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Aeroflex IFR 6015, Operation Manual

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Aeroflex IFR 6015 Operation Manual Download Page 20

     

O P E R A T I O N   M A N U A L  
I F R   6 0 1 5  

 

1 - S E R V I C E   U P O N   R E C E I P T   O F   M A T E R I A L S    

S u b j e c t   t o   E x p o r t   C o n t r o l ,   s e e   C o v e r   P a g e   f o r   d e t a i l s .  

  P a g e   1  

O c t   1 / 1 6  

S ER V I C E  U PO N   R EC EI PT  O F  M AT E R I AL

 

U n p a c k i n g  

S p e c i a l - d e s i g n   p a c k i n g   m a t e r i a l   i n s i d e   t h i s   s h i p p i n g   c a r t o n   p r o v i d e s   m a x i m u m   p r o t e c t i o n   f o r   t h e  
I F R   6 0 1 5 .     A v o i d   d a m a g i n g   t h e   c a r t o n   a n d   p a c k i n g   m a t e r i a l   d u r i n g   e q u i p m e n t   u n p a c k i n g .     U s e   t h e  
f o l l o wi n g   s t e p s   f o r   u n p a c k i n g   t h e   I F R   6 0 1 5 .  

  C u t   a n d   r e m o v e   t h e   s e a l i n g   t a p e   o n   t h e   c a r t o n   t o p   a n d   o p e n   t h e   c a r t o n .  

  G r a s p   t h e   I F R   6 0 1 5   t r a n s i t   c a s e   f i r m l y ,   wh i l e   r e s t r a i n i n g   t h e   s h i p p i n g   c a r t o n ,   a n d   l i f t   t h e  

e q u i p m e n t   a n d   p a c k i n g   m a t e r i a l   v e r t i c a l l y .  

  P l a c e   t h e   I F R   6 0 1 5   t r a n s i t   c a s e   a n d   e n d   c a p   p a c k i n g   o n   a   s u i t a b l e   f l a t ,   c l e a n   a n d   d r y   s u r f a c e .  

  R e m o v e   t h e   p r o t e c t i v e   p l a s t i c   b a g   f r o m   t h e   I F R   6 0 1 5   t r a n s i t   c a s e .  

  P l a c e   p r o t e c t i v e   p l a s t i c   b a g   a n d   e n d   c a p   p a c k i n g   m a t e r i a l   i n s i d e   s h i p p i n g   c a r t o n .  

  S t o r e   t h e   s h i p p i n g   c a r t o n   f o r   f u t u r e   u s e   s h o u l d   t h e   I F R   6 0 1 5   n e e d   t o   b e   r e t u r n e d .  

C h e c k i n g   U n p a c k e d   E q u i p m e n t  

  I n s p e c t   t h e   e q u i p m e n t   f o r   d a m a g e   i n c u r r e d   d u r i n g   s h i p m e n t .     I f   t h e   e q u i p m e n t   h a s   b e e n  

d a m a g e d ,   r e p o r t   t h e   d a m a g e   t o   A e r o f l e x .  

  C h e c k   t h e   e q u i p m e n t   a g a i n s t   t h e   p a c k i n g   s l i p   t o   s e e   i f   t h e   s h i p m e n t   i s   c o m p l e t e .     R e p o r t   a l l  

d i s c r e p a n c i e s   t o   A e r o f l e x .

 

 

I F R   6 0 1 5   w i t h   S t a n d a r d   A c c e s s o r i e s  

 

D E S C R I P T I O N  

P AR T   N U M B E R  

Q T Y  

I F R   6 0 1 5  

7 2 4 2 4  

1  

P o w e r   S u p p l y  

6 7 3 6 6  

1  

A n t e n n a  

9 1 7 7 1  

1  

B r e a k o u t   B o x  

6 4 5 8 0  

1  

A n t e n n a   S h i e l d  

6 4 7 4 9  

1  

1 2   I N .   C o a x i a l  
C a b l e   ( A n t e n n a )  

6 2 4 0 1  

1  

7 2   I N .   C o a x i a l  
C a b l e   ( A n t e n n a )  

1 1 2 8 3 0  

1  

5   A   F u s e  

5 6 0 8 0  

1  

T r a n s i t   C a s e  

1 0 2 4 1  

1  

P o w e r   C o r d    
( U S   o n l y )  

6 2 3 0 2  

1  

P O W E R   C O R D  
( E U R O P E A N )  

6 4 0 2 0  

1  

O p e r a t i o n   M a n u a l  
( C D )  

6 0 9 7  

1  

G e t t i n g   S t a r t e d  
M a n u a l   ( p a p e r )  

6 1 0 0  

1  

 

      

 

 

 

A n t e n n a   C o u p l e r   a n d   C a b l e  

 

O P T I O N AL  

A C C E S S O R I E S  

P AR T   N U M B E R  

Q T Y  

D e s k   T o p   S t a n d  

6 3 6 5 6  

1  

T r i p o d  

6 7 4 7 4  

1  

T r i p o d ,   D o l l y ,  

S t a n d  

8 2 5 5 3  

1  

2 5   f t   T N C / T N C  

C O A X I A L   C A B L E  

6 2 4 6 2  

1  

5 0   f t   T N C / T N C  

C O A X I A L   C A B L E  

8 6 3 3 6  

1  

U C - 5 8 4   D u a l  

A n t e n n a   C o u p l e r  

K i t  

1 1 2 3 4 9  

1  

U C - 5 8 4   S i n g l e  

A n t e n n a   C o u p l e r  

K i t  

1 1 2 3 5 0  

1  

M a i n t e n a n c e  
M a n u a l   ( C D )  

6 0 9 5  

1  

Summary of Contents for IFR 6015

Page 1: ...l data under the jurisdiction of the Export Administration Regulations EAR 15 CFR 730 774 It cannot be transferred to any foreign third party without the specific prior approval of the U S Department...

Page 2: ...ored in a retrieval system or transmitted in any form or by any means electronic mechanical photocopying recording or otherwise without the prior permission of the publisher Original Printing Mar 2005...

Page 3: ...Subject to Export Control see Cover Page for details OPERATION MANUAL IFR 6015 THIS PAGE INTENTIONALLY LEFT BLANK...

Page 4: ...le Statement For continued EMC compliance all external cables must be double shielded For continued EMC compliance all external cables must be 3 meters or less in length Nomenclature Statement In this...

Page 5: ...OPERATION MANUAL IFR 6015 Subject to Export Control see Cover Page for details THIS PAGE INTENTIONALLY LEFT BLANK...

Page 6: ...l that may supply or be supplied with AC or DC voltage DC TERMINAL Terminal that may supply or be supplied with DC voltage AC TERMINAL Terminal that may supply or be supplied with AC or alternating vo...

Page 7: ...OPERATION MANUAL IFR 6015 Subject to Export Control see Cover Page for details THIS PAGE INTENTIONALLY LEFT BLANK...

Page 8: ...ls DECLARATION OF CONFORMITY The Declaration of Conformity Certificate included with the Unit should remain with the Unit Aeroflex recommends the operator reproduce a copy of the Declaration of Confor...

Page 9: ...OPERATION MANUAL IFR 6015 Subject to Export Control see Cover Page for details THIS PAGE INTENTIONALLY LEFT BLANK...

Page 10: ...2 Section 3 Specifications 1 3 Section 4 Shipping 1 4 Section 5 Storage 1 5 Appendix A Connector Pin Out Tables Appendix B Metric British Imperial Conversion Table with Nautical Distance Conversions A...

Page 11: ...OPERATION MANUAL IFR 6015 TABLE OF CONTENTS Subject to Export Control see Cover Page for details Page 2 Oct 1 16 THIS PAGE INTENTIONALLY LEFT BLANK...

Page 12: ...before attempting to operate this equipment Refer all servicing of unit to qualified technical personnel ORGANIZATION This manual is divided into the following Chapters and Sections CHAPTER 1 OPERATI...

Page 13: ...OPERATION MANUAL IFR 6015 INTRODUCTION Subject to Export Control see Cover Page for details Page 2 Oct 1 16 THIS PAGE INTENTIONALLY LEFT BLANK...

Page 14: ...3 ADS B GEN 1 1 2 8 2 6 4 GICB 1 1 2 8 2 6 5 Advisory Circular 1 1 2 9 2 7 TACAN Setup Antenna 1 1 2 9 2 8 TACAN Setup Direct Connect 1 1 2 9 2 9 TACAN Testing 1 1 2 10 2 10 TCAS Setup Antenna 1 1 2...

Page 15: ...ept 1 2 4 52 4 5 2 TCAS Testing 1 2 4 55 4 5 3 TCAS Setup 1 2 4 55 4 5 4 TCAS Screen 1 2 4 60 4 5 5 Setup Scenario Data Screen 1 2 4 63 4 5 6 Monitor Screens 1 2 4 65 4 5 6 1 Surveillance Monitor 1 2...

Page 16: ...a Construction 1 2 4 38 Composite TACAN Beacon Signal 1 2 4 39 Airborne Receiver Block Schematic 1 2 4 40 TACAN Pulse Signals 1 2 4 41 AN ARN 84 V TACAN Control Panel 1 2 4 42 15 Hz Cardioid Antenna P...

Page 17: ...OPERATION MANUAL IFR 6015 1 LIST OF TABLES Subject to Export Control see Cover Page for details Page 2 Oct 1 16 THIS PAGE INTENTIONALLY LEFT BLANK...

Page 18: ...Field Valid Data 1 2 4 58 ARA Field Valid Data 1 2 4 59 FS Field Display Data 1 2 4 59 DR Field Display Data 1 2 4 59 CVC Field Display Data 1 2 4 66 VRC Field Display Data 1 2 4 66 CHC Field Display...

Page 19: ...OPERATION MANUAL IFR 6015 1 LIST OF TABLES Subject to Export Control see Cover Page for details Page 4 Oct 1 16 THIS PAGE INTENTIONALLY LEFT BLANK...

Page 20: ...re the shipping carton for future use should the IFR 6015 need to be returned Checking Unpacked Equipment Inspect the equipment for damage incurred during shipment If the equipment has been damaged re...

