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Extra 300LT 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 T
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 T 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 300LT LOG OF REVISIONS Dates of issue for original and revised pages: Date and sign of approval: Original ..........6. April 2010 EASA MAJOR CHANGE APPROVAL 10030180 Date of Approval ......... 1. June 2010 Revision No. 1 ........31. May 2012 Approved under the authority of DOA N°...
  • Page 4 Pilot´s Operating Handbook EXTRA 300LT LOG OF EFFECTIVE PAGES Page Date Page Date Title ......... 6. April 2010 i thru ii ........22. April 2015 iii thru vi ........6. April 2010 1-1 thru 1-8 ......6. April 2010 2-1 ........6. November 2012 2-2 thru 2-5 ......
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  • 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 300LT WARNINGS, CAUTIONS AND NOTES The following definitions apply to Warnings, Cautions, and Notes: WARNING => Operating procedures, techniques, etc., which could result in personal injury or loss of life if not carefully followed. CAUTION => Operating procedures, techniques, etc., which could result in damage to equipment if not carefully followed.
  • Page 8 Pilot´s Operating Handbook EXTRA 300LT 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: 6. April 2010...

  • Page 9: Table Of Contents

    Pilot´s Operating Handbook Section 1 EXTRA 300LT General SECTION 1 GENERAL Table of Contents Paragraph Page 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 ..........................1-4 1.3.3...
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  • Page 11: Description

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

  • Page 12: Main Data

    Section 1 Pilot´s Operating Handbook General EXTRA 300LT 1.3.2 MAIN DATA - Length 7.01 m (23.00 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)

  • Page 13: Engine

    Pilot´s Operating Handbook Section 1 EXTRA 300LT General ENGINE Manufacturer: Textron-Lycoming Williamsport Plant PA 17701 USA. Type: Lycoming AEIO-580-B1A Rated power: 315 HP/235 kW @ 2700 RPM 303 HP/226 kW @ 2600 RPM 286 HP/213 kW @ 2400 RPM PROPELLER Manufacturer: MT-Propeller Entwicklung GmbH, Federal Republic of Germany.

  • Page 14: Loading

    Section 1 Pilot´s Operating Handbook General EXTRA 300LT 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 300LT 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 300LT 1.11 CONVERSION TABLE 1 - 8 Page Date: 6. April 2010...
  • Page 17 Pilot´s Operating Handbook Section 2 EXTRA 300LT Limitations SECTION 2 LIMITATIONS Table of Contents Paragraph Page GENERAL ..........................2-3 AIR SPEED (IAS) ....................... 2-3 CROSS-WIND COMPONENT ....................2-3 ENGINE ..........................2-3 2.4.1 Fuel ............................. 2-3 2.4.2 Engine Limitations ....................... 2-4 PROPELLER ........................
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  • Page 19: General

    This aircraft is certified under Type Certification Data Sheet (T.C.D.S. EASA.A.362). Any exceedance of given limitations has to be reported by the pilot so that necessary inspection or maintenance procedures according to the MAINTENANCE MANUAL EA 300LT can be performed . AIR SPEED (IAS)

  • Page 20: Engine Limitations

    Section 2 Pilot´s Operating Handbook Limitations EXTRA 300LT 2.4.2 ENGINE LIMITATIONS a) Rotational Speed Maximum Take-Off and Maximum Continuous: 2700 rpm b) Oil-temperature - Maximum 118°C (245°F) c) Oil capacity - Maximum sump capacity: 15.13 L (16 US.qt) - Minimum sump capacity: 8.51 L...

  • Page 21: Propeller

    Pilot´s Operating Handbook Section 2 EXTRA 300LT Limitations PROPELLER MT-Propeller Entwicklung GmbH, Federal Republic of Germany, Type: MTV-9-B-C/C198-25 Maximum rotational speed - Take-Off and Maximum Continuous: 2700 rpm WEIGHT LIMITS Max allowed empty weight: - Normal category 723 kg (1594 lbs)

  • Page 22: Acrobatic Maneuvers

    Section 2 Pilot´s Operating Handbook Limitations EXTRA 300LT 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. 2.8.2 ACROBATIC FLIGHT The plane is designed for unlimited acrobatics (wing tank must be empty). Inverted flight maneuvers are limited to max 4 minutes.

  • Page 23: Load Factor

    Pilot´s Operating Handbook Section 2 EXTRA 300LT 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: Flight Crew Limits

    Section 2 Pilot´s Operating Handbook Limitations EXTRA 300LT 2.10 FLIGHT CREW LIMITS Minimum crew is one pilot in the rear seat. Solo flying from rear seat only. Maximum 2 persons are allowed. For hearing protection noise supression (passive or active) communication headsets are required.

  • Page 25: Operating Placards

    Pilot´s Operating Handbook Section 2 EXTRA 300LT Limitations 2.14.2 OPERATING PLACARDS V = 160 KTS (ACRO) V = 296 km/h (ACRO) V = 143 KTS (NORMAL) V = 265 km/h (NORMAL) (near the airspeed indicator) The markings and placards installed in 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 300LT FUEL SELECTOR VALVE WING TANKS usable 142 L (37.5 US GAL) CENTER (ACRO) TANK usable 67 L (17.7 US GAL) (in both cockpits next to the fuel selector) WING TANK MUST BE EMPTY FOR ACROBATICS.
  • Page 27 Pilot´s Operating Handbook Section 2 EXTRA 300LT Limitations PROP HIGH RPM LOW RPM (On RPM control in the rear cockpit) MIXTURE RICH LEAN (On mixture control in the rear cockpit) THROTTLE OPEN CLOSE (Near throttle control in both cockpits) CANOPY LOCK...
  • Page 28 Section 2 Pilot´s Operating Handbook Limitations EXTRA 300LT WING TANK DRAIN (Near the LH drain valve in the bottom fuselage cover) CENTER TANK DRAIN (Near the RH drain valve in the bottom fuselage cover) GASCOLATOR DRAIN (Near the drain valve on the RH lower side of the firewall)
  • Page 29 Pilot´s Operating Handbook Section 2 EXTRA 300LT Limitations Approved acrobatic maneuvers and recommended entry airspeeds Maneuvers Airspeeds Maneuvers Airspeeds min KIAS max KIAS min KIAS max KIAS Segment: Horizontal Line Aileron roll 45°climbing Snap roll 90° up "Tail-slide" 45° diving...

  • Page 30: Instrument Markings

    Section 2 Pilot´s Operating Handbook Limitations EXTRA 300LT 2.14.3 INSTRUMENT MARKINGS AIRSPEED INDICATOR green arc 65 KIAS (120 km/h) - 160 KIAS (296 km/h) yellow arc 160 KIAS (296 km/h) - 221 KIAS (409 km/h) red line 221 KIAS (409 km/h)

  • Page 31: Kinds Of Operation Equipment List

    Pilot´s Operating Handbook Section 2 EXTRA 300LT Limitations MANIFOLD PRESSURE INDICATOR green range 10 " Hg - 30 " 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 32: Baggage

    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. 2.16 BAGGAGE The use of baggage is limited to operation in the normal catgegory.
  • Page 33 Pilot´s Operating Handbook Section 3 EXTRA 300LT Emergency Procedures SECTION 3 EMERGENCY PROCEDURE Table of Contents Paragraph Page INTRODUCTION ........................3-3 3.0.1 General ..........................3-3 3.0.2 General Behaviour in Emergency Situations ................. 3-3 AIRSPEEDS FOR EMERGENCY OPERATION ..............3-4 OPERATIONAL CHECKLIST ....................3-4 3.2.1...
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  • Page 35: Introduction

    Pilot´s Operating Handbook Section 3 EXTRA 300LT 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 36: Airspeeds For Emergency Operation

    Section 3 Pilot´s Operating Handbook Emergency Procedures EXTRA 300LT AIRSPEEDS FOR EMERGENCY OPERATION Stall speed 65 KIAS (120 km/h) Engine failure after take-off 85 KIAS (157 km/h) Best recommended gliding speed (glide angle 1 : 6,2) -Normal & Acro III Category 950 kg (2095 lbs)

  • Page 37: Oil System Malfunction

    Pilot´s Operating Handbook Section 3 EXTRA 300LT 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 85 KIAS (157 km/h) 2. Throttle REDUCE TO IDLE 3. Engine oil temperature OBSERVE INDICATION 4.

