Pointer 8000 ELT Handleiding

Pointer Niet gecategoriseerd 8000 ELT

Lees hieronder de đź“– handleiding in het Nederlandse voor Pointer 8000 ELT (17 pagina's) in de categorie Niet gecategoriseerd. Deze handleiding was nuttig voor 217 personen en werd door 2 gebruikers gemiddeld met 4.5 sterren beoordeeld

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AIRCRAFT EMERGENCY LOCATOR
TRANSMITTER
OPERATION AND INSTALLATION
INSTRUCTIONS FOR
MODEL 8000 (AF)
FOR HORIZONTAL MOUNTING IN FIXED WING AIRCRAFT OR
ANGULAR MOUNTING IN ROTARY WING AIRCRAFT
TSO-C126
FCC ID: PNT8000xxx
WARNING!
FOR AVIATION EMERGENCY USE ONLY.
UNAUTHORIZED OPERATION PROHIBITED.
CONTENTS
SECTION 1 DESCRIPTION 2
SECTION 2 DIGITAL MESSAGES 4
SECTION 3 PRE-INSTALLATION 4
SECTION 4 INSTALLATION INSTRUCTIONS 5
SECTION 5 FUNCTIONAL TESTING 9
SECTION 6 OPERATING INSTRUCTIONS 11
SECTION 7 BATTERY INFORMATION AND REPLACEMENT 12
SECTION 1
DESCRIPTION
1.1 Pointer 8000 ELT is a self-contained Emergency Locator Transmitter capable of
automatic or manual operation (AF).
1.2 Pointer 8000 ELT conforms to the new TSO-C126 Digital ELT specification. This
requires that each ELT transmits a unique identifying message, greatly reducing the
impact of false alarms which troubled previous AM 121.5 MHz ELT technology.
1.3 Pointer 8000 ELT is designed to withstand forced landing and crash environment
conditions and survive in an operable condition. The highest quality materials and
components have been selected for manufacturing to insure rugged, reliable equipment.
1.4 Automatic activation is accomplished by a deceleration sensing inertia switch. The inertia
switch is designed to activate when the unit senses crash-specific longitudinal inertia
forces as described in TSO-C91A.
NOTE: When properly installed, parallel to the line of flight, POINTER 8000 ELT will
not activate due to turbulence, normal operation, or aerobatics.
1.5 The Pointer 8000 ELT assembly (P/N 8000-X(Y))(see Figure 1) consists of:
A A high-impact, high visibility, fire retardant, waterproof case.
B A fused battery pack consisting of three Lithium-Manganese Dioxide “D” cells in an
impact resistant polystyrene foam housing (P/N 8007-6).
C An impact-sensing "G" switch tailored to the requirements of aircraft ELT application.
D Two solid-state transmitters, operating at assigned emergency frequencies of 121.5 MHz
and 406.037 MHz. The 121.5 MHz transmission is modulated by a distinctive down-
1
MASTER SWITCH
ON-OFF-AUTO
REMOTE CONTROL JACK
406/121 MHz RF
OUTPUT ANTENNA
GPS ANTENNA
(optional)
RF LED
BATTERY LED
TEST/RESET SWITCH
FIGURE 1. POINTER 8000 OPERATING DETAILS
SWITCH GUARD
OFF
REMOTE JACK
AUTO
ON
PUSH TO TEST
PUSH TO RESET
MASTER
SWITCH
TEST RESULTS
STEADY
BLINKING
GPS
ANTENNA
FAILED
PASSED
RF OUTPUT
ANTENNA
BATTERY
RF
TEST DURATION 10 SEC
sweeping audio tone. The 406 MHz transmitter features a ±1ppm frequency base,
enabling precise doppler-shift triangulation from low earth orbit. The transmission is
modulated with international NOAA/SARSAT/COSPAS telemetry code identifying the
individual ELT and, indirectly, its registered aircraft and owner.
E RF output coaxial connector.
F 2 status indicator LEDs, one for the battery and one for RF output levels.
G A Master “ON-OFF-AUTO” toggle switch.
H A "TEST" pushbutton switch.
I A Remote Control and Status-Indicator connection jack.
J Optionally, an internal GPS receiver and additional coaxial connector for its antenna.
This option can add position data to the digital message.
1.6 The Pointer 8000 ELT accessories (see Figure 2) consist of:
A Dual-frequency RF antenna (P/N 3001-15).
B Antenna interconnection cable (P/N 3002-10).
2

Product specificaties

Merk: Pointer
Categorie: Niet gecategoriseerd
Model: 8000 ELT

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