Page 21: ...OPERATION MANUAL IFR 6015 1 SERVICE UPON RECEIPT OF MATERIALS Subject to Export Control see Cover Page for details Page 2 Oct 1 16 THIS PAGE INTENTIONALLY LEFT BLANK...

Page 22: ...II ADS B MON GICB and TIS Functional modes in future manual releases ADS B GEN XPDR Auto Test provides a full FAR Part 43 Appendix F test All normal user verified parameters are displayed on one scre...

Page 23: ...tion section has been modified to reflect current technologies and improvements Aeroflex has met all FAA requirements and recommends that the user of this type of equipment review the appropriate FAR...

Page 24: ...illuminates when Test Set is receiving replies XPDR Mode or replying to interrogations DME TACAN Mode CTRS Adjusts display contrast BKLT Adjusts display backlight RANGE Increases DME TACAN range and...

Page 25: ...lect UNITS Set to preferred units To change default antenna gain values STEP PROCEDURE 1 Select ANTENNA TYPE Select the appropriate type based on the part number of the antenna Selections are OLD 7005...

Page 26: ...ter B AT 2 5 H r P R E V P A R A M S E T U P X P D R D I A G A N T E N N A B O T T O M R F P O R T A N T E N N A A N T R A N G E A N T H E I G H T T O P 5 0 0 m 1 0 0 m B O T T O M 5 0 0 m 0 0 m A N T...

Page 27: ...OFF NOTE To run diversity test set DIVERSITY to ON and install boot to bottom top antenna T14 Select CHECK CAP STet to YES T15 Select PW R LIM Set to FAR 43 T 2 4 XPDR SETUP AND TESTING DIRECT CONNECT...

Page 28: ...elect COUPLER LOSS Set to loss found on coupler 8 Select UUT ADDRESS Set to AUTO NOTE If aircraft is on the ground set to MANUAL and enter in MANUAL ADDRESS Mode S all calls do not work when the aircr...

Page 29: ...S 5 P O W E R F R E Q P A S S 6 S AL L C AL L P A S S 7 S R E P L Y T I M IN G P A S S 8 S R E P L Y P A S S 9 U F 0 P A S S 1 0 U F 4 P A S S 1 1 U F 5 P A S S 1 2 U F 1 1 P A S S R E T U R N S E L E...

Page 30: ...O S Q T R R U N T E S T B D S D A T A A D S B MO N D F 1 7 R E T U R N 3 Press RUN TEST soft key to start test When a specific extended squitter BDS is captured AVAIL will be displayed to the right of...

Page 31: ...S B A D S B S T O R E D AT A R E T U R N 2 6 4 GICB STEP PROCEDURE 1 Press XPDR Mode Key until ADS B GICB Main Menu is displayed A V A I L B AT 2 5 H r 1 0 5 A I R B O R N E P O S AV A I L 2 0 6 S U...

Page 32: ...STEP PROCEDURE 1 Mount Directional Antenna on Test Set and position friction hinge so Directional Antenna is as shown Connect short RF coaxial cable between Antenna Connector and Test Set ANT Connect...

Page 33: ...n All TACAN test data is displayed on this screen C H A N 1 7 X R F L V L 8 0 d B m F R E Q 9 7 8 0 M H z R A T E 1 0 0 0 k t s I N RANGE 100 00 nm B AT 2 5 H r B R G 2 7 0 d e g ID E N T MO R S E R E...

Page 34: ...2 5 F T AN T C A B L E L O S S 4 5 d B A N T G A I N d B i S Q U IT T E R S O N 1 0 3 G H z 7 1 AL T R E P O R T I N G O N 1 0 9 G H z 6 1 D I S P L A Y E D AL T R E L AT I V E T E S T S E T A A A 9 2...

Page 35: ...ter time Verify TCAS bearing reads 0 15 NOTE If Radio Altimeter Altitude is below 500 ft RA s are inhibited NOTE TCAS I systems do not issue RA s 14 Press STOP TEST Soft Key to stop test 2 12 TIS SETU...

Page 36: ...4 1 8 2 2 3 R N G n m 6 0 0 4 0 0 3 0 0 2 0 0 1 0 0 AL T f t 3 5 0 0 2 0 0 0 1 0 0 0 5 0 0 0 AL T R AT E C L I MB L E V E L L E V E L C L I MB L E V E L H D G d e g 2 3 4 1 7 8 5 6 2 2 0 T R AF F IC...

Page 37: ...shows the selected target parameters in accordance with the selections TIS STATUS field indicates TIS connection status ADDR indicates UUT Aircraft Address ALT UUT field displays UUT aircraft altitud...

Page 38: ...y charging temperature range 5 to 40 C The battery should be charged every three months minimum or disconnected for long term inactive storage periods of more than six months The Battery must be remov...

Page 39: ...lled by an internal battery charger 1 6 BATTERY RECHARGING Refer to 1 2 1 Figure 1 STEP PROCEDURE 1 Connect AC Line Cable to either AC PW R Connector on the DC Power Supply and an appropriate AC power...

Page 40: ...an front panel buttons and display face with soft lint free cloth If dirt is difficult to remove dampen cloth with water and a mild liquid detergent 2 Remove grease fungus and ground in dirt from surf...

Page 41: ...OPERATION MANUAL IFR 6015 1 2 1 Subject to Export Control see Cover Page for details Page 4 Oct 1 16 THIS PAGE INTENTIONALLY LEFT BLANK...

Page 42: ...see Cover Page for details Page 1 Oct 1 16 2 CONTROLS CONNECTORS AND INDICATORS IFR 6015 Front Panel Figure 1 REMOTE VIDEO SYNC RF I O ANT REMOTE XPDR TCAS TACAN SETUP FREQ RF LVL CTRS BKLT TACAN INT...

Page 43: ...nector 1 31 AUX OUT Connector 2 32 AUX OUT Connector 3 33 AUX OUT Connector 4 34 BACKLIGHT Key 19 CHARGE Indicator 21 CONTRAST Key 25 DC POW ER Connector 3 DECREMENT SELECT Data Key 26 RF LEVEL Key 14...

Page 44: ...Key Selects Transponder Auto Test Screen 10 TCAS MODE Select Key Selects TCAS Auto Test Screen ITEM DESCRIPTION 11 TACAN MODE Select Key Selects TACAN Test Screen 12 SETUP Key Displays the SETUP Menu...

Page 45: ...T O E X I T ITEM DESCRIPTION 26 DECREMENT SELECT Data Key Decrements data in slewable fields such as RF LVL This Key also selects data in fields that have fixed functions such as ECHO and SQUITTER 27...

Page 46: ...e for software update and test data dump not active in first release 36 USB DEVICE Connector Remote Control Interface 37 ALTITUDE ENCODER Connector Interface for external encoding altimeter 38 AUX IN...

Page 47: ...OPERATION MANUAL IFR 6015 1 2 2 Subject to Export Control see Cover Page for details Page 6 Oct 1 16 Directional Antenna Figure 2 Breakout Box Front View Figure 3...

Page 48: ...OPERATION MANUAL IFR 6015 1 2 2 Subject to Export Control see Cover Page for details Page 7 Oct 1 16 Breakout Box Top View Figure 4 Breakout Box Bottom View Figure 5...

Page 49: ...OPERATION MANUAL IFR 6015 1 2 2 Subject to Export Control see Cover Page for details Page 8 Oct 1 16 THIS PAGE INTENTIONALLY LEFT BLANK...

Page 50: ...P P C C O M _ P A S S C F F L _ P A S S P P C R A M _ C F C P L D _ P A S S P P C F L _ N V R B AT _ P A S S P P C R MT _ P A S S U S B _ P A S S K E Y P AD _ P A S S F P G A _ P A S S B AT _ F A IL...

Page 51: ...U R N S E L F T E S T STEP PROCEDURE 3 Press SELF TEST Soft Key to display the Self Test Screen B AT 2 5 H r R U N T E S T S E T U P S E L F T E S T D U M P I N F O C F R A M _ P P C C O M _ C F F L _...

Page 52: ...ders that apply the widest system limits Mode S Transponder level is automatically determined European Enhanced Surveillance test capability allows decode and display of GICB derived BDS register cont...

Page 53: ...1 2 3 4 5 D F 1 7 D E T E C T E D N O F L T ID A A 5 0 A A A C 3 4 2 1 5 3 0 3 2 0 4 1 F S 5 N O AL E R T S P I I N A I R V S I N A I R C O U N T R Y U n i t e d S t a t e s R U N T E S T T E S T L I...

Page 54: ...S B Tests ATCRBS Class B transponders 4 GENERIC MODE S Tests Mode S transponders specifically when the class of the transponder is unknown 5 MODE S CLASS A Tests Mode S Class A transponders 6 MODE S C...

Page 55: ...e DATA Keys to slew the data Parameters are ANTENNA TOP or BOTTOM RF PORT Selects ANTENNA ANT CONNECTOR or DIRECT CONNECT via RF I O Connector ANT CABLE LEN or DIR CABLE LEN or CPL CABLE LEN Selection...

Page 56: ...ICB screens STEP PROCEDURE If NO is selected BDS 1 7 1 8 1 9 is not verified and the Test Set will extract the BDS and display content NOTE Some transponders reply to BDS requests even though BDS 1 7...

Page 57: ...tional characteristics of each functional mode of the Test Set B AT 2 5 H r P R E V P A R A M S E T U P G E N E R A L H W T O O L S P W R D O W N 1 0 m i n s E R P U N IT S d B m U N IT S M E T E R S...

Page 58: ...B AT 2 5 H r E N T E R B A C K S P A C E S E T U P S T O R E N A M E A B C D E F G H IJ K L MN O P Q R S T U V W X Y Z a b c d e f g h i j k l m n o p q r s t u vw x y z 0 2 3 4 5 6 7 8 8 9 _ 4 0 0 D...

Page 59: ...screen the Auto Test Screen and up to 19 additional test screens Auto Test completes a full FAR Part 43 Appendix F Test providing decode and display of Elementary and Enhanced surveillance GICB extra...

