background image

� 

Zf, 

Pilot Operating Handbook 

5.3 

Cruise speeds 

Altitude 

Engine 

IAS 

CAS 

speed 

ft 

rpm 

knot 

mph 

knot 

mph 

4200 

77 

89 

77 

88 

4500 

86 

99 

85 

98 

4800 

95 

109 

93 

107 

1000 

5000 

101 

116 

98 

113 

5300 

110 

126 

106 

122 

5500 

116 

133 

111 

128 

5800 

125 

143 

119 

137 

4200 

75 

86 

75 

86 

4500 

83 

96 

82 

94 

4800 

92 

106 

90 

104 

3000 

5000 

97 

112 

95 

109 

-

5300 

106 

122 

103 

118 

5500 

112 

129 

108 

124 

5800 

120 

139 

116 

133 

4200 

72 

83 

72 

83 

4500 

80 

92 

79 

91 

4800 

88 

101 

86 

99 

5000 

5000 

94 

108 

92 

106 

5300 

102 

1'/7 

99 

114 

5500 

107 

124 

104 

120 

5800 

116 

134 

112 

129 

4200 

69 

79 

70 

80 

4500 

77 

88 

77 

88 

4800 

84 

97 

83 

96 

7000 

5000 

90 

103 

88 

101 

5300 

97 

112 

95 

109 

5500 

103 

118 

100 

115 

5800 

111 

127 

107 

123 

4200 

65 

75 

66 

76 

4500 

73 

84 

73 

84 

4800 

80 

93 

80 

92 

9000 

5000 

85 

98 

84 

97· 

5300 

93 

107 

91 

104 

5500 

98 

112 

95 

109 

5800 

105 

121 

102 

117 

Date of Issue: 0412009 

Revision: 3. 0 

5-4

-

II 

Summary of Contents for SportCruiser 09SC284

Page 1: ...Revision S Sp po or rt tC Cr ru ui is se er r i S Sp po or rt tC Cr ru ui is se er r Pilot s Operating Handbook Airplane Registration Number N107BK Airplane Serial Number 09SC284 Date of Issue 0412009...

Page 2: ...Revision S Sp po or rt tC Cr ru ui is se er r ii Intentionally left blank Date of Issue 0412009...

Page 3: ...i is s d de es si ig gn ne ed d a an nd d m ma an nu uf fa ac ct tu ur re ed d b by y Czech sport aircraft a s Na Z honech 1177 212 686 04 Kunovice Czech Republic Website www czechsportaircraft com E...

Page 4: ...Revision S Sp po or rt tC Cr ru ui is se er r iv Intentionally left blank Date of Issue 0412009...

Page 5: ...Initial 01 2007 CH W E Pilot static probe change 2 0 All Valid for Pilot static probe 12 2007 CH W E AVIATIK WA037383 only Control surfaces defie tion 2 1 II II formal faults removal 0i 20J8 CH W E V...

Page 6: ......

Page 7: ......

Page 8: ......

Page 9: ......

Page 10: ......

Page 11: ......

Page 12: ......

Page 13: ......

Page 14: ......

Page 15: ......

Page 16: ......

Page 17: ......

Page 18: ......

Page 19: ......

Page 20: ......

Page 21: ......

Page 22: ...kg Max landing weight 1 320 lb 600 kg Max weight of fuel 180 lb 82 kg Max baggage weight in rear fuselage 40 lb Max baggage weight in each wing locker 44 lb WARNING 18 kg 20 kg Do not exceed maximum t...

Page 23: ......

Page 24: ......

Page 25: ......

Page 26: ......

Page 27: ......

Page 28: ......

Page 29: ......

Page 30: ......

Page 31: ......

Page 32: ...stated otherwise the performance stated in this section is valid for maximum take off weight and under ISA conditions The performance shown in this seciion is valid for aircraft fitted with given ROT...

Page 33: ...ding distances RUNWAY Landing distance over Landing run distance SURFACE SO ft obstacle braked ft ft CONCRETE 591 180 GRASS 558 197 5 2 Rate ofclimb Conditions Max continuous power Best rate of Rate o...

Page 34: ...109 5300 106 122 103 118 5500 112 129 108 124 5800 120 139 116 133 4200 72 83 72 83 4500 80 92 79 91 4800 88 101 86 99 5000 5000 94 108 92 106 5300 102 1 7 99 114 5500 107 124 104 120 5800 116 134 11...

Page 35: ......

Page 36: ......

Page 37: ...CY PROCEDURES 6 1 Engine failure 6 2 6 2 In flight engine starting 6 3 6 3 Smoke and fire 6 3 6 4 Glide 6 5 6 5 Landing emergencies 6 5 6 6 Recovery from unintentional spin 6 7 6 7 Other emergencies 6...

Page 38: ...t static probe These emergency procedures are valid for standard WOOD COMP KLASSIC 17013 R three composite blade in ground adjustable propeller 6 1 Engine Failure 6 1 1 Engine failure during take off...

Page 39: ......

Page 40: ......

Page 41: ......

Page 42: ......

Page 43: ......

Page 44: ......

Page 45: ......

Page 46: ......

Page 47: ......

Page 48: ......

Page 49: ......

Page 50: ......

Page 51: ......

Page 52: ......

Page 53: ......

Page 54: ......

Page 55: ......

Page 56: ......

Page 57: ......

Page 58: ......

Page 59: ......

Page 60: ......

Page 61: ......

Page 62: ......

Page 63: ......

Page 64: ......

Page 65: ......

Page 66: ......

Page 67: ......

Page 68: ......

Page 69: ......

Page 70: ......

Page 71: ......

Page 72: ......

Page 73: ...ue on in next training step Training can be performed by Flight Instructor or by the experienced pilot who has minimum 20 hours on the SportCruiser Type Rating Training Procedure Ground Training befor...

Page 74: ......

Page 75: ......

Page 76: ......

Page 77: ...plane Information contained in this Supplement add or replace information from the basic Pilot Operating Handbook in the further mentioned parts only Limitations procedures and information not mention...

Page 78: ...STEMS DESCRIPTION 2 1 Airplane description Cockpit Instrument panel layout of SportCruiser aircraft s n 09SC284 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 3...

Page 79: ...onder 7 Vertical speed indicator 26 PS Engineering Intercom 8 Altimeter 27 Flaps control switch 9 Transceiver 28 Flaps position indicator 10 GPS 29 Throttle 11 Compass 30 Choke 12 Fuel pressure gauge...

Page 80: ...pressure an J emper t 11 0 aL g0 Fuel pre S Jre a111 qua tity 9auges CHT indicator Voltme e Engine hours counter MiscP i anec s equipment G 205 tri n cc111trol a 1d PTT on tne 0n ro1 1 L lq Trirrs em...

Page 81: ...nt 2 5 Oil Type of coolant used in engine Specification ASTM D 3306 WI TL 774C Mixture ratio coolant water 50 50 Max coolanttemperature 248 FJ 120 C Type of oil used in enwne AeroShell Oil Sport P tu...

Page 82: ...ponder 0 l ng A 350 i wc 1 anco Artex MEAO El T Airgizmos Can iri 95 C J 1 sn as Engine RP h 1rJ aftlr o Oil pressu1 and tempera a qauges A CHT ina cator Fuel pressuru and quantity ga1 ges Voltmeter E...

Reviews: