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1.3 SPECIFICATIONS
PART NUMBER:
FAA CERTIFICATION:
RTCA COMPLIANCE:
SIZE:
WEIGHT:
CHASSIS GROUND:
POWER REQUIREMENTS:
CONNECTOR TYPE:
INTERFACE (S):
OPERATING TEMPERATURE:
STORAGE TEMPERATURE:
ALTITUDE:
SCHEDULED MAINTENANCE
SERVICE LIFE:
Page 1-4
March 15, 2018
CP-2500
Installation Manual
9080-17250-( )
9080-17250-01 (TSO-C154c)
9080-17250-02 and 9080-17250-12 (TSO-151c, TSO-C154c,
TSO-C147a, and TSO-C195a)
Listed are current certifications at time of publication, contact Field Service
Engineering for latest certification information.
Environmental Category: DO-160G
Other: DO-282B, [DO-197A and DO-317B (9080-17250-02 and
9080-17250-12)]
See environmental qualification form in Appendix B.
See outline drawings in installation section.
0.5 lbs (0.23 kg)
Bonding impedance between aircraft ground and the CP-2500
Chassis must be less than 2.5 milliohms.
+ 11.0 to 33.0 Volts DC,
4 Watts Max Startup. 2 Watts Nominal.
Mating Connector: 15 pin sub D, (P/N 425-015-2052)
RS-232
-20 to +55 C (-4 to +131 F)
-55 to +85 C (-67 to +185 F)
Maximum Operating Altitude 20,000ft.
Decompression 8,000ft to 20,000ft.
Overpressure -15,000ft.
No scheduled maintenance interval applicable.
The instrument has unlimited service life
General Information
0040-17251-01
Revision D
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