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100% found this document useful (1 vote)
561 views19 pagesAk 950
Uploaded by
EleazarCopyright
© © All Rights Reserved
We take content rights seriously. If you suspect this is your content, claim it here.
Available Formats
Download as PDF or read online on Scribd
/ 19
Document No.: IM-950
INSTALLATION & OPERATION MANUAL
for
P/N AK-950 — GNS 430/500W/530/530W
(GARMIN INTERNATIONAL INC.)
GPS / NAV SWITCHING & ANNUNCIATOR PANEL
Per TSO-C129a, RTCA DO-208 and DO-160c Requirements
AMERI-KING CORPORATION
17881 Sampson Lane
‘Huntington Beach, CA 92648
‘Tel: (714) 842-8555
Fax: (714) 842-4235,
Email: sales@ameri-king.com
Website: woyw.ameri-king. com (OPS | WAV SWITCHING & ANNUNCIATOR PANEL
TABLE OF CONTENTS
Table of Contents
SECTION |
GENERAL INFORMATION
Scope 3
Description or 3
Technical Characteristics 6
Front Panel Controls and Annunciations
Controls
Annunciat
Interface
Equipment Limitations
Major Components
Accessories supplied
SECTION I
INSTALLATION AND TEST
Unpacking and Inspecting Equipment 13
13
13
13
15
15
15
Mechanical Installation .
Equipment Location
Cooling
Additional Annunciations
Additional Relays
Routing of Cables .......
Electrical Installation ......
Post Installation Test...
Pre Installation Tests...
Operating Instructions
34
3.2
at
4.2
43
1
24
34
3.2
3.3
(Ps / Nav SWITCH
AANNUNCIATOR PANEL
TABLE OF CONTENTS (CONT'D)
SECTION It
OPERATION
General
Operation
SECTION IV
WARRANTY AND SERVICE
Limited Warranty
Repair Service
Factory Comprehensive Test Service
LIST OF FIGURES
Outline Drawing for all Series
Cutout Dimensions for Panel Mounting ..
‘Schematic Pinout for Connector
Electrical Schematic Diagram .....
ing Diagram .
APPENDIX A.
Environmental Qualification form RTCA / DO160C ....
23
23
14
16
18
19
28 WW
12
INSTALLATION AND OPERATION MANUAL, MODEL AK-960
(GPS / HAV SWITCHING & ANNUNCIATOR PANEL
SECTION 1
GENERAL INFORMATION
SCOPE
This manual contains information necessary for the
installation, test and operation of the model AK-950L,
GPS / NAV Switching and Annunciator Panel, manufactured
by Ameri - King Corporation, California, U.S.A.
DESCRIPTION
BOL is a self-contained GPS / NAV Switching and
jor Panel. It combines all the necessary functions
required for switching HSI / CDI data inputs between a
conventional NAV (VOR) receiver and the approach-certified
GPS receiver.
In 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 all Series for all
‘Models’ Annunciation Displays and Switches.
The following GPS system are applicable:
Model AK-950 —- GNS 430/500W/530/530W
for GNS 430/500W/530/530W
Garmin International Inc.
INSTALLATION ANO OPERATION MANUAL, MODEL AK-#60
(QFE / NAV SWITCHING & ANNUNCIATOR PANEL
1.080 —+}
FIGURE 1-1a.
OVERALL DIMENSIONS.
OUTLINE DRAWING
P/N AK-950 — GNS 430/500W/530/530W
GPS/NAV Switching and Annunciator Panel INSTALLATION AMO OPERATION MAMUAL, MODEL AK-260
(OPE | WAY SYAITCHING & ARMUNCIATOR PANEL
INSTALLATION AND OFERATION MANUAL, MODEL AK-960
‘OPS / WAV SWITCHING A ANMUNCIATOR PANEL
1.3 TECHNICAL CHARACTERISTICS
‘SREGIFICATIONS: SHARACTERISTICS;
‘TSO COMPLIANCE: TSO - C1294
PHYSICAL CHARACTERISTICS:
* PANEL CUTOUT SIZE Panel Mounted,
‘AND WEIGHT: 1.00" x 2.12"
0.3 bs
GENERAL SPECIFICATIONS:
* POWER INPUT: (10.0 - 32.2) vde
(5.9 - 7.4) Watts Nominal
0.214 Amp. @ 28 Vdc, Nominal.
0.630 Amp. @ 14 Vdc, Nominal,
0.664 Amp. @ 28 Vdc, Momentary
Test Mode only.