  • Page 38: Precautionary Landing With Engine Power

    Section 3 Pilot´s Operating Handbook Emergency Procedures EXTRA 300LT 3.3.2 PRECAUTIONARY LANDING WITH ENGINE POWER 1. Seat belts, shoulder harnesses SECURE 2. Airspeed 85 KIAS (157 km/h) 3. Selected field FLY OVER, noting terrain and obstructions, then reaching a safe altitude and airspeed 4.

  • Page 39: Engine Fire In Flight

    Pilot´s Operating Handbook Section 3 EXTRA 300LT Emergency Procedures 3.4.3 ENGINE FIRE IN FLIGHT 1. Mixture IDLE CUT OFF 2. Fuel shutoff valve OFF (Pull & Turn) 3. Battery switch 4. Alternator switch 5. Airspeed 100 KIAS (185 km/h), find your airspeed/attitude...

  • Page 40: Emergency Exit After Turn Over

    Section 3 Pilot´s Operating Handbook Emergency Procedures EXTRA 300LT EMERGENCY EXIT AFTER TURN OVER 1. Battery switch 2. Alternator switch 3. Fuel shutoff valve OFF (Pull & Turn) 4. Seat belts OPEN 5. Parachute harnesses (if wearing a parachute) OPEN 6.
  • Page 41 Pilot´s Operating Handbook Section 4 EXTRA 300LT Normal Procedures SECTION 4 NORMAL PROCEDURES Table of Contents Paragraph Page GENERAL ..........................4-3 4.0.1 Airspeeds for Normal Operation ................... 4-3 4.0.2 Checklist and Procedures ....................4-3 PREFLIGHT INSPECTION ....................4-4 CHECKLIST PROCEDURES ....................4-4 STARTING PROCEDURES ....................
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  • Page 43: General

    Pilot´s Operating Handbook Section 4 EXTRA 300LT Normal Procedures GENERAL 4.0.1 AIRSPEEDS FOR NORMAL OPERATION CATEGORY ACRO I ACRO II ACRO III NORMAL 820 kg 870 kg 950 kg 950 kg (1808 lbs) (1918 lbs) (2095 lbs) (2095 lbs) KIAS (km/h)

  • Page 44: Preflight Inspection

    Section 4 Pilot´s Operating Handbook Normal Procedures EXTRA 300LT 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 45 Pilot´s Operating Handbook Section 4 EXTRA 300LT Normal Procedures 2. Trailing edge CHECK 3. Fuel tank vent opening (right landing gear) CHECK 4. Fuel quantity CHECK 5. Fuel tank filler cap CHECK 6. Wing fuel tank drain DRAIN FOR AT LEAST 4 SECONDS TO CLEAR SUMP OF POSSIBLE WATER;...

  • Page 46: Starting Procedures

    Section 4 Pilot´s Operating Handbook Normal Procedures EXTRA 300LT 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 47: Take-Off Procedure

    Pilot´s Operating Handbook Section 4 EXTRA 300LT Normal Procedures TAKE-OFF PROCEDURE 4.5.1 BEFORE TAKE-OFF Before you line up at the runway for take-off: Oil pressure and oil temperature CHECK Magnetos CHECK as follows: Engine RPM: 1800 min Pay attention to the three small LEDs in the "Status" area on the upper left corner of...

  • Page 48: Climb

    Section 4 Pilot´s Operating Handbook Normal Procedures EXTRA 300LT CLIMB Climbs may be performed up to 2700 RPM. RPM above 2400 should, however, be used only when necessary for maximum performance in order to avoid unnecessary noise. Turn boost pump "OFF".

  • Page 49: Normal Landing

    Pilot´s Operating Handbook Section 4 EXTRA 300LT Normal Procedures N O T E Stall speed will be: MTOW = 820 kg (1808 lbs): 60 KIAS (111 km/h) MTOW = 870 kg (1918 lbs): 62 KIAS (115 km/h) MTOW = 950 kg (2095 lbs): 65 KIAS (120 km/h) 4.8.4...

  • Page 50: Acrobatic Maneuvers

    Section 4 Pilot´s Operating Handbook Normal Procedures EXTRA 300LT 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 51 Pilot´s Operating Handbook Section 4 EXTRA 300LT Normal Procedures - 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. The speed will gradually decrease to 0.

  • Page 52: Spin

    Section 4 Pilot´s Operating Handbook Normal Procedures EXTRA 300LT 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 53 Pilot´s Operating Handbook Section 4 EXTRA 300LT Normal Procedures No determination has been made by the Federal Aviation Administration that the noise levels of this aircraft are or should be acceptable or unacceptable for operation at, into, or out of any airport.
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  • Page 55 Pilot´s Operating Handbook Section 5 EXTRA 300LT Performance SECTION 5 PERFORMANCE Table of Contents Paragraph Page 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 ....................5-6 STALL SPEED ........................
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  • Page 57: General

    Pilot´s Operating Handbook Section 5 EXTRA 300LT 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 58 Section 5 Pilot´s Operating Handbook Performance EXTRA 300LT TAKE-OFF § 5.5 shows the Take-Off Distance. Example: T/O Weight: 950 kg (2095 lbs) Ground Roll: 223 m (732 ft) (decreased by 8% due to headwind): 205 m (673 ft) Total Distance to clear a 50 ft obstacle:...

  • Page 59: Isa Conversion

    Pilot´s Operating Handbook Section 5 EXTRA 300LT Performance LANDING § 5.13 shows the Landing Distance. Example: Landing Weight: 870 kg (1918 lbs) Ground Roll: 202 m (663 ft) (decreased by 15% due to headwind): 171 m (561 ft) Total Distance to clear a 50 ft obstacle:...

  • Page 60: Airspeed Calibration

    Section 5 Pilot´s Operating Handbook Performance EXTRA 300LT AIRSPEED CALIBRATION N O T E Indicated airspeed assumes zero instrument error 5 - 6 Page Date: 6. April 2010...

  • Page 61: Stall Speed

    Pilot´s Operating Handbook Section 5 EXTRA 300LT Performance STALL SPEED CONDITION: POWER IDLE FORWARD C/G STALL SPEEDS ANGLE OF BANK WEIGHT CATEGORY 0° 30° 45° 60° 1,15 g 1,41 g kg (lbs) KIAS (km/h) KIAS (km/h) KIAS (km/h) KIAS (km/h)

  • Page 62: Take-Off Performance

    Section 5 Pilot´s Operating Handbook Performance EXTRA 300LT 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 63 Pilot´s Operating Handbook Section 5 EXTRA 300LT Performance Take-off distance in feet for take-off roll (Roll) and take-off distance over 50 ft obstacle (50 ft) Weight 820 kg (1808 lbs), Rotating speed: 65 KIAS (120 km/h) OAT => -20°C (-4°F) -10°C (14°F) 0°C (32°F) 10°C (50°F) 20°C (68°F) 30°C (86°F) 40°C (104°F)

  • Page 64: Rate Of Climb Performance

    Section 5 Pilot´s Operating Handbook Performance EXTRA 300LT RATE OF CLIMB PERFORMANCE 5 - 10 Page Date: 6. April 2010...

  • Page 65: Time, Distance, Fuel To Climb

    Pilot´s Operating Handbook Section 5 EXTRA 300LT Performance TIME, DISTANCE, FUEL TO CLIMB Page Date: 6. April 2010 5 - 11...

  • Page 66: Range

    Section 5 Pilot´s Operating Handbook Performance EXTRA 300LT RANGE 5 - 12 Page Date: 6. April 2010...

  • Page 67: Endurance

    Pilot´s Operating Handbook Section 5 EXTRA 300LT Performance ENDURANCE Page Date: 6. April 2010 5 - 13...

  • Page 68: Cruise Speeds

    Section 5 Pilot´s Operating Handbook Performance EXTRA 300LT 5.10 CRUISE SPEEDS 5 - 14 Page Date: 6. April 2010...

  • Page 69: Cruise Performance

    Pilot´s Operating Handbook Section 5 EXTRA 300LT Performance 5.11 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 70: Time, Distance, Fuel To Descent

    Section 5 Pilot´s Operating Handbook Performance EXTRA 300LT 5.12 TIME, DISTANCE, FUEL TO DESCENT 5 - 16 Page Date: 6. April 2010...

