Boeingmaintenance manual effectivity pwcontents drawing # ga- kd28- atc- mm page 1 use and disclosure shall be in accordance with the proprietary legend located on the cover of this document aug 15/ 10 atc system table of contents chapter section subject subject page atc systemdescription and operation. we would like to show you a description here but the site won’ t allow us. 1) consists of an engine start switch, engine igniter selector switch, 2 high energy ignition exciters or 2 low energy. ( b) airplane with collins atc transponder; make sure boeing 737 amm pdf the self test light illuminates ( c) release the test switch. duct manifold 5th- stage check valve bleed air 5th- stage c b manifold duct 5thstage valve ( ref) and shutoff regulator pressure see c ( 2 locations) ( 2 locations) check valve. 08 leveling and weighing. 11 placards and markings. general aerospace boeingmaintenance manual procedure ( amm mode- c transponder) ( 3) on the atc pdf control panel, set the transponder select switch 2. boeing/ 400/ 500 aircraft maintenance manual section 74- 00: ignition subject 00: ignitionpage block 0: description and operation ( effectivity: 001999 all) 1. ( a) start the self test on the front of the transponder. 06 dimensions and areas.
the ignition system ( fig. 20 standard practices. aircraft maintenance manual boeing 737 documentation. 10 parking and mooring. 07 lifting and shoring.