6 - 14 Page Date: 19. February 2014
Section 6
Weight and Balance and Equipment List
PilotĀ“s Operating Handbook US
EXTRA 330LX
1 Diplexer Comant Industries CI 507 FA4057 0.09 3.90 O
1 Course Deviation Ind. Garmin/Mid Continent GI-102A FA3010 0.64 1.54 O
1 Course Deviation Ind./GS Garmin/Mid Continent GI-106A FA3003 0.64 1.54 O
1 Transponder (Mode S) Becker BXP6401-2-(01) 31860-PG 0.80 1.60 O
1 Transp. (Mode A&C) Garmin GTX 327 FA3009-PG 0.95 1.75 O
1 Transponder (Mode S) Garmin GTX 328 32839-PG 1.50 1.73 O
1 Transponder (Mode S) Garmin GTX 330 30334-PG 1.50 1.73 O
1 Transponder (Mode S) Garmin GTX 33 33775-PG 2.00 3.02 O
1 Transp. (mode A&C) Becker ATC-4401 31002-PG 0.73 1.60 O
1 Blind Encoder Module Becker BE-6400-01 32100 1.10 1.39 O
1 Altitude Blind Encoder ACK A-30 02239 0.20 1.50 O
(grey code)
1 Altitude Blind Encoder ACK A-30.8 (or higher) 32960 0.20 1.50 O
(serial output)
1 Transponder Antenna Comant Industries CI 105 32269 0.11 0.14 O
1 ELT Artex ME 406 32173-PG 1.42 2.60 O
Including ELT Antenna Artex or 110-773 33524 0.08 3.00 O
Rami AV-200 33965 0.08 3.00 A
1 Intercom Northern Airborne NAT AA83-001 31659-PG 0.28 1.55 O
1 Panel Dock AirGizmos GPSMAP 696 33665 0.25 1.60 O
1 Panel Dock AirGizmos GPSMAP 796 34175 0.27 1.60 O
1 Remote Audio Panel Garmin GMA 35 33902-PG 1.00 1.53 O
Cowling (54)
1 Cowling (CRP) Extra EA-83001.0 9.20 -0.57 R
1 Cowling (GRP) Extra EA-83003.0 10.60 -0.57 A
1 Cowling (CRP, incl. Landing Extra EA-8E001.0 9.20 -0.57 A
Light provision)
Canopy (56)
1 Standard Canopy Extra 26301.000-LV 26301.000-VF 13.50 1.69 R
1 Single Seat Canopy Extra EA-86411.0 86411.001-VF 13.20 1.69 A
Propeller (61)
1 3-Blade Propeller MT-Propeller MTV-9-B-C/ 32285 30.50 -1.15 R
C198-25
1 Spinner MT-Propeller P-810-2 31415 0.80 -1.20 R
1 4-Blade Propeller MT-Propeller MTV-14-B-C/ 33970 30.60 -1.15 A
C190-130
1 Spinner MT-Propeller P-967 31560 0.80 -1.20 A
1 Governor MT-Propeller P-880-41 32941 1.10 -0.91 R
(max 2600 RPM)
reserved
1 Governor Woodward A-210988 01209 1.10 -0.91 A
QTY ITEM MANUFACT. MODEL NO PART OR P/N WEIGHT ARM R* INST
(kg) (m) A
O
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