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5.8

Horizontal Speeds

The following tables give indicated airspeeds (IAS) and corresponding True Air Speeds 

(TAS) versus altitude, for various engine speeds.

4000 rpm

4200 rpm

4500 rpm

4800 rpm

5000 rpm

5200 rpm

5500 rpm

5750 rpm

8000 ft

ISA

68 mph IAS

73 mph IAS

80 mph IAS

87 mph IAS

92 mph IAS

96 mph IAS

103 mph IAS

109 mph IAS

68 mph CAS

72 mph CAS

79 mph CAS

85 mph CAS

90 mph CAS

94 mph CAS

100 mph CAS

105 mph CAS

77 mph TAS

82 mph TAS

89 mph TAS

96 mph TAS

101 mph TAS

106 mph TAS

113 mph TAS

119 mph TAS

6000 ft

ISA

71 mph IAS

76 mph IAS

83 mph IAS

91 mph IAS

96 mph IAS

101 mph IAS

109 mph IAS

115 mph IAS

71 mph CAS

75 mph CAS

82 mph CAS

89 mph CAS

94 mph CAS

98 mph CAS

105 mph CAS

111mph CAS

77 mph TAS

82 mph TAS

90 mph TAS

97 mph TAS

102 mph TAS

107 mph TAS

115 mph TAS

121 mph TAS

4000 ft

ISA

74 mph IAS

79 mph IAS

87 mph IAS

95 mph IAS

100 mph IAS

106 mph IAS

114 mph IAS

120 mph IAS

73 mph CAS

78 mph CAS

85 mph CAS

93 mph CAS

97 mph CAS

102 mph CAS

110 mph CAS

116 mph CAS

78 mph TAS

83 mph TAS

91 mph TAS

98 mph TAS

103 mph TAS

109 mph TAS

116 mph TAS

123 mph TAS

2000 ft

ISA

77 mph IAS

82 mph IAS

91 mph IAS

99 mph IAS

105 mph IAS

110 mph IAS

119 mph IAS

126 mph IAS

76 mph CAS

 81 mph CAS

89 mph CAS

96 mph CAS

101 mph CAS

106 mph CAS

114 mph CAS

121 mph CAS

78 mph TAS

83 mph TAS

91 mph TAS

99 mph TAS

104 mph TAS

110 mph TAS

118 mph TAS

124 mph TAS

0 ft

ISA

80 mph IAS

85 mph IAS

94 mph IAS

103 mph IAS

109 mph IAS

115 mph IAS

124 mph IAS

132 mph IAS

79 mph CAS

84 mph CAS

92 mph CAS

100 mph CAS

105 mph CAS

111 mph CAS

119 mph CAS

126 mph CAS

79 mph TAS

 84 mph TAS

92 mph TAS

100 mph TAS

105 mph TAS

111 mph TAS

119 mph TAS

126 mph TAS

5.9

Endurance

The following  table give fuel consumptions, endurances and ranges for specific 
engine speeds.

Fuel tank capacity

65 litres

14.3 Imp. gals.

Fuel reserve 

*

11 litres

2.4 Imp. gals. 

Reserve is indicated by a yellow warning lamp on the dash.

At 2000 ft altitude ISA conditions:

Engine speed

rpm

4200

4500

4800

5000

5200

5500

Fuel consumption

l/hr

9

11

13

14

15

18

Imp. gal/hr

2.0

2.4

2.9

3.1

3.3

4.0

IAS

mph

82

91

99

105

110

119

CAS

mph

81

89

96

101

106

114

Total endurance

hours

7.2

5.9

5.0

4.6

4.3

3.6

Total range

stat. miles

580

520

480

470

460

410

naut. miles

510

450

420

410

400

360

Reserve endurance

hours

1.2

1.0

0.8

0.8

0.7

0.6

Reserve range

miles

100

90

80

80

80

70

POH/EUR/01

Issue 2

Page 32 of 42

Содержание EV-97 teamEUROSTAR UK

Страница 1: ...EV 97 teamEUROSTAR UK...

Страница 2: ...n compliance with the information and limitations contained herein This POH must be available on board the aeroplane WARNING This aeroplane is not fitted with a certified engine A power failure can oc...

Страница 3: ...Amendment Record Issue Details of Change Date Authorised 1 Initial issue 14 07 03 2 Addition of optional hourmeter and warning lamp P37 16 8 04 POH EUR 01 Issue 2 Page 3 of 42...

