B.
Do a leak test of the P2 and copilot S1 systems (
NOTE:
The static fittings on the drain collector tubes and the ADC are quick−disconnect
fittings. The leak test is necessary only if the regulatory authority of the country of
aircraft registration makes a leak test mandatory.
C.
Remove all tools, equipment, and unwanted materials from the work area.
D.
Close the access door that follows:
PANEL
NAME
MANUAL NO
REFERENCE
811
Main Avionics Compartment Door
Internal PSA Document
EFFECTIVITY: Ref page 1 of Blue Page
CRJ-700/900
AIRCRAFT MAINTENANCE MANUAL
PSA AIRLINES, INC REVISION
AMM - Insert after Task 34-11-00-100-805-A01 of AMM 34-11-00
NOTE:
The leak test is not required due to system quick-disconnect fittings meeting FAR
regulations approved by the FAA.
34-11-00-100-805-A01-PSA Rev D
Remove Rev 34-11-00-100-805-A01-PSA Rev C dated 04/03/17 and insert 34-11-00-100-805-A01-PSA Rev D dated 08/13/18
08/13/18
Page 4 of 5
Audited By TSS Dept. 10/17/18
Blue Page Current For Rev. 59
Audited By TSS Dept. 05/02/19
Blue Page Current For Rev. 61
