Document ID: chunk:federal_register_of_legislation:F2006B03954:body:0
Version: federal_register_of_legislation:F2006B03954
Segment Type: other
Provision Reference: 
Character Range: 0–1178

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Beechcraft 50 (Twin Bonanza) Series Aeroplanes

AD/BEECH 50/30 Engine Emergency Placard 9/79

 Applicability: All models.

            Requirement: Inspect emergency engine shutdown procedure placard on overhead or instrument panel for legibility and condition. If defaced or missing, fabricate a new placard using letters of 3mm height and affix to either overhead or instrument panel.

            Placard to read:

               EMERGENCY ENGINE SHUTDOWN PROCEDURES

                   1. MIXTURE CONT-IDLE CUT-OFF

2.        FUEL SELECTOR-OFF

3.        OIL SHUT-OFF HDL-UP AND LKD

4.        PROP CONTROL-FEATHERED

5.        THROTTLE-FULLY OPEN

6.        BOTH BOOST PUMPS-OFF

7.        MAGNETO SWITCH-OFF

8.        ALTNTR/GEN SWITCH OFF

 Compliance: Within 100 hours' time in service after 30 September 1979.

            Background: As the original engine emergency shutdown procedure decal may have become defaced or be otherwise illegible a more durable placard is to be installed as per a recent FAA requirement.