  • Page 71: Landing Performance

    Pilot´s Operating Handbook Section 5 EXTRA 300LT Performance 5.13 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 72 Section 5 Pilot´s Operating Handbook Performance EXTRA 300LT Landing distance in feet for landing roll (Roll) and landing distance over 50 ft obstacle (50 ft) Weight 820 kg (1808 lbs), approach speed: 79 KIAS (146 km/h) OAT => -20°C (-4°F) -10°C (14°F) 0°C (32°F) 10°C (50°F) 20°C (68°F) 30°C (86°F) 40°C (104°F)
  • Page 73 Pilot´s Operating Handbook Section 6 EXTRA 300LT Weight and Balance and Equipment List SECTION 6 WEIGHT & BALANCE & EQUIPMENT LIST Table of Contents Paragraph Page GENERAL ..........................6-3 AIRCRAFT WEIGHING PROCEDURE ................. 6-3 6.2.1 Owners Weight and Balance Record ..................6-4 CENTER OF GRAVITY CALCULATION (SAMPLE PROBLEM) ...........
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  • Page 75: General

    Pilot´s Operating Handbook Section 6 EXTRA 300LT 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 76: Owners Weight And Balance Record

    Section 6 Pilot´s Operating Handbook Weight and Balance and Equipment List EXTRA 300LT 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 77: Center Of Gravity Calculation (Sample Problem)

    Pilot´s Operating Handbook Section 6 EXTRA 300LT Weight and Balance and Equipment List CENTER OF GRAVITY CALCULATION (SAMPLE PROBLEM) PILOT COPILOT BAGGAGE FUEL Position Rear Seat Front Seat ACRO & CENTER on Sheet 2 67 LTR (17.7 US GAL) (kg)
  • Page 78 Section 6 Pilot´s Operating Handbook Weight and Balance and Equipment List EXTRA 300LT CENTER OF GRAVITY CALCULATION (SAMPLE PROBLEM, SHEET 2) 6 - 6 Page Date: 6. April 2010...

  • Page 79: Sample

    Pilot´s Operating Handbook Section 6 EXTRA 300LT Weight and Balance and Equipment List 6.3.1 Sample Take-off Condition: Aircraft Empty Weight 690.0 kg (1521.2 lbs) Pilot On Rear Seat 99.0 kg ( 218.3 lbs) Copilot On Front Seat 99.0 kg ( 218.3 lbs) Baggage 10.0 kg...

  • Page 80: Loading Weights And Moments

    Section 6 Pilot´s Operating Handbook Weight and Balance and Equipment List EXTRA 300LT LOADING WEIGHTS AND MOMENTS PILOT REAR SEAT COPILOT FRONT SEAT PILOT & PARACHUTE Arm = 207cm (81.5 inch) Arm = 98 cm (38.4 inch) WEIGHT MOMENT MOMENT...

  • Page 81: Weights And Moments Limits

    Pilot´s Operating Handbook Section 6 EXTRA 300LT Weight and Balance and Equipment List WEIGHTS AND MOMENTS LIMITS Example: At 850 kg (1874 lbs) and 68000 kgcm (59031 in lbs) the C/G location is 80.0 cm (31.5") aft of ref datum Page Date: 6.

  • Page 82: Equipment List

    Section 6 Pilot´s Operating Handbook Weight and Balance and Equipment List EXTRA 300LT EQUIPMENT LIST EXTRA 300LT S/N: ITEM MANUFACTURER MODEL NO PART NO WEIGHT ARM INST. (kg) Mooring (10) Wing Tie Down Rings Extra 83801.002-01-FB 0.05 1.07 Canopy Lock Extra 83401.001-LK...
  • Page 83 Pilot´s Operating Handbook Section 6 EXTRA 300LT Weight and Balance and Equipment List ITEM MANUFACTURER MODEL NO PART NO WEIGHT ARM INST. (kg) Elec. Fuel Pump Andair PX580-TC-XT 33551 0.47 -0.04 Fuel Selector Allen 390144 0.19 0.73 Fuel Lines in Fuselage...
  • Page 84 Section 6 Pilot´s Operating Handbook Weight and Balance and Equipment List EXTRA 300LT ITEM MANUFACTURER MODEL NO PART NO WEIGHT ARM INST. (kg) Airspeed Ind., rear United Instr. UI8030 B.900 33875 0.32 1.61 (dual scale) Airspeed Ind., rear (kts) Mikrotechna Praha LUN 1106.K2B4/LT...
  • Page 85 Pilot´s Operating Handbook Section 6 EXTRA 300LT Weight and Balance and Equipment List ITEM MANUFACTURER MODEL NO PART NO WEIGHT ARM INST. (kg) RSM w/o GPS Aspen 910-00003-002 0.91 3.95 Optional Hour Meters Flight Timer Winter FSZM1510 01605 0.15 1.55...
  • Page 86 Section 6 Pilot´s Operating Handbook Weight and Balance and Equipment List EXTRA 300LT ITEM MANUFACTURER MODEL NO PART NO WEIGHT ARM INST. (kg) Transponder Antenna Comant Industries CI 105 32269 0.11 0.14 Artex ME 406 32173-PG 1.42 2.60 ELT Antenna (for Artex)
  • Page 87 Pilot´s Operating Handbook Section 6 EXTRA 300LT Weight and Balance and Equipment List ITEM MANUFACTURER MODEL NO PART NO WEIGHT ARM INST. (kg) Engine Controls (76) RPM Vernier Control ACS Products Co. 00113 0.71 0.82 Mixture Vernier Control ACS Products Co.
  • Page 88 Section 6 Pilot´s Operating Handbook Weight and Balance and Equipment List EXTRA 300LT ITEM MANUFACTURER MODEL NO PART NO WEIGHT ARM INST. (kg) Oil System (79) Single Oilcooler rear Aero Classics 31417 1.65 -0.22 Low Temperature 300 Option Breather Line Kit...
  • Page 89 Pilot´s Operating Handbook Section 7 EXTRA 300LT Description and Operation of Aircraft and Systems SECTION 7 DESCPRIPTION & OPERATION OF AIRCRAFT AND SYSTEMS Table of Contents Paragraph Page THE AIRCRAFT ........................7-3 FUSELAGE ......................... 7-3 WINGS ..........................7-4 EMPENNAGE ........................7-4 FLIGHT CONTROL SYSTEM ....................
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  • Page 91: The Aircraft

    EXTRA 300LT is a light weight, robust, single piston-engined, two-seat aircraft with a fuselage structure in tig-welded steel-tube construction. The landing gear, wing, and tail are made of epoxy, reinforced with glass- and carbonfiber.

  • Page 92: Wings

    EMPENNAGE The EXTRA 300LT 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 93: Flight Control System

    FLIGHT CONTROL SYSTEM 7.5.1 PRIMARY CONTROL SYSTEM The EXTRA 300LT 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 94: Instrument Panel (Rear Cockpit)

    Section 7 Pilot´s Operating Handbook Description and Operation of Aircraft and Systems EXTRA 300LT 7.6.1 INSTRUMENT PANEL (REAR COCKPIT) Figure 1, Instrument Panel AUTO WARNING BACK BACK BOOST STROBE LEFT RIGHT LANDING BATTERY AVIONIC VOLTAGE PUMP LIGHTS LIGHTS PEDAL PEDAL LIGHT 7½...
  • Page 95 Pilot´s Operating Handbook Section 7 EXTRA 300LT Description and Operation of Aircraft and Systems Position Item Fig. 1 G-meter Volt/Amperemeter Airspeed indicator Magn. direction indicator Altimeter Manifold pressure / fuel flow Trim position indicator RPM Indicator Transponder Magneto selector switch and starter...

  • Page 96: Instrument Panel (Front Cockpit)

    Section 7 Pilot´s Operating Handbook Description and Operation of Aircraft and Systems EXTRA 300LT 7.6.2 INSTRUMENT PANEL (FRONT COCKPIT) Normally the instument panel in the front cockpit is only equipped with: - Airspeed indicator - Altimeter indicator. LANDING GEAR The landing gear is a composite construction with a multichamber fiberglass spring in a tail-wheel design.