Page 60: ...N T E S T T E S T L I S T X P D R A U T O T E S T C O N F I G C O N F I G G E N E R I C M O D E S A N T E N N A B O T T O M S E L E C T A N T PASS L E V E L 4 4 Auto Test completes and displays Parame...

Page 61: ...nd OCTAL FS Flight Status The number preceding the text identifies the RTCA DO 181C FS code assignment Indications are ALERT NO ALERT SPI NO SPI AIRBORNE ON GROUND obtained from DF4 VS Vertical Status...

Page 62: ...test list and choose desired test NOTE The test runs until stopped Each pass through the test sequence updates the PASS FAIL indication 1 A C D E C D R S L S P A S S 2 A C F 1 F 2 S P A C E W ID T H...

Page 63: ...E S T B AT 2 5 H r R U N T E S T P R E V T E S T X P D R 3 A C D E C D R S L S N E X T T E S T 3 A C O D E 2 6 2 0 I D E N T X P U L S E A 4 A 2 A 1 B 4 B 2 B 1 C 4 C 2 C 1 D 4 D 2 D 1 X D E C O D E R...

Page 64: ...s including the P2 SLS pulse When P2 level is set at 9 dB and replies are 90 the test indicates PASS If replies are 90 the test indicates FAIL When P2 level is set at 0 dB and replies are 1 the test i...

Page 65: ...s are 90 An arrow identifies FAIL Sets P1 to P3 pulse spacing to outer high must not reply values 3 85 s for Mode 1 and 5 85 s for Mode 2 The test indicates PASS if percent replies are 10 or FAIL if p...

Page 66: ...identified by an arrow F1 to F2 spacing is 20 30 s 0 10 s F1 F2 pulse widths are 0 45 s 0 10 s Reply Delay The Test Set interrogates UUT with Modes 3A and C The test verifies reply delay minus range...

Page 67: ...ied by an arrow F1 to F2 spacing is 20 30 s 0 10 s F1 F2 pulse widths are 0 45 s 0 10 s Reply Delay The Test Set interrogates UUT with Modes 1 and 2 The test verifies reply delay minus range delay is...

Page 68: ...s selected with DATA Keys Top and Bottom measurements are averaged and values are displayed NOTE When an ATCRBS configuration is selected non diversity transponder only the Bottom antenna measurement...

Page 69: ...eceived during the MTL Test sequence PASS FAIL limits are applied NOTE MTL PASS FAIL limits are determined by the selected configuration Refer to Appendix F 3A C Difference The Test Set interrogates w...

Page 70: ...test decodes and displays the discrete address reported in the DF11 replies Mode S All Call The Test Set interrogates UUT with a Mode S All Call UF11 AA FFFFFF 6 dB above MTL verifying DF11 replies a...

Page 71: ...1 d B S L S O N N O R E P L Y O F F R E P L Y S Q T R D F 1 1 P E R IO D 1 0 0 s D F 1 7 D E T E C T E D Y E S R E P L Y R AT IO 1 0 0 R E P L Y R AT IO 8 1 d B m 0 I N V AL I D A A P A S S D I V E R...

Page 72: ...by an arrow DF17 Detected The Test Set monitors the UUT DF17 extended squitters and confirms detection by displaying YES Test displays NO if DF17 s are not detected Invalid AA The Test Set interrogate...

Page 73: ...ayed If test fails due to wrong address DF11 address is displayed UF0 AQ bit is 1 for requesting airspeed information in DF0 RI field NOTE AC field blanks out if invalid data is received for that fiel...

Page 74: ...orted during Mode Test Testing FS Flight Status ICAO amendment 77 transponders only reply to Mode S discrete interrogations when installation is in ground state Refer to para 1 2 4 3 2 for UUT ADDRESS...

Page 75: ...3 5 5 5 6 5 8 5 9 6 1 6 2 R U N T E S T M O R E I N F O P R E V T E S T X P D R U F 1 1 N E X T T E S T R E T U R N F AIL B AT 2 5 H r D F 1 6 V S 0 IN A I R S L 0 R I 0 N O O N B O A R D T C A S M V...

Page 76: ...ode S altitude to Mode C altitude The Test Set interrogates with UF20 Comm A altitude request RR 17 long reply DI 7 RRS 0 requesting a BDS 1 0 data link capability report 6 dB above MTL verifying a DF...

Page 77: ...data link capability report 6 dB above MTL verifying a DF21 reply is received If reply is not received test interrogates for BDS 3 0 TCAS sensitivity status message ID code reported in DF21 is compare...

Page 78: ...eport determines the level of transponder under test If level 3 is reported test is not run and NOT CAPABLE is displayed B AT 2 5 H r R U N T E S T P R E V T E S T X P D R E L E M E N T S U R V 1 N E...

Page 79: ...E ME N T S U R V 2 N E X T T E S T B D S 1 7 0 5 0 6 0 7 0 8 0 9 0 A 2 0 2 1 4 0 4 1 4 2 4 3 4 4 4 5 4 8 5 0 5 1 5 2 5 3 5 4 5 5 5 6 5 F 6 0 B D S 1 8 0 0 0 0 0 0 0 0 0 0 0 0 0 0 B D S 1 9 0 0 0 0 0 0...

Page 80: ...8 Specific Services GICB Capability Report BDS 1 9 BDS 1 9 Interrogates with UF4 RR 17 DI 7 and RRS 9 DF20 reply BDS register content displayed as 14 HEX digits Each bit set indicates capability supp...

Page 81: ...ers the ADS B option is required NOTE BDS Data Items not available are identified by displaying N A in the data field NOTE If Check Cap is enabled BDS 1 7 is verified to confirm availability of BDS 4...

Page 82: ...C 4 C 2 C 1 D 4 D 2 R U N T E S T S E L E C T S O U R C E Altitude Encoder Altitude Encoder performs these functions Decodes and displays altitude in feet and binary code grey code from encoding altim...

Page 83: ...ft Key 4 3 6 DIRECT CONNECT PROCEDURE STEP PROCEDURE 1 Connect long RF coaxial cable between the aircraft antenna feeder cable and Test Set RF I O Connector 2 Power On Aircraft and configure aircraft...

Page 84: ...ot completely depressed against the aircraft but the Test Set will not measure functions accurately 2 Connect long RF coaxial cable between the Antenna Coupler and Test Set RF I O Connector 3 Power On...

Page 85: ...borne TCAS equipped aircraft do not detect UUT at altitude causing false RA s and TA s The 20 dB isolation of the antenna shield may cause various tests to fail which is normal 4 3 9 OVER THE AIR SIMU...

Page 86: ...ich is 63 MHz apart from the beacon s channel The interval between the interrogation transmission and the reply reception provides the aircraft with the slant range from the ground station This inform...

Page 87: ...r for approximately 60us after accepting the direct path interrogation thereby ignoring the echo interrogation In the DME interrogator a different method is employed to provide echo protection for ref...

Page 88: ...thout the large antennas or site errors characteristic of the civil very high frequency omnidirectional range VOR with a bearing accuracy of 1 As in DME operation is on 252 channels spaced 1 MHz apart...

Page 89: ...der is approximately 33 in 84 cm in diameter and contains nine parasitic elements which impart a 135 Hz amplitude modulation peak at every 40 degrees On the same rotating shaft reference pulse generat...

Page 90: ...OPERATION MANUAL IFR 6015 1 2 4 Subject to Export Control see Cover Page for details Page 39 Oct 1 16 Composite TACAN Beacon Signal Figure 11...

Page 91: ...hase of the amplitude modulation of the received signal varies In the airborne receiver the 15Hz and 135Hz sine waves are detected filtered and compared with the decoded reference bursts to provide a...

Page 92: ...t Control see Cover Page for details Page 41 Oct 1 16 Reference Groups The MRB consists of 12 pairs of 3 5us width pulses spaced at 12us and 30us between pulse pairs The ARB s consist of 13 single pul...

Page 93: ...RN 84 V TACAN Control Panel Figure 14 Air to Air Tacan Interrogators such as the Rockwell Collins AN ARN 118 has the following capabilities Normal REC Receive Ident tone and bearing from ground TACAN...

Page 94: ...es The directional 15Hz cardioid pattern is used to determine angle of arrival by finding the peak amplitude of the received squitter Transmit 15Hz MRB and Squitter pulses Inverse T R Receive Ident to...

Page 95: ...ULSES A A INTERROGATION PULSE PAIRS 150Hz INTERROGATIONS PULSE PAIRS A A RANGE REPLIES SINGLE PULSE A A X BEACON A A Y BEACON RANGE REPLIES SINGLE PULSE 1350Hz SQUITTER 1350Hz IDENT EQUALIZER PULSES 1...

Page 96: ...RM 2 P ul s e R ng Re pl y 2 70 0 Hz S Q TR 1 35 0 Hz I DEN T 1 5H z 1 35 Hz MRB ARB s UU T Di s pl a y TAC AN Mode N O RM AL T R REC 2 P ul s e I nterr Com pos i te Si gnal 2 P ul s e R ng Re pl y SQ...

Page 97: ...5Hz MRB Display Range Bearing REC Mode Bearing Only B A T 2 5 H r BR G 2 7 0 0 de g ID E N T M OR S E TX FR EQ 1 04 1 0 0 M H Z ER P 25 0 W A TTS PR F 1 50 H z A A R EP LY D ELA Y 6 2 0 00 us P1 W ID...

Page 98: ...IDE NT TA C A N A A R N G O NL Y STO P RAT E C H A N 17 X R F LV L 4 2 0 dB m FR E Q 1 1 04 MH z R A TE 10 0 0 kt s IN RANGE 100 00 nm IN OUT Direct Connect or Radiated 6015 Mode A A RNG Only 1Pulse...

Page 99: ...lect fixed BRG values 90 230 320 degrees In TEST MODE 5 VARIABLE Bearing may selected 0 to 359 deg in 0 5 deg steps using Up Down data slew keys IDENT 1350Hz Morse Ident selectable MORSE TONE OFF Four...

Page 100: ...alues 0kts In TEST MODE 3 AN ARM 184 RANGE Keys select fixed RANGE values 0 2400kts In TEST MODE 4 2650 2655 RANGE Keys select fixed RANGE values 0kts In TEST MODE 5 VARIABLE RATE keys increment or de...

