory for the fuelage fuel tank system of the EXTRA 300L. 922.2 LIMITATIONS The following data deviate from the data given in Section 2 of this Handbook: 922.2.1 Fuel...

  • Page 264: Performance

    Section 922 Pilot´s Operating Handbook Center Tank Increased Capacity EXTRA 300L 922.5 PERFORMANCE 922.5.1 Cruise Performance Range and Endurance values for a T/O Weight of 950 kg (2095 lb) including fuel for warm-up and Take-Off from SL, max. cont. Power climb to cruising altitude, and a reserve of 21 L (5.55 gal) for 45 minutes with 45% Power.

  • Page 265: Range

    Pilot´s Operating Handbook Section 922 EXTRA 300L Center Tank Increased Capacity 922.5.2 Range Page Date: 5. December 2008 922 - 5...

  • Page 266: Endurance

    Section 922 Pilot´s Operating Handbook Center Tank Increased Capacity EXTRA 300L 922.5.3 Endurance 922 - 6 Page Date: 5. December 2008...

  • Page 267: Weight And Balance

    Pilot´s Operating Handbook Section 922 EXTRA 300L Center Tank Increased Capacity 922.6 WEIGHT AND BALANCE LOADING WEIGHTS AND MOMENTS TOTAL FUEL CAPACITY: 189 L (49.9 US gal) FUEL ACRO & CENTER TANK WING TANK kg x cm kg x cm...

  • Page 268: Description Of The System

    Section 922 Pilot´s Operating Handbook Center Tank Increased Capacity EXTRA 300L 922.7 DESCRIPTION OF THE SYSTEM (Refer to Figure 922-1) The center fuel tank (5) with increased fuel capacity is installed in the same place and in the same manner as the standard fuel center tank. This includes the vent line (2) and the fuel filler (3) location.
  • Page 269 Pilot´s Operating Handbook Section 923 EXTRA 300L GARMIN GTX 328 Transponder SECTION 923 GARMIN GTX 328 TRANSPONDER Table of Contents Paragraph Page SECTION 923 GARMIN GTX 328 TRANSPONDER 923.1 GENERAL ......................... 923-3 923.1.1 Mode Selection Keys ......................923-4 923.1.2 Code Selection ......................... 923-4 923.1.3...
  • Page 270 Section 923 Pilot´s Operating Handbook GARMIN GTX 328 Transponder EXTRA 300L Left blank intentionally 923 - 2 Page Date: 5. December 2008...

  • Page 271: General

    Pilot´s Operating Handbook Section 923 EXTRA 300L GARMIN GTX 328 Transponder 923.1 GENERAL The Garmin GTX 328 panel mounted Mode S VFR Transponder is a radio transmitter and receiver that fulfills the role of the airborne beacon equipment according to the requirements of the Air Traffic Radar Beacon System (ATCRBS).

  • Page 272: Mode Selection Keys

    Section 923 Pilot´s Operating Handbook GARMIN GTX 328 Transponder EXTRA 300L 923.1.1 MODE SELECTION KEYS Powers off the GTX 328. Pressing STBY, ON or ALT Key powers on the transponder displaying the last active identification code. STBY Selects the standby mode. When in standby mode, the transponder will not reply to any inter- rogations.

  • Page 273: Keys For Other Gtx 328 Functions

    Pilot´s Operating Handbook Section 923 EXTRA 300L GARMIN GTX 328 Transponder Avoid selecting codes 0000, 7500, and all codes in the 7600-7777 range. These codes trigger special indicators in automated facilities. An aircraft’s transponder code is used for ATC tracking purposes, therefore exercise care when making routine code changes! 923.1.3 KEYS FOR OTHER GTX 328 FUNCTIONS...

  • Page 274: Configuration Mode

    Section 923 Pilot´s Operating Handbook GARMIN GTX 328 Transponder EXTRA 300L 'ALTITUDE MONITOR' The ALTITUDE MONITOR function is not available in this installation. 'OAT/DALT' The OAT/DALT function is not available in this installation (no temperature input). 'COUNT UP TIMER' Controlled by the START/STOP and CLR keys. Pressing the CLR key zeros the display.

