TBM
700
SUPPLEMENT 15
“KEITH” VAPOR CYCLE COOLING SYSTEM
Page 9.15.2
Edition 1 -- November 30, 2010
Rev. 0
SECTION 1
GENERAL
This supplement provides information necessary for airplane utilization when
the ”KEITH” vapor cycle cooling system is installed on TBM 700 airplane
equipped with MOD70--0276--00.
SECTION 2
LIMITATIONS
These limitations supplement those of standard airplane described in
Section 2 ”Limitations” of the basic Pilot’s Operating Handbook.
The vapor cycle cooling system can be operated with :
-- a Ground Power Unit,
-- engine running with ”GENERATOR” selector on MAIN.
The system must be OFF :
-- when engine is started,
-- when ”AIRFRAME DE--ICE” switch is ON,
-- when ”PROP DE--ICE” switch is ON,
-- when ”GENERATOR” selector is on ST--BY.
SECTION 3
EMERGENCY PROCEDURES
The instructions specific to the use of the ”KEITH” vapor cycle cooling system
in connection with the emergency procedures are described in Section 3
”Emergency procedures” of the basic Pilot’s Operating Handbook.