VAL Avionics INS 422 Installation & Owner's Manual

Summary of INS 422

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    Original issue 1 avionics limited ins 422 integrated navigation system installation/owners manual vpn 701034 june 2001.

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    A v i o n i c s l i m i t e d i n s 4 2 2 i n t e g r a t e d n a v i g a t i o n s y s t e m installation/owners manual june 2001 © 2001 by val avionics, ltd. All rights reserved printed in the u. S. A. Val avionics, ltd. Will continually improve product quality and performance. Information contain...

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    A v i o n i c s l i m i t e d table of contents section i general information paragraph 1.1 introduction 1.2 description of equipment 1.3 technical characteristics 1.4 units and accessories required (supplied) 1.5 accessories required (not supplied) 1.6 license requirements 1.7 statement of complian...

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    A v i o n i c s l i m i t e d section ii installation paragraph 2.1 general information 2.2 unpacking and inspecting 2.3 equipment installation 2.3.1 avionics cooling requirements for panel mounted equipment 2.3.2 pre-installation information 2.3.3 antenna installation 2.3.4 audio interface 2.3.5 ha...

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    A v i o n i c s l i m i t e d section iii operation paragraph 3.1 power on unit 3.2 controls and accessories of the front panel 3.3 operation 3.4 auto-dimmer photocell illustrations figure 1 . 0 m o u n t i n g t e m p l a t e 1 . 1 f r o n t - r e a r - s i d e d i m e n s i o n s 1 . 2 f u n c t i...

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    A v i o n i c s l i m i t e d ins 422 installation/owners manual original issue – june 2001 vpn 701034 5 section i general information paragraph 1.1 introduction this manual provides information relative to the physical, mechanical and electrical characteristics of the ins 422 integrated navigation ...

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    A v i o n i c s l i m i t e d 1.3 technical specifications specifications characteristics environmental: (rtca/do160d) vor rtca/do-196 localizer rtca/do-195 glideslope rtca/do-192 marker beacon rtca/do-143 class b physical dimensions: height 3.32 inches (8.44cm) width 3.45 inches (8.76cm) depth 10.8...

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    A v i o n i c s l i m i t e d ins 422 installation/owners manual original issue – june 2001 vpn 701034 7.

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    A v i o n i c s l i m i t e d 1.4 units and accessories supplied 1.4.1 ins 422 installation kit (vpn 651001) vpn description quantity 501067 screw 3/8” 6-32 6 550022 bnc connector 3 550062 contact terminal 10 701034 installation manual 1 750014 connector and harness assembly 1 501057 fibernut, 6-32 ...

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    A v i o n i c s l i m i t e d ins 422 installation/owners manual original issue – june 2001 vpn 701034 9 section ii paragraph installation 2.1 general information this section provides interconnect diagrams and installation criteria for the ins 422 navigation receiver. By following these instruction...

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    A v i o n i c s l i m i t e d 2.3 equipment installation the ins 422 installation will conform to standards designated by the customer, installing agency and existing conditions as to the unit location and type of installation. However, the following suggestions should be considered before installin...

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    A v i o n i c s l i m i t e d 2.3.2.1 panel location the ins 422 is rigidly mounted in a standard 3.125” round cutout on the aircraft panel. Once a location has been selected, a visual inspection should be made of the area directly behind the panel which, will be occupied by the ins 422 and harness ...

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    A v i o n i c s l i m i t e d 2.3.3 nav/glideslope/marker antenna installation navigation, glideslope and marker antennae should be installed as per faa advisory circular ac43.13-2a methods and guidelines and the appropriate manufacturers instructions. Navigation couplers can be utilized to provide ...

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    A v i o n i c s l i m i t e d 2.4 post- installation checkout an operation performance flight test should be made after the installation to ensure satisfactory performance of the equipment in its intended environment. The installing agency using appropriate ramp testing equipment should verify prope...

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    A v i o n i c s l i m i t e d 2.4.1 post-installation adjustments the ins 422 has been calibrated and adjusted at the factory. Additional adjustments required by the installing agency (with specialized, precision test equipment) to fine tune the localizer and glideslope display indications can be ac...

