Ameri-King AK-950L User manual
Docwnent No.: IM-950
INSTALLATION & OPERATION MANUAL
For
PIN
AK-950-L-GPS 400/500 GNC 420/520
(GARMIN INTERNATIONAL INC. GPS)
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
The document reference is online, please check the correspondence between the online documentation and the printed version.
INSTALLATION AND OPERATION
MANUAL,
MODEL
AK-950
OPS
1
NAV
SWITCHINO & ANNUNCIATOR PANEL
TABLE
OF
CONTENTS
Table
of
Contents
SECTION 1
GENERAL INFORMATION
1.1 Scope
................................................................
3
1.2
1.3
1.4
1
.4.
1
1.4.2
1.4.3
Description
......................................................... 3
Technical
Characteristics
...... .
..
...........
..
........
..
..
..
..
10
Front
Panel
Contrais
and
Annunciations
.................. 12
Contrais
....................................................... 12
Annunciations
............................................... 13
Interface
....................................................... 16
1.5
Equipment
Limitations
.........................................
.
20
1.6
1.7
Major
Components
..............................................
.
Accessories
supplied
..................
.
SECTION
Il
INSTALLATION
AND
TEST
2. 1
Unpacking
and
lnspecting
Equipment
....................
..
2. 2
Mechanical
Installation
.........................................
.
2.2
.1
2.2.2
2.2.3
2.2.4
2.2.5
Equipment
Location
.......................................
.
Cooling
........................................................
.
Additional
Annunciations
................................
.
Addition
al
Relays
...........................................
.
Routing
of
Ca
bles
..........................................
.
2.3 Electrical
Installation
............................................
.
21
21
22
22
22
22
24
24
24
24
2.4
Post
Installation
Test
..
.. ..
..
.. .
..
.
.. ..
.
.. .. ..
..
.. .. .. .. .. .. .. ..
.
40
2.4.1
Pre
Installation
Tests
.......................................
40
2.4.2
Operating
Instructions
.....................................
40
1
3.1
3.2
4.1
4.2
4.3
1.1
2.1
3.1
3.2
3.3
INSTALLATION
AND
OPERATION
MANUAL,
MODEL
AK-950
OPS
1
NAV
SWITCHING &
ANNUNCIATOR
PANEL
TABLE OF CONTENTS (CONT'D)
SECTION Ill
OPERATION
General
.............................................................
.
Ore
ration
SECTION
IV
WARRANTY
AND
SERVICE
44
44
Limited
Warranty
.................................................
48
Repair
Service
....................................................
.
Factory
Comprehensive
Test
Service
LIST OF FIGURES
50
50
Outline
Drawing
for
ali Series ...... ...... .. .... .. ............ 4
Cutout
Dimensions
for
Panel
Mounting
....... .. .. .... .. ..
23
Schematic
Pinout
for
Connector
..
.......
.....
....
....
.. ....
25
Electrical Sc
hematie
Dia
gram
....... ..... ........... .. .......
27
Wiring
Diagram
....................................................
28
APPENDIX A
Environmental
Qualification
form
RTCA
1DO
160C
.... 51
2
The document reference is online, please check the correspondence between the online documentation and the printed version.
.1
.2
SCOPE
OPS
1 NAV SWITCHINO lo ANNUNCIATOR PANEL
SECTION 1
GENERAL INFORMATION
This manual
contains
information
necessary
for
the
installation,
test
and operation
of
the model
AK-950,
GPS
1
NA
V
Switching
and
Annunciator
Panel, manufactured
by Ameri -King Corporation, California,
U.S.A.
DESCRIPTION
The
AK-950
is a self-contained GPS 1
NAV
Switching
and .
Annunciator
Panel.
lt
combines ali the necessary
functions
required
for
switching
HSI 1 CDI data
inputs
between a
conventional
NA
V (VOR) receiver and the approach-certified
GPS
receiver.
ln
addition, the
AK-950
contains severa!
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 lite,
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
systems
are applicable:
* GPS 400/500 and
GNC
4:20/520
(GARMIN INTERNATIONAL INC.)
3
lNSIALlAIIUN
AND OPERA
liON
MANUAL.
