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|  MIL-N-81497A(AS)
External Wiring - External wiring shall be in
3.3.3.2.1
accordance with EI-554.
Control Panels - All rack or console mounted con-
3.3.4
trol panels shall conform to the applicable requirements of MIL-C-6781
Type I except as specified herein.
Control Panel Front Panels - All control panel
3.3.4.1
front panel details shall conform to MIL-C-6781 (Type I), MIL-P-7788
(Class-l) except as specified herein. The configuration of all panels
must be approved by the procuring activity prior to pre-production
testing.
3.3.4.1.1
Panel Front;
Control, Gyroscope Assembly - In
accordance with Figure 1.
3.3.4.1.2
Panel, Front: Control, Navigation - In accordance
with Figure 2.
Panel, Front: Indicator, Position - In accordance
3.3.4.1.3
with Figure 3.
Interchangeability - The equipment shall meet the
3.3.5
interchangeability requirements specified in MIL-E-5400.
Interference Control - The generation of radio inter-
3.3.6
ference by the equipment and the vulnerability of the equipment to
radio interference shall be controlled within the limits of MIL-I-6181.
Short duration interference levels shall be in accordance with 3.3.2
of MIL-I-6181.
Maintainability - The equipment shall meet the main-
3.3.7
tainability requirements specified herein.
In Flight Maintenance - In flight maintenance shall
3.3.7.1
not be a requirement for the equipment. However, the equipment shall
provide both visual and electrical failure indications in the event
of malfunction.
Flight Line Maintenance - The equipment shall be
3.3.7.2
designed to permit corrective maintenance to be performed within a
mean time of 30 minutes (MIN) for 95 percent of all detected system
failures.
Corrective maintenance shall consist of fault isolation
to an individual unit (LRU), unit replacement, and equipment checkout.
The 30 MIN shall not include equipment warm-up and alignment time.
LRU malfunction displays shall be provided on the Control, Gyroscope
Assembly. Flight line maintenance shall be accomplished in a Self Test
submode.
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