Narco Avionics MK12D TSO Скачать руководство пользователя страница 6

SEPTEMBER 1998  

 

 

 

 

 

 

 

                

REV. E 

 

2.6  REMOVAL AND INSTALLATION 

The existing MK12 or MK12A can be removed by first disconnecting all cables and 
then releasing the locking screw at the rear of the unit. The MK12B's have a front 
mounted cam lock that can be released by removing the snap in button on the trim 
panel and using a screw driver to release the radio ( some MK12B's may be installed 
in MK12 or MK12A trays and they would use the rear locking screw). Before 
installing the MK-12DR all existing cables and connectors should be inspected and 
cleaned. To install the MK-12DR route the cables the same as before and connect the 
antenna cables to the back of the unit. The MK-12DR should then be secured with 
either the rear latching screw. If replacing an MK12B a rear quater turn latching 
screw must be used.  These should be available at most shops.  If DME or Glideslope 
channeling is needed refer to section 2.7 for instructions. For ease of removal the 
MK-12DR has a convenient handle that is released with a phillips head screw. The 
existing power unit is not needed and can be removed, the included adapter plug must 
be installed at the end of the power unit cable ( black wire to airframe ground ) Fig 2-
7. 

 

Warning! Failure to remove the power unit will do severe damage to the 

 MK12D/R.

 

 
2.7  KEEP ALIVE AND REMOTE CHANNELING ( P5 ) 

Keep alive is no longer needed on the newer versions of the MK12D/R. Reference to 
keep alive on P5 is kept to be consistant with earlier versions.  For installations 
requiring Glideslope and/or DME channeling table 2-1 list the pin connections on P5. 
To enable 2 of 5 Glideslope channeling pin 8 should be connected to ground. The 
original Glideslope and DME channeling cables should be cut off the MK12(A/B) 
and wired to P5 using a DB37 female connector ( supplied ). Refer to figures 2-2, and 
2-3 for these channeling connections. 
 

PIN # 

FUNCTION 

PIN # 

FUNCTION 

108.1/110.1, A-MHZ 

20 

109.1/111.1, A-KHZ 

108.3/110.3, B-MHZ 

21 

109.3/111.3, B-KHZ 

108.5/110.5, C-MHZ 

22 

109.5/111.5, C-KHZ 

108.7/110.7, D-MHZ 

23 

109.7/111.7, D-KHZ 

108.9/110.9, E-MHZ 

24 

109.9/111.9, E-KHZ 

G.S. ACTIVATE 

25 

50 KHZ 

7 A/B 

26 GROUND 

8 2/5 

ENABLE 

27 ARINC 

9  

28  

10  

29 KEEP 

ALIVE 

11  

30  

12 SWITCHED 

A+ 

31 GROUND 

13  

32 50 

KHZ 

14 

 

33 

NARCO 'L', E-KHZ 

15 

NARCO 'A', E-MHZ 

34 

NARCO 'K', D-KHZ 

16 

NARCO 'E', D-MHZ 

35 

NARCO 'J', C-KHZ 

17 

NARCO 'D', C-MHZ 

36 

NARCO 'H', B-KHZ 

18 

NARCO 'C', B-MHZ 

37 

NARCO 'F', A-KHZ 

19 

NARCO 'B', A-MHZ 

 

 

TABLE 2-1 

P-5 FUNCTIONS 

Содержание MK12D TSO

Страница 1: ...NARCO AVIONICS MK12D TSO MK12 MK12A MK12B REPLACEMENT RADIO ADDENDUM INSTALLATION MANUAL 03118 0620R NARCO AVIONICS INC 270 COMMERCE DRIVE FT WASHINGTON PA 19034 U S A PRINTED IN U S A JUNE 1999 ...

Страница 2: ...ere changed at each revision level The affected page number the revision level and the date of the change are listed Additionally the date and revision level is changed on the bottom of the affected pages PAGE DATE REV PAGE DATE REV PAGE DATE REV PAGE DATE REV PAGE DATE REV 3 10 96 D 5 10 96 D 5 09 98 E 6 09 98 E 8 06 99 F 9 06 99 F JUNE 1999 REV F ...

Страница 3: ... or Narco 11 wire DME channeling 2 0 INSTALLATION 2 1 INTRODUCTION The MK 12DR is a direct replacement for the MK12 MK12A MK12B NAV COM units It s specifications meet or exceed those of the unit it is replacing 2 2 TECHNICAL SPECIFICATION AND PERFORMANCE ADJUSTMENTS The MK 12DR is a specially modified MK 12D Cessna unit The mechanical modifications effect the physical size latching method and inte...

Страница 4: ...eet the appropriate TSO otherwise the TSO will not be valid NAV Receiver The NAV receiver of the MK 12DR is designed to meet VOR TSO C40b and Localizer TSO C36c Class C The MK 12DR when replacing a MK12 MK12A or MK12B will typically be used with one of the VOA series indicator converters The following table lists these units and their TSO s if applicable INDICATOR CONVERTER TSO VOA 4 VOA 5 NONE VO...

Страница 5: ...el The MK12DR TSO has a solid state speaker amplifier for improved audio response and reliability and this type amplifier cannot be paralleled For these installation it is recommended that the installation be modified according to figure 2 1 Warning Failure to comply with this section will cause damage to one or both units FIG 2 1 JUNE 1996 REV C 5 ...

