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ORIGINAL: APRIL 27, 2007 

REVISION 15: JANUARY 30, 2012 

DGT105608 

Copyright© 2007 by Dassault Aviation. 

All rights reserved. No part of this work may be reproduced or copied 

in any form or by any means without written permission 

of Dassault Aviation 

FALCON 7X 

Airplane 

Flight Manual 

LIST OF SECTIONS 

A DASSAULT (~AVIAT ON 

GENERAL 

INTRODUCTION 

List of sections 

SECTION 0 - GENERAL 

SECTION 1 - LIMITATIONS. 

SECTION 2 - EMERGENCY PROCEDURES. 

SECTION 3 - ABNORMAL PROCEDURES. 

SECTION 4 - NORMAL PROCEDURES. 

SECTION 5 - PERFORMANCE. 

ANNEXES. 

SUPPLEMENTS. 

CONFIGURATION DEVIATION LIST. 

0-000-05 

PAGE 1/2 

Issue 3 

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PAGE 2/2 INTRODUCTION Airplane 

Issue 3 List of sections Flight Manual 

INTENTIONALLY LEFT BLANK ) 

DGT105608 

EASA APPROVED 
FALCON 7X 

Airplane 

Flight Manual 

A DASSAULT <'~AVIATION 

ABNORMAL 

GENERAL 

SECTION 3 -ABNORMAL PROCEDURES 

3-000-00 

PAGE 1/2 

Issue 1 

DGT105608 

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3-000-00 ABNORMAL FALCON 7X 

PAGE2/2 GENERAL Airplane 

Issue 1 Flight Manual 

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DGT105608 

EASA APPROVED 

A DASSAULT <~AVIATION 
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Airplane GENERAL PAGE 1/6 

Flight Manual Table of content Issue 5 

TABLE OF CONTENTS 

GENERAL 

- Table of content .. ......... ... .................... ... ...... .... ............ ...... .. ........ ..... .... .. ...... ............. ............ 3-000-01 

- Introduction ................................ ....... ...................... ............................................................... 3-000-10 

AIR DATA SYSTEM 

- Slip compensation malfunction .. ... .......... ....... ... ....... .. .. ..... ... ..... .. .... ...... ..... ... ............. .... ......... 3-100-05 

- ADS failure ...................... ......... ............ .... .... .. ......... ......... ... .... .... .... ................................ ....... 3-100-10 

- Lost or misleading ADS information ...... ................ .. ...................... ... ................ ...... .... .. .. ........ 3-100-15 

- Heat system failure ........ .... .. ........ .. ..... .. ... .. .. .... ............. .......... .............. .................. ................ 3-100-20 

- Heat system off .. .. ............................ .. .. ............. ............................................................. ........ 3-100-25 

AFCS (AUTOMATIC FLIGHT CONTROL SYSTEM) 

- AFCS failure .. .. ............ .. .......... .. .......... .. ..... .. .. .. ....... ......................... .. ........................... .. .. .. ... 3-110-05 

- AFCS miscompare .. ...... ......................................................................................................... 3-110-10 

ANTI ICE 

- Ice detection ..................................... ..... ... .............. ... .. ................... ......... ... ... ............ ..... ........ 3-120-05 

- A/I detection system failure .......... ...... .................................. .. .......... ...... ................ ...... .. .. ...... 3-120-1 0 

- A/1 engine system malfunction ...... .. .. .......... ................ .. .. ........ .. .. .. ...... ........ ........ .......... ........ .. 3-120-15 

- A/I Sduct system malfunction .......... ........ ................ .. .. .................................. .. .. .......... .. ......... 3-120-20 

- A/I wing system malfunction ........ ............ .......... .. ...................... .. ........................................... 3-120-25 

- All brake system failure ..... .. .. .. ...... ........ ................ ........... .. .................. .. .. ............ ...... .. ...... .... 3-120-30 

- All stall warning offset ............ ........ ...... .............................. ........ ............ .. .. .......... .. ................ 3-120-35 

APU 

- APU malfunction ................... .. .. ........ ... ... .. ............................... .. .. .................. .. ............ .......... 3-130-05 

AVIONICS 

- One MAU channel failure (Cancelled) .......... .................. ........................................................ 3-140-05 

- One MAU channel failure (A/C with M566) .......... ............ .. .............. ..................................... 3-140-05A 

