TITLE PAGE INFORMATION MANUAL EXTRA 330LX MANUFACTURER EXTRA Flugzeugproduktions- und Vertriebs- GmbH Flugplatz Dinslaken 46569 Hünxe, Federal Republic of Germany WARNING 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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Pilot´s Operating Handbook EXTRA 330LX SECTION 0 LOG OF REVISIONS Dates of issue for original and revised pages: Date and sign of approval: Original ........................................ 4. February 2011 EASA MAJOR CHANGE APPROVAL 10034512 Date of Approval .................................. 8. April 2011 Revision No. 1 ................................... 31. May 2012 Approved under the authority of DOA N° EASA.21J.073 (ANAC Validation Process; EASA Project N° 0010017605) Date of Approval ..........
Pilot´s Operating Handbook EXTRA 330LX LOG OF EFFECTIVE PAGES Page Date Title .................................. 4. February 2011 i thru ii ......................... 29. September 2014 iii thru vi ............................ 4. February 2011 1-1 thru 1-4 ...................... 4. February 2011 1-5 .............................. 29. September 2014 1-6 thru 1-8 ...................... 4. February 2011 2-1 .................................. 6. November 2012 2-2 thru 2-4 ...................... 4.
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Pilot´s Operating Handbook EXTRA 330LX 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 Flugzeugproduktions- und Vertriebs- GmbH. THIS MANUAL IS FURNISHED TO THE CIVIL AVIATION AUTHORITIES AS A PART OF THE CERTIFICATION MATERIAL FOR THIS MODEL. NOTES This Flight Manual applies only to the aircraft whose nationality and registration marks are noted on the title page.
Pilot´s Operating Handbook EXTRA 330LX 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. NOTE => An operating procedures, technique, etc., which is considered essential to emphasize.
Pilot´s Operating Handbook EXTRA 330LX MAIN TABLE OF CONTENTS Section vi Page 1 GENERAL 1-1 2 LIMITATIONS 2-1 3 EMERGENCY PROCEDURES 3-1 4 NORMAL PROCEDURES 4-1 5 PERFORMANCE 5-1 6 WEIGHT & BALANCE/EQUIPMENT LIST 6-1 7 AIRPLANE & SYSTEMS DESCRIPTIONS 7-1 8 AIRPLANE HANDLING, SERVICE & MAINTENANCE 8-1 9 SUPPLEMENTS 9-1 Page Date: 4.
Pilot´s Operating Handbook EXTRA 330LX Section 1 General SECTION 1 GENERAL Table of Contents Paragraph Page 1.0 DESCRIPTION .................................................................................................................... 1-3 1.1 SPECIFICATION OF CLASS ............................................................................................... 1-3 1.2 MANUFACTURER ...............................................................................................................
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Pilot´s Operating Handbook EXTRA 330LX 1.0 Section 1 General DESCRIPTION The fuselage of the EXTRA 330LX 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. 1.1 SPECIFICATION OF CLASS The aircraft is certified in normal and acrobatic category. 1.
Section 1 General 1.3.2 Pilot´s Operating Handbook EXTRA 330LX MAIN DATA - Length - Height - Span - Wheel base - Wheel track 1.3.3 WING - Wing span - Wing-area - Airfoil Root: - Airfoil Tip: - Chord Root: - Chord Tip: - MAC - Aileron area (without horn balance) - Aileron area (with horn balance) - Aileron deflection 1.3.4 1.55 m² (16.68 ft²) Wortmann FX 71-L-150/30 RUDDER - Area (without horn balance) - Area (with horn balance) - Rudder deflection 1-4 0.768 m² (8.27 ft²) up 25°, toler.
Pilot´s Operating Handbook EXTRA 330LX 1.4 Section 1 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 1.5 PROPELLER Manufacturer: MT-Propeller Entwicklung GmbH, Federal Republic of Germany. Type: MTV-9-B-C/C 198-25 3-blade constant speed. Type: MTV-14-B-C/C 190-130 4-blade constant speed. 1.5.
Section 1 General 1.7 Pilot´s Operating Handbook EXTRA 330LX OIL (Cont.) Average ambient air temperature Mil-L6082 grades Mil-22851 ashless dispersant grades - 18°C til 21°C (0°F - 70°F) SAE 30 SAE 30,40 or 20W40 - 18°C til 32°C (0°F - 90°F) SAE 20W50 SAE 20W50 or 15W50 < -12°C (10°F) SAE 20 SAE 30 or 20W30 (single or multi - viscosity aviation grade oils see latest issue of Textron Lyc. S.I. No. 1014) 1.8 1.9 LOADING Wing loading @ MTOW Normal/Acrobatic III Acrobatic II Acrobatic I 88.
Pilot´s Operating Handbook EXTRA 330LX Section 1 General Meteorological terminology 1.10 ISA International standard atmospheric condition OAT Outside air temperature SECONDARY TERMINOLOGY fpm Feet/minute ft Feet = 0.3048 m in inch = 2.54 cm m Meter L Litres US.gal US (liquid) gallon = 3.79 litres US.qt US (liquid) quart = 0.946 litres hp Horse power (english) h Hour kts Knots (nm/h) = 1.852 kilometer per hour km/h Kilometer per hour lbs English pound = 0.
Section 1 General 1.11 1-8 Pilot´s Operating Handbook EXTRA 330LX CONVERSION TABLE Page Date: 4.
Pilot´s Operating Handbook EXTRA 330LX Section 2 Limitations SECTION 2 LIMITATIONS Table of Contents Paragraph Page 2.1 GENERAL ............................................................................................................................ 2-3 2.2 AIR SPEED (IAS) ................................................................................................................ 2-3 2.3 CROSS-WIND COMPONENT ...................................................................................
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Pilot´s Operating Handbook EXTRA 330LX 2.1 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. Observance of these operating limitations is required by national aviation regulations.
Section 2 Limitations 2.4.2 Pilot´s Operating Handbook EXTRA 330LX ENGINE LIMITATIONS a) Maximum Rotational Speed Take-Off and Maximum Continuous: 2700 rpm* N O T E* Applicable RPM limitations approved for the MTV-9-B-C/C 198-25 propeller must be observed. Refer to Section 2.5. b) Oil-temperature - Maximum 118°C (245°F) c) Oil capacity - Maximum sump capacity: - Minimum sump capacity: 15.13 L 8.51 L (16 US.qt) ( 9 US.
Pilot´s Operating Handbook EXTRA 330LX 2.5 Section 2 Limitations PROPELLER MT-Propeller Entwicklung GmbH, Federal Republic of Germany a) Standard: MTV-9-B-C/C198-25, 3-blade constant speed b) Alternative: MTV-14-B-C/C190-130, 4-blade constant speed Maximum rotational speed - Take-Off and Maximum Continuous: 2600 rpm* N O T E* RPM limitation due to compliance with applicable noise protection requirements (ICAO Annex 16 and FAR 36).
Section 2 Limitations Pilot´s Operating Handbook EXTRA 330LX 2.8 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. The structure is designed for full aileron control input up to 185 KIAS (343 km/h) in combination with 2/3 of the applicable max.
Pilot´s Operating Handbook EXTRA 330LX Section 2 Limitations Maneuvers Recommended entry speeds IAS Symbol Remarks min knots (km/h) max knots (km/h) VS VNE 80 (148) VNE 90° up VA VNE 45° diving VS VNE reduce throttle 90° diving VS VNE reduce throttle 1/4 Loop climb.
Section 2 Limitations 2.10 Pilot´s Operating Handbook EXTRA 330LX 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. The rear cockpit is equipped with a complete set of airplane controls and instruments. 2.11 KINDS OF OPERATION LIMITS Only VFR flights at day are allowed.
Pilot´s Operating Handbook EXTRA 330LX 2.14.2 Section 2 Limitations OPERATING PLACARDS VA= 154 KTS (ACRO) VA= 138 KTS (NORMAL) or VA= 285 km/h (ACRO) VA= 256 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.
Section 2 Limitations Pilot´s Operating Handbook EXTRA 330LX FUEL SELECTOR VALVE WING TANKS usable 120 L (31.7 US GAL) CENTER (ACRO) TANK usable 67 L (17.7 US GAL) OFF (in both cockpits next to the fuel selector) WING TANK MUST BE EMPTY FOR ACROBATICS. USABLE FUEL 120L (31.7 US GAL). (On the rear instrument panel beneath wing tank fuel capacity indicator) CENTER TANK INDICATION SHOWS "ZERO" IN LEVEL FLIGHT BELOW 9 L (2.4 US GAL). UNUSABLE FUEL 2 L (0.
Pilot´s Operating Handbook EXTRA 330LX Section 2 Limitations PROP LOW RPM HIGH RPM (On RPM control in the rear cockpit) MIXTURE LEAN RICH (On mixture control in the rear cockpit) THROTTLE CLOSE OPEN (Near throttle control in both cockpits) CANOPY LOCK LOCK UNLOCK (near canopy locking handles of each cockpit) VENT OPEN (Near the eyeball-type adjustable vents) CAUTION Particular caution must be exercised when performing maneuvers at speeds above VA [154 KIAS (285 km/h)].
Section 2 Limitations Pilot´s Operating Handbook EXTRA 330LX 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) USE STRAIGHT MINERAL OIL FOR A MINIMUM OF 50 HOURS (On the inside of the separate hatch / upper cowling) 3.