  • Page 97: Power Plant

    Pilot´s Operating Handbook Section 7 EXTRA 300LT Description and Operation of Aircraft and Systems 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 98: Engine Installation

    Position up = WING TANK 7.10.9 EXHAUST SYSTEM A complete Gomolzig 6 in 1 System with integrated silencer is installed on the 300LT. 7.11 FUEL SYSTEM The fuel system (refer to Figure 3) consists of two separate, independent tanks: - Acro & center tank in the fuselage...
  • Page 99 Pilot´s Operating Handbook Section 7 EXTRA 300LT Description and Operation of Aircraft and Systems Figure 3, Fuel System Page Date: 6. April 2010 7 - 11...

  • Page 100: Electrical System

    Section 7 Pilot´s Operating Handbook Description and Operation of Aircraft and Systems EXTRA 300LT Wing Tank: The wing provides an integral fuel tank compartment on each side located behind the main spar with a capacity of 76 liters (20.1 US Gal.) each. Each side of the wing has a 2" diameter filler cap for gravity refueling.
  • Page 101 Pilot´s Operating Handbook Section 7 EXTRA 300LT Description and Operation of Aircraft and Systems Figure 4, Electrical System Page Date: 6. April 2010 7 - 13...

  • Page 102: Baggage Compartment

    Section 7 Pilot´s Operating Handbook Description and Operation of Aircraft and Systems EXTRA 300LT 7.14 BAGGAGE COMPARTMENT A baggage compartment is installed behind the pilot’s seat in the aft main fuselage cover. The compartment may be used only for low density items such as clothes. It is limited to a baggage weight of 10 kg (22 lbs).
  • Page 103 Pilot´s Operating Handbook Section 7 EXTRA 300LT Description and Operation of Aircraft and Systems Figure 5, Baggage Compartment Page Date: 6. April 2010 7 - 15...
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  • Page 105 Pilot´s Operating Handbook Section 8 EXTRA 300LT Handling, Servicing and Maintenance SECTION 8 HANDLING, SERVICING & MAINTENANCE TABLE OF CONTENTS Paragraph Page INTRODUCTION ........................8-3 AIRPLANE INSPECTION PERIODS ..................8-3 PILOT CONDUCTED PREVENTIVE MAINTENANCE ............8-3 ALTERATIONS OR REPAIR ....................8-3 SERVICING .........................
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  • Page 107: Introduction

    Pilot´s Operating Handbook Section 8 EXTRA 300LT 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 108: Servicing

    Section 8 Pilot´s Operating Handbook Handling, Servicing and Maintenance EXTRA 300LT 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 109 Pilot´s Operating Handbook Section 9 EXTRA 300LT Supplements SECTION 9 SUPPLEMENTS SUPPLEMENTS SECTION 9 SUPPLEMENTS Doc-No. EA-0D701.1 SUPPLEMENTS ........................3 Table of Contents Section Pages Supplements ........................4 p.  Steerable Tail Wheel ..................... 4 p.  Electric Pedal Adjustment ..................... 4 p.
  • Page 110 Section 9 Pilot´s Operating Handbook Supplements EXTRA 300LT  Reserved ......................... 0 p.  KANNAD 406 AF COMPACT/INTEGRA ELT ..............8 p. 9 - 2 Page Date: 22. April 2015...

  • Page 111: Supplements

    Notes The described systems and equipment are certified by the EASA for the EXTRA 300LT. 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.
  • Page 112 Section 9 Pilot´s Operating Handbook Supplements EXTRA 300LT Left blank intentionally 9 - 4 Page Date: 6. April 2010...

  • Page 113: Steerable Tail Wheel

    Section 901 Pilot´s Operating Handbook Steerable Tail Wheel EXTRA 300LT SECTION 901 STEERABLE TAIL WHEEL Table of Contents Paragraph Page 901.1 GENERAL ......................... 901-3 901.2 LIMITATION ........................901-3 901.3 EMERGENCY PROCEDURES ................... 901-3 901.4 NORMAL PROCEDURES ....................901-3 901.5 PERFORMANCE ......................901-3 901.6...
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  • Page 115 901.1 GENERAL To improve taxi and handling quality, the EXTRA 300LT 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 116 Section 901 Pilot´s Operating Handbook Steerable Tail Wheel EXTRA 300LT 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 117: Electric Pedal Adjustment

    Pilot´s Operating Handbook Section 902 EXTRA 300LT Electric Pedal Adjustment SECTION 902 ELECTRIC PEDAL ADJUSTMENT Table of Contents Paragraph Page 902.1 GENERAL ......................... 902-3 902.2 LIMITATIONS ........................902-3 902.3 EMERGENCY PROCEDURES ................... 902-3 902.4 NORMAL PROCEDURES ....................902-3 902.5 PERFORMANCE ......................902-3 902.6...
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  • Page 119 902.1 GENERAL To improve seat and control convenience, the EXTRA 300LT is equipped with an electric 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 120 Section 902 Pilot´s Operating Handbook Electric Pedal Adjustment EXTRA 300LT 902.7 DESCRIPTION OF THE SYSTEM The electrical pedal adjustment system consists of a foot rest and the rudder pedal itself, including brake pedal and brake cylinder. An S-shaped cable leader is attached to the rudder pedal, through which the control cable runs from the rudder actuator arm to the front cable attachment at the steel frame.

  • Page 121: Cabin Heating System

    Pilot´s Operating Handbook Section 903 EXTRA 300LT Cabin Heating System SECTION 903 CABIN HEATING SYSTEM Table of Contents Paragraph Page 903.1 GENERAL ......................... 903-3 903.2 LIMITATIONS ........................903-3 903.3 EMERGENCY PROCEDURES ................... 903-3 903.4 NORMAL PROCEDURES ....................903-3 903.5 PERFORMANCE ......................903-3 903.6...
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  • Page 123 903.1 GENERAL The 300LT can be equipped with a cabin heating system, which allows feeding the front and rear cockpit independently with warm air. The system uses fresh outside air, which is heated up by the engine exhaust muffler. The system is controlled by two handles in the rear cockpit.
  • Page 124 Section 903 Pilot´s Operating Handbook Cabin Heating System EXTRA 300LT 903.7 SYSTEM DESCRIPTION On the left front engine baffle a 3” air intake (1, figure 1) with screen is positioned. From there fresh air is routed through a 3" ducting (2) to the exhaust muffler heat shroud (3), where it is heated up.

  • Page 125: Accelerometer Tl-3424_Ext

    Pilot´s Operating Handbook Section 904 EXTRA 300LT Accelerometer TL-3424_EXT SECTION 904 ACCELEROMETER TL-3424_EXT Table of Contents Paragraph Page 904.1 GENERAL ......................... 904-3 904.2 LIMITATIONS ........................904-3 904.3 EMERGENCY PROCEDURES ................... 904-3 904.4 NORMAL PROCEDURES ....................904-3 904.5 PERFORMANCE ......................904-3 904.6...
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  • Page 127 ACCELEROMETER TL-3424_EXT 904.1 GENERAL The TL-3424_EXT accelerometer can be installed as an option in the 300LT. It is used in a special password protected configuration. This configuration helps the pilot to operate the aircraft within limits. In detail the TL-3424_EXT accelerometer allows: 1.
  • Page 128 Section 904 Pilot´s Operating Handbook Accelerometer TL-3424_EXT EXTRA 300LT 904.6 WEIGHT AND BALANCE Refer to the Equipment List in Section 6 of this Handbook. 904.7 DESCRIPTION The complete installation consists of: 1 TL-3424_EXT Accelerometer 2 G/V LIMITS WARNING LIGHT 3 RS-232c (D-SUB 9 pins [female]) The TL-3424_EXT is complete weight acceleration management.
  • Page 129 Pilot´s Operating Handbook Section 904 EXTRA 300LT Accelerometer TL-3424_EXT The TL-3424_EXT checks all measured values at two levels - for a warning and an alarm limit signalization. If the measured values are above the warning limit and below the alarm limit an intermitted sound is heard on the head set and the G/V LIMIT WARNING LIGHT flashes.
  • Page 130 Section 904 Pilot´s Operating Handbook Accelerometer TL-3424_EXT EXTRA 300LT SYMBOLS The following symbols are used in the TL-3424_EXT display. Display Symbol Meaning  recording to memory Recording paused Acceleration values indicated up/down arrows storing expected, release buttons when setting arrows vanish CONTROLLING THE INSTRUMENT VIA NAV-MENU There are black labels on the display.

