Ameri-king АК-451-Series Instrukcja Użytkownika Strona 1

Document No. ICA-451 OPERATIONS AND INSTRUCTIONS FOR CONTINUED AIRWORTHINESS (ICA) MANUAL FOR MODEL AK-45

19 The ELT may be ID coding programming during the aforementioned 20 seconds window period. If no programming happened the ELT will then enter the

212.3.3.1 Monitor 121.5 MHz using the Aircraft Com Receiver or Portable Hand Held Receiver. Turn the Squelch all the way up or ON. 2.3.3.2 Ensure

232.3.5.2 Transmitter Self-Test: Turn and hold the main switch, from the "OFF" position to the "SELF TEST" position. The Green

25 Front label Back label FORWARD To Activate: Lift & flip the switch to the “ON” position Verify: The G

27by a rapid reversing action. Verify that the ELT has been activated by use of the Wattmeter, the Airplane’s VHF Radio Communications Receiver when

29Note: If there is no programming command input in this time window, the ELT will enter the Self-Test mode, and you cannot program the ELT. In this

31site is instantly known due to the aircraft's navigation system position data communication with the ELT. Without the position data being tran

333.1.10.4 24-Bit Address Installation Test (mandatory for Installations reprogramming by Ameri-King’s authorized dealer): Verify the 24 Bit Addre

353.2 PERIODIC MAINTENANCE (INSTRUCTION FOR CONTINUED AIRWORTHINESS FOR CANADIAN INSTALLATION: REFERENCES: Canadian Aviation Regulations CAR S

37Adjust the reference amplitude to place the peak of the carrier slightly above the top graticule fine. Enable the "fine" amplitude adjust

3DOCUMENT NO.: IM-451 REV. NC APPLICABILITY Model/Part No.: Fixed Whip Antenna 451017-1B 406/121.5 MHz Or Fixed Rod Antenna 451017-2A 406/121.5/24

393.2.3.4 Current draw tests: CAUTION: The following tests involve measurement of the lithium battery pack. Exercise extreme caution to avoid causi

41PERIODIC MAINTENANCE CHECK LIST WITH COMPLIANCE CROSS REFERENCES In the United States, minimum maintenance requirements for ELTs are stated in FAR

43 FAR 91.207(d); 91.409 and 43 Appendix D. Transport Canada Civil Aviation Part V Airworthiness Standards Chapter 551.104 (d) (1) (VI) Battery cap

45 (D) Battery Replacement And Recharging (Checks are to be performed every year) 1.4.1 ELT Main Battery Replacement Check 1.4.2 ELT Remote Unit

53.1.3 Corrosion Inspection for Remote Wiring Modular Cable ...26 3.1.4 Expiration Date Check...

7SECTION I GENERAL INFORMATION 1.1 SCOPE This manual contains information necessary for the Operations and Instructions for Continued Airworthine

9PHYSICAL CHARACTERISTICS: • SIZE AND WEIGHT: Main Unit: (4.27”Wx2.95”Hx5.64”L) 1lbs 14oz Remote Unit: (1.58”W x 0.65”H x 2.00”L) 1.0 oz Tr

11Arnav Systems Inc.: • R50, R50i, STAR 5000, FMS 5000, MFD (Multi-Functional Display). II Morrow: • FLYBUDDY, 2001 NMS Trimble Nav Inc.: • NAV

131.4 BATTERY REPLACEMENT INSTRUCTIONS 1.4.1 ELT MAIN UNIT BATTERY REPLACEMENT INSTRUCTIONS The Ameri-King Corp. Model AK-451 ELT is designed to u

151.4.2 ELT REMOTE UNIT BATTERY REPLACEMENT INSTRUCTIONS The ELT Remote Unit is designed to be powered by a Duracell DL1/3NB 3 Volt Lithium Batteri

17weights and severe penetrator tests, and continue to operate normally. Continued operation in a temperature range of -20 degrees Celsius to +55 deg