Ameri-King AK-950L User manual
Document No.: ' IM-950
INSTALLATION
& OPERATION
MANU
AL
for
·-·
·------
--
-----
PIN
AK-950
L-
GNS
430/
/530/S30W
(GARMIN
INTERNATfONAL
INC.)
GPS 1NAV SWITCHING & ANNUNCIATOR PANEL
''
Per TSO-C129a, RTCA D0-208 and D0-160c Requirements
AMERI-KING CORPORATION
17881 Sampson Lane
Huntington Beach, CA 92648
Tel: (714) 842-8555
Fax: (714) 842-4235
Email: [email protected]
Website: www.ameri-king.com
: ;
~
24-62·91
The document reference is online, please check the correspondence between the online documentation and the printed version.
1.1
1.2
1.3
1.4
1.4.1
1.4.2
1.4.3
1.
5
1.6
1.7
2.1
2.2
2.2.1
2.2.2
2.2.3
2.2.4
2.2.5
2.3
2.4
2.4.1
2.4.2
INS 1
ALLA
li
UN
ANU
Uf't:ll"
IIUI"
IVI"I"U"L,
"IUUI:L
Hl\
.,;_,v
GPS 1
NAV
SWITCI-IING &
ANNUNCIATOR
PANEL
TABLE OF CONTENTS
Table
of
Contents ···············································
SECTION 1
GENERAL INFORMATION
Scope
................................................................
3
Description ..................................................... .... 3
Technical Characteristics
......................................
6
Front Panel Contrais and Annunciations .................. 8
Contrais
.......................................................
8
Annunciations ......... ...................................... 9
Interface ....................................................... 10
Equipment Limitations ............ .. ............................
11
Major Components ............... ................................
11
Accessories supplied .............. ............ ................ ..
11
SECTION
Il
INSTALLATION
AND
TEST
Unpacking and lnspecting Equipment ...................... 13
Mechanical Installation .............. .................... ........
13
Equipment Location ........................................ 13
Cooling
.........................................................
13
Additional Annunciations ............ ............. .. ...... 15
Additional
Rel
ays ............................................ 15
Rou
ting
of
Ca
bles ........ ................................... 15
Electrical Installation ............................................. 15
Post Installation Test .... ........ .
..
.... .............. .. .........
21
Pre
Installation Tests ... ...... ....
......
.....
......
......
...
21
Operating Instructions .....................................
21
1
3.1
3.2
4.1
4.2
4.3
1.1
2.1
3.1
3.2
3.3
INS 1
ALLA
li
UN
ANU
UPtHA
li
UN
MANUAL,
MUUEl
AK-!IbU
GPS 1
NAV
SWITCHINO
&
ANNUNCIATOR
PANEL
...
,.,
TABLE
OF
CONTENTS CCONT"D)
SECTION
Ill
OPERATION
General
..............................................................
23
Operation
SECTION
IV
WARRANTY
AND
SERVICE
23
Limited
Warranty
.......................................
....
......
25
Repair Service .....................................................
27
Factory Comprehensive Test Service
......................
27
LIST OF FIGURES
Outline Drawing
for
ali Series ................................ 4
Cutout
Dimensions
for
Panel
Mounting
...................
14
Schematic Pino
ut
for
Connecter ..
~.........................
16
E~ectrical
Schematic Diagraîn ................................
18
Wiring Diagram
.......................................
:............ 19
APPENDIX A
Environmental Qualification
form
RTCA 1
D0160C
....
28
2
24-62·91
The document reference is online, please check the correspondence between the online documentation and the printed version.
1.1
1.2
INSTALLATION AND OPERATION
MANUAL,
MODEL
AK-960
OPS
1
NAV
SWITCHINO & ANNUNCIATOR PANEL
SCOPE
SECTION 1
GENERAL INFORMATION
This manual contains information necessary for the
installation, test and operation
of
the model AK-950L,
GPS
1NAV Switching and Annunciator Panel, manufactured
by Ameri -King Corporation, California, U.S.A.
DESCRIPTION
The
AK-950L
is
a self-contained
GPS
1 NAV Switching and
Annunciator Pimel.
lt
combines
ali
the necessary functions
required for
switching
HSI
1
CDI
data inputs between a
conventional NAV (VOR) receiver and the approach-certified
GPS
receiver.
ln addition, the
AK-950L
contains several
GPS
status
annunciations
used
to indicate
modes
selected
by the front
panel switches and various inputs from the
GPS
receiver.
Features include Incandescent lamps
with
16,000
hours
average life, built in
Automatic
Dimming and Test for
Annunciator Panel.
Refer
to
figure
1-1
for Outline Drawing for ali Series for ali
Models' Annunciation Displays and Switches.
The following
GPS
system are applicable:
Model AK-950
L-
GNS 430/' /530/530W
for GNS 430/ /S30/S30W
Garmin International Inc.
3
INSTALLATION AND OPERATION MANUA1, MODEJ,;AK-860
OPS
1
NAV
SWITCHINO & ANNUNCIATOR PANEL
2.830
l l
~
1.050
~
FIGURE
1-1a.
OVERALL DIMENSIONS
Ql.JlJINE DRAWING
PIN AK-950
L-
GNS
430/;,
""
/530/530W
GPS/NAV
Switching
and Annunciator Panel
4
24-62·91
The document reference is online, please check the correspondence between the online documentation and the printed version.