  • Page 131: External Power

    Pilot´s Operating Handbook Section 905 EXTRA 300LT External Power SECTION 905 EXTERNAL POWER Table of Contents Paragraph Page 905.1 GENERAL ........................905-3 905.2 LIMITATIONS ........................905-3 905.3 EMERGENCY PROCEDURES ..................905-3 905.4 NORMAL PROCEDURES ....................905-3 905.5 PERFORMANCE ......................905-4 905.6...
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  • Page 133 EXTERNAL POWER 905.1 GENERAL The EXTRA 300LT can be equipped with an external power receptacle system. This system provides the capability to start the engine independent of the board battery and further allows feeding the electrical system for longer periods.
  • Page 134 Section 905 Pilot´s Operating Handbook External Power EXTRA 300LT CAUTION Pay attention to objects and persons in the propeller operating area! Hold the canopy tight! 8. Apply the brakes. 9. Engage starter. 10.When engine fires release the ignition switch back to "BOTH".

  • Page 135: Digital Rpm Indicator

    Pilot´s Operating Handbook Section 906 EXTRA 300LT Digital RPM Indicator SECTION 906 DIGITAL RPM INDICATOR Table of Contents Paragraph Page 906.1 GENERAL ......................... 906-3 906.2 LIMITATIONS ........................906-3 906.3 EMERGENCY PROCEDURES ................... 906-3 906.4 NORMAL PROCEDURES ....................906-3 906.5 PERFORMANCE ......................906-3 906.6...
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  • Page 137 Pilot´s Operating Handbook Section 906 EXTRA 300LT Digital RPM Indicator DIGITAL RPM INDICATOR 906.1 GENERAL The EXTRA 300LT is as standard equipped with the "P-1000" Digital rpm indicator 906.2 LIMITATIONS Not affected. 906.3 EMERGENCY PROCEDURES Not affected. 906.4 NORMAL PROCEDURES Not affected 906.5...
  • Page 138 Section 906 Pilot´s Operating Handbook Digital RPM Indicator EXTRA 300LT Magneto-Control RPM range RPM- restriction Status Display Operation placard: Hours Clear Trap Press-and-hold Operation placard: buttons Press-and-release 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 139 Pilot´s Operating Handbook Section 906 EXTRA 300LT Digital RPM Indicator OPERATION BUTTONS There are three panel buttons. Each button has two modes of operation. PRESS-AND-HOLD operation mode (press and hold for more than 2/3 of a second) This operation mode is placarded above each button.(Hours, Clear,Trap)
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  • Page 141 Pilot´s Operating Handbook Section 907 EXTRA 300LT Smoke System SECTION 907 SMOKE SYSTEM Table of Contents Paragraph Page 907.1 GENERAL ......................... 907-3 907.2 LIMITATIONS ........................907-3 907.3 EMERGENCY PROCEDURES ................... 907-3 907.4 NORMAL PROCEDURES ....................907-4 907.5 PERFORMANCE ......................907-5 907.6...
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  • Page 143: Smoke System

    EXTRA 300LT Smoke System SMOKE SYSTEM 907.1 GENERAL For performing at airshows, the EXTRA 300LT may optionally be equipped with a smoke system. 907.2 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 144: Normal Procedures

    Section 907 Pilot´s Operating Handbook Smoke System EXTRA 300LT FIRE IN FLIGHT 1. Switch "SMOKE ARM" CAUTION If the fire (after the smoke system is shut off) will not extinguish proceed as follows: 2. Mixture IDLE CUT OFF 3. Fuel selector valve OFF (Pull &...

  • Page 145: Performance

    Pilot´s Operating Handbook Section 907 EXTRA 300LT Smoke System CAUTION A shut-off failure of the refill process can be recognized by smoke oil spilling out of the vent line. In this case, turn off refill switch. The floating device switch in the main smoke oil tank has to be checked accordingly.
  • Page 146 Section 907 Pilot´s Operating Handbook Smoke System EXTRA 300LT throttle lever. For filling the smoke oil tanks the "SMOKE REFILL" switch needs to be ON. After the refill process is completed the "SMOKE REFILL" has to switched OFF. When both switches ("SMOKE ARM"...

  • Page 147: Handling, Servicing And Maintenance

    Pilot´s Operating Handbook Section 907 EXTRA 300LT Smoke System 907.8 HANDLING, SERVICING AND MAINTENANCE At every refilling: - Check automatic shut-off Additionally during the 100h Check for the DUAL PUMP SYSTEM - Check the system for leakage (lines, fittings, tanks)
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  • Page 149: Single Seat Canopy

    Pilot´s Operating Handbook Section 908 EXTRA 300LT Single Seat Canopy SECTION 908 SINGLE SEAT CANOPY Table of Contents Paragraph Page 908.1 GENERAL ......................... 908-3 908.2 LIMITATIONS ........................908-3 908.3 EMERGENCY PROCEDURES ................... 908-3 908.4 NORMAL PROCEDURES ....................908-3 908.5 PERFORMANCE ......................908-3 908.6...
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  • Page 151 Pilot´s Operating Handbook Section 908 EXTRA 300LT Single Seat Canopy SINGLE SEAT CANOPY 908.1 GENERAL For airshow performances the standard canopy can be replaced by a single seat canopy, which gives a gorgeous appearance. 908.2 LIMITATIONS With the single seat canopy installed the aircraft is limited to the categories NORMAL and ACRO I.
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  • Page 153: Artex Me-406 Elt

    Pilot´s Operating Handbook Section 909 EXTRA 300LT ARTEX ME-406 ELT SECTION 909 ARTEX ME-406 ELT Table of Contents Paragraph Page 909.1 GENERAL ......................... 909-3 909.2 LIMITATIONS ........................909-3 909.3 EMERGENCY PROCEDURES ................... 909-4 909.4 NORMAL PROCEDURES ....................909-4 909.5 PERFORMANCE ......................909-4 909.6...
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  • Page 155: General

    ARTEX ME-406 ELT 909.1 GENERAL To improve the passive security, the EXTRA 300LT 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 156: Emergency Procedures

    Section 909 Pilot´s Operating Handbook ARTEX ME-406 ELT EXTRA 300LT 909.3 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 157: System Description

    Pilot´s Operating Handbook Section 909 EXTRA 300LT ARTEX ME-406 ELT 909.7 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 158: Handling, Servicing And Maintenance

    Section 909 Pilot´s Operating Handbook ARTEX ME-406 ELT EXTRA 300LT 909.8 HANDLING, SERVICING AND MAINTENANCE 909.8.1 TRANSMITTER TEST ARTEX recommends that the ELT be tested every 1-2 months. Follow the steps outlined in the 909.8.2 SELF TEST paragraph. N O T E The self-test time is accumulated in a register on the battery pack.
  • Page 159 Pilot´s Operating Handbook Section 909 EXTRA 300LT 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 161: Nat Aa83-001 Intercom

    Section 910 Pilot´s Operating Handbook NAT AA83-001 Intercom EXTRA 300LT SECTION 910 NAT AA83-001 INTECOM Table of Contents Paragraph Page 910.1 GENERAL ........................910-3 910.1.1 Installation Adjustments ....................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 163 Section 910 Pilot´s Operating Handbook NAT AA83-001 Intercom EXTRA 300LT 910.1 GENERAL The AA83-001 is a stereo voice-activated intercom, providing full intercom capabilities for pilot and copilot. Further passenger features are not used in the configuration installed. The AA83-001 also provides transmit capability for pilot and co-pilot to a single COM radio or audio selector panel.
  • Page 164 Section 910 Pilot´s Operating Handbook NAT AA83-001 Intercom EXTRA 300LT 910.3 EMERGENCY PROCEDURES Not applicable 910.4 NORMAL PROCEDURES Not applicable 910.5 PERFORMANCE Not applicable 910.6 WEIGHT AND BALANCE Refer to the Equipment List in Section 6 of this Handbook. 910.7 SYSTEM DESCRIPTION 910.7.1 CONTROLS AND INDICATORS...
  • Page 165 Section 910 Pilot´s Operating Handbook NAT AA83-001 Intercom EXTRA 300LT ICS VOL/PILOT VOX This control is a fluted concentric rubber knob on the top of the panel. The inner (front) knob is the ICS VOL control, which is used to set intercom volume. It is at minimum volume when fully counterclockwise (ccw).
  • Page 166 Section 910 Pilot´s Operating Handbook NAT AA83-001 Intercom EXTRA 300LT 910.7.2 OPERATION VOX OPERATION The VOX control is used to set the level of audio required to activate the microphones. The AA83-001 provides three modes of intercom operation, selected by the position of the VOX control.
  • Page 167 Section 910 Pilot´s Operating Handbook NAT AA83-001 Intercom EXTRA 300LT The copilot will be unable to monitor any transceiver activity, although he retains full ICS and music functions. This mode is ‚fail-passive‘ meaning that it requires no power to operate and is the same mode the box goes into automatically when power is lost to the AA83-001.
  • Page 168 Section 910 Pilot´s Operating Handbook NAT AA83-001 Intercom EXTRA 300LT The relative volume of the music can be changed from the panel by the knob marked with a musical note. Below is a simple chart to aid in understanding audio switching in the NORMAL Operation mode.

