Справочник Пользователя для Honeywell International Inc. WLUWIFIM010
CAGE CODE:
97896
SCALE: NONE
SIZE: A
DWG NO.
REV:
SHEET 11
HIF-1472R6(1)
Test Name
Source
Category
Boeing Requirements
Normal Steady State Voltage
Boeing 787B3-0147 Rev C, Sect
3.3.3.1.B.5.5.1
3.3.3.1.B.5.5.1
QTPR Sect 8.2.
Test (32.8VDC) exceeds SCD WLANU180
(29.5VDC)
Test (32.8VDC) exceeds SCD WLANU180
(29.5VDC)
Voltage Ripple
Boeing 787B3-0147 Rev C, Sect
3.3.3.1.B.5.5.2
3.3.3.1.B.5.5.2
QTPR Sect 8.4.
Normal Voltage Transients
Boeing 787B3-0147 Rev C, Sect
3.3.3.1.B.6.1
3.3.3.1.B.6.1
QTPR Sect 8.5.
SCD WLANU181 requires longer transient
(150mS) than Boeing 787B3-0147 Rev-C
(50mS).
SCD WLANU181 requires longer transient
(150mS) than Boeing 787B3-0147 Rev-C
(50mS).
Voltage Spike
Boeing 787B3-0147 Rev C, Sect
3.3.3.1.B.6.2 which is equivalent to DO-160
(E)
3.3.3.1.B.6.2 which is equivalent to DO-160
(E)
QTPR Sect 8.6.
Supplementary Voltage
Transients
Transients
Boeing 787B3-0147 Rev C, Sect 3.3.3.1.1.
QTPR Sect 8.7
Supplementary Trapezoidal
Transients
Transients
Boeing 787B3-0147 Rev C, Sect
3.3.3.2.B.7.1.
3.3.3.2.B.7.1.
QTPR Sect 8.8
Abnormal Steady-State And
Abnormal Transients
Abnormal Transients
Boeing 787B3-0147 Rev C, Sect
3.3.3.2.B.8.1.
3.3.3.2.B.8.1.
QTPR Sect 8.9 and 8.10
DC Reverse Polarity
Boeing 787B3-0147 Rev C, Sect 3.4.2.
QTPR Sect 8.11
Load Equipment Influence
Boeing 787B3-0147 Rev C, Sect 3.4.3.
QTPR Sect 8.12
EME Related Tests
Electrostatic Discharge (ESD)
Susceptibility
Susceptibility
Boeing D6-16050-5 Rev C, Section 7.1
QTPR Sect 11
AF Electric Field Susceptibility
- Wiring
- Wiring
Boeing D6-16050-5 Rev C, Section 7.2.1
QTPR Sect 9.4
AF Magnetic Field
Susceptibility - Wiring
Susceptibility - Wiring
Boeing D6-16050-5 Rev C, Section 7.2.2
QTPR Sect 9.3
AF Magnetic Field
Susceptibility - Equipment
Susceptibility - Equipment
Boeing D6-16050-5 Rev C, Section 7.2.3
QTPR Sect 9.2
Conducted RF Susceptibility
Boeing D6-16050-5 Rev C, Section 7.3.1
QTPR Sect 9.6
Radiated RF Susceptibility
Boeing D6-16050-5 Rev C, Section 7.3.2
QTPR Sect 9.7
Ground Injected Transient
Susceptibility
Susceptibility
Boeing D6-16050-5 Rev C, Section 7.4.1
QTPR Sect 10.3
Pin-Injected Transient
Susceptibility
Susceptibility
Boeing D6-16050-5 Rev C, Section 7.4.2
QTPR Sect 10.1
Cable-Injected Transient
Susceptibility
Susceptibility
Boeing D6-16050-5 Rev C, Section 7.4.3
QTPR Sect 10.2
Lightning Induced Multiple-
Burst Transient Susceptibility
Burst Transient Susceptibility
Boeing D6-16050-5 Rev C, Section 7.4.4
QTPR Sect 10.4
Induced Spikes Susceptibility
Boeing D6-16050-5 Rev C, Section 7.5
QTPR Sect 9.5
AF Capacitive Coupling
Boeing D6-16050-5 Rev C, Section 8.1.1.
QTPR Sect 9.9
AF Inductive Coupling
Boeing D6-16050-5 Rev C, Section 8.1.2
QTPR Sect 9.10
RF Conducted Emissions
Boeing D6-16050-5 Rev C, Section 8.2.1
X
QTPR Sect 9.11
RF Radiated Emissions
Boeing D6-16050-5 Rev C, Section 8.2.2
X
QTPR Sect 9.12
Table 7-5 FCC License
Description
FCC CFR
Wi-Fi Operation
47 CFR 15.247
7.3.
System Operation
There are no user controls located on the WLU. The TWLU and CWLUs are managed, monitored, configured,
and controlled by the WLAN Manager function. WLAN Manager is hosted on the CIS-MS Server. These
wireless devices need to be configured dynamically so that they comply with country regulations when the
aircraft lands.