MODEl
AK-960
OPS 1 NAV SWITCHINO lo ANNUNCIATOR PANEL
Q[
__
2.830
~
1050
~~
C•
INH:c
AUT~~TERMI
MS~J
0
NAV
iOBSI
APR
WPl
GPS,
TEST
~
~
0
(~el
0 0
FIGURE
1-1
a OVERALL DIMENSIONS
OUTLINE DRAWING
FOR
ALL SERIES
4
The document reference is online, please check the correspondence between the online documentation and the printed version.
2.2.3
2.2.4
2.2.5
INSTALLATION
AND
OPERATION
MANUAL,
MODEL
AK-950
GPS 1
NAV
SWITCHING
&
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 1 CDI. Spare relay
contacts
on the
AK-950
connector
may
be used
for
this
purpose.
ADDITIONAL
RELAYS
The
AK-950
contains
3 relay pales. Some installations
may
require
more
than
24
pales
due
to
data lines, superflags, etc.
If
this
should
occur,
you
may
use one spare relay pole
ta
switch
additional relays. ln cases
where
it
may
be more desirable
to
have ali
the
relay
switching
done
at
a rem
ote
location, (i.e.:
remote
mounted
equipment),
one relay pole on the
AK-950
may
be used
for
switching
this
bank
of
relays. Please
note
that
the
maximum
relay
contact
rating
for
the
AK-950
is 2 amps
OC.
ROUTING
OF
CABLES
Care
must
be
taken
not
ta
bundle
the
AK-950
logic
and
law
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.
A
void
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
ta
figure
3-3
Use
at
least
24
AWG
wire
for
ali
connections.
You
MUST
use shielded
wire
where
shawn.
A
void
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.
INSTALLATION
AND OPERATION
MANUAL,
MODEL
AK-960
OPS
1
NAV
SWITCHINO.
ANNUNCIATOR PANEL
CONNECTOR
REAR
YIEW
OF
CONNECTOR
5 6 7 8 9
10
11
12
13
14
15
16
17 18
• • • • • • • • • • • • • • • • • • • •
21
22 23 24 25 26 27 28 29 30
31
32 33
34 35
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-Oensily
0-Subminialure
Conneclor
r-
1
2
3
4
f------
5
f------
6
7
8
9
10
11
12
1--------
13
14
15
16
17
18
19
20
21
22
23
f------
24
f-------
25
f-----
26
27
28
29
30
31
~-------·--
32
33
34
35
36
37
M
FIGURE
3-1
a
SCHEMA
TIC
PINOUT
FOR CONNECTOR
The document reference is online, please check the correspondence between the online documentation and the printed version.
36
39
INSTALLATION
AND
OPERATION
MANUAL,
MODEL
AK-860
OPS 1
NAV
8WITCHINO
&.
ANNUNCIATOR
PANEL
40
--
OC
GROUNO
41
42
43
44
45
46
47
48
49
50
51
52
53
54
55
56
57
58
59
60 -
RELAY
#21 - C
61
62
-INTEG
Annunciator
Ait
Gnd
Input
63
64
65 -
RELAY
#21 -
NC
66
--
NAV
Annunciator
Ait
Gnd
Input
67
66
69
--
RELAY
#2t
-
NO
70
--
GPS
Annunciator
Ait
Gnd
Input
71
--
APR
Annunciator
Ait
Gnd
Input
72
----c-
AUTO
Annunciator
Ait
Gnd
Input
73 OBS.
SWITCH
(Moméhtary
Ground
Output)
].!
75
76
77
76
OBS
Annunciator
Ait
Gnd
Input
MSG
0
1\nnunciator
Ait
Gnd
Input
WPT
Annunciator
Ait
Gnd
Input
--
TERM
Annunciator
Ait
Gnd
Input
+
14/26
VOC
POWER
INPUT
FIGURE
3-1
b SCHEMATIC PINOUT
FOR
CONNECTOR
17
INSTALLATION
AND
OPERATION
MANUAL,
MODEL
AK-860
OPS 1
NAV
SWITCHINO
a.
