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Extra 300L, Information Manual

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921 - 10

Page Date: 5. December 2008

Pilot´s Operating Handbook

EXTRA 300L

Section 921
Lycoming AEIO-580-B1A Engine

921.5.4

Cruise Performance Chart Configuration 2

Configuration:
T/O Weight

950 kg (2095 lb)

Acro & Center Tank Fuel Capacity

  69 L (18.2 US gal)

Total Fuel Capacity

189 L (49.9 US gal)

Range and Endurance values include fuel for warm-up and Take-Off from SL, max. 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.

Manif. Power Setting

Fuel

TAS

IAS

Endur.

Range

Mixture

Press.

Consumption

1*

1*

2*

[ft] (m) [rpm]

[inHg]

[%]

[hp]

[L/h] [gal/h]

[kts] (km/h) [kts] (km/h) [h]

[nm] (km)

Best ...

2000  2700*

26.5

91

286

88.2 (23.3)

182.6 (338)

173 (320) 1.73

317 (587)

Power

(610)

2400

24.0

71

225

68.7 (18.2)

167.6 (310)

160 (296) 2.22

373 (691)

Power

2200

23.2

62

195

50.5 (13.3)

159.3 (295)

152 (282) 3.03

481 (891)

Economy

2000

22.5

52

165

42.6 (11.3)

150.2 (278)

144 (267) 3.59

538 (996)

Economy

2000

19.4

43

135

36.5 (9.6)

139.9 (259)

134 (248) 4.18

584 (1082) Economy

4000  2700*

24.5

85

267

82.7 (21.9)

181.5 (336)

168 (311) 1.85

333 (617)

Power

(1219) 2400

23.4

71

225

68.7 (18.2)

170.9 (317)

158 (293) 2.22

378 (700)

Power

2200

22.7

62

195

50.5 (13.3)

162.4 (301)

150 (278) 3.02

487 (902)

Economy

2000

21.8

52

165

42.6 (11.3)

153.1 (284)

142 (263) 3.57

544 (1007) Economy

2000

19.0

43

135

36.5 (9.6)

142.6 (264)

133 (246) 4.18

591 (1095) Economy

6000  2700*

22.8

79

248

77.6 (20.5)

180.5 (334)

162 (300) 1.97

351 (650)

Power

(1829) 2500

22.2

71

225

69.8 (18.4)

174.3 (323)

156 (289) 2.19

377 (698)

Power

2200

22.2

62

195

50.5 (13.3)

165.6 (307)

149 (276) 3.00

493 (913)

Economy

2000

21.5

52

165

42.6 (11.3)

156.1 (289)

141 (261) 3.55

551 (1020) Economy

2000

18.5

43

135

36.5 (9.6)

145.4 (269)

131 (243) 4.12

598 (1107) Economy

8000  2700*

21.0

73

231

73.4 (19.4)

179.6 (333)

166 (307) 2.08

367 (680)

Power

(2438)  2675*

20.7

71

225

71.9 (19.0)

177.8 (329)

156 (289) 2.12

371 (687)

Power

2350

20.6

62

195

52.0 (13.7)

169.0 (313)

147 (272) 2.90

485 (898)

Economy

2050

20.6

52

165

43.0 (11.4)

159.3 (295)

139 (257) 3.49

552 (1022) Economy

10000  2700*

19.8

69

215

69.6 (18.4)

178.6 (331)

151 (280) 2.19

382 (707)

Power

(3048) 2500

19.2

62

195

53.6 (14.2)

172.4 (319)

146 (270) 2.81

476 (882)

Economy

2150

19.3

52

165

43.7 (11.5)

162.5 (301)

138 (256) 3.42

549 (1017) Economy

*

This RPM setting is not allowed for airplanes equipped with a 3-blade propeller MTV-9-B-C/C 198-
25 operated in the normal category, in which noise protection requirements must be complied with.

N O T E

1* For temperatures above/ below  Standard (ISA), increase/decrease Range 1,7% and

Endurance 1,1% for each 10°C (18°F) above/below Standard Day Temperature for
particular altitude.

2* Leaning with exhaust gas temperature (EGT) gage:

For the adjustment "Best Power", first lean the mixture to achieve the top exhaust
temperature (peak EGT) and then enrich again until the exhaust temperature is 100°F
lower than peak EGT.
For the adjustment "Best Economy",  simply lean the mixture to achieve the top
exhaust temperature (peak EGT).

 W A R N I N G

Risk of engine overheating.
Always return the mixture to full rich before increasing power settings.

Page Date: 20. January 2016

Summary of Contents for 300L

Page 1: ...slaken 46569 Hünxe Federal Republic of Germany TITLE PAGE W A R N I N G This is an Information Manual and may be used for general purposes only This Information Manual is not kept current It must not be used as a substitute for the official FAA EASA Approved Pilot s Operating Handbook required for operation of the airplane ...

Page 2: ...Left blank intentionally ...

Page 3: ...ber2005 EASA Approval N EASA A A 01319 DateofApproval 20 November2006 EASA Approval N EASA A C 08351 DateofApproval 24 July 2008 EASA Approval N EASA A C 10781 DateofApproval 18 February2009 Approved under the authority of DOA N EASA 21J 073 ECO ÄM 300 09 07 DateofApproval 6 April 2009 EASA Approval N 10026766 DateofApproval 7 August 2009 Approved under the authority of DOA N EASA 21J 073 FAA Vali...

Page 4: ...8 20 April 2002 LOGOFEFFECTIVEPAGES 6 9 thru 6 16 20 January2016 7 1 20 September2006 7 2 20 April 2002 7 3 thru 7 4 31 March 2009 7 5 thru 7 8 20 April 2002 7 9 31 March 2009 7 10 15 December2005 7 11 20 January2016 7 12thru7 13 15 December2005 7 14 8 October 2009 7 15thru7 16 20 April 2002 8 1 thru 8 4 20 April 2002 9 1 5 December2008 9 2 20 January2016 9 3 31 March 2009 9 4 20 April 2002 901 1t...

Page 5: ...20 4 20 January2016 920 5thru920 10 31 March 2009 921 1 20 January2016 921 2 5 December2008 921 3 8 October 2009 921 4thru921 5 20 January2016 921 6 19 April 2012 921 7 20 January2016 921 8thru921 9 19 April 2012 921 10 20 January2016 921 11thru921 16 19 April 2012 922 1thru922 3 5 December2008 922 4 20 January2016 922 5thru922 8 5 December2008 923 1thru923 2 5 December2008 923 3 20 January2016 92...

Page 6: ...ncludingrevisionsandanyrelevantsupplements Pages of this Airplane Flight Manual must not be exchanged and no alterations of or additions to the approved contents may be made without the EXTRA Flugzeugproduktions undVertriebs GmbH EASAapproval The editor has the copyright of this Flight Manual and is responsible for edition of revisions amendmentsandsupplements Amendments which affect the airworthi...

Page 7: ...t in death or serious injury C A U T I O N Indicates a hazardous situation which if not avoided could result in minor or mode rate injury Additional information given in this manual are also marked by boxed textmarkers in the middle of the page and are written in semi bold characters N O T I C E Is used to address practices not related to physical injury N O T E Represents an useful or remarkable ...

Page 8: ...L MAINTABLEOFCONTENTS Section Page 1 GENERAL 1 1 2 LIMITATIONS 2 1 3 EMERGENCYPROCEDURES 3 1 4 NORMALPROCEDURES 4 1 5 PERFORMANCE 5 1 6 WEIGHT BALANCE EQUIPMENTLIST 6 1 7 AIRPLANE SYSTEMSDESCRIPTIONS 7 1 8 AIRPLANEHANDLING SERVICE MAINTENANCE 8 1 9 SUPPLEMENTS 9 1 ...

Page 9: ... 3 1 2 MANUFACTURER 1 3 1 3 TECHNICAL DATA 1 3 1 3 1 3 View Drawing 1 3 1 3 2 Main Data 1 3 1 3 3 Wing 1 4 1 3 4 Horizontal Tail 1 4 1 3 5 Elevator 1 4 1 3 6 Vertical Tail 1 4 1 3 7 Rudder 1 4 1 4 ENGINE 1 4 1 5 PROPELLER 1 5 1 5 1 Exhaust Systems Optional 1 5 1 6 FUEL 1 5 1 7 OIL 1 5 1 8 LOADING 1 6 1 9 TERMINOLOGY 1 6 1 10 SECONDARY TERMINOLOGY 1 7 1 11 CONVERSION TABLE 1 8 Page Date 16 March 20...

Page 10: ...1 2 Page Date 20 April 2002 Section 1 General Pilot s Operating Handbook EXTRA 300L Left blank intentionally ...

Page 11: ...gear are manufactured of composite material The aircraft is a two seater with the rear seat instrumented for pilot in comand 1 1 SPECIFICATION OF CLASS The aircraft is certified in normal and acrobatic category T C D S EASA A 362 1 2 MANUFACTURER EXTRAFlugzeugproduktions undVertriebs GmbH FlugplatzDinslaken 46569Hünxe Federal Republic of Germany 1 3 TECHNICALDATA 1 3 1 3 VIEWDRAWING Page Date 31 M...

Page 12: ...S Chord Root 1 85 m Tip 0 88 m MAC 1 404 m 4 61 ft Aileron area 2 x 0 855 m 2 x 9 20 ft Aileron deflection up down 30 tolerance 2 1 3 4 HORIZONTALTAIL Span 3 20 m 10 50 ft Area 2 56 m 27 56 ft Airfoil WortmannFX71 L 150 30 1 3 5 ELEVATOR Area 0 77 m 8 29 ft Elevator deflection up down 25 tolerance 2 Trim tab deflection up 40 down 50 tolerance 5 1 3 6 VERTICALTAIL Area 1 39 m 14 96 ft Airfoil Wortm...

Page 13: ...ard system PN EA 300 NSD GO3 606500 Complete 6 in 1 System with integrated Silencer PN EA 300 606000 1 6 FUEL Fuel type AVGAS 100 100 LL for alternate fuel grades see later issues of Textron Lycoming S I No 1070 Minimum 100 130 octane Maximum 115 145 octane Total fuel capacity 171 L 45 1US gal Wingtanks 2 x 60 L 120 L 31 7US gal Acro center tank 51 L 13 4US gal Usable fuel capacity in the system 1...

Page 14: ...8 kg m Normal 76 6 81 3 kg m Acrobatic 1 seat 2 seats Powerloading 3 17 kg hp Normal 2 73 2 90 kg hp Acrobatic 1 seat 2 seats 1 9 TERMINOLOGY Air Speeds CAS Calibrated Air Speed CAS is the same as TAS True Air Speed in standard atmospheric condition at sea level KCAS Calibrated speed in knots GS Groundspeed IAS Indicated air speed KIAS Indicated speed in knots TAS True air speed It s the same as C...

Page 15: ...US liquid gallon 3 79 litres US qt US liquid quart 0 946 litres hp Horsepower english h Hour kts Knots nm h 1 852 kilometer per hour km h Kilometer per hour lbs English pound 0 4536 kg hPa hekto Pascal inHg Inches of mercury MP Manifoldpressure PA Pressure altitude ft nm Nautical miles 1 852 km rpm Revolutionsperminute CG Centerof gravity Arm Arm is the horizontal distance from reference datum Mom...

Page 16: ...1 8 Page Date 20 April 2002 Section 1 General Pilot s Operating Handbook EXTRA 300L 1 11 CONVERSIONTABLE Page Date 16 March 2009 ...

Page 17: ... 2 Acrobatic Flight 1 Seat 2 5 2 7 3 Acrobatic Flight 2 Seats 2 6 2 8 ACROBATIC MANEUVERS 2 6 2 8 1 Normal Flight 2 6 2 8 2 Acrobatic Flight 2 6 2 9 LOAD FACTOR 2 7 2 9 1 Normal Flight 2 7 2 9 2 Acrobatic Flight 2 8 2 10 FLIGHT CREW LIMITS 2 8 2 11 KINDS OF OPERATIONAL LIMITS 2 8 2 11 1 Structural Temperature Colour Limitation 2 8 2 12 MAXIMUM OPERATING ALTITUDE 2 8 2 13 TIRE PRESSURE 2 8 2 14 MAR...

Page 18: ...2 2 Page Date 20 April 2002 Pilot s Operating Handbook EXTRA 300L Section 2 Limitations Left blank intentionally ...

Page 19: ...d for the acrobatic category only for normal category refer to corresponding limitations This aircraft is certified under Type Certification Data Sheet T C D S EASA A 362 Any exceedance of given limitations has to be reported by the pilot so that necessary inspection or maintenance procedures according to the SERVICE MANUAL EA 300 L can be performed 2 2 AIR SPEED IAS NeverExceedSpeed VNE 220 knots...

Page 20: ...ty 15 13 L 16 US qt Minimum sump capacity 8 51 L 9 US qt d Oil pressure MinimumIdling 172 kPa 25 Psi Normal 379 655 kPa 55 95 Psi Starting Warmup TaxiandTake Off 793 kPa 115 Psi W A R N I N G It is normal for the oil pressure to flicker from 10 to 30 psi 69 to 207 kPa when going from upright to inverted flight During knife edge flights and zero g flights oil pressure may drop and the oil system ma...

Page 21: ...c Category only as ICAO Annex 16 grants an exception for airplanes specially designed for acrobatic purposes 2 6 WEIGHT LIMITS Max allowed empty weight Normal category 745 kg 1643lbs Acrobatic category 1 seat 701 kg 1546lbs 2 seats 665 kg 1466lbs Max allowed T O weight Normal category 950 kg 2095 lbs Acrobatic category 1 seat 820 kg 1808 lbs 2 seats 870 kg 1918 lbs Max allowed landing weight 950 k...

Page 22: ...rs If acrobatic maneuvers will be performed with a co pilot or passenger the pilot should ensure that the co pilot passenger has been properly briefed on the physiological effects of high g maneuvers This briefing should include accepted muscles straining and breathing techniques to counter the physiological effects of high g maneuvers During the flight the pilot should ensure the co pilot passeng...

Page 23: ...ng 80 148 VNE 90 up VA VNE 45 diving VS VNE reducethrottle 90 diving VS VNE reducethrottle 1 4 Loop climb 100 185 190 352 Looping 100 185 190 352 Stall turn 100 185 190 352 Aileron roll 80 148 VA fulldeflection Snap roll 80 148 140 259 tail slide 100 185 190 352 Spin VS Inverted spin VS Knife edge 150 278 10 s Inverted Flight VS 190 352 4 min 2 9 LOAD FACTOR 2 9 1 NORMAL FLIGHT 6 g 3 g Page Date 2...

Page 24: ...ucture is qualified up to 72 C 161 6 F Structure temperatures composite above 72 C 161 6 F are not permitted Not to exceed this temperature limit color specification for composite structure manufacturer document EA 03205 19 has to be complied with To check the temperature inside the cockpit potential green house effect a reversible temperature indicator STRUCTURAL OVERHEAT INDICATOR is applied on ...

Page 25: ...IS CATEGORY OR IN THE NORMAL CATEGORY ARE CONTAINED IN THE AIRPLANE FLIGHT MANUAL APPLICABLE RPM LIMITATION MUST BE OBSERVED THIS AIRPLANE IS CERTIFICATED on the rear instrument panel FOR VFR DAY OPERATION OPERATION IN KNOWN ICING CONDITIONS IS PROHIBITED F U E L near each filler cap AVGAS 100 100 LL OIL on the separate hatch upper cowling in both cockpits near selector valve handle NOSE DOWN NEUT...

Page 26: ...ar pump switch on the instrument panel in the rear cockpit ON OFF NO SMOKING in both cockpits USE OF HEADSET IS REQUIRED on the right side of both USE OF PARACHUTE IS RECOMMENDED instrument panels NO BAGGAGE on Lexan cover aft pilot s seat if installed MAGNETIC near Mag Dir Indicator DIRECTION INDICATOR CALIBRATION LOW RPM PROP HIGH RPM on RPM control unit in the rear cockpit LEAN MIXTURE RICH on ...

Page 27: ...ax min max Segment Horizontal Line V V Aileron roll 148 293 45 climbing 148 V Snap roll 148 259 90 up 293 V Tail slide 185 352 45 diving V V Spin V 90 diving V V Inverted spin V 1 4 Loop climb 185 352 Inverted flight V 352 Less than 4 min Loop 185 352 Knife edge 278 Stall turn 185 352 Less than 10 s S NE NE NE S NE S S NE S S km h km h km h Approved acrobatic maneuvers and recommended entry airspe...

