### EFFECTIVITY : ALL Page 1/1 « DASSAULT AVIATION Proprie tary Data » 10/JUN/2011 DGT 107838 Revision 1 CP009 - EASA Approved 

## FALCON 7X - CHAPTE R 5-40-00 after Rev01
SECTION 5. CMRs AND OTHER ALI THAN FATIGUE and DAMAGE TOLERANCE's (scheduled ALI CDCCLs and AL I from qualification tests)
Before CP009 dated 10/Jun/2011 :

- No task for OPERATIONAL TEST OF THE HSTA ELECTRIC MOTORS REVERSION
After CP009 dated 10/Jun/2011:

MPD task Code Oper Origin Title Max Limit comment effectivity 27-40-00-710-801 01 CMR OPERATIONAL TEST OF TH E HSTA ELECTRIC MOTORS REVERSION 1850 FH A/C with M 1236 or with SB 211

embodied09004000804f9dcd - RELEASED - Certification Repository

### FALCON 7X Airplane Flight Manual OPERATING TECHNIQUES OPERATING TECHNIQUES Trim malfunction 

### 2-100-85 PAGE 1 / 2

CP055

DGT 105608 EASA APPROVEDDASSAULT AVIATION Proprietary Data 

### PITCH TRIM RUNAWAY
Pitch Trim Runaway Possibly: FCS: TRIM LIMIT , FCS: THS DEGRAD , FCS: ALTN LAWS ACTIVE and AFCS: AP FAIL messages in CAS.

 Counteract using Side Stick

 Counteract using the manual pitch trim

 Emergency panel: TRIM EMERG pushbutton .............................................................................. Push  Status light ...................................................................................................... Amber ON  FCS: THS DEGRAD , FCS: ALTN LAWS ACTIVE and AFCS: AP FAIL appear

### 2-100-85 OPERATING TECHNIQUES OPERATING TECHNIQUES Trim malfunction 

### FALCON 7X Airplane Flight Manual PAGE 2 / 2

CP055

DGT 105608 EASA APPROVEDDASSAULT AVIATION Proprietary Data

INTENTIONALLY LEFT BLANK

### FALCON Airplane Flight Manual Limitations AIRSPEED, MACH AND LOAD FACTORS Airspeed and Mach 

### 1-150-10 PAGE 1 / 2

CP056

DGT105608 EASA APPROVEDDASSAULT AVIATION Proprietary Data 

### MAXIMUM OPERATING LIMIT SPEED: VMO / MMO

VMO / MMO ENVELOPE Unless otherwise specified, limits are expressed in terms of indicated values. Instrument error is assumed to be zero.

MAXIMUM OPERATING LIMITS MMO = 0.85 VMO = 320 kt

### 1-150-10 Limitations AIRSPEED, MACH AND LOAD FACTORS Airspeed and Mach 

### FALCON Airplane Flight Manual PAGE 2 / 2

CP056

DGT105608 EASA APPROVEDDASSAULT AVIATION Proprietary Data WARNING

OVERSPEED PROTECTIONS AND AURAL WARNINGS ARE NOT TRIGGERED AT MMO / VMO.

CAUTION The maximum operating limit speed MMO / VMO must not be deliberately exceeded in any regime of flight (climb, cruise, descent) unless a higher speed is authorized for flight tests or pilot training.

### FALCON Airplane Flight Manual Limitations AVIONICS Automatic flight control system 

### 1-250-05 PAGE 1 / 2

CP056

DGT105608 EASA APPROVEDDASSAULT AVIATION Proprietary Data 

### AUTOMATIC PILOT Autopilot must not be engaged for take-off or landing. - Minimum height to engage autopilot after take-off ........................................................................ 40 0 ft - Minimum height for autopilot operation except during approach .................................................. 400 ft - Minimum height for autopilot operation during approach without path reference ........................ 120 ft - Minimum height for autopilot operation during approach with vertical path reference (ILS-CAT1) ....................................................................................... ... 80 ft

CAUTION - Above 35,000ft and airspeed below 230 KIAS Do not use airbrakes AB1 position while automatic pilot is in use in roll mode with a bank angle above 28. - Above 25,000ft and airspeed below 250 KIAS Do not use airbrakes AB2 position while automatic pilot is in use.