- Two MAU channels failure (Cancelled) .. .............................................................. .............. .. ... 3-140-10 

- Two MAU channels failure (A/C with M566) .................. .......... .............. .................. ............. 3-140-10A 

- MAU channel high temperature .. .. .. ............ .. .......... ..... .. .... ........................ .. ........ ............ ...... . 3-140-15 

- Display Unit failure ...... ...... ............................................................... .... .. ................................ 3-140-20 

- Display Unit high temperature ...... .................................................... ............ ................ .. ........ 3-140-25 

- AGM failure ...... .. ......... ............................................................................................. .............. 3-140-30 

- ceo failure .......... .. .......... ........................................................................ ...................... ........ 3-140-35 

- Aural warning failure .................... ......... ......................... ................. .................................... .. .. 3-140-40 

- Control 1/0 failure ...... ................... .. .. ............ .. ........................................................................ 3-140-45 

Jt DASSAULT .(~AVIAT ON 

DGT105608 

EASA APPROVED 
3-000-01 ABNORMAL FALCON 7X 

PAGE 2/6 GENERAL Airplane 

Issue 5 Table of content Flight Manual 

- TCAS failure, Weather radar failure, TAWS failure .. .................... ........... .... .......... .................. 3-140-50 

- IRS malfunction ............................................................... ............................................... ... .. ... 3-140-55 

- FMS malfunction .............. .. ................................... .......... ..................................... ............ .. .... 3-140-60 

- Radio altimeter failure (Cancelled) ............... ..................... ...... ............................. .. ............... . 3-140-65 

- Radio altimeter failure (A/C with M566) ......................................................................... ....... 3-140-65A 

- Sensor miscompare (Cancelled) ............................................................................................ 3-140-70 

- Sensor miscompare (A/C with M566) ....................... ............. ............ ................................... 3-140-70A 

- CAS miscompare ................................................................................................................... 3-140-75 

- Navigation system failure .................. ............................................................................. ........ 3-140-80 

BLEED 

- APU bleed malfunction .... .. ................ ....................... .................... .......................................... 3-150-05 

- Bleed failure ....................................................................... .. .................................................. 3-150-10 

- HP bleed failure ........................................ .. ............................................ ................................ 3-150-15 

- Bleed low temperature ........... ........... .. ................... ....... .. .. ..................................... ... ............. 3-150-20 

- Bleed high temperature (Cancelled) ............ .. .. ...... ......... ........................................................ 3-150-25 

- Bleed high temperature (A/C with M566) .. ... ............. ......... .. .................... ............................. 3-150-25A 

- Cross bleed malfunction ......................................................................................................... 3-150-30 

COMMUNICATION 

- Radio cabinet failure ........ ................. .. ........................................................................ ............ 3-160-05 ) 

- Radio cabinet overheat .......................................................................................................... 3-160-10 

-Audio control panel failure .. ...................................................................................... .. ............ 3-160-15 

- VHF COM failure ......... ...... ........................... .. ..................... ................................................... 3-160-20 

- VHF COM overheat. ......... ............ .. ..................................................................................... .. . 3-160-25 

- HF COM failure ............... ....................................................................................................... 3-160-30 

- Transponder failure .. ........................... .................................. ....................... .......................... 3-160-35 

- SATCOM failure ......................... ............... ............... .............................................................. 3-160-40 

CONDITIONING 

- Conditioning high temperature ............. ....... ........................................................................... 3-170-05 

- Baggage compartment air conditioning failure (Cancelled) ... .. ... .......... .................. ......... ........ 3-170-10 

- Baggage compartment air conditioning failure (A/C with M566) ...... .... .................................. 3-170-1 OA 

- Crew air conditioning failure (Cancelled) ................................................................................ 3-170-15 

- Crew air conditioning failure (A/C with M566) ....................................................................... 3-170-15A 

- Pax air conditioning failure .......... ........ .......... ....... ............................ ...................................... 3-170-20 

- Conditioning pack malfunction ......... ........... .. ................................. ... ... .............. .............. ....... 3-170-25 

- Ground vent valve malfunction ... .......................................... ............... ...... .. ... ....................... . 3-170-30 

- Recirculation valve malfunction .... ... .. .............................. .... ............. ... ................................... 3-170-35 