  • Page 275: Limitations

    Pilot´s Operating Handbook Section 923 EXTRA 300L GARMIN GTX 328 Transponder 923.2 LIMITATIONS Not applicable. 923.3 EMERGENCY PROCEDURES 923.3.1 IMPORTANT CODES 7600 Loss of communications. 7500 Hijacking. 7700 Emergency (All secondary surveillance radar sites are ready to receive this code at all times).
  • Page 276 Section 923 Pilot´s Operating Handbook GARMIN GTX 328 Transponder EXTRA 300L Left blank intentionally 923 - 8 Page Date: 5. December 2008...
  • Page 277 Pilot´s Operating Handbook Section 924 EXTRA 300L ASPEN EFD1000 PILOT PFD SECTION 924 ASPEN EFD1000 PILOT PFD Table of Contents Paragraph SECTION 924 ASPEN EFD1000 PILOT PFD Page 924.1 GENERAL ......................... 924-3 924.2 LIMITATIONS ........................924-3 924.2.1 Placards and Decals ......................924-3 924.3...
  • Page 278 Section 924 Pilot´s Operating Handbook ASPEN EFD1000 PILOT PFD EXTRA 300L Left blank intentionally 924 - 2 Page Date: 31. March 2009...

  • Page 279: General

    Moving maps are also displayed when an external GPS is installed and connected to the EFD1000 PILOT PFD. In the EXTRA 300L the EFD1000 PILOT PFD is used as a secondary (back-up) instrument system. N O T E Due to the capabilities of the aircraft - especially the extreme agility with high angular rates - the EFD1000 PILOT PFD cannot be operated reliably in acrobatics.

  • Page 280: Emergency Procedures

    Section 924 Pilot´s Operating Handbook ASPEN EFD1000 PILOT PFD EXTRA 300L The following electronic placard is provided on the EFD1000 PILOT PFD display whenever the RSM GPS is providing position data for the basemap display: „RSM GPS REVERSION EMER USE ONLY“...

  • Page 281: Pilot Controls Overview

    Pilot´s Operating Handbook Section 924 EXTRA 300L ASPEN EFD1000 PILOT PFD 924.7.2 PILOT CONTROLS OVERVIEW Pilot interaction with the EFD1000 PILOT PFD is accomplished through two knobs with push/rotate function and 11 buttons located on the display bezel. Refer to Figure 2. Two control knobs are used to control pilot settable bugs and references.

  • Page 282: Display Screen And Control Layout

    Pilot´s Operating Handbook ASPEN EFD1000 PILOT PFD EXTRA 300L In the unlikely event that the normal power control is not working, the EFD1000 PILOT PFD may be forced to shut down by first pulling the PFD circuit breaker and then pressing and holding the REV button for at least 5 seconds.

  • Page 283: Control Knobs

    Pilot´s Operating Handbook Section 924 EXTRA 300L ASPEN EFD1000 PILOT PFD 924.7.5 CONTROL KNOBS General Two control knobs on the EFD bezel are used to adjust pilot editable data fields. The left knob adjusts data fields on the left side of the display, and the right knob adjusts data fields on the right side of the display.

  • Page 284: Knob Sync Function

    Section 924 Pilot´s Operating Handbook ASPEN EFD1000 PILOT PFD EXTRA 300L Indicated Airspeed Bug Set To set the indicated airspeed bug, repeatedly PUSH the left control knob until the IAS field is enabled for editing. ROTATE the knob to the desired setting.

  • Page 285: Back Light Control

    Pilot´s Operating Handbook Section 924 EXTRA 300L ASPEN EFD1000 PILOT PFD COMPASS PRESENTATION FORMAT Hot Key 3 toggles the compass between a 360 rose display and a 100 deg ARC display. BASEMAP AND DECLUTTER LEVEL Hot Key 4 is used to enable the basemap and control the amount of basemap symbology that is presented to the pilot.