1.575 Amp. @ 14 Vdc, Momentary
Test Mode only.
* LAMP BULB TYPE: ual lamp'for each Annunciator.
PIN 6838 for 28 Vdc.
PIN 8111 for 14 Ve.
TI Incandescent; 16,000 hours
average life,
* RELAY IYPE:
~ No. of available Poles: 3 Poles; Double throws
+ Switching Current /
2 Amp /'220 Vde maximum
2 Amp / 220 Vdc maximum
50 mili - ohm max
: Gold overtay
+ Switching Tim {1 - 2) milf seconds
= Insulation Resistance: "1,000 mega - ohm @ 600 Vde
+ Life Expectancy: 100 million mechanical operations
.2 million electrical operations @30Vde
+ Coil Resistance 2880 Ohm @ 24 Vdc;
1028 Ohm @ 12 Vdc.
6 INSTALLATION AND OPERATION MANUAL, MODEL AK.960
INSTALLATION AND OPERATION MANUAL, MODEL AX-960 (OPS / NAV SWITCHING & ANNUNCIATOR PANEL
(OF8 WAV SWITCHING & ANHUNGIATOR PANEL
1.4 FRONT PANEL CONTROLS AND ANNUNCIATIONS
* AUTO DIMMING: il
AUTO DIMMU a 1.4.1 CONTROLS
ee eee CONTROLS FOR MODELS AK-950 - GNS430 (GARMIN):
* RICA D0-208 Ato
7 ; CDI Switch: Momentary action Switch, when
1 GAT: C1ACIKXXSXXXSXXXXBXB pressed, will select NAV (VOR) or
+ TEMP, AND ALTITUDE: Category A2 & D1 GPS presentation on HSI / CDI
Low Temperature: -20 deg. C Operating;
-85 deg. C Storage. 08S Switch Momentary Switch, when pressed, will
High Temperature: +70 deg. C Operating; select AUTO / HOLD OBS Sequence
+85 deg. C Storage. Mode.
+ TEMP. VARIATION: Category ©
2 deg, & minimum per minute TEST: Push Button switch for TEST function
for all Annunciation lamps.
* HUMIDITY: Category A
95% RH, 50 hours operating
* sHOCK: 6G, 11 4/2 msec, operational
186,11 4/2 msec, crash safety
* VIBRATION: Categories M and N
+ MAGNETIC EFFECT: Category A
Less than 0.3 m
+ POWER INPUT: Category B
Normal Operating: (10.0- 18.1) Vde
(20.0- 30.3) Vde
Abnormal Operating:(11.0-16.1) Vide
(22.0- 32.2) Vde
* VOLTAGE SPIKE: Category B
* AUDIO FREQ. CONDUCTED
‘SUSCEPTIBILITY: Category B
* INDUCED SIGNAL
SUSCEPTIBILITY: Category A.
RE PUIBILITY: Category T
* EMISSION OF RF ENERGY: Catagory A 14.2
14.2.4
INSTALLATION AND OPERATION MANUAL, MODEL AK 950
(OPS / NAV SWITCHING & ANNUNCIATOR PANEL
ANNUNCIATIONS
ANNUNCIATIONS FOR AK-950
- GNS 430 / 530
(GARMIN):
YLOC (Whitel: NAV {VOR} information presented on the
GNS
GPS (Green): GPS information presented on the
GNS
TERM (Green): GPS is active engaged in the Terminal
mode.
APR (Greenl: GPS is actively engaged in the approach
mode.
QBS (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 Intergrity Alert, from
the GPS receiver.
INSTALLATION AND OPERATION MANUAL, MODEL AK-960
1.4.3 INTERFACE
1.4.3.1
DI Switeh:
(Pin 67)
08S Switch:
(Pin 71)
vioc:
(Pin 62)
Gps
(Pin 68)
(Pin 74)
=e
(Pin 77)
APR:
(Pin 73)
MSG/WPTIINTEG
(Pins 75/76/62)
All Internal
Relay Coils,
(vel
(Pin 69)
SWITCHING & ANNUNCIATOR PANEL
INTERFACE FOR P/N AK-950- GNS430/500W/530/530W.