Страница 6: ...r plug must be installed at the end of the power unit cable black wire to airframe ground Fig 2 7 Warning Failure to remove the power unit will do severe damage to the MK12D R 2 7 KEEP ALIVE AND REMOTE CHANNELING P5 Keep alive is no longer needed on the newer versions of the MK12D R Reference to keep alive on P5 is kept to be consistant with earlier versions For installations requiring Glideslope ...

Страница 7: ...FIG 2 2 GLIDESLOPE CHANNELING FIG 2 3 DME CHANNELING JUNE 1996 REV C 7 ...

Страница 8: ... jumper plug Fig 2 4 2 8 1 PIPER SPECIAL There were a number of MK12s manufactured as Piper specials Refer to Figure 2 5 to see the rear panel of a Piper special Figure 2 7 lists what the connections of P301 were and the appropriate connections on the MK12D R A mating connector for P301 of the MKD R would have to be found to complete the installation Fig 2 5 T 102 J 101 T 101 P 101 P 301 J 301 JUN...

Страница 9: ...16 NC P501 JUMPER PLUG CONNECTIONS PIN PIN 3 7 4 6 5 12 8 16 11 13 FIG 2 6 MK12D R MK12 P5 J301 1 A 18 01 110 1 6 B GLIDESCOPE ACTIVATE 24 C 109 9 111 9 2 D 108 3 110 3 7 E 10 20 A B BANK CONTROL CANNEL CONTROL 23 F 109 7 111 7 3 H 108 5 110 5 25 J N C 50 KHz 46 RZA UGRS 22 K 109 5 111 5 4 L 108 7 110 7 TO AIRCRAFT GROUND M GROUND 21 N 109 3 111 3 5 P 108 9 110 9 20 R 109 1 111 1 P301 1 S OMNI LOC...

Страница 10: ...ONT PANEL 2 9 1 COM Section Operation COM DISPLAY The left side of the display identifies the COM Active COMmunications frequency and the letter T when lit to indicate that the Mike Key is depressed and the Unit is transmitting The right side of the display identifies the COM Standby frequency COM OFF VOL PULL TEST OFF is the maximum counterclockwise rotation of this control Clockwise rotation pas...

Страница 11: ...or KHz knobs COM TRANSFER Pressing this white arrowed momentary switch flips the display The Standby frequency becomes the Active and the Active becomes the Standby A second depression exchanges the frequencies 2 9 2 NAV Section Operation NAV DISPLAY The left side of the display identifies the NAV Active communications frequency The right side of the display identifies the NAV Standby frequency NA...

Страница 12: ...dicator appears unaffected verify that the station being received is the station selected prior to the blackout pull IDENT If you are still set to your desired frequency continue your flight it can be presumed that you had a display or a display circuit failure If the COM DISPLAY should have a total blackout verify that the COM is still set to the frequency selected prior to the blackout Verificat...

Страница 13: ...wing what frequency you had set in Active and Standby windows it is now a matter of rotating the KHz and MHz knobs clockwise incrementing and counterclockwise decrementing detent by detent KHz 25 KHz steps MHz 1 MHz steps to change frequencies Remember all entries go into the Standby display window before they can be transferred to the Active display memory Should it appear that in changing freque...

Страница 14: ... and most important is a complete inspection of the installation to be sure that all aircraft flight controls operate freely with full travel or deflection Since these procedures cover Units with and without glideslope simply bypass those functions glideslope which do not apply to the system being tested A remote mounted Marker Beacon or Glideslope Receiver whose operation is dependent upon the NA...

Страница 15: ...2DR ON and observe that the Active display reads 114 15 and the Standby 110 50 B General 1 Set NAV Active channel to a VOR frequency 2 Rotate the VOL IDENT control clockwise until NAV Receiver noise is heard in the speaker and headphones Note IDENT knob must be pulled out Note presence of NAV and GS warning flags and centered Left Right and Up Down needles 3 Modulate test equipment 30 with 1020 Hz...

Страница 16: ...ight Deflection should be to the end of the Blue and Yellow areas on the Indicator 3 Remove modulation or decrease test equipment RF output to minimum NAV flag should be visible E Glideslope 1 Set test equipment and NAV Active channel to a GS frequency Verify that the Glideslope Receiver is channeled correctly All 40 Glideslope channels should be checked D DME 1 Set test equipment and NAV active c...

Страница 17: ...ommend to perform the following checks and adjustments A Check all avionics under actual operating conditions for abnormal indications ignition noise audio distortion at in flight volume settings rotating beacon noise interference between avionics equipments etc B Look for variations in performance due to various landing gear and flight control surface configurations All of these tests must be per...

Страница 18: ...l confirmation of on glide path condition 3 While on glide path maneuver aircraft through normal pitch and roll attitudes Left Right and Up Down indicators should perform normally and a warning flag should not be visible at anytime DME A Verify DME channeling when in flight 2 11 2 COM section A flight test should be performed to check the antenna pattern and system compatibility A Flying at an alt...

Страница 19: ...JUNE 1996 REV C 19 ...

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