Page 28: ...si 90 Psi or 55 Psi 95 Psi yellow arc 90 Psi 100 Psi or 95 Psi 115 Psi red line 100 Psi or 115 Psi OIL TEMPERATURE INDICATOR yellow arc 140 F green arc 140 F 210 F yellow arc 210 F 245 F red line 245 F CYLINDERHEAD TEMPERATURE INDICATOR yellow arc 150 F green arc 150 F 435 F yellow arc 435 F 500 F red line 500 F RPM INDICATOR green arc 700 RPM 2400 RPM yellow arc 2400 RPM 2700 RPM red line 2700 RP...

Page 29: ...he particular kind of operation indicated NORMAL ACROBATIC 1 seat 2 seats COMMUNICATION 1 Transceiver VHF 1 1 1 ELECTRICAL POWER 1 Battery 1 1 1 2 Alternator 1 1 1 3 Ammeter 1 1 1 FLIGHT CONTROL SYSTEM 1 Elevator trim control 1 1 1 2 Stall warning 1 1 1 FUEL 1 Boost pump 1 1 1 2 Fuel quantity indicator 2 2 2 3 Manifold pressure 1 1 1 4 Fuel flow indicator 1 1 1 5 Fuel pressure 0 0 0 LIGHT 1 Wing t...

Page 30: ...that either the equipment or system or both were not required for type certification for that kind of operation Either equipment or systems in addition to those listed above may be required by the national operating regulations The asterisks used in the above list mean that latest national aviation regulations must be observed in determining whether the equipment and or system are required Accordi...

Page 31: ...f Roll 3 4 3 2 2 Engine Failure immediately after Take off 3 4 3 2 3 Engine Failure during Flight Restart Process 3 4 3 2 4 Oil System Malfunction 3 5 3 2 5 Alternator Failure 3 5 3 3 FORCED LANDINGS 3 5 3 3 1 Emergency Landing without Engine Power 3 5 3 3 2 Precautionary Landing with Engine Power 3 5 3 4 FIRES 3 6 3 4 1 During Start on Ground 3 6 3 4 2 If Engine Fails to Start 3 6 3 4 3 Engine Fi...

Page 32: ...3 2 Page Date 20 April 2002 Section 3 Emergency Procedures Pilot s Operating Handbook EXTRA 300L Left blank intentionally ...

Page 33: ...rst transmission There after the ground station should be kept informed of the progress of the flight and of any changes or developments in the emergency Three basic rules apply to most emergencies and should be observed by each aircrew member 1 Maintain aircraft control 2 Analyze the situation and take proper action 3 Land as soon as possible as soon as practical The meaning of as soon as possibl...

Page 34: ...nt 15 Knots 27 km h 3 2 OPERATIONALCHECKLIST 3 2 1 ENGINE FAILURE DURING TAKE OFF ROLL 1 Throttle IDLE 2 Brakes APPLY 3 Mixture IDLE CUT OFF 4 Ignition switch OFF 5 Master switch OFF 3 2 2 ENGINE FAILURE IMMEDIATELY AFTER TAKE OFF Stall speed 60 KIAS 111 km h 1 Airspeed 80 KIAS 148 km h 2 Mixture IDLE CUT OFF 3 Fuel shutoff valve OFF Pull Turn 4 Ignition switch OFF 5 Master switch OFF 6 Forced lan...

Page 35: ...w voltage monitor CHECK INDICATION 3 Red light off CONTINUE FLIGHT If red light illuminates again 4 Land AS SOON AS PRACTICAL 3 3 FORCED LANDINGS 3 3 1 EMERGENCY LANDING WITHOUT ENGINE POWER 1 Seat belts shoulder harnesses SECURE 2 Airspeed 80 KIAS 148 km h 3 Mixture IDLE CUT OFF 4 Fuel shutoff valve OFF Pull Turn 5 Ignition switch OFF 6 Master switch OFF 7 Touchdown SLIGHTLY TAIL LOW 8 Brakes OPT...

Page 36: ... for one minute 4 Engine SHUT DOWN 5 After engine stop ABANDON aircraft and inspect for damage 6 Fire EXTINGUISH using fire extinguisher if available W A R N I N G Risk of burns due to flames shooting out Do not open engine compartment access doors while engine is on fire 3 4 2 IF ENGINE FAILS TO START 1 Cranking CONTINUE 2 Throttle FULL OPEN 3 Mixture IDLE CUT OFF 4 Fuel shutoff valve OFF Pull Tu...

Page 37: ...nearest airfield With extremely rapid ice build up select a suitable off airport landing field 3 6 UNINTENTIONAL SPIN Refer to section 4 Normal Procedures acrobatic maneuver spin recovery 3 7 MANUALBAIL OUT When in an emergency situation that requires abandoning the aircraft and while wearing a parachute which is at least strongly recommended for acrobatics 1 Informyourpassenger 2 Reduce speed to ...

Page 38: ... O T E If canopy fails to open break the canopy 6 Aircraft EVACUATE ASAP 3 9 ELEVATOR CONTROL FAILURE In case of elevator control failure the aircraft can be flown with the elevator trim In this case trim nose up to the desired speed and control horizontal flight or descend with engine power For landing trim nose up and establish a shallow descend by adjusting throttle To flair the plane gently in...

Page 39: ...4 4 2 CHECKLIST PROCEDURES 4 4 4 3 STARTING PROCEDURES 4 6 4 3 1 Cold Engines 4 6 4 3 2 Hot Engines 4 6 4 4 TAXIING THE AIRCRAFT 4 6 4 5 TAKE OFFPROCEDURE 4 7 4 5 1 BeforeTake Off 4 7 4 5 2 Take Off 4 7 4 6 CLIMB 4 7 4 7 CRUISE 4 7 4 8 LANDINGPROCEDURES 4 8 4 8 1 Descent 4 8 4 8 2 Approach 4 8 4 8 3 Before Landing 4 8 4 8 4 Normal Landing 4 8 4 9 GO AROUND 4 9 4 10 SHUTDOWN 4 9 4 11 LEAVING THEAIR...

Page 40: ...4 2 Page Date 20 April 2002 Section 4 Normal Procedures Pilot s Operating Handbook EXTRA 300L Left blank intentionally ...

Page 41: ...48 85 157 90 167 onFinal 72 133 74 137 78 144 Go AroundSpeed 90 167 95 176 100 185 Recommended Airspeed For Flight In Rough Air max VA 158 293 158 293 140 259 Max Demonstrated Cross WindComponent 15 kts 27 15 kts 27 15 kts 27 4 0 2 CHECKLIST AND PROCEDURES This handbook contains the checklist and procedures to operate the aircraft in normal and acrobatic operation The pilot should be familiar with...

Page 42: ...ter switch OFF 7 Fuel selector ACRO CENTER TANK N O T E Although safe operation does not require the use of the tanks in a specific sequence it is recommended to set fuel selector to ACRO CENTER TANK position 2 Empennage 1 All round inspection canopy surfaces stabilizers elevator trim tab rudder and tailwheel CHECK 2 Horizontal stabilizer attachment bols CHECK FOR FREEPLAY BY MOVING THE TIP OF THE...

Page 43: ...F POSSIBLE WATER CHECKCLOSED 7 Exhaust silencer if installed CHECK FOR DAMAGE AND SECURE ATTACHMENT 5 Left wing 1 Left landing gear wheel and brakes CHECK 2 Fuel quantity CHECK 3 Fuel tank filler cap CHECK 4 Pitot cover REMOVE 5 Trailing edge CHECK 6 Aileron freedom of movement and security CHECK 6 Before starting engine 1 Preflight inspection COMPLETE 2 Passenger briefing COMPLETE 3 Parachute han...

Page 44: ...lease the ignition switch back to BOTH 8 Move mixture control slowly and smoothly to FULL RICH 9 Check the oil pressure gauge If minimum oil pressure is not indicated within 30 seconds shut off the engine and determine trouble 4 3 2 HOT ENGINES Because of the fact that the fuel percolates and the system must be cleared of vapor it is recommended to use the same procedure as outlined for cold engin...

Page 45: ...tion Turn boost pump ON check indicator movement on the fuel flow gauge Check flight control free and correct Set trim to appropriate takeoff position half way nose down 4 5 2 TAKE OFF Set throttle smoothly to max and let the airspeed go up to 60 65 KIAS 111 120 km h A light pressure on the stick lifts the tail to horizontal position Rotate the aircraft at 65 KIAS 120 km h On reaching climb speed ...

Page 46: ...RICH 3 Airspeed reduce to approach speed 4 Propeller set to low pitch HIGH RPM N O T E It is recommended to set the RPM to 2400 during approach and landing in order to avoid unnecessary noise In case of Go Around RPM control must be set to max RPM before applying po wer 4 8 3 BEFORE LANDING 1 Landing approach proceed 2 Airspeed on final maintain 78 KIAS 144 km h 3 Elevator trim adjust N O T E Stal...

Page 47: ... altitude and airspeed are reached Proceed as follows 1 RPM control HIGH RPM Full forward 2 Throttle OPEN Take off power 3 Airspeed Minimum 90 KIAS 167 km h rotate to go around altitude 4 10 SHUTDOWN 1 Boost pump OFF 2 Engine Run for 1 min at 1000 RPM 3 Dead cut check Perform 4 Avionic master switch OFF if installed 5 Mixture IDLE CUT OFF 6 Ignition switch OFF 7 Master switch OFF 4 11 LEAVING THE ...

Page 48: ...ighpermissibleloadfactorsoftheairplanemayexceedtheindividualphysiological limits of pilot or passenger This fact must be considered when pulling or pushing high g s 4 12 2 MANEUVERS W A R N I N G Particular caution must be exercised when performing maneuvers at speeds above VA 158 KIAS 293 km h Large or abrupt control inputs above this speed may impose unacceptably high loads which exceed the stru...

Page 49: ...on snap rolls Watch VA 158 KIAS 293 km h for aileron rolls with max deflection Snap rolls should not be performed at speeds above 140 KIAS 259 km h Segment 1 4 loop climbing The minimum recommended speed is 100 KIAS 185 km h If the maneuver is to be followed by a vertical line a higher entry speed is required depending on the expected length of the line A complete loop can be performed at speeds a...

Page 50: ... E If ever disorientation should occur during spins normal or inverted one method always works to stop the spin Poweridle Kick rudder to the heavier side this will always be against spin direction Take hands off the stick The spin will end after 1 2 turn The plane will be in a steep dive in a side slip Recovery to normal flight can be performed easily N O T E After six turns of spinning the altitu...

Page 51: ...L 5 3 5 1 1 Performance Charts 5 3 5 1 2 Definitions of Terms 5 3 5 1 3 Sample Problem 5 3 5 2 ISA CONVERSION 5 5 5 3 AIRSPEED CALIBRATION 5 6 5 4 STALL SPEED 5 7 5 5 TAKE OFF PERFORMANCE 5 8 5 6 RATE OF CLIMB PERFORMANCE 5 9 5 7 TIME TO CLIMB FUEL TO CLIMB 5 10 5 8 RANGE AND ENDURANCE 5 11 5 9 FUEL CONSUMPTION 5 12 5 10 CRUISE PERFORMANCE 5 13 5 11 LANDING PERFORMANCE 5 14 ...

Page 52: ...5 2 Page Date 20 April 2002 Pilot s Operating Handbook EXTRA 300L Section 5 Performance Left blank intentionally ...

Page 53: ...uired for the particular flight 5 1 1 Performance Charts Performance data are presented in tabular or graphical form to illustrate the effect of diffe rent variables Sufficiently detailed information are provided in the tables so that conservative values can be selected and used to determine the particular performance figure with reasonable accuracy All speeds in this chapter are Indicated Air Spe...

Page 54: ...al CRUISE Cruise Altitude and Power Setting should be determined for most economical fuel consumption and several other considerations In an altitude of 8000 ft 2438 m and a Power Setting of 65 a Fuel Consumption of 52 L H 13 7 US Gal H and 3 25 NM L 12 3 NM US Gal can be obtained by Fig 5 9 RANGE AND ENDURANCE Fig 5 8 presents Range and Endurance values for a T O Weight of 950 kg 2095 lbs includi...

Page 55: ...Page Date 20 April 2002 5 5 Section 5 Performance Pilot s Operating Handbook EXTRA 300L 5 2 ISA CONVERSION ISA Conversion of pressure altitude and outside air temperature ...

Page 56: ...5 6 Page Date 20 April 2002 Pilot s Operating Handbook EXTRA 300L Section 5 Performance 5 3 AIRSPEEDCALIBRATION N O T E Indicated airspeed assumes zero instrument error Page Date 16 March 2009 ...

Page 57: ...RWARD C G STALL SPEEDS ANGLE OF BANK WEIGHT CATEGORY 0 30 45 1g 1 15 g 1 41 g kg lbs KIAS km h KIAS km h KIAS km h 950 Normal 60 65 72 2095 111 120 133 870 ACRO 2 seat 57 61 68 1918 106 113 126 820 ACRO 1 seat 55 59 65 1808 102 109 120 Max altitude loss during stall recovery is approximately 100 ft 30 m Page Date 16 March 2009 ...

Page 58: ... ft m ft lbs km h 950 65 SL 96 315 207 679 115 377 248 813 133 436 285 935 2095 120 2000 610 115 377 248 814 138 453 298 978 160 525 342 1122 4000 1219 138 453 298 978 166 545 357 1171 192 630 410 1345 6000 1829 166 545 358 1175 199 653 429 1407 230 755 492 1614 870 62 SL 78 256 167 548 93 305 200 656 107 351 230 755 1918 115 2000 610 94 308 200 656 112 367 240 787 128 420 276 906 4000 1219 112 36...

Page 59: ...Page Date 20 April 2002 5 9 Section 5 Performance Pilot s Operating Handbook EXTRA 300L 5 6 RATEOFCLIMBPERFORMANCE Page Date 16 March 2009 ...

Page 60: ...UEL TO CLIMB EXAMPLE WEIGHT 850 KG 1874 LBS ALT 2000 ft ISA 8000 ft ISA TIME TO CLIMB 3 1 min FUEL TO CLIMB 4 4 ltr 1 16 US Gal WEIGHT KG LBS 2095 lbs 1654 lbs 1874 lbs 2029 lbs 1544 1654 1764 1874 1985 2095 LTR US GAL 0 53 1 59 2 64 3 70 4 76 5 81 FUEL TO CLIMB CONDITIONS MAX CONT POWER CLIMB AT VY SPEED ISA ...

Page 61: ...ook EXTRA 300L 5 8 RANGEANDENDURANCE CONDITION T O WEIGHT 950 KG 2095 LBS TOTAL FUEL CAP 171 LTR 45 13 US GAL INCL WARM UP T O 5 LTR 1 3 US GAL RESERVE 21 LTR 5 5 US GAL UNUSABLE FUEL 5 5 LTR 1 45 US GAL T O FROM SL AND MAX T O POWER CLIMB TO CRUISING ALTITUDE ISA CONDITIONS ...

Page 62: ...ook EXTRA 300L Section 5 Performance 5 9 FUELCONSUMPTION EXAMPLE PA 8000 ft ISA POWER SETTING 65 FUEL CONSUMPTION 52 LTR HRS 13 7 GAL HRS 3 25 NM LTR 12 3 NM GAL 15 1 13 2 11 4 9 5 7 6 5 7 3 8 1 9 NM GAL 23 8 21 1 18 5 15 9 13 2 10 6 7 9 5 3 2 6 GAL HOUR ...

Page 63: ...onomy 8000 2700 21 8 77 231 73 4 19 4 179 5 332 156 289 1 79 314 582 Power 2438 2675 21 5 75 225 71 9 19 0 177 8 329 155 287 1 82 318 589 Power 2350 21 5 65 195 52 0 13 7 169 0 313 147 272 2 49 415 769 Economy 2050 21 4 55 165 43 0 11 4 159 3 295 139 257 2 99 472 874 Economy 2000 18 8 45 135 36 5 9 6 148 4 287 130 241 3 51 517 957 Economy 10000 2700 20 2 72 215 69 6 18 4 178 5 331 151 280 1 88 327...

Page 64: ...1 548 1798 185 607 586 1923 2095 167 2000 610 181 594 558 1831 188 617 580 1903 197 646 602 1975 4000 1219 192 630 592 1942 199 653 615 2018 208 682 639 2096 6000 1829 203 666 627 2057 211 692 652 2139 220 722 678 2224 870 85 SL 158 518 488 1601 164 538 507 1663 171 561 527 1729 1918 157 2000 610 165 541 518 1699 175 574 537 1762 181 594 558 1831 4000 1219 177 581 548 1798 185 607 570 1870 192 630...

Page 65: ...ntents Paragraph Page SECTION 6 WEIGHTAND BALANCEAND EQUIPMENT LIST 6 1 GENERAL 6 3 6 2 AIRCRAFT WEIGHING PROCEDURE 6 3 6 2 1 Owners Weight and Balance Record 6 4 6 3 CENTER OF GRAVITYCALCULATION SAMPLE PROBLEM 6 5 6 3 1 Sample 6 7 6 3 2 Weight and Balance Record Sheet 6 7 6 4 LOADING WEIGHTS AND MOMENTS 6 8 6 5 WEIGHTS AND MOMENTS LIMITS 6 9 6 6 EQUIPMENT LIST 6 10 ...

