SERVICE KIT
SK 208-179B
(4) Attach t he TKS wire assembly to the S2034-1 Mo unt with one S2209 Tie.
L. (Refer to Figu re 14, View A-A.) Install the MS24524-23 BACKUP Swi tch (S 1024) and the C15Green
Tip on the 9910616-5 LED LAA Switch P late Assembly.
M. Install the MS24524-27 MAX FLOW Swi tch ( S 1023) and the C15Green Tip on the 9910616-5 LED
LAA Switch Plate Assembly.
N. Inst all the MS27407-1 PRIMARY Switch (S1022) and the C15Green Tip on the 9910 616-5 LED
LAA Switch Plate Assembly.
O. Wit h the kept attachment hardware, install t he 9910616-5 LED LAA Switch Plate A s s embly. (Ref er
to the Model 208 Maintenance Manual, Chapter 31, Ins trument and Control P anels - M aintenance
Practices.)
P. (Refer to Figure 12 and F igure 14.) Make sure t hat the TK S Cable Assembly is connected correctly
at all positions.
Q. (Refer to Figure 12.) In the low-profile TKS fairing, install t he con nec to rs from the TKS fluid and
equipme nt pack to JD003 an d J D004.
R. Inst all 2677 124-2 L SW PNL wiring in accordance with Figure 12, Sheet 1.
S. Install 267712 3-3 Windshield Ic e Detect Li ght L SW PNL wiring in ac co rdanc e w ith Fi gure 12,
Sheet 2.
20. As appl icable, accomplish SK 208-180 (or late st re vision) or SK208-175B (or latest revision) Low Airspeed
Awareness Sys tem In stallation fo r Airpl anes with TKS.
NOTE: Part Number SK208-180 (or latest revision) and part num ber SK208-175B (or latest r ev ision)
are separate items an d are not inc luded with S K 208-179 Low-Profile TKS Ice P rot ec tion System
Installation for Model 208B Airpl anes with Provisions.
21. Decrease the up angle of the elevators to 22 degrees, +1 degree or −0 degre e, as follows: (Ref er to the
Model 208 Maintenance Manual, Chapter 27, Elevat or - Maintenance Practices.)
A. Set the elevator to 22 to 23 degrees on t he UP mark on the elev ato r ri gging protractor.
B. Do the adjustm ent of th e up s top bo lt as necessary.
22. (Refer to Figure 10.) I nstall the necessary placards for t he TKS anti-ice system installation as follows:
A. (Refer t o Fig ure 10, View A-A and View B-B.) E dge seal the 7000-03 Solvent Caution Placa rds
with clear polyurethane enamel topc oat. (Refer to the Maintenanc e Manual, Chapter 20, Exte rior
Finish - Clean ing/ Painting.)
B. (Refer to Figure 10, Detail A.) Install the 2605076-14 Placard-TKS Filler Cap on t he left side of the
fuselage as follows:
(1) Clean area whe re placard is to be ins talled w ith i so propy l alcohol. (Refer to t he Maintenance
Manual, Chapter 20, Solvents, Sealants and Adhesives - Maintenance Pr ac t ices.)
(2) Install t he 2605076-14 Pl ac ard-TKS Filler Cap on the left side of t he fuselag e in the position
shown.
(3) Edge seal t he 2605076-14 Placard-TKS Filler Cap wi th clear polyurethane enamel top co at.
(Refer to t he Maintenance Manual, Chapter 20, Ext erior Finish - Cleaning/Pa inting.)
C. (Refer to Figure 10, View C-C.) Inst all the 2105015-7 Operational Limitations Placard adjacent
to the ov erhead console as follow s:
(1) Remov e the installed operationa l lim itations placard that is adjacent t o the overhead console.
(2) Clean the area where the new plac ard is to be installed with isopropyl alcohol. (Refer to the
Maintenance M anual, C hapt er 20, Solvents, Sealants and Adhesives - Maintenance Practice s.)
(3) Install t he 2105015-7 Ope rational Lim itat ions Placard adjacen t to the overhead cons ole in
the approximate posit ion shown.
SK208-179B
Page 30 February 7, 2013
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