ANNUNCIATOR
PANEL
AK-950L-( )
Jv
78
-+
14/28
VDC
POWER
INPUT
40
r---
OC
GROUHD
62
75
76
72
74
71
77
73
INTEG
ANNUNCIATOR
(Aiternate
Ground
Input)
MSG
ANNUNCIATOR
(A!ternate
Ground
Input)
WPT
ANNUNCIATOR
(Aiternate
Ground
Input)
AUTO
ANNUNCIA
TOR
(Aiternate
Ground
Input)
OBS ANNUNCIA
TOR
(Aiternate
Ground
Input)
APR
ANNUNCIATOR
(Ait;rnate
Ground
Input)
TERM
ANNUNCIATOR
iAiternate
Ground
Input)
OBS
SWITCH
(Momentary
Ground
Output)
66
NAV
ANNUNCIA
TOR
'
(Aiternate
Ground
Input)
70
GPS
ANNUNCIATOR
(Aiternate
Ground
Input)
HAV
60
_l;!l
~~-----------------------i
65 '
't"'---------...:-t
69
GPS
--
----·
~
FIGURE
3-2
ELECTRICAL
SCHEMATIC
OIAGRAM
18
The document reference is online, please check the correspondence between the online documentation and the printed version.
a:=
Q{f)
t-I
<{:::::-
uO
0~
z
>-
<{ u
z c
<{ U)
CJ)
co
INS
1
/\llA
liON
ANO
OPEH/\
liON
MANUAL,
MOOEL
AK-950
GPS 1
NAV
SWITCHINO & ANNUNCIATOR PANEl
CONNE
CT
OR
AK-950L-( )
--
;...L
-
0 c
('.j
0>
/NAY
ANNUNC.
8
1--------t
66
t---
NAV
ANNUNC. (GROUND INPUT)
70
--
GPS
ANNUNC. (GROUND INPUT)
::{
(/)
Il
NA
V ANNUNC 7
J--------1
00-o
0
a.>
N
1
~<{
RElAY !ENGAGE
=i-
a-:-
Nu
~
Ir)
c tNTEGAnnunc
ô=
N
Cil
IWPT
Annunr
3
'<!"
§ rrERM
Ann.
4
u
-~
&~
jAPR
Annunc.
5
r--
MSG
Ann.
6
'"0
.E
OBS
Annunc
7
§
~UTO
Ann.
-
c 8
.Ë
0 OBS
Mom
S"
71f------
0
~
Ir)
Q ,---
0
.,....
0 P4001
......
'<!"
tzl
+1
~/7R
voc 0 2
0-
--
f3
A 1
'7
NOTES:
65
--
RELAY #21 •
NC
69
-RELAY #21
·NO
1---
1---
1---
1---
1---
-
1---
62
1-'NTEG
Green
Annunc.
76
1--
WPT
Amber
Annunc.
77 ~. TERM Green
Annunc.
71
t--
APR Green
Annunc.
.--
75
'1-
MSG
Amoer
""nunc.
74
1-
OBS Green
Annunc.
72
t-'-
AUTO
White
Annunc.
73
t--
OBS
Mom
Switch
40
-
OC
GROliNO
60 -
RELAY
# 21--c
78
--
+1~/28
VOC
POW[R
vy-
UIPlJT
1.
Refer
lo
GPS
Monuloclurer's
lnslallolion
Monual
for
Actuel
lnslollollon.
2.
Ali
Wires
ore
24
AWG
minimum.
Reloy
NC
shown
ln
NAV
selecled.
Relay
NO
shawn
in GPS
selecled.
FIGURE
3.3
WIRING DIAGRAM
for
AK-950L-
()
with
KI-208A/209A
(AIIied Signais lnc.)
19
The document reference is online, please check the correspondence between the online documentation and the printed version.
GPS 1
NA
V SWITCHING &
ANNUNCIA
TOR
PANEL
1.3
TECHNICAL CHARACTERISTICS
SPECIFICATIONS:
TSO COMPLIANCE:
PHYSICAL
CJ
IARACTERISTICS:
• PANEL CUTOUT SIZE
AND
WEIGHT:
GENERAL SPECIFICATIONS:
• POWER INPUT:
•
LAMP
BULB TYPE:
•
RELA
Y TYPE:
-No.
of
available Potes:
-
Switching
Current 1
Voltage:
-Carrying Current 1
Voltage:
-Contact Resistance:
-Contact Material:
-
Switching
Time:
-lnsulation Resistance:
-Life Expectancy:
-Coil Resistance
CHARACTERISTICS:
TSO-
C129a
Panel
Mounted,
1.00"
x
2.12"
0.31bs
(10.0-
32.21 Vdc
(5.9-
7.41
Watts
Nominal
0.214
Amp.@
28
Vdc, Nominal.