Page 66: ...6 2 Page Date 20 April 2002 Section 6 Weight and Balance and Equipment List Pilot s Operating Handbook EXTRA 300L Left blank intentionally ...

Page 67: ...that the aircraft is loaded properly 6 2 AIRCRAFTWEIGHINGPROCEDURE The aircraft weight is determined by weighing all three wheel loads simultaneously by three scales with the aircraft levelled Upperfuselagereferencelinehorizontal Datum line for weight arms x is the fire wall X1 distance fire wall main wheel X2 distance fire wall tail wheel XN distance fire wall item N XG distance fire wall Center ...

Page 68: ...plane 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 1 Owners Weight and Balance Record Enter below all weight change data from aircraft log book EXTRA300L SERIALNUMBER Date Descriptionof Weightchange Runningempty modification Added Removed weight Wt kg Arm cm Moment kg cm Wt kg Moment kg cm lbs ...

Page 69: ...1 LTR 120LTR 13 4 US GAL 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 3 6 90 198 5 37 81 5 60 132 3 86 4 190 5 7 90 198 5 90 198 5 8 90 198 5 37 81 5 90 198 5 PILOT ACRO TANK COPILOT WING TANK RearSeat Fuel Front Seat Fuel Position 51 LTR 101LTR 13 4 US GAL 26 7 US GAL kg lbs kg lbs kg lbs kg lbs 9...

Page 70: ...6 6 Page Date 20 April 2002 Section 6 Weight and Balance and Equipment List Pilot s Operating Handbook EXTRA 300L 6 3 CENTER OF GRAVITY CALCULATION SAMPLE PROBLEM ...

Page 71: ...ht 660 0 kg 1455 lbs 950 0 kg 2094 4lbs To find C G follow line Pilot Rear Seat from Empty Weight to 90 kg 198 5 lbs Point 1 Continue on line Copilot Front Seat to 90 kg Point 7 Now follow line Fuel via Point 8 51 L 13 5 US gal Acro Fuel to Point 9 101 L 26 6 US gal Fuel in Wing Tank FIND Weight 950 kg 2094 4lbs C G 75 4 cm 29 6inch 6 3 2 Weight and Balance Record Sheet WEIGHT ARM MOMENT EMPTYWEIG...

Page 72: ...36 80 176 16560 14344 7840 6758 85 187 17595 15240 8330 7180 90 198 18630 16137 8820 7603 FUEL MAX 171 LITER 45 1 US GAL FUEL ACRO CENTER TANK WINGTANK LITER KG KG x CM LITER KG KG x CM USGAL LBS LBS x IN USGAL LBS IN x LBS 9 2 4 6 5 14 3 182 157 10 2 6 7 2 15 9 360 313 20 5 3 14 4 31 8 420 365 20 5 3 14 4 31 8 721 629 25 6 6 18 0 39 7 529 459 40 10 6 28 8 63 5 1442 1257 30 7 9 21 6 47 6 638 553 6...

Page 73: ...ction 6 Weight and Balance and Equipment List Pilot s Operating Handbook EXTRA 300L 6 5 WEIGHTS AND MOMENTS LIMITS EXAMPLE At 790 KG 1741 LBS and 64000 kgcm the C G location is 81 0 cm 31 9 aft of ref datum Page Date 20 January 2016 ...

Page 74: ... 68 R Avstar Lyc PN 61M26404 1 Mech Fuel Pump Crane Lear Romec RG9080 J4A 0 86 0 15 R Lyc PN 62E22581 1 Mech Fuel Pump Hartzell Engine Tech 200F 5002 0 86 0 15 A Lyc PN 62E23186 1 El FuelPump Weldon Tool 8120 M or B8120 M 1 10 0 04 R 1 OilCooler Stewart Warner 8406 R 1 40 0 90 R 1 2 Oil Cooler Stewart Warner 8406 R 1 40 0 20 R 1 Low Temperature Extra 83301 0 20 0 01 A Breather Line Kit 1 Single Oi...

Page 75: ...eller P 880 41 1 10 0 91 A 7 Switches CutlerHammer div 0 28 1 63 R 7 Switches Kissling div 0 28 1 63 A 11 Circuit Breaker Potter Brumfield div 0 50 1 60 R 11 Circuit Breaker ETA or Klixon div 0 30 1 60 A 1 Main Bus Fuseholder MTA 03 00360 0 03 0 02 O 1 Main Bus Strip Fuse MTA 02 00300 O 40 Amps 1 PCB Auto Fuse EXTRA 83290 1 0 01 0 03 O 1 Fuel Cont Probe VDO 226 801 015 001 G 0 12 0 49 R Wing Tank ...

Page 76: ... O or Bendix or Jaeger or Century 1 Accelerometer EZE Technologies DA 55 0 16 1 60 O 1 ELT and Antenna Pointer 3000 10 0 90 2 60 O 1 ELT System ARTEX ME 406 1 42 2 60 A 1 Turn Bank Ind United Instruments 9501 2 TSO C3b 0 55 1 63 O 1 Turn Bank Ind Castleberry C101 TSO C101T 0 55 1 63 O 1 Horizon electric digital RC Allen RCA 2600 2 0 tilt 0 24 1 63 O 1 Horizon electric digital RC Allen RCA 2600 2 0...

Page 77: ... 62 A metric 1 Vertical Speed Ind United Instruments UI7030 M C 194 0 35 1 62 A metric 1 Vertical Speed Ind United Instruments UI7030C 27 0 35 1 62 A 1 Vertical Speed Ind Mikrotechna Praha LUN 1144 B0B1 0 40 1 61 A fpm 1 Vertical Speed Ind Mikrotechna Praha LUN1144 F0B1 0 40 1 61 A m s 1 EGT CHT Westach 2 DA 1 0 07 1 62 O 1 EGTProbe Westach 712 2 DWK 0 06 0 37 O 1 CHTProbe Westach 712 7 DK 0 05 0 ...

Page 78: ...eviation Ind Garmin MidContinent GI 102A 0 64 1 54 O 1 Course Deviation Ind Garmin MidContinent GI 106A 0 64 1 54 A 1 GPS Antenna Garmin AeroAntenna GA35 0 21 3 92 O 1 EFIS Aspen EFD1000PFD 1 31 1 60 O 1 Remote Sensor Module Aspen RSM 0 09 4 00 O 1 Transponder Bendix King KT 73 1 64 1 73 O 1 Transponder Bendix King KT 76A 0 89 1 75 O 1 Transponder Filser TRT 600 LAST 0 70 1 60 O 1 Transponder Fils...

Page 79: ...5 0 40 0 03 R 1 Starter Solenoid Switches Kidde 22735 0 40 0 03 R 1 Low Voltage Light OAK MS25041 2 0 02 1 63 R 1 Starter Engaged Light OAK MS25041 4 0 02 1 63 O 1 Ignition Switch TCM 10 357200 1 0 15 1 63 R 2 Wheel Cleveland 40 151 4 00 0 33 R 2 Main Wheel Tires Div 5 00 5 6PR 3 90 0 33 R 1 Tail Wheel 5 EXTRA steerable 5 50 5 23 R 1 Tail Wheel 6 Assy Special Products 5 90 5 23 A Soft Aviation Inc...

Page 80: ...k 60 L EXTRA 86713 010 LK 3 90 0 30 A 1 Fuel Selector Allen 6 S 122 0 19 0 73 R 1 Safety Cover EXTRA 86803 1 1 68 3 03 O Polycarbonate 1 DualPump EXTRA 86100 8 80 0 16 O Smoke System without Pumps 2 SmokeOilPump ITT Jabsco 8860 1203 3 60 0 10 O Inject and Refill 2 SmokeOilPump ITT Jabsco 23620 3003 4 40 0 10 O Inject and Refill 1 Smoke Oil Pump Johnson F3B 19 12V 2 00 0 05 O Injection 1 Smoke Oil ...

Page 81: ...dinal Flight Control System 7 5 7 5 3 Lateral Flight Control System 7 5 7 5 4 Directional Flight Control System 7 5 7 5 5 Secondary Control 7 5 7 6 INSTRUMENTATION 7 6 7 6 1 Instrument Panel Rear Cockpit 7 6 7 6 2 Instrument Panel Front Cockpit 7 8 7 7 LANDING GEAR 7 8 7 8 SEATS SEAT BELTS 7 9 7 9 CANOPY 7 9 7 10 POWER PLANT 7 10 7 10 1 Engine 7 10 7 10 2 Oil System 7 11 7 10 3 Engine Installation...

Page 82: ...7 2 Page Date 20 April 2002 Section 7 Description and Operation of Aircraft and Systems Pilot s Operating Handbook EXTRA 300L Left blank intentionally ...

Page 83: ...ord RISK appears on the red spot of this structural overheat indicator immediately and flying is prohibited When the structure cools down below this temperature limit the word RISK disappears and you may go on with the preflight checklist a Below 72 C 161 6 F b At 72 C 161 6 F or above The standard aircraft is designed to operate within a range of ambient air temperature from 20 C to 44 C 4 F to 1...

Page 84: ...span of each R L and L H wing The ailerons are supported at three points in spherical bearings pressed into aluminium brackets To reduce pilot s hand forces the hinge line of the ailerons is positioned 25 of the aileron depth at the root and 21 5 at the tip Furthermore the ailerons are equipped with spades to decrease pilot forces Ailerons are controlled via the center bracket To prevent flutter t...

Page 85: ...by sealed ball bearings from the torque tube to the ailerons The ailerons are statically as well as dynamically balanced dynamically with spades The ailerons are supported by lubricated sealed bearings 7 5 4 DIRECTIONAL FLIGHT CONTROL SYSTEM The dual rudder pedals with brake pedals are adjustable and operate the rudder through a cable system Springs keep the cables under tension when they are not ...

Page 86: ...oth cockpits Instruments and placards can be provided with markings in either metric or English units The colour markings in instruments follow US FAR part 23 recommendation see section 2 7 6 1 INSTRUMENT PANEL REAR COCKPIT For instrument panel arrangement of the rear cockpit refer to Fig 7 6 1 which includes standard and optional equipment marked as such Fig 7 6 1 1 2 3 4 5 6 15 14 13 12 11 10 9 ...

Page 87: ...er x 10 g meter x 11 Manifold pressure Fuel Flow x 12 Altimeter x 13 Master switch x 14 Fuel Quantity Acro Tank x 15 Fuel Quantity Wing Tank x 16 Vertical speed indicator x 17 Turn and bank indicator x 18 Artificial horizon x 19 Fuel pressure x 20 Intercom button x 21 Directional gyro x 22 RPM control Prop governor x 23 Mixture control x 24 Throttle lever x 25 Stick x 26 Radio button x 27 Fuel shu...

Page 88: ...d with the following positions 3 Airspeed indicator 12 Altimeter indicator 20 Intercom button 24 Throttle 25 Stick 26 Radio button 27 Fuel shutoff valve 7 7 LANDINGGEAR 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 The tail wheel has a solid rubber tire...

Page 89: ...nged in a way that one has to be closed to the right side the other one to the left During acrobatic maneuvers the seat belt system should be tightened firmly 7 9 CANOPY The canopy is manufactured in one section and can be manually operated by interior locking handles located on the left side on the canopy To open the canopy from inside proceed as follows Pull together the interior locking handles...

Page 90: ...eights The following accessories are included in the power plant installation Fuel Injector Bendix Magnetos Slick Alternator Electrosystems Starter B C Fuel pump GatesLear Shielded ignition system Propeller governor drive Transistor voltage regulator Overvoltage relay The engine is operated with the following manual controls Throttle control dual RPM control Fuel mixture control The propeller gove...

Page 91: ...es and oil grades refer to Section 1 7 7 10 3 ENGINEINSTALLATION The engine is supported by four shock mounts type LORD or 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 glass fibre carbonfibre reinforced epoxy The parts are fixed by a...

Page 92: ...s available 7 11 FUEL SYSTEM The fuel system consists of two separate independent tanks Acro center tank in the fuselage Wing tank LH and RH 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 ...

Page 93: ...ad conditions The masterswitch is located on the rear instrument panel Circuit protection against overvoltage is provided by the voltage regulator The maximum load taken from the alternator is 40 amp A 12 V leak proof battery is connected across the alternator output to stabilize the supply and to maintain all essential services in the event of an alternator failure and when the engine is not oper...

Page 94: ...e Date 20 April 2002 Section 7 Description and Operation of Aircraft and Systems Pilot s Operating Handbook EXTRA 300L Standard and Optional Equipment shown Page Date 08 October 2009 SCHEMATIC ELECTRICAL SYSTEM ...

Page 95: ...n of Aircraft and Systems Pilot s Operating Handbook EXTRA 300L 7 13 CABIN ENVIRONMENT CONTROL A ventilation system in the canopy on the left side is provided for the supply of fresh air to the cabin Left and right at the rear seat are eyeball type adjustable vents ...

Page 96: ...7 16 Page Date 20 April 2002 Section 7 Description and Operation of Aircraft and Systems Pilot s Operating Handbook EXTRA 300L Left blank intentionally ...

Page 97: ...A 300L SECTION 8 HANDLING SERVICING AND MAINTENANCE TABLE OF CONTENTS Paragraph Page SECTION 8 HANDLING SERVICING AND MAINTENANCE 8 1 INTRODUCTION 8 3 8 2 AIRPLANE INSPECTION PERIODS 8 3 8 3 PILOT CONDUCTED PREVENTIVE MAINTENANCE 8 3 8 4 ALTERATIONS OR REPAIR 8 3 8 5 SERVICING 8 4 8 6 GROUND HANDLING 8 4 ...

Page 98: ...8 2 Page Date 20 April 2002 Section 8 Handling Servicing and Maintenance Pilot s Operating Handbook EXTRA 300L Left blank intentionally ...

Page 99: ...a complete inspection after every 100 flights hours with a minor check after 50 hours The Airworthiness Authority may require other inspections by the issuance of airworthiness directives applicable to the aircraft engine propeller and components The owner is responsible for compliance with all applicable airworthiness directives and periodical inspections 8 3 PILOT CONDUCTED PREVENTIVE MAINTENANC...

Page 100: ... The tail wheel leg can be used as third point to tie down the airplane If the aircraft is parked in the open it must be protected against the effects of weather the degree of protection depending on severity of the weather conditions and the expected duration of the parking period When the airplane is parked in good weather conditions for less than a half day park the aircraft headed into the win...

Page 101: ...wer 6 p 906 Digital RPM Indicator 6 p 907 Long Range Wing Tank Capacity 6 p 908 Airtow Hook 8 p 909 Smoke System 6 p 910 ACRO III Category 8 p 911 Single Seat Canopy 4 p 912 FILSER TRT 600 Transponder 8 p 913 FILSER TRT 800 Transponder 8 p 914 GARMIN GTX 327 Transponder 6 p 915 GARMIN GTX 330 Transponder 8 p 916 BENDIX KINGKT 76ATransponder 6 p 917 BENDIX KINGKT 73Transponder 8 p 918 BECKERATC2000...

Page 102: ...andbook EXTRA 300L 924 ASPENEFD1000PILOTPFD 12 p 925 GARMINGNC420W 8 p 926 ARTEXME 406ELT 8 p 927 AIRPLANESREGISTEREDINBRAZILANDOPERATINGUNDERTHE AGÊNCIANACIONALDEAVIAÇÃOCIVILREQUIREMENTS 6 p 928 LANDINGLIGHTLED 4 p 929 GARMINGTN635 650 750 16 p Page Date 20 January 2016 ...

Page 103: ...ht of these Supplements and is responsible for edition of revisions The log of effective pages is found on the preceding pages of this Pilot s OperatingHandbook Each Supplement section e g steerable tailwheel covers only a single system device or piece of equipment and is a self contained miniature Pilot s Operating Handbook The owner is responsible for incorporating prescribed amendments and shou...

Page 104: ...9 4 Page Date 20 April 2002 Section 9 Supplements Pilot s Operating Handbook EXTRA 300L Left blank intentionally ...

Page 105: ... TAIL WHEEL Table of Contents Paragraph Page SECTION 901 STEERABLE TAIL WHEEL 901 1 GENERAL 901 3 901 2 LIMITATION 901 3 901 3 EMERGENCY PROCEDURES 901 3 901 4 NORMAL PROCEDURES 901 3 901 5 PERFORMANCE 901 3 901 6 WEIGHT AND BALANCE 901 3 901 7 DESCRIPTION OF THE SYSTEM 901 3 901 8 HANDLING SERVICING AND MAINTENANCE 901 4 ...

