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