- XBLEED valve malfunction ..................................................................................................... 3-170-40 

- Optional Humidifier malfunction .... .. ... .. ....................... .. ...... .. ............... ................ ................... 3-170-45 

DGT105608 

EASA APPROVED 

If DASSAULT <'~ VI TION 
FALCON 7X ABNORMAL 3-000-01 

Airplane GENERAL PAGE 3/6 

Flight Manual Table of content Issue 5 

DOORS 

- Door malfunction ................................................................................................................ .... 3-180-05 

ELEC 

- Battery high temperature and disconnection .......................................................................... 3-190-05 

- Aft distribution box hi temp (Cancelled) .. .. .. .... .................................................................. ...... 3-190-10 

- Aft distribution box hi temp (A/C with M566) ......................................................................... 3-190-1 OA 

- One or two generators failure (Cancelled) .. .......................................... .. .................... ............ 3-190-15 

- One or two generators failure (A/C with M566) ............ ........ ................................................. 3-190-15A 

- Bus tie misconfig and failure (Cancelled) ................................................................................ 3-190-20 

- Bus tie misconfig and failure (A/C with M566) ........................ .. .. .................................. .. ...... 3-190-20A 

- Autoshed (Cancelled) ................ ...... ............... ....................... ................................................. 3-190-25 

- Autoshed (A/C with M566) ....................... .. .. .. ..... .............................. ............................ ........ 3-190-25A 

- LH MAIN bus failure (Cancelled) ............ ........................................ ............ ............................ 3-190-30 

- LH MAl N bus failure (A/C with M566) ............ ........................ .............................. ........ ......... 3-190-30A 

- RH MAIN bus failure (Cancelled) ............................................................................................ 3-190-35 

- RH MAIN bus failure (A/C with M566) .................................................................................. 3-190-35A 

- LH ESS bus failure (Cancelled) ...................................................... .................... ........ ...... ...... 3-190-40 

- LH ESS bus failure (A/C with M566) ..................................................................................... 3-190-40A 

- RH ESS bus failure (Cancelled) ............ ...................... .......................... ...... ...................... .. .. . 3-190-45 

- RH ESS bus failure (A/C with M566) ........................................................................ ............ 3-190-45A 

- Loss of ESS LH bus and SPDB (Cancelled) ...................... .......................................... .......... . 3-190-50 

- Loss of ESS LH bus and SPDB (A/C with M566) ................................................................. 3-190-50A 

- Loss of ESS RH bus and SPDB (Cancelled) .................................... ........ ............................ .. 3-190-55 

- Loss of ESS RH bus and SPDB (A/C with M566) ................................................................. 3-190-55A 

- Loss of MAl N LH bus and SPDB (Cancelled) .. ....................................................................... 3-190-60 

- Loss of MAl N LH bus and SPDB (A/C with M566) .. .............................. .. .............................. 3-190-60A 

- Loss of MAIN RH bus and SPDF (Cancelled) ......................................................................... 3-190-65 

- Loss of MAl N RH bus and SPDB (A/C with M566) .................................... .......................... . 3-190-65A 

- Loss of two buses (Cancelled) .......................... .. .. .............................. ................................... 3-190-70 

- Loss of two buses (A/C with M566) ........ ... .. ... ............... .... .... ......... ... .. ...... ...... ..................... 3-190-70A 

- Unwanted RAT deployment. ......... .. ... ......... ... ........................ .. .. ................................ .. ... ........ 3-190-75 

ENGINES 

- Engine failure in flight ........ ................................................................................... .................. 3-200-05 

- Abnormal start and Shutdown (Cancelled) ............................................................ .............. .. . 3-200-10 

- Abnormal start and Shutdown (A/C with M566) .................. .... ........................ ...................... 3-200-1 OA 

- Airstart (Cancelled) ................. ............................................................................................. .. . 3-200-15 

- Airstart (A/C with M566) ....... ...... .. .. ... .. ..................... ........... .. ............... ........ ........................ 3-200-15A 

- Airstart (A/C with M566 and M 1245) ..................................................................................... 3-200-15B 

- Throttle inoperative ........... ... ........ ............... .. .. ........... ... .. ................. .. ... .... .. .................... ....... . 3-200-20 

.:... Fuel filter bypass ... ................................................... .............................................................. 3-200-25 

