Side-Power SEP 100/185 T Wartungshandbuch Seite 19
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Page Date: 4. February 2011 2 - 3
Pilot´s Operating Handbook
EXTRA 330LX
Section 2
Limitations
2.1 GENERAL
This section includes operating limitations, instrument markings, and basic placards
necessary for the safe operation of the aircraft, its engine, standard systems, and standard
equipment. The limitations included in this section have been approved by the EASA.
Observance of these operating limitations is required by national aviation regulations.
N O T E
In case of an aircraft equipped with specific options additional information required
for safe operation will be contained in Section 9 "Supplements".
Instrument markings and placards are provided 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 MAINTENANCE MANUAL EXTRA
330LX can be performed .
2.2 AIR SPEED (IAS)
Never Exceed Speed V
NE
219 knots (406 km/h)
Max. Structural Cruising Speed (Normal Cat.) V
NO
138 knots (256 km/h)
Max. Structural Cruising Speed (Acro Cat. I , II, III) V
NO
154 knots (285 km/h)
Maneuver Speed (Normal Cat.) V
A
138 knots (256 km/h)
Maneuver Speed (Acro Cat. I , II, III) V
A
154 knots (285 km/h)
Max. Aileron Control Inputs (Acro Cat. I , II, III) up to 185 knots (343 km/h)
2.3 CROSS-WIND COMPONENT
Max. demonstrated cross-wind component for take-off and landing is 15 knots (27 km/h).
2.4 ENGINE
Engine-type: Textron-Lycoming AEIO-580-B1A
Rated maximum power: 235 kW (315 HP) @ 2700 rpm.
2.4.1 FUEL
Minimum grade aviation gasoline: 100/100LL; for alternate fuelgrades see latest revision of
Lycoming S.I. No. 1070.
Total fuel capacity: 189 L (49.9 US.gal)
Usable fuel capacity: 187 L (49.4 US.gal)
Total fuel capacity for acrobatic in acro & center tank: 69 L (18.2 US.gal)
Usable fuel capacity for acrobatic in acro & center tank: 67 L (17.7 US.gal)
For acrobatic flight wing tanks must be empty.
- EXTRA 330LX 1
- Page Date: 4. February 2011 i 3
- Page Date: 29. September 2014 4
- Page Date: 4. February 2011 v 7
- Left blank intentionally 10
- Section 1 11
- 1.11 CONVERSION TABLE 16
- Section 2 19
- Limitations 19
- TC-NUMBER: * 24
- AVGAS 100/100LL 25
- NO SMOKING 26
- THROTTLE OPEN 27
- MIXTURE RICH 27
- NO HANDHOLD 28
- Section 3 33
- Emergency Procedures 33
- Section 4 43
- Normal Procedures 43
- Section 5 55
- Performance 55
- 5.2 ISA CONVERSION 59
- 5.3 AIRSPEED CALIBRATION 60
- 5.6 RATE OF CLIMB PERFORMANCE 63
- 5.8 RANGE 65
- 5.9 ENDURANCE 66
- Section 6 69
- PILOT COPILOT 76
- REAR SEAT FRONT SEAT 76
- EXAMPLE: 77
- 6.6 EQUIPMENT LIST 78
- EXTRA 330LX S/N: 78
- Reserved 80
- Section 7 87
- Figure 1, Instrument Panel 92
- Figure 3, Fuel System 97
- Figure 4, Electrical System 99
- Section 8 101
- Pilot´s Operating Handbook 101
- Section 9 107
- Supplements 107
- Section 901 109
- Steerable Tail Wheel 109
- Section 902 113
- Electric Pedal Adjustment 113
- Section 903 117
- Cabin Heating System 117
- Section 904 121
- Accelerometer TL-3424_EXT 121
- Section 905 127
- External Power 127
- Section 907 137
- Smoke System 137
- Section 908 145
- Single Seat Canopy 145
- Page Date: 4. Februar 2011 145
- Section 909 149
- ARTEX ME-406 ELT 149
- Section 910 157
- NAT AA83-001 Intercom 157
- HEADSET ONLY 159
- Section 911 165
- BECKER ATC 4401 Transponder 165
- Section 912 173
- BECKER BXP 6401 Transponder 173
- Section 913 183
- GARMIN GTX 327 Transponder 183
- GARMIN GTX 327Transponder 186
- 8 and 9 keys 187
- Section 914 189
- GARMIN GTX 328 Transponder 189
- Section 915 197
- GARMIN GTX 330 Transponder 197
- Section 916 205
- GARMIN GNC 420W/GNS 430W 205
- GARMIN GPS 208
- Section 917 215
- ASPEN EFD1000/500 System 215
- Section 918 225
- EI MVP-50P 225
- Section 919 233
- Landing Light 233
- No change 236
- Section 920 237
- Airtow Hook 237
- TAKE-OFF DISTANCE 242
- Not affected 249
- Section 922 251
- GARMIN GTN 635/650/750 251
- Section 923 267
- EXTRA 300LC 267
- 923.1.2 OPERATION 270
- CONTROLS 270
- Section 924 277
- KANNAD AF 406 ELT 277
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