Page 106: ...901 2 Page Date 20 April 2002 Section 901 Steerable Tail Wheel Pilot s Operating Handbook EXTRA 300L Left blank intentionally ...

Page 107: ...be checked during the preflight check 901 5 PERFORMANCE Changes in flight performance due to installation of the steerable tailwheel are not notice able The given basic performance data under section 5 are still valid 901 6 WEIGHT AND BALANCE A change of the running empty weight and resulting C G position after installation of the steerable tailwheel is neglectable because of minor differences in ...

Page 108: ...rating Handbook EXTRA 300L 901 8 HANDLING SERVICING AND MAINTENANCE During 50 hour inspection the bearing steelsleeve has to be lubricated on the point of lubricating Additionally all parts of the tailwheel have to be inspected visually for deforma tions cracks and corrosion ...

Page 109: ...DAL ADJUSTMENT Table of Contents Paragraph Page SECTION 902 ELECTRIC PEDALADJUSTMENT 902 1 GENERAL 902 3 902 2 LIMITATIONS 902 3 902 3 EMERGENCY PROCEDURES 902 3 902 4 NORMAL PROCEDURES 902 3 902 5 PERFORMANCE 902 3 902 6 WEIGHT AND BALANCE 902 3 902 7 DESCRIPTION OF THE SYSTEM 902 3 902 8 HANDLING SERVICING AND MAINTENANCE 902 4 ...

Page 110: ...902 2 Page Date 20 April 2002 Section 902 Electric Pedal Adjustment Pilot s Operating Handbook EXTRA 300L Left blank intentionally ...

Page 111: ...hat purpose the pedals have to be adjusted to a position which allows full control inputs of rudder and aileron simultaneously as well as full rudder control input in conjunction with full applied brakes the pedals may be stepless adjusted inflight independently by two switches located on the instrument panel Pay attention to symmetrical adjustment of left and right pedal 902 5 PERFORMANCE Not aff...

Page 112: ...g Handbook EXTRA 300L attachment A full travel from the most rearward to the most forward position takes approxi mately 15sec 902 8 HANDLING SERVICING AND MAINTENANCE Not affected FORWARD BACK LH RH PEDALADJUST PEDAL ADJUST CONTROL SWITCHES CIRCUIT BREAKER 7 5A Page Date 8 October 2009 ...

Page 113: ...OMETER Table of Contents Paragraph Page SECTION 903 ELECTRONIC ACCELEROMETER 903 1 GENERAL 903 3 903 2 LIMITATIONS 903 3 903 3 EMERGENCY PROCEDURES 903 3 903 4 NORMAL PROCEDURES 903 3 903 5 PERFORMANCE 903 3 903 6 WEIGHT AND BALANCE 903 3 903 7 DESCRIPTION AND OPERATION OF THE SYSTEM 903 3 903 8 HANDLING SERVICING AND MAINTENANCE 903 9 ...

Page 114: ...903 2 Page Date 20 April 2002 Section 903 Electronic Accelerometer Pilot s Operating Handbook EXTRA 300L Left blank intentionally ...

Page 115: ...ction procedure according to the SERVICE MANUAL EA 300 L Instrument markings Electronic Accelerometer DSA 12 red range 12 g 10 g yellow range 10 g 8 g green range 8 g 8 g yellow range 8 g 10 g red range 10 g 12 g 903 3 EMERGENCY PROCEDURES Not affected 903 4 NORMAL PROCEDURES Not affected 903 5 PERFORMANCE Not affected 903 6 WEIGHT AND BALANCE Not affected 903 7 DESCRIPTION AND OPERATION OF THE SY...

Page 116: ...igned by an A as first character of every line The Current Extreme Values change if the Instantaneous Acceleration is greater than the last positive or lower than the last negative Current Extreme Value the positive or the negative The Current Extreme Values can be reset to 0g by pushing the buttons TOTAL EXTREME VALUE B Eventhough the two Current Extreme Values are reset to 0g there will remain a...

Page 117: ...tored in the long term memory inside the instrument Additionally time and date these Absolute Extreme Values occurred are stored These dates can be shown by the LC Display by pushing the buttons The Output of the Absolute Extreme Values is signed by a C as first character of the two LC Display lines The Absolute Extreme Values only change if an Instantaneous Value occurs that is greater than the p...

Page 118: ...two seconds after the power on of the instrument Both the Current Extreme Value and the Total Extreme Value are reset to 0g The LCD shows A 0 0 g A 0 0 g After two seconds the Instrument changes automatically into the Normal Operating Mode 2 THE NORMAL OPERATING MODE In the Normal Operating Mode the instrument outputs the Instantaneous Acceleration and the Current Extreme Values The Instantaneous ...

Page 119: ... Total extreme values These values are the maximums of positive and negative acceleration that occurred since the last reset of these values They are signed with a B as first charac ter of a line like the following example B 8 4 g B 4 2 g In case you want to reset these two values you have to press S2 and the instrument sets the Total Extreme Values to 0g and returns into the Normal Operating Mode...

Page 120: ...ternoon If you want to set the clock you have to push S1 for another time otherwise the instrument returns into the Normal Operating Mode 7 SETTING OF THE CLOCK push button five times S1 You can only set the clock if you know the right four digit code If you push S1 for five times the LC Display shows a request to enter the code You can change the code digit by pushing S2 To confirm your input of ...

Page 121: ...umbers The wrongly changed number is exchanged by its old value 903 8 HANDLING SERVICING AND MAINTENANCE If the absolute extreme value C indicates that the operating limits have been exceeded the manufacturer must be informed The battery inside which is used for the clock power supply backup is expected to have a lifetime of 5 to 10 years A weak battery can be exchanged by the manufacturer only ...

Page 122: ...903 10 Page Date 20 April 2002 Section 903 Electronic Accelerometer Pilot s Operating Handbook EXTRA 300L Left blank intentionally ...

Page 123: ...NSMITTER Table of Contents Paragraph Page SECTION 904 EMERGENCY LOCATOR TRANSMITTER 904 1 GENERAL 904 3 904 2 LIMITATIONS 904 3 904 3 EMERGENCY PROCEDURES 904 4 904 4 NORMAL PROCEDURES 904 6 904 5 PERFORMANCE 904 6 904 6 WEIGHT AND BALANCE 904 6 904 7 DESCRIPTION AND OPERATION OF THE SYSTEM 904 6 904 8 HANDLING SERVICING AND MAINTENANCE 904 7 ...

Page 124: ...Section 904 Emergency Locator Transmitter 904 2 Page Date 20 April 2002 Pilot s Operating Handbook EXTRA 300L Left blank intentionally ...

Page 125: ...utomatically after a crash or manual activity on the emergency frequencies of 121 5 MHz civilian and 243 0 MHz military 904 2 LIMITATIONS The operation limitations are not effected due to the installation of the POINTER 3000 ELT For the location and operation of the transmitter the following placards have to be attached in the aircraft ELT located here placard outside on the left fuselage board in...

Page 126: ...send a signal on the emergency frequencies of 121 5 MHz and 243 0 MHz B Control of the ELT If the aircraft receiver is operable listen on 121 5 MHz for ELT transmission Ensure that whip antenna is clear of obstruction Aircraft accident or forced landing A Manual activation B Warbling tone on headset 121 5 MHz D Removal of ELT from A C Stay close to the downed aircraft to permit easier spotting by ...

Page 127: ...e ANT recepta cle Extend antenna fully N O T E Do not use the AUTO position 5 Turn unit master switch to ON position E Best transmission may be obtained by Keeping antenna vertical Standing transmitter upright on a metallic surface such as an aircraft wing or stabilizer If terrain prohibits good transmission such as a deep valley or canyon place the transmit ter on the high ground or hold in hand ...

Page 128: ...itter is a POINTER 3000 ELT from the POINTER INC Tempe Arizona After an activation the necessity signal is transmitted on the 121 5 MHz and the 243 0 MHz for a period of 48 hours at 20 respectively 2 hours at 50 The inertia switch releases the necessity signal after a G force of 5 2 0 g in aircraft longitudinal axis and a duration of 11 5 0 milliseconds When properly installed parallel to the line...

Page 129: ... emergency situation would be forced landing with an impact insufficient to activate the Rolamite G switch AUTO used to arm the Pointer Portable for automatic activation by the G switch only OFF used to de activate transmitter after automatic activation by the G switch 904 8 HANDLING SERVICING AND MAINTENANCE Visually inspect the unit at regular intervals for cleanliness and secureness Check whip ...

Page 130: ...Section 904 Emergency Locator Transmitter 904 8 Page Date 20 April 2002 Pilot s Operating Handbook EXTRA 300L Left blank intentionally ...

Page 131: ...e of Contents Paragraph Page SECTION 905 EXTERNAL POWER 905 1 GENERAL 905 3 905 2 LIMITATIONS 905 3 905 3 EMERGENCY PROCEDURES 905 3 905 4 NORMAL PROCEDURES 905 3 905 5 PERFORMANCE 905 4 905 6 WEIGHT AND BALANCE 905 4 905 7 DESCRIPTION OF THE SYSTEM 905 5 905 8 HANDLING SERVICINGAND MAINTENANCE 905 5 Page Date 20 January 2016 ...

Page 132: ...Section 905 External Power 905 2 Page Date 20 April 2002 Pilot s Operating Handbook EXTRA 300L Left blank intentionally ...

Page 133: ...verheating the following placard has to be attached on the rear instrument panel with an indicator arrow to the receptacle 905 3 EMERGENCYPROCEDURES Notaffected 905 4 NORMALPROCEDURES The following starting procedures are recommended however the starting conditions may necessitate some variation from these procedures 1 PerformPre flightinspection 2 Set propeller governor control to High RPM positi...

Page 134: ...he propeller operating area Hold the canopy tight 9 Start engine 10 When engine fires release the ignition switch back to BOTH 11 Pull the external power plug from the board receptacle 12 Move mixture control slowly and smoothly to FULL RICH 13 Check the oil pressure gauge If minimum oil pressure is not indicated within 30 seconds shut off the engine and determine trouble 14 Masterswitch ON 905 5 ...

Page 135: ... located at the left side of the firewall above the starter relais For the avoidance of sparks this relais does not switch before a safe contact from plug to receptacle will be ensured During the engine start the master switch has to be switched in OFF position for the disconnection of the battery from the aircraft electric circuit 905 8 HANDLING SERVICINGANDMAINTENANCE Not affected Page Date 20 J...

Page 136: ...Section 905 External Power 905 6 Page Date 20 April 2002 Pilot s Operating Handbook EXTRA 300L Left blank intentionally ...

Page 137: ...ATOR Table of Contents Paragraph Page SECTION 906 DIGITALRPM INDICATOR 906 1 GENERAL 906 3 906 2 LIMITATIONS 906 3 906 3 EMERGENCYPROCEDURES 906 3 906 4 NORMALPROCEDURES 906 3 906 5 PERFORMANCE 906 4 906 6 WEIGHT AND BALANCE 906 4 906 7 DESCRIPTION AND OPERATION OF THE SYSTEM 906 4 906 8 HANDLING SERVICINGAND MAINTENANCE 906 6 ...

Page 138: ...Section 906 DigitalRPMIndicator 906 2 Page Date 20 April 2002 Pilot s Operating Handbook EXTRA 300L Left blank intentionally ...

Page 139: ...of the indicator is placarded with the unchanged engine RPM operating range Additionally the operating RPM ranges are indicated on the large green yellow and red LEDs These LEDs are located on the upper right corner of the indicator face ModelP100 230 635 00 max 2600RPM ModelP100 230 643 00 max 2700RPM 906 3 EMERGENCYPROCEDURES Notaffected 906 4 NORMALPROCEDURES The Normal Procedures have to be ch...

Page 140: ...WEIGHTANDBALANCE Notaffected 906 7 DESCRIPTIONANDOPERATIONOFTHESYSTEM The operation of the indicator is straight forward After power is supplied to the indicator the engine is started and the self tests are performed the default display of the engine RPM appears on the display The default display is insured via the use of internal timers that will restore the display to the current RPM even in the...

Page 141: ...l yellow indicator is illuminated when there is a difference of more than 50 RPM between the right and left tachometers This indicator also may flicker during extreme RPM excursions of the engine OPERATIONBUTTONS There are three panel buttons Each button has two modes of operation PRESS AND HOLD operation mode press and hold for more than 2 3 of a second Thisoperationmodeisplacardedaboveeachbutton...

Page 142: ...hanism exists to mask either tachometer from the display leaving the remaining tachometer to determine magneto ignition problems Quickly pressing and releasing the left button L causes the tachometer to mask the left tachometer Quickly pressing and releasing the right button R causes the tachometer to mask the righttachometer Dimmer DIM Quickly pressing and releasing the middle button DIM causes t...

Page 143: ...TY Table of Contents Paragraph Page SECTION 907 LONG RANGE WING TANK CAPACITY 907 1 GENERAL 907 3 907 2 LIMITATIONS 907 3 907 3 EMERGENCYPROCEDURES 907 3 907 4 NORMALPROCEDURES 907 3 907 5 PERFORMANCE 907 4 907 6 WEIGHT AND BALANCE 907 5 907 7 DESCRIPTION OF THE SYSTEM 907 6 907 8 HANDLING SERVICINGAND MAINTENANCE 907 6 Page Date 16 March 2009 ...

Page 144: ...Section 907 Long Range Wing Tank Capacity 907 2 Page Date 20 April 2002 Pilot s Operating Handbook EXTRA 300L Left blank intentionally ...

Page 145: ...0 Total fuel capacity 205 L 54 1 US Gallons Wingtank 154 L 2 x 77 L 40 7 US Gallons Acro Center Tank 51 L 13 4 US Gallons Usable fuel capacity in the system 199 5 L 52 7 US Gallons For acrobatic flight wing tanks must be empty Usable fuel capacity for acrobatic 45 5 L 12 0 US Gallons WEIGHT LIMITS Max allowed empty weight Normal category 716 kg 1578lbs PLACARD The existing FUEL SELECTOR VALVE plac...

Page 146: ...84 597 1105 Economy 2000 19 3 45 135 36 5 9 6 145 4 269 131 243 4 46 647 1199 Economy 8000 2700 21 8 77 231 73 4 19 4 179 5 332 156 289 2 25 397 736 Power 2438 2675 21 5 75 225 71 9 19 0 177 8 329 155 287 2 29 402 745 Power 2350 21 5 65 195 52 0 13 7 169 0 313 147 272 3 14 526 973 Economy 2050 21 4 55 165 43 0 11 4 159 3 295 139 257 3 78 598 1107 Economy 2000 18 8 45 135 36 5 9 6 148 4 287 130 241...

Page 147: ... KG KG x CM Litre KG KG x CM USGAL LBS LBS x IN USGAL LBS IN x LBS 9 2 4 6 5 14 3 182 157 10 2 6 7 2 15 9 360 313 20 5 3 14 4 31 8 420 365 20 5 3 14 4 31 8 721 629 25 6 6 18 0 39 7 529 459 40 10 6 28 8 63 5 1442 1257 30 7 9 21 6 47 6 638 553 60 15 9 43 2 95 3 2164 1886 35 9 2 25 2 55 6 746 648 80 21 1 57 6 127 0 2885 2514 40 10 6 28 8 63 5 855 742 100 26 4 72 0 158 8 3607 3144 45 11 9 32 4 71 4 96...

Page 148: ...al capacity Each side of the wing has a 2 diameter filler cap for gravity refuelling The long range tank has two compartments in either wing which are separated by a slosh rib Due to the interconnection the fuel level of the left and right integral tank will equalize during refuelling within reasonable time For max fuel capacity the first filled side has to be filled once again The wing tank can b...

Page 149: ...W HOOK Table of Contents Paragraph Page SECTION 908 AIRTOW HOOK 908 1 GENERAL 908 3 908 2 LIMITATIONS 908 3 908 3 EMERGENCY PROCEDURES 908 4 908 4 NORMAL PROCEDURES 908 4 908 5 PERFORMANCE 908 5 908 6 WEIGHT AND BALANCE 908 7 908 7 DESCRIPTION OF THE SYSTEM 908 7 908 8 HANDLING SERVICING AND MAINTENANCE 908 7 ...

Page 150: ...Section 908 Airtow Hook 908 2 Page Date 20 April 2002 Pilot s Operating Handbook EXTRA 300L Left blank intentionally ...

Page 151: ...replacement instruction UA 300 4 95 Air tow release TOST E 85 Glider MTOW of the glider 765Kg 1687 lbs Max air towing speed of the glider 152 km h or above Air tow cable and breaking piece weak links Length of the synthetic tow between 40 m 130 ft and 60 m 195 ft Ultimate load of the air tow max 850 kp 1875 lbs If tows with higher ultimate load are used a breaking piece weak links of max 850 kp 18...