### 1-250-05 Limitations AVIONICS Automatic flight control system 

### FALCON Airplane Flight Manual PAGE 2 / 2

CP056

DGT105608 EASA APPROVEDDASSAULT AVIATION Proprietary Data



### AUTOTHROTTLE The autothrottle must not be engaged for take-off, go-around and landing.
- Minimum height to engage autothrottle in climb after take-off ...................................................... 400 ft - Minimum height to disengage autothrottle at landing ...................................................................... 50 ft

### FALCON Airplane Flight Manual Limitations FLIGHT MANAGEMENT AND NAVIGATION SYSTEM Flight Management and navigation system 

### 1-400-05 PAGE 1 / 10 CP056

DGT105608 EASA APPROVEDDASSAULT AVIATION Proprietary Data 

### OPERATION BARO-SETTING Below transition altitude or level, altimeter setting must be set to QNH to use VNAV and VSD. FMS Barometric VNAV guidance during approach i ncluding the approach transition, final approach segment, and the missed approach procedure is not temperature compensated. Unless a temperature limitation is reflected on the approach chart, operating at uncompensated minimum IFR altitudes will not provide expected terrain and obstacle clearance for temperatures below ISA.



### AVIONICS WINDOW

FMS SPEED TAB - AUTO Spd Tab: - In descent, the crew must not select “Vmo/Mmo”, - Crew must ensure that selected speeds are below 0.85/320 kt.



### FLIGHT MANAGEMENT WINDOW - Alt/Spd Tab: - If CRZ Spd is in “manual”, the crew must check that selected speeds are below 0.85/320 kt. - If CRZ Spd is in “LRC” or “Max End”, the cr ew must check that selected speeds are below 0.85/320 kt. - The crew must not use “Max Spd”.



### SENSORS WINDOW

FMS OPERATING MODE FMS support synchronous and single-mode operation. Selecting synchronous for an FMS which is in single operation will result in th e synchronization of that FMS with the Pilot Flying FMS (Master FMS). NAVIGATION MODE AND PERFORMANCE GPS: GPS, as installed, has been found to comply with the requirements for the use of GPS for IFR oceanic, domestic en route, and terminal area operations, as defined in JAA Leaflet No. 3 REV 1, when used in conjunction with the Pre-flight In tegrity Prediction Softwar e, part number 050-03462- 0003 or later approved prediction program. The statements here-above are valid if there is no FMS and/or GPS related failure message/label on the PDU / MDU. GPS updating must be disabled when operating in countries whose national airspace is not referenced to the WGS-84 reference datum in accordance with the criteria of AC20-130A, unless other appropriate procedures are used. NAVIGATION RNP flight operations are subject to GPS satellite av ailability and/or navaid coverage for the selected route. Navigation based on DME/DME or VOR/DME updating modes is permitted but may be

### 1-400-05 Limitations FLIGHT MANAGEMENT AND NAVIGATION SYSTEM Flight Management and navigation system 

### FALCON Airplane Flight Manual PAGE 2 / 10 CP056

DGT105608 EASA APPROVEDDASSAULT AVIATION Proprietary Data restricted by the availability or performance of the app licable ground nava ids. Crews should deselect (NOTAM) ground navaids that are not to be used for navigation.


### NAVIGATION MAP (INAV, VSD) AND LOG (WPT LIST):

INAV AND VSD DATA LAYERS INAV including VSD (obstacle, terrain) are provided for advisory purpose only. AIRWAYS layer should be used for flight planning on gr ound to avoid cluttering INAV display in flight. INAV including VSD must not be displayed with amber DGR in HSI or displayed EPU above 15NM. GRAPHICAL FLIGHT PLANNING Hold dialog box: - The FMS does not always take into account the published maximum Holding Pattern speed. Only the protection area calculated in accordance with the FAA (7130-3) model is taken into account. - Adapt and stabilize the airplane speed 2 minutes prior th e airplane over flies the fix for the first time. - Check that the FMS message HIGH HOLDING GRD SPD is out when passing the fix.



### CRUISE PERFORMANCE FUEL, TIME and SMART PERF prediction information are provided for advisory purpose only and must not be used for flight planning.



### SID / STAR / APPROACHES / TERMINAL PROCEDURES

WARNING INSERTING AND ACTIVATING A NEW APPROACH OR A NEW FPLN WILL RESET MINIMUMS SELECTIONS. THEREFORE, THEY SHOULD BE VERIFIED AFTER SUCH ACTION.

CAUTION- It is crew responsibility to check the system-proposed VGP angle against the chartpublished descent angle. - Once VGP is armed, no pi lot intervention should be made to ease the capture. Steep App check box must only be used during steep approach operation.

NOTE During holding pattern Flight Director mode may revert from VPATH to PATH mode.
- It is crew responsibility to check procedures retrieved from data base with SID / STAR / approach charts.

