61-101-00802.EF1 Revision J Page | 22
(4) If value is not within tolerance, reject probe.
Note: The following values are valid as of this publication’s release date and are
provided as a reference. Refer to the Aircraft Maintenance manual for actual
test values.
Aircraft C90, C90A / B / GT / GTi / GTx & C99
100-380006-11, -69, -105, -139, -143, -175
100-380006-13, -67, -103, -187
100-380006-37, -71, -107, -141, -145, -173
100-380006-7, -73, -109, -183
Nacelle (C90 / C90A / B
/ GT / GTi / GTx)
100-380006-49, -79, -97, -125, -185
100-380006-77, -113, -171
Table 5 Probe Capacitance Empty (pF)
Aircraft A100, B100, E90 & F90
100-380006-11, -69, -105, -139, -143, -175
100-380006-13, -67, -103, -187
100-380006-37, -71, -107, -141, -145, -173
100-380006-93, -121, -179
100-380006-95, -123, -181
100-380006-7, -73, -109, -183
100-380006-43, -75, -111, -189
Nacelle (for A100, B100,
F90)
100-380006-41, -77, -113, -171
Table 6 Probe Capacitance Empty (pF)
Aircraft 200, 250, 300, 350 / 350i & 360
100-380006-11, -69, -105, -139, -143, -175
100-380006-55, -81, -115, -177
100-380006-37, -71, -107, -141, -145, -173
100-380006-93, -121, -179
100-380006-95, -123, -181
100-380006-41, -77, -101, -113, -147, -171
100-380006-35, -85, -119, -169, -197
100-380006-33, -57, -83, -117, -149, -151,
-167
Table 7 Probe Capacitance Empty (pF)