Provides a momentary logic low, to the
GNS receiver, for Switching between
VLOC and GPS Source.
Provides a momentary logic low, to the
GNS receiver, for Switching between
Automatic and Hold Mode, for GPS
Waypoint Sequencing.
Receives an alternate logic low from the
GNS to annunciate VLOC.
Receives an alternate logic low from the
GNS to annunciate GPS.
Receives an alternate logic: low from the
GNS to annunciate AUTO.
Receives an alternate logic low from the
GNS to ahnunciate OBS.
Receives an alternate logic low from the
GNS to annunciate TERM.
Receives an alternate logic low from the
GNS to annunciate APR.
Receives an alternate lagi low from.
the GNS to annunciate MSGAVPTIINTES.
Receives
Alternate Low Logie
il Equipment,
te activate all Intamal Relays,
Relays #9 thru #20)
10 INSTALLATION AND OPERATION MANUAL, MODEL AK.950
PSINAV SWITCHING & ANNUNCIATOR PANEL
1.5 EQUIPMENT LIMITATIONS
The AK-950 series control units contain specific 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 GPS/NAV switching & Annunciator Panel is approved
for installation with the following model number only’
GPS model GNS 430 / SOOW / 530 / 530W
smin 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. It is the responsibility of those desiring
{o install this article either on or within a specific 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 / CDI will be inoperative in both NAV (VOR) and GPS
1.6 MAJOR COMPONENTS
The system is comprised of one major component, the AK-950,
GPS/NAV Switching and Annunciator Panel
1.7 ACCESSORIES SUPPLIED
1.7.1 INSTALLATION KIT
PARTNO. — DESCRIPTION
‘9500001 PI, Mating Connector Kit.
High Density D Subminiature Conn.
Plug, 78 Female Crimped Pins, with
Backshell and Thumbscrews,
PIN 162X 11989X & FK22SL05
(Conee Corporation)
W
INSTALLATION AND OPERATION MANUAL, MODEL AK-980
GPSINAV SWITCHING & ANNUNCIATOR PANEL,
9500002 Optional Pre-fabricated Cable
Assembly with MIL-SPEC shielded
Cable, including:
MIL-W-22759/18-24-9
M27500-1-24-1G.
M17500-1-24-TG:
TYPE OF MATING CONNECTOR
Hi Density D-Subminiature Connector, 78 Female Sockets Plug.
Information for Crimping Tool.
1, Hand Crimping Toot: M22520/2-01
Daniel P/N AFMA
2. Positioner: M22520/2-06
Daniel P/N Kal
3. Extract/Removal Tool: M81969/1-04
Daniel PAN 91067-1
Daniel Manufacturing Inc
6103 Anno Ave.
Orlando, FL 32809
‘Tel (407) 855-6161
Fax (407) 855-6884
4, Vendor Sources: 24
22
224
2.2.2
INSTALLATION AND OPERATION MANUAL, MODEL AK-950
SECTION II
INSTALLATION AND TEST
UNPACKING AND INSPECTING EQUIPMENT
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.
MECHANICAL INSTALLATION
‘The AK-950 is designed with the installer in mind, All
accessories which are required for completing system
installation are provided, including Pre-fabricated Wiring Cable
Assembly,
EQUIPMENT 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 / CDI
that will be displaying the FPS information. The unit depth,
with connector attached, must also be taken into
consideration.
Avoid mounting close to heater vents or other high heat
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.
13
INGTALLATION ANO OPERATION MANUAL, MODEL AK.960
(OPS / NAV SWITCHING & ANNUNCIATOR PANEL,
6.125
thru hole for
4-40 seraw
(4 pus)
2.1 CUTOUT DIMENSIONS FOR PANEL MOUNTING
14 223
224
2.2.5
23
MNSTALLATION AND OPERATION MANUAL, MODEL AX-960
ADDITIONAL ANNUNCIATIONS
Depending upon the installation and approving agency, you may
bbe required to provide additional NAV Source Select external
annunciators near the HS! / CDI. Spare relay contacts on the
AK-960 connector may be used for this purpose.
