Daher TBM 850, Pilot'S Information Manual

Page: 932 / 1225

SUPPLEMENT 48
”HONEYWELL” KTA 870 TAS SYSTEM
T B M
850
Page 9.48.5 Rev. 0
SECTION 5
PERFORMANCE
The installation and the operation of the ”HONEYWELL” KTA 870 TAS
SYSTEM do not change the basic performance of the airplane described in
Section 5 ”Performance” of the basic Pilot’s Operating Handbook.
SECTION 6
WEIGHT AND BALANCE
Information hereafter supplement the one given for the standard airplane in
Section 6 ”Weight and balance” of the basic Pilot’s Operating Handbook.
A
or
O
OPTIONAL EQUIPMENT
EQUIPMENT
SUPPLIER
WEIGHT
per unit
lb
(kg )
ARM
in.
(m )
34 -- NAVIGATION
A TAS system KTA 870
coupled with GARMIN G1000 system
(OPT70--034--061D)
HONEYWELL 9.17
(4.160)
133.07
(3.380)
PIM - DO NOT USE FOR FLIGHT OPERATIONS