0.530
Amp.@
14
Vdc, Nominal.
0.654
Amp.
@
28
Vdc,
Momentary
Test
Mode
only.
1.575
Amp.
@
14
Vdc,
Momentary
Test
Mode
only.
Duallamp
for
each
Annunciator.
PIN
6838
for
28
Vdc.
PIN
8111
for
14
Vdc.
Tl
Incandescent;
16,000
hours
average fife.
24
Pales, Double
throws
2
Amp
1
220
Vdc
maximum
2
Amp
1
220
Vdc
maximum
50
milli -
ohm
max
Gold overlay
(1
-
21
milli -seconds
1,000
mega -ohm @
500
Vdc
1
00
million mechanical operations
.2 million electrical operations @30Vdc
2880
Ohm
@
24
Vdc;
1028
Ohm
@
12
Vdc.
10
The document reference is online, please check the correspondence between the online documentation and the printed version.
••
-
-,
-·••,,
,..__
~
.,,
,.~··•
•
._,
'""
...........
•
·••
-../UV
GPS
1 NAV SWITCHINO & ANNUNCIATOR PANEL
• AUTO DIMMING: Built in
ENVIRONMENTAL TEST SPECIFICATI.ONS:
* RTCA
D0-208
A
1/01
• RTCA
D0-160C
ENV. CA
T.:
C1
AC/XXXSXXXSXXXXBXB
• TEMP.
AND
ALTITUDE:
Low
Temperature:
High Temperature:
* TEMP. VARIATION:
* HUMIDITY:
• SHOCK:
* VIBRATION:
* MAGNETIC EFFECT:
• POWER INPUT:
Category
A2
& 01
-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
+
/-
2 msec, operational
15
G,
11
+/-2 msec, crash
safety
Categories M and N
Category A
Less than
0.3
rn
Category B
Normal Operating: (
10.0-
15.11 Vdc
(20.0-
30.31 Vdc
Abnormal
Operating:(11.0
-16.11 Vdc
{22.0-
32.21 Vdc
* VOLTAGE SPIKE: Category B
*\AUDIO
FREO. CONDUCTED.
SUSCEPTIBILITY: Category B
• INDUCED SIGNAL
SUSCEPTIBILITY: Category A
•
RF
SUSCEPTIBIUTY: Category T
• EMISSION
OF
RF
ENERGY: Category A
11
1.4
1.4.1
li<<>
,,.lv~
olUI~
ANU
UttllA
loON
"IAIWAL.
MOOEL
AK·9b0
OPS 1 NAV SWITCHINO & ANNUNCIATOR PANEL
FRONT PANEL CONTROLS
AND
ANNUNCIA
TIONS
CONTAOLS
1.4.1.1
CONTROLS
FOR
MODEL
AK-950
NAV
1GPS:
TEST:
Alternate action
switch,
when
pressed,
will
select NAV
{VO~I
or
GPS
presentation on HSI 1CDI.
Push
Button
switch
for
TEST
function
for
ali
Annunciation
lamps.
12
The document reference is online, please check the correspondence between the online documentation and the printed version.
-····~
....
._
,.,,
...
'""n'"'II-\IUM
t'ANt:L
1.4.2
ANNUNCIATIONS
1.4.2.1 ANNUNCIATIONS
FOR
MODEL
AK-950
NAV
(Green):
GPS (Blue):
NA
V (VOR)
information
presented
on
the
HSI
or
CDI.
GPS
information
HSI
or
CDI.
13
presented
on
the
1.4.3
1.4.3.1
GPS
1
NAV
SWITCHING
&
ANNUNCIATOR
PANEL
INTERFACE
INTERFACE FOR
MODEL
AK-950
INTEG Receives an
ground
logic
input
(Pin
62)
The
INTEG
Annunciator
shall
be
illuminated.
16
The document reference is online, please check the correspondence between the online documentation and the printed version.
