PITOT/AOA PROBES - REMOVAL
AMM-34-10-10-001-C-801
1. General
A.
This task gives the procedures to remove the Pitot/Angle of Attack (AOA) probes.
B. There are two Pitot/AOA probes on the fuselage, forward of the cockpit. Access
procedures for the right Pitot/AOA probe are given in Job Setup.
NOTE: In the event the grounding jumper needs to be replaced, the entire probe must be
removed.
NOTE: In the event that the auxiliary heater needs to be replaced, the entire probe must
be removed.
2. Job Set-Up
SUBTASK AMM-34-10-10-001-C-921-001
A.
Make aircraft safe for maintenance. Refer to AMM-20-00-01-051-801 – Make Safe For
Maintenance.
B. To gain access to remove the left Pitot/AOA probe remove the access panel that follows:
• 211 CT - Nose Access Panel
C. To gain access to remove the right Pitot/AOA, use the Air Conditioning controls to open
the VCS doors, as follows:
(1) Connect AMC to right armrest USB port. Refer to Fig. 402.
(2) On the MFD ENVIR page, establish the following conditions:
• AIR COND: AUTO
• AFT Fan: AUTO
• FWD Fan: AUTO
• Cockpit Temp: MAX COOL
• Cabin Temp: MAX COOL
(3) Make sure the Forward and Aft VCS doors have fully opened. Refer to
AMM-21-00-00-071-801 – Air Conditioning - Adjustment/Test, .
Refer to Fig. 403.
D. Remove power from the aircraft.
CAUTION: AFT VCS DOOR MUST BE DISABLED TO PREVENT PERSONAL INJURY
AND DAMAGE TO EQUIPMENT IF AIRCRAFT POWER IS
INADVERTENTY APPLIED.
(1) Once electrical power is removed, disconnect the electrical connector on the aft VCS
door actuator.
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 401-Rem
Sep 30/20
© 2020 Eclipse Aerospace, Inc.
To Next Page
Loading...
Need help?
General
