SOCATA TBM 700 - Page 435

SECTION 6
WEIGHT AND BALANCE
T B M
700 PILOT’S INFORMATION MANUAL
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Contents
Page 6.5.49
Rev. 9
ARM
in.
(m)
WEIGHT
per unit
lb
(kg)
EQUIPMENT
SUPPLIER
REQUIRED (R) OR STANDARD (S)
OR OPTIONAL (A or O)
EQUIPMENT
ITEM
OPT70
S/
R/
A/
O
77 – ENGINE INDICATING
R Compressor turbine
tacho–generator (Ng)
MIL–G–26611C GEU–7/A
QPL (AIRCRAFT
APPLIANCES
AND EQUI. LTD)
0.981
(0.445)
108.27
(2.750)
R Gas generator speed indicator
(Ng) 523278
AMETEK 0.705
(0.320)
157.48
(4.000)
O Gas generator speed indicator
(Ng) 5428–703–91–03
MORS 1.290
(0.585)
151.57
(3.850)
R Propeller speed indicator 523277 AMETEK 0.705
(0.320)
157.48
(4.000)
O Propeller speed indicator
5428–704–91–03
MORS 1.290
(0.585)
151.57
(3.850)
R Power turbine tacho–generator
MIL–G–26611C GEU–7/A
QPL (AIRCRAFT
APPLIANCES
AND EQUI. LTD)
0.981
(0.445)
55.12
(1.400)
R Torquemeter 523276 AMETEK 0.705
(0.320)
157.48
(4.000)
O Torquemeter 5428–750–91–03 MORS 1.257
(0.570)
151.57
(3.850)
R Torque transducer CZ 52E8–G SAGEM/
SCHLUMBERG
ER
0.452
(0.205)
55.12
(1.400)
O Torque transducer 8107.200.00.10 MORS 0.463
(0.210)
53.54
(1.360)
77–12 – Fuel management
S Flowmeter 90 12 00 :
S –Indicator 455–6110 ARNAV 0.331
(0.150)
157.48
(4.000)
S –Transmitter 455–2069–02 ARNAV 0.661
(0.300)
106.30
(2.700)