Page 152: ...RACTICAL 908 4 NORMAL PROCEDURES Preflight inspection starting procedures take off procedure and the following climbing flight have to be carry out in accordance with Chapter 4 Normal procedure In addition to this procedures the following points have to be observed A PRIOR TO THE TAKE OFF A release test needs to be conducted to determine safe release operation The test shall be made on both aircra...

Page 153: ... paved level runway no wind takeoff weight of the towing aircraft 820Kg 1808lbs Liftoff speed T O 65 KIAS 120 Km h indicated Obstacle clearance speed over 15m 50ft 70 KIAS 130 Km h indicated For every 5 kts 9 km h headwind the takeoff T O distance can be decreased by 5 For every 2 kts 4 km h tailwind up to 10 kts 19 km h the T O distance is increased by 10 N O T E All values are valid for single p...

Page 154: ... m ft m ft m ft SL 176 577 287 942 196 643 320 1050 217 712 355 1165 240 787 393 1289 265 869 433 1421 291 955 476 1562 2000 610 205 673 334 1096 228 748 373 1224 253 830 414 1358 280 919 458 1503 309 1014 505 1657 340 1115 555 1821 4000 1219 239 784 391 1283 267 876 436 1430 296 971 484 1588 328 1076 535 1755 362 1188 591 1939 398 1306 650 2133 6000 1829 280 919 458 1503 313 1027 511 1677 347 113...

Page 155: ...orce glider with m 600 kg 1323 lbs PA 0 C 32 F OAT 10 C 50 F 20 C 68 F 30 C 86 F ft m ft min m s ft min m s ft min m s ft min m s ___SL 1280 6 5 1210 6 1 1150 5 8 1080 5 5 1000 305 1210 6 1 1145 5 8 1080 5 5 1015 5 2 2000 610 1140 5 8 1080 5 5 1010 5 1 950 4 8 3000 914 1080 5 5 1005 5 1 940 4 8 880 4 5 4000 1219 1005 5 1 935 4 7 870 4 4 810 4 1 5000 1524 935 4 7 870 4 4 800 4 1 740 3 8 6000 1829 8...

Page 156: ...t 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 908 8 HANDLING SERVICING AND MAINTENANCE Service and maintenance needs to be conducted in accordance with the latest operation handbook Typ E 85 of the manufacturer TOST GmbH Germany Additionally during the 100 h inspection the bowden cable and the release handle hav...

Page 157: ...e of Contents Paragraph Page SECTION 909 SMOKE SYSTEM 909 1 GENERAL 909 3 909 2 LIMITATIONS 909 3 909 3 EMERGENCYPROCEDURES 909 4 909 4 NORMALPROCEDURES 909 4 909 5 PERFORMANCE 909 5 909 6 WEIGHT AND BALANCE 909 5 909 7 DESCRIPTION OF THE SYSTEM 909 6 909 8 HANDLING SERVICINGAND MAINTENANCE 909 7 Page Date 20 January 2016 ...

Page 158: ...Section 909 Smoke System 909 2 Page Date 20 April 2002 Pilot s Operating Handbook EXTRA 300L Left blank intentionally ...

Page 159: ...flight control before you activate the smoke system 4 Recommended Manifold pressure min 20 Hg 5 The activation of the smoke system on ground is only allowable for a brief system test 6 The operation of the smoke system is not allowable for the standard exhaust 6 into 2 PC 63104 with mounted external silencer NSD GO3 606500 7 Wearing a parachute is strongly recommended Operating Markings Placards P...

Page 160: ...n OPEN 4 If smoke persists in the cockpit land AS SOON AS PRACTICAL 909 4 NORMALPROCEDURES The smoke system includes features for refilling the smoke tanks and smoke generation A REFILL A separate refill hose is delivered with the smoke system which has to be used for filling the smoke oil tanks from the paraffin oil supply cansister or barrel 1 Refill hose CONNECT hose nipple to quick connector a...

Page 161: ...e oil tank has to be checked accordingly B SMOKEGENERATION 1 Bad weather window and ventilation CLOSE 2 SMOKE ARM Switch ON 3 Manifold Pressure minimum 20 Hg 4 Switch in the throttle lever forsmokegeneration ON OFF C A U T I O N Smoke might enter the cockpit via the air vents during reverse maneuvers for example tail slide It is recommended to operate the smoke system only in forward flight 909 5 ...

Page 162: ...f An additional injection pump placed at the firewall within the engine compartment pumps the smoke oil from the floptube smoke oil tank through a solenoid valve and the injector nozzle into the hot exhaust gas to generate smoke The system consists of Main smoke oil tank with float switch Floptube smoke oil tank Refill pump in the pilot compartment with quick connector in the belly fairing Injecti...

Page 163: ...filling placed at the instrument panel Only 1 circuit breaker for pump and control placed at the instrument panel 909 8 HANDLING SERVICINGANDMAINTENANCE At every refilling Checkautomaticshut off Additionally during the 100h Check for the DUAL PUMP SYSTEM Check the system for leakage lines fittings tanks Check the smoke oil tanks for proper attachment Check the function of the solenoid valve Clean ...

Page 164: ...ndbook EXTRA 300L After each flight with activated Smoke System Clean the aircraft belly fairing and the rudder cable from smoke oil contamination N O T E The rudder cables might suffer from increased wear when they are covered with smoke oil and dust Page Date 20 January 2016 ...

Page 165: ...e of Contents Paragraph Page SECTION 910 ACRO III CATEGORY 910 1 GENERAL 910 3 910 2 LIMITATIONS 910 3 910 3 EMERGENCY PROCEDURES 910 4 910 4 NORMAL PROCEDURES 910 4 910 5 PERFORMANCE 910 5 910 6 WEIGHT AND BALANCE 910 6 910 7 DESCRIPTION AND OPERATION OF AIRCRAFT AND ITS SYSTEMS 910 8 910 8 HANDLING SERVICING AND MAINTENANCE 910 8 ...

Page 166: ...Section 910 Acro III Category 910 2 Page Date 20 April 2002 Pilot s Operating Handbook EXTRA 300L Left blank intentionally ...

Page 167: ...d empty weight 745 kg 1643 lbs Max allowed T O weight 950 kg 2095 lbs WEIGHT AND C G ENVELOPE Weight forward C G rear C G MTOW 950 kg 2095 lbs and below 67 1 cm 26 4 84 1 cm 33 1 LOAD FACTOR 6g 6g for two seat occupied MTOW 950 kg 2095 lbs OPERATINGPLACARDS VA 158 Kts Acro I II III or VA 293 km h Acro I II III near airspeed indicator VA 140 Kts Normal VA 259 km h Normal ACROBATIC 10 G 1 PILOT MTOW...

Page 168: ...0 111 62 115 65 120 65 120 Climb Vx 87 161 89 165 93 172 93 172 Vy 96 178 99 183 104 193 104 193 Recommended Normal ClimbSpeed 100 185 105 194 110 204 110 204 Max Cruise 185 343 185 343 185 343 185 343 Landing Approach 80 148 85 157 90 167 90 167 onFinal 72 133 74 137 78 144 78 144 Go AroundSpeed 90 167 95 176 100 185 100 185 Recommended Airspeed For Flight In Rough Air max VA 158 293 158 293 158 ...

Page 169: ...RWARD C G ANGLE OF BANK STALL SPEEDS WEIGHT CATEGORY 0 30 45 1g 1 15 g 1 41 g KIAS km h KIAS km h KIAS km h 950 kg Normal ACRO III 60 65 72 2095lbs 111 120 133 870 kg ACRO II 2 seat 57 61 68 1918lbs 106 113 126 820 kg ACRO I 1 seat 55 59 65 1808lbs 102 109 120 Max altitude loss during stall recovery is approximately 100 ft 30 m Page Date 16 March 2009 ...

Page 170: ...Section 910 Acro III Category 910 6 Page Date 20 April 2002 Pilot s Operating Handbook EXTRA 300L CENTER OF GRAVTITY CALCULATION SAMPLE PROBLEM 910 6 WEIGHTANDBALANCE ...

Page 171: ... 910 Acro III Category Page Date 20 April 2002 910 7 Pilot s Operating Handbook EXTRA 300L EXAMPLE At 790 KG 1741 LBS and 640000 kgcm the C G location is 80 0 cm 31 4 aft of ref datum WEIGHT AND MOMENT LIMITS ...

Page 172: ...n 910 Acro III Category 910 8 Page Date 20 April 2002 Pilot s Operating Handbook EXTRA 300L 910 7 DESCRIPTIONANDOPERATIONOFAIRCRAFTANDITSSYSTEMS Notaffected 910 8 HANDLING SERVICINGANDMAINTENANCE Notaffected ...

Page 173: ...OPY Table of Contents Paragraph Page SECTION 911 SINGLE SEAT CANOPY 911 1 GENERAL 911 3 911 2 LIMITATIONS 911 3 911 3 EMERGENCY PROCEDURES 911 3 911 4 NORMAL PROCEDURES 911 3 911 5 PERFORMANCE 911 3 911 6 WEIGHT AND BALANCE AND EQUIPMENT LIST 911 3 911 7 DESCRIPTION OF THE SYSTEM 911 3 911 8 HANDLING SERVICE AND MAINTENANCE 3 ...

Page 174: ...Section 911 Single Seat Canopy 911 2 Page Date 20 April 2002 Pilot s Operating Handbook EXTRA 300L Left blank intentionally ...

Page 175: ...r starting engine check front seat area and ensure seat belts and shoulder harness of front seat are completely removed or fastened and secured so that nothing can obstruct the freemovementofcontrols 911 5 PERFORMANCE Notaffected 911 6 WEIGHTANDBALANCEANDEQUIPMENTLIST Refer to the equipment list in section 6 911 7 DESCRIPTIONOFTHESYSTEM The single seat canopy has been designed to easily replace th...

Page 176: ...Section 911 Single Seat Canopy 911 4 Page Date 20 April 2002 Pilot s Operating Handbook EXTRA 300L Left blank intentionally ...

Page 177: ...TRT 600 TRANSPONDER Table of Contents Paragraph Page SECTION 912 FILSER TRT 600 TRANSPONDER 912 1 GENERAL 912 3 912 1 1 Front Panel Operation 912 3 912 1 2 System Operation 912 5 912 1 3 Error Reporting Fault Codes 912 7 912 2 LIMITATIONS 912 8 912 3 EMERGENCY PROCEDURES 912 8 912 4 NORMAL PROCEDURES 912 8 912 5 PERFORMANCE 912 8 ...

Page 178: ...Section 912 FILSER TRT 600 Transponder 912 2 Page Date 15 December 2005 Pilot s Operating Handbook EXTRA 300L Left blank intentionally ...

Page 179: ...uisition capability Furthermore the TRT 600 has a built in barometric pressure altitude coder in 100 ft increments NOTE Refer to latest edition of Filser TRT 600 Pilot s Operation Manual Doc No 03 200 010 11 to get familiar with the TRT 600 Transponder The following illustration of the front panel of the TRT 600 will assist the operator to understand this Mode S Transponder 912 1 1 FRONTPANELOPERA...

Page 180: ...O only ACS Mode A C and S full active ARROWS UP AND DOWN To activate the inserted SQUAWK CODE from the lower standby line to the upper active position the button with the UP AND DOWN ARROWS shall be pressed IDENT The IDENT push button causes the special position identification pulse SPI to be transmitted for a period of 18 seconds FID In the Standby Mode the Aircraft Identification Flight Identifi...

Page 181: ...st be pressed for more then two seconds or the AVIONIC MASTER switch must be placed to the OFF position ACS is the default operation mode and the transponder replies to Mode A C and S interrogations The pressure altitude will be displayed as Flight Level SQUAWK SELECTION Squawk selection is done with the four rotating knobs to provide 4096 identification codes The assignments of the knobs starting...

Page 182: ... the ATC controller requests it For switching off altitude reporting the MODE button has to be pressed until A S is displayed The altitude display shows FL to indicate that the altitude reporting is not active Now the transponder will reply on Mode C interrogations with Mode C frames only and Mode S interrogations with FL000 0000ft instead of the actual altitude IDENT PressingtheIDTpushbuttoncause...

Page 183: ...Z b The authorized service station should program a default FID that can be the tail number of the aircraft c The pilot has to change the FID manually if necessary 912 1 3 ERROR REPORTING FAULT CODES Thetransponder sreception transmission altitudeandpowersupplyaremonitoredperiodically This self testing routine is permanently active in the background If any error occurs due to an internal malfuncti...

Page 184: ...ta displayed means digital checksum error After a few seconds the display shows normal operating condition but with inhibited Mode S The transponder will work with Mode A C only You will need to consult an authorized service station to enter the ICAO aircraft address see TRT 600 Installation Manual Please consult your airworthinessauthorityfornationalprocedures N O T E If no valid ICAO 24 bit airc...

Page 185: ... TRT 800 TRANSPONDER Table of Contents Paragraph Page SECTION 913 FILSER TRT 800 TRANSPONDER 913 1 GENERAL 913 3 913 1 1 Front Panel Operation 913 3 913 1 2 System Operation 913 5 913 1 3 Error Reporting Fault Codes 913 7 913 2 LIMITATIONS 913 8 913 3 EMERGENCYPROCEDURES 913 8 913 4 NORMALPROCEDURES 913 8 913 5 PERFORMANCE 913 8 ...

Page 186: ...Section 913 FILSER TRT 800 Transponder 913 2 Page Date 15 December 2005 Pilot s Operating Handbook EXTRA 300L Left blank intentionally ...

Page 187: ...vides acquisition and extended squitter capability Furthermore the TRT 800 has a built in barometric pressure altitude coder in 100 ft increments N O T E Refer to latest edition of Filser TRT 800 Pilot s Operation Manual Doc No 03 210 010 11 to get familiar with the TRT 800 Transponder ThefollowingillustrationofthefrontpaneloftheTRT800 willassisttheoperatortounderstandthis ModeSTransponder 913 1 1...

Page 188: ...O only ACS Mode A C and S full active ARROWS UP AND DOWN To activate the inserted SQUAWK CODE from the lower standby line to the upper active position the button with the UP AND DOWN ARROWS shall be pressed IDENT The IDENT push button causes the special position identification pulse SPI to be transmitted for a period of 18 seconds FID In the Standby Mode the Aircraft Identification Flight Identifi...

Page 189: ... OFF must be pressed for more then two seconds or the AVIONIC MASTER switch must be placed to the OFF position ACS is the default operation mode and the transponder replies to Mode A C and S interrogations The pressure altitude will be displayed as Flight Level SQUAWK SELECTION Squawk selection is done with the four rotating knobs to provide 4096 identification codes The assignments of the knobs s...

Page 190: ...essary if the ATC controller requests it For switching off altitude reporting the MODE button has to be pressed until A S is displayed The altitude display shows FL to indicate that the altitude reporting is not active Now the transponder will reply on Mode C interrogations with Mode C frames only and Mode S interrogations with FL000 0000ft instead of the actual altitude IDENT PressingtheIDTpushbu...

Page 191: ...s ZZZZZZZ b The authorized service station should program a default FID that can be the tail number of the aircraft c The pilot has to change the FID manually if necessary 913 1 3 ERROR REPORTING FAULT CODES Thetransponder sreception transmission altitudeandpowersupplyaremonitoredperiodically This self testing routine is permanently active in the background If any error occurs due to an internal m...

Page 192: ...ata displayed means digital checksum error After a few seconds the display shows normal operating condition but with inhibited Mode S The transponder will work with Mode A C only You will need to consult an authorized service station to enter the ICAO aircraft address see TRT800 Installation Manual Please consult your airworthinessauthorityfornationalprocedures N O T E If no valid ICAO 24 bit airc...

Page 193: ...DER Table of Contents Paragraph Page SECTION 914 GARMIN GTX 327 TRANSPONDER 914 1 GENERAL 914 3 914 1 1 Mode Selection Keys 914 3 914 1 2 Code Selection 914 4 914 1 3 Keys for other GTX 327 Functions 914 4 914 2 LIMITATIONS 914 5 914 3 EMERGENCY PROCEDURES 914 6 914 3 1 Important Codes 914 6 914 4 NORMAL PROCEDURES 914 6 914 5 PERFORMANCE 914 6 ...

Page 194: ...Section 914 GARMIN GTX 327Transponder 914 2 Page Date 15 December 2005 Pilot s Operating Handbook EXTRA 300L Left blank intentionally ...

Page 195: ... attitudes N O T I C E Damage possible due to current peaks The GTX 327 should be turned off before starting or shutting down aircraft engine TheGTX327TransponderispoweredonbypressingtheSTBY ALTorONkeys orbytheAVIONIC MASTERswitch Afterpoweronastart uppagewillbedisplayedwhiletheunitperformsaselftest 914 1 1 MODESELECTIONKEYS OFF PowersofftheGTX327 STBY Powersonthetransponderinstandbymode Atpoweron...