Страница 4: ...oeuvring Load Factor 13 2 11 Crew 14 2 12 Kind of Operations 14 2 13 Fuel 14 2 14 Maximum Passenger Seating 14 2 15 Other Limitations 14 2 16 Limitations Placards 15 SECTION 3 EMERGENCIES 17 3 1 Intro...

Страница 5: ...SECTION 6 WEIGHT AND BALANCE 34 6 1 Introduction 34 6 2 Permitted Cockpit Loads 34 SECTION 7 AEROPLANE AND SYSTEMS DESCRIPTION 35 7 1 Introduction 35 7 2 Airframe 35 7 3 Cockpit Controls 36 7 4 Landin...

Страница 6: ...vation of the corresponding procedure leads to a minor or possible long term degradation of the flight safety NOTE Draws attention to any special item not directly related to safety but which is impor...

Страница 7: ...Length 5 98 m 19 62 ft Width 1 04 m 3 41 ft Height 2 34 m 7 67 ft Horizontal tail unit Span 2 5 m 8 20 ft Area 1 95 m2 20 99 ft2 Elevator area 0 8 m2 8 60 ft2 Vertical tail unit Height 1 24 m 4 07 ft...

Страница 8: ...1 4 3 Three view drawing 8 1 m 26 57 ft 2 5 m 8 2 ft 2 34 m 7 7 ft 1 9 62 ft 5 98 m 2 25 m 7 38 ft 0 94 m 3 1 ft 4 42 ft 1 35 m 1 6 m 5 25 ft 3 42 ft 1 04 m POH EUR 01 Issue 2 Page 8 of 42...

Страница 9: ...may be overstressed by full control movement VNO Maximum structural cruising speed 118 Do not exceed this speed except in smooth air and then only with caution VFE Maximum Flap Extending speed 77 Do n...

Страница 10: ...sure min 0 15 bar max 0 4 bar Oil Automotive engine oil of registered brand with gear additives but not aircraft oil refer to engine Operator s Manual API classification SF or SG Propellers and Manufa...

Страница 11: ...powerplant instruments are installed in the EV 97 teamEurostar UK aeroplane with the following markings Minimum Limit Normal Operating Caution Range Maximum Range Engine speed RPM 1400 1400 5200 5200...

Страница 12: ...ument markings Fuel gauge A fuel reserve of 11 litres 2 42 Imp gals is indicated by yellow warning lamp 2 7 Weight Empty weight standard equipment max 268 kg 591 lbs NOTE Actual empty weight is stated...

Страница 13: ...intentional spins are prohibited 2 10 Manoeuvring Load Factor POH EUR 01 Issue 2 Page 13 of 42 LOAD FACTOR 0 10 V V V V S0 S1 A NE 20 30 40 50 60 70 80 90 100 110 120 130 140 150 160 170 180 190 200...

Страница 14: ...eter iii Magnetic compass iv Slip ball 2 13 Fuel Regular or premium unleaded automobile fuel to EN228 minimum RON 90 AVGAS 100LL The higher lead content in AVGAS can result in wear of valve seats and...

Страница 15: ...100 mph VFE Flaps extended max speed 77 mph VS Stall speed flaps extended 36 mph ENGINE LIMITATIONS Maximum take off max 5 minutes 5800 rpm Max continuous 5200 rpm Idle approx 1400 rpm Max CHT 150 C M...

Страница 16: ...f 268 kg a customised placard may be used for revised load limits CG Limits Operating C G range 250 425 mm AOD Datum is wing leading edge In the baggage area In view of both occupants Adjacent to the...

Страница 17: ...1 Speed glide at 68 mph 2 Altitude below 160 ft 50 m land in take off direction over 160 ft 50 m choose landing area 3 Wind find direction and velocity 4 Landing area choose free area without obstacl...

Страница 18: ...nto consideration 3 4 Smoke and fire 3 4 1 Fire on the ground 1 Fuel cock shut off 2 Throttle fully open 3 Master switch switch off 4 Ignition switch off 5 Abandon the aeroplane Extinguish fire if pos...

Страница 19: ...eeded 5 MAYDAY report your location if possible 6 Fuel cock shut off 7 Ignition switch off 8 Master switch switch off 3 7 Precautionary landing A precautionary landing is generally carried out in the...

Страница 20: ...controllable spin if normal piloting techniques are used The following standard procedure can be used to recover from an intentional spin 1 Throttle reduced to idle 2 Control stick ailerons neutralise...

Страница 21: ...8 mph 2 Throttle set for 1 3 power 3 If possible leave the icing area 4 Increase the engine power gradually to cruise conditions after 1 2 minutes If engine power cannot be recovered make a precaution...