Jf DASSAULT DGT105608 

(~ A v I A T I 0 N EASA APPROVED 
3-000-01 ABNORMAL FALCON 7X 

PAGE 4/6 GENERAL Airplane 

Issue 5 Table of content Flight Manual 

) 

- Lubrication system ...... ................................................ ................ ..................... .. .................... 3-200-30 

- Excessive parameters ... .. ..... ............................... ..................................... .............................. 3-200-35 

- Surge protection failure ............. ... ...... ...................... .. ......................... .. ...................... ........... 3-200-40 

- Excessive vibration .. ............. ................ .. ................ ..................... ........................... ................ 3-200-45 

- One or two engines inoperative .. ....... ... ........ ............ .. ........ ...................... .......... .. ...... .... ........ 3-200-50 

FLIGHT CONTROL 

- Computer or laws (Cancelled) ......... .. .. ......... .................................. .. ............. .... ...... ............ ... 3-210-05 

- Computer or laws (A/C with M566) .......................................................................... ... .......... 3-21 0-05A 

- Sensor or actuator malfunction (Cancelled) ............... ... .. ............ .. .................... ....... ............... 3-210-10 

- Sensor or actuator malfunction (A/C with M566) .......................... ..................... .. ... .............. 3-21 0-1 OA 

- Sensor or actuator malfunction (A/C with M566 and M 1245) ................. ....... .. .............. .... .... 3-21 0-1 OB 

- Trim malfunction .................................. ....................... ............................... ............................. 3-210-15 

- Airbrakes malfunction ................ ........... .................................................. ........ ...................... .. 3-210-20 

- Slats/Flaps malfunction (Cancelled) .................... ................ .. .. ............................................... 3-210-25 

- Slats/Flaps malfunction (A/C with M566) ...................... ........... ...... .. ... ......................... .. ....... 3-21 0-25A 

FIRE PROTECTION 

- Detection failure .......... ........ ................... .. ............ .. ... ........ ... ..... ............................................. 3-220-05 

FUEL ) 

- Low pressure (Cancelled) .................................................. .................................. .......... ....... .. 3-230-05 

- Low pressure (A/C with M566) .......... .. ........................ ............................ ............. ..... .. ......... 3-230-05A 

- Fuel quantity asymmetry .. .. ... .. .................. ...... ...... ........... ............ .. .. ...................................... 3-230-10 

- Fuel system malfunction ....... .... ................................... ..... .......................... ...... ....... ............... 3-230-15 

GEAR AND BRAKE 

- Gear system malfunction .. .... ... ............ .............................. ............ ... ... ..... ....... ... ..... ........ ....... 3-240-05 

- Hydraulic failure on brakes .... ... .......................... .. .. ....... .......... ... .. .. .................... .. .. ................ 3-240-10 

- Brake system malfunction ........ .......................................... .......... ........... .. .......... ................... 3-240-15 

- Nose Wheel steering malfunction ............. ............. ................ ......... ... ............. .... .. .. ................ 3-240-20 

- Tire low pressure ......... ..... .... .. .. .. ........... ...... .............. ........ ............................................... .. .... 3-240-25 

HYDRAULIC 

- Hydraulic low pressure (Cancelled) ...................... ........ .... .................................................... .. 3-250-05 

- Hydraulic low pressure (A/C with M566) ................................ ... ...... .. .... .... ...... ... .. .. .. ............. 3-250-05A 

- Hydraulic low quantity ................................. .. ............................. ............................. ............... 3-250-10 

- Hydraulic high temperature ............................ ............ ..... ......................... .... .................. ....... . 3-250-15 

- Hydraulic system malfunction ............... ...................... ........... .... .... ......... .............. .. ................ 3-250-20 

OXYGEN 

- Oxygen failure ............. .......... .. .... .... ................. ........................... ................... ... .................... . 3-260-05 

DGT105608 

EASA APPROVED 

J1 DASSAULT <~AVIAT ON 
FALCON 7X ABNORMAL 3-000-01 

Airplane GENERAL PAGE 5/6 

Flight Manual Table of content Issue 5 

PRESSURIZATION 

- BAG VENT valve malfunction (Cancelled) .. .. ... ........... ............ .. ... .. .................. .. ........... .... ...... 3-270-05 