Page 196: ...terference 7600 Loss of communications 7700 Emergency 7777 Military interceptor operations Never squawk this code 0000 Military use Not enterable Care should be taken not to select the code 7500 and all codes in the 7600 7777 range which trigger special indicators in automated facilities Only the code 7500 will be decoded as the hijack code An aircraft s transponder code if available is utilized t...

Page 197: ...include Contrast and Display Brightness depending on configuration refer to the screen description below SCREEN DESCRIPTION PRESSURE ALT Displays the altitude data supplied to GTX 327 in feet hundreds of feets i e flight level or meters depending on configuration FLIGHT TIME Displays the Flight Time which is controlled by the START STOP key COUNT UP TIMER Controlled by the START STOP and CLR keys ...

Page 198: ...URES 914 3 1 IMPORTANTCODES 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 199: ...PONDER 915 1 GENERAL 915 3 915 1 1 Mode Selection Keys 915 4 915 1 2 Code Selection 915 4 915 1 3 Keys for other GTX 330 Functions 915 5 915 1 4 Function Display 915 5 915 1 5 Configuration Mode 915 6 915 1 6 Altitude trend indicator 915 6 915 1 7 Failure Annunciation 915 6 915 2 LIMITATIONS 915 7 915 3 EMERGENCY PROCEDURES 915 7 915 3 1 Important Codes 915 7 915 4 NORMAL PROCEDURES 915 7 915 5 PE...

Page 200: ...Section 915 GARMIN GTX 330 Transponder 915 2 Page Date 15 December 2005 Pilot s Operating Handbook EXTRA 300L Left blank intentionally ...

Page 201: ...n standard conditions The unit also features flight timers The Traffic Information Service TIS is not available in this installation N O T E The GTX 330 owner accepts all responsibility for obtaining the proper license before using the transponder The coverage you can expect from the GTX 330 is limited to line of sight Low altitude or aircraft antenna shielding by the aircraft itself may result in...

Page 202: ... selection is done with eight keys 0 7 that provide 4 096 active identification codes Pushingoneofthesekeysbeginsthecodeselectionsequence Thenewcodewillnotbeactivated until the fourth digit is entered Pressing the CLR key will move the cursor back to the previous digit Pressing the CLR key when the cursor is on the first key of the code or pressing the CRSR key during code entry will remove the cu...

Page 203: ...the display Displayed data includes Pressure Altitude Flight Time Count Up timer Count Down timers In the Configuration Mode steps through function pages START STOP Starts and stops the Count Up Count Down and flight timers In the Configuration Mode steps through functions in reverse CRSR InitiatesstartingtimeentryfortheCountDowntimerandcancelstranspondercodeentry Returns cursortolastcodedigitwith...

Page 204: ...AST This page is only displayed if manual contrast mode is selected in Configuration Mode Contrast is controlled by the 8 and 9 keys DISPLAY This page is only displayed if manual backlighting mode is selected on Configuration Mode Backlighting is controlled by the 8 and 9 keys 915 1 5 CONFIGURATION MODE The configuration is normally set at time of installation including the unique Mode S aircraft ...

Page 205: ...3 EMERGENCYPROCEDURES 915 3 1 IMPORTANTCODES 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 206: ...Section 915 GARMIN GTX 330 Transponder 915 8 Page Date 15 December 2005 Pilot s Operating Handbook EXTRA 300L Left blank intentionally ...

Page 207: ... KT 76A TRANSPONDER Table of Contents Paragraph Page SECTION 916 BENDIX KING KT 76A TRANSPONDER 916 1 GENERAL 916 3 916 1 1 Code Selection 916 3 916 1 2 Reply Light 916 4 916 1 3 Testing the KT 76A 916 4 916 2 LIMITATIONS 916 4 916 3 EMERGENCY PROCEDURE 916 4 916 4 NORMAL PROCEDURE 916 5 916 4 1 Squawk Ident 916 5 916 5 PERFORMANCE 916 5 ...

Page 208: ...Section 916 BENDIX KING KT 76A Transponder 916 2 Page Date 15 December 2005 Pilot s Operating Handbook EXTRA 300L Left blank intentionally ...

Page 209: ...h a continuos report of your altitude which are automatically updated in 100 foot increments N O T E The KT 76A owner accepts all responsibility for obtaining the proper license before using the transponder 916 1 1 CODESELECTION TheIdentificationCodeselectionisdonewith4ATCRBSCodeSelectorKnobsthatprovide4 096 active identification codes Each of the 4 Code Selector Knobs selects a separate digit of ...

Page 210: ...EPLY LIGHT During normaloperation the flashingReplyLightindicates that theKT 76Aisfunctioning properly and replying to interrogations from ground radar Interrogations occur at 10 15 second intervals corresponding to each radar sweep Frequently the reply light will blink almost continuously meaning that the transponder is responding to interrogations from several radar stations 916 1 3 TESTING THE ...

Page 211: ...select knobs As soon as aircraft is airborne switch the function selector to ON Your KT 76A is now operating in Mode A or normalmode To operate in Mode C or altitude reporting mode turn the function selector to ALT if aircraft is equipped with altitude encoding equipment 916 4 1 SQUAWK IDENT When you are asked to ident by ATC briefly press the IDENT push button Your aircraft will be positively ide...

Page 212: ...Section 916 BENDIX KING KT 76A Transponder 916 6 Page Date 15 December 2005 Pilot s Operating Handbook EXTRA 300L Left blank intentionally ...

Page 213: ...NG KT 73 TRANSPONDER 917 1 GENERAL 917 3 917 1 1 Function Selector Knob 917 4 917 1 2 Code Selection 917 4 917 1 3 Buttons selectors for other KT 73 Functions 917 5 917 1 4 Function Display 917 6 917 1 5 Programming Mode 917 6 917 1 6 Air Ground Switching 917 6 917 1 7 FailureAnnunciation 917 7 917 2 LIMITATIONS 917 7 917 3 EMERGENCYPROCEDURES 917 7 917 4 NORMALPROCEDURES 917 7 917 5 PERFORMANCE 9...

Page 214: ...Section 917 BENDIX KINGKT73Transponder 917 2 Page Date 31 March 2009 Pilot s Operating Handbook EXTRA 300L Left blank intentionally ...

Page 215: ...ngthecode replysymbolandmodeofoperation theKT73screenwilldisplay pressurealtitude Thedisplayedpressurealtitudemaynotagreewiththeaircraft sbaro corrected altitude under non standard conditions TheTrafficInformationService TIS andAutomaticDependentSurveillance Broadcast ADS B is not available in this installation N O T E The KT 73 owner accepts all responsibility for obtaining the proper license bef...

Page 216: ...ions InadditionthedisplaybrightnesscanbemanuallyadjustedbyrotatingtheBRT knob GND Selects the Ground mode displaying GND in the altitude window When in Ground mode the transponder will not reply to ATCRBS ATCRBS Modes S All Call and Mode S only All Call interrogations It will continue to generate Mode S squitter transmissions and reply to discretely addressed Mode S interrogations ON Powers on the...

Page 217: ...dentification SPI Pulse for 18 seconds identifying your transponder return from others on the air traffic controller s screen The word IDT will appear in the left lower corner of the altitude window while the IDT mode is active When the Function Selector Knob in test mode TST pressing the IDT button will return the brightness to the default factory value VFR Momentarily pressing the VFR Pushbutton...

Page 218: ...s selected SBY SBY is displayed in the altitude window when SBY mode is selected by the Function Selector Knob In addition the ID code is displayed in the right window the ident window GND GND is only displayed on the left side altitude window when the aircraft is on ground The ID code is shown on the right side the ident window FLT IDT The FLT IDT is annunciated and the flight ID is illuminated i...

Page 219: ...de of the displays will illuminate 917 2 LIMITATIONS Not applicable 917 3 EMERGENCY PROCEDURES 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 917 4 NORMAL PROCEDURES Not applicable 917 5 PERFORMANCE ...

Page 220: ...Section 917 BENDIX KINGKT73Transponder 917 8 Page Date 31 March 2009 Pilot s Operating Handbook EXTRA 300L Left blank intentionally ...

Page 221: ...e of Contents Paragraph Page SECTION 918 BECKER ATC 2000 TRANSPONDER 918 1 GENERAL 918 3 918 1 1 Built in Test 918 4 918 1 2 Squawk selection 918 4 918 1 3 Mode A Operation 918 5 918 1 4 Mode A and C Operation 918 5 918 2 LIMITATIONS 918 5 918 3 EMERGENCY PROCEDURES 918 5 918 3 1 Important Codes 918 5 918 4 NORMAL PROCEDURES 918 6 918 5 PERFORMANCE 918 6 ...

Page 222: ...Section 918 BECKER ATC 2000 Transponder 918 2 Page Date 15 December 2005 Pilot s Operating Handbook EXTRA 300L Left blank intentionally ...

Page 223: ...i l l e n a p f o n o i t p e c x e h t i w p u m r a w e b u t r e t t i m s n a r T Y B S A e d o m o t s d n o p s e r r e d n o p s n a r T N O e d o c t e s e h t h t i w n o i t a g o r r e t n i d n a A e d o m o t s d n o p s e r r e d n o p s n a r T T L A n o i t a g o r r e t n i C e d o m n o i t a l u m i s n o i t a g o r r e t n i y b t s e t n i t l i u B T S E T p u t h g i l t s ...

Page 224: ...er simulates interrogation prompting a reply The reply indication is given by the reply lamp illuminating 918 1 2 SQUAWK SELECTION Squawk selection is done with the four rotating knobs to provide 4096 identification codes 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 0021 The VFR code...

Page 225: ...a special identification pulse SPI pulse being transmitted permitting instant identification of the aircraft on the ATC radar system 918 1 4 MODE A AND C OPERATION 1 Postion mode switch to ALT on ATC request only The transponder then responds with dialed code causing REPLY lamp to light up and additionally transmits the height of the aircraft to ATC 2 Press the IDENT button briefly when requested ...

Page 226: ...Section 918 BECKER ATC 2000 Transponder 918 6 Page Date 15 December 2005 Pilot s Operating Handbook EXTRA 300L 918 4 NORMALPROCEDURES Notapplicable 918 5 PERFORMANCE Notapplicable ...

Page 227: ...nd indicators 919 4 919 1 2 Switching on the unit pre flight check 919 4 919 1 3 Squawk selection 919 5 919 1 4 Flight operation in Mode A transponder reply code only 919 7 919 1 5 Flight operation in Mode A C reply code and altitude code 919 7 919 1 6 Squawk Ident 919 7 919 1 7 Test 919 7 919 1 8 Configuration Mode 919 8 919 2 LIMITATIONS 919 8 919 3 EMERGENCY PROCEDURES 919 8 919 3 1 Important C...

Page 228: ...919 2 Page Date 15 December 2005 Pilot s Operating Handbook EXTRA 300L Section 919 BECKER ATC 4401 Transponder Left blank intentionally ...

Page 229: ... Beacon System ATCRBS Its functionality includes replying to ATCRBS Mode A and Mode C interrogations It operates on radar frequencies receiving ground radar interrogations at 1030 MHz and transmitting a coded response of pulses to ground based radar on a frequency of 1090 MHz The ATC4401isequippedwithIDENTcapabilitythatactivatestheSpecialPositionIdentification SPI pulse N O T E The ATC 4401 owner ...

Page 230: ...C A e d o M d n a A e d o M n I 8 1 x o r p p a r o f e d o c y l p e r A e d o M e h t o t l a n o i t i d d a e s l u p m i n o i t a c i f i t n e d i C L e h t f o e n i l m o t t o b e h t n i s r a e p p a t d I e m i t s i h t g n i r u D s d n o c e s y a l p s i d E y a l p s i d C L e n i l 2 e n i l p o t n o i t a c i d n i e d o C e l b i s s o p e r a 7 7 7 7 o t 0 0 0 0 m o r f s e ...

Page 231: ...sor appears only in the code display and is indicated by the flashingdigit Ifnocursorisvisible thefirstdigitflashesafteraclockwiserotationandthe last digit after a counter clockwise rotation When the code is being changed in the ON or ALT position the transponder temporarily switches to the standby mode The active time of the cursor and the rate of flashing can be changed in the configuration mode...

Page 232: ...code b Pressing button F or G again within 3 seconds reactivates the previously set reply code N O T E When the unit is delivered the store buttons are not assigned a code This means that if these buttons are pressed for 0 5 seconds is shown in the code display and the transponder then switches back to the previously active code IMPORTANT CODES 1200 The VFR code for any altitude in the US Refer to...

Page 233: ...on alpha charlie or charlie switch the transponder to ALT using mode switch A 3 The transponder replies using the code set and in response to mode C requests it tansmits the flight level of the aircraft to ATC A triangle on the left next to the code signals the transponder replies 919 1 6 SQUAWK IDENT After a squawk ident request from ATC press Ident button IDT D briefly This transmits an addition...

Page 234: ...0 in the top line of the display Switch OFF the transponder at such E fault indications 919 1 8 CONFIGURATION MODE The configuration Mode is used to set the unit on the ground and must not be called up in flight Refer to BECKER s Pilot s Guide for further information 919 2 LIMITATIONS Not applicable 919 3 EMERGENCY PROCEDURES 919 3 1 IMPORTANT CODES 7600 Loss of communications 7500 Hijacking 7700 ...

Page 235: ... Switching on the Unit pre flight check 920 4 920 1 3 Display 920 5 920 1 4 Squawk Selection 920 5 920 1 5 Squawk Ident 920 6 920 1 6 Selftests of the Unit BITs 920 6 920 1 7 Selection Mode 920 7 920 1 8 Flight Operation in Mode A C S reply code and altitude code 920 9 920 1 9 VFR Code Activation 920 10 920 1 10 Configuration Mode 920 10 920 2 LIMITATIONS 920 10 920 3 EMERGENCY PROCEDURES 920 10 9...

Page 236: ...920 2 Page Date 31 March 2009 Pilot s Operating Handbook EXTRA 300L Section 920 BECKER BXP 6401 Transponder Left blank intentionally ...

Page 237: ...dar BeaconSystem ATCRBS ItsfunctionalityincludesreplyingtoATCRBSModeA CandModeS interrogations It operates on radar frequencies receiving ground radar interrogations at 1030 MHz and transmitting a coded response of pulses to ground based radar on a frequency of 1090 MHz The BXP6401isequippedwithIDENTcapabilitythatactivatestheSpecialPositionIdentification SPI pulse N O T E The BXP 6401 owner accept...

Page 238: ...f o e d o m y r a t o r s g n i t t e s e g n a h c o t h c t i w s y r a t o R n r u t r e p s p e t s 6 1 C n o t t u B n o t t u b h s u P B f o e d o m m o r f r o s g n i t t e s r o f t i g i d o t t i g i d m o r f p m u j o t h s u P t x e n e h t o t u n e m e n o y e k r e t n e n a s a d e s u y l l a r e n e g D T D I n o t t u b h s u P o t n o i t i d d a n i I P S r e i f i t n e d ...

Page 239: ...e standby mode until requested by the ground station ATC to transmit a code e g squawk alpha 6426 2 Using the rotary switch B and the button C set the 4 digit code requested by ATC as follows a Usingswitch C movethecursortotheparticulardigit Digits0to7canthenbesetusingtherotary switch B N O T E S Whilst settings are taking place the transmission branch of the transponder is inhibited to prevent un...

Page 240: ...oller Idt appearsinthebottomlineoftheLCdisplayduring this time 920 1 6 SELFTESTS OF THE UNIT BITS Thefollowingdifferenttestsareintegratedinthetransponderorcanbetriggeredatthetransponder 1 The IBIT Initiated Built in Test can be activated in any mode excluding the configuration mode withthepushof F and G atthesametime Theactionstartswiththeleadingedgeofthesecond pushed button The IBIT works as foll...

Page 241: ... Address Module If a flight plan exists it has to be checked which AI has to be used If a Flight Number is assigned it has to be entered If a Company Call Sign is mentioned this has to be entered To enter it see below ItwillbestoredintheEEPROMofthecontrolhead Inthiscasetheindicationonthedisplay changes to FN Flight Number If the Call Sign Tail Number is mentioned no change as it is the default set...

Page 242: ... spaces 8 Store the changes with STO button F For leaving the setting procedure without storing push the SEL button G N O T E Aircraft Identifier Flight Number consists of max 7 characters on the left hand side oriented No dashes or spaces shall be included If the FN con sists of less than 7 characters the remaining characters on the right side shall be filled with spaces SWITCHING BACK TO DEFAULT...

