APPENDIX A-1 -- ASE/AIRCRAFT MATRIX

 

 

AIRCRAFT SURVIVABILITY EQUIPMENT

AH-

1F

AH-

64A

AH-

64D

OH-

58C

OH-

58D

UH-

1H/V

UH-

60A/L

UH-

60Q

CH-

47D

MH-

47E

MH-

60K

EH-

60A

RC-

12

AN/APR-39(V)1

X

X

  

X

X

X

X

  

X

        

AN/APR-39(V)2

                      

X

X

AN/APR-39A(V)1

X

X

X

X

X

  

X

X

X

X

X

    

AN/APR39A(V)2*

                          

AN/APR-44(V)1/3

        

X

  

X

    

X

X

  

X

AN/ALQ-136(V)1

X

                        

AN/ALQ-136(V)2

                  

X

X

  

X

AN/ALQ-136(V)5

  

X

X

                    

AN//ALQ-162(V)2

                      

X

  

AN/ALQ-162(V)3

                    

X

  

X

AN/ALQ-162(V)4

                  

X

      

M-130 (CHAFF)

X

X

X

      

X

X

  

X

X

X

X

AN/ALQ-144A(V)1

        

X

  

X

X

    

X

X

  

AN/ALQ-144A(V)3

X

X

X

                    

AN/ALQ-156(V)1

                

X

        

AN/ALQ-156(V)2

                      

X

X

IR PAINT

X

X

X

X

X

X

X

X

X

X

X

X

X

M-130 (FLARE)

                

X

X

  

X

X

AVR-2

X

                        

AVR-2A

  

X

X

  

X

        

X

X

    

THE AN/APR-39A(V)2 WILL ONLY BE INSTALLED ON USN/USMC AIRCRAFT (SEE PAGE 17)

 

APPENDIX A-2 -- AVIONICS/AIRCRAFT MATRIX

 

 

AVIONICS

EQUIPMENT

AH-

1F

AH-

64A

AH-

64D

OH-

58C

OH-

58D

UH-

1H/V

UH-

60A/L

UH-

60Q

CH-

47D

MH-

47E

MH-

60K

EH-

60A

RC-

12

AN/ARC-164

X

X

X

X

X

X

X

X

X

X

X

X

  

AN/ARC-199

      

X

X

X

X

  

X

        

AN/ARC-220(V)1

  

X

      

X

X

  

X

    

X

  

AN/ARC-220(V)2

    

X

  

X

    

X

  

X

X

    

IMPROVED DATA MODEM

    

X

  

X

    

X

          

IMPROVED FM

X

X

X

X

X

X

X

X

X

    

X

  

AN/AYD-1

          

X

X

X

X

X

X

    

AN/ANS-128B

            

X

  

X

        

AN/ASN-128C

              

X

          

AN/APN-209(V)

    

X

  

X

  

X

X

X

X

X

X

  

H-764G EGI

  

X

X

  

X

        

X

X

    

AMPS

  

X

X

  

X

  

X

X

X

        

A2C2S

            

X

            

 

APPENDIX A-3 -- COMMUNICATIONS COMPONENT/AIRCRAFT MATRIX

 

 

RADIO

FM #1

KY

FM #2

KY

VHF-AM

KY

UHF-AM

KY

HF

KY

AIRCRAFT

ARC-201

KY-58

ARC-201

KY-58

ARC-186

KY-58

ARC-164

KY-58

ARC-2201

KY-100

AH-64A

RT-1476A3

1

RT-1354/

ARC-186

(SHARED2)

  

RT-1354

(SHARED2)

  

RT-1518C

  

ARC-220

1

AH-64D

(PLANNED)

RT-1478D

(SIP)

1

PART

OF SIP

RT-1478D

(SIP)

1

PART

OF SIP

RT-1300B

  

RT-1614

1

BUS

INTERFACE5

ARC-220

W/O

CDU

1

BUS

INTERFACE5

UH-60A/L

RT-1477A/C

1

RT-1477A/C

1

RT-1300A

  

RT-1518C

1

ARC-220

1

UH-60Q

MEDEVAC

(PLANNED)

RT-1478D

(SIP)

1

PART

OF SIP

RT-1478D

(SIP)

1

PART

OF SIP

ARC-2224

  

RT-1614

ON BUS

CONTROLLED

BY A/C CDU6

1

BUS

INTERFACE5

ARC-220

W/O

CDU

1

BUS

INTERFACE5

OH-58C

RT-1476A

1

RT-1476A

1

RT-1354

  

RT-1518C

      

OH-58D

RT-1478A

 

1

ON BUS

RT-1478A

1

(SHARED)

ON BUS5

RT-1300B

0

(SHARED)

ON BUS

RT-1614

0

(SHARED)

ON BUS

ARC-220

W/O

CDU

1

BUS

INTERFACE5

OH-58D

(PLANNED)

RT-1478D

(SIP)

1

PART

OF SIP

RT-1478D

(SIP)

1

PART

OF SIP

RT-1300B

1

RT-1614

1

ARC-220

W/O

CDU

1

BUS

INTERFACE5

CH-47D

RT-1476A3

1

    

RT-1354

  

RT-1518C

  

ARC-220

1

AH-1F

RT-1476A

1

    

RT-1354

  

RT-1518C

      

UH-1H

RT-1477A

1

RT-1476A

  

RT-1354

OR

RT-1300A

  

RT-1518()

OR

RT-1504

      

UH-1V

MEDEVAC

RT-1477A

1

RT-1476A

  

RT-1354

OR

RT-1300A

  

RT-1518()

OR

RT-1504

  

ARC-220

1

 

NOTES: 1. ARC-220 SYSTEM: Receiver/Transmitter RT-1749

Power Amp/Coupler AM-7531

CDU C-12436

2. On the AH-64A, the VHF-FM #2 and VHF-AM share the RT-1354/ARC-186 using one antenna.

3. Only one SINCGARS Radio is installed in the CH-47D and AH-64A.

4. ARC-222 is a VHF-AM/FM Multiband Radio and is controlled by a bus with an emergency control head in the event of dual bus failure.

5. A bus interface is required for COMSEC control from the aircraft bus. There is no bus compatible KY device at this time.

6. Blackhawk is considering using the RT-1614 (bus controlled) by converting the RT-1518C or through CECOM management. (6/96)

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

A-2

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

A-3

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

A-4