  • Page 286: Map Range Control

    Section 924 Pilot´s Operating Handbook ASPEN EFD1000 PILOT PFD EXTRA 300L 924.7.10 MAP RANGE CONTROL The EFD1000 PILOT PFD basemap range may be set to ranges of 2.5, 5, 10, 15, 20, 30, 40, 60, 80, 100, and 200 nautical miles. Map range is measured from the own ship position to the outside of the compass arc.

  • Page 287: Main Menu Operation

    Pilot´s Operating Handbook Section 924 EXTRA 300L ASPEN EFD1000 PILOT PFD RSM GPS Amber annunciation presented on the left edge of the display to indicate when a configured GPS flight plan and mapping data is invalid or not available. RSM GPS REVERSION...

  • Page 288: Handling, Servicing And Maintenance

    · ENABLE or DISABLE the display of V-Speeds · Perform an AHRS RESET. V-Speed Setting Pages This page is configured by EXTRA according to the speed values given in Section 4.0.1 of this Handbook. Values can be changed by the pilot. Power Settings Page The POWER SETTINGS page is used to monitor and control the source of power to the EFD1000 PILOT PFD, including overriding automatic power states.
  • Page 289 Pilot´s Operating Handbook Section 925 EXTRA 300L GARMIN GNC 420W SECTION 925 GARMIN GNC 420W Table of Contents SECTION 925 GARMIN GNC 420W Paragraph Page 925.1 GENERAL ......................... 925-3 925.1.1 GPS/WAAS TSO-C146a Class 3 Operation: ..............925-3 925.1.2 Class II Oceanic, Remote, and other Operations: .............. 925-3 925.2...
  • Page 290 Section 925 Pilot´s Operating Handbook GARMIN GNC 420W EXTRA 300L Left blank intentionally 925 - 2 Page Date: 31. March 2009...

  • Page 291: General

    Pilot´s Operating Handbook Section 925 EXTRA 300L GARMIN GNC 420W 925.1 GENERAL The Garmin GNC 420W GPS Navigator is a panel-mounted unit that contains a GPS receiver for GPS navigation plus VHF Com radio in an integrated unit with a moving map and color display. The GNC 420W features a graphical display which may also be used to depict terrain data.

  • Page 292: Limitations

    Pilot´s Operating Handbook GARMIN GNC 420W EXTRA 300L of five degrees. The GNC 420W also has the ability to predict RAIM availability at any waypoint in the database if WAAS corrections are expected to be absent or disabled. This AFMS does not constitute an operational approval for Oceanic or Remote area operations.

  • Page 293: Normal Procedures

    Pilot´s Operating Handbook Section 925 EXTRA 300L GARMIN GNC 420W LOSS OF INTEGRITY MONITORING If Loss of Integrity Monitoring message is displayed, revert to an alternate means of navigation appropriate to the route and phase of flight or periodically cross-check the GPS guidance to other, approved means of navigation.

  • Page 294: Weight & Center Of Gravity

    Section 925 Pilot´s Operating Handbook GARMIN GNC 420W EXTRA 300L 925.6 WEIGHT & CENTER OF GRAVITY Refer to the equipment list in Section 6 of this Handbook. 925.7 SYSTEM DESCRIPTION 925.7.1 KEY AND KNOB FUNCTIONS LEFT-HAND KEYS AND KNOBS The COM power/volume knob controls unit power and communications radio volume. Press momentarily to disable automatic squelch control.
  • Page 295 Pilot´s Operating Handbook Section 925 EXTRA 300L GARMIN GNC 420W The small right knob (CRSR) is used to select between the various pages within one of the groups listed above. Press this knob momentarily to display the on-screen cursor. The cursor allows you to enter data and/or make a selection from a list of options.