NTALLATION
AND
Ol"fRAnoN
MAHVAL,
MOOEL
AK-160
OPI
1
NAV
SWITCHINO
lo
ANHUNCIATOR
PANEL
5
INSTALLATION
AND
OPERATION
MANUAL,
MOOEL
AK-960
OPS 1
NAV
SWITCHINO
..
ANNUNCIATOR
PANEL
1.3
TECHNICAL CHARACTERISTICS
§PECIFICATIONS:
TSO COMPLIANCE:
PHYSICAL CHARACTERISTICS:
• PANEL CUTOUT
SIZE
AND WEIGHT:
GENERAL SPECIFICATIONS:
•
POWER
INPUT:
• LAMP
BULB
TYPE:
• RELAY
TYPE:
-No.
of
avallable Polos:
-Switching Current 1
Voltage:
-Carrying Current 1
Voltage:
• Contact Resistance:
Contact Material:
• Switching
lime:
-lnsulation Resistance:
-
lite
Expectancy:
-Coll Resistance
CHARACTERISTICS;
ISO·
C129a
Panel Mounted,
1.00"
x
2.12"
0.31bs
(10.0-
32.2) Vdc
(5.9 -'7.4) Watts Nominal
0.214
Amp. @
28
Vdc, Nominal.
0.630
Amp.@
14
Vdc, Nominal.
0.654
Anip. @
28
Vdc, Momentary
Test Mode only.
1.575
Amp. @
14Vdc,
Momentary
TE!st
Mode
~nly.
Dual lamp'
for
each Annunclator.
PIN
6838
for
28
Vdc.
P/N
8111
for
14
Vdc.
Tl
Incandescent;
16,000
hours
average lite.
3 Polos; bouble
throws
2 Amp
/•220
Vdc maximum
2 Amp 1
220
Vdc maximum
60 milli • ohm max
Gold overtay
(1 · 2) milli • seconds
1,000
r:n~ga
·ohm
@
600
Vdc
1
00
million mechanical operations
.2 million electrical operations @30Vdc
2880
Ohm @
24
Vdc; ·
1028
Ohm @
12
Vdc.
6 '
24-62·91
The document reference is online, please check the correspondence between the online documentation and the printed version.
INSTALLATION AND OPERATION
MANUAL,
MODEL
AK-960
OPS
1
NAV
SWITCHINO & ANNUNCIATOR PANEL
• AUTO DIMMING: Built in
ENVIRONMENTAL TEST SPECIFICATIONS:
• RTCA
D0-208
A1/D1
• RTCA
D0-160C
ENV. CAT.:
ClAC/XXXSXXXSXXXXBXB
• TEMP. AND ALTITUDE:
Low
Temperature:
High Temperature:
• TEMP. VARIATION:
• HUMIDITY:
• SHOCK:
• VIBRATION:
• MAGNETIC
EFFECT:
•
POWER
INPUT:
Category
A2
&
D1
-20
deg. C Operating;
-55
deg. C Storage.
+
70
deg. C Operating;
+
85
deg. C Storage.
Category C
2 deg. C minimum per minute
Category A
95%
RH,
50
hours operating
6
G,
11
+
1-
2 msec, operational
15
G,
11
+
1-2
msec, crash safety
Categories M and N
Category A
Less than
0.3
m
Category B
Normal Operating: (
10.0-
15.1) Vdc
(20.0-
30.3) Vdc
Abnormal Operating:(
11
.0
-16.
1)
V
de
(22.0-
32.21 Vdc
• VOLTAGE
SPIKE:
Category B
• AUDIO
FREO.
CONDUCTED
SUSCEPTIBILITY: Category B
• INDUCED SIGNAL
SUSCEPTIBILITY: Category A
•
RF
SUSCEPTIBILITY: Category T
• EMISSION
OF
RF
ENERGY:
Category A
1.4
1.4.1
1.4.
1.1
INSTALLATION AND OPERATION
MANUAL,
MODEL
AK-960
GPS
1
NAV
SWITCHING & ANNUNCIATOR PANEL
FRONT PANEL CONTROLS
AND
ANNUNCIATIONS
CONTROLS
CONTROLS
FOR
MODELS
AK-950-
GNS530 (GARMIN):
CDI
Switch:
OBS
Switch:
TEST:
Momentary
action
Switch,
when
pressed, will select NAV (VORI
or
GPS
presentation on HSI 1CDI.
Momentary
Switch,
when pressed,
will
select AUTO 1 HOLD
OBS
Sequence
Mode.
Push Button
switch
for
TEST
function
for
ali Annunciation lamps.
8
24-62·91
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1.4.2
INSTALLATION
AND
OPERATION
MANUAL,
MODEL
AK-960
GPS
1
NAV
SWITCHING & ANNUNCIATOR PANEL
ANNUNCIATIONS
1.4.2.1 ANNUNCIATIONS
FOR
AK-950
l - GNS
430
/
530
IGARMINl:
VLOC (White):
NAV
(VORI
information
presented on
the
GNS
GPS
(Green):
GPS
information
presented on the
GNS
TERM (Green):
GPS
is active engaged in the Terminal
mode.
APR (Green):
GPS
is
actively
engaged in
the
approach
mode.
OBS (Green):
GPS
waypoint
Sequencing is in Hold Mode.
AUTO (White): GPS
waypoint
Sequencing is in
Auto
Mode.