INSTALLA
Tl
ON AND OPERATION 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 madel GNS 400 1500 1GNC 420 1520
Garmin Internationallnc.
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
iffurther
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
NA
V (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:
PART NO. DESCRIPTION
9500001
Pl,
Mating Connector Kit.
High Density D Subminiature Conn.
Plug, 78 Female Crimped Pins, with
Backshell and Thumbscrews.
PIN
162X 11989X & FK22SL05
(Canee Corporation)
20
INSTALLATION AND
OPERATION
MANUAL,
MODEL
AK-950
GPS/NAV
SWITCHING
& ANNUNCIATOR PANEL
9500002 Optional Pre-fabricated Cable
Assembly with MIL-SPEC shielded
Cable, including:
MIL-W-22759118-24-9
M27500-1-24-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.
1.
Hand Crimping
Too1:
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
21
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
2.2.2
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
daim.
Retain
the
container
and
packaging
material
for
possible
future
use.
MECHANICAL
INSTALLATION
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
connector
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.
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
other
equipment.
Means
of
providing
a
gentle
air
flow
will be a plus.
22
INSTAllATION
AND
OPERATION MANUAl, MODEl AK-960
OPS 1
NAV
SWITCHINO
lo
ANNUNCIATOR
PANEL
+ 0
1.000
0.750
2.470
R.130
(4 PLS)
0.125
thru
hale
for
4-40
screw
(4 PLS)
FIGURE
2.1
CUTOUT
DIMENSIONS
FOR
PANEL
MOUNTING
23
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
2.4
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-950
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
to
GPS
Manufacturer's
Installation Manual
for
complete
GPS
System
Operating
Instructions.
The
following
paragraphs
described Lamp BAT 1
DIM
1
Test
and GPS 1
NAV
Switching
functions
o"'ly.
2.4.2.1
OPERATING INSTRUCTIONS FOR MODEL
AK-950
Turn
off
the
avionics
master
switch
and
connect
the
mating
connector
to
the
AK-950.
Turn on the avionics
master
switch
and
the
AK-950
should
come
on
with
the
following
annunciations:
1.
NAVorGPS
Momentarily
press
the
TEST
Switch,
ali
annunciations
should
light.
Select
NAV
using
the
NAV
1GPS
button.
The
presentation
on
the HSI 1CDI
will
now
be
information
from
the
VOR receiver.
Using a VOR
test
generator
or
equivalent
VOR signal,
verity
that
the
presentation
and
operation
of
the
HSI 1CDI is
correct.
This
will
include
course
resolver,
left-right
meter,
ta-from
meter
and nav
warn
flag.
40
INSTALLATION AND OPERATION MANUAL, MODEL
AK-950
GPS
1
NAV
SWITCHING & ANNUNCIATOR PANEL
l
he
ILS
Override
feature
(if Pin
63
is
connected)
may
be
tested
by
tuning
the
connected
NAV
Radio
to
an ILS
frequency.
Verity
that
the
Blue GPS
Annunciator
extinguishes
and
bath
the Green ILS and
NA
V
Annunciators
illuminate,
regardless
of
tite
selection
of
the
NA
V/GPS
switch.
Using
the
appropriate
tc:st
signal
generators,
verify
that
the
ILS and 1
or
Glide Slope
data is
correctly
displayed
on
the
HSI and 1
or
CDI.
Tune
the
connected
NA
V Radio
back
to
a
standard
VOR
frequency.
Verity
that
the
Blue GPS
Annunciator
again
illuminates
and
that
the
GPS
datais
then
correctly
displayed
on
the HSI and 1
or
CDI.
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
to
dim
the
annunciators. Rotate
the
Potentiometer
counter-clockwise
to
make
the
annunciators
brighter.
3. Do
not
use excessive
inward
force
on the
alignment
tool,
and
do
not
use excessive
rotational
force.
Damage
may
result. 41
The document reference is online, please check the correspondence between the online documentation and the printed version.
INSTALLATION
AND
OPERATION
MANUAL,
MOOEL
AK-960
OPS 1
NAV
SWITCHINO &
ANNUNCIATOR
PANEL
3.1 GENERAL
SECTION
Ill
OPERATION
This
section
describes the operation
of
the
GPS
1
NA
V
Switching
and Relampable
Annunciator
Panel,
Model
AK-950.