  • Page 296: Default Nav Page

    Section 925 Pilot´s Operating Handbook GARMIN GNC 420W EXTRA 300L 925.7.2 DEFAULT NAV PAGE During most flights, the default NAV, map and NAVCOM pages will be the primary pages used for navigation. The default NAV page displays a graphic course deviation indicator (CDI), the active leg of your flight plan (as defined by the current „from“...
  • Page 297 Pilot´s Operating Handbook Section 926 EXTRA 300L ARTEX ME-406 ELT SECTION 926 ARTEX ME-406 ELT Table of Contents Paragraph SECTION 926 ARTEX ME-406 ELT Page 926.1 GENERAL ......................... 926-3 926.2 LIMITATIONS ........................926-3 926.3 EMERGENCY PROCEDURES ................... 926-4 926.4 NORMAL PROCEDURES ....................926-4 926.5...
  • Page 298 Section 926 Pilot´s Operating Handbook ARTEX ME-406 ELT EXTRA 300L Left blank intentionally 926 - 2 Page Date: 31. March 2009...

  • Page 299: General

    ARTEX ME-406 ELT 926.1 GENERAL To improve the passive security, the EXTRA 300/L can be equipped with an optional Emergency Locator Transmitter ARTEX ME-406. In the event of a crash, the ME-406 activates automatically (automatic fixed „AF“ configuration), and transmits the standard swept tone on 121.5 MHz lasting until battery power is gone. This 121.5 MHz signal is mainly used to pinpoint the beacon during search and rescue operations.

  • Page 300: Emergency Procedures

    Section 926 Pilot´s Operating Handbook ARTEX ME-406 ELT EXTRA 300L 926.3 EMERGENCY PROCEDURES • In case of a forced landing turn the remote switch in the rear panel to the "ON" position prior to touch down. Although the ELT will be activated automatically after an aircraft accident or forced landing with high G-force, •...

  • Page 301: System Description

    Pilot´s Operating Handbook Section 926 EXTRA 300L ARTEX ME-406 ELT 926.7 SYSTEM DESCRIPTION The ELT installation consists of the ELT unit and a buzzer, both fastened to the fuselage structure aft of the back seat, an antenna located on the main fuselage cover behínd the cockpit, and a remote switch with LED indication located on the instrument panel.

  • Page 302: Handling, Servicing And Maintenance

    Section 926 Pilot´s Operating Handbook ARTEX ME-406 ELT EXTRA 300L 926.8 HANDLING, SERVICING AND MAINTENANCE 926.8.1 TRANSMITTER TEST ARTEX recommends that the ELT be tested every 1-2 months. Follow the steps outlined in the 926.8.2 SELF TEST paragraph. N O T E The self-test time is accumulated in a register on the battery pack.
  • Page 303 Pilot´s Operating Handbook Section 926 EXTRA 300L ARTEX ME-406 ELT • If this error code persists there may be a problem with the antenna installation. This can be checked with a VSWR meter. Check the antenna for opens, shorts, resistive ground plane connection.
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  • Page 305 Pilot´s Operating Handbook Section 927 EXTRA 300L AIRPLANES REGISTERED IN BRAZIL SECTION 927 AIRPLANES REGISTERED IN BRAZIL AND OPERATING UNDER THE AGÊNCIA NACIONAL DE AVIAÇÃO CIVIL REQUIREMENTS Table of Contents Paragraph Page  927.1 GENERAL ......................... 927-3 927.2 LIMITATIONS ........................927-4 927.2.1...
  • Page 306 Section 927 Pilot´s Operating Handbook AIRPLANES REGISTERED IN BRAZIL EXTRA 300L Left blank intentionally 927 - 2 Page Date: 19. April 2012...

  • Page 307: General

    Pilot´s Operating Handbook Section 927 EXTRA 300L AIRPLANES REGISTERED IN BRAZIL 927.1 GENERAL This supplement is approved by the EASA on behalf of the „Agência Nacional de Aviação Civil“ – ANAC for Brazilian registered aircraft, in accordance with the „Regulamento Brasileiro da Aviação Civil“...