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    A v i o n i c s l i m i t e d 2.4.2 periodic maintenance the ins 422 does not require any regular general maintenance except as described in this section. A. Vor checks vor accuracy checks required for ifr flight must be performed on the ins 422 every 30 days to verify the unit does not exceed the a...

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    A v i o n i c s l i m i t e d ins 422 installation/owners manual original issue – june 2001 vpn 701034 16 section iii operation paragraph 3.1 power on unit it is recommended that power to the ins 422 be turned on only after engine start-up. This procedure increases the reliability of the solid-state...

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    A v i o n i c s l i m i t e d 3.3 operating instructions 3.3.1 initial turn on on initial activation, the frequency 112.50 mhz is tuned and displayed. The three marker lights, localizer course and glidepath deviation light bars will be momentarily fully illuminated (when off frequency or out of rece...

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    A v i o n i c s l i m i t e d the appropriate marker lamp will illuminate with associated audio tone: outer marker (blue) 400 hz middle marker (amber) 1300 hz fan marker (white) 3000 hz indicating the aircraft position throughout the approach. With marker audio present, a marker audio mute feature c...

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    A v i o n i c s l i m i t e d 3.3.3 vor mode the frequencies for vor stations are assigned from 108.00 mhz to 117.95 mhz. When the vor frequency is selected and the aircraft is out of range of the vor station, a flagged condition indicated by a full light bar in both directions vertical and horizont...

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    A v i o n i c s l i m i t e d mounting template figure 1.0 ins 422 installation/owners manual original issue – june 2001 vpn 701034 20 drawing no. 900422-ins1.

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    A v i o n i c s l i m i t e d front/rear/side dimensions figure 1.1 drawing no. 900422-ins2 ins 422 installation/owners manual original issue – june 2001 vpn 701034 21.

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    A v i o n i c s l i m i t e d functions and operation on/off / vol / brg / mkr mute outer marker (blue) gs ctr adj * located under front mounting screws access to loc & gs cent adjust middle marker (amber) fan/inner marker (white) mhz select 1 4 khz select * 5 vor/loc horizonal frequency & bearing d...

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    A v i o n i c s l i m i t e d pin out, function & wire color for p1201 p-1201 ( wiring side view ) ( vpn 550045 ) ins 422 p1201 note: the ins 422 comes with a standard factory wire harness. The description of the wire color and function is listed in the above table. The remaining pin terminals for e...

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    A v i o n i c s l i m i t e d installation and interconnection diagram fuse for circuit protection. 1) use 5 amp circuit breaker or aux audio input aux audio input headphone audio (tip) memory keep alive headset ground (sleeve) aircraft ground is not utilized val intercom option be installed when th...

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    A v i o n i c s l i m i t e d alignment access locations figure 1.5 drawing no. 900422-ins7 ins 422 installation/owners manual original issue – june 2001 vpn 701034 25.

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    A v i o n i c s l i m i t e d bnc and cable assembly (a) cut the cable end square. Remove jacket, braid, and cut dielectric 1/4". Cut cable jacket back only an additional 1/32". Be care- ful not to nick the braid. Flare the braid to accept the cone. Split the jacket 1/4" in 2 places 180 degrees apar...

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    A v i o n i c s l i m i t e d p1205 mechanical assembly figure 1.7 drawing no. 900422-ins6 ins 422 installation/owners manual original issue – june 2001 vpn 701034 27.

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    A v i o n i c s l i m i t e d revision history and instructions manual title : ins 422 installation manual revision : original issue 06/01 part number : vpn 801004 add, delete or replace pages as indicated page action remarks ins 422 installation/owners manual original issue – june 2001 vpn 701034 2...

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    A v i o n i c s l i m i t e d environmental qualification form the ins 422 has been tested to the following environmental categories per procedures defined in rtca/do-160d. Environmental qualification form nomenclature: ins 422 part no.: 801004 manufacturer: val avionics, ltd 3280 25 th st s.E. Sale...

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    A v i o n i c s l i m i t e d ins 422 integrated navigation system factory warranty the equipment delivered with this standard factory warranty is manufactured by val avionics, ltd. And is guaranteed against defective materials and workmanship for one year from date of original retail purchase. Any ...