Ameri-king ak-450 elt manual

 · Ameri-King Corporation Document IM, “INSTALLATION OPERATION MANUAL,” Revision A, dated Octo; and Ameri-King Start Printed Page Corporation Document IM, “INSTALLATION AND OPERATION MANUAL,” Revision NCh, dated July 5, ; specify accomplishing certain inspections of the ELT but do not . a Model AK() and AK() series ELT produced by Ameri-King Corporation. (j) Optional Terminating Action Doing the applicable action specified in paragraph (j)(1) or (j)(2) of this AD terminates the actions. Ameri-King AK Series Installation And Operation Manual. Page 1 July 5, INSTALLATION AND OPERATION MANUAL MODEL AK () Series MHz ELT Emergency Locator Transmitter with GPS/NAV position AMERI - KING CORPORATION Sampson Lane Huntington Beach, CA Tel: () Fax: () Email: .

The reported ELT failures were not a mix of TSO-C91 units and TSO-C91a units. As stated in the NPRM, we received 73 reports of ELT failures for Ameri-King Corporation Model AK() series ELTs, which are approved under TSO-C91a, and AK() series ELTs, which are approved under TSO-C91a and TSO-C The FAA has issued an airworthiness directive (AD) requiring repetitive inspections of Ameri-King Corp. Model AK and AKseries emergency locator transmitters (ELTs) in response to multiple reports of ELT failures and a report of “noncompliance to quality standards and manufacturer processes.”. ELT AK Janu 7of10 NOTE FordetaileddescriptionseeInstallationandOperation Manual For Model AK, document No. IM, Rev. A dated 10/18/95 or later applicable version, which is delivered with the ELT. SECTION 8 AIRPLANE HANDLING, SERVICING AND MAINTENANCE TESTING ELT FUNCTION NOTE The ELT function should be tested every 3 months.

Description: The AK ELT from Ameri-King is FAA TSO-C91a approved and meets FCC rule for improved satellite detection. It. except that the aircraft has an Ameri-King AK ELT installed. Here is a copy of the AD and the ELT manual it references. AK This is important during Portable Use. Mini Remote Control Panel with independent Battery built-in, therefore Interface with Aircraft Electrical Power is not.