Page 101: ...OR Selects ANTENNA ANT CONNECTOR or DIRECT CONNECT via RF I O Connector or DIR W COUPLER ANT CABLE LEN or DIR CABLE LEN or CPL CABLE LEN Selections 1 to 75 FT STEP PROCEDURE ANT CABLE LOSS or DIR CABL...

Page 102: ...is AERO TEST MODE Selects test mode for Range Range Rate and Bearing parameters Mode selections are 1 DoD 2 AN ASM 663 3 AN ARM 184 4 2650 2655 5 VARIABLE When the Test Mode VARIABLE is selected Repl...

Page 103: ...lay The IFR 6015 is used with the directional antenna attached allowing the user to move the test set to different locations and headings from the Aircraft UUT 4 5 1 TCAS OPERATION CONCEPT TCAS is a s...

Page 104: ...e Threshold ft TA RA TA RA TA RA ALIM 1000 2 20 N A 0 30 N A 850 N A 1000 2350 3 25 15 0 33 0 20 850 300 2350 5000 4 30 20 0 48 0 35 850 300 5000 10 000 5 40 25 0 75 0 55 850 350 10 000 20 000 6 45 30...

Page 105: ...intruding aircraft is considered to be potentially hazardous Depending on altitude TCAS II displays a TA when the time to CPA is between 20 and 48 sec Resolution Advisory A solid red square indicates...

Page 106: ...and transponder Mode S address Reply Parameters Screen allows control over Mode S DF0 DF11 and DF16 field content 4 5 3 SETUP SETUP TCAS SCREEN SETUP TCAS Screen contains parameters which determine o...

Page 107: ...UNITS parameter determines feet or meters STEP PROCEDURE STEP PROCEDURE ANT HEIGHT Test Set Antenna to TCAS antenna height difference 1 to 99 ft or 0 5 to 30 0 m NOTE UNITS parameter determines feet...

Page 108: ...owing displayed Downlink Format DF fields and subfields All fields are displayed in hexadecimal Unless otherwise specified both single and continuous SLEW key depressions change values by 1 USER CONTR...

Page 109: ...d 600 kts D 600 kts and 1200 kts E 1200 kts RI Field Acquisition Valid Data Table 8 Rlt Enter air to air Reply Information for a tracking report The RIt field contains TCAS capability data The field c...

Page 110: ...to 30 for coordination reply messages default value The test set transmits the VDS field in DF16 part of MV field CLI Enter Coordination Lock Indicator 0 is Off 1 is On The test set transmits the CLI...

Page 111: ...E Q 1 0 3 0 0 0 0 MH z E R P 5 7 0 d B m R A N G E 2 1 0 0 n m I N A L T 1 0 0 0 f t T C A S S T AT U S T R A C K I N G S T AT U S N O N T H R E AT E N C O U N T E R 0 0 0 R U N T E S T P R E V P A R...

Page 112: ...cenarios STEP PROCEDURE 1 Refer to para 1 2 4 7 for Directional Antenna use and setup procedure 2 Press TCAS Mode Key to display TCAS Test Screen 3 Set following parameters by pressing NEXT PARAM and...

Page 113: ...Range is 0 to 10000 fpm CONVERGE When converge is ON altitude rate is automatically calculated to achieve collision at 0 nm and 0 ft relative to UUT Range STOP and Alt STOP fields are blanked when con...

Page 114: ...TCAS Screen or SETUP TCAS Screen by pressing the STORE RECALL Soft Key The Setup Scenario Screen allows the recall of nine factory predetermined scenarios and the Storage and Recall of up to 16 user...

Page 115: ...pecific scenario use the Data Select Keys to select a specific scenario Press the RECALL Soft Key RETURN Press the RETURN Soft Key to display the previous screen NOTE Scenarios are also selected by us...

Page 116: ...y displayed in E TCAS mode STEP PROCEDURE 1 Connect UUT to IFR 6015 RF I O Connector or IFR 6015 Directional Antenna facing towards UUT Antenna to Antenna Connector 2 Perform the Setup Procedure para...

Page 117: ...VC Field Display Data Table 14 VRC The Vertical Resolution Advisory Complement is received in UF16 part of MU field 1 2 4 Table 15 VRC FIELD DEFINITION 0 No complement sent 1 Don t descend 2 Don t cli...

Page 118: ...ogator STEP PROCEDURE PC Refer to 1 2 4 Table 19 for the Protocol field received in UF4 UF5 UF20 and UF21 to verify operating commands sent to the transponder INPUT DATA DEFINITION 0 No changes in tra...

Page 119: ...the aircraft i e TCAS sensitivity level setting STEP PROCEDURE INTERVAL The IFR 6015 displays time from the start of one interrogation to the start of the next interrogation The IFR 6015 looks for the...

Page 120: ...rently active If set to 1 the RA indicated by the ARA subfield has been terminated The one is set for 18 sec 1 sec ARA The ARA field indicates all current Active Resolution Advisories being transmitte...

Page 121: ...of the reporting aircraft INTERVAL The INTERVAL field displays the time interval in seconds between the latest two TCAS Broadcast Messages received nominally 10 sec for each interrogator STEP PROCEDUR...

Page 122: ...g the Whisper Shout Monitor screen Default value is restored upon exit from the screen STEP PROCEDURE 6 Press RUN Soft Key to initiate Monitor mode The IFR 6015 displays latest whisper shout sequence...

Page 123: ...terrogations received in latest sequence W S SEQUENCE INTERVAL The IFR 6015 displays time from the start of one whisper shout sequence to the start of the next whisper shout sequence The IFR 6015 look...

Page 124: ...ACCURACY 7 Press RUN Soft Key to initiate test operation 8 Verify UUT visual and audio operation Verify Traffic Advisory at 40 sec until encounter time Verify Resolution Advisory at 25 sec until encou...

Page 125: ...initiate test operation 32 Verify TCAS bearing is correct 15 33 Press STOP Soft Key to terminate test operation 34 Reposition Test Set to a Z Test Location Stay at same distance from UUT as establish...

Page 126: ...rcraft the IFR 6015 Mode A code is compared with codes stored in a pilot entered list and if identified the E TCAS display flashes the displayed code The E TCAS symbology differs from TCAS II as follo...

Page 127: ...eral seconds apart In contrast a system using ADS B creates and listens for periodic position and intent reports from aircraft These reports are generated and distributed using precise instruments suc...

Page 128: ...DF17 or DF18 GICB Select DF20 or DF21 for GICB BDS transfer 4 Press the RETURN softkey to display the previous screen SETUP TEST DATA The SETUP ADS B Screen allows storage and recall of all SETUP ADS...

Page 129: ...layed 4 6 3 ADS B GICB MAIN Press the XPDR mode key twice to display the ADS B GICB Main Menu B AT 2 5 H r A D S B M O N G I C B A D S B G I C B M A I N A D S B G E N A D V C I R C Press the ADS B MON...

Page 130: ...om subsystem NOTE Installation must be in the airborne state to transmit airborne position AA Aircraft Address in HEX and OCTAL COUNT Indications Displays total squitters received since test was run r...

Page 131: ...es and displays surface position NOTE Installation must be in the ground state to transmit surface position AA Aircraft Address in HEX and OCTAL COUNT Indications Displays total squitters received sin...

Page 132: ...0 2 NM 370 4 m NIC 7 1 0 Rc 0 3 NM 555 6 m NIC 6 0 1 Rc 0 6 NM 1111 2 m 0 0 Rc 0 1 NM 1111 2 m or unknown NIC 0 9 Not Present 0 0 Airborne Position Message Rc 7 5 m NIC 11 10 0 0 Rc 25 m NIC 10 11 1 1...

Page 133: ...704 km h 2 kt 0 436 km h 0 25 kt steps 13 38 3 704 km h 2 kt Ground Speed 27 78 km h 15 kt 0 926 km h 0 50 kt steps 39 93 27 78 km h 15 kt Ground Speed 129 64 km h 70 kt 1 852 km h 1 00 kt steps 94 10...

Page 134: ...on meters 0 0 0 LEFT NO DATA 0 1 2 1 0 4 1 1 6 1 0 0 RIGHT 0 0 1 2 1 0 4 1 1 6 Lateral Axis GPS Antenna Offset Encoding Table 19 Longitudinal Axis GPS Antenna Offset Encoding ME Bit Message Bit Upper...

Page 135: ...ategory NOTE ADLP Air Data Link Processor must be installed or transponder must have embedded ADLP to receive data from subsystem AA Aircraft Address in HEX and OCTAL COUNT Indications Displays total...

Page 136: ...t was run ME message field displayed in 14 digit HEX format PERIOD Indications Displays DF17 18 squitter period in seconds NOTE ADLP Air Data Link Processor must be installed or transponder must have...

Page 137: ...which BDS register is being displayed followed by its description 0 A Extended Squitter Event Driven Register TYPE Specifies class and accuracy of data Refer to table A 2 RTCA DO 260B NOTE Refer to I...

Page 138: ...I Part 1 Chapter 5 and RTCA DO 260 DO 260A and DO 260B for detailed description of data fields DF17 18 Receives extended squitter decodes and displays Aircraft Status NOTE ADLP Air Data Link Processor...

Page 139: ...X format PERIOD Indications Displays DF17 18 squitter period in seconds TTI Threat Type Indicator DO 260B only Indications 0 No identity data in TID 1 TID contains a Mode S transponder address 2 TID c...

Page 140: ...ft Address in HEX and OCTAL COUNT Indications Displays total squitters received since test was run ME message field displayed in 14 digit HEX format PERIOD Indications Displays DF17 18 squitter period...

Page 141: ...RAFT 7 RESERVED ADS B MON BDS 6 2 ST1 A V A I L B AT 2 5 H r B D S 6 2 T S S S U B T Y P E 1 T Y P E 2 9 D F 1 7 A A 3 A C 4 2 1 1 6 5 4 2 0 4 1 C O U N T 1 0 0 0 M E 0 0 0 0 0 0 0 0 0 0 0 0 0 0 P E R...

Page 142: ...CP Status of MCP FCU DO 260B only Indications 0 No Mode Information is being provided in ME bits 48 49 50 or 52 Message bits 80 81 82 or 84 1 Mode Information is deliberately being provided in ME bits...

