AD/BEECH 23/36 - Stabilator Trim Tab Actuator Rod
1AD/BEECH 23/36 - Stabilator Trim Tab Actuator Rod
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Image unavailable in extracted text Beechcraft 19, 23 and 24 Series Aeroplanes
AD/BEECH 23/36 Stabilator Trim Tab Actuator Rod 8/78
Applicability: Models B19 with S/Nos. MB-558 through MB-886.
Models C23 with S/Nos. M-1413, M-1414, M-1416 to M-1418, M-1420 to M-1422, M-1424 to M-1438, M-1440 to M-1446, M-1448 to M-2009, M-2011 to M-2015, M-2017 to M-2020.
Models B24R and C24R with S/Nos. MC-151 to MC-559, MC-561 to MC-563, MC-565 to MC-568, MC-571.
Requirement: Action in accordance with Beechcraft SI No. 0994. Compliance: Within 25 hours time in service after 3 July 1978.