MSG (Amber):
GPS
message alert,
from
the
GPS
receiver.
WPT (Amber):
GPS
waypoint
alert,
from
the
GPS
receiver.
INTEG
(Amber):
INTEG
lntergrity
Alert,
from
the
GPS
receiver.
9
INSTALLATION
AND
OPERATION
MANUAL,
MODEL
AK-960
GPS
1
NAV
SWITCHING & ANNÙNCIATOR PANEL
1.4.3
INTERFACE
1.4.3.1
INTERFACE
FOR
P/N
AK-950
l - GNS
430
1
530
COl
Switch:
(Pin 67)
OBS
Switch:
(Pin
73
l
VLOC:
(Pin 62)
GPS:
(Pin 66)
AUTO:
(Pin 72)
OBS:
(Pin 74)
TERM:
(Pin 77)
APR:
(Pin
·71;
Provides a
momèntary
logic
low,
to
the
GNS receiver,
for
Switching
between
VLOC and
GPS
Source.
Provides a
momentary
logic
law,
to
the
GNS
recèi~er,
for
Switching
between
.
.,
,.
Automatic
and Hold Mode,
for
GPS
Waypoint
Sequencing.
Receives an alternate logic
law
from
the
GNS
to
annunciata VLOC.
Receives an alternate logic
law
from
the
GNS
to
annunciata GPS.
l'
' -
Receives an alternate logic-
law
from
the
GNS
to
annunciata AUTO.
Receives an alternate logic
law
from
the
GNS
to
annunciata OBS.
Receives an alternate logic
law
from
the
GNS
to
annunciata TERM.
Receives an alternate logic
law
from
the
GNS
to
annunciata APR.
MSG 1
WPT
1
INTEG:
(Pins
75
1
Receives
an
alternate
logic
Law
from
the
GNS
to
annunciate
MSG
1
WPT
1 INTEG.
76
1
62)
10
24-62·91
The document reference is online, please check the correspondence between the online documentation and the printed version.
INSTALLATION AND
OPERA
Tl
ON
MANUAL,
MODEL
AK-950
GPS/NAV
SWITCHING
& ANNUNCIATOR
PANEL
1.5
EQUIPMENT
LIMITATIONS
The AK-950 series control units contain specifie dash numbers to be
used with various GPS receivers. The installer must match the correct
controller part number with the GPS receiver being installed.
This equipment GPSINAV switching & Annunciator Panel is approved
for installation with the following mode! number only:
GPS mode! GNS 430 1530 1530W
Garmin International Inc.
Installation
of
this equipment to any other GPS
is
disapproved.
The condition and tests required for TSO approval
of
this article are
minimum performance standards.
lt
is the responsibility
ofthose
desiring
to install this article either on or within a specifie type or class
of
aircraft
to determine that the aircraft installation conditions are within the TSO
standards. The article may be installed only
if
further evaluation by the
applicant documents an acceptable installation and
is
approved by the
Administrator.
NOTE: Anytime the AK-950 is disconnected or removed from the
aircraft, the HSI 1CDI will be inoperative in both NAY (VOR) and GPS.
1.6
MAJOR
COMPONENTS
The system
is
comprised
of
one major component, the AK-950,
GPSINAV Switching and Annunciator Panel.
1.7
ACCESSORIES
SUPPLIED
1.7.1 INSTALLATION KIT:
PARTNO.
DESCRIPTION
9500001
Pl,
Mating Connector Kit.
High Density D Subminiature Conn.
Plug,
78
Female Crimped Pins, with
Backshell and Thumbscrews.
PIN 162X 11989X & FK22SL05
(Conec Corporation)
11
INSTALLA
Tl
ON AND
OPERA
Tl
ON MANUAL,
MO
DEL
AK-950
GPSINAV
SWITCHING
& ANNUNCIA
TOR
PANEL
9500002 Optional Pre-fabricated Cable
Assembly with MIL-SPEC shielded
Cable, including:
MIL-W-22759118-24-9
M27500-l-24-TG-2-T-14
M17500-1-24-TG-3-T-14
TYPE
OF
MA
TING
CONNECTOR
Hi Density D-Subminiature Connector,
78
Female Sockets Plug.
Information for Crimping Tool.
l.
Hand Crimping Tool: M22520/2-01
2.
Positioner:
3.
Extract/Removal Tool:
4.
Vendor Sources:
Daniel
PIN
AFMA
M22520/2-06
Daniel PIN
K41
M81969/1-04
Daniel PIN 91067-1
Daniel Manufacturing Inc.
6103 Anno Ave.
Orlando, FL 32809
Tel (407) 855-6161
Fax(407)855-6884
12
24-62·91
The document reference is online, please check the correspondence between the online documentation and the printed version.
INSTALLATION
AND
OPERATION MANUAL,
MODEL
AK-960
OPS 1
NAV
SWITCHINO & ANNUNCIATOR
PANEL
SECTION
Il
INSTAllATION
AND
TEST
2.1
UNPACKING
AND
INSPECTING EOUIPMENT
2.2
2.2.1
Extreme care
when
unpacking the equipment. Visual inspection
of
the equipment
for
evidence
of
damage incurred during
shipment.
Any
claim should be
promtly
filed
with
the
transportation
company.
Save the shipping container
to
subtantiate the claim. Retain the container and packaging
material
for
possible
future
use.