3.2
OPERATION
3.2.1
OPERATION FOR
MODEL
AK-950
NAV
1
GPS
ALTERNA
TE
SWITCH
OPTIONAL
ILS OVERRIDE
FUNCTION
Pushing the
NA
V 1
GPS
switch
selects the
navigation
source (VOR 1ILS 1LOC
or
GPSI
to
be displayed on the HSI
or
COl.
Although
it
may
be displayed on the
GPS
unit'
s
built-in
CDI, course
information
is aIso
displayed
on the panel-mounted HSI or CDI
when
executing
an approach utilizing
GPS
navigational
data.
This
Optional
Glide Slope 1ILS Override
Feature
will
force
the
AK-950
automatically
switch
to
the
NA
V
mode,
regardless
of
the
position
of
the
NA
V/GPS
switch,
provided
that
the
connected
NA
V
Receiver is
tuned
to
an ILS
frequency.
ln
this
mode,
the
Blue GPS
Annunciator
will
extinguish
and
the
Green
NA
V
Annunciator
will
illuminate
accordingly.
The
information
presented
on
the
HSI or
COl
will
then
be
from
the
NAV
(VORI
only.
INSTALLATION
AND
OPERATION
MANUAL,
MODEL
AK-960
OPS/
NAY
SWITCHINO &
ANNUNCIATOR
PANEL
45
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
GPS
1
NAV
SWITCHING & ANNUNCIATOR PANEL
UMITED 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
under
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
48
INSTALLATION AND OPERA
liON
MANUAL,
MUUI:L
AIHit>U
GPS
1
NAV
SWITCHING & ANNUNCIATOR PANEL
factory;
changes in
calibration
occuring
as a
result
of
normal
use
of
the
equipment;
the
cost
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 billed
at
cast.
An
estimate
will
be
submitted
for
approval before repair 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
C.O.D.
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
Corp.
of
form(s)
337
or
8130-().
THE IMPLIED
WARRANTY
AND
ALL OTHER IMPLIED
WARRANTIES ARE HEREBY EXCLUDED.
AMERI-
KING CORP.
MAKES
NO OTHER
WARRANTY
OR
REPRESENTATION OF
ANY
KINO WHATSOEVER EXPRESSED
OR
IMPLIED,
AND
ALL
IMPLIED
WARRANTIES
INCLUDING
ANY
WARRANTY
OF
MERCHANTABILITY
OR
FITNESS
FOR
A PARTICULAR PURPOSE
ARE HEREBY
DISCLAIMED.
AMERI -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.
49
The document reference is online, please check the correspondence between the online documentation and the printed version.
INSTALLATION AND OPERATION
MANUAl,
MODEl
AK-960
GPS 1 NAV SWITCHING & ANNUNCIATOR
PANEl
42
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
compléted
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.
50
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
APPENIUX
_
_A
ENVIRONMENTAL
QUALIFICATION
FORM
RTCA 1
D0160C
NOMENCLATURE:
AK-950
GPS
1
NAV
SWITCIIING
AND
RELAMI'ABLE
ANNUNCIATOR
PANEL
MOIJLL
NO:
/\K-'!50
TSONO:
Cl29
CL/\SS
Al
MANUFACTURER:
AMERI-
KING
CORI'.
Conditions
Temp. & Altitude
Low temperature
lligh
Temperature
ln-f<Iight Loss
of
Cooling
Altitude
Decompression
Overpressure
------~---·
--
Temp. Variation
--------
--
-----------
llumidity
---
--~-
---
-
--------
--
--
Shock
Operational
Crash Safety
!------------~---~-~----
--
Vibration
-------------
-~-~
Explosion
Waterproofness
18842
BROOKIIURST
ST.
FOUNTAIN
V
AILEY,
CA
92708
Section Description
of
Conducted Tests
4.0
Equipment tested to Categories
A2&
Dl
4.5.1
4.5.2
&
4.5.3
4.5.4
Cooling air not required
4.6.1
4.6.2
4.6.3
5.0
Equipment tested to Category C
-
--------~-----
6.0
Equipment tested to Category A
--~-~--
--
7.0
Equipment tested
per
D0-160C
7.2
Par.