ADDITIONAL RELAYS
ROUTING OF CABLES
Care must be taken not to bundle the AK-960 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
shown on the installation print. Avoid sharp bends in cabling
and routing near aircraft control cables.
ELECTRICAL INSTALLATION
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 all connections. You
MUST use shielded wire where shown. Avoid sharp bends and
routing cable near high energy sources. Care must be taken to
tie the harness away from aircraft controls and cables. Normal
tallation techniques should be applied.
16
INSTALLATION AND OPERATION MANUAL, MODEL AK.060
FIGURE 3-10
"NAV SWITCHING & ARMUNCIATOR PANEL
CONNECTOR
REAR VIEW OF CONNECTOR
jalure Connector
fine
f2-6
n3-c
parc
Ws
ye-c
ree
ne-e
noee
mo-c
mec
mr-c
msec
merc
ns-c
nese
nrac
ne-c
no -c
po-c
er
Fr = NC
W3- Ne
pean
ys ene
4e = NC
v7 anc
vee nc
#O- NC
#10 ~ NC
AL ANC
nid = Ne
ns = NC
as
#15 ~ NC
#16 ~ NC
7 = NC
SCHEMATIC PINOUT FOR CONNECTOR
16 IWTALLATION AND OPERATION MANUAL, MODEL AK-960
{OFS / NAY AWITCHING & ANNUNCIATOR PANEL
RELAY #18 = NC
— eeuay #19 ~ NC
o¢ GROUND
#1 = NO
42- NO
23 ~ NO
4a NO
+5 - NO
46 - NO
v7 - NO
ry
$3 = No
y10 ~ No.
any = No.
W12 ~ No
3 - x0
v4 = 40.
Hs = 00
6 - x0
an? = xO
ae - x0
RELAY #19 = NO
INTEG Annunciator Alternate Ground Input
— ILS Auto Override
— RELAY 420 — NC.
VLOC Annunciator Alternate. Ground input
CDI Momentary Switch Output
RELAY #20 ~ NO {Open Circuit input
Al Relays Coils |-ve) {AI GND Input ~ NO Positions)
|— GPS Annunciator Ground Input
APR Annunciator Ground Input
| AUTO Annunciater Alternate Ground Input
— OBS Momentary Switch Output
= OBS Asnunciator Altern
Ground Input
te Ground Input
J— WPF Anncnciator Alternate Ground Input
| — TERGa Annunclator Alternate Ground Input
—— #14728: vDC POWER INPUT
FIGURE 3-1b SCHEMATIC PINOUT FOR CONNECTOR
W
INSTALLATION ANO OPERATION MANUAL, MODEL AK.960
(GPR / WAV SWITCHING & ANMUNCIATOR PANEL,
P/N AK-950- GNS430/500W/530/530W
— spre woe rome meat
All Relays Coils (ve)
(Alt GND Input = NO Positions)
(Open Circuit Input = NC Positions)
INTEG Amber Annunc.
(Alternate Ground Input)
VLOC White Annunc.
(Alternate’ Ground Input)
70GPS Green Annunc.
(Alternate, Ground Input)
76; WPT Amber Annunc.
(Alternate Ground Input)
77 TERM Green Annunc.
(Alternate Ground Input)
71 -APR Green Annunc.
(Alternate Ground Input)
75}MSG Amber Annunc.
(Alternate Ground Inpitt)
74 |-OBS Green Annunc
(Alternate Ground Input)
72}AUTO White Annunc.
(Alternate Ground Input)
67 -CDI Mom Switch
(Mometary Ground Output)
'73|-OBS Mom Switch
(Momentary Ground Output)
FIGURE 3-2 ELECTRICAL SCHEMATIC DIAGRAM
18 WISTALLATION AND OPERATION MANUAL, MODEL AK-960
(GPS | NAV SWITCHING & ANNUNCIATOR PANEL
P/N AK-950- GNS430/500W/530/530W
Al Relays Coils (ve)
{Alt GND Input = NO Positions)
(Open Circuit Input = NC Positions)
INTEG Amber Annunc.
VLOC White Annune.
GPS Green Annunc:
WPT Amber Annunc.
TERM Green Annunc.
APR Green Annunc:
MSG Amber Annune.
OBS Green Annunc:
AUTO White Annunc.