  • Page 308: Limitations

    Section 927 Pilot´s Operating Handbook AIRPLANES REGISTERED IN BRAZIL EXTRA 300L 927.2 LIMITATIONS 927.2.1 ENGINE The following Textron-Lycoming engines are certified: 1) Engine-type AEIO-540-L1B5 with rated maximum 300HP@2700RPM 2) Engine-type AEIO-580-B1A with rated maximum 315HP@2700RPM 927.2.2 KINDS OF OPERATIONAL LIMITS Operation is limited to VFR-day.

  • Page 309: Weight & Center Of Gravity

    Pilot´s Operating Handbook Section 927 EXTRA 300L AIRPLANES REGISTERED IN BRAZIL 927.6 WEIGHT & CENTER OF GRAVITY Not affected. 927.7 SYSTEM DESCRIPTION Not affected. 927.8 HANDLING, SERVICING AND MAINTENANCE Not affected. Page Date: 19. April 2012 927- 5...
  • Page 310 Section 927 Pilot´s Operating Handbook AIRPLANES REGISTERED IN BRAZIL EXTRA 300L Left blank intentionally 927 - 6 Page Date: 19. April 2012...
  • Page 311 Section 928 Pilot´s Operating Handbook Landing Light EXTRA 300L SECTION 928 LANDING LIGHT SECTION 928 LANDING LIGHT Table of Contents Paragraph Page 928.1 GENERAL ......................... 928-3 928.2 LIMITATION ........................928-3 928.3 EMERGENCY PROCEDURES ................... 928-3 928.4 NORMAL PROCEDURES ....................928-3 928.5...
  • Page 312 Section 928 Pilot´s Operating Handbook Landing Light EXTRA 300L Left blank intentionally 928 - 2 Page Date: 17. January 2013...

  • Page 313: General

    Section 928 Pilot´s Operating Handbook Landing Light EXTRA 300L LANDING LIGHT 928.1 GENERAL To improve the visibility of the aircraft during approach and landing a landing light can be integrated in the RH lower cowling. 928.2 LIMITATION No change. 928.3 EMERGENCY PROCEDURES No change.

  • Page 314: Handling, Servicing And Maintenance

    Section 928 Pilot´s Operating Handbook Landing Light EXTRA 300L 928.8 HANDLING, SERVICING AND MAINTENANCE No change. 928 - 4 Page Date: 17. January 2013...
  • Page 315 Pilot´s Operating Handbook Section 929 EXTRA 300L GARMIN GTN 635/650/750 SECTION 929 GARMIN GTN 635/650/750 Table of Contents Paragraph Page 929.1 GENERAL ......................... 929-3 929.2 LIMITATIONS ........................929-3 929.2.1 Placards ........................... 929-5 929.2.2 SD Card ..........................929-5 929.2.3 Terrain ..........................929-5 929.2.4...
  • Page 316 Section 929 Pilot´s Operating Handbook GARMIN GTN 635/650/750 EXTRA 300L Left blank intentionally 929 - 2 Page Date: 20. January 2016...

  • Page 317: General

    Pilot´s Operating Handbook Section 929 EXTRA 300L GARMIN GTN 635/650/750 929.1 GENERAL This Airplane Flight Manual Supplement (AFMS) is written for the Garmin GTN 635/650/750 units. The Garmin GTN 635 is a GPS (WAAS/SBAS capable) panel-mounted unit that includes an airborne VHF communications transceiver.
  • Page 318 Section 929 Pilot´s Operating Handbook GARMIN GTN 635/650/750 EXTRA 300L Figure 2, GTN 750 Display Layout The system must utilize main software version 2.00, GPS software version 4.0, COM software version 2.01 and NAV software version 6.01 or later EASA/FAA approved versions. Valid and compatible databases must be installed and contain current data.

  • Page 319: Placards

    Pilot´s Operating Handbook Section 929 EXTRA 300L GARMIN GTN 635/650/750 929.2.1 PLACARDS GARMIN GPS limited to VFR use only (In close proximity to the GTN unit in clear view of the pilot) (Next to the GTN unit GPS circuit breaker)

  • Page 320: Glove Use

    Section 929 Pilot´s Operating Handbook GARMIN GTN 635/650/750 EXTRA 300L 929.2.6 GLOVE USE No device may be used to cover fingers used to operate the GTN unless the Glove Qualification Procedure located in the Pilot's Guide has been successfully completed. The Glove Qualification Procedure is specific to a pilot/glove/GTN unit combination.

