Environmental Qualifications
Apollo SL50 / SL60 Installation Manual
43
A
PPENDIX
C - E
NVIRONMENTAL
Q
UALIFICATIONS
The Apollo SL50 and SL60 have been tested to the following environmental categories per
procedures defined in RTCA/DO-160C or DO-160D.
Environmental Qualification Form
Model:
Part No:
TSO No:
SL50
430-6040-4xx
TSO-C129
SL60
430-6040-6xx
TSO-C129, TSO-C37d,
TSO-C38d, TSO-C128
Manufacturer:
II Morrow Inc.
2345 Turner Road SE
Salem, Oregon 97302
Conditions
DO-160C
Section
Description of Conducted Tests
Temperature and Altitude
4.0
Equipment tested to Category C1 with
In-flight Loss of Cooling
4.5.4
No cooling required
Altitude
4.6.1
Equipment tested to 35,000 feet
Overpressure
4.6.3
Equipment tested for overpressure
Temperature Variation
5.0
Equipment tested to Category C, 2
°
C/min
Humidity
6.0
Equipment tested to Category A, standard humidity
environment
Operational Shocks and Crash
Safety
7
Equipment tested for both operational and crash safety
shocks. (Equipment operated normally after the crash safety
shocks.)
Vibration
8.0
Equipment tested without shock mounts to Categories B, M,
& N
Explosion Proofness
9.0
Equipment identified as Category X, no test required
Waterproofness
10.0
Equipment identified as Category X, no test required
Fluids Susceptibility
11.0
Equipment identified as Category X, no test required
Sand and Dust
12.0
Equipment identified as Category X, no test required
Fungus Resistance
13.0
Equipment identified as Category X, no test required
Salt Spray
14.0
Equipment identified as Category X, no test required
Magnetic Effect
15.0
Equipment is Class Z
Power Input
16.0
Equipment tested to Categories A & B
Voltage Spike
17.0
Equipment tested to Category A
Audio Frequency Conducted
Susceptibility - Power Inputs
18.0
Equipment tested to Categories A & B
Induced Signal Susceptibility
19.0
Equipment tested to Category Z
Radio Frequency Susceptibility
(Radiated and Conducted)
20
Equipment tested to Category U
Emission of Radio Frequency
Energy
21
Equipment tested to Category Z
Lightning Induced Transient
Susceptibility
22.0
Equipment tested to -
Category B3 for the GPS navigation connections (37 pin)
Category B1 for the GPS antenna connector
Categories A3 and B2 for the comm connections
Lightning Direct Effects
23.0
Equipment identified as Category X, no test required
Icing
24.0
Equipment identified as Category X, no test required
Remarks:
The Apollo SL60 has been tested to the following environmental categories per procedures
defined in RTCA/DO-160D to support helicopter installations.
Summary of Contents for Apollo SL50 GPS
Page 1: ...Apolloâ Model SL50 GPS Model SL60 GPS VHF COMM Installation Manual February 2002 560 0957 02 ...
Page 4: ...NOTES ...
Page 8: ...Table of Contents iv Apollo SL50 SL60 Installation Manual NOTES ...
Page 16: ...Introduction 8 Apollo SL50 SL60 Installation Manual NOTES ...
Page 36: ...Installation 28 Apollo SL50 SL60 Installation Manual NOTES ...
Page 44: ...Specifications 36 Apollo SL50 SL60 Installation Manual NOTES ...
Page 46: ...Limitations 38 Apollo SL50 SL60 Installation Manual NOTES ...
Page 50: ...Periodic Maintenance 42 Apollo SL50 SL60 Installation Manual NOTES ...
Page 54: ...Accessories 46 Apollo SL50 SL60 Installation Manual NOTES ...
Page 62: ......