Page
165
The ELT (AF)(AP) has an automatic activation G-Switch. It is activated automatically upon a crash or
manually operated.
If for any reason, a fixed mounting is not required, the ELT (AF)(AP) can be used as a Portable Device, due to it ‘s
manual operated hand use Portability. Check Local and/or national regulations for this issue.
The model AK-451-(S) consists of an ELT main unit with integral antenna and a portable soft case.
The Main Unit features include: • ON / OFF / ARM Main Switch
•
Green ON Light (Red Light for AK-450)
•
RESET Push Button Switch
The Remote Unit features include: (Red Light for AK-450)
•
ON Push Button Switch
•
Green ON Light (Red Light for AK-450)
•
RESET Push Button Switch.
All functions of the AK-451 are under micro-controller control. A self-test routine checks ELT operation and
installation, then presents the results as visual and auditory
‘error code’ to aid in troubleshooting and to indicate status. Software is approved per requirements of RTCA/DO-
178B for level D software.
The battery pack consists of four D-size lithium, and is field replaceable. Rated life is
5 years or one hour of use, whichever comes first, as specified by FAR 91.207©.
(AK-450 has 6 cells “D” Size DURACELL)
Installation kits are available that contain all major components needed to install the beacon.
Application and Equipment Limitation
This manual constitutes FAA approved data as described in AC 43.9-1F, paragraph (h)(2) and AC 43-210, chapter
2, paragraph 201(a)(6) for major alterations. Not all installations are “major”; consult your local FAA ACO for
clarification.
In Canada, Installation of an ELT in an aeronautical product is carried out under a Supplemental Type Certificate
(STC). This is a separate regulatory requirement and should therefore refer to Ameri-King Document No. ICA-451
for the Operations and Instructions for Continued Airworthiness (ICA).
The conditions and tests required for TSO approval of this article are minimum performance standards. It is the
responsibility of those desiring to install this article on a specific type or class of aircraft to determine that the
aircraft installation conditions are within the TSO standards. TSO articles must have separate approval for
installation in an aircraft. The article may be installed only if further evaluation by the applicant documents an
acceptable installation and it is approved by the FAA Administrator. The article may be installed only if performed
under 14 CFR parts 43 or the applicable airworthiness requirement. For installations outside of the US,
contact your local civil aviation authority for guidance (Ref. TSO-C126 paragraph D).
Lithium battery safety concerns include the possibility of fire, venting violently, and venting of toxic gases (Ref.
TSO-C126 paragraph 5.a.(2)).
PHYSICAL CHARACTERISTICS:
•
SIZE AND WEIGHT:
Main Unit:
(4.27”Wx2.95”Hx5.64”L) 1lbs 14oz (AK-450 3 lbs. 1 oz.)
Remote Unit:
(1.58”W x 0.65”H x 2.00”L) 1.0 oz Transport Blade type, 451 017-3:
600 Knots
airspeed, 1.4 lbs Business Rod type, 451 017-2:
350 Knots airspeed, 0.5 lb
General Aviation whip type,
451 017-1:
300 Knots airspeed, 0.25 lb
Portable Antenna, 451 017-4:
(17”L) 4.0 oz
Mounting Tray & Velcro holder: (4.51”W x 0.75”H x 5.87”L) 4.0 oz
•
CASE AND COLOR:
No Sharp Edges, High Impact, Flame Retorted, Fire Resistant, Waterproof, High, Temperature ABS Plastic, Safety
International Orange Color.
Appendix F Page 2
Summary of Contents for 912 Dragonfly
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Page 25: ...Page 24 Drawing 1 ...
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Page 37: ...Page 36 Note for Hydraulic Brakes see Appendix B Drawing 7 ...
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Page 79: ...Page 78 Wiring1 jpg Drawing 28a ...
Page 80: ...Page 79 Wiring2 jpg Drawing 28b ...
Page 81: ...Page 80 elecLights jpg Drawing 28c ...
Page 83: ...Page 82 Drawing 29 ...
Page 85: ...Page 84 Drawing 30 ...
Page 92: ...Page 91 Appendix B Brakes Manual for BX1320 BX1000 Appendix B Page 1 ...
Page 93: ...Page 92 Appendix B Page 2 ...
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Page 104: ...Page 103 Figure 1a Description of Display Pages ...
Page 105: ...Page 104 Figure 1b Description of Display Pages ...
Page 138: ...Page 137 Appendix C EIS 4000 912 914 ...
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Page 140: ...Page 139 Appendix C EIS 4000 912 914 ...
Page 141: ...Page 140 Appendix C EIS 4000 912 914 End Appendix C ...
Page 155: ...Page 154 Appendix E2 Powerfin Prop Page 2 ...
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Page 164: ...Page 163 Appendix E2 Powerfin Prop Page 11 End of Appendix E2 ...
Page 187: ...Page 186 By Memphis Soaring FIGURE 3 Common Signals ...