Page 143: ...er to RTCA DO 260A Appendix A section A 1 8 Figure A 10 replaces BDS 6 3 with BDS 6 5 Both BDS 6 3 and 6 5 are supported and data displayed is identical COUNT Indications Displays total squitters rece...

Page 144: ...AS RA Active Indications 0 TCAS II or ACAS resolution advisory inactive 1 TCAS II or ACAS resolution advisory active ID Ident Switch Indications YES Ident active NO Ident not active HRZ REF Horizontal...

Page 145: ...N T E S T P R E V T E S T MO N B D S 6 5 S U R P R E V T E S T R E T U R N BDS Indicates which BDS register is being displayed followed by its description 6 5 Aircraft Operational Status Surface Subt...

Page 146: ...ENT Switch Active Receiving ATC Services 1 Reserved 2 Reserved 3 Reserved SDA System Design Assurance Data DO 260B only Indications 0 Unknown or No Safety Effect 1 Minor 2 Major 3 Hazardous SAF Single...

Page 147: ...EPU 7 408 km 4NM 3 EPU 3 704 km 2NM 4 EPU 1852 m 1NM 5 EPU 926 m 0 5NM 6 EPU 555 6 m 0 3NM 7 EPU 185 2 m 0 1NM 8 EPU 92 6 m 0 05NM 9 EPU 30 m 0 016NM 10 EPU 10 m 0 0054NM 11 EPU 3 m 0 0016NM 12 Reser...

Page 148: ...t s N A D S B B AR O AL T 2 0 0 0 0 f t X P D R B A R O A L T 2 0 1 0 0 f t AL T IT U D E E R R O R 1 0 0 f t G E O M E T R I C AL T 2 0 2 2 5 f t R U N T E S T A D V C I R C 2 0 1 6 5 A I R N E X T P...

Page 149: ...Unambiguous Longitude decoded using Local algorithm or Compact Position Reporting CPR algorithm depending on Position setting NACP Indications 0 EPU 18 52 km 1 EPU 18 52 km 2 EPU 7 408 km 3 EPU 3 704...

Page 150: ...sory active MODE 3 A CODE DO 260B only 4 digit OCTAL field Indications 0000 to 7777 IDENT Ident Switch Indications YES Ident active NO Ident not active EMERG PRIOR CODE Indications 0 NO EMERGENCY 1 GE...

Page 151: ...n in ADSB Setup for gross position discrepancy NIC is derived from the combination of NIC Supplement A and NIC Supplement C of BDS 6 5 BDS 0 8 Extended Squitter Identification and Category is monitore...

Page 152: ...o Safety Effect 1 Minor 2 Major 3 Hazardous RA ACTIVE TCAS RA Active Indications 0 TCAS II or ACAS resolution advisory inactive 1 TCAS II or ACAS resolution advisory active LEN WIDTH Aircraft Length a...

Page 153: ...s either via the Antenna port or RF I O port The squitters are encoded via data entered in individual data screens B AT 2 5 H r 1 0 5 A I R B O R N E P O S E N A B L E D 2 0 6 S U R F AC E P O S E N A...

Page 154: ...orithm depending on Position setting LONG Encoded Longitude Indications Unambiguous Longitude decoded using Local algorithm or Compact Position Reporting CPR algorithm depending on Position setting PO...

Page 155: ...urface position NOTE Installation must be in the ground state to transmit surface position AA Aircraft Address in HEX and OCTAL COUNT Indications Displays total squitters sent since test was run ME me...

Page 156: ...DLP Air Data Link Processor must be installed or transponder must have embedded ADLP to receive data from subsystem AA Aircraft Address in HEX and OCTAL COUNT Indications Displays total squitters sent...

Page 157: ...data from subsystem NOTE Installation must be in the airborne state to transmit airborne velocity AA Aircraft Address in HEX and OCTAL COUNT Indications Displays total squitters sent since test was r...

Page 158: ...T U R N BDS Indicates which BDS register is being displayed followed by its description 0 A Extended Squitter Event Driven Register TYPE Specifies class and accuracy of data Refer to table A 2 RTCA D...

Page 159: ...nnex 10 Vol lII Part 1 Chapter 5 and RTCA DO 260 DO 260A and DO 260B for detailed description of data fields DF17 18 Sends extended squitter for Aircraft Status NOTE ADLP Air Data Link Processor must...

Page 160: ...as run ME message field displayed in 14 digit HEX format PERIOD Indications Displays DF17 18 squitter period in seconds TTI Threat Type Indicator Indications 0 No identity data in TID 1 TID contains a...

Page 161: ...Installation must be in the airborne state to transmit target state and status AA Aircraft Address in HEX and OCTAL COUNT Indications Displays total squitters sent since test was run ME message field...

Page 162: ...FT 7 RESERVED ADS B GEN BDS 6 2 ST1 A V A I L B AT 2 5 H r B D S 6 2 T S S S U B T Y P E 1 T Y P E 2 9 D F 1 7 A A 3 A C 4 2 1 1 6 5 4 2 0 4 1 C O U N T 1 0 0 0 M E 0 0 0 0 0 0 0 0 0 0 0 0 0 0 P E R I...

Page 163: ...tion Engaged Indications 0 VNAV Mode is NOT Active or Unknown 1 VNAV Mode is Active MCP Status of MCP FCU Indications 0 No Mode Information is being provided in ME bits 48 49 50 or 52 Message bits 80...

Page 164: ...format PERIOD Indications Displays DF17 18 squitter period in seconds NOTE ADLP Air Data Link Processor must be installed or transponder must have embedded ADLP to receive data from subsystem SUBTYPE...

Page 165: ...Ident not active HRZ REF Horizontal Reference Direction Indications TRUE NORTH MAG NORTH Magnetic North NIC A Navigation Integrity Category Supplement A Indications DO 260A only 0 Rc unknown 1 Rc 20 N...

Page 166: ...ted and data displayed is identical COUNT Indications Displays total squitters sent since test was run ME message field displayed in 14 digit HEX format PERIOD Indications Displays DF17 18 squitter pe...

Page 167: ...r surface ADS B participants surface position message heading or ground track determination bit Indications N A Airborne 0 Target Heading Reported 1 Track Angle Reported SIL SUP SIL Supplement Indicat...

Page 168: ...E A V A I L B AT 2 5 H r 1 3 1 D MS P C A P R P T 1 2 8 A V A IL 1 4 1 E M S P C A P R P T 2 9 5 6 AV A I L 1 5 1 F M S P C A P R P T 5 7 6 3 AV A I L 1 6 2 0 F L I G H T I D AT AV A I L 1 7 2 1 A I...

Page 169: ...IPTIONS GICB BDS 0 5 A V A I L B AT 2 5 H r B D S 0 5 A I R B O R N E P O S T Y P E 1 4 D F 2 0 A A 3 A C 4 2 1 1 6 5 4 2 0 4 1 MB 0 0 0 0 0 0 0 0 0 0 0 0 0 0 L AT 3 7 3 9 0 N L O N G 9 7 2 5 4 8 W P...

Page 170: ...0 N L O N G 9 7 2 5 4 8 W MO V ME N T 2 k t s T N U T C H D G 2 3 0 d e g P O S G L O B A L N I C 7 R c 0 2 n m 3 7 0 4 m R U N T E S T P R E V T E S T G I C B B D S 0 6 N E X T T E S T R E T U R N U...

Page 171: ...1 1 6 5 4 2 0 4 1 MB 0 0 0 0 0 0 0 0 0 0 0 0 0 S U R F A C E S Q T R T R A N S R AT E H IG H AL T T Y P E B A R O E S S 0 0 0 0 0 0 0 0 0 0 0 0 0 0 R U N T E S T P R E V T E S T G I C B B D S 0 7 A V...

Page 172: ...ink Processor must be installed or transponder must have embedded ADLP to receive data from subsystem AA Aircraft Address in HEX and OCTAL MB message field displayed in 14 digit HEX format EMIT CAT SE...

Page 173: ...ing NOTE ICAO DOC 9688 First edition of ICAO Mode S Specific Service manual not supported Indications 0 NOT ASSIGNED 1 VEL OVR GND NORM Velocity Over Ground Normal 2 VEL OVER GND SUPER Velocity Over G...

Page 174: ...BNET VER NBR Indications 0 127 SI CAP Indications YES surveillance identifier code capability NO no surveillance identifier code capability CONT FLAG Indications YES a continuation report may be found...

Page 175: ...V T E S T G I C B B D S 1 A P R E V T E S T R E T U R N GICB BDS 1 8 1 C A V A I L B AT 2 5 H r B D S 1 B S P E C IF IC S E R V 4 D F 2 0 A A 3 A C 4 2 1 1 6 5 4 2 0 4 1 MB F F F F F F F F F F F F F...

Page 176: ...E V T E S T R E T U R N A V A I L B AT 2 5 H r B D S 1 F M S P C A P R P T 5 7 6 3 D F 2 0 A A 3 A C 4 2 1 1 6 5 4 2 0 4 1 MB F F F F F F F F F F F F F F U P L I N K 5 7 5 8 5 9 6 0 6 1 6 2 6 3 D O W...

Page 177: ...A Aircraft Address in HEX and OCTAL MB message field displayed in 14 digit HEX format Flight Id is seven characters GICB BDS 2 1 A V A I L B AT 2 5 H r B D S 2 1 A I R C R AF T R E G D F 2 0 A A 3 A C...

Page 178: ...ompliment bit 55 58 displayed in binary RAT RA Terminated indicator bit 59 displayed in binary Note Normally 0 until an RA is terminated then will be 1 for 18 seconds TIDA Threat Identity Data Altitud...

Page 179: ...format NOTE ADLP Air Data Link Processor must be installed or transponder must have embedded ADLP to receive data from subsystem MCP FCU SEL ALT Mode Control Panel Flight Control Unit Selected Altitud...

Page 180: ...52 for detailed description of data fields GICB BDS 4 2 A V A I L B AT 2 5 H r B D S 4 2 W A Y P O IN T P O S D F 2 0 A A 3 A C 4 2 1 1 6 5 4 2 0 4 1 MB 0 0 0 0 0 0 0 0 0 0 0 0 0 0 L AT IT U D E 3 2 5...