- BAG VENT valve malfunction (A/C with M566) ................................................ .. .................. 3-270-05A 

- Pressurization system malfunction (Cancelled) ........................ ............. ...... ........................... 3-270-10 

- Pressurization system malfunction (A/C with M566) ............. ......... .... .......................... ......... 3-270-1 OA 

- Cabin overpressure (Cancelled) ...... ..... ................... .. .... ........... .......... .. ................ .................. 3-270-15 

- Cabin overpressure (A/C with M566) ......... ................ .. .. ... ....... ...................... ....................... 3-270-15A 

- Abnormal cabin altitude ......................... ... ...... .. .. ........... ............ .. ....... ... .. .. ...... ....................... 3-270-20 

THRUST REVERSERS 

- Thrust reverser malfunction ... ... ....... ....... .............. .. .... ............ .... ....................... .......... ........... 3-280-05 

WATER 

- Water heater overheat. ....... ................ ... ............ ... ... .. ..... .. ........... ... ... ... ................... ... ...... .. .... 3-290-05 

- Liquid leak in baggage compartment ....... ... ................................ ......... ... .. ......... ............... ...... 3-290-10 

WINDSHIELD 

- Windshield failure ............. ................................ ....... ..... ........................... ... ..... .. ..... .... .......... .. 3-300-05 

- Crack and Bubbles ......................................... .. ......... ...... ... ....................... .. ..... ... .. ........ ......... 3-300-1 0 

- Windshield heater fault .. ........................ .. .... ................... ............................ ............. ..... ..... ..... 3-300-15 

A DASSAULT .(~AVIATION 

DGT105608 

EASA APPROVED 

."! 

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3-000-01 ABNORMAL FALCON 7X 

PAGE 6/6 GENERAL Airplane 

Issue 5 Table of content Flight Manual 

) 

INTENTIONALLY LEFT BLANK 

) 

DGT105608 

EASA APPROVED 
FALCON 7X ABNORMAL 

Airplane AVIONICS 

Flight Manual Sensor miscompare (AIC with M566) 

ATT MISCOMPARE 

Both PDUs: Amber 5 miscompare annunciation. 

Other effects: 

- AP is disengaged, 

- All FD modes are canceled. 

3-140-70A 

PAGE 1/6 

Issue 2 

• Cross-check with Secondary Flight Display or IRS 3 and determine the faulty IRS. 

• Corresponding~ pushbutton ................. .................................... .. ..... .. ...... Push to select valid IRS 

0 On ADI .... .. ...... ..... .. ................... ......... ... ................... ..... ..... Amber IImJ or White liB 

AL T MISCOMPARE 

Both PDU: Amber ~ miscompare displayed on altitude scale, 

AP may disengage and FD vertical modes are cancelled. 

• Cross-check with Secondary Flight Display and determine the faulty ADS. 

• If the faulty ADS can be determined without ambiguity: 

• Corresponding ~ pushbutton .................................................... .. .. .. Push to select correct ADS 

0 On ADI ..... .. .................... .. ..................................... ... ...... White M•l'.il or amber r!mJl 

• Corresponding~ pushbutton ............................. Push to select IRS associated to selected ADS 

0 On ADI ...... .............................. .... .................. .. ...... ............ White 11m or amber IImJ 

• If the faulty ADS can not be determined: 

• Use ~ pushbutton to identify two consistent altitude indications. 

• If ADS 1 and ADS 3 give consistent altitude indications: 

• LH ~ pushbutton ...... ........................................... .................. .. ... ......... . Push to select ADS 1 

• RH ~ pushbutton ..... ................. .......... .......... ............... .... .... .. .............. Push to select ADS 3 

0 On RH ADI ................................. ........... .... .......... ... ................... · ............... White ~ 

• RH ~pushbutton ........................... ....... ........... ....... .. .. ......... .................. . Push to select IRS 3 

0 On RH ADI ...... .. .. ...... .. ........ .. ... .. ........... ... ... .... .. .... ................ .. ................... White liB 

• If ADS 2 and ADS 3 give consistent altitude indications: 

• LH ~ pushbutton .. ..... .. .. .. ......... .. .. .............. ... .. ... ..................... .... .. ....... Push to select ADS 3 

0 On LH AD I ...... ......... .. .. ... ................. ........... .. ......... ........................... ... ... .. White ~ 

