Eclipse EA500 Maintenance Manual page 51

N. Use PRC-Desoto aerodynamic smoothing sealant (PR-2050) to close gaps and seal
around Pitot/AOA probes.
Maintenance Practices.
4. Job Close-Up
SUBTASK AMM-34-10-10-041-C-921-002
CAUTION: MAKE SURE ANY PACKING/MATERIALS SUPPLIED WITH THE UNIT ARE
REMOVED AND NOT LEFT IN PLACE BETWEEN THE PROBE BODY AND
THE AIRCRAFT AFTER INSTALLATION.
A. If applicable, discard packing block after installation.
B. Do an inspection/check of the (applicable) Pitot/AOA probe following installation. Refer to
AMM-34-10-00-021-801 – Flight Environment Data - Inspection/Check.
C. Reconnect the electrical connectors on the aft VCS door actuator if removed.
D. Apply power to the aircraft.
(1) Connect AMC to right armrest USB port. Refer to
(2) Make sure that the Forward and Aft VCS doors have fully closed if opened. Refer to
AMM-21-00-00-071-801 – Air Conditioning - Adjustment/Test,
Refer to Fig.
E. Do adjustment/test of the Pitot/AOA probe(s) following installation. Refer to
AMM-34-10-00-071-801 – Flight Environment Data - Adjustment/Test.
CAUTION: DURING THIS TEST, THE HEATERS WILL BE COMMANDED ON BY THE
SYSTEM. RH AND LH PITOT/AOA PROBES WILL HEAT UP TO
APPROXIMATELY 500°C. HARM TO PERSONNEL OR EQUIPMENT CAN
OCCUR IF TOUCHING THE PROBES. DO NOT LEAVE ON FOR
EXTENDED TIME. ALLOW 10 MINUTES AFTER TEST FOR PROBES TO
COOL.
F. Do adjustment/test of the Pitot/AOA probe heat. Refer to
Pitot and Static Anti-Ice System - Adjustment/Test
G. Install access panel that follows as necessary:
• Install 211 CT - Nose Access Panel. Refer to
Access Panels.
H. Remove power from the aircraft.
I. Remove all tools, equipment and unwanted material from work area.
J. If all other maintenance is complete, return aircraft to service. Refer to
AMM-20-00-02-051-801 – Return To Service (After Maintenance).
EFFECTIVITY: ALL, POST MB 500-34-027 AND MB
500-34-028
EA500 Aircraft Maintenance Manual — 06-117751
AMM-20-08-00-051-801 – Sealants and Adhesives -
403.
© 2020 Eclipse Aerospace, Inc.
Temporary Revision No. 34-21
Fig. 402.
.
AMM-30-30-00-071-C-801 –
.
AMM-06-50-00-051-801 – Aircraft
34-10-10
CONFIG C
Page 403-Inst
Sep 30/20