Page 243: ... inversion 10 sec is introduced if no action happens Nothing stored as long as F is not pressed N O T E It is possible to leave the setting procedure with SEL button G at any time and normal mode is available then Indication SEL on the display changes back to mode indication If STO button F was not used no change has been stored 920 1 8 FLIGHTOPERATIONINMODEA C S REPLYCODEANDALTITUDECODE 1 WhenATC...

Page 244: ...ecodedisplayandthetransponder then switches back to the previously active code 920 1 10 CONFIGURATION MODE The configuration mode is available from SBY mode only To get into configuration mode press button SEL G turn rotary encoder B until CFG appears in the bottom row of the display Refer to BECKER s Pilot s Guide for available options 920 2 LIMITATIONS Not applicable 920 3 EMERGENCYPROCEDURES 92...

Page 245: ...ing Placards 921 4 921 2 5 Instrument Markings 921 5 921 2 6 Maximum OperatingAltitude 921 5 921 3 EMERGENCYPROCEDURES 921 5 921 4 NORMALPROCEDURES 921 5 921 4 1 Noise Level 921 5 921 5 PERFORMANCE 921 6 921 5 1 Cruise Performance Chart Configuration 1 921 7 921 5 2 Range Configuration 1 921 8 921 5 3 Endurance Configuration 1 921 9 921 5 4 Cruise Performance Chart Configuration 2 921 10 921 5 5 R...

Page 246: ...921 2 Page Date 5 December 2008 Pilot s Operating Handbook EXTRA 300L Section 921 Lycoming AEIO 580 B1A Engine Left blank intentionally ...

Page 247: ...ng propellers 1 TypeMTV 9 B C C200 15 3 bladeconstantspeed 2 TypeMTV 14 B C C190 17 4 blade constant speed 3 TypeMTV 9 B C C198 25 3 bladeconstantspeed 921 2 LIMITATIONS The following data deviate from the values given in Section 2 of this handbook 921 2 1 Engine Limitations a Rotational Speed MaximumTake OffandMaximumContinuous 2700RPM N O T E Applicable RPM limitations approved for individual pr...

Page 248: ...raph 921 2 5 following rotational speed limitations applyfortheMTV 9 B C C198 25propeller MaximumTake Off andMaximumContinuous 2600RPM N O T E RPM limitation due to compliance with applicable noise protection requirements ICAO Annex 16 and FAR 36 However for non US registered airplanes an enhanced rotational speed limitation of 2700 RPM may be permissable when registered in the Acrobatic Category ...

Page 249: ...4 1 Noise Level ThenoiselevelwithsilencerGomolzigEA300 606000 6in1 andpropellerMTV 9 B C C198 25 at 2600 RPM has been established in accordance with ICAO Annex 16 as 77 8 dB A In addition The noise level with silencer Gomolzig EA300 606000 6 in 1 and propeller MTV 9 B C C 198 25 at 2600 RPM has been established in accordance with FAR 36 Appendix G incl Amdt 36 28 as 77 5 dB A No determination has ...

Page 250: ...rmanceChartsandrelatedDrawingshavebeenadaptedwithregardto thepowersettings Thepowersettingsareadjusted tomatchtheabsolutepowervaluesintheHP column of the Cruise Performance Chart presented in Section 5 of this handbook For this reason the values of the power setting column deviate from the common values 75 65 etc In the Cruise Performance Chart for configuration 2 the increased fuel capacity of th...

Page 251: ... 18 5 43 135 36 5 9 6 145 4 269 131 243 3 53 512 948 Economy 8000 2700 21 0 73 231 73 4 19 4 179 6 333 166 307 1 79 314 582 Power 2438 2675 20 7 71 225 71 9 19 0 177 8 329 156 289 1 82 318 589 Power 2350 20 6 62 195 52 0 13 7 169 0 313 147 272 2 49 415 769 Economy 2050 20 6 52 165 43 0 11 4 159 3 295 139 257 2 99 472 874 Economy 10000 2700 19 8 69 215 69 6 18 4 178 6 331 151 280 1 88 327 606 Power...

Page 252: ...921 8 Page Date 5 December 2008 Pilot s Operating Handbook EXTRA 300L Section 921 Lycoming AEIO 580 B1A Engine 921 5 2 Range Configuration 1 Page Date 19 April 2012 ...

Page 253: ...Page Date 5 December 2008 921 9 Pilot s Operating Handbook EXTRA 300L Section 921 Lycoming AEIO 580 B1A Engine 921 5 3 Endurance Configuration 1 Page Date 19 April 2012 ...

Page 254: ... 162 300 1 97 351 650 Power 1829 2500 22 2 71 225 69 8 18 4 174 3 323 156 289 2 19 377 698 Power 2200 22 2 62 195 50 5 13 3 165 6 307 149 276 3 00 493 913 Economy 2000 21 5 52 165 42 6 11 3 156 1 289 141 261 3 55 551 1020 Economy 2000 18 5 43 135 36 5 9 6 145 4 269 131 243 4 12 598 1107 Economy 8000 2700 21 0 73 231 73 4 19 4 179 6 333 166 307 2 08 367 680 Power 2438 2675 20 7 71 225 71 9 19 0 177...

Page 255: ...Page Date 5 December 2008 921 11 Pilot s Operating Handbook EXTRA 300L Section 921 Lycoming AEIO 580 B1A Engine 921 5 5 Range Configuration 2 Page Date 19 April 2012 ...

Page 256: ...921 12 Page Date 5 December 2008 Pilot s Operating Handbook EXTRA 300L Section 921 Lycoming AEIO 580 B1A Engine 921 5 6 Endurance Configuration 2 Page Date 19 April 2012 ...

Page 257: ... 3607 3144 45 11 9 32 4 71 4 964 836 120 31 7 86 4 190 5 4328 3771 50 13 2 36 0 79 3 1073 931 55 14 5 39 6 87 3 1182 1026 60 15 9 43 2 95 2 1290 1120 65 17 2 46 8 103 2 1399 1215 69 18 2 49 7 109 6 1487 1291 Also refer to the Equipment List in Section 6 which has been revised 921 7 DESCRIPTION The AEIO 580 B1A engine is characterized by the following performance data Rated power at 2700 RPM 315 HP...

Page 258: ...921 14 Page Date 5 December 2008 Pilot s Operating Handbook EXTRA 300L Section 921 Lycoming AEIO 580 B1A Engine Figure 921 1 Center Tank Versions Page Date 19 April 2012 ...

Page 259: ...9 US gal capacity configuration2 Ineachconfigurationthecentertanksarelocatedabovetheacrotank 1 having 9 L 2 4 US gal fuel quantity They are installed in the same place and in the same manner This includes the vent line 2 and the fuel filler 5 location However the steel tubes of the fuselage carryingthe60Ltankanditsmountinghavebeenreinforced Theconfiguration1fuelquantityprobe 3 is located in front ...

Page 260: ...921 16 Page Date 5 December 2008 Pilot s Operating Handbook EXTRA 300L Section 921 Lycoming AEIO 580 B1A Engine Page Date 19 April 2012 Left blank intentionally ...

Page 261: ...922 922 1 GENERAL 922 3 922 2 LIMITATIONS 922 3 922 2 1 Fuel 922 3 922 2 2 Weight Limits 922 3 922 2 3 Placards 922 3 922 3 EMERGENCYPROCEDURES 922 3 922 4 NORMALPROCEDURES 922 3 922 5 PERFORMANCE 922 4 922 5 1 Cruise Performance 922 4 922 5 2 Range 922 5 922 5 3 Endurance 922 6 922 6 WEIGHT AND BALANCE 922 7 922 7 DESCRIPTION OF THE SYSTEM 922 8 922 8 HANDLING SERVICINGAND MAINTENANCE 922 8 ...

Page 262: ...Section 922 Center Tank Increased Capacity 922 2 Page Date 5 December 2008 Pilot s Operating Handbook EXTRA 300L Left blank intentionally ...

Page 263: ...sable fuel capacity for acrobatic 67 L 17 7 US gal 922 2 2 Weight Limits Max allowed empty weight Normalcategory 729 kg 1607 lb Acrobatic category I 686 kg 1512 lb 922 2 3 Placards The following placards replace the existing placards in both cockpits nearselectorvalvehandle On the rear instrument panel next to the fuel quantity indicator 922 3 EMERGENCYPROCEDURES Notaffected 922 4 NORMALPROCEDURES...

Page 264: ...107 Economy 8000 2700 21 8 77 231 73 4 19 4 179 5 332 156 289 2 08 367 680 Power 2438 2675 21 5 75 225 71 9 19 0 177 8 329 155 287 2 12 371 687 Power 2350 21 5 65 195 52 0 13 7 169 0 313 147 272 2 90 485 898 Economy 2050 21 4 55 165 43 0 11 4 159 3 295 139 257 3 49 552 1022 Economy 2000 18 8 45 135 36 5 9 6 148 4 275 130 241 4 10 604 1119 Economy 10000 2700 20 2 72 215 69 6 18 4 178 5 331 151 280 ...

Page 265: ...Section 922 Center Tank Increased Capacity Page Date 5 December 2008 922 5 Pilot s Operating Handbook EXTRA 300L 922 5 2 Range ...

Page 266: ...Section 922 Center Tank Increased Capacity 922 6 Page Date 5 December 2008 Pilot s Operating Handbook EXTRA 300L 922 5 3 Endurance ...

Page 267: ... 14 3 182 157 10 2 6 7 2 15 9 360 313 20 5 3 14 4 31 8 420 365 20 5 3 14 4 31 8 721 629 25 6 6 18 0 39 7 529 459 40 10 6 28 8 63 5 1442 1257 30 7 9 21 6 47 6 638 553 60 15 9 43 2 95 3 2164 1886 35 9 2 25 2 55 6 746 648 80 21 1 57 6 127 0 2885 2514 40 10 6 28 8 63 5 855 742 100 26 4 72 0 158 8 3607 3144 45 11 9 32 4 71 4 964 836 120 31 7 86 4 190 5 4328 3771 50 13 2 36 0 79 3 1073 931 55 14 5 39 6 ...

Page 268: ... fuel filler 3 location However the tank is increased in down and rearward direction The steel tubes of the fuselage carrying the tank and the tank mounting are reinforced The fuel contents probe 4 has been changed while the indicator is still the same The total fuel capacity of the center tank is 60 L 15 9 US gal The total fuel capacity of the acro tank 1 is 9 L 2 4 US gal The usable fuel quantit...

Page 269: ...ONDER 923 1 GENERAL 923 3 923 1 1 Mode Selection Keys 923 4 923 1 2 Code Selection 923 4 923 1 3 Keys for other GTX 328 Functions 923 5 923 1 4 Function Display 923 5 923 1 5 Configuration Mode 923 6 923 1 6 Altitude trend indicator 923 6 923 1 7 FailureAnnunciation 923 6 923 2 LIMITATIONS 923 7 923 3 EMERGENCYPROCEDURES 923 7 923 3 1 Important Codes 923 7 923 4 NORMALPROCEDURES 923 7 923 5 PERFOR...

Page 270: ...Section 923 GARMIN GTX 328 Transponder 923 2 Page Date 5 December 2008 Pilot s Operating Handbook EXTRA 300L Left blank intentionally ...

Page 271: ... also features flight timers The Traffic Information Service TIS is not available in this installation N O T E The GTX 328 owner accepts all responsibility for obtaining the proper license before using the transponder The coverage you can expect from the GTX 328 is limited to line of sight Low altitude or aircraft antenna shielding by the aircraft itself may result in reduced range Range can be im...

Page 272: ...also respondstointerrogationsfromTCASequippedaircraft 923 1 2 CODESELECTION Codeselectionisdonewitheightkeys 0 7 providing4 096activeidentificationcodes Pushing one of these keys begins the code selection sequence Digits that are not yet entered appear as dashes The new code is activated when the fourth digit is entered Pressing the CLR Key moves the cursor back to the previous digit Pressing the ...

Page 273: ...nd Display if manual control and backlighting is selected in the installation configuration START STOP Starts and stops the Count Up Count Down and Flight timers CRSR Initiates starting time entry for the Count Down timer and cancels transponder code entry CLR Resets the Count Up Count Down and Flight timers Cancels the previous keypress during code selection and Count Down entry Returns cursor to...

Page 274: ...on configuration Contrast is controlled by the 8 and 9 keys DISPLAY Thispageisonlydisplayedifmanualbacklightingmodeisselectedduringinstallationconfiguration Backlighting is controlled by the 8 and 9 keys 923 1 5 CONFIGURATIONMODE The configurartion mode is not active TheGTX328 soptionsarenormallysetattimeofinstallation TorequestanychangesoftheGTX 328 parameters contact an authorized Garmin Aviatio...

Page 275: ... 3 EMERGENCYPROCEDURES 923 3 1 IMPORTANTCODES 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 NORMALPROCEDURES Notapplicable 923 5 PERFORMANCE Notapplicable ...

Page 276: ...Section 923 GARMIN GTX 328 Transponder 923 8 Page Date 5 December 2008 Pilot s Operating Handbook EXTRA 300L Left blank intentionally ...

Page 277: ...R OF GRAVITY 924 4 924 7 SYSTEM DESCRIPTION 924 4 924 7 1 General 924 4 924 7 2 Pilot Controls Overview 924 5 924 7 3 Power Control 924 5 924 7 4 Display Screen and Control Layout 924 6 924 7 5 Control Knobs 924 7 924 7 6 Setting Flight Instruments 924 7 924 7 7 Knob Sync Function 924 8 924 7 8 Hot Key Operation 924 8 924 7 9 Back Light Control 924 9 924 7 10 Map Range Control 924 10 924 7 11 Disp...

Page 278: ...Section 924 ASPENEFD1000PILOTPFD 924 2 Page Date 31 March 2009 Pilot s Operating Handbook EXTRA 300L Left blank intentionally ...

Page 279: ...ailable time delayed TheEFD1000PILOTPFDmodeldoesnotsupportdisplayofnavigationdatafrompanel mounted GPS navigators VOR Localizer radios etc See Section 924 7 of this Aircraft Flight Manual Supplement for a description of the operation of the EFD1000 PILOT PFD System The EFD1000 PILOT PFD System must utilize the software version described below or later approvedversions Thesystemsoftwareversionforth...

Page 280: ...andbook 924 7 SYSTEMDESCRIPTION 924 7 1 GENERAL The EFD1000 PILOT PFD system is a flat panel LCD flight instrument that presents the pilot with displays of attitude airspeed altitude vertical speed slaved compass slip skid and rate of turn information Thedisplayheadincorporatesasolid stateAirDataandAttitudeHeadingReference System ADAHRS toprovidedatafortheflightinstruments TheADAHRSsystemusesdataf...

Page 281: ...sviceversa Amessageispresentedduring the normal power down sequence to enable the pilot to abort the shutdown and switch to internal battery TheAHRSwillperformaninternaltestduringEFD1000PILOTPFDpowerup Theaircraftshould remainstationaryduringtheAHRSpowerupandalignmentsequence Iftheaircraftismovedduring AHRS alignment it will take longer for accurate attitude and heading information to be presented...

Page 282: ...b 11 Not Used 12 Not Used 13 Not Used 14 Micro SD Card slot 15 Automatic Dimming Photocell 16 Attitude Indicator 17 Aircraft Symbol 19 Roll Pointer 20 Slip Skid Indicator 21 Airspeed Indicator Tape 22 Selected Airspeed Field 23 Airspeed Drum Pointer 24 Altitude Alert 25 Selected Altitude Field 26 Altitude Drum Pointer 27 Altitude Tape 34 True Airspeed 35 Barometric Pressure Setting Field 36 Ground...

Page 283: ...refer to Aspen Pilot s Guide for more information The home state for the left knob is CRS Right control knob TherightcontrolknobcontrolsHeadingBug HDG AltitudeBug ALT andBarometricPressure Setting BARO editable fields in that order The home state for the right knob is HDG 924 7 6 SETTINGFLIGHTINSTRUMENTS The following procedures are used to adjust pilot editable data on the EFD1000 PILOT PFD Headi...

Page 284: ...matelyonesecondtheactivedatatypewillbe sync d as follows Table 1 Knob Sync Operation 924 7 8 HOTKEYOPERATION During normal operations the five line select soft keys on the lower right side of the display bezel arereferredtoas HotKeys HotKeysprovidesingle actionaccesstofrequentlyusedfunctions An electronic legend adjacent to each Hot Key indicates its hot key function When the legend is green thefu...

Page 285: ...l measures the ambient light allowing an automatic dimming mode to be selected by the pilot Manualdimmingcontrolisenabledbythepilottooverridethephotocellinputandadjustthedisplay to any desired intensity level except off In either mode the bezel key backlighting is maintained at a fixed brightness level Toadjustbacklightintensity presstheMENUbuttonandthenpresstheleftcontrolknobtotoggle betweenauto ...