• LH IIRSI pushbutton .. .. ............ .. .................... .. ......... .. ......... .................... ..... Push to select IRS 3 

0 On RH ADI ... .. ... ........................................................ ............................... .. White liB 

• RH ~ pushbutton ........ ..................................... ... ... ........ ... .... .. ....... .. .... Push to select ADS 2 

AJC with M566 or SB 7X-100 

DGT105608 

EASA APPROVED 
3-140-70A ABNORMAL FALCON 7X 

PAGE 2/6 AVIONICS Airplane 

Issue 2 Sensor miscompare (AIC with M566) Flight Manual 

• If ADS 3 and ADS 4 give consistent altitude indications: 

• LH and RH ~ pushbutton .... ... .......... ..... .............................. ................. Push to select ADS 3 

0 On both AD I .... ............................... .... ......... .. .. ..... .. ..... ............ .. ........... .... Amber !m!] 

• LH and RH §§!pushbutton .......... .. ............. ....... ... ........ .... ... ..... .......... .. .. ... Push to select IRS 3 

0 On both AD I ................................ ... .... .......................... ........ .............. .. .... .. Amber !Ia 

• In other cases: 

•Apply TOTAL LOSS OF CONSISTENT ADS INFORMATION procedure (section 3-100-15). 

+ 

FPV MISCOMPARE 

Both PDU: Amber a annunciation. 

• On non coupled side: §§! pushbutton ................... ... ........ ........ ... ......... ............. Push to select IRS 3 

0 On corresponding ADI ... .... ............ ........... ....... ... ...................... ........ ... ....... White !Ia 

• If a goes out: 

• End of procedure ~ 

• If a remains on: 

• On non coupled side revert to the previous IRS. 

• On coupled side ~ pushbutton .... ........................... ... ............... ..... ... .......... Push to select IRS 3 

0 On corresponding ADI .... .......... .. .... ............ .. ... .......... .. ........ .... ... .... ..... .. .. ... White tJD 

CAUTION 

Comparing with Secondary Flight Display Flight Path Symbol in climb or descent may lead to 

erroneous conclusions. 

HOG MISCOMPARE 

Both PDU: Amber !D annunciation. 

• Cross-check with Secondary Flight Display (except at high latitude) or IRS 3 and determine the 

faulty IRS. 

-~pushbutton on faulty side ........... .. ............... ............ .............. ............... Push to select valid IRS 

0 On ADI ... .......... ..... ..... .. ............ .......... ....... ...... .................. Amber tiD or White l[:mE 

DGT105608 

EASA APPROVED 

AJC with M566 or SB 7X-100 A DASSAULT (~AVIAT ON 
FALCON 7X ABNORMAL 

Airplane AVIONICS 

Flight Manual Sensor miscompare (AIC with M566) 

lAS MISCOMPARE 

Both PDU: Amber [m displayed on airspeed scale, 

AP may disengage and all FD modes are cancelled. 

• Cross-check with Secondary Flight Display and determine the faulty ADS. 

• If the faulty ADS can be determined without ambiguity: 

3-140-70A 

PAGE 3/6 

Issue 2 

~pushbutton on faulty side .. .. .. ................ .. ............. ........ ......... ... .... Push to select correct ADS 

0 On ADI ........... ..................... ............. : ... .. ..................... .... White amE or amber ~ 

• If the faulty ADS can not be determined: 

• Use~ pushbuttons to identify two consistent airspeed indications. 

• If ADS 1 and ADS 3 give consistent airspeed indications: 

• LH ~ pushbutton ....... .... ........ .... ... .. .. .... .... ... .. ........... .. .. .. .. ..... ... ............ Push to select ADS 1 

• RH ~ pushbutton ....... ... ............ .. .................. ................................ ..... .. Push to select ADS 3 

0 On RH ADI .. ........... .... .. ... ... .. .............................. .. ... ... .... ......... .... .... ...... ... White amE 

• If ADS 2 and ADS 3 give consistent airspeed indications: 

• LH ~ pushbutton ............... ......... .................... .. .. ...... ...... .. ................. ... Push to select ADS 3 

0 On LH ADI .. ................ .. .. ...... ................... .. ............................... ... .......... ... White amE 

• RH ~ pushbutton .......... .. .......... ..... .... .................................. .... ... ......... Push to select ADS 2 

• If ADS 3 and ADS 4 give consistent airspeed indications: 

• LH and RH ~ pushbutton ..... .. .... .. .......... .. .......... ...................... ............ Push to select ADS 3 

0 On both AD I .... .. .. ... .. ... ...... ..... ...................................... ............................ Amber amE 

• In other cases: 

•Apply TOTAL LOSS OF CONSISTENT ADS INFORMATION procedure (section 3-100-15). 