  • Page 321: Normal Procedures

    Pilot´s Operating Handbook Section 929 EXTRA 300L GARMIN GTN 635/650/750 B) DEAD RECKONING MODE If the amber Dead Reckoning (DR) Mode message is displayed, the course guidance will be removed from the CDI. The airplane position will be based on the last valid GPS position, then estimated by Dead Reckoning methods.

  • Page 322: Weight & Center Of Gravity

    Section 929 Pilot´s Operating Handbook GARMIN GTN 635/650/750 EXTRA 300L 929.6 WEIGHT & CENTER OF GRAVITY Refer to the equipment list in Section 6 of this Handbook. 929.7 SYSTEM DESCRIPTION 929.7.1 TOUCHSCREEN, KEY AND KNOB FUNCTIONS Controls are a combination of a dual concentric rotary knob and push-keys on the bezel with the color display providing information as well as active touch areas on the display.

  • Page 323: Secure Digital Card

    Pilot´s Operating Handbook Section 929 EXTRA 300L GARMIN GTN 635/650/750 Figure 3, GTN 6xx XPDR Operation 929.7.2 SECURE DIGITAL CARD A Secure Digital (SD) card is used to load and store various types of data and for various database updates. Ensure the GTN unit is powered off before inserting or removing an SD card.

  • Page 324: Remote Transponder Operation

    Section 929 Pilot´s Operating Handbook GARMIN GTN 635/650/750 EXTRA 300L Figure 4, GTN 750 XPDR Operation 929.7.4 REMOTE TRANSPONDER OPERATION Optionally, a remote transponder (GTX 33) can be controlled via the GTN 635/650/750 unit. Touch the transponder window to enter the transponder operation page. See figures 3 and 4 for the GTN 6xx and the GTN 750 respectively.
  • Page 325 Pilot´s Operating Handbook Section 929 EXTRA 300L GARMIN GTN 635/650/750 STANDBY 1. Touch the Mode key to show a list of available modes (directly accessible from the transponder operation page on the GTN 750). Touch the Standby key to place the transponder into Standby mode.

  • Page 326: Remote Audio Panel Operation (Gtn 750 Only)

    Section 929 Pilot´s Operating Handbook GARMIN GTN 635/650/750 EXTRA 300L IMPORTANT CODES: 1200 The VFR code for any altitude in the US (Refer to ICAO standards elsewhere) 7000 The VFR code commonly used in Europe (Refer to ICAO standards) 7500 Hijack code (Aircraft is subject to unlawful interference)
  • Page 327 Pilot´s Operating Handbook Section 929 EXTRA 300L GARMIN GTN 635/650/750 2. Touch the Mon key to toggle between the automatically selected monitored channel (selected Mic) and the other available channels. AUDIO SPLIT MODE 1. While the Audio Control page is displayed, touch the Split Mode key to display Crew Intercom selections.
  • Page 328 Section 929 Pilot´s Operating Handbook GARMIN GTN 635/650/750 EXTRA 300L PLAYBACK CONTROLS 1. While the Audio Control page is displayed, touch the Playback Controls key to display the Playback Controls selections. 2. Touch the Playback Volume arrows to set volume.

  • Page 329: Map Page

    Pilot´s Operating Handbook Section 929 EXTRA 300L GARMIN GTN 635/650/750 To acknowledge or advance to the next page, touch Continue. 929.7.7 MAP PAGE During most flights, the Map page will be used for situational awareness. The Map page displays Airports, NAVAIDs, airspace, airways, land data (highways, cities, lakes, rivers, borders, etc.) with...
  • Page 330 Section 929 Pilot´s Operating Handbook GARMIN GTN 635/650/750 EXTRA 300L Left blank intentionally 929 - 16 Page Date: 20. January 2016...

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