COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 107 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Radio Communication and Navigation Equipment
AD/RAD/63 KT 76A ATC Transponder 10/98
Applicability: AlliedSignal KT 76A Air Traffic Control (ATC) Transponders, part numbers 066- 1062-00, -10 and -02 with serial numbers 93,000 through 109,999 inclusive.
Note: These transponders are known to be installed on, but not limited to, the following series of aircraft:
Manufacturer Aircraft Series
Cessna Aircraft Company 172, 182, T182, R182, 206, P206, U206, TP206, 210, T210, P210, 310, E310,
T310 and 421
Twin Commander Aircraft Company 500, 520, 560, 680, 681, 685, 690, 695
and 720
The New Piper Aircraft Corporation (formerly known as Piper Aircraft Corporation)
Raytheon Aircraft Corporation (formerly known as Beech Aircraft Corporation)
PA-31, PA-32 and PA-34
E33, F33, G33, 35, J35, K35, L35, M35, P35, S35, V35, 36, A26, B36, D55, E55, 56, A56, 58, 58A, 95, B95, D95 and E95
Mooney Aircraft Corporation M20 McDonnell Douglas Helicopter Company 500N
Requirement: Replace the two resistor network modules, RM401 and RM402, with new glass- coated parts in accordance with the ‘Modification Procedure’ section of AlliedSignal Service Bulletin SB KT 76A-7 dated July 1996. (When accomplished, this replacement is referred to as Mod 7.)
Note: FAA AD 98-14-03 Amdt 39-10637 refers.
Compliance: Prior to installation in an aircraft, but no later than 10 September 1999. This Airworthiness Directive becomes effective on 10 September 1998.
Background: The FAA has advised that KT 76A ATC transponders have been identified as transmitting misleading encoding altimeter information to ground-based ATC radar sites and proximate Traffic Alert and Collision Avoidance System (TCAS) equipped aircraft. The actions specified by this directive are intended to prevent the transmission of misleading encoding altimeter information from affected aircraft.