Pilot´s Operating Handbook EXTRA 330LX Section 2 Limitations Approved acrobatic maneuvers and recommended entry airspeeds Maneuvers Airspeeds Maneuvers Airspeeds min KIAS max KIAS min KIAS max KIAS Horizontal Line VS VNE Aileron roll 80 185 45°climbing 80 VNE Snap roll 80 13 90° up VA VNE "Tail-slide" 100 190 45° diving VS VNE Spin VS ---- 90° diving VS VNE Inverted spin VS ---- 1/4 Loop climb.
Section 2 Limitations 2.14.
Pilot´s Operating Handbook EXTRA 330LX Section 2 Limitations MANIFOLD PRESSURE INDICATOR green range 2.15 10 " Hg - 30 " Hg KINDS OF OPERATION EQUIPMENT LIST The aircraft may be operated in day VFR when the appropriate equipment is installed and operable. No Pilot's Operating Handbook Supplement grants approval for IFR operation. Flight in icing conditions is prohibited.
Section 2 Limitations Pilot´s Operating Handbook EXTRA 330LX NORMAL ACROBATIC 1 seat 2 seats ENGINE INDICATION 1. RPM indicator 4. Manifold pressure indicator 2. Exhaust gas temperature indicator 3. Cylinder head temperature indicator 1 1 0 1 1 1 0 1 1 1 0 1 1 1 1 1 1 1 0 0 1 1 1 1 * 0 1 0 1 0 * * 1 1 1 1 OIL 1. Oil temperature indicator 2. Oil pressure indicator FLIGHT CREW EQUIPMENT 1. Parachute rear 2. Parachute front 3. Seat belt rear 4. Seat belt front 5. Headset rear 6.
Pilot´s Operating Handbook EXTRA 330LX Section 3 Emergency Procedures SECTION 3 EMERGENCY PROCEDURE Table of Contents Paragraph Page 3.0 3.0.1 3.0.2 INTRODUCTION .................................................................................................................. 3-3 General ................................................................................................................................ 3-3 General Behaviour in Emergency Situations ...........................................
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Pilot´s Operating Handbook EXTRA 330LX 3.0 INTRODUCTION 3.0.1 GENERAL Section 3 Emergency Procedures 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. Thorough knowledge of these procedures will enable the aircrew to better cope with an emergency. The steps should be performed in the listed sequence.
Section 3 Emergency Procedures 3.
Pilot´s Operating Handbook EXTRA 330LX 3.2.4 Section 3 Emergency Procedures LOSS OF OIL PRESSURE 1. Positive "g" Apply If oil pressure is not regained then: 2. Airspeed 3. Throttle 4. Engine oil temperature 5. Land 90 KIAS (167 km/h) REDUCE AS REQUIRED OBSERVE INDICATION ASAP BE PREPARED FOR POWER OFF LANDING WARNING If oil pressure drops to 0 psi (kPa) the propeller pitch changes automatically to coarse (high) pitch with a corresponding decrease in RPM. 3.2.5 HIGH OIL TEMPERATURE 1. 2. 3. 4. 3.2.
Section 3 Emergency Procedures Pilot´s Operating Handbook EXTRA 330LX 3.3 FORCED LANDINGS 3.3.1 EMERGENCY LANDING WITHOUT ENGINE POWER 1. 2. 3. 4. 5. 6. 7. 8. 9. 3.3.2 Seat belts, shoulder harnesses Airspeed Mixture Fuel shutoff valve Ignition switch Battery switch Alternator switch Touchdown Brakes SECURE 90 KIAS (167 km/h) IDLE CUT OFF OFF (Pull & Turn) OFF OFF OFF SLIGHTLY TAIL LOW OPTIMUM BRAKING PRECAUTIONARY LANDING WITH ENGINE POWER 1. Seat belts, shoulder harnesses 2. Airspeed 3.
Pilot´s Operating Handbook EXTRA 330LX 3.4.2 3.4.3 Section 3 Emergency Procedures IF ENGINE FAILS TO START 1. Cranking 2. Throttle 3. Mixture 4. Fuel shutoff valve CONTINUE FULL OPEN IDLE CUT OFF OFF (Pull & Turn) If fire is extinguished: 5. Battery switch 6. Alternator switch 7. Ignition switch 8. Engine compartment OFF OFF OFF INSPECT ENGINE FIRE IN FLIGHT 1. 2. 3. 4. 5. Mixture Fuel shutoff valve Battery switch Alternator switch Airspeed 6. Land 3.5 ICING 3.5.
Section 3 Emergency Procedures 3.8 Pilot´s Operating Handbook EXTRA 330LX EMERGENCY EXIT AFTER TURN OVER 1. 2. 3. 4. 5. 6. Battery switch Alternator switch Fuel shutoff valve Seat belts Parachute harnesses (if wearing a parachute) Canopy handle OFF OFF OFF (Pull & Turn) OPEN OPEN PULL TO OPEN NOTE If canopy fails to open break the canopy. 7. Aircraft 3.9 EVACUATE ASAP ELEVATOR CONTROL FAILURE In case of elevator control failure the aircraft can be flown with the elevator trim.
Pilot´s Operating Handbook EXTRA 330LX Section 4 Normal Procedures SECTION 4 NORMAL PROCEDURES Table of Contents Paragraph Page 4.0 4.0.1 4.0.2 GENERAL ............................................................................................................................ 4-3 Airspeeds for Normal Operation ........................................................................................... 4-3 Checklist and Procedures .........................................................................
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Pilot´s Operating Handbook EXTRA 330LX 4.0 GENERAL 4.0.
Section 4 Normal Procedures Pilot´s Operating Handbook EXTRA 330LX 4.1 PREFLIGHT INSPECTION 4.1.1 EXTERIOR INSPECTION ILLUSTRATION 3 4 2 1 5 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. 4.2 CHECKLIST PROCEDURES 1) Cockpit 1. Pilot's Operating Handbook 2. Airplane weight and balance 3. Ignition switch 4. Battery switch 5. Fuel quantity indicators 6. Battery switch 7.
Pilot´s Operating Handbook EXTRA 330LX 6. Wing fuel tank drain 7. Right landing gear, wheel 8. Stall warning vane Section 4 Normal Procedures DRAIN FOR AT LEAST 4 SECONDS TO CLEAR SUMP OF POSSIBLE WATER; CHECK CLOSED CHECK CHECK 4) Nose 1. Engine oil dipstick 2. Propeller and spinner 3. Air inlet 4. Acro & center fuel tank drain 5. Fuel filter drain 6.
Section 4 Normal Procedures Pilot´s Operating Handbook EXTRA 330LX 4.3 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. 3. Open throttle approximately 1/4 travel. 4. Turn boost pump "ON". 5.
Pilot´s Operating Handbook EXTRA 330LX 4.5 TAKE-OFF PROCEDURE 4.5.
Section 4 Normal Procedures 4.6 Pilot´s Operating Handbook EXTRA 330LX CLIMB Climbs may be performed up to maximum continuous RPM. RPM above 2400 should, however, be used only when necessary for maximum performance in order to avoid unnecessary noise. Turn boost pump "OFF". 4.7 CRUISE 1. Altitude 2. Throttle/RPM 3. Mixture 4. Trim 5. Fuel 4.8 LANDING PROCEDURES 4.8.1 DESCENT 1. 2. 3. 4. 5.
Pilot´s Operating Handbook EXTRA 330LX Section 4 Normal Procedures NOTE Stall speed will be: MTOW = 820 kg (1808 lbs): MTOW = 870 kg (1918 lbs): MTOW = 950 kg (2095 lbs): 4.8.4 59 KIAS (109 km/h) 61 KIAS (113 km/h) 64 KIAS (119 km/h) NORMAL LANDING 1. Landing PERFORM as practicable with respect to surface and weather condition As desired 2. Landing light NOTE The rudder is effective down to 30 KIAS (56 km/h) 3. Touchdown 4. Throttle 5. Braking 4.
Section 4 Normal Procedures 4.12 ACROBATIC MANEUVERS 4.12.1 GENERAL Pilot´s Operating Handbook EXTRA 330LX NOTE 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. For maneuver limits refer to Section 2 LIMITATIONS. After termination of acrobatic maneuvers the artificial horizon (if installed) must be reset if possible.
Pilot´s Operating Handbook EXTRA 330LX Section 4 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. NOTE In extremely long lines a RPM decay may occur. This is related to a loss of oil pressure. Positive g´s should be pulled immediately in order to protect the engine. Oil pressure will return immediately.
Section 4 Normal Procedures 4.12.3 Pilot´s Operating Handbook EXTRA 330LX 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. - Ailerons against spin direction will make the spin flatter. - Ailerons into spin direction will lead to a spiral dive.
Pilot´s Operating Handbook EXTRA 330LX Section 4 Normal Procedures and - FAR 36 Appendix G, Amendment 28 as 77.5 dB(A) The noise level with silencer Gomolzig EA300-606000 (6 in 1) and propeller MTV-14-B-C/C 190130 at 2600 RPM has been established in accordance with - ICAO Annex 16, 6th Edition incorporating Amendment 10, Volume 1, Chapter 10 as 74.2 dB(A). and - FAR 36 Appendix G, Amendment 28 as 74.
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Pilot´s Operating Handbook EXTRA 330LX Section 5 Performance SECTION 5 PERFORMANCE Table of Contents Paragraph Page SECTION 5 5.1 5.1.1 5.1.2 5.1.3 GENERAL ............................................................................................................................ Performance Charts ............................................................................................................. Definitions of Terms ............................................................................
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Pilot´s Operating Handbook EXTRA 330LX Section 5 Performance SECTION 5 PERFORMANCE 5.1 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.