MECHANICALINSTALIATION
The
AK-950
is designed
with
the installer in mind. Ali
accessories
which
are required
for
completing system
installation are provided, including Pre-fabricated Wiring Cable
Assembly.
EOUIPMENT LOCATION
The
AK-950
must
be
mounted
as
close
to
the
pilot's
field
of
view
as
possible. The preferable location is near the HSI 1CDI
that
will
be displaying the
FPS
information.
The
unit
depth,
with
connecter
atttached,
must
also be taken
into
consideration.
Avoid
mounting
close
to
heater vents
or
other high heat
sources.
The indicator is secured in place behind the panel since
it
is
designed
for
rear
mount
only. Make a panel
cutout
as
shown
in Figure
2-1.
Secure the
indicator
in place
with
four
4-40
x
3/8
to
1
.0"
flat
head phillips
screws.
2.2.2
COOLING
No direct cooling is required.
As
with
any electronic
equipment, overall reliability
may
be increased
if
the
AK-950
is
not
located near any high heat source
or
crowded
next
to
ether
equipment. Means
of
providing a gentle air
flow
will
be a plus.
•13
INSTALLATION
AND
OPERATION
MA~~AL,
MODEL
AK-960
OPS 1
NAY
SWITCHINO
a.
ANNUNCIATOR
PANEL
R.130
{4 PLS)
l~
+cv
1.000
o.
750
0.175
~2.120-~
2.470
~~----1
(11.125
fhru
hole
for
4-40
screw
(4
PLS)
FIGURE
2.1 CUTOUT DIMENSIONS
FOR
PANEL
MOUNTING
14
24-62·91
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2.2.3
2.2.4
2.2.5
INSTALLATION AND OPERATION
MANUAL,
MODEL
AK-960
OPS
1
NAV
SWITCHINO & ANNUNCIATOR PANEL
ADDITIONAL ANNUNCIATIONS
Depending upon the installation and approving agency, you may
be
required
to
provide additional
NA
V Source Select external
annunciators near the HSI 1COl. Spare relay
contacts
on the
AK-950
connector
may
be used
for
this purpose.
ADDITIONAL RELAYS
ROUTING
OF
CABLES
Care
must
be taken
not
to
bundle the
AK-950
logic and
low
level signal lines
with
any high energy sources. Examples
of
these sources include
400
Hz
AC, Comm, DME,
HF
and
transponder
transmitter
coax.
Always
use shielded
wire
when
shawn
on the installation
print.
Avoid sharp bends in cabling
and routing near
aircraft
control
cables.
2.3
ELECTRICALINSTALLATION
Refer
to
figure 3-1
for
Schematic Pinout
Assignment
for
Connector, and figure
3-2
for
Electrical Schematic Diagram.
Wire the
aircraft
harness according
to
figure
3-3
Use at least
24
AWG
wire
for
ali connections. Vou
MUST use shielded
wire
where
shawn.
Avoid sharp bends and
routing cable near high energy sources. Care
must
be taken
to
tie the harness
away
from
aircraft
contrais and cables. Normal
installation techniques should be applied.
15
IN8TALLATION AND OPERATION MANUAL, MODEL
Al-160
OPS
1
NAV
SWITCHINO.
ANNUNCIATOR PANEL
CONNECTOR
REAR
VIEW
OF"
CONNECTOR
1 2 3 4 5 6 7 8 9 10
Il
12
13 14 15 16 17 18
19
20
• • • • • • • • • • • • • • • • • • • •
21
22
23 24 25 26
27
28 29 JO
31
32
JJ
34
J5
36 37
38
39
• • • • • • • • • • • • • • • • • • •
40 41 42 43 44 45 46 47 48
49
50
51
52
53
54
55
56 57 58 59
• • • • • • • • • • • • • • • • • • • •
60
61
62
63
64
65 66
67 68 69
70
71
72
73 74 75
76
77
78
• • • • • • • • • • • • • • • • • • •
000
78,
HI-Oenslty
0-Subminloture
Connecter
r-;-
2
3
4
5
f.------·.
6
7
8
9
10
11
12
1------
13
14
15
16
17
18
19
20
21
22
23
24
25
26
27
28
29
30
31
32
33
34
35
36
37
M
FIGURE
3-1
a
SCHEMA
TIC
PINOUT
FOR
CONNECTOR
16
24-62·91
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INSTALLATION
AND
OPERATION
MANUAL,
MODEL
Al·860
OPS
1
NAV
SWITCHINO
a.
ANNUNCIATOR
PANEL
OC
GROUND
INTEG
Annunciator
Alternate
Ground Input
VLOC Annunciator Alternate Ground Input
CDI
Momentary
Switch
Output
-GPS
Annunciator
Ground
Input
APR
Annunciator
Ground
Input
-AUTO
Annunciator
Alternats
Ground Input
-OBS
Momentary
Switch
Output
. OBS Annunciator
Alternats
Ground Input
MSG Annunciator
Alternats
Ground Input
-WPT
Annunciator
Alternats
Ground Input
TERf.!l
Annunciator
Alternats
Ground Input
+
14/28
VDC
POWER
INPUT
FIGURE
3-"1 b SCHEMA
TIC
PINOUT
FOR
CONNECTOR
17
MTALLATION
AND
OPERATION
MANUAL,
MODEL
Al-860
OPS
1
NAV
SWITCHINO
a.
