Cessna 560 - Page 36

Aug 13/2004 560-34-114
Revision 2 - Jan 2/2007 Page 32
Citation SERVICE BULLETIN
SB560-34-114
NEW P/N QUAN-
TITY
KEY WORD OLD P/N INSTRUCTIONS/
DISPOSITION
9622012-36 1 Angle
9622012-39 1 Angle
9622012-41 1 Angle
9622012-43 1 Angle
9622012-45 1
Channel
9622012-47 1 Angle
9622012-52 1
Shear Clip
9622012-58 1
Hat Section
9622012-60 11 Access Panel
9622012-61 1 Panel
9622012-63 1
Clip
9622012-68 1 Tee
9622012-69 1
Shear Tie Pa
nel
9690564-1 1
TCAS II Cable Assembly
NOTE: In addition to SB560-34-114-0 Kit, the following will be necessary to accomplish this service bulletin
on airplanes that do not have the TCAS I system installed and will have the 066-01146-1211 TCAS II
Computer installed at location Option C.
NEW P/N QUAN-
TITY
KEY WORD OLD P/N INSTRUCTI
ONS/
DISPOSITION
SB560-34-114-4 1 Kit, consisting of the following
parts:
MS21073L08
1 Nutplate
MS21075L06N 6 Nutplate
MS21075
-8N 6 Nutplate
MS24694S5
2
Screw
MS27039-0808
8
Screw
MS35206-230
2
Screw
MS35207-261
2
Screw
S1050-1 4 Grommet
S1741-
14Anchor
S2526-2
2
Block and Connector
S2800-39
2
Connector Kit
S2899L1.0
1
Circuit Breaker
S2899L5.0
1
Circuit Breaker
066-0
1146-1211
1 TCAS II Processor