  • Page 169: Becker Atc 4401 Transponder

    Section 911 Pilot´s Operating Handbook BECKER ATC 4401 Transponder EXTRA 300LT SECTION 911 BECKER ATC 4401 TRANSPONDER Table of Contents Paragraph Page 911.1 GENERAL ......................... 911-3 911.1.1 Controls and indicators ..................... 911-4 911.1.2 Switching on the unit (pre-flight check) ................911-4 911.1.3...
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  • Page 171: General

    Section 911 Pilot´s Operating Handbook BECKER ATC 4401 Transponder EXTRA 300LT 911.1 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 172: Controls And Indicators

    Section 911 Pilot´s Operating Handbook BECKER ATC 4401 Transponder EXTRA 300LT 911.1.1 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 173: Squawk Selection

    Section 911 Pilot´s Operating Handbook BECKER ATC 4401 Transponder EXTRA 300LT 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 174 Section 911 Pilot´s Operating Handbook BECKER ATC 4401 Transponder EXTRA 300LT 1 Storing a new VFR code: a Set the code to be stored in accordance with section B. b Press store push-button STO (J), the set code then flashes.

  • Page 175: Flight Operation In Mode A (Transponder Reply Code Only)

    Pilot´s Operating Handbook BECKER ATC 4401 Transponder EXTRA 300LT 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 176: Configuration Mode

    Section 911 Pilot´s Operating Handbook BECKER ATC 4401 Transponder EXTRA 300LT 2 A permanent test runs in the background of the transponder operation. The built-in FPGA organizes the required resources for this. The transmitter recognizes a missmatching or own abnormal behavior and delivers an alarm signal to the FPGA.

  • Page 177: Becker Bxp 6401 Transponder

    Pilot´s Operating Handbook Section 912 EXTRA 300LT BECKER BXP 6401 Transponder SECTION 912 BECKER ATC 6401 TRANSPONDER Table of Contents Paragraph Page 912.1 GENERAL ......................... 912-3 912.1.1 Controls and Indicators ..................... 912-4 912.1.2 Switching on the Unit (pre-flight check) ................912-4 912.1.3...
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  • Page 179: General

    Pilot´s Operating Handbook Section 912 EXTRA 300LT BECKER BXP 6401 Transponder 912.1 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 180: Controls And Indicators

    Section 912 Pilot´s Operating Handbook BECKER BXP 6401 Transponder EXTRA 300LT 912.1.1 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 181: Display

    Pilot´s Operating Handbook Section 912 EXTRA 300LT 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 182: Squawk Ident

    Section 912 Pilot´s Operating Handbook BECKER BXP 6401 Transponder EXTRA 300LT 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 183: Selection Mode

    Pilot´s Operating Handbook Section 912 EXTRA 300LT 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 184 Section 912 Pilot´s Operating Handbook BECKER BXP 6401 Transponder EXTRA 300LT 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 185: Flight Operation In Mode A/C/S (Reply Code And Altitude Code)

    Pilot´s Operating Handbook Section 912 EXTRA 300LT 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 186: Vfr Code Activation

    Section 912 Pilot´s Operating Handbook BECKER BXP 6401 Transponder EXTRA 300LT 912.1.9 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 187: Garmin Gtx 327 Transponder

    Pilot´s Operating Handbook Section 913 EXTRA 300LT GARMIN GTX 327 Transponder SECTION 913 GARMIN GTX 327 TRANSPONDER Table of Contents Paragraph Page 913.1 GENERAL ......................... 913-3 913.1.1 Mode Selection Keys ......................913-3 913.1.2 Code Selection ......................... 913-4 913.1.3 Keys for other GTX 327 Functions ..................913-4 913.2...
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  • Page 189 Pilot´s Operating Handbook Section 913 EXTRA 300LT GARMIN GTX 327 Transponder 913.1 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 190 Pilot´s Operating Handbook GARMIN GTX 327Transponder EXTRA 300LT Powers on the transponder in Mode A and Mode C. At power on the last active identification code will be selected. In ALT mode, the transponder replies to identification and altitude interrogations, as indicated by the Reply Symbol.
  • Page 191 Pilot´s Operating Handbook Section 913 EXTRA 300LT GARMIN GTX 327 Transponder Sets the transponder code to the pre-programmed VFR code selected in the Configuration Mode. Pressing the VFR key again will restore the previous identification code. START/STOP Starts and stops the Count Up and Count Down timers.
  • Page 192 Section 913 Pilot´s Operating Handbook GARMIN GTX 327Transponder EXTRA 300LT 913.2 LIMITATIONS Not applicable. 913.3 EMERGENCY PROCEDURES 913.3.1 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 193: Garmin Gtx 328 Transponder

    Pilot´s Operating Handbook Section 914 EXTRA 300LT GARMIN GTX 328 Transponder SECTION 914 GARMIN GTX 328 TRANSPONDER Table of Contents Paragraph Page 914.1 GENERAL ......................... 914-3 914.1.1 Mode Selection Keys ......................914-4 914.1.2 Code Selection ......................... 914-4 914.1.3 Keys for other GTX 328 Functions ..................914-5 914.1.4...
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  • Page 195: General

    Pilot´s Operating Handbook Section 914 EXTRA 300LT GARMIN GTX 328 Transponder 914.1 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 196: Mode Selection Keys

    Section 914 Pilot´s Operating Handbook GARMIN GTX 328 Transponder EXTRA 300LT 914.1.1 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 197: Keys For Other Gtx 328 Functions

    Pilot´s Operating Handbook Section 914 EXTRA 300LT 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! 914.1.3 KEYS FOR OTHER GTX 328 FUNCTIONS...

  • Page 198: Configuration Mode

    Section 914 Pilot´s Operating Handbook GARMIN GTX 328 Transponder EXTRA 300LT '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 199: Limitations

    Pilot´s Operating Handbook Section 914 EXTRA 300LT GARMIN GTX 328 Transponder 914.2 LIMITATIONS Not applicable. 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).
  • Page 200 Section 914 Pilot´s Operating Handbook GARMIN GTX 328 Transponder EXTRA 300LT Left blank intentionally 914 - 8 Page Date: 6. April 2010...

  • Page 201: Garmin Gtx 330 Transponder

    Pilot´s Operating Handbook Section 915 EXTRA 300LT GARMIN GTX 330 Transponder SECTION 915 GARMIN GTX 330 TRANSPONDER Table of Contents Paragraph Page 915.1 GENERAL ......................... 915-3 915.1.1 Mode Selection Keys ......................915-4 915.1.2 Code Selection ......................... 915-4 915.1.3 Keys for other GTX 330 Functions ..................915-5 915.1.4...
  • Page 202 Section 915 Pilot´s Operating Handbook GARMIN GTX 330 Transponder EXTRA 300LT Left blank intentionally 915 - 2 Page Date: 6. April 2010...