~NMUMCIATOR
PAfiEl
AK-950
L-
GNS 430/' ·/530/530W
-
+14/2e
VDC
I'OW[P
llfi'Ul
-OC
CROUHD
62
INTEG
Amber
Annunc.
{Aiternate Ground Input)
VLOC
White
Annunc.
(Alternat~:
Grou
nd
Input)
GPS
Green
Annunc.
(Aiternate.
Gn:>Und
Input)
WPT
Alllher
Annunc.
(Aiternate
Gràund
Input)
77
TERM Green
Annunc.
(Aiternate
Ground
Input)
71
APR Green
Annunc.
(Aiternate
Ground Input)
75
MSG
Amber
Annunc.
(Aiternate
Ground Input)
74
OBS Green
Annunc.
(Aiternate
Ground Input)
AUTO
White
Annunc.
(Aiternate
Ground
Input)
COl
Mom
Switch
(Mometary
Ground Output)
OBS
Mom Switch
(Momentary
Ground Output)
FIGURE
3-2
ELECTRICAL SCHEMATIC DIAGRAM
18
24-62·91
The document reference is online, please check the correspondence between the online documentation and the printed version.
0
(Y)
Lt)
i
en
z
~
c
E
...
co
~
INSTALLATION AND OPERATION
MANUAL,
MODEL
AK-960
OPS
1
NAV
SWITCHINO & ANNUNCIATOR PANEL
PIN
AK-950
L-
GNS
430/"
----
r
:
INTEG
Anrl
~
62
~
INTEG
Amber
Annunc.
VLOC Ann. 1 66 VLOC White Annunc.
GPS
Annunc 2
70
GPS
Green Annunc.
WPT
Annunr
3 76 WPT Amber Annunc.
TERM Ann. 4 77 TERM Green Annunc.
·APR Annunc. 5
71
APR
Green Annunc_
MSG Ann. 6
76
MSG Amber Annunc.
OBS
Annunc- 7
74
OBS
Green Annunc.
[. 1
72
AUTO White Annunc.
COl
Mom
Sw
7'l
57
COl
Mom
Switch
OBS
Mom..êV~
71
73
OBS
Mom
Switch
,-
40
-
OC
CROUND
.........
Ps~q,
ri--
78
____
+14/28
VDC
POW[R INPUT
+
VV'
+14/28
VOC
()
6-
2A
/530/S30W
NOJU:
1.
Reler
16
GPS
Monuloclurer's
lnslollolion
Manuel
lor
Acluol
lnsloll'llion.
2.
Ali
Wlres
ore
24
AWG
minimum.
FIGURE 3_3
WJRJNG
DIAGRAM
for
AK-950L-
( )
for GNS 430/' /530/530W Garmin International Inc.
1~
24-62·91
The document reference is online, please check the correspondence between the online documentation and the printed version.
0
(Y)
--t
1
Cf)
z
<.9
c
E
'-
co
<.9
INSTALLATION AND OPERATION
MANUAL,
MODEL
AK-950
GPS
1
NAV
SWITCHING & ANNUNCIATOR PANEL
COHN[ClOR
AK-950
L -
GNS
430
1
530
r
~
INTEG Ann. 9
62
INTEG
Amber
Annunc.
VLOC
Ann.
1 66 VLOC
White
Annunc.
GPS
Annunc
2
70
GPS Green
Annunc.
WPT
Annunr
3
76
WPT
Amber
Annunc.
fTERM
Ann.
4
77
TERM Green
Annunc.
APR
Annunc.
5
1--
71
APR Green
Annunc.
MSG
Ann.
6
75
MSG
Amber
Annunc.
OBS
Annunc.
7
74
OBS Green
Annunc.
AUTO
Ann.
8
72
AUTO
White
Annunc.
CDI
Mom
Sw
7~
,_
67
CDI
Mom
Switch
OBS
Mom
Sv
71
1-·
73
OBS
Mom
Switch
1 40
--
OC
CROUND
'-r
P400,1
ri-
78
1 - +
14/28
YDC
POWfR INPUT
,l,
~
+14/28
YDC
0
0-
2A
NOT~?:
1.
Refer
16
GPS
Monufoclurer's
lnslollolion
Monuol
for
Acluol
lnslall'llion.
2.
Ail
Wires
ore
24
AWG
minimum.
FIGURE
3.3
WIRING
DIAGRAM
for
AK-950L-
( )
with
GNS-430
(Garmin
International
lnc.)
19
24-62·91
The document reference is online, please check the correspondence between the online documentation and the printed version.
2.4
INSTALLATION
AND
OPERATION
MANUAL,
MODEL
AK-960
GPS
1
NAV
SWITCHINO &
ANNUNCIATOR
PANEL
POST INSTALLATION TEST
After
completing
the
mechanical installation,
the
following
Post
Installation Function Tests
must
be performed.
2.4.1
PRE
INSTALLATION TESTS
2.4.2
With
the
AK-950L
disconnected,
turn
on
the
avionics master
switch
and
verity
that
the
aircraft
power
of
14
1
28
Vdc
are
on Connector Pin
78
(Annunciator
Power). Using an Ohm
Meter,
verity
that
Pin
40
is
aircraft
ground.
OPERATING INSTRUCTIONS
Refer
ta
GPS
Manufacturer'
s Installation Manual
for
complete
GPS
System Operating
Instructions.