### FALCON Airplane Flight Manual Limitations FLIGHT MANAGEMENT AND NAVIGATION SYSTEM Flight Management and navigation system 

### 1-400-05 PAGE 3 / 10 CP056

DGT105608 EASA APPROVEDDASSAULT AVIATION Proprietary Data - Approach procedures retrieved from data base cannot be modified by the crew. - For approach procedures retrieved from data base where only one approach transition (IAF) is proposed, this transition w ill not be automatically selected by the system. It is crew responsibility to select this approach transition or not (vector to FAF), depending on the intended trajectory to execute the approach. - Some approaches and STAR procedures are not in the data base. This is because of the way some procedures are defined by the controlling agency and the limitations of the FMS.

### 1-400-05 Limitations FLIGHT MANAGEMENT AND NAVIGATION SYSTEM Flight Management and navigation system 

### FALCON Airplane Flight Manual PAGE 4 / 10 CP056

DGT105608 EASA APPROVEDDASSAULT AVIATION Proprietary Data 

### FMS-BASED APPROACHES The following table describes the approach procedur es approved for automatic execution with the FMS (i.e. use of LNAV/VNAV flight director gui dance, either flown manually or coupled to the autopilot). FMS navigation mode must be checked prior to IAF. Performing a Vertical Direct TO (VDTO) on an alti tude constrained FAF will lead to a late activation capability, and may result in a steep f light path angle up to minus 10 degrees. Whatever the kind of FMS-based approach, following one of the 3 events, the approach must be discontinued:

- UNABLE RNP in FMS message window (I-NAV),
or - Green APPR not displayed prior to FAF (ADI),
or - Amber DGR displayed (HSI).
Observing the Minimum Safe Altitude and obst acle clearances remains crew responsibility. Prior to executing an FMS based approach, the RNP Value on the sensor page shall be set to the value indicated in the first column. The FMS navigation and synchronization modes shall be checked against the second and third columns.
Approach type and RNP Approved FMS navigation mode Special considerations Specific events following which the approach must be discontinued
NDB orNDBDME

RNP 0.6 (or lower) GPS Dual FMS synchro NAV: FMS..-GPS 1+2 POS MISC NAV: FMS/GPS 1+2 MONIT message in CAS Single FMS andprocedurespecified NAVAID available and displayed in the HSI DME-DME Dual FMS synchro NAV: FMS..-GPS 1+2 POS MISC message in CAS Single FMS andprocedurespecified NAVAID available and displayed in the HSI

### FALCON Airplane Flight Manual Limitations FLIGHT MANAGEMENT AND NAVIGATION SYSTEM Flight Management and navigation system 

### 1-400-05 PAGE 5 / 10 CP056

DGT105608 EASA APPROVEDDASSAULT AVIATION Proprietary Data Approach type and RNP Approved FMS navigation mode Special considerations Specific events following which the approach must be discontinued
VOR

RNP 0.5 (or lower) GPS Dual FMS synchro NAV: FMS..-GPS 1+2 POS MISC NAV: FMS/GPS 1+2 MONIT message in CAS Single FMS andprocedurespecified NAVAID available and displayed in HSI DME-DME Dual FMS synchro NAV: FMS..-GPS 1+2 POS MISC message in CAS Single FMS andprocedurespecified NAVAID available and displayed in HSIVORDME, provided theprocedurespecified NAVAID has DME capability Dual FMS synchro NAV: FMS..-GPS 1+2 POS MISC message in CAS Single FMS andprocedurespecified NAVAID available and displayed in HSI

### 1-400-05 Limitations FLIGHT MANAGEMENT AND NAVIGATION SYSTEM Flight Management and navigation system 

### FALCON Airplane Flight Manual PAGE 6 / 10 CP056

DGT105608 EASA APPROVEDDASSAULT AVIATION Proprietary Data Approach type and RNP Approved FMS navigation mode Special considerations Specific events following which the approach must be discontinued
VORDME or TACAN

RNP 0.5 (or lower) GPS Dual FMS synchro NAV: FMS..-GPS 1+2 POS MISC NAV: FMS/GPS 1+2 MONIT message in CAS Single FMS andprocedurespecified NAVAID available and displayed in HSI DME-DME Dual FMS synchro NAV: FMS/GPS 1+2 MONIT message in CAS Single FMS andprocedurespecified NAVAID available and displayed in HSI VOR-DME Dual FMS synchro NAV: FMS..-GPS 1+2 POS MISC message in CAS Single FMS andprocedurespecified NAVAID available and displayed in HSI RNAV