Section 5 Performance Pilot´s Operating Handbook EXTRA 330LX TAKE-OFF Take-Off Distance is shown by Fig. 5.5 Example: -T/O Weight: -Ground Roll: -Total Distance to clear a 50 ft obstacle: 870 kg (1918 lbs) 112 m (367 ft) 248 m (813 ft) These distances are well within the available field length incl. the 8 kts (15 km/h) headwind. RATE OF CLIMB Fig. 5.6 shows the Rate Of Climb using Take-off Power The Rate of Climb at 2000 ft (610 m): 2320 ft/min (11.
Pilot´s Operating Handbook EXTRA 330LX 5.2 Section 5 Performance ISA CONVERSION ISA Conversion of pressure altitude and outside air temperature Page Date: 4.
Section 5 Performance 5.3 Pilot´s Operating Handbook EXTRA 330LX AIRSPEED CALIBRATION CAS [km/h] 90 110 130 150 170 190 210 230 250 270 290 310 330 350 370 390 410 220 410 210 390 200 370 190 350 180 330 170 310 160 KIAS 270 140 250 130 230 IAS [km/h] 290 150 120 210 110 190 100 170 90 80 150 70 130 60 110 50 90 50 60 70 80 90 100 110 120 130 140 150 160 170 180 190 200 210 220 KCAS NOTE Indicated airspeed assumes zero instrument error 5-6 PageDate: Date:4.16.
Pilot´s Operating Handbook EXTRA 330LX 5.
Section 5 Performance 5.5 Pilot´s Operating Handbook EXTRA 330LX TAKE-OFF PERFORMANCE Power : Runway: T/O Power Concrete NOTE 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%. On a solid, dry and plain grass runway, the T/O is increased by 15%.
Page Date: 4. February 2011 2000 ft (ISA) 2320 ft/min PA: ROC: -20°C -10°C (-36°F) (-18°F) Max. power, full rich, 2600 rpm MTOW +10°C +20°C (+18°F) (+36°F) (181) (193) (187) (1874) (2095) (1985) +3 0° C (8 6° +2 F) 0° C (6 8° +1 F) 0° C -2 10 0° (5 0° °C C 0° C( ( F) 32 (1 -4 4 °F °F °F ) ) ) 1520 ft/min 8000 ft (ISA) 850 KG (1874 LBS) Power: (176) (1764) (170) (1654) KIAS (km/h) (lbs) VY Weight 5.
5 - 10 1654 1764 1874 1985 850 KG (1874 LBS) 2000 ft (ISA) => 8000 ft (ISA) WEIGHT / KG 2095 (LBS) 0 .53 1.59 1654 lbs 2.64 3.70 4.76 FUEL TO CLIMB 1874 lbs 2029 lbs TIME TO CLIMB: 3.1 min FUEL TO CLIMB: 4.4 ltr (1.16 US Gal.) EXAMPLE WEIGHT: ALT: LTR 5.81 (US GAL.) 2095 lbs 5.7 1544 CONDITIONS: MAX. CONT. POWER CLIMB AT VY SPEED; ISA Section 5 Performance Pilot´s Operating Handbook EXTRA 330LX TIME TO CLIMB, FUEL TO CLIMB Page Date: 4.
Pilot´s Operating Handbook EXTRA 330LX 5.8 Section 5 Performance RANGE Page Date: 4.
Section 5 Performance 5.9 5 - 12 Pilot´s Operating Handbook EXTRA 330LX ENDURANCE Page Date: 4.
Pilot´s Operating Handbook EXTRA 330LX 5.10 Section 5 Performance CRUISE PERFORMANCE Configuration: T/O Weight Acro & Center Tank Fuel Capacity Total Fuel Capacity 950 kg (2095 lb) 69 L (18.2 US gal) 189 L (49.9 US gal) Range and Endurance values include 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. 2 L (0.53 US gal) unusable fuel is taken into account. (At ISA-Conditions.) PA Eng.
Section 5 Performance 5.11 Pilot´s Operating Handbook EXTRA 330LX LANDING PERFORMANCE Power : Runway: Brakes: Idle Concrete maximum NOTE 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%. OAT Landing Airspeed weight 0°C (32°F) Land. Roll Land. Roll 30°C (86°F) kg (lbs) KIAS (km/h) ft (m) m (ft) Land.
Pilot´s Operating Handbook EXTRA 330LX Section 6 Weight and Balance and Equipment List SECTION 6 WEIGHT AND BALANCE AND EQUIPMENT LIST Table of Contents Paragraph SECTION 6 WEIGHT AND BALANCE AND EQUIPMENT LIST Page 6.1 GENERAL ............................................................................................................................ 6-3 6.2 6.2.1 AIRCRAFT WEIGHING PROCEDURE .................................................................................
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Pilot´s Operating Handbook EXTRA 330LX 6.1 Section 6 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. A comprehensive list of all equipment available for this aircraft is included. It is the responsibility of the pilot to ensure that the aircraft is loaded properly. 6.
Section 6 Weight and Balance and Equipment List Pilot´s Operating Handbook EXTRA 330LX 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: Situation before adding item: Wo, Xo = Airplane weight, CG position Wn, Xn = Weight, distance from fire wall of item to add New Weight of airplane and new CG: W = Wo + Wn XG = Wo x Xo + Wn x Xn : CG position W 6.2.
Pilot´s Operating Handbook EXTRA 330LX 6.3 Section 6 Weight and Balance and Equipment List CENTER OF GRAVITY CALCULATION (SAMPLE PROBLEM) PILOT Rear Seat Position ACRO-TANK Fuel 51 LTR (13.4 US GAL) COPILOT Front Seat WING-TANK Fuel 120 LTR (31,7 US GAL) (kg) (lbs) (kg) (lbs) (kg) (lbs) (kg) (lbs) 1 90 198.5 - - - - - - 2 90 198.5 37 81.5 - - - - 3 90 198.5 37 81.5 - - 86.4 190.5 4 90 198.5 - - 60 132.3 - - 5 90 198.5 37 81.5 60 132.
Pilot´s Operating Handbook EXTRA 330LX 6.3 CENTER OF GRAVITY CALCULATION (SAMPLE PROBLEM) Section 6 Weight and Balance and Equipment List 6-6 Page Date: 4.
Pilot´s Operating Handbook EXTRA 330LX 6.3.1 Section 6 Weight and Balance and Equipment List Sample Take-off Condition: Pilot On Rear Seat Copilot On Front Seat 51 L Fuel in Acro Tanks 101 L Fuel In Wing Tanks Aircraft Empty Weight 90.0 kg 90.0 kg 37.0 kg 73.0 kg 660.0 kg ======== 950.0 kg ( 198.5 lbs) ( 198.5 lbs) ( 81.5 lbs) ( 160.9 lbs) (1455 lbs) ========== (2094.4 lbs) To find C/G, follow line "Pilot Rear Seat" from Empty Weight to "90 kg" [198.5 lbs] (Point 1).
Section 6 Weight and Balance and Equipment List 6.4 Pilot´s Operating Handbook EXTRA 330LX LOADING WEIGHTS AND MOMENTS OCCUPANTS : max. 2 PILOT WEIGHT COPILOT Pilot REAR SEAT FRONT SEAT + Parachute Arm = 207cm (81.5 inch) Arm = 98 cm (38.
Pilot´s Operating Handbook EXTRA 330LX 6.5 Section 6 Weight and Balance and Equipment List WEIGHTS AND MOMENTS 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: 4.
Section 6 Weight and Balance and Equipment List 6.6 EQUIPMENT LIST QTY ITEM Pilot´s Operating Handbook EXTRA 330LX EXTRA 330LX MANUFACT. MODEL NO S/N: PART OR P/N WEIGHT ARM R* INST (kg) (m) A O Mooring (10) 2 Wing Tie Down Rings Extra 8C801.002 0.05 1.07 O 1 Canopy Lock Extra 83401.001-LK 0.25 1.90 O 3.70 0.20 O Venting and Heating (21) 1 Heater Extra EA-8D606 Option 300/LT KBS01 1 Battery Concorde RG-25 XC 03617 10.40 0.
Pilot´s Operating Handbook EXTRA 330LX QTY ITEM Section 6 Weight and Balance and Equipment List MANUFACT. MODEL NO PART OR P/N WEIGHT ARM R* INST (kg) (m) A O Fuel System (28) 1 Elec. Fuel Pump Weldon Tool B8120-M 1.10 -0.04 R 1 Elec. Fuel Pump Andair PX580-TC-XT 0.47 -0.04 A 1 Fuel Selector Allen 6 S 122 390144 0.19 0.73 R + Fuel Lines in Fuselage Parker/Statoflex PTFE Type 124 33315 1.65 0.70 R 1/2 Fuel Cont. Probe Wing VDO 226 801 015 001 FM4006 0.12 0.
Section 6 Weight and Balance and Equipment List QTY ITEM Pilot´s Operating Handbook EXTRA 330LX MANUFACT. MODEL NO PART OR P/N WEIGHT ARM R* INST (kg) (m) A O 1 Airspeed Ind. front (kts) Mikrotechna Praha LUN 1106.K2B4/SC 34155 0.50 0.65 A 1 Airspeed Ind. front (km/h) Mikrotechna Praha LUN 1106.P2B4/SC 34156 0.50 0.65 A 1 Airspeed Indicator rear (kts) United Instr. UI8030 B.882 32811 0.32 1.61 R 1 Airspeed Indicator rear (kts/km/h) United Instr. UI8030 B.896 33630 0.