CDI Mom Switch
OBS Mom Switch
Garmin GNS 430/500W/530/530W
414/28 ve powee meut
Hotes: ee
1 Refer 16 GPS Manutacturer's ti
2. A Wires are 24-RWG minimum
lallaion Manvol for Actual Instetation
FIGURE 3.3 WIRING DIAGRAM for AK-950 - ()
with Garmin GNS 430/500W/530/530W. me po NAV STNG & ANNUNCIATOR PANEL
P/N AK-950- GNS430/500W/530/530W
All Relays Coile ve)
{AIC GND Input = NO Positions)
(Open Cireult Input = NC Positions)
VLoc Ann.
VLOC White Annune.
GPs Annunc}2 GPS Green Annunc.
Wer Annune|3 WPT Amber Annune,
TERM Ann. TERM Green Annunc.
JAPR Annunc|5 APR Green Annunc,
IMsG Ann. MSG Amber Annune.
loBs Annunc}7 AUTO White Annune.
JAUTO Ann. [a |__|} OBS Green Annune.
—_ CDI Mom Switch
—+ OBS Mom Switch
[CDI Mom Sw} 7:
OBS Mom Svl74
40} 0c enounn
14728 v6 0,0
Notts:
1 Reler 46 GPS Manufacturer's Installaion Monuol for Actua! Instollaton,
2. All Wiees ore 24-AWG. minimum,
Garmin GNS 430/500W/530/530W
I
i 4 114/28 voc roweR iPur
FIGURE 3.3 WIRING DIAGRAM for AK-950 - ()
with Garmin GNS 430/500W/530/530W
19 24
244
2.4.2
24.21
(GPS / WAV SWITCHING & ANRUNCIATOR PANEL
POST INSTALLATION TEST
After completing the mechanical installation, the following Post
Installation Function Tests must be performed.
PRE INSTALLATION TESTS
With the AK-950 disconnected, turn on the avionics master
switch and verify that the aircraft power of 14 / 28 Vdc are
‘on Connector Pin 78 (Annunciator Power). Using an Ohm
Meter, verify 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 BRT / DIM / Test and VLOC / GPS Switching
function only.
OPERATING INSTRUCTIONS FOR MODEL AK-950 -GNS530
(GARMIN):
‘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
neiatio
1. VLOC or GPS
2. AUTO or OBS
Momentarily press the TEST Switch, all annunciations
should fight.
Select VLOC using the CDI Button. The presentation on the
GNS- will now be information from the VOR receiver.
Select GPS using the CDI Button. The presentation on the
GNS- will now be information from the GPS receiver.
21
2.4.2.6
INSTALLATION ANO OPERATION MANUAL, MODEL AK-960
‘oPs NAV SWITCHING & ANNUNCIATOR PANEL
Please refer to 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-960.
AUTO DIMMING TEST:
A Photocell provides tne 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
22 31
3.2
3.24
GENERAL
(OPS / NAV SWITCHING & ANNUNCIATOR PANEL
SECTION Ill
OPERATION
‘This section describes the operation of the GPS / NAV Switching
and Annunt
OPERATION
\ciator Panel, Model AK-950L
OPERATION FOR MODELS AK-950 - GNS530
(GARMIN)
VLociGPs
Pushing the CDI Switch selects the
MOMENTARY navigation source (VOR / ILS / LOC or GPS)
SWITCH
Gps
oBs
SWITCH
msc
wet
ANNUNC,
to be displayed on the GNS
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
(sirspace 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
vioc
GPs
Auto
oBs
TERM
APR
Msc
weT
(OPS / NAV SWITCHING & ANNUNCIATOR PANEL,
The VLOC / GPS / AUTO / OBS / TERM / APR
MSG / WPT Annunciator is automatically lit
upon the GNS- iates the corresponding
status / mode Indication,
ANNUNC.
24 INSTALLATION AND OPERATION MANUAL, MODEL AR. 960
SECTION IV
WARRANTY
LIMITED WARRANTY
All 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
retumed 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 clai
This limited warranty does not cover or apply to any of the
followings, including: misuse of the equipment; installation or
operation not in accordance with factory instructions; accidents
oF negligent damage; alterations of any manner; repair by other
28
INSTALLATION AND OPERATION MANUAL, MODEL AK.960
{0P3 HAV SWITCHING & ARMUNCIATOR 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 personal 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 all such injuries or damage.