Page 286: ...ling the PFD circuit breaker pressing and holding the REV button for 5 Seconds will produce in an immediate system shut down When external power is available PFD circuit breaker reset pressing and holding the REV button for 5 seconds will result in a system restart 924 7 12 WARNING CAUTION ANDADVISORYSUMMARY WARNINGS ONBAT 53 REM Red annunciation presented below the aircraft symbol whenever the EF...

Page 287: ... the menu press the MENU button again Menu items are shown exclusively in the lower half of the EFD1000 PILOT PFD display in the region below the data bar MAINMENUNAVIGATION OncetheMainmenuisactivated rotatingthelowerrightcontrolknobselectsbetweenthevarious menupages Thecurrentmenupageisindicatedbythepagenameandlegend page of and by the location of the green segment within the segmented menu navig...

Page 288: ...ertotheEFD1000 PILOTPFD includingoverridingautomaticpowerstates FromthePOWERSETTINGSPagethe pilot may Switch to Battery Power from External Power Switch to External Power from Battery Power Shut down or Re Start the unit View the External Power Source Voltage View the Internal Battery Status 924 8 HANDLING SERVICINGANDMAINTENANCE If the temperature sensor of the RSM is suspected to fail it is advi...

Page 289: ...Class 3 Operation 925 3 925 1 2 Class II Oceanic Remote and other Operations 925 3 925 2 LIMITATIONS 925 4 925 2 1 Placards 925 4 925 3 EMERGENCY ABNORMALPROCEDURES 925 4 925 3 1 Emergency Procedures 925 4 925 3 2 Abnormal Procedures 925 4 925 4 NORMALPROCEDURES 925 5 925 5 PERFORMANCE 925 5 925 6 WEIGHT CENTER OF GRAVITY 925 6 925 7 SYSTEM DESCRIPTION 925 6 925 7 1 Key and Knob Functions 925 6 92...

Page 290: ...Section 925 GARMINGNC420W 925 2 Page Date 31 March 2009 Pilot s Operating Handbook EXTRA 300L Left blank intentionally ...

Page 291: ...ere you will also find further information 925 1 1 GPS WAASTSO C146ACLASS3OPERATION TheGarminGNC420WusesGPSandWAAS withinthecoverageofaSpace BasedAugmentation System complying with ICAO Annex 10 for enroute terminal area non precision approach operations including GPS orGPS and RNAV approaches andapproachprocedureswith verticalguidance including LNAV VNAV and LPV Navigation is accomplished using t...

Page 292: ...ediction Program for operators requiring this capability Refer to your appropriate civil aviation authorities for these authorizations 925 2 LIMITATIONS The system must utilize main software version 3 00 and GPS software version 3 0 or later FAA approved versions A valid and compatible database must be installed and contain current data ThefunctionalityoftheGNC420WmaybeusedforVFRnavigationpurposes...

Page 293: ...rest airport NRST field 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 925 4 NORMALPROCEDURES TO ACTIVATE AN EXISTING FLIGHT PLAN 1 Press FPL and turn the small right knob to d...

Page 294: ...d VLOC frequency fields The COM flip flop key is used to swap the active and standby COM frequencies Press and hold to select emergency channel 121 500 MHz RIGHT HANDKEYSANDKNOBS The range key RNG allows you to select the desired map scale Use the up arrow side of the key to zoom out to a larger area or the down arrow side to zoom in to a smaller area Thedirect tokeyprovidesaccesstothedirect tofun...

Page 295: ...oflightplanfeatureisalsoavailablefromthe flight plan key N O T E Whenever the GNC 420W 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 The scroll bar graphically indicates the number of additional items available within the selected category Simply press the small right knob to activate the cursor and tur...

Page 296: ...tNAVpagedisplaysagraphiccoursedeviationindicator CDI theactiveleg ofyourflightplan asdefinedbythecurrent from and to waypoints andsixuser selectabledata fields The default settings for these fields are distance to waypoint DIS desired track DTK bearing to waypoint BRG ground speed GS ground track TRK and estimated time en route ETE ThedefaultNAVpageisselectedbypressingandholdingtheCLRkeyorturningt...

Page 297: ...EXME 406ELT 926 1 GENERAL 926 3 926 2 LIMITATIONS 926 3 926 3 EMERGENCYPROCEDURES 926 4 926 4 NORMALPROCEDURES 926 4 926 5 PERFORMANCE 926 4 926 6 WEIGHT CENTER OF GRAVITY 926 4 926 7 SYSTEM DESCRIPTION 926 5 926 7 1 Switch Operation 926 5 926 7 2 Self Test Mode 926 5 926 8 HANDLING SERVICINGAND MAINTENANCE 926 6 926 8 1 Transmitter Test 926 6 926 8 2 Self Test 926 6 ...

Page 298: ...Section 926 ARTEXME 406ELT 926 2 Page Date 31 March 2009 Pilot s Operating Handbook EXTRA 300L Left blank intentionally ...

Page 299: ...eps and the panel LED pulses periodically The time between pulses lengthen after a predetermined transmitter on time N O T E In October 2000 the International Cospas Sarsat Program announced at its 25th Council SessionheldinLondon UKthatitplanstoterminatesatelliteprocessingofdistresssignals from 121 5 and 243 MHz emergency beacons on February 1 2009 Accuracy Doppler positioning is employed using b...

Page 300: ...ence Attempt contact with rescue aircraft with the radio transceiver set to a frequency of 121 5 MHz If no contact is established switch the remote switch to the ON position immediately If the function of the remote switch is in doubt proceed as follows Remove quick pins from the backrest adjustment and swivel the backrest forward to get access to the ELT unit Use the unit master switch at the ELT...

Page 301: ...hould be taken when transporting or shipping the ELT not to move the switch or allow packing material to become lodged such as to toggle the switch 926 7 2 SELFTESTMODE Upon turn off from ON back to ARM state the ELT automatically enters a self test mode that transmits a 406 MHz test coded transmission that monitors certain system functions before returningtothe ARM mode Thetransmissionisignoredby...

Page 302: ...st duration to exceed 5 seconds A false alarm may be generated Any time the ELT is activated it is transmitting a 121 5 MHz distress signal After approximately 50 seconds a live 406 MHz distress signal is transmitted and is considered valid by the satellite system Whenever the ELT is switched from ON to ARM a 406 MHz signal is transmitted however it is specially coded as a self test signal that is...

Page 303: ...this error code the ELT must be sent back for repairorreplacement 5Flashes Indicates that ELT has not been programmed or is incorrectly programmed Does notindicateerroneousorcorruptedprogrammeddata 6Flashes Indicates that the G switch loop between pins 5 and 12 at the D sub connector is not installed ELT will not activate during a crash Check that the harness D sub jumper is installed by verifying...

Page 304: ...Section 926 ARTEXME 406ELT 926 8 Page Date 31 March 2009 Pilot s Operating Handbook EXTRA 300L Left blank intentionally ...

Page 305: ...LIMITATIONS 927 4 927 2 1 ENGINE 927 4 927 2 2 KINDS OF OPERATIONALLIMITS 927 4 927 2 3 OPERATING PLACARDS 927 4 927 3 EMERGENCYPROCEDURES 927 4 927 4 NORMALPROCEDURES 927 4 927 5 PERFORMANCE 927 4 927 6 WEIGHT CENTER OF GRAVITY 927 5 927 7 SYSTEM DESCRIPTION 927 5 927 8 HANDLING SERVICINGAND MAINTENANCE 927 5 EASAApproved On Behalf of ANAC of Brazil __________________________ Date __________ Maxi...

Page 306: ...Section 927 AIRPLANESREGISTEREDINBRAZIL 927 2 Page Date 19 April 2012 Pilot s Operating Handbook EXTRA 300L Left blank intentionally ...

Page 307: ...906 Digital RPM Indicator 907 Long Range Wing Tank Capacity 908 AirtowHook 909 Smoke System 910 ACROIIICategory 911 Single Seat Canopy 912 FILSERTRT600Transponder 913 FILSERTRT800Transponder 914 GARMINGTX327Transponder 915 GARMINGTX330Transponder 916 BENDIX KINGKT76ATransponder 917 BENDIX KINGKT73Transponder 918 BECKERATC2000Transponder 919 BECKERATC4401Transponder 920 BECKERBXP6401Transponder 921...

Page 308: ...pplemental means for navigation only Wide Area Augmentation System WAAS functionality Since the WAAS is not available in Brazil any kind of Global Navigation Satellite System GNSS approaches is prohibited even though optional GPS System installed e g GARMIN GNC420W may be capable of receiving WAAS 927 2 3 OPERATINGPLACARDS The following placard has to be attached to the aircraft replacing the rela...

Page 309: ...ANESREGISTEREDINBRAZIL Page Date 19 April 2012 927 5 Pilot s Operating Handbook EXTRA 300L 927 6 WEIGHT CENTEROFGRAVITY Notaffected 927 7 SYSTEMDESCRIPTION Notaffected 927 8 HANDLING SERVICINGANDMAINTENANCE Notaffected ...

Page 310: ...Section 927 AIRPLANESREGISTEREDINBRAZIL 927 6 Page Date 19 April 2012 Pilot s Operating Handbook EXTRA 300L Left blank intentionally ...

Page 311: ...NDING LIGHT 928 1 GENERAL 928 3 928 2 LIMITATION 928 3 928 3 EMERGENCYPROCEDURES 928 3 928 4 NORMALPROCEDURES 928 3 928 5 PERFORMANCE 928 3 928 6 WEIGHT AND BALANCE 928 3 928 7 DESCRIPTION OF THE SYSTEM 928 3 928 8 HANDLING SERVICINGAND MAINTENANCE 928 4 SECTION928 LANDINGLIGHT Table of Contents Paragraph Page ...

Page 312: ...928 2 Page Date 17 January 2013 Section 928 Landing Light Pilot s Operating Handbook EXTRA 300L Left blank intentionally ...

Page 313: ...be integrated in the RH lower cowling 928 2 LIMITATION Nochange 928 3 EMERGENCYPROCEDURES Nochange 928 4 NORMALPROCEDURES Nochange 928 5 PERFORMANCE Nochange 928 6 WEIGHTANDBALANCE Refer to the Equipment List in section 6 of this Handbook 928 7 DESCRIPTIONOFTHESYSTEM The landing light is controlled by the LANDING LIGHT switch on the right instrument panel The system is protected by the LANDING LIG...

Page 314: ...928 4 Page Date 17 January 2013 Section 928 Landing Light Pilot s Operating Handbook EXTRA 300L 928 8 HANDLING SERVICINGANDMAINTENANCE Nochange ...

Page 315: ...MERGENCY ABNORMALPROCEDURES 929 6 929 3 1 Emergency Procedures 929 6 929 3 2 Abnormal Procedures 929 6 929 4 NORMALPROCEDURES 929 7 929 5 PERFORMANCE 929 7 929 6 WEIGHT CENTER OF GRAVITY 929 8 929 7 SYSTEM DESCRIPTION 929 8 929 7 1 Touchscreen Key and Knob Functions 929 8 929 7 2 Secure Digital Card 929 9 929 7 3 Selecting com nav frequencies 929 9 929 7 4 Remote transponder operation 929 10 929 7...

Page 316: ...Section 929 GARMINGTN635 650 750 929 2 Page Date 20 January 2016 Pilot s Operating Handbook EXTRA 300L Left blank intentionally ...

Page 317: ...onder GTX 33 The GTN 650 750 also feature NAV functionality Additionally the GTN 750 can be used to display Charts and to control the optional GMA 35 remote audio panel Thissupplementiswrittenformainsoftwareversion2 00 GPSsoftwareversion4 0 COMsoftware version2 01andNAVsoftwareversion6 01andisnotsuitableforearliersoftwareversions Some differencesinoperationmaybeobservedwhencomparingtheinformationi...

Page 318: ... compatible databases must be installed and contain current data Thenavigationdataincl forfinalapproachsegmentsprovidedbytheGTNseries e g movingmap CDI depiction is for situational awareness only and should not be relied upon for navigation Do not use SafeTaxi or ChartView functions as the basis for ground maneuvering SafeTaxi and ChartViewaretobeusedforthepilottoorienthimselfontheairportsurfaceto...

Page 319: ...serve as a situational awareness tool only By itself it may not provideeithertheaccuracyorthefidelityonwhichtobasedecisionsandplanmaneuverstoavoid terrain or obstacles 929 2 4 TRAFFIC TISONLY TrafficmaybedisplayedontheGTNwhenconnectedtoanapprovedoptionalTIStrafficdevice This systemiscapableofprovidingtrafficmonitoringandalertingtothepilot Trafficshownonthedisplay mayormaynothavetrafficalertingavai...

Page 320: ...OF REMOTE AUDIO PANEL FUNCTIONS IF INSTALLED WITH GTN 750 PullINTERCOMcircuitbreaker N O T E This procedure will restore COM operation on the GTN 750 The intercom functions will not be available 929 3 2 ABNORMALPROCEDURES GPSNAVIGATIONINFORMATIONNOTAVAILABLEORINVALID IfGTN635 650 750GPSnavigationinformationisnotavailableorinvalidtheGTNwillenteroneof two modes Loss of Integrity LOI mode or Dead Rec...

Page 321: ... of the list is the nearest airport To review the other nearest airports touch the Up and Down keys to scroll through the list 3 Touch the desired airport to select it The selected airport will be displayed in the Waypoint page 4 Touch the Activate key or press the small right knob to activate the selection 5 The Map page will now be displayed with the new Direct To course 929 4 NORMALPROCEDURES T...

Page 322: ...ger in the desired direction Touchscreen keys are placed at the lower portion of the display The keys vary depending on the page selected Touch the key to perform the function or access the described information You can return to the previous page or exit the current function by touching the Back key KEYS QuicklyreturntotheHomepagebypressingtheHOMEkey PressandholdtheHOMEkeytoreach the Map page The...

Page 323: ... the NAV window active for editing The standby frequency in blue is active for editing Turn the large right knob to select the desired megahertz MHz value Turnthesmallrightknobtoselectthedesiredkilohertz kHz value Pressthesmall right knob to transfer the standby frequency to the active window USINGTOUCHSCREEN Touch the Standby window A pull down keypad will appear with the current Standby frequenc...

Page 324: ...emotetransponder GTX33 canbecontrolledviatheGTN635 650 750unit Touch thetransponderwindowtoenterthetransponderoperationpage Seefigures3and4fortheGTN 6xx and the GTN 750 respectively IDENT 1 Touch the IDENT key once to reply with an identifying squawk code 2 The IDENT key text will change to green to indicate active Ident Figure 4 GTN 750 XPDR Operation ...

Page 325: ...ed ALTITUDEREPORTING 1 Touch the Altitude Reporting key for Mode C operation 2 The transponder will be On and will transmit its squawk code and altitude when interrogated An ALT annunciation will appear when the squawk code is transmitted VFR 1 Touch the VFR key to set the VFR squawk code 1200 or 7000 depending on location see below SELECTINGASQUAWKCODE Theselectedsquawkcodewillalwaysbeinuse Asyou...

Page 326: ... is utilized to enhance the tracking capabilities of the ATC facility therefore care should be taken when making routine code changes 929 7 5 REMOTEAUDIOPANELOPERATION GTN750ONLY The remote audio panel GMA 35 can be operated from the GTN 750 only It incorporates an intercom functionality The Passenger Address Cabin Speaker Marker Beacon and Telephone functionalities are not used See Figure 5 for t...

Page 327: ...l 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 Touch the Split Mode key again to toggle the Crew Intercom selection off 3 Touch the Crew Intercom key to toggle activation of the Crew Intercom allowing the Pilot and Co Pilot to talk to each other 4 Touch the desired Pilot and...

Page 328: ...lch level automatically When enabled the Auto Squelch key will display a green bar 6 Touch the Squelch arrows to set the desired Squelch level 7 Touch the Back key to return to the Intercom Setup page 8 Touch the Music 1 or Music 2 keys to set their configuration 9 Select the recipients for Music Distribution by touching any combination of the Pilot and Co Pilot keys 10 Touch the Radio and or Inte...

Page 329: ...e used as an airport moving map display AMMD SafeTaxiandChartviewaretobeusedbytheflightcrewtoorientthemselvesontheairportsurface to improve pilot situational awarness during ground operations 929 7 9 TRAFFICDISPLAY OPTIONAL Traffic may be displayed on the GTN when connected to an approved TIS traffic device e g GTX 330orGTX33 TheTISinformationisonlyavailableintheUS TheGarminGTN6xxor7xxCockpit Refe...

Page 330: ...Section 929 GARMINGTN635 650 750 929 16 Page Date 20 January 2016 Pilot s Operating Handbook EXTRA 300L Left blank intentionally ...

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