Pilot´s Operating Handbook EXTRA 330LX QTY ITEM Section 6 Weight and Balance and Equipment List MANUFACT. MODEL NO 1 Remote Sensor Module (RSM) w GPS Aspen 910-00003-001 1 RSM Installation bracket Extra EA-86206.10 PART OR P/N in 33846, 33291, 34020 & 34021 WEIGHT ARM R* INST (kg) (m) A O 0.91 3.95 O 0.19 3.95 O Optional Multi-Function Display (ASPEN) 1 Electr. Flight Display (EFD1000) Aspen 910-00001-001 in 33292, 33293, 34024 & 34025 1.32 1.55 O 1 Electr.
Section 6 Weight and Balance and Equipment List QTY ITEM Pilot´s Operating Handbook EXTRA 330LX MANUFACT. MODEL NO PART OR P/N WEIGHT ARM R* INST (kg) (m) A O 1 Diplexer Comant Industries CI 507 FA4057 0.09 3.90 O 1 Course Deviation Ind. Garmin/Mid Continent GI-102A FA3010 0.64 1.54 O 1 Course Deviation Ind./GS Garmin/Mid Continent GI-106A FA3003 0.64 1.54 O 1 Transponder (Mode S) Becker BXP6401-2-(01) 31860-PG 0.80 1.60 A 1 Transp.
Pilot´s Operating Handbook EXTRA 330LX QTY ITEM Section 6 Weight and Balance and Equipment List MANUFACT. MODEL NO PART OR P/N WEIGHT ARM R* INST (kg) (m) A O 1 Governor (max 2600 RPM) MT-Propeller P-880-41 32941 1.10 -0.91 R 1 Governor (max 2700 RPM) MT-Propeller P-880-5 31509 1.10 -0.91 A 1 Governor (max 2700 RPM) Woodward A-210988 01209 1.10 -0.91 A Powerplant (7X) Engine 1 Engine Lycoming AEIO-580-B1A (R/H)ENPL-RT10427 32712 191.72 -0.
Section 6 Weight and Balance and Equipment List QTY ITEM MANUFACT. 1 EGT/CHT Indicator UMA 1 1 EGT Probe CHT Probe UMA UMA Pilot´s Operating Handbook EXTRA 330LX MODEL NO PART OR P/N D2-ET1K7KCT600J-01 2BU20 2B18 or 2B02 33438 JPI Flowscan Shadin FS-450 201-B or FXT-201 680501 or 680600 30611-PG JPI JPI JPI JPI JPI JPI JPI Flowscan Shadin EDM700/800 M-111 M-113 (S-Plug Gask.) 400510 400500-L 604010 420809 201-B or FXT-201 680501 or 680600 31530-PG WEIGHT ARM R* INST (kg) (m) A O 0.07 1.
Pilot´s Operating Handbook EXTRA 330LX QTY ITEM Section 6 Weight and Balance and Equipment List MANUFACT. MODEL NO PART OR P/N WEIGHT ARM R* INST (kg) (m) A O 1 Starter High-Torque inline Sky-Tec 149-12NL 30552 4.26 -0.85 A 1 Starter Engaged Light OAK MS25041-4 31732 0.02 1.63 O 1 Batt. Charger Cable Extra Assy 03543 O 1 External Power Cable Extra Assy 31730 O 1 Smoke Filling Hose Extra Assy 86100.000-24 O Ground Equipment Page Date: 29. 4.
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Pilot´s Operating Handbook EXTRA 330LX Section 7 Description and Operation of Aircraft and Systems SECTION 7 DESCPRIPTION & OPERATION OF AIRCRAFT AND SYSTEMS Table of Contents Paragraph Page 7.1 THE AIRCRAFT ................................................................................................................... 7-3 7.2 FUSELAGE ......................................................................................................................... 7-3 7.3 WINGS ..........................
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Pilot´s Operating Handbook EXTRA 330LX Section 7 Description and Operation of Aircraft and Systems SECTION 7 DESCPRIPTION AND OPERATION OF AIRCRAFT AND SYSTEMS 7.1 THE AIRCRAFT The aircraft EXTRA 330LX is designed and developed by EXTRA Flugzeugproduktions- und Vertriebs- GmbH, Flugplatz Dinslaken, 46569 Hünxe, Federal Republic of Germany, in accordance with the U.S.
Section 7 Description and Operation of Aircraft and Systems 7.3 Pilot´s Operating Handbook EXTRA 330LX WING The wing is a CRP construction. The dual chamber main spar - being a fail safe design consists of carbon roving caps combined with CRP webs. Core foam is a PVC foam. The wing shell is built by a Honeycomb sandwich with CRP laminates. Wing box ribs are made of carbon fiber composite with honeycomb core. The ribs in the nose section are made of wood.
Pilot´s Operating Handbook EXTRA 330LX 7.5 FLIGHT CONTROL SYSTEM 7.5.1 PRIMARY CONTROL SYSTEM Section 7 Description and Operation of Aircraft and Systems The EXTRA 330LX is standard equipped with full dual primary flight controls including front and rear sticks and adjustable rudder pedals. The primary control surfaces are operated through a direct mechanical linkage. 7.5.2 LONGITUDINAL FLIGHT CONTROL SYSTEM Front and rear sticks are interconnected by a push rod inside the torque tube.
Section 7 Description and Operation of Aircraft and Systems 7.6.1 Pilot´s Operating Handbook EXTRA 330LX INSTRUMENT PANEL (REAR COCKPIT) Figure 1, Instrument Panel 1 2 BATTERY 7 TRIM 12V 8 9 3 4 5 6 12 13 14 ALTERNATOR ALTERNATOR 10 11 15 16 17 18 Figure 2, Switches, Circuit Breaker 7-6 Page Date: 4.
Pilot´s Operating Handbook EXTRA 330LX Position Fig. 1 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 Position Fig. 2 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 Section 7 Description and Operation of Aircraft and Systems Item COM G-meter Volt/Amperemeter Airspeed indicator Magn.
Section 7 Description and Operation of Aircraft and Systems 7.6.2 Pilot´s Operating Handbook EXTRA 330LX INSTRUMENT PANEL (FRONT COCKPIT) Normally the instument panel in the front cockpit is only equipped with: - Airspeed indicator - Altimeter indicator. 7.7 LANDING GEAR The landing gear is a composite construction with a multichamber fiberglass spring in a tail-wheel design. The main wheels have a size of 5-5.50 and they are equipped with hydraulic disc brakes.
Pilot´s Operating Handbook EXTRA 330LX 7.10 POWER PLANT 7.10.1 ENGINE Section 7 Description and Operation of Aircraft and Systems The power plant consists of one Textron-Lycoming six-cylinder, horizontally opposed, aircooled, direct drive, fuel injection engine type with inverted oil system. The AEIO-580-B1A engine is characterized by the following performance data: - Rated power at 2700 RPM: 315 HP (234.9 kW). - Rated power at 2600 RPM: 303 HP (225.9 kW). - Rated power at 2400 RPM: 286 HP (213.3 kW).
Section 7 Description and Operation of Aircraft and Systems 7.10.3 Pilot´s Operating Handbook EXTRA 330LX ENGINE INSTALLATION The engine is supported by four shock mounts (type BARRY CONTROLS), to the tig-welded steel tube engine mount which is attached to the fuselage with four bolts on the firewall axis. The engine cowling is divided into two parts, a lower and an upper part both made of glassfibre/carbonfibre reinforced epoxy.
Pilot´s Operating Handbook EXTRA 330LX Section 7 Description and Operation of Aircraft and Systems Figure 3, Fuel System Page Date: 4.
Section 7 Description and Operation of Aircraft and Systems Pilot´s Operating Handbook EXTRA 330LX Wing Tank: The root section of each wing - in front of main spars forms an integral fuel tank providing two interconnected tanks with 120 liters (31,7 US GAL.) total capacity. Each side of the wing has a 2" diameter filler cap for gravity refueling. The wing tank can be completely emptied in flight. Acro & Center Tank: An Acro tank 9 liters (2,3 US Gal.
Pilot´s Operating Handbook EXTRA 330LX Section 7 Description and Operation of Aircraft and Systems Figure 4, Electrical System Page Date: 4.
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Pilot´s Operating Handbook EXTRA 330LX Section 8 Handling, Servicing and Maintenance SECTION 8 HANDLING, SERVICING & MAINTENANCE TABLE OF CONTENTS Paragraph Page 8.1 INTRODUCTION .................................................................................................................. 8-3 8.2 AIRPLANE INSPECTION PERIODS .................................................................................... 8-3 8.3 PILOT CONDUCTED PREVENTIVE MAINTENANCE .........................................
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Pilot´s Operating Handbook EXTRA 330LX Section 8 Handling, Servicing and Maintenance SECTION 8 HANDLING, SERVICING AND MAINTENANCE 8.1 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. c) A service manual with revision service may be procured from the manufacturer. 8.
Section 8 Handling, Servicing and Maintenance 8.5 Pilot´s Operating Handbook EXTRA 330LX 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). 8.6 GROUND HANDLING a) Due to its low weight and the free swiveling tail wheel two persons can easily move the airplane by hand. b) To tie down the airplane ring plates are provided at the wing tips.
Pilot´s Operating Handbook EXTRA 330LX Section 9 Supplements SECTION 9 SECTION 9 SUPPLEMENTS SECTION 9 SUPPLEMENTS Doc-No. EA-0E701.1 9 SUPPLEMENTS ..................................................................................................................... 3 Table of Contents Section 9 Pages Supplements ................................................................................................................... 4 p. 901 F Steerable Tail Wheel ..........................................
Section 9 Supplements Pilot´s Operating Handbook EXTRA 330LX 923 F f.u.n.k.e. TRT800H Transponder .................................................................................. 10 p. 924 F KANNAD 406 AF COMPACT/INTEGRA ELT .................................................................... 8 p. 9-2 Page Page Date: Date: 29. September 4.