  • Page 203: General

    Pilot´s Operating Handbook Section 915 EXTRA 300LT 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 204: Mode Selection Keys

    Section 915 Pilot´s Operating Handbook GARMIN GTX 330 Transponder EXTRA 300LT 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 205: Keys For Other Gtx 330 Functions

    Pilot´s Operating Handbook Section 915 EXTRA 300LT 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 206: Configuration Mode

    Section 915 Pilot´s Operating Handbook GARMIN GTX 330 Transponder EXTRA 300LT '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 207: Limitations

    Pilot´s Operating Handbook Section 915 EXTRA 300LT 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 209: Garmin Gnc 420W/Gns 430W

    Pilot´s Operating Handbook Section 916 EXTRA 300LT GARMIN GNC 420W/GNS 430W SECTION 916 GARMIN GNC 420W/GNS 430W Table of Contents Paragraph Page 916.1 GENERAL ......................... 916-3 916.2 LIMITATIONS ........................916-3 916.2.1 Placards ........................... 916-4 916.3 EMERGENCY/ABNORMAL PROCEDURES ..............916-4 916.3.1 Emergency Procedures ....................
  • Page 210 Section 916 Pilot´s Operating Handbook GARMIN GNC 420W/GNS 430W EXTRA 300LT Left blank intentionally 916 - 2 Page Date: 6. April 2010...

  • Page 211: General

    Pilot´s Operating Handbook Section 916 EXTRA 300LT GARMIN GNC 420W/GNS 430W 916.1 GENERAL The Garmin GNC 420W/GNS 430W 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.

  • Page 212: Placards

    Section 916 Pilot´s Operating Handbook GARMIN GNC 420W/GNS 430W EXTRA 300LT 916.2.1 PLACARDS GARMIN GPS (In the clear view of the pilot) limited to VFR use only (Next to the GNC 420W/GNS 430W circuit breaker) 916.3 EMERGENCY/ABNORMAL PROCEDURES 916.3.1 EMERGENCY PROCEDURES Not affected.

  • Page 213: Normal Procedures

    Pilot´s Operating Handbook Section 916 EXTRA 300LT GARMIN GNC 420W/GNS 430W 3. Turn the small right knob to display a window showing up to nine nearby airports. 4. Continue turning the small right knob to scroll through the list and highlight the desired airport.
  • Page 214 Pilot´s Operating Handbook GARMIN GNC 420W/GNS 430W EXTRA 300LT The small left knob (COM/VLOC) is used to tune the kilohertz (kHz) value (to the right of the decimal point) of the standby frequency for the communications transceiver (COM) or the VLOC receiver, whichever is currently selected by the tuning cursor.

  • Page 215: Default Nav Page

    Pilot´s Operating Handbook Section 916 EXTRA 300LT GARMIN GNC 420W/GNS 430W The flight plan key (FPL) allows you to create, edit, activate and invert flight plans, as well as access approaches, departures and arrivals. A closest point to flight plan feature is also available from the flight plan key.
  • Page 216 Section 916 Pilot´s Operating Handbook GARMIN GNC 420W/GNS 430W EXTRA 300LT Left blank intentionally 916 - 8 Page Date: 6. April 2010...
  • Page 217 Pilot´s Operating Handbook Section 917 EXTRA 300LT ASPEN EFD1000/500 System SECTION 917 ASPEN EFD1000/500 Table of Contents Paragraph Page 917.1 GENERAL ......................... 917-3 917.1.1 Equipment Configuration ....................917-4 917.2 LIMITATIONS ........................917-4 917.2.1 Placards and Decals ......................917-4 917.3 EMERGENCY PROCEDURES ................... 917-6 917.4...

  • Page 218: Aspen Efd1000/500 System

    Section 917 Pilot´s Operating Handbook ASPEN EFD1000/500 System EXTRA 300LT Left blank intentionally 917 - 2 Page Date: 6. April 2010...

  • Page 219: General

    The standard internal battery in the EFD1000 or EFD500 is capable of providing 30 or more minutes of operation at typical cockpit temperatures if aircraft power to the system fails. An Emergency Backup Battery is not installed. In the EXTRA 300LT the EFD1000/500 system is used as a secondary (back-up) instrument system. CAUTION Due to the capabilities of the aircraft - especially the extreme agility with high angular rates - the EFD1000/500 System cannot be operated reliably in acrobatics.

  • Page 220: Equipment Configuration

    Additional information can be found in these documents as well. 917.1.1 EQUIPMENT CONFIGURATION The table below shows the various possible configurations of Aspen equipment for the 300LT. Refer to the Equipment List in Section 6 to verify, which configuration is actually installed in your aircraft.
  • Page 221 Pilot´s Operating Handbook Section 917 EXTRA 300LT ASPEN EFD1000/500 System Figure 1, Equipment Configuration Page Date: 6. April 2010 917 - 5...

  • Page 222: Emergency Procedures

    Section 917 Pilot´s Operating Handbook ASPEN EFD1000/500 System EXTRA 300LT 917.3 EMERGENCY PROCEDURES Not affected due to the use as a secondary instrument. 917.4 NORMAL PROCEDURES Not affected due to the use as a secondary instrument. 917.5 PERFORMANCE Not affected.

  • Page 223: Databases (Efd1000/500 Mfd Only)

    GPS groundspeed is greater than 50 kts (58 mph). N O T E The EXTRA 300LT doesn’t feature a pitot heating system. So the „CHECK PITOT HEAT“ amber annunciation shall be taken as a note, that a failure of the pitot/static system has been detected.

  • Page 224: Rsm Gps Usage

    Section 917 Pilot´s Operating Handbook ASPEN EFD1000/500 System EXTRA 300LT Database Includes Update Database Limitations Type Cycle Provider High resolution terrain data for Americas, Delivered Jeppesen Terrain International, or Worldwide geographic regions. with unit, mail order Terrain depiction is limited to the region between 65...

  • Page 225: Geographic Reservation

    Pilot´s Operating Handbook Section 917 EXTRA 300LT ASPEN EFD1000/500 System Battery operation should be expected any time the aircraft charging system is unable to maintain a voltage at the EFD of 12.3 V. Under these circumstances, should the aircraft dispatch the EFD will transition to battery shortly after reaching flying speed.
  • Page 226 Pilot´s Operating Handbook ASPEN EFD1000/500 System EXTRA 300LT The EFD1000/500 MFD display of terrain and obstacle information is advisory only. In addition, the system does not provide terrain or obstacle alerts. Not all obstacles within a given region will be charted.

  • Page 227: Evolution Synthetic Vision (Optional)

    Pilot´s Operating Handbook Section 917 EXTRA 300LT ASPEN EFD1000/500 System 917.7.8 EVOLUTION SYNTHETIC VISION (OPTIONAL) N O T E Navigation or maneuvering based solely on the EFD1000 or MFD500 Synthetic Vision background display and associated Terrain Warning System (TWS) is not authorized. The Pilot in command has the responsibility to use accepted visual procedures to avoid terrain and other obstacles.

  • Page 228: Aspen Pfd As Encoded Altitude Source

    Pilot´s Operating Handbook ASPEN EFD1000/500 System EXTRA 300LT if the aircraft continues on the collision path. In addition, the terrain is colored based on the aircraft proximity to the terrain; yellow when the aircraft is within 500 feet vertically of the terrain or obstacle, and red when the aircraft is within 100 feet vertically.
  • Page 229 Pilot´s Operating Handbook Section 918 EXTRA 300LT EI MVP-50P SECTION 918 EI MVP-50P Table of Contents Paragraph Page 918.1 GENERAL ......................... 918-3 918.2 LIMITATIONS ........................918-3 918.2.1 Instrument markings ......................918-3 918.3 EMERGENCY PROCEDURES ................... 918-4 918.4 NORMAL PROCEDURES ....................918-4 918.5...
  • Page 230 Section 918 Pilot´s Operating Handbook EI MVP-50P EXTRA 300LT Left blank intentionally 918 - 2 Page Date: 6. April 2010...

  • Page 231: General

    The following features are not available in the configuration installed in the EXTRA 300LT: - External dimmer potentiometer - External warning and caution light...

  • Page 232: Emergency Procedures

    Section 918 Pilot´s Operating Handbook EI MVP-50P EXTRA 300LT 918.3 EMERGENCY PROCEDURES Not affected. 918.4 NORMAL PROCEDURES Magneto Check - Check the magnetos at 1800 RPM. Allowed drop is 175 RPM (max. difference 50 RPM). - Check Alternator Output. - Move also the propeller control through its complete range to check operation and return to full "HIGH RPM"...
  • Page 233 Pilot´s Operating Handbook Section 918 EXTRA 300LT EI MVP-50P 918.7 SYSTEM DESCRIPTION The MVP-50P Main Engine Screen displays the primary engine and aircraft instruments. This screen is displayed on power-up and is the screen that should be monitored for most of the flight.

