Daher-Socata TBM 900 Pilot's Information Manual page 644

PILOT'S OPERATING HANDBOOK
S/ ITEM
R/ OPT70
A/ or
O MOD70
S
S 0176-00A
A 0226-00A
S
S
Edition 0 -- October 31, 2013
Rev. 1
REQUIRED (R) OR STANDARD (S)
OR OPTIONAL (A or O) EQUIPMENT
34-24 - ADI and standby horizon
Electronic stand-by indicator
(integrated in MOD70-0335-34 ESI 2000 : see 34-11)
L-3 COMMUNICATION AVIONICS SYSTEMS
34-28 - Electronic flight instrumentation system
Integrated Flight Deck System G1000 composed of :
- PFD1 GDU 1040A
- PFD2 GDU 1040A
- MFD GDU 1500A
- Engine/Airframe Interface Unit # 1 GEA 71
- Engine/Airframe Interface Unit # 2 GEA 71
- Integrated Avionics Unit # 1 GIA 63W
- Integrated Avionics Unit # 2 GIA 63W
- MFD remote controller GCU 475
G1000 Synthetic Vision System
34-31 - Marker
MARKER antenna DM N27-3
Receiver
(integrated in the GMA 1347C dual audio systems : refer to
ATA 23)
LIST OF EQUIPMENT
GARMIN
GARMIN
GARMIN
GARMIN
GARMIN
GARMIN
GARMIN
GARMIN
GARMIN
DORNE & MARGOLIN
WEIGHT
ARM
per unit
in.
lb
(m)
(kg)
2.75 154.29
(1.250) (3.919)
6.53 155.71
(2.96) (3.955)
6.53 155.71
(2.96) (3.955)
8.66 155.20
(3.93) (3.942)
2.53 150.63
(1.15) (3.826)
2.53 150.63
(1.15) (3.826)
7.21 149.37
(3.27) (3.794)
7.21 149.37
(3.27) (3.794)
0.82 157.83
(0.37) (4.009)
/ /
0.750 129.92
(0.340) (3.300)
/ /
Page 21