Pilot´s Operating Handbook EXTRA 330LX 9 SUPPLEMENTS 9.1 Introduction Section 9 Supplements Section 9 "Supplements" of the Pilot´s Operating Handbook contains all information, necessary for a safe and efficient operation of the airplane when equipped with one or more of the various optional systems and equipment not provided with the standard airplane. 9.2 Notes The described systems and equipment are certified by the EASA for the EXTRA 330LX.
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Section 901 Steerable Tail Wheel Pilot´s Operating Handbook EXTRA 330LX SECTION 901 STEERABLE TAIL WHEEL Table of Contents Paragraph Page 901.1 GENERAL ......................................................................................................................... 901-3 901.2 LIMITATION ..................................................................................................................... 901-3 901.3 EMERGENCY PROCEDURES .......................................................
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Pilot´s Operating Handbook EXTRA 330LX 901 STEERABLE TAIL WHEEL 901.1 GENERAL Section 901 Steerable Tail Wheel To improve taxi and handling quality, the EXTRA 330LX 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. 901.
Section 901 Steerable Tail Wheel 901.8 Pilot´s Operating Handbook EXTRA 330LX HANDLING, SERVICING AND MAINTENANCE During 50 hour inspection, the bearing steel sleeve has to be lubricated on the point of lubricating. Additionally all parts of the tailwheel have to be inspected visually for deformations, cracks and corrosion. 901 - 4 Page Date: 4.
Pilot´s Operating Handbook EXTRA 330LX Section 902 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 ..............................................
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Pilot´s Operating Handbook EXTRA 330LX 902 ELECTRIC PEDAL ADJUSTMENT 902.1 GENERAL Section 902 Electric Pedal Adjustment To improve seat and control convenience, the EXTRA 330LX 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. 902.
Section 902 Electric Pedal Adjustment 902.7 Pilot´s Operating Handbook EXTRA 330LX 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.
Pilot´s Operating Handbook EXTRA 330LX Section 903 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 ........................................................
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Pilot´s Operating Handbook EXTRA 330LX 903.1 Section 903 Cabin Heating System GENERAL The 330LX 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. 903.2 LIMITATIONS The operation limitations are not affected due to the installation of the cabin heat system.
Section 903 Cabin Heating System 903.7 Pilot´s Operating Handbook EXTRA 330LX 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. A selector box (4) is placed on the engine side of the firewall. Using the main handle (9) the warm air can there be guided into the cockpit or dumped overboard.
Pilot´s Operating Handbook EXTRA 330LX Section 904 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 ..............................................
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Pilot´s Operating Handbook EXTRA 330LX 904 ACCELEROMETER TL-3424_EXT 904.1 GENERAL Section 904 Accelerometer TL-3424_EXT The TL-3424_EXT accelerometer can be installed as an option in the EXTRA 330LX. 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. displaying current acceleration values, 2. displaying the minimum and maximum acceleration, 3.
Section 904 Accelerometer TL-3424_EXT 904.6 Pilot´s Operating Handbook EXTRA 330LX 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. The instrument incorporates a high-precision sensor for measuring acceleration in the vertical axis.
Pilot´s Operating Handbook EXTRA 330LX Section 904 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. If the measured value exceeds the alarm limit a continuous sound is heard on the head set and the G/V LIMIT WARNING LIGHT illuminates continuously.
Section 904 Accelerometer TL-3424_EXT Pilot´s Operating Handbook EXTRA 330LX SYMBOLS The following symbols are used in the TL-3424_EXT display. Display Symbol Meaning Z recording to memory ll Recording paused ACC 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. Each is affiliated to the left and the right button. The left label is for the Left button.
Pilot´s Operating Handbook EXTRA 330LX Section 905 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 .......................................................................
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Pilot´s Operating Handbook EXTRA 330LX Section 905 External Power 905 EXTERNAL POWER 905.1 GENERAL The EXTRA 330LX 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. 905.2 LIMITATIONS The operation limitations are not affected due to the installation of the external power receptacle system.
Section 905 External Power Pilot´s Operating Handbook EXTRA 330LX 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". 11.Move mixture control slowly and smoothly to "FULL RICH". 12.Check the oil pressure gauge. If minimum oil pressure is not indicated within 30 seconds, shut off the engine and determine trouble. 13.Battery switch "ON". 14.
Pilot´s Operating Handbook EXTRA 330LX Section 906 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 ......................................................
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Pilot´s Operating Handbook EXTRA 330LX Section 906 Digital RPM Indicator 906 DIGITAL RPM INDICATOR 906.1 GENERAL The EXTRA 330LX is as standard equipped with an "P-1000" Digital rpm indicator. Depending on the category in which the aircraft is operated, one of the following models is used: P100-230-635-00 (max. 2600 rpm) P100-230-643-00 (max. 2700 rpm, for aerial work) . 906.2 LIMITATIONS The operation limitations are not affected by the installation of the "P-1000" Digital RPM indicator.
Section 906 Digital RPM Indicator Pilot´s Operating Handbook EXTRA 330LX Magneto-Control RPM range RPMrestriction Status Display Hours L Clear Trap DIM R buttons 906.6 Operation placard: Press-and-hold Operation placard: Press-and-release WEIGHT AND BALANCE Refer to the Equipment List in Section 6 of this Handbook. 906.7 DESCRIPTION AND OPERATION OF THE SYSTEM The operation of the indicator is straight-forward.
Pilot´s Operating Handbook EXTRA 330LX Section 906 Digital RPM Indicator RPM RANGES The face of the indicator is placarded with the respective engine rpm operating range. Additionally the 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.
Section 906 Digital RPM Indicator Pilot´s Operating Handbook EXTRA 330LX 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. However, a mechanism exists to mask either tachometer from the display, leaving the remaining tachometer to determine magneto/ignition problems.
Pilot´s Operating Handbook EXTRA 330LX Section 907 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 ........................................................................
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Pilot´s Operating Handbook EXTRA 330LX Section 907 Smoke System 907 SMOKE SYSTEM 907.1 GENERAL For performing at airshows, the EXTRA 330LX may optionally be equipped with a smoke system. 907.
Section 907 Smoke System Pilot´s Operating Handbook EXTRA 330LX FIRE IN FLIGHT 1. Switch "SMOKE ARM" OFF CAUTION If the fire (after the smoke system is shut off) will not extinguish proceed as follows: 2. Mixture 3. Fuel selector valve 4. Battery switch 5. Airspeed 6. Land 7.
Pilot´s Operating Handbook EXTRA 330LX Section 907 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. B) SMOKE GENERATION 1. Bad weather window and ventilation 2. "SMOKE ARM" Switch 3. Manifold Pressure 4.
Section 907 Smoke System Pilot´s Operating Handbook EXTRA 330LX 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" and "SMOKE REFILL") are in the ON position, the smoke system is not energized and will not run. A pump (reversed polarity) fills the floptube smoke oil tank through a quick connector located in the aircraft belly fairing.
Pilot´s Operating Handbook EXTRA 330LX 907.
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Pilot´s Operating Handbook EXTRA 330LX Section 908 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 ............................................................
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Pilot´s Operating Handbook EXTRA 330LX 908 SINGLE SEAT CANOPY 908.1 GENERAL Section 908 Single Seat Canopy 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. In the NORMAL category the aircraft can be flown only with the pilot in the rear seat. 908.3 EMERGENCY PROCEDURES Not affected. 908.
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Pilot´s Operating Handbook EXTRA 330LX Section 909 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 ...............................................................
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Pilot´s Operating Handbook EXTRA 330LX 909.1 Section 909 ARTEX ME-406 ELT GENERAL To improve the passive security, the EXTRA 330LX 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.
Section 909 ARTEX ME-406 ELT 909.3 Pilot´s Operating Handbook EXTRA 330LX 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, • turn additionally the remote switch in the rear panel to the "ON" position.
Pilot´s Operating Handbook EXTRA 330LX 909.7 Section 909 ARTEX ME-406 ELT 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. The switch has the positions ARM and ON. 909.7.
Section 909 ARTEX ME-406 ELT Pilot´s Operating Handbook EXTRA 330LX 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. NOTE The self-test time is accumulated in a register on the battery pack. The register records activation time in 30 second increments so all activations will count as at least 30 seconds, even if the actual time is much less.
Pilot´s Operating Handbook EXTRA 330LX Section 909 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. 4 Flashes Low power detected. Occurs if output power is below about 33 dBm (2 watts) for the 406 signal or 17 dBm (50 mW) for the 121.5 MHz output. Also may indicate that 406 signal is off frequency.
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Section 910 NAT AA83-001 Intercom Pilot´s Operating Handbook EXTRA 330LX SECTION 910 NAT AA83-001 INTERCOM Table of Contents Paragraph Page 910.1 910.1.1 GENERAL ......................................................................................................................... 910-3 Installation Adjustments .................................................................................................... 910-3 910.2 LIMITATIONS .................................................................
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Section 910 NAT AA83-001 Intercom Pilot´s Operating Handbook EXTRA 330LX 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.
Section 910 NAT AA83-001 Intercom 910.3 Pilot´s Operating Handbook EXTRA 330LX 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 910 - 4 Page Date: 4.
Pilot´s Operating Handbook EXTRA 330LX Section 910 NAT AA83-001 Intercom 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). As the knob is rotated clockwise (cw), the ICS volume for the crew increases. The ICS is muted during transmit operations.
