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QA-3000 Product Family
The QA-3000 GPS
WAAS Receiver Family is intended to be used in all airborne avionics applications.
With an MTBF of 50,000 hours, the QA-3000 upgrades equipment capability
with a miniaturized GPS. The QA 3000 specification includes TSO C129a, TSO
C145a, Primary Means, and PA. The QA 3000 includes pRAIM, FDE, and BIT. The
QA 3000 product family includes the following:
Mark
I
Certification: TSO C129 Class B1, B2, C1, C2 and software upgrade to TSO
C145a Beta Class1.
MARK II
Certification: TSO C129 Class B1, B2, C1, C2 and TSO C145a Beta Class1.
MARK III Certification:
TSO C129 Class B1, B2, C1, C2 and TSO C145a Beta Class 2.
Weight: 9 ounces (max)
Dimensions (inches): H (0.75) x L (4.0) x W (2.4)
Electrical
I/F: TTL/RS 422, 5 VDC, +/-15V VDC,
RS 232, GPS Antenna
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QA-5000
Product Family
The QA-5000 GPS
WAAS Receiver Family is intended to be used in all airborne avionics
applications where size and weight are critical. With an MTBF of 40,000
hours, the QA-5000 upgrades equipment capability with a miniaturized GPS.
The QA 5000 specification includes TSO C129a, TSO C145a, Primary Means, and
PA. The QA 5000 includes pRAIM, FDE, and BIT. The QA 5000 product family
includes the following:
·
Mark I
Certification: TSO C129 Class B1, B2, C1, C2 and software upgrade to TSO
C145a Beta Class1.
·
MARK II Certification: TSO
C129 Class B1, B2, C1, C2 and TSO C145a Beta Class1.
·
MARK III Certification: TSO C129
Class B1, B2, C1, C2 and TSO C145a Beta Class 2.
Weight: 3.5 lbs (max)
Dimensions (inches): H (5.1) x L (7.1) x W (1.87)
Electrical
I/F: D-Type, ARINC 429, 28 VDC, RS
232 (test only), BNC Antenna
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QA-7000 Product Family
The QA-7000 GPS WAAS Receiver Family is
intended for airline use with its 1 MCU standard ATR configuration. With an
MTBF of 45,000 hours, the QA-7000 upgrades aircraft systems with GPS WAAS
capability. The QA 7000 specification includes TSO C129a, TSO C145a, Primary
Means, and PA. The QA 7000 includes pRAIM, FDE, and BIT. The QA 7000 product
family includes the following:
·
Mark I
Certification: TSO C129 Class B1, B2, C1, C2 and software upgrade to TSO
C145a Beta Class1.
·
MARK II Certification: TSO C129
Class B1, B2, C1, C2 and TSO C145a Beta Class1.
·
MARK III Certification: TSO C129 Class
B1, B2, C1, C2 and TSO C145a Beta Class 2.
Weight: 4.5 lbs (max)
Dimensions (inches): 1 MCU, H (7.64) x L (15.23) x W (1)
Electrical
I/F: ARINC 600, ARINC 429, 28 VDC
For more information go to the Quantum
Avionics customer service link care.html.
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All
Quantum Avionics products are designed and qualified to meet FAA/EASA
standards.
Hardware:
RTCA DO-160 (latest)
Prog.
Hardware: RTCA DO-254
Software:
RTCA DO-178B
Safety:
SAE ARP 4761
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For
Near Real Time Iono grid status, see the William J. Hughes FAA Technical
Center web site
for the ACB-430 National Satellite Test Bed at:
http://www.nstb.tc.faa.gov/RT_VerticalProtectionLevel.htm

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