  • Page 234: Instrument Panel Layout

    Section 918 Pilot´s Operating Handbook EI MVP-50P EXTRA 300LT 918.7.1 INSTRUMENT PANEL LAYOUT Generally an alternate panel is used to carry the MVP-50. For that reason the circuit breaker layout also changes as shown in Figure 2. Figure 2, Alternate Panel Layout...

  • Page 235: Airplanes Registered In Brazil And Operating Under The Agência Nacional De Aviação Civil Requirements

    Pilot´s Operating Handbook Section 921 EXTRA 300LT AIRPLANES REGISTERED IN BRAZIL SECTION 921 AIRPLANES REGISTERED IN BRAZIL AND OPERATING UNDER THE AGÊNCIA NACIONAL DE AVIAÇÃO CIVIL REQUIREMENTS Table of Contents Paragraph Page SECTION 921 921.1 GENERAL ......................... 921-3 921.2 LIMITATIONS ........................921-4 921.2.1...
  • Page 236 Section 921 Pilot´s Operating Handbook AIRPLANES REGISTERED IN BRAZIL EXTRA 300LT Left blank intentionally 921 - 2 Page Date: 31. May 2012...
  • Page 237 Pilot´s Operating Handbook Section 921 EXTRA 300LT AIRPLANES REGISTERED IN BRAZIL 921.1 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 238 Section 921 Pilot´s Operating Handbook AIRPLANES REGISTERED IN BRAZIL EXTRA 300LT 921.2 LIMITATIONS 921.2.1 KINDS OF OPERATIONAL LIMITS Operation is limited to VFR-day. Use of GPS is prohibited as primary means for navigation. Optional GPS is approved as supplemental means for navigation only.
  • Page 239 Pilot´s Operating Handbook Section 921 EXTRA 300LT AIRPLANES REGISTERED IN BRAZIL 921.8 HANDLING, SERVICING AND MAINTENANCE Not affected. Page Date: 31. May 2012 921- 5...
  • Page 240 Section 921 Pilot´s Operating Handbook AIRPLANES REGISTERED IN BRAZIL EXTRA 300LT Left blank intentionally 921 - 6 Page Date: 31. May 2012...

  • Page 241: Garmin Gtn 635/650/750

    Pilot´s Operating Handbook Section 922 EXTRA 300LT GARMIN GTN 635/650/750 SECTION 922 GARMIN GTN 635/650/750 Table of Contents Paragraph Page 922.1 GENERAL ......................... 922-3 922.2 LIMITATIONS ........................922-3 922.2.1 Placards ........................... 922-5 922.2.2 SD Card ..........................922-5 922.2.3 Terrain ..........................922-5 922.2.4...
  • Page 242 Section 922 Pilot´s Operating Handbook GARMIN GTN 635/650/750 EXTRA 300LT Left blank intentionally 922 - 2 Page Date: 6. November 2012...

  • Page 243: General

    Pilot´s Operating Handbook Section 922 EXTRA 300LT GARMIN GTN 635/650/750 922.1 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 244 Section 922 Pilot´s Operating Handbook GARMIN GTN 635/650/750 EXTRA 300LT 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 245: Placards

    Pilot´s Operating Handbook Section 922 EXTRA 300LT GARMIN GTN 635/650/750 922.2.1 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 246: Glove Use

    Section 922 Pilot´s Operating Handbook GARMIN GTN 635/650/750 EXTRA 300LT 922.2.6 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 247: Normal Procedures

    Pilot´s Operating Handbook Section 922 EXTRA 300LT 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 248: Weight & Center Of Gravity

    Section 922 Pilot´s Operating Handbook GARMIN GTN 635/650/750 EXTRA 300LT 922.6 WEIGHT & CENTER OF GRAVITY Refer to the equipment list in Section 6 of this Handbook. 922.7 SYSTEM DESCRIPTION 922.7.1 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 249: Secure Digital Card

    Pilot´s Operating Handbook Section 922 EXTRA 300LT GARMIN GTN 635/650/750 Figure 3, GTN 6xx XPDR Operation 922.7.2 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 250: Remote Transponder Operation

    Section 922 Pilot´s Operating Handbook GARMIN GTN 635/650/750 EXTRA 300LT Figure 4, GTN 750 XPDR Operation 922.7.4 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 trnasponder operation page. See figures 3 and 4 for the GTN 6xx and the GTN 750 respectively.
  • Page 251 Pilot´s Operating Handbook Section 922 EXTRA 300LT 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 252: Remote Audio Panel Operation (Gtn 750 Only)

    Section 922 Pilot´s Operating Handbook GARMIN GTN 635/650/750 EXTRA 300LT 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 253 Pilot´s Operating Handbook Section 922 EXTRA 300LT GARMIN GTN 635/650/750 3. The selected Mic will be shown in the MIC window. MONITOR 1. Monitor is automatically selected for the associated Com Mic Radio. 2. Touch the Mon key to toggle between the automatically selected monitored channel (selected Mic) and the other available channels.

  • Page 254: Powering Up The Gtn 635/650/750

    Section 922 Pilot´s Operating Handbook GARMIN GTN 635/650/750 EXTRA 300LT 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 255: Map Page

    Pilot´s Operating Handbook Section 922 EXTRA 300LT GARMIN GTN 635/650/750 To acknowledge or advance to the next page, touch Continue. 922.7.7 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 256 Section 922 Pilot´s Operating Handbook GARMIN GTN 635/650/750 EXTRA 300LT Left blank intentionally 922 - 16 Page Date: 6. November 2012...
  • Page 257 Pilot´s Operating Handbook Section 924 EXTRA 300LT KANNAD AF 406 ELT SECTION 924 KANNAD 406 AF COMPACT/INTEGRA ELT Table of Contents Paragraph Page 924.1 GENERAL ......................... 924-3 924.2 LIMITATIONS ........................924-3 924.3 EMERGENCY PROCEDURES ................... 924-4 924.4 NORMAL PROCEDURES ....................924-4 924.5...
  • Page 258 Section 924 Pilot´s Operating Handbook KANNAD AF 406 ELT EXTRA 300LT Left blank intentionally 924 - 2 Page Date: 22. April 2015...

  • Page 259: General

    924.1 GENERAL To improve the passive security, the EXTRA 300LT can be equipped with an optional Emergency Locator Transmitter KANNAD AF 406 COMPACT or INTEGRA ELT. In the event of a crash, the AF 406 activates automatically (automatic fixed „AF“ configuration), and transmits the standard swept tone on 121.5 MHz lasting until the battery is depleted.

  • Page 260: Emergency Procedures

    Section 924 Pilot´s Operating Handbook KANNAD AF 406 ELT EXTRA 300LT 924.3 EMERGENCY PROCEDURES • In case of a forced landing switch the remote switch in the rear instrument 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 261: Performance

    Pilot´s Operating Handbook Section 924 EXTRA 300LT KANNAD AF 406 ELT • Switch from position „OFF“ to position „ARM“ or press RESET & TEST on the Remote Control Panel (ensure that the ELT switch is in position „ARM“). Close to the end of the self-test a short (3-4 sweeps) 121.5 transmission is made.

  • Page 262: Switch Operation

    Section 924 Pilot´s Operating Handbook KANNAD AF 406 ELT EXTRA 300LT 924.7.1 SWITCH OPERATION In a crash, an acceleration activated crash sensor (G-switch) turns the ELT ‘on’ automatically. Activation is also accomplished by switching the cockpit mounted remote switch or the switch on the ELT to the 'ON' position.

  • Page 263: Battery Replacement

    Pilot´s Operating Handbook Section 924 EXTRA 300LT KANNAD AF 406 ELT 924.8.2 BATTERY REPLACEMENT Carried out by an accredited PART 145 or FAR 145 (or equivalent) maintenance station. BATTERY REPLACEMENT REQUIREMENTS Battery replacement is mandatory: • after more than 1 hour of real transmission (cumulated duration);...
  • Page 264 Section 924 Pilot´s Operating Handbook KANNAD AF 406 ELT EXTRA 300LT Left blank intentionally 924 - 8 Page Date: 22. April 2015...

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