The
following
paragraphs
described Lamp BAT 1DIM 1
Test
and VLOC 1
GPS
Switching
function
only.
2.4.2.1
OPERATING INSTRUCTIONS
FOR
MODEL
AK-950l-
GNS530
(GARMIN):
Turn
off
the avionics master
switch
and
connect
the
mating
connector
ta
the
AK-950L.
Turn
on the avionics master
switch
and the
AK-950L
should come on
with
the
following
annunciations:
1. VLOC
or
GPS
2. AUTO
or
OBS
Momentarily
press
the
TEST
Switch,
ali annunciations
should light.
Select
VlOC
using the COl Button. The presentation on the
GNS-
will
now
be
information
from
the VOR receiver.
Select
GPS
using the COl Button. The presentation on the
GNS-
will
now
be
information
from
the
GPS
receiver.
21
INSTALLATION
AND
OPERATION
MANUAL,
MODEL
AK-960
GPS
1
NA
V
SWITCHING
&
ANNUNCIA
TOR PANEL
Please refer
ta
the
GNS~530
Garmin's
Installation Manual
for·
the remaining
system
tests.
No periodic maintenance or calibration is necessary
for
continued
airworthiness
of
the
AK-950.
2.4.2.6
AUTO
DIMMING TEST:
A Photocell provides the
Auto
Dimming
function.
This can be
tested
by
covering
the
Photocell
by
hand and observing
the
change in brightness.
NOTE: 1. There is
an
Adjustment
Potentiometer located on
the side
of
the
unit.
Adjustment
should be made
when
the
unit
is installed in aircraft, and
with
night
time
lighting conditions.
2. Rotate
the
Potentiometer
clockwise
ta
dim
the
annunciators. Rotate the Potentiometer
coun~er-clockwise
to
make the annunciators brighter.
3. Do
not
use excessive in
ward
force on
the
alignment tool, and
do
not
use excessive rotational force.
Damage may result.
22
24-62·91
The document reference is online, please check the correspondence between the online documentation and the printed version.
3.1
3-2
INSTALLATION
AND
OPERATION
MANUAL,
MODEL
AK-950
GPS
1
NAV
SWITCHING & ANNUNCIATOR PANEL
GENERAL
SECTION
Ill
OPERATION
This section describes the operation
of
the
GPS
1NAV Switching
and Annunciator Panel, Madel
AK-950L.
OPERATION
3.2.1
OPERATION
FOR
MODELS
AK-950L-
GNS530
IGARMIN):
VLOC/GPS Pushing the CDI
Switch
selects the
MOMENTARY navigation source IVOR 1ILS 1LOC or
GPS)
SWITCH
ta
be
displayed or. the
GNS
GPS
OBS
SWITCH
MSG
WPT
ANNUNC.
Pushing the
GPS
OBS
switch
will cycle
the
GPS
receiver Waypoint Sequences,
between AUTO and HOLD mode.
The MSG annunciator is automatically
lit
when the
GPS
receiver initiates a message
lairspace warnings, steep turns, etc.).
MSG annunciation is automatically extinguished
by the
GPS
receiver. The WPT annunciator
flashes
as
the active
waypoint
in the
GPS
receiver
is approached along the route
of
flight.
23
INSTALLATION
AND
OPERATION
MANUAL,
MODEL
AK-950
GPS
1
NAV
SWITCHING & ANNUNCIATOR PANEL
VLOC
GPS
AUTO
OBS
TERM
APR
MSG
WPT
ANNUNC.
The VLOC 1
GPS
1AUTO 1OBS 1TERM 1APR
MSG 1WPT Annunciator is automatically
lit
upon the GNS- initiates the corresponding
status 1mode Indication.
24
24-62·91
The document reference is online, please check the correspondence between the online documentation and the printed version.
4.1
INSTAllATION
AND
OPERATION MANUAl, MODEl AK-960
OPS 1
NAV
SWITCHINO & ANNUNCIATOR PANEl
LIMITED
WARRANTY
SECTION
IV
WARRANTY
Ali
equipments
manufactured
by
Ameri-King
Corp. are
guaranteed
against
defective
materials
and
workmanship
for
a period
of
two
years.
Any
equipment
found
to
be
defective
due
to
material and
workmanship
during
this
limited
warranty
will
be repaired and
put
in original
manufactured
operating
condition.
An
option
of
extended
third
and
fourth
year
limited
warranty
become
valid
at
the end
of
this
second
year,
which
will
warrant
to
the original
owner.
This
Ameri-King
Corp.
warranty
is
void
unless
the
Warranty
Registration Card is filled
out
and
returned
to
Amer-King
Corp.
within
15
days
after
original
installation.
Ameri-King
Corp.
's
liability
und
er
this
warranty
is
limited
to
servicing, repairing, replacing
or
adjusting
any
equipment
returned
prepaid
to
the
factory
by
express
written
or
oral
authorization
for
that
purpose
and
to
repair
or
replace
defective
parts
thereof.
Repaired
equipment
will
be
returned
to
the
equipment
user
freight
pre-paid.
Shipping
charge
will
be paid one
way
only
by
Ameri-King
Corp.
Upon
discovery
of
a
condition
believed
to
be caused
by
a
defect
in
manufacturing,
Amer-King
Corp.
must
be
notified.