Страница 22: ...ght inspection The pre flight inspection is vitally important because incomplete or careless inspection could cause an accident The following pre flight inspection procedure is recommended by the airc...

Страница 23: ...Oil quantity check between dipstick marks In cases where the engine has not been run for some time oil can drain into the engine crankcase making the oil tank level appear low If the level does appear...

Страница 24: ...Flaps check function 6 Engine controls throttle check friction set 7 Fuel cock check turned on It is recommended that the fuel cock be left on at all times 8 Fuel gauge fuel quantity check 9 Master s...

Страница 25: ...difference between circuits A and B should be 120 rpm Set max power to check max speed with given propeller check engine temperatures and pressures Check pick up acceleration from idle to max power I...

Страница 26: ...b Speed 72 mph 3 Trim adjust 4 Instruments CHT oil temp and pressure within limits CAUTION If the cylinder head temperature or oil temperature exceeds its limit reduce the climb angle to increase airs...

Страница 27: ...ack the stick after touch down to hold the nose wheel up as long as possible Push the control stick when the nose wheel touches the ground The landing run can be shortened by braking 4 4 15 Baulked la...

Страница 28: ...suitable for stopping the engine by switching the ignition off If necessary cool the engine at 2500 2750 rpm to stabilise the temperatures prior to engine shut down 4 4 18 Flight in rain When flying...

Страница 29: ...dition and using average piloting techniques If not stated otherwise the performances given in this section are valid for the max take off weight and flight under ISA conditions 5 2 Airspeed Indicator...

Страница 30: ...a level and an ambient temperature of 15 C 59 F Runway Surface Take off run distance Take off distance over 50 ft 15 m obstacle ft m ft m CONCRETE 620 189 1195 364 SHORT GRASS 662 202 1280 390 5 5 Lan...

Страница 31: ...50 700 750 800 850 900 50 55 60 65 70 75 80 85 90 95 100 105 110 Airspeed IAS mph Rate of climb ft min 0 ft ISA 2000 ft ISA 4000 ft ISA 6000 ft ISA 8000 ft ISA EV 97 EUROSTAR 55 60 65 70 75 80 85 90 9...

Страница 32: ...000 ft ISA 77 mph IAS 82 mph IAS 91 mph IAS 99 mph IAS 105 mph IAS 110 mph IAS 119 mph IAS 126 mph IAS 76 mph CAS 81 mph CAS 89 mph CAS 96 mph CAS 101 mph CAS 106 mph CAS 114 mph CAS 121 mph CAS 78 mp...

Страница 33: ...ht is unavoidable reduce the engine speed to the minimum to sustain safe flight 5 12 Demonstrated crosswind performance Max permitted cross wind velocity for take off and landing 11 mph 10 kts Max per...

Страница 34: ...o which this POH applies Procedures for weighing the aircraft and the calculation method for establishing the permitted payload range are contained in the Maintenance Manual for the EV 97 teamEUROSTAR...

Страница 35: ...ction in the nose is separated from the crew by a firewall to which the engine mount is attached 7 2 2 Wing The rectangular wing is a monospar construction with an auxiliary rear spar for the aileron...

Страница 36: ...ring system is connected directly to the rudder control 7 5 Seats and safety belts The aeroplane has two side by side seats which are fixed non adjustable Each seat is equipped with a four point safet...

Страница 37: ...nder horizontally opposed spark ignition engine with one central camshaft push rod OHV and the following features Liquid cooled cylinder heads ram air cooled cylinders Dry sump forced lubrication Dual...

Страница 38: ...er voltage in the event of battery disconnection A voltmeter mounted on the instrument panel monitors the battery voltage Normal readings lie in the range 12 to 14 4 volts Distribution and Services Th...

Страница 39: ...clear to ensure that it functions properly The lowest parts of the pitot and static hoses lie on the left hand side of the cockpit immediately in front of the seat If water is visible in the hoses at...

Страница 40: ...should be performed by the manufacturer Refer to the Rotax 912 Operator s Manual for engine maintenance Maintain the prop according to its manual Refer to the Maintenance Manual for the EV 97 teamEuro...

Страница 41: ...ted on the lower surfaces of the wing It is also necessary to tie down the nose wheel landing gear and the tail skid to the ground When parking for a long time it is recommended that the cockpit canop...

Страница 42: ...clean the aircraft surface Oil spots on the aircraft surface except the canopy may be cleaned with petrol Clean the canopy only by washing it with lukewarm water and detergent Use either a soft clean...

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