Page 181: ...ed description of data fields GICB BDS 5 0 B AT 2 5 H r B D S 5 0 T R AC K T U R N D F 2 0 A A 3 A C 4 2 1 1 6 5 4 2 0 4 1 MB 0 0 0 0 0 0 0 0 0 0 0 0 0 0 R O L L AN G L E 4 0 1 d e g G N D S P E E D 5...

Page 182: ...ons N A Not Available 16384 to 16352 ft minute resolution 32 ft min NOTE Refer to ICAO manual on Mode S specific services DOC 9688 AN 952 and RTCA DO 260A V2 for detailed description of data fields GI...

Page 183: ...icator Indications 0 No identity data in TID 1 TID contains a Mode S transponder address 2 TID contains altitude range and bearing data 3 Not assigned TIDA Threat Identity Data Altitude Indications Mo...

Page 184: ...on must be in the airborne state to transmit target state and status NOTE Autopilot must be engaged and stimulated by sensor data for some fields to display data AA Aircraft Address in HEX and OCTAL M...

Page 185: ...Y P E 1 S IL 0 S IL S U P 1 N A C 0 L N AV 0 V N A V 1 MC P 1 A U T O P 1 A H M E 1 A P M O D E 1 T C AS O P N O S E L E C T E D AL T IT U D E 2 1 7 9 2 f t T Y P E 1 B A R O P R E S S U R E 8 4 3 2 m...

Page 186: ...age bits 80 81 82 or 84 AUTO P Autopilot Engaged Indications 0 Autopilot is NOT Engaged or Unknown e g not actively coupled and flying the aircraft 1 Autopilot is Engaged e g actively coupled and flyi...

Page 187: ...7 RESERVED VERSION MOPS Version Number Indications 0 DO 260 1 DO 260A 2 DO 260B CC FMT Capability Class ME BITS 9 24 airborne ME BITS 9 20 surface 0000 FFFF airborne 000 FFF surface ARV Air Reference...

Page 188: ...nknown 1 Rc 20 NM DO 260B only Refer to Table 17 BAQ Barometric Altitude Quality DO 260A GVA Geometric Vertical Accuracy DO 260B Indications 0 Unknown or 150 m 1 150 m 2 45 m 3 Reserved NIC BARO Navig...

Page 189: ...er must have embedded ADLP to receive data from subsystem SUBTYPE Indications 0 AIR Airborne Status message 1 SUR Surface Status message 2 RESERVED 3 RESERVED 4 RESERVED 5 RESERVED 6 RESERVED 7 RESERV...

Page 190: ...eported 1 Track Angle Reported SIL SUP SIL Supplement Indications 0 Unknown 1 1x10 3 per flight 2 1x10 5 per flight 3 1x10 7 per flight SIL Surveillance Integrity Level Indications 0 Unknown 1 1x10 3...

Page 191: ...ons currently provide 60 nautical mile coverage including a 5 mile buffer required for TIS coverage A Mode S equipped aircraft requests TIS data via a downlink message at 1090 MHz The ground station s...

Page 192: ...able loss range 0 0 to 20 9 dB ANT RANGE Test Set Antenna to transponder antenna horizontal range 6 to 250 Enter parameters for BOTTOM and TOP antenna if installation has diversity capability NOTE UNI...

Page 193: ...3500 ft ALT RATE Sets Altitude Rate annunciation on TIS display indications CLIMB LEVEL DESCEND UNUSED HDG Sets target Heading TRAFFIC Sets target traffic status on TIS display PROX Proximity TRFC Tra...

Page 194: ...OPERATION MANUAL IFR 6015 1 2 4 Subject to Export Control see Cover Page for details Page 143 Oct 1 16 TIS Operation Flow Chart Figure 25...

Page 195: ...T Connector via 72 in coaxial cable Mount Directional Antenna on tripod and point at UUT antenna XPDR XPDR antennas are top and bottom mounted on airframe Verify which antenna s istransponder antenna...

Page 196: ...oser than 6 feet to ensure that the antenna far field is tested TCAS Most TCAS installations have top and bottom directional antennas Some aircraft are fitted with an omni directional bottom antenna F...

Page 197: ...OPERATION MANUAL IFR 6015 1 2 4 Subject to Export Control see Cover Page for details Page 146 Oct 1 16 Suggested Layout to Reduce Multipath Errors Figure 26...

Page 198: ...OPERATION MANUAL IFR 6015 1 2 4 Subject to Export Control see Cover Page for details Page 147 Oct 1 16 Ramp Testing Figure 27...

Page 199: ...rol see Cover Page for details Page 148 Oct 1 16 4 8 BREAKOUT BOX The Breakout Box accessory provides access to individual user interfaces via standard connectors The Test Set REMOTE Connector provide...

Page 200: ...89Y Preset 3 1 to 126 X or Y Preset 4 18X 18Y 47X 47Y 100X 100Y 123X 123Y Accuracy 10 kHz Output Level Antenna Port Range T R Norm T R Inverse A A Beacon A A Inverse 67 to 5 dBm at Antenna port T R RN...

Page 201: ...l Fixed Reply Delay 62 s 100 ns A A Y Channel Fixed Reply Delay 74 s 100 ns Range Delay X and Y Channel Range Variable Mode 0 to 450 00 nmi Preset 1 0 3 10 30 100 200 300 400 nmi Preset 2 0 10 150 297...

Page 202: ...e or Selectable four letter code Frequency 1350 Hz Accuracy 2 Hz Equalizer pulse pair position 100 s 10 s from Ident pair A A X and A A Y Pulse Spacing Single pulse Selection Tone or Selectable four l...

Page 203: ...e Spacing A A X or Y 30 s 0 1 s ARB T R X Group 6 pulse pairs Pulse Spacing 12 s 0 1 s Pulse Pair Spacing 24 s 0 1 s T R Y Group 13 single pulses Pulse Spacing 15 s 0 1 s 15 135 Hz Modulation Modulati...

Page 204: ...1025 00 to 1150 00 MHz Resolution 10 kHz Accuracy 20 kHz Interrogation Pulse Width P1 and P2 Pulse W idths Range 2 00 to 5 00 s Resolution 1 ns Accuracy 50 ns Interrogation Pulse Spacing P1 to P2 Spa...

Page 205: ...5 dB Accuracy 2 dB Distance to UUT Antenna 6 to 200 ft with supplied antenna RF I O Connector MTL 6 dB typical automatically controlled Range 115 to 47 dBm Resolution 0 5 dB Accuracy 95 to 47 dBm 1 dB...

Page 206: ...ns Mode S P6 Short DPSK Block 16 25 s 50 ns P6 Long DPSK Block 30 25 s 50 ns P5 0 80 s 50 ns Intermode P4 Short 0 80 s 50 ns P4 Long 1 60 s 50 ns Interrogation Pulse Rise and Fall Times All Modes Rise...

Page 207: ...000 MHz Resolution 10 kHz Accuracy 50 kHz Receiver Sensitivity Radiated MTL Range 67 to 79 dBm into 0 dBi antenna Resolution 0 1 dB Accuracy 2 dB typical Receiver Sensitivity Direct Connection MTL Ran...

Page 208: ...ccuracy 20 ns Pulse Widths F1 and F2 Range 0 25 to 0 75 s Resolution 1 ns Accuracy 20 ns Mode S Preamble Range 0 25 to 0 75 s Resolution 1 ns Accuracy 20 ns Pulse Amplitude Variation Range Mode S Rela...

Page 209: ...ft with supplied antenna RF I O Connector Automatic mode 68 dBm at 10 nmi range automatically controlled Manual Mode Range 115 to 47 dBm Resolution 0 5 dB Accuracy 95 to 47 dBm 1 dB 115 to 95 dBm 2 dB...

Page 210: ...plitudes ATCRBS 1 dB relative to F1 Mode S 1 dB relative to P1 Reply Pulse Rise and Fall Times All Modes Rise Time 50 to 100 ns Fall Time 50 to 200 ns Percent Reply Range 0 to 100 Resolution 10 Accura...

Page 211: ...0 us Mode S P1 to P2 2 0 us Accepts 200 ns Rejects 10 Replies 1 0 us P1 to SPR 4 75 us Accepts 200 ns Rejects 10 Replies 1 5 us Suppresion ATCRBS P2 or S1 0 5dB above level of P1 10 Replies ERP at 10...

Page 212: ...e for details Page 13 Oct 1 16 TCAS MODE UUT MEASUREMENTS cont Direct Connection Peak Pulse Power at 1030 MHz cont Frequency Range 1029 900 to 1030 100 MHz Resolution 1 kHz Accuracy 10 kHz TCAS Broadc...

Page 213: ...50 typical Maximum Input Level 10 W peak 1 2 W average VSWR 1 7 1 Video Type Output Impedance 50 typical Generate Video Level 0 2 to 1 5 Vpp into 50 1030 MHz at 67dBm Receive Video Level Proportional...

Page 214: ...ions 10 of the nominal voltage Transient Overvoltages According to Installation Category II Environmental Test Set Use Pollution Degree 2 Altitude 4800 m Operating Temperature 20 C to 55 C N OTE 2 Sto...

Page 215: ...lass 2 Temperature Operating MIL PRF 28800F Class 2 N OTE 4 Temp Non Operating MIL PRF 28800F Class 2 NOT E 5 Transit Drop MIL PRF 28800F Class 2 Safety Compliance UL 61010B 1 EN 61010 1 CSA 22 2 No 6...

Page 216: ...1 SLS level is automatically controlled in the SLS LEVEL test NOTE 2 Battery charging temperature range is 5 to 40 C controlled by internal charger NOTE 3 Li Ion Battery must be removed below 20 C an...

Page 217: ...OPERATION MANUAL IFR 6015 1 3 1 Subject to Export Control see Cover Page for details Page 18 Oct 1 16 THIS PAGE INTENTIONALLY LEFT BLANK...

Page 218: ...or repair required Model Number Serial Number Shipping Containers Test Sets must be repackaged in original shipping containers using Aeroflex packing molds If original shipping containers and material...