No
equipment
to
be
shipped
to
Ameri-King
Corp.
without
prior
authorization.
Any
equipment
returned
to
Ameri-King
Corp.
should
be
accompanied
by
a failure report, in
writing,
giving
full
particulars
in
support
of
the
claim.
This
limited
warranty
does
not
caver
or
apply
to
any
of
the
followings,
including:
misuse
of
the
equipment;
installation
or
operation
not
in
accordance
with
factory
instructions;
accidents
or
negligent
damage;
alterations
of
any
manner;
repair
by
other
25
INSTAllATION
AND
OPERATION MANUAL, MODEl AK-960
OPS 1
NAV
SWITCHINO & ANNUNCIATOR PANEl
factory;
changes in calibration
occuring
as a result
of
normal
use
of
the
equipment;
the
cast
of
labor, material,
or
other
expense
incidental
to
the repair,
installation,
removal
from
the
aircraft
or
replacement
of
the
equipment;
damaged during
shipment
or
installation;
any
persona! injuries
or
damage
to
property
resulting
from
the
installation
or
the
operation
of
the
equipment
or
the
failure
of
the
equipment
or
any
part
thereof, the
equipment
user assumes
the
risks
of
ali such injuries
or
damage.
ln such cases,
the
repair
will
be bitled
at
cast.
An
estimate
will
be
submitted
for
approval
before
~epair
is initiated.
Any
equipment
which
is
returned
for
warranty
and
found
not
to
be
defective
shall be charged a
minimum
handling and service
charge and
returned
e.a.o.
No
warranty
will
be activated.
for
Ameri-King
Corp.
products
unless the
installation
is approved
by
an
FAA
Certified Installer
and the
warranty
card is
completed
by
the
supplying
dealer
or
upon receipt
by
Ameri-King
Coq~.
of
form(s)
337
or
8130-().
THE IMPLIED
WARRANTY
AND
ALL OTHER IMPLIED
WARRANTIES ARE HEREBY EXCLUDED.
AMEAI-
KING CORP.
MAKES
NO OTHER
WARRANTY
OR
REPRESENTATION
OF
ANY
KI
ND
WHA
TSOEVER EXPRESSED
OR
IMPLIED,
AND
ALL
IMPLIED WARRANTIES INCLUDING
ANY
WARRANTY
OF
MERCHANTABILITY
OR
FITNESS FOR A PARTICULAR PURPOSE
ARE HEREBY DISCLAIMED.
AMER! -KING CORP.'S
MAXIMUM
LIABILITY HEREUNDER IS
LIMITED TO THE PURCHASED PRICE OF THE PRODUCT. IN NO
EVENT SHALL AMER!- KING CORP.
BE
LIABLE FOR
ANY
CONSEOUENTIAL, INDIRECT, INCIDENTAL
OR
SPECIAL
DAMAGES
OF
ANY
NATURE ARISING FROM THE SALE
OR
USE
OF
THE PRODUCT, WHETHER BASED IN CONTRACT, TORT,
STRICT LIABILITY
OR
OTHERWISE.
26
24-62·91
The document reference is online, please check the correspondence between the online documentation and the printed version.
INSTALLATION AND OPERATION
MANUAL,
MODEL
AK-960
OPS
1
NAV
SWITCHINO & ANNUNCIATOR PANEL
4.2
REPAIR SERVICE
Ali
equipments
manufactured
by
Ameri-King
Corp.
must
be
repaired
at
the
facility
of
Ameri-King
Corp.
Ali
the
repair services shall be
performed
and
completed
within
3 days
upon
repairing
estimate
is approved
by
equipment
user
or
installation dealer.
4.3
FACTORY COMPREHENSIVE TEST SERVICE
Factory Comprehensive
Test
Service is available. There is a
service charge
for
this
service.
Ali
equipments
returned
for
Factory
Comprehensive
Test
Service
must
be
sent
freight
prepaid.
27
24-62·91
The document reference is online, please check the correspondence between the online documentation and the printed version.
INSTALLATION AND OPERATION
MANUAL,
MODEL
AK-960
.
OPS
1
NAV
SWITCHINO
1.
ANNUNCIATOR
PANEl
APPENDIX A
ENVIRONMENTAL QUALIFICATION FORM
RTCA 1
D0160C
NOMENCLATURE: AK-950 GPS 1 NAV SWITCIUNG AND
RELAMPADLI! ANNUNCtATOR PANEL
MODEL NO: AK-950 TSO NO:
Cl29
CLASS Al
MANUFACTURER:
AMERI-
KING CORP.
Conditions
Temp. & Altitude
Low temperature
High Temperature
ln-Fiight Loss
of
Cooling
Altitude
Decompression
Overpressure
Tcmp. Variation
Humidity
Shock
Operational
Crash Safety
Vibration
Explosion
Waterproofness
18842 BROOKIIURST ST.
FOUNTAIN VALLEY, CA 92708
Section Description
of
Conducted Tests
4.0
Equipment tested to Categories
A2&D1
4.5.1
4.5.2
&
4.5.3
4.5.4
Cooling air not requited
4.6.1
4.6.2
4.6.3
5.0
Equipment tested to Categoty C
6.0 Equipment tested
to
Category A
7.0
Equipment tested pel'
D0-160C
7.2
Par. 1.2.1
7.3
8.0
Equipment tested wîthout shock-
mountS
to
Categories M & N
(Table 8-1)
9.0
Equipment identified as
Category X; no test required
10.0 Equipment identified as
Category X, no test requîred
.