Section 910 NAT AA83-001 Intercom 910.7.2 Pilot´s Operating Handbook EXTRA 330LX 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. LIVE ICS When the VOX control is positioned fully ccw to the LIVE position, all mics will be live, and any sound picked up will be processed by the ICS system (hot mic).
Section 910 NAT AA83-001 Intercom Pilot´s Operating Handbook EXTRA 330LX 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. In this way, switch over is immediate for the pilot and there is no possibility of lost communication because of a lack of pilot action.
Section 910 NAT AA83-001 Intercom Pilot´s Operating Handbook EXTRA 330LX 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.
Section 911 BECKER ATC 4401 Transponder Pilot´s Operating Handbook EXTRA 330LX SECTION 911 BECKER ATC 4401 TRANSPONDER Table of Contents Paragraph Page 911.1 911.1.1 911.1.2 911.1.3 911.1.4 911.1.5 911.1.6 911.1.7 911.1.8 GENERAL ......................................................................................................................... 911-3 Controls and indicators .....................................................................................................
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Section 911 BECKER ATC 4401 Transponder Pilot´s Operating Handbook EXTRA 330LX 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). Its functionality includes replying to ATCRBS Mode A and Mode C interrogations.
Section 911 BECKER ATC 4401 Transponder 911.1.1 A Pilot´s Operating Handbook EXTRA 330LX CONTROLS AND INDICATORS OFF/SBY/ON/ALT rotary mode switch with 4 detent positions OFF position : Transponder is switched off (expect panel lighting). SBY position : Standby mode is switched on. ON position : Mode A is switched on. ALT position : Mode A+C is switched on.
Section 911 BECKER ATC 4401 Transponder Pilot´s Operating Handbook EXTRA 330LX 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). NOTE 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).
Section 911 BECKER ATC 4401 Transponder Pilot´s Operating Handbook EXTRA 330LX 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. 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. d If neither button (F) or (G) is pressed within 3 seconds, the flashing stops and the storage operation is aborted.
Section 911 BECKER ATC 4401 Transponder Pilot´s Operating Handbook EXTRA 330LX 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.
Section 911 BECKER ATC 4401 Transponder Pilot´s Operating Handbook EXTRA 330LX 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. 3 A further test of the unit is triggered, if the VFR1 button (F) and VFR2 button (G) are pressed simultaneously.
Section 912 BECKER BXP 6401 Transponder Pilot´s Operating Handbook EXTRA 330LX SECTION 912 BECKER ATC 6401 TRANSPONDER Table of Contents Paragraph Page 912.1 912.1.1 912.1.2 912.1.3 912.1.4 912.1.5 912.1.6 912.1.7 912.1.8 912.1.9 912.1.10 GENERAL ......................................................................................................................... 912-3 Controls and Indicators .....................................................................................................
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Pilot´s Operating Handbook EXTRA 330LX 912.1 Section 912 BECKER BXP 6401 Transponder 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). Its functionality includes replying to ATCRBS Mode A, C and Mode S interrogations.
Section 912 BECKER BXP 6401 Transponder 912.1.1 Pilot´s Operating Handbook EXTRA 330LX CONTROLS AND INDICATORS A Mode Selector Rotary switch with 4 positions OFF position : Transponder is switched off SBY position : Standby mode is switched on ON position: Mode A/S is switched on. Transmission of altitude information is suppressed ALT position: Mode A/C/S is switched on and the altitude information is transmitted.
Section 912 BECKER BXP 6401 Transponder Pilot´s Operating Handbook EXTRA 330LX NOTE 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. 912.1.3 DISPLAY Transponder’s code is displayed in the top line using high readability font, at all times in modes SBY, ON, ALT.
Section 912 BECKER BXP 6401 Transponder Pilot´s Operating Handbook EXTRA 330LX 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.
Section 912 BECKER BXP 6401 Transponder Pilot´s Operating Handbook EXTRA 330LX 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. Negative results are indicated on the display with 'FAILURE'. The transpondermay be not switched into ON or ALT mode if any failure was found. The PBIT takes not longer than 1 second.
Section 912 BECKER BXP 6401 Transponder Pilot´s Operating Handbook EXTRA 330LX 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. 4 Rotate (B) to change this character. 5 Push (C) to set the cursor to the next character. 6 Repeat steps 4 and 5 until the flight number is entered.
Section 912 BECKER BXP 6401 Transponder Pilot´s Operating Handbook EXTRA 330LX 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). 1 Rotate (B) to the indication 'VFR=XXXX'. 2 First push to button (C) now left digit of the code is inverted. 3 Now the digit can be changed with (B). 4 Second push to button (C) now next left digit of the code is inverted.
Section 912 BECKER BXP 6401 Transponder 912.1.9 Pilot´s Operating Handbook EXTRA 330LX 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. 2 Pressing push-button (J) again within 3 seconds reactivates the previously-set reply code. NOTE When the unit is delivered, the VFR button is not assigned a code. This means that if this button is pressed for 0.
Pilot´s Operating Handbook EXTRA 330LX Section 913 GARMIN GTX 327 Transponder SECTION 913 GARMIN GTX 327 TRANSPONDER Table of Contents Paragraph Page 913.1 913.1.1 913.1.2 913.1.3 GENERAL ......................................................................................................................... 913-3 Mode Selection Keys ........................................................................................................ 913-3 Code Selection .............................................
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Pilot´s Operating Handbook EXTRA 330LX 913.1 Section 913 GARMIN GTX 327 Transponder 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 groundbased radar on a frequency of 1090 MHz.
Section 913 GARMIN GTX 327Transponder Pilot´s Operating Handbook EXTRA 330LX ALT 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. Replies to altitude interrogations include standard pressure altitude received from a separate encoder. 913.1.
Pilot´s Operating Handbook EXTRA 330LX Section 913 GARMIN GTX 327 Transponder VFR 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. CRSR Initiates entry of starting time for the Count Down timer and cancels transponder code entry.
Section 913 GARMIN GTX 327Transponder 913.2 Pilot´s Operating Handbook EXTRA 330LX 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). See the Airman’s Information Manual (AIM) for a detailed explanation of identification codes. 913.4 NORMAL PROCEDURES Not applicable. 913.5 PERFORMANCE Not applicable. 913 - 6 Page Date: 4.
Pilot´s Operating Handbook EXTRA 330LX Section 914 GARMIN GTX 328 Transponder SECTION 914 GARMIN GTX 328 TRANSPONDER Table of Contents Paragraph Page 914.1 914.1.1 914.1.2 914.1.3 914.1.4 914.1.5 914.1.6 914.1.7 GENERAL ......................................................................................................................... 914-3 Mode Selection Keys ........................................................................................................ 914-4 Code Selection .............
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Pilot´s Operating Handbook EXTRA 330LX 914.1 Section 914 GARMIN GTX 328 Transponder 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). Its functionality includes replying to ATCRBS Mode A and C and Mode S interrogations.
Section 914 GARMIN GTX 328 Transponder 914.1.1 Pilot´s Operating Handbook EXTRA 330LX MODE SELECTION KEYS OFF 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 interrogations. ON Selects Mode A. In this mode the transponder replies to interrogations, as indicated by the Reply Symbol. Replies do not include altitude information.
Pilot´s Operating Handbook EXTRA 330LX Section 914 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.
Section 914 GARMIN GTX 328 Transponder Pilot´s Operating Handbook EXTRA 330LX '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. 'COUNT DOWN TIMER' Controlled by START/STOP, CLR, and CRSR keys. The initial Count Down time is entered with the 0 - 9 keys.
Pilot´s Operating Handbook EXTRA 330LX 914.2 Section 914 GARMIN GTX 328 Transponder 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). See the Airman’s Information Manual (AIM) for a detailed explanation of identification codes. 914.4 NORMAL PROCEDURES Not applicable. 914.5 PERFORMANCE Not applicable. Page Date: 4.
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Pilot´s Operating Handbook EXTRA 330LX Section 915 GARMIN GTX 330 Transponder SECTION 915 GARMIN GTX 330 TRANSPONDER Table of Contents Paragraph Page 915.1 915.1.1 915.1.2 915.1.3 915.1.4 915.1.5 915.1.6 915.1.7 GENERAL ......................................................................................................................... 915-3 Mode Selection Keys ........................................................................................................ 915-4 Code Selection .............
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Pilot´s Operating Handbook EXTRA 330LX 915.1 Section 915 GARMIN GTX 330 Transponder 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). Its functionality includes replying to ATCRBS Mode A and C and Mode S interrogations.
Section 915 GARMIN GTX 330 Transponder 915.1.1 Pilot´s Operating Handbook EXTRA 330LX MODE SELECTION KEYS OFF 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. ON Selects Mode A. At power on the last active identification code will be selected. In this mode the transponder replies to interrogations, as indicated by the Reply Symbol. Replies do not include altitude information.
Pilot´s Operating Handbook EXTRA 330LX Section 915 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. 915.1.
Section 915 GARMIN GTX 330 Transponder Pilot´s Operating Handbook EXTRA 330LX '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. 'OAT/DALT' The OAT/DALT function is not available in this installation (no temperature input). 'COUNT UP TIMER' The count up timer is controlled by the START/STOP and CLR keys.
Pilot´s Operating Handbook EXTRA 330LX 915.2 Section 915 GARMIN GTX 330 Transponder 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). See the Airman’s Information Manual (AIM) for a detailed explanation of identification codes. 915.4 NORMAL PROCEDURES Not applicable. 915.5 PERFORMANCE Not applicable. Page Date: 4.
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Pilot´s Operating Handbook EXTRA 330LX Section 916 GARMIN GNC 420W/GNS 430W SECTION 916 GARMIN GNC 420W/GNS 430W Table of Contents Paragraph Page 916.1 GENERAL ......................................................................................................................... 916-3 916.2 916.2.1 LIMITATIONS ................................................................................................................... 916-3 Placards ............................................................