Page 219: ...Set with polyethylene sheeting to protect finish Place Test Set into shipping container making sure Test Set is securely seated in bottom packing mold Place top packing mold over top of Test Set and...

Page 220: ...whenever the Test Set is stored for extended periods Disconnect Test Set from any electrical power source Disconnect the wire harness connecting the battery to the Test Set and remove the battery Ref...

Page 221: ...OPERATION MANUAL IFR 6015 1 5 1 Subject to Export Control see Cover Page for details Page 2 Oct 1 16 THIS PAGE INTENTIONALLY LEFT BLANK...

Page 222: ...TYPE SIGNAL TYPE INPUT OUTPUT SYNC BNC TTL OUTPUT VIDEO BNC TTL OUTPUT DC POWER 2 5 mm CIRCULAR 2 5 mm center 5 5 mm outer diameter center positive 11 to 32 Vdc INPUT RF I O TNC RF 30 W CW MAX INPUT...

Page 223: ...put 8 A4 Input Altitude Encode Input 9 C2 Input Altitude Encode Input 10 C4 Input Altitude Encode Input 11 GND Ground System Ground 12 REM_IN1 Input General Purpose Input 13 REM_OUT2 Output General Pu...

Page 224: ...1 VBUS_DN1 Supply 5V supply for USB device port 32 VBUS_DN1 Supply 5V supply for USB device port 33 VBUS_UP Supply 5V supply input from USB host 34 GND_UP Ground Ground for USB host port 35 GND Ground...

Page 225: ...OPERATION MANUAL IFR 6015 APPENDIX A Subject to Export Control see Cover Page for details Page 4 Oct 1 16 THIS PAGE INTENTIONALLY LEFT BLANK...

Page 226: ...sec knots 0 5921 miles feet 5280 ft sec miles hr 0 6818 miles km 1 609 ft sec 2 cm sec 2 30 48 miles meters 1609 ft sec 2 m sec 2 0 3048 miles nmi 0 8684 grams ounces 0 03527 miles hr ft sec 1 467 in...

Page 227: ...OPERATION MANUAL IFR 6015 APPENDIX B Subject to Export Control see Cover Page for details Page 2 Oct 1 16 THIS PAGE INTENTIONALLY LEFT BLANK...

Page 228: ...OPERATION RS 232 Last Used Setup XPDR Screen FIELD F ACTORY POWER UP ANTENNA SELECTION Bottom Last Used RF PORT Antenna Last Used ANTENNA RANGE 12 ft Last Used ANTENNA HEIGHT 1 ft Last Used DIR CABLE...

Page 229: ...ast Used ANT CABLE 1 ft Last Used ANT CABLE LOSS 0 1 dB Last Used ANT GAIN 0 96 GHZ 7 5 dB Last Used ANT GAIN 1 03 GHZ 7 1 dB Last Used ANT GAIN 1 09 GHZ 6 1 dB Last Used ANT GAIN 1 15 GHZ 5 0 dB Last...

Page 230: ...DE S Last Used ANTENNA Bottom Last used LEVEL Blank Blank REPLIES Blank Blank FREQ Blank Blank TOP ERP Blank Blank TOP MTL Blank Blank BOT ERP Blank Blank BOT MTL Blank Blank A CODE Blank Blank C ALT...

Page 231: ...E LOSS 0 1dB Last used ANT GAIN 1 03GHZ 7 1dB Last used ANT GAIN 1 09GHZ 6 1dB Last used SQUITTERS ON Last used ALT REPORTING ON Last used DISPLAYED ALT Relative Last used TEST SET AA A92493 Last used...

Page 232: ...used LAT 90 0 O N Last used LONG 180 0 0 E Last used ADS B GEN DF17 Last used ADS B MON DF17 Last used GICB DF20 Last used ADS B GEN BDS 0 5 Screen FIELD F ACTORY POWER UP TYPE 9 9 DF 18 Last used AA...

Page 233: ...ER UP TYPE 5 5 DF 17 Last used AA A92492 A92492 PERIOD 1 00 s 1 00 s LAT 0 0 0 N 0 0 0 N LONG 0 0 0 E 0 0 0 E MOVEMENT No info No info T N UTC N UTC HDG 0 deg 0 deg ADS B GEN BDS 0 8 Screen FIELD F AC...

Page 234: ...NACV 0 0 N S 0 kts N 0 kts N HDG SUBTYPE 1 vel ovr gnd norm 1 vel ovr gnd norm VERT RATE 0 ft min 0 ft min GEO ALT DIFF FROM BARO 0 ft 0 ft SOURCE GEO GEO INTENT CHANGE NO NO AIRSPEED AIRSPEED TYPE IF...

Page 235: ...A92492 A92492 PERIOD 1 00 s 1 00 s VERT DATA SOURCE INFO Not used Not used TARG ALT CAP HLDG ALT HLDG ALT VERT MODE IND Unknown Unknown SIL 0 0 TARG ALT TYPE FL FL NIC BARO 0 0 TARG ALT 0 ft 0 ft TAR...

Page 236: ...UP TYPE 31 31 DF 18 Last used AA A92492 A92492 PERIOD 1 00 s 1 00 s SUBTYPE D airborne D airborne NAC D D BAQ D D SIL 0 0 TC 0 0 CDTI 0 0 ARV 0 0 TS 0 0 RA 0 0 VER NBR Do 260 Do 242 Do 260 Do 242 NOT...

Page 237: ...sed DIR CABLE LOSS 1 2 dB Last used ANT CABLE 1 ft Last used ANT CABLE LOSS 0 1 dB Last used ANT GAIN 1 03 GHz 7 1 Last used ANT GAIN 1 09 GHz 6 1 Last used UUT ADDRESS Auto Auto MANUAL AA 000000 Last...

Page 238: ...a BDS B Definition Subfield BIT Built In Test BOT Bottom bps Bits per Second BR Bridge Rectifier BT Battery C C Celsius or Centigrade CA Transponder Capability CC Crosslink Capability ccw Counterclock...

Page 239: ...Subfield IN Input INTERR Interrogation I O Input Output ITM Intermode K KE Control ELM kg Kilogram 10 3 Grams kHz Kilohertz 10 3 Hertz km Kilometer 10 3 meters Kts Knots Velocity L LCA Logic Cell Arra...

Page 240: ...loscope SCPI Standard Commands for Programmable Instruments organization SD Special Designator Sec Second SL Sensitivity Level SLM Standard Length Message SLS Side Lobe Suppression SPI Special Identif...

Page 241: ...OPERATION MANUAL IFR 6015 APPENDIX D Subject to Export Control see Cover Page for details Page 4 Oct 1 16 THIS PAGE INTENTIONALLY LEFT BLANK...

Page 242: ...OPERATION MANUAL IFR 6015 APPENDIX E Subject to Export Control see Cover Page for details Page 1 Oct 1 16 APPENDIX E BREAKOUT BOX Breakout Box Top View Figure 1 Breakout Box Front View Figure 2...

Page 243: ...port 2 H_D In Out USB Host Data Compliment 3 H_D In Out USB Host Data True 4 GND_DN1 Ground Ground for USB device port USB HOST Connector Table Table 1 2 USB DEVICE CONNECTOR PIN NO SIGNAL NAME SIGNA...

Page 244: ...2 A2 Input Altitude Encode Input 3 A4 Input Altitude Encode Input 4 B1 Input Altitude Encode Input 5 B2 Input Altitude Encode Input 6 B4 Input Altitude Encode Input 7 C1 Input Altitude Encode Input 8...

Page 245: ...TYPE DESCRIPTION 1 REM_IN1 Input General Purpose Input 2 REM_IN2 Input Timestamp Reset LVTTL Trigger In 3 REM_IN3 Input General Purpose Input 4 REM_IN4 Input General Purpose Input 5 GND Ground System...

Page 246: ...1 16 5 RS 232 CONNECTOR PIN NO SIGNAL NAME SIGNAL TYPE DESCRIPTION 1 2 HOST_TXD BIPOLAR RS 232 Data Output 3 HOST_RXD BIPOLAR RS 232 Data Input 4 5 GND Ground System Ground 6 7 HOST_CTS BIPOLAR RS 232...

Page 247: ...er Page for details Page 6 Oct 1 16 6 AUX OUT CONNECTORS CONNECTOR SIGNAL TYPE DESCRIPTION AUX OUT 1 Output Mode S Interrogation Trigger AUX OUT 2 Output ATCRBS Interrogation Trigger AUX OUT 3 Output...

Page 248: ...A4 Input Altitude Encode Input 9 C2 Input Altitude Encode Input 10 C4 Input Altitude Encode Input 11 GND Ground System Ground 12 REM_IN1 Input General Purpose Input 13 REM_OUT2 Output General Purpose...

Page 249: ...N1 Supply 5 V supply for USB device port 32 VBUS_DN1 Supply 5 V supply for USB device port 33 VBUS_UP Supply 5 V supply input from USB host 34 GND_UP Ground Ground for USB host port 35 GND Ground Syst...

Page 250: ...48 5 to 57 0 74 3 1090 1 MODE S CL B OPT POW 51 0 to 57 0 74 3 1090 3 MK10A MK12 M4 55 0 to 59 0 75 3 1090 1 MK12 S M4 55 0 to 59 0 75 3 1090 0 5 DIR w Coupler Configuration TX Power dBm RX MTL dBm T...

Page 251: ...S CLASS B 48 5 71 1090 3 MODE S CL B OPT FRQ 48 5 71 1090 1 MODE S CL B OPT POW 51 0 71 1090 3 MK10A MK12 M4 55 0 72 1090 1 MK12 S M4 55 0 72 1090 0 5 DIR w Coupler Configuration TX Power dBm RX MTL...

Page 252: ...le contains Mode S address blocks for countries whose tail numbers are decoded by the IFR 6000 For an expanded list of Mode S codes refer to Appendix H COUNTRY ADDRESS BLOCK Belgium 448000 448FFF Cana...

Page 253: ...OPERATION MANUAL IFR 6015 APPENDIX G Subject to Export Control see Cover Page for details Page 2 Oct 1 16 THIS PAGE INTENTIONALLY LEFT BLANK...