28
INSTALLATION AND OPERATION
MANUAL,
MODEL
AK-960
OPS
1
NAV
SWITCHINO 1. ANNUNCIATOR PANEL
ENVIRONMENTAL QUALIFICATION (Cont'd)
' '
Conditions Section Description
of
Conducted Tests
''
Fluids Susceptibility 11.0 Equipment identified as
Category X, no test required
Sand and Oust 12.0 Equipment identified as
C::ategory
X, no test required
Fungus 13.0 Equipment identified as
Category X, no test required
/
Salt Spray 14.0 Equipment identified as
C~tegqry
X, no test required
Magnetic Effect 15.0 •i
/•
'1.
Equipment tested to Class A
!
.,,
Power Input 16.0 1
~quipment
tested to Category B
Voltage Spike 17.0 Equipment tested to Category B
,_
...
Audio Frequency 18.0 Equlpment tested. to Category B
Susceptibility . '
1.
lnduced Signal 19.0 .Equipment tested to Category A
Susceptibility
Radio Frequency 20.0 Squipment tested to Category T
Susceptibility
Radio Frequency
21.0
Equipment tested to Category A
Emissions 1
•i
Lightning Induced
22.0
Equipment identified as
Transient
éategory
X, no test required
:
Susceptibility (
Lightniug Direct 23.0 Equipment ideotified as
Effects Category X,
no
test required
Icing
24.0
Equipment identified
as
Category X, no
t~t
required
29
24-62·91
The document reference is online, please check the correspondence between the online documentation and the printed version.
INSTALLATION
AND
OPERATION
MANUAL,
MODEL
AK-950
GPS
1
NAV
SWITCHING &
ANNUNCIATOR
PANEL
APPENDIX B
FAA
TSO 1
PMA
1STC approved Letters
for
Model
AK-950-
( )
30
24-62·91
The document reference is online, please check the correspondence between the online documentation and the printed version.
US
Department
of
Transportation
Federal
Aviation
Administration
NOV
22
1996
TRANSPORT
AIRPLANE
DIRECTORA
TE
AIRCRAFT
CERTIFICATION
SERVICE
LOS
ANGELES
AIRCRAFT
CERTIFICATION
OFFICE
3960
PARAMOUNT
BOULEVARD
LAKEWOOD,
CALIFORNIA
90712-4137
Arneri-King Corporation
Mr. Keith Van
18842
Brookhurst
Street
Fountain Valley, California 92708
DearMr.Van:
Ameri-King Corporation,
GPS/NA
V Switching and Annunciator Panel,
Technical Standard
Order
C 129a
Y
our
application dated November
7,
1996, requesting the issuance
of
a Technical Standard
Order
(TSO)
authorization
in
accordance with the procedural requirements
of
Federal Aviation
Regulation (FAR) Part 21, Subpart O. Based upon
your
data and statement
ofconformance
certifying your article(s) has met the requirements
of
FAR Part 21, Subpart
0,
and the minimum
performance standards
ofTSO
C 129a
(Ref
FAR 21.605), authorization
is
hereby granted for the
following
DESCRIPTION
AK-950-( ) Series
GPS/NAV
Switching and Annunciator Panel
For
your
information,
the
conditions and tests required for
TSO
approval are minimum
performance standards.
The
article(s) may be installed on
or
within a specifie type
or
class
of
aircraft only
iffurther
evaluation by the user/installer documents
an
acceptable installation that is
approved by
the
Administrator
The
quality control procedures contained
in
your quality control manual, currently on file at the
Phoenix Manufacturing Inspection Satellite Oftice, and your statement that those
procedures
will
be
applied
to
the manufacturer
of
the subject article(s) at the above address, are considered
adequate
in
accordance with FAR 21 143.
Effective this date, your authorization to use
TSO
procedures
is
extended to include the subject
article(s) You may identity the article(s) with the applicable
TSO
markings as required by
TSO
Cl29a.
As recipient
of
this
TSO
authorization,
exceptas
provided
in
FAR
2U(d),
you are required
ta
report any failure, malfunction,
or
defect
in
any product or part manufactured by you
or
your
contracted suppliers, and which you have determined has resulted
or
cou
Id
result
in
any
of
the
occurrences listed
in
FAR
21
3(c)
The
report should be communicated initially by telephone
to
the Superviser, Technical and Administrative Support Staff, ANM-1 03L,
(31
0) 627-5300, within
24 hours after
it
has been determined the failure has occurred, and followed up with a written
notice. FAA Form 8010-4 (Malfunction
or
Defect Report)
or
other
appropriate
format is
acceptable
in
transmitting the required details.
As
required by FAR 21.613(b), you must also
notity the FAA when you no longer manufacture a
TSO
approved article
This authorization pertains only
ta
manufacturing operations at the above address This office
must be notified
in
advance
of
any proposed facility relocation to preclude interruption while
awaiting quality control approval
ofthat
fàcility
Sincerely,
,
..
Michael Murphy, Manager,
Technical and Administrative
Support
Staff
ANM-IOJL
24-62·91
The document reference is online, please check the correspondence between the online documentation and the printed version.
The document reference is online, please check the correspondence between the online documentation and the printed version.
Other manuals for AK-950L
1
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