~ 

I· LOC OR GS MISCOMPARE 

Both PDU: Amber [!ili or m annunciation. 

• Determine the faulty ILS, if possible: 

• Select the correct ILS source for both sides. 

• If the faulty ILS is not identified: 

• Do not perform an ILS approach. 

A DASSAULT (~AVIATfON 

AJC with M566 or SB 7X-1 00 

DGT105608 

EASA APPROVED 
3-140-70A ABNORMAL FALCON 7X 

PAGE 4/6 AVIONICS Airplane 

Issue 2 Sensor miscompare (AIC with M566) Flight Manual 

RA MISCOMPARE 

- Both PDU: Amber m annunciation. 

• If amber RA flag is temporarily displayed during initial climb and disappears when wings are 

levelled: 

• Disregard this temporary amber m flag. 

• End of procedure. rEI 

• If amber RA flag remains in any phase of flight: 

• ~ pushbutton on faulty side ........ ... ............. ... ........ .. .... ......... .... ...... Push to select cross-side RA 

0 On both AD I .. ... .. ............ .... ................... .. .. .. ................ .......... ......... Amber lm1] or im'fJ • ATC!TCAS .................. ..... .. .. ........ ... ..... .... .. ................. ................ ....................... .... ... TA only select 

.... AT THE END OF DESCENT AND BEFORE LANDING GEAR EXTENSION 

• Until landing, check that the remaining RA indication is not locked-up. 

• If remaining RA indication is locked-up: 

NOTE 

An incorrect remaining RA indication may be followed by misleading symptoms, such as: 

- Misleading aural warnin s from EGPWS and unew cted "Gear" aural warning, 

- Unexpected MifiJ;jNa l•r•WW and l!aMIB•1~! iji#}i~[•iliJij!! messages, 

- Landing gear indication possibly displayed amber until the landing gear extension. 

NOTE 

IFCS: PITCH AUTOTRIM INOPI CAS message may appear: corresponding procedure has to be 

completed. 

CAUTION 

- Autothrottle may switch to retard mode upon landing gear extension. 

- Autothrottle and autopilot low speed protections may be inoperative, as well as the 

"INCREASE SPEED" aural warning. 

- FD G/S guidance may be wrong. 

- Autotrim may be still active during flare . 

.... PRIOR TO FINAL APPROACH AND BEFORE LANDING GEAR EXTENSION: 

• AT ....... .. .. ......................... .. ..... .. .. ........ .... ................................................................ .. Disconnect 

• HUD combiner (if installed) ..... .. .. .................................. ...................................................... Stow 

DGT105608 

AJC with M566 or SB ?X-1 00 

EASA APPROVED 
FALCON 7X ABNORMAL 3-140-70A 

Airplane AVIONICS PAGE 5/6 

Flight Manual Sensor miscompare (AIC with M566) Issue 2 

NOTE 

CATEGORY IIILS Approaches are not authorized. 

CATEGORY I ILS APPROACH 

• Perform the approach using raw data. 

• AP .. ...... ....................... ... ............ ......... ....................................................................... Disengage 

• FD (both sides) .. ..... ........ ....... ................. .... .............. ...................... .. ............................ . Remove 

OTHER APPROACHES 

• AP ................. ... .. ... .. .......... ..................... ................ ...................... .. ....... .................... As required 

• FD (both sides) ......... ..... ........................ ............ .. .. . ~ ......................................... .. .. .... As required 

AJC with M566 or SB ?X-1 00 

DGT105608 

EASA APPROVED 
3-140-70A ABNORMAL FALCON 7X 

PAGE 6/6 AVIONICS Airplane 

Issue 2 Sensor miscompare (AIC with M566) Flight Manual 

INTENTIONALLY LEFT BLANK 

A/C with M566 or SB ?X-1 00 

DGT105608 

EASA APPROVED