Page 254: ...E00000 E3FFFF Cambodia 70E000 70EFFF Armenia 600000 6003FF Cameroon 034000 034FFF Australia 7C0000 7FFFFF Canada C00000 C3FFFF Austria 440000 447FFF Cape Verde 096000 096FF Azerbaijan 600800 600BFF Ce...

Page 255: ...B2000 0B2FFF Iran Islamic Rep 730000 737FFF Equatorial Guinea 042000 042FFF Iraq 728000 72FFFF Eritrea 202000 2023FF Ireland 4CA000 4CAFFF Estonia 511000 5113FF Israel 738000 73FFFF Ethiopia 040000 04...

Page 256: ...0C2FFF Malta 4D2000 4D23FF Papua New Guinea 898000 898FFF Marshall Islands 900000 9003FF Paraguay E88000 E88FFF Mauritania 05E000 05D3FF Peru E8C000 E8CFFF Mauritius 060000 0603FF Philippines 758000 7...

Page 257: ...00 601BFF Slovakia 505C00 505FFF Uganda 068000 068FFF Slovenia 506C00 506FFF Ukraine 508000 50FFFF Solomon Islands 897000 8973FF United Arab Emirates 896000 896FFF Somalia 078000 078FFF United Kingdom...

Page 258: ...en an immediate action is to be taken to avoid the assignment of an unauthorized 24 bit aircraft address It is intended that the temporary address is to be relinquished as soon as practicable when the...

Page 259: ...OPERATION MANUAL IFR 6015 APPENDIX H Subject to Export Control see Cover Page for details Page 6 Oct 1 16 THIS PAGE INTENTIONALLY LEFT BLANK...

Page 260: ...rborne on the ground alert Special Position Identification SPI etc 2 3 DATA LINK COMMUNICATIONS The discrete addressing and digital encoding allow Mode S transmissions to be used as digital data links...

Page 261: ...rveillance 17 1 0001 27 or 83 AP 24 18 1 0010 27 or 83 AP 24 19 1 0011 27 or 83 AP 24 20 1 0100 PC 3 RR 5 DI 3 SD 16 MA 56 AP 24 Comm A Altitude Request 21 1 0101 PC 3 RR 5 DI 3 SD 16 MA 56 AP 24 Comm...

Page 262: ...Extended Squitter 18 1 0010 CF 3 AA 24 ME 56 PI 24 Extended Squitter 19 1 0011 27 or 83 P 24 20 1 0100 FS 3 DR 5 UM 6 AC 13 MB 56 AP 24 Comm B Altitude Reply 21 1 0101 FS 3 DR 5 UM 6 ID 13 MB 56 AP 2...

Page 263: ...DF 11 Acquisition Squitter DF17 Extended Squitter or All Call reply to report transponder capability Codes are 0 Signifies no communications capability surveillance only no ability to set CA code 7 ei...

Page 264: ...contains IIS MBS MES LOS RSS TMS 2 SD used for extended squitter surface control 3 SD contains SIS LSS RRS 4 6 Not assigned 7 SD contains IIS RRS LOS TMS DR 5 9 13 X Requests extraction of downlink m...

Page 265: ...l NOTE The same information may also appear in the IIS subfields SI Surveillance Identifer lower 4 bits of 6 bit SI code NOTE Surveillance Identifier is derived from CL and IC fields of UF11 or direct...

Page 266: ...eports data link service s supported by the installation If all bits are Zeros no Comm A data link services are supported AIS 48 41 88 X Aircraft Identification reported when a surveillance or Comm A...

Page 267: ...nstallations report additional capabilities in various formats assigned to BDS2 codes other than 0 as requested by interrogator specified in the RRS subfield of SD CFS 4 41 44 X Continuation subfield...

Page 268: ...ield reports the identity of the interrogator See SD and UM fields SRS 16 9 24 X If a Comm C interrogation UF 24 contains RC 3 the SRS subfield contains a list of segment request authorizations for DE...

Page 269: ...Messages transmitted by TCAS without horizontal resolution capability HRC is set to 0 The codes are 0 No horizontal resolution advisory complement sent 1 Intruder TCAS sense is turn left do not turn...

Page 270: ...Messages VRC 2 45 46 X Vertical Resolution Advisory Complement The codes are 0 No vertical resolution advisory complement sent 1 Don t descend 2 Don t climb 3 Not assigned VSB 4 61 64 X Encoded Sense...

Page 271: ...6 X Is set to 3 for Coordination Reply Message VDS2 4 37 40 X Is set to 0 for Coordination Reply Message NC 4 5 8 X Provides the segment number transmitted in an uplink ELM and is part of a Comm C int...

Page 272: ...Disregard lockout reply with probability 1 2 10 Disregard lockout reply with probability 1 4 11 Disregard lockout reply with probability 1 8 12 Disregard lockout reply with probability 1 16 13 14 15 D...

Page 273: ...ssigned RL 1 9 X Command sent in UF 0 16 solicits DF 0 reply if Zero and DF 16 reply if One only if transponder is associated with Airborne Collision Avoidance System ACAS equipment Otherwise in UF 0...

Page 274: ...e All Call lockout to Mode S Only All Calls UF 11 from the Interrogator indicated in IIS of the interrogation If LOS is set to Zero no change in lockout state is commanded LOS is sent only if DI 1 or...

Page 275: ...code RRS 4 24 27 X Reply Request subfield sent when DI 3 contains coding corresponding to the requested BDS2 code RSS 2 27 28 X Reservation Status subfield sent when DI 1 requests transponder to repor...

Page 276: ...32 X Tactical Message subfield sent when DI 1 or 7 contains coding for linking the Comm A message segments The codes are 0 No Action 1 Unlinked Priority 2 Unlinked Acknowledge 3 Unlinked Priority Ack...

Page 277: ...as no meaning for aircraft with RI 0 no on board capability to generate resolution advisories UF 5 1 5 X The first field in all uplink formats is the transmission descriptor in all interrogations UM 6...

Page 278: ...0 1 I Y 9 1 0 1 0 J Z 1 0 1 1 K 1 1 0 0 L 1 1 0 1 M 1 1 1 0 N 1 1 1 1 O SP SPACE code 6 Bit Character Set for AIS Subfield Table 4 SRS OR TAS SUBFIELD VALUE OCTAL HEXADECIMAL NUMBER OF SEGMENTS 100000...

Page 279: ...12 C 1101 15 13 D 1110 16 14 E 1111 17 15 F 10000 20 16 10 Number Systems Conversion Table 6 UF FIELDS 0 VS b CC b SL d RI d AC h o AA h o 4 FS d DR d UM h IDS d IIS d AC h o AA h o 5 FS d DR d UM h...

Page 280: ...sing individual user interfaces via standard connectors Antenna Shield Used with Antenna Clamp Assembly to cover UUT Antenna not being tested 12 in Coaxial Cable Used to connect Test Set ANT Connector...

Page 281: ...a Clamp Assembly inside the slot in the Antenna Shield Plate aligning captive screws into the respective screw holes 2 Tighten captive screws STEP PROCEDURE 3 Cover UUT Antenna with Antenna Shield Loo...

Page 282: ...e coupler is completely depressed tightly against the aircraft Lock coupler into place by pushing white lever on the side of the coupler into a down and locked position STEP PROCEDURE NOTE Coupler mus...

Page 283: ...OPERATION MANUAL IFR 6015 APPENDIX J Subject to Export Control see Cover Page for details Page 2 Oct 1 16 THIS PAGE INTENTIONALLY LEFT BLANK...

Page 284: ...es for example there is a 10 probability the target acquisition time increases by more than ten sec NOTE The table only applies when testing one UUT Antenna Other UUT Antennas are shielded disabled or...

Page 285: ...OPERATION MANUAL IFR 6015 APPENDIX K Subject to Export Control see Cover Page for details Page 2 Oct 1 16 THIS PAGE INTENTIONALLY LEFT BLANK...

Page 286: ...1 REMOTE Connector App A p 2 Controls Connectors and Indicators 1 2 2 p 1 Description 1 1 1 p 1 E TCAS 1 2 4 p 75 External Cleaning 1 2 1 p 3 Factory Power Up Presets App C Functional Capabilities 1 1...

Page 287: ...een 1 2 4 p 60 Setup 1 2 4 p 55 Setup Antenna 1 1 2 p 11 Setup Scenario Data Screen 1 2 4 p 63 Surveillance Monitor 1 2 4 p 65 Testing 1 1 2 p 11 1 2 4 p 55 TIS Mode General description 1 2 4 p 139 Mo...

Page 288: ...OPERATION MANUAL IFR 6015 Subject to Export Control see Cover Page for details FOR QUALIFIED SERVICE PERSONNEL ONLY BATTERY FUSE INSTRUCTIONS...

Page 289: ...OPERATION MANUAL IFR 6015 Subject to Export Control see Cover Page for details THIS PAGE INTENTIONALLY LEFT BLANK...

Page 290: ...e unit and clarified in the text AC OR DC TERMINAL Terminal that may supply or be supplied with ac or dc voltage DC TERMINAL Terminal that may supply or be supplied with dc voltage AC TERMINAL Termina...

Page 291: ...TO NOR REMOVED FROM CIRCUITS WITH POWER ON PC BOARDS W HEN TAKEN OUT OF THE SET MUST BE LAID ON A GROUNDED CONDUCTIVE MAT OR STORED IN A CONDUCTIVE STORAGE BAG REMOVE ANY BUILT IN POWER SOURCE SUCH AS...

Page 292: ...6 Install the two lower bumpers and tighten the two captive screws in each bumper 8 in lbs BATTERY REPLACEMENT Refer to Figure 1 STEP PROCEDURE 1 Verify the IFR 6000 is OFF and not connected to AC po...

Page 293: ...OPERATION MANUAL IFR 6015 Subject to Export Control see Cover Page for details Page 2 Oct 1 16 Battery and Fuse Replacement Figure 1...

Page 294: ...reserve the right to make design changes without notice Go to http ats aeroflex com about us quality standard hardware warranty for Sales and Service contact information EXPORT CONTROL WARNING This do...

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