Eclipse EA500 Maintenance Manual page 42

3. Procedure
SUBTASK AMM-34-10-10-001-C-011-001
(Refer to Fig. 401.)
A. Disconnect electrical connector
B. Remove jam nut
bracket (16) by removing .
C. Disconnect electrical connector
D. Disconnect Pitot tube assembly
E. Disconnect Pitot/AOA Auxiliary Heater electrical connector
F. Remove jam nut
remove connector
G. For the LH Pitot/AOA probe
washer (9) , flat washer
hole (12) in the aircraft structure.
H. For the RH Pitot/AOA probe
washer (10) , grounding jumper
aircraft structure.
I. Remove five screws
J. Remove Pitot/AOA probe
aircraft.
NOTE: Do not remove grounding jumper from probe unless it needs to be replaced.
K. If required for the LH Pitot/AOA probe
washer (13) , and grounding jumper
L. If required for the RH Pitot/AOA probe
washer (13) , and grounding jumper
EFFECTIVITY: ALL, POST MB 500-34-027 AND MB
500-34-028
EA500 Aircraft Maintenance Manual — 06-117751
(17) from aircraft wiring harness.
(15) from electrical connector
(2) from Pitot/AOA probe
(3) from Pitot/AOA probe
(15) from Pitot/AOA Auxiliary Heater electrical connector
(17) from bracket (16) .
(Fig. 401, Sheet
(10) , grounding jumper
(Fig. 401, Sheet
(7) , and the hex head screw
(5) that attach Pitot/AOA probe
(4) with grounding jumper
(Fig. 401, Sheet
(7) from the Pitot/AOA probe
(Fig. 401, Sheet
(7) from the Pitot/AOA probe
© 2020 Eclipse Aerospace, Inc.
Temporary Revision No. 34-21
(17) and remove electrical connector from
(4) .
(4) .
(17) from aircraft harness.
2), remove the self locking nut
(7) , and the hex head screw
3), remove the self locking nut
(11) from hole
(4) to structure (1)
(7) attached and gasket
2), remove the screw
(4) .
3), remove the screw
(4) .
(17) and
(8) , lock
(11) from
(8) , flat
(12) in the
.
(6) from
(14) ,
(14) ,
34-10-10
CONFIG C
Page 402-Rem
Sep 30/20