7.2.1
7.3
----
-~~-~
----
.
8.0
Equipment tested without shock-
mounts to Categories M & N
(Table 8-1)
9.0
Equipment identified as
Category X, no test required
10.0
tquipment
identified as
Category X, no test required
51
INS
1
ALLA
IIUN
ANU
Ut'~H.A
IIUN
MANU
AL,
MUUt:L
Ar\·UOU
OPS
1
NAV
SWITCHING & ANNUNCIATOR PANEL
ENVIRONMENTAL
QUALIFICATION (Cont'd)
Conditions Section Description
of
Conducted
Tests
f<Iuids
Susceptibility
11.0
Equipment
identified as
Category X, no test required
Sand and Dust 12.0 Equipment identified as
Category X, no test required
-
f<ungus
13.0
Equipment identified as
Category X, no test required
Salt Spray
14.0
Equipment ideutified as
Category X, no test
required
--
Magnetic Effect
15.0
Equipment tested to Class A
l'ower
Input
16.0
Equipment tested to
Category
B
---
Voltage Spike 17.0 Equipment tested to Category B
. -
-~--
·---~-~--
Audio f<requency
18.0
Equipment tested to
Category
B
Susceptibility
lnduced Signal
19.0
Equipment tested to
Category
A
Susceptibility
Radio Frequency
20.0
Equipment tested to
Category
T
Susceptibility
Radio Frequency
21.0
Equipment tested to
Category
A
Emissions
Lightning Induced
22.0
Equipment identified as
Transient Category X, no test required
Susceptibility
Lightning Direct
23.0
Equipment identified as
Effects Category X, no test required
king
24.0
Equipment
identified as
Category X, no tèst required
52
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
The document reference is online, please check the correspondence between the online documentation and the printed version.
U.S.
Depart
ment
olltonspoclalion
Federal
Aviation
Administration
NOV
22
1996
TRANSPORT
AIRPLANE Dl
RECTO
RA
TE
AIRCRAFTCERTIFICATION
SERVICE
LOS
ANGELES
AIRCRAFT
CERTIFICATION
OFFICE
3960 PARAMOUNT BOULEVARD
LAKEWOOD,
CALIFORNIA
90712-4137
Ameri-King Corporation
Mr. Keith Van
18842 Brookhurst Street
Fountain Valley, California 92708
Dear Mr.Van: Ameri-King Corporation,
GPS/NA
V Switching and Annunciator Panel,
Technical Standard Order C
l29a
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, Subpar1 O. Based upon y
our
data and statement
of
conforrnance
certil)'ing 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 GPSINAV 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
aircrafi only
iffhrther
evaluation by the user/installer documents an acceptable installation that
is
approvcd by the Administrator
The quality control procedures contained
in
your quality control manual, currently
on
file
at
the
Phoenix Manufacturing Inspection Satellite Oflice. and your statement thal 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 identify the article(s) with the applicable TSO markings as required
by
TSO
Cl29a.
As recipient
of
this TSO authorization,
exceptas
provided
in
FAR
21.3(d), you are tequired
to
report any failure, nmlfunction,
or
defect
in
any product
or
part manufactured by you
or
your
contracted suppliers. and which you have delermined has resulted
or
could result
in
any
of
the
occurrences listed
in
FAR 21.3(c). The report should be connnunicated initially by telephone
to
the Supervisor, Technical and Administrative Support Staff. ANM-103L, (310) 627-5300, within
24 hours aller
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 fonnat
i~
acceptable
in
transmitring the required details.
As
requircd by FAR
2161J(b).
you must also
notify the FAA when you no longer manufacture a
TSO
approved an
ide.
This aurhorization pertains only to manufacturing operations at the above address. This office
must be nolified in
ad
vance
of
any proposed facility relocation to preclude interruption while
awaiting quality control approval
ofthat
fàcility.
Sincerely,
1 - Michael Murphy. Manager,
Technical and Administrative
Support
Stail
ANM-IOJL
1
The document reference is online, please check the correspondence between the online documentation and the printed version.
Other manuals for AK-950L
1
This manual suits for next models
1
Table of contents
Other Ameri-King GPS manuals