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Pilot´s Operating Handbook EXTRA 330LX 916.1 Section 916 GARMIN GNC 420W/GNS 430W 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. The GNC 420W/GNS 430W features a graphical display which may also be used to depict terrain data. The GNS 430W also features NAV functionality. This supplement is written for main software version 3.
Section 916 GARMIN GNC 420W/GNS 430W 916.2.1 Pilot´s Operating Handbook EXTRA 330LX PLACARDS GARMIN GPS limited to VFR use only (In the clear view of the pilot) (Next to the GNC 420W/GNS 430W circuit breaker) 916.3 EMERGENCY/ABNORMAL PROCEDURES 916.3.1 EMERGENCY PROCEDURES Not affected. 916.3.
Pilot´s Operating Handbook EXTRA 330LX Section 916 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. 5. Press ENT to confirm the selected airport, and ENT to activate the direct-to function. 916.4 NORMAL PROCEDURES TO ACTIVATE AN EXISTING FLIGHT PLAN: 1. Press FPL and turn the small right knob to display the flight plan catalog. 2.
Section 916 GARMIN GNC 420W/GNS 430W Pilot´s Operating Handbook EXTRA 330LX 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. Press this knob momentarily to toggle the tuning cursor between the COM and VLOC frequency fields. The COM flip-flop key is used to swap the active and standby COM frequencies.
Pilot´s Operating Handbook EXTRA 330LX Section 916 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. NOTE Whenever the GNC 420W/GNS 430W is displaying a list of information that is too long for the display screen, a scroll bar will appear along the right-hand side of the display.
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Pilot´s Operating Handbook EXTRA 330LX Section 917 ASPEN EFD1000/500 System SECTION 917 ASPEN EFD1000/500 Table of Contents Paragraph Page 917.1 917.1.1 GENERAL ......................................................................................................................... 917-3 Equipment Configuration ................................................................................................... 917-4 917.2 917.2.1 LIMITATIONS ............................................................
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Pilot´s Operating Handbook EXTRA 330LX 917.1 Section 917 ASPEN EFD1000/500 System GENERAL This Airplane Flight Manual Supplement (AFMS) applies to avionics installations of the following display combinations: 1. 2. 3. 4. 5.
Section 917 ASPEN EFD1000/500 System Pilot´s Operating Handbook EXTRA 330LX This supplement is written for MAP SOFTWARE RELEASE 2.4.1 and IOP SOFTWARE RELEASE 2.0.2 and is not suitable for earlier software versions. Some differences in operation may be observed when comparing the information in this supplement to later software versions. Verify the information herein depending on the configuration installed with the EFD1000 PFD and/or EFD1000/500 MFD Pilot's Guide(s) (Doc.
Pilot´s Operating Handbook EXTRA 330LX Section 917 ASPEN EFD1000/500 System Figure 1, Equipment Configuration Page Date: 4.
Section 917 ASPEN EFD1000/500 System 917.3 Pilot´s Operating Handbook EXTRA 330LX 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. 917.6 WEIGHT & CENTER OF GRAVITY Refer to the Equipment List in Section 6 of this Handbook. 917.7 SYSTEM DESCRIPTION 917.7.1 GENERAL Refer to the Aspen Pilot's Guide(s) as specified in paragraph 917.
Pilot´s Operating Handbook EXTRA 330LX Section 917 ASPEN EFD1000/500 System a „CHECK PITOT HEAT“ message as a reminder to the pilot to check for ice accumulating on the pitot probe. An „ATTITUDE FAIL“ annunciation will accompany the „CHECK PITOT HEAT“ amber annunciation, and will be presented when indicated airspeed is less than 30 KIAS (35 mph) and GPS groundspeed is greater than 50 kts (58 mph). NOTE The EXTRA 330LX doesn’t feature a pitot heating system.
Section 917 ASPEN EFD1000/500 System Database Type NavData Cultural Obstacles 917.7.4 Includes Update Cycle Database Provider Limitations High resolution terrain data for Americas, Delivered Jeppesen International, or Worldwide geographic regions.
Pilot´s Operating Handbook EXTRA 330LX Section 917 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. 917.7.
Section 917 ASPEN EFD1000/500 System Pilot´s Operating Handbook EXTRA 330LX 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. The pilot is responsible for terrain and obstacle avoidance by visual means. NOTE Maneuvering based solely on the EFD1000 traffic display is not authorized. The pilot in command has the responsibility to see and avoid traffic.
Pilot´s Operating Handbook EXTRA 330LX 917.7.8 Section 917 ASPEN EFD1000/500 System EVOLUTION SYNTHETIC VISION (OPTIONAL) NOTE 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. NOTE Flight with an expired database is not recommended.
Section 917 ASPEN EFD1000/500 System Pilot´s Operating Handbook EXTRA 330LX 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. NOTE Synthetic Vision and the associated Terrain Warning System are dependant on accurate barometric altitude.
Pilot´s Operating Handbook EXTRA 330LX Section 918 EI MVP-50P SECTION 918 EI MVP-50P Table of Contents Paragraph Page 918.1 GENERAL ......................................................................................................................... 918-3 918.2 918.2.1 LIMITATIONS ................................................................................................................... 918-3 Instrument Markings ............................................................................
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Pilot´s Operating Handbook EXTRA 330LX 918.1 Section 918 EI MVP-50P GENERAL The MVP-50P is a Glass Panel Engine Monitor that provides both analog and digital displays with digits that blink and change colors when yellow or red operating ranges are reached. All of these features are designed to alert the pilot the moment any monitored function exceeds its normal operating limit.
Section 918 EI MVP-50P Pilot´s Operating Handbook EXTRA 330LX FUEL PRESSURE INDICATOR green range red line 918.3 0 psig 14 psig 14 psig 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" position.
Pilot´s Operating Handbook EXTRA 330LX 918.6 Section 918 EI MVP-50P WEIGHT & CENTER OF GRAVITY Refer to the equipment list in Section 6 of this Handbook. 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.
Section 918 EI MVP-50P Pilot´s Operating Handbook EXTRA 330LX NOTE Any instrument can fail at any time. Acquire proper training to safely operate this aircraft without the use of this instrument. Refer to the Operating Instructions for further operating and safety information. 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 918 - 6 Page Date: 29.
Pilot´s Operating Handbook EXTRA 330LX Position Fig. 2 1 2 3 4 5 6 7 8 9 10 11 12 13 14 918.8 Section 918 EI MVP-50P Item Alternator warning light incl.
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Section 919 Landing Light Pilot´s Operating Handbook EXTRA 330LX SECTION 919 LANDING LIGHT Table of Contents Paragraph Page 919.1 GENERAL ......................................................................................................................... 919-3 919.2 LIMITATION ..................................................................................................................... 919-3 919.3 EMERGENCY PROCEDURES .....................................................................
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Pilot´s Operating Handbook EXTRA 330LX 919 LANDING LIGHT 919.1 GENERAL Section 919 Landing Light To improve the visibility of the aircraft during landing approach a landing light can be integrated in the RH lower cowling. 919.2 LIMITATION No change. 919.3 EMERGENCY PROCEDURES No change. 919.4 NORMAL PROCEDURES No change. 919.5 PERFORMANCE No change. 919.6 WEIGHT AND BALANCE Refer to the Equipment List in section 6 of this Handbook. 919.
Section 919 Landing Light 919.8 Pilot´s Operating Handbook EXTRA 330LX HANDLING, SERVICING AND MAINTENANCE No change. 919 - 4 Page Date: 4.
Pilot´s Operating Handbook EXTRA 330LX Section 920 Airtow Hook SECTION 920 AIRTOW HOOK Table of Contents Paragraph SECTION 920 AIRTOW HOOK Page 920.1 GENERAL ......................................................................................................................... 920-3 920.2 LIMITATIONS ................................................................................................................... 920-3 920.3 EMERGENCY PROCEDURES .................................................
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Pilot´s Operating Handbook EXTRA 330LX 920.1 Section 920 Airtow Hook GENERAL The EXTRA 330LX 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. 920.
Section 920 Airtow Hook 920.3 Pilot´s Operating Handbook EXTRA 330LX EMERGENCY PROCEDURES A) ABORTED TAKE OFF 1. Pilot of the glider 2. Throttle 3. Mixture 4. Brakes INFORM IDLE IDLE CUT OF APPLY AS PRACTICAL B) ENGINE FAILURE IMMEDIATELY AFTER TAKEOFF Stall speed: 64 KIAS (119 km/h) 1. Pilot of the glider 2. Air tow 3. Airspeed 4. Mixture 5. Fuel shutoff valve 6. Ignition switch 7. Master switch 8.
Pilot´s Operating Handbook EXTRA 330LX Section 920 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. 920.
