True Blue Power
®
17
Manual Number 9017680
a division of Mid-Continent Instrument Co., Inc.
Revision G, July 17, 2019
SECTION 5
CONFORMANCE
5.1
CONTINUED AIRWORTHINESS STATEMENT
No periodic scheduled maintenance or calibration is necessary for continued airworthiness of the TI1200
Series Static Inverter. If the unit fails to perform to specifications, the unit must be removed and serviced
by Mid-Continent Instruments and Avionics or their authorized designee.
5.2
ENVIRONMENTAL QUALIFICATION STATEMENT
NOMENCLATURE:
Static Electrical Power Inverter
MODEL NUMBER:
TI1200, TI1202, TI1204
TSO NUMBER:
C73
MANUFACTURERS SPECIFICATIONS:
Minimum Performance Specifications: Test Specification (TS)
501, Test Data Sheet (TDS) 501
QUALIFICATION STANDARD:
RTCA DO-160G
CONDITIONS
SECTION
DESCRIPTION OF TEST
Temperature and Altitude
Low Temperature
High Temperature
In-Flight Loss of Cooling
Decompression
Overpressure
4
4.5.1
4.5.2
4.5.5
4.6.2
4.6.3
Category F3(Y)
Operating Low Temp = -55C
Operating High Temp = +70C
Category Y = 300 minutes, +40C, 75%
Altitude = +55,000 ft
-15,000 ft
Temperature Variation
5
Category S2
Humidity
6
Category B
Operational Shock and
Crash Safety
7
Category B
Vibration
8
Category R, Curve C, C1
Category U, Curve G
[(RCC1)(UG)]
Explosion
9
Category H
Waterproofness
10
Category W
Fluids
11
Category X
Sand and Dust
12
Category X
Fungus
13
Category X
Salt Spray
14
Category X
Magnetic Effect
15
Category Z
Power Input
16
Category A(RI)
Voltage Spike
17
Category A
Audio Frequency Conducted
Susceptibility
18
Category R
Induced Signal Susceptibility
19
Category AC
Radio Frequency Susceptibility
20
Category R
Emission of Radio Frequency
Energy
21
Category B
Lightning Induced Transient
Susceptibility
22
Category A3
Lightning Direct Effects
23
Category X
Icing
24
Category X
ESD
25
Category A
Flammability
26
Category C
Table 5.2: List of DO-160G Category Qualifications by Section