In such cases, the repair will be billed at cost. An estimate will
be submitted for approval beford Yepair is initiated.
Any equipment which is retumed for warranty and found not to
be defective shall be charged a minimum handling and service
charge and returned C.0.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 forms) 337 or 8130-l.
THE IMPLIED WARRANTY AND ALL OTHER IMPLIED
WARRANTIES ARE HEREBY EXCLUDED. AMERI- KING CORP.
MAKES NO OTHER WARRANTY OR REPRESENTATION OF ANY
KIND 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 AMERI- KING CORP. BE LIABLE FOR ANY
CONSEQUENTIAL, 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 a2
a3
INSTALLATION AND OPERATION MANUAL, MODEL AK-960
(OPS | NAV SWITCHING & ANNUNCIATOR PANEL
REPAIR SERVICE
All equipments manufactured by Ameri-King Corp. must be
repaired at the facility of Ameri-King Corp.
All the repair services shall be performed and completed within
3 days upon repairing estimate is approved by equipment user or
installation dealer.
FACTORY COMPREHENSIVE TEST SERVICE
Factory Comprehensive Test Service is available, There is a
service charge for this service. All equipments returned for
Factory Comprehensive Test Service must be sent freight
prepaid,
27 INSTALLATION AND OPERATION MANUAL, MODEL AK 960
‘OPS / NAV SWITCHING & ANNUNCIATOR PANEL
APPENDIX_A
ENVIRONMENTAL QUALIFICATION FORM
RTCA / DOIGOC
NOMENCLATURE: AK 9S0 GPS / NAV. SWITCHING AND
RELAMPABLE ANNUNCIATOR PANEL
MODELNO: AK98% — TSONO: C29 CLASS AT
MANUFACTURER: AMERI- KING CORP,
842 DROOKIURST ST.
FOUNTAIN VALLEY, CA 92708
Daspion of Conti Tes
Temp. & Altiude x Equipment tested to Categories
AL&DI
Low temperature
High Temperature
In-Flight Loss of i Cooling air not requited
Cooling
Altitude
Decompression
Overpressure
INSTALLATION ANO OPERATION MANUAL, MODEL AK-960
(PS / NAV SWITCHING & ANNUNCIATOR PANEL
ENVIRONMENTAL QUALIFICATION (Cont'd)
Fluids Susceptibiti Equipment identified as
Category X, no test required
Sand and Dust . ‘Equipment identi
Category X, no test required
Equipment identified as
Category X, no test required
Salt Spray
Magnetic Effect
‘Temp. Variation Equipment tested to Category C
Humidity Equipment tested to Category A
Shock . Equipment tested per DO-160C
Operational Par. 7.2.1
Crash Safety
Vibration Equipment tested without shock-|
‘mounts to Categories M & N
(Table 8-1)
Explosion Equipment identitied as
Category X, no test requited
‘Waterprootness ‘Equipment identified as
Category X, no test required
28
Radio Frequency
Susceptibility
Lightning Induced
Transient
Susceptibility
Equipment identified as
Category X, no test required
Lightning Direct
Effects
Equipment identified as
Category X, no test required
Equipment identified as
Category X, no tést required INSTALLATION AND OPERATION MANUAL, MODEL AK.960
‘OFS | NAV SWITCHING & ANNUNCIATOR PANEL
APPENDIX B
FAA TSO / PMA / STC approved Letters
for Model AK-950 - ( }
30 e snantro ambane wnecroesTE
Ye oeparme [AIRCRAFT CERTIFICATION SERVICE
{LOS ANGELES AIRCRAFT CERTIFICATION OFFICE.
Pestana 23960 PARAMOUNT BOULEVARD
LAKEWOOD, CALIFORNIA 90712-4137
pov 22 6
‘Aart King Corporation
Me Keith Van
18842 rookberst Stet
Femtin Vay, Carn 92708
Amer-King Conportion,
LGPSINAY Switching ad Antaeator Pavel
Techical Stand Order C1294
Your application dated November 7,196, rquetng the eunce of» Tehri! Standard Order
(150) aheizationn accordance withthe procedralrequtements of Federal Aviation
Regulation (FAR) Part 21, Sobpat ©. Based upon your dla and tater! of conformance