920 - 6 T/0 roll m (ft) 134 (440) 156 (512) 183 (600) 214 (702) 252 (827) 15 m (50 ft) m (ft) 219 (719) 256 (840) 299 (981) 350 (1148) 411 (1348) T/0 roll m (ft) 176 (577) 205 (673) 239 (784) 280 (919) 329 (1079) 15 m (50 ft) m (ft) 287 (942) 334 (1096) 391 (1283) 458 (1503) 538 (1765) PA ft (m) SL 2000 (610) 4000 (1219) 6000 (1829) 8000 (2438) T/0 roll m (ft) 220 (722) 257 (843) 300 (984) 351 (1152) 413 (1355) 15 m (50 ft) m (ft) 360 (1181) 419 (1375) 489 (1604) 574 (1883) 674 (2211) OAT -10°C (14°
Pilot´s Operating Handbook EXTRA 330LX Section 920 Airtow Hook CLIMBRATE Conditions: Power: 2500 Rpm and full throttle, mixture rich, Speed of the aircraft tow: 80 KIAS = 148 Km/h, Weight of the towing aircraft: m = 820 Kg (1808 lb) Tow force: glider with m = 350 kg (772 lbs) PA ft (m) • _ _SL 1000 (305) 2000 (610) 3000 (914) 4000 (1219) 5000 (1524) 6000 (1829) 7000 (2134) 8000 (2438) 0°C (32°F) OAT 10°C (50°F) 20°C (68°F) 30°C (86°F) ft/min m/s ft/min m/s ft/min m/s ft/min m/s 1610 1540 147
Section 920 Airtow Hook 920.6 Pilot´s Operating Handbook EXTRA 330LX WEIGHT AND BALANCE Not affected. 920.7 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. 920.
Pilot´s Operating Handbook EXTRA 330LX Section 921 AIRPLANES REGISTERED IN BRAZIL SECTION 921 AIRPLANES REGISTERED IN BRAZIL AND OPERATING UNDER THE AGÊNCIA NACIONAL DE AVIAÇÃO CIVIL REQUIREMENTS Table of Contents Paragraph SECTION 921 Page 921.1 GENERAL ............................................................................................................................... 3 921.2 921.2.1 921.2.2 LIMITATIONS .....................................................................................
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Pilot´s Operating Handbook EXTRA 330LX 921.1 Section 921 AIRPLANES REGISTERED IN BRAZIL 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“ – RBAC 21, Section 21.29. The information contained within this supplement is to be used in conjunction with the basic AFM/ POH and supplements.
Section 921 AIRPLANES REGISTERED IN BRAZIL Pilot´s Operating Handbook EXTRA 330LX 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.
Pilot´s Operating Handbook EXTRA 330LX 921.8 Section 921 AIRPLANES REGISTERED IN BRAZIL HANDLING, SERVICING AND MAINTENANCE Not affected. Page Date: 12. 31.
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Pilot´s Operating Handbook EXTRA 330LX Section 922 GARMIN GTN 635/650/750 SECTION 922 GARMIN GTN 635/650/750 Table of Contents Paragraph Page 922.1 GENERAL ......................................................................................................................... 922-3 922.2 922.2.1 922.2.2 922.2.3 922.2.4 922.2.5 922.2.6 922.2.7 LIMITATIONS ................................................................................................................... 922-3 Placards ................
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Pilot´s Operating Handbook EXTRA 330LX 922.1 Section 922 GARMIN GTN 635/650/750 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. The GTN 650 & 750 units include all of the features of the GTN 635 in addition to airborn VOR/localizer (LOC) and glideslope (G/S) receivers. The GTN 750 features a larger display.
Section 922 GARMIN GTN 635/650/750 Pilot´s Operating Handbook EXTRA 330LX 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. The navigation data incl. for final approach segments provided by the GTN series (e.g.
Pilot´s Operating Handbook EXTRA 330LX 922.2.1 Section 922 GARMIN GTN 635/650/750 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) INTERCOM 922.2.2 (Next to the GMA 35 Remote Audio Panel circuit breaker, if installed) SD CARD Proper function of any of the units is predicated on the SD card being present. 922.2.
Section 922 GARMIN GTN 635/650/750 922.2.6 Pilot´s Operating Handbook EXTRA 330LX 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. 922.2.7 DEMO MODE Demo mode may not be used in flight under any circumstances. 922.3 EMERGENCY/ABNORMAL PROCEDURES 922.3.
Pilot´s Operating Handbook EXTRA 330LX Section 922 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. All information normally derived from GPS will become less accurate over time. SEARCHING A NEARBY AIRPORT To select a nearby airport as a direct-to waypoint: 1.
Section 922 GARMIN GTN 635/650/750 922.6 Pilot´s Operating Handbook EXTRA 330LX 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.
Pilot´s Operating Handbook EXTRA 330LX Section 922 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. 922.7.3 SELECTING COM/NAV FREQUENCIES Tuning control normally remains in the COM window and will return after 30 seconds of inactivity.
Section 922 GARMIN GTN 635/650/750 Pilot´s Operating Handbook EXTRA 330LX 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. IDENT 1. Touch the IDENT key once to reply with an identifying squawk code. 2.
Pilot´s Operating Handbook EXTRA 330LX Section 922 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. The transponder will still be powered, but will not transmit information. The active transponder indication and Ident annunciation will be grayed to show they are disabled. GROUND 1.
Section 922 GARMIN GTN 635/650/750 Pilot´s Operating Handbook EXTRA 330LX 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) 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.
Pilot´s Operating Handbook EXTRA 330LX Section 922 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. AUDIO SPLIT MODE 1. While the Audio Control page is displayed, touch the Split Mode key to display Crew Intercom selections. 2.
Section 922 GARMIN GTN 635/650/750 Pilot´s Operating Handbook EXTRA 330LX 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. 3. Touch the Backward, Play or Forward keys to control the playback of the currently selected recording. 4. Touch the Previous or Next keys to select a recording. INTERCOM SETUP 1.
Pilot´s Operating Handbook EXTRA 330LX Section 922 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.
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Section 923 f.u.n.k.e TRT800H Transponder Pilot´s Operating Handbook EXTRA 300LC SECTION 923 f.u.n.k.e. TRT800H TRANSPONDER Table of Contents Paragraph Page 923.1 923.1.1 923.1.2 923.1.3 923.1.4 923.1.5 923.1.6 923.1.7 923.1.8 923.1.9 923.1.10 923.1.11 GENERAL ......................................................................................................................... 923-3 Features .............................................................................................................
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Pilot´s Operating Handbook EXTRA 300LC 923.1 Section 923 f.u.n.k.e TRT800H Transponder GENERAL NOTE In order to operate the Mode S transponder it is necessary to request an ICAO 24-bit Aircraft Address at the responsible national aviation authorities. The received Code is assigned to the specific transponder/aircraft and must be configured within the transponder. The 24-bit address is stored in an external memory which allows the transponder being exchanged without requiring any further configuration.
Section 923 f.u.n.k.e TRT800H Transponder 923.1.2 Pilot´s Operating Handbook EXTRA 300LC OPERATION CONTROLS 923 - 4 Page Date: 12.
Pilot´s Operating Handbook EXTRA 300LC I/O ON/OFF Switch ON: Switch OFF: Section 923 f.u.n.k.e TRT800H Transponder press I/O button for approx. 0,5 s press I/O button for approx. 3 s VFR VFR activate/deactivate VFR Squawk (press shortly) store active Squawk as VFR/VFRW-Squawk (press button 3 s) CHANGE change between active and standby-Squawk works as cursor back button (opposite function of the cursor button) during entering values and also for navigating backwards through the configuration menu.
Section 923 f.u.n.k.e TRT800H Transponder 923.1.3 Pilot´s Operating Handbook EXTRA 300LC DISPLAY-CONTRAST In active mode (not standby) press for 2 s. Display indicates “CON” Now adjust contrast (CON) with rotary knob. Return to normal operation: press 923.1.4 or wait 5 s. FLIGHT-ID (FID) The FID is an identifier required for Mode S Operation. During future application of flight plans a FID could be assigned on a per flight basis.
Pilot´s Operating Handbook EXTRA 300LC 923.1.7 Section 923 f.u.n.k.e TRT800H Transponder TRANSPONDER MODE SELECTION Press MODE (repeatedly) to select from following Modes: • STBY „Standby“ Transponder does not respond to any interrogation. Squitter and ADS-B output is not active. • A C S „Mode A+C+S“ Standard condition; transponder responds to mode A, C and S interrogations. • A – S „Mode A+S, no C“ Altitude is not transmitted (neither on C nor on S requests).
Section 923 f.u.n.k.e TRT800H Transponder 923.1.
Pilot´s Operating Handbook EXTRA 300LC 923.2 Section 923 f.u.n.k.e TRT800H Transponder 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). See the Airman’s Information Manual (AIM) for a detailed explanation of identification codes. 923.4 NORMAL PROCEDURES Not applicable. 923.5 PERFORMANCE Not applicable. Page Date: 12.
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Pilot´s Operating Handbook EXTRA 330LX Section 924 KANNAD AF 406 ELT SECTION 924 KANNAD 406 AF COMPACT/INTEGRA ELT Table of Contents Paragraph 924.1 Page GENERAL ......................................................................................................................... 924-3 924.2 LIMITATIONS ................................................................................................................... 924-3 924.3 EMERGENCY PROCEDURES ...............................................
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Pilot´s Operating Handbook EXTRA 330LX 924.1 Section 924 KANNAD AF 406 ELT GENERAL To improve the passive security, the EXTRA 330LX 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. This 121.
Section 924 KANNAD AF 406 ELT 924.3 Pilot´s Operating Handbook EXTRA 330LX 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, • switch additionally the remote switch in the rear panel to the "ON" position.
Pilot´s Operating Handbook EXTRA 330LX • Section 924 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. • confirm this on the aircraft radio.
Section 924 KANNAD AF 406 ELT 924.7.1 Pilot´s Operating Handbook EXTRA 330LX 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. To deactivate the ELT switch the switch on the ELT unit to the ‘OFF’ position.
Pilot´s Operating Handbook EXTRA 330LX 924.8.2 Section 924 KANNAD AF 406 ELT 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); • before or on the battery expiration date; • after use in an emergency; • after an inadvertant activation of unknown duration.
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