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3. Procedure

SUBTASK AMM-34-10-10-001-C-011-001

(Refer to Fig. 401.)

Disconnect electrical connector (17) from aircraft wiring harness.

B. Remove jam nut (15) from electrical connector (17) and remove electrical connector from

bracket (16) by removing .

C. Disconnect electrical connector (2) from Pitot/AOA probe (4) .

D. Disconnect Pitot tube assembly (3) from Pitot/AOA probe (4) .

E. Disconnect Pitot/AOA Auxiliary Heater electrical connector (17) from aircraft harness.

F. Remove jam nut (15) from Pitot/AOA Auxiliary Heater electrical connector (17) and

remove connector (17) from bracket (16) .

G. For the LH Pitot/AOA probe (Fig. 401, Sheet 2), remove the self locking nut (8) , lock

washer (9) , flat washer (10) , grounding jumper (7) , and the hex head screw (11) from

hole (12) in the aircraft structure.

H. For the RH Pitot/AOA probe (Fig. 401, Sheet 3), remove the self locking nut (8) , flat

washer (10) , grounding jumper (7) , and the hex head screw (11) from hole (12) in the

aircraft structure.

I. Remove five screws (5) that attach Pitot/AOA probe (4) to structure (1) .

J. Remove Pitot/AOA probe (4) with grounding jumper (7) attached and gasket (6) from

aircraft.

NOTE: Do not remove grounding jumper from probe unless it needs to be replaced.

K. If required for the LH Pitot/AOA probe (Fig. 401, Sheet 2), remove the screw (14) ,

washer (13) , and grounding jumper (7) from the Pitot/AOA probe (4) .

If required for the RH Pitot/AOA probe (Fig. 401, Sheet 3), remove the screw (14) ,

washer (13) , and grounding jumper (7) from the Pitot/AOA probe (4) .

EA500 Aircraft Maintenance Manual — 06-117751

Temporary Revision No. 34-21

EFFECTIVITY: ALL, POST MB 500-34-027 AND MB

500-34-028

34-10-10

CONFIG C

Page 402-Rem

Sep 30/20

Eclipse EA500 User Manual

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