Honeywell Bendix, Installation Manual, Page: 9 / 26

BENDIX/KING KI 208, KI 209
Rev 4, Aug 2002 IM 006-00140-0004 Page 1-3
PART NUMBER DESCRIPTION QTY VENDOR PART NUMBER
030-02227-0005 Shell, Connector Plug 1 Burndy SMS12P-1
030-02227-0009 Hood, Conn (2 pieces) 1 Burndy SMS12H1
030-02227-0023 Pin, Female Crimp 12 Burndy SC20M-6TK6
088-00706-0000 Tool, Adjustment 1
1.5 ACCESSORIES REQUIRED, BUT NOT SUPPLIED
1.5.1 Antenna.
1.5.2 Interconnecting Cables.
1.5.3 Receiver.
1.5.4 Mooring Plate P/N 073-00044-0001.
1.5.5 Adapter Plate P/N 073-00045-0000 (Front mounting only).
1.5.6 Punch Refer to Figure 2-5 (P/N 155-05235-0000) or other
appropriate drawing.
1.5.7 Filing Template Refer to Figure 2-5 (P/N 155-05235-0000) or other
appropriate drawing.
1.5.8 Crimp Tool Burndy Hytool M8ND
1.5.9 Extraction Tool Handle P/N 005-02012-0012, Burndy RXT20-4P3
1.5.10 Extraction Tool Tip P/N 005-02012-0013, Burndy RXK20-25
1.6 LICENSE REQUIREMENTS
None.
1.7 REQUIREMENTS FOR TSO’D VOR/ILS/GLIDESLOPE SYSTEM
Units used in conjunction with the KI 208, KI 209 must meet the specifications listed
below to comprise a completely TSO’d navigation system.
1.7.1 Navigation Receiver Requirements For Use with KI 208, KI 209.
1.7.1.1 The navigation receiver shall be authorized to the standards of TSO C40a,
C40b, C40c, and/or TSO C36c, C36d, C36e.
1.7.1.2 VOR phase error shall not exceed 1.5°.
1.7.1.3 Variation in VOR composite output to not exceed ±3 dB from 0.500 Vrms as
the RF input level of a Standard VOR Test Signal to the receiver is varied from
10 uV to 10,000 uV.
RELEASED FOR THE EXCLUSIVE USE BY: AIRCRAFT ELECTRONICS ASSOCIATION
UP536434