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Page Date: 4. February 2011 7 - 3
Section 7
Description and Operation of Aircraft and Systems
Pilot´s Operating Handbook
EXTRA 330LX
SECTION 7
DESCPRIPTION AND OPERATION
OF AIRCRAFT AND SYSTEMS
7.1 THE AIRCRAFT
The aircraft EXTRA 330LX is designed and developed by EXTRA Flugzeugproduktions- und
Vertriebs- GmbH, Flugplatz Dinslaken, 46569 Hünxe, Federal Republic of Germany, in
accordance with the U.S. Federal Aviation Regulations, part 23, categories normal and
acrobatic to fullfill the primary flight training, normal operation rules and acrobatic training up
to the unlimited acrobatic level.
EXTRA 330LX is a light weight, robust, single piston-engined, two-seat aircraft with a fuselage
structure in tig-welded steel-tube construction.
The landing gear, wing, and tail are made of epoxy, reinforced with glass- and carbonfiber.
The items are qualified up to 72°C (161,6°F). Not to exceed this temperature limit an
appropriate colour specification for composite structure is given by the manufacturer
document EA-03205.19.
To check the temperature inside the cockpit (potential "green house" effect) a reversible
temperature indicator (STRUCTURAL OVERHEAT INDICATOR) is applied on the wing main
spar in the carry-through section. After reaching the temperature limit of 72°C (161,6°F) the
word "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 111°F) at sea level. It is possible to start the engine using the aircraft
battery at -20°C (-4°F) without preheating. Below -10°C (+14°F) OAT a special oil breather line
must be adapted (available as kit).
7.2 FUSELAGE
The fuselage structure consists of a steel tube construction integrating the wing and
empennage connections as well as the seats. The fuselage except the rear lower part, is
faired with an aramid/carbon laminate shell. Within the exhaust area stainless steel sheet
metal is used. The upper fuselage body surface is one part from firewall to vertical stabilizer
including the correlated canopy frame. Only the lower rear part of the fuselage is covered with
Ceconite
®
102.
The canopy frame itself is constructed by carbon laminate. The canopy is one part, opens to
the right and is held in the open position by a belt. Emergency jettisonning is achieved by
simply unlatching the canopy. For additional pilot protection a roll bar is installed behind the
rear pilots seat.
CAUTION:
While the word
RISK
appears, flying
is prohibited !
STRUCTURAL
OVERHEAT
INDICATOR
EXTRA
RISK
CAUTION:
While the word
RISK
appears, flying
is prohibited !
STRUCTURAL
OVERHEAT
INDICATOR
EXTRA
- 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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