RNP 0.3 GPS Dual FMS synchro NAV: FMS..-GPS 1+2 POS MISC NAV: FMS/GPS 1+2 MONIT message in CAS or GPS RAIM UNAVAILABLE or GPS RAIM ABOVE LIMIT FMS message DME-DME unless otherwise indicated on the approach chart Dual FMS synchro NAV: FMS..-GPS 1+2 POS MISC NAV: FMS/GPS 1+2 MONIT message in CAS

GPS
RNP 0.3 GPS Dual FMS synchro NAV: FMS..-GPS 1+2 POS MISC NAV: FMS/GPS 1+2 MONIT message in CAS or GPS RAIM UNAVAILABLE or GPS RAIM ABOVE LIMIT FMS message

### FALCON Airplane Flight Manual Limitations FLIGHT MANAGEMENT AND NAVIGATION SYSTEM Flight Management and navigation system 

### 1-400-05 PAGE 7 / 10 CP056

DGT105608 EASA APPROVEDDASSAULT AVIATION Proprietary Data Approach type and RNP Approved FMS navigation mode Special considerations Specific events following which the approach must be discontinued
NDB orNDBDME

RNP 0.6 (or lower) GPS Dual FMS synchro NAV: FMS..-GPS 1+2 POS MISC NAV: FMS/GPS 1+2 MONIT message in CAS Single FMS andprocedurespecified NAVAID available and displayed in HSI DME-DME Dual FMS synchro NAV: FMS..-GPS 1+2 POS MISC message in CAS Single FMS andprocedurespecified NAVAID available and displayed in HSI

### 1-400-05 Limitations FLIGHT MANAGEMENT AND NAVIGATION SYSTEM Flight Management and navigation system 

### FALCON Airplane Flight Manual PAGE 8 / 10 CP056

DGT105608 EASA APPROVEDDASSAULT AVIATION Proprietary Data Approac h type and RNP Approved FMS navigatio

n mode Special considerations Specific events following which the approach must be discontinued
VOR

RNP 0.5 (or lower) GPS Dual FMS synchro NAV: FMS..-GPS 1+2 POS MISC NAV: FMS/GPS 1+2 MONIT message in CAS Single FMS andprocedurespecified NAVAID available and displayed in HSIDMEDME Dual FMS synchro NAV: FMS..-GPS 1+2 POS MISC message in CAS Single FMS andprocedurespecified NAVAID available and displayed in HSIVORDME provided the procedure specified NAVAID has DME capability Dual FMS synchro NAV: FMS..-GPS 1+2 POS MISC message in CAS Single FMS andprocedurespecified NAVAID available and displayed in HSI

### FALCON Airplane Flight Manual Limitations FLIGHT MANAGEMENT AND NAVIGATION SYSTEM Flight Management and navigation system 

### 1-400-05 PAGE 9 / 10 CP056

DGT105608 EASA APPROVEDDASSAULT AVIATION Proprietary Data Approac

h type and RNP Approved FMS navigatio

n mode Special considerations Specific events following which the approach must be discontinued
VORDME or TACAN

RNP 0.5 (or lower) GPS Dual FMS synchro NAV: FMS..-GPS 1+2 POS MISC NAV: FMS/GPS 1+2 MONIT message in CAS Single FMS andprocedurespecified NAVAID available and displayed in HSIDMEDME Dual FMS synchro NAV: FMS/GPS 1+2 MONIT message in CAS Single FMS andprocedurespecified NAVAID available and displayed in HSIVORDME Dual FMS synchro NAV: FMS..-GPS 1+2 POS MISC message in CAS Single FMS andprocedurespecified NAVAID available and displayed in HSI RNAV

RNP 0.3 GPS Dual FMS synchro NAV: FMS..-GPS 1+2 POS MISC NAV: FMS/GPS 1+2 MONIT message in CAS or GPS RAIM UNAVAILABLE or GPS RAIM ABOVE LIMIT FMS messageDMEDME unless otherwise indicated on the approach chart Dual FMS synchro NAV: FMS..-GPS 1+2 POS MISC NAV: FMS/GPS 1+2 MONIT message in CAS

GPS
RNP 0.3 GPS Dual FMS synchro NAV: FMS..-GPS 1+2 POS MISC NAV: FMS/GPS 1+2 MONIT message in CAS or GPS RAIM UNAVAILABLE or GPS RAIM ABOVE LIMIT FMS message

### 1-400-05 Limitations FLIGHT MANAGEMENT AND NAVIGATION SYSTEM Flight Management and navigation system 

### FALCON Airplane Flight Manual PAGE 10 / 10 CP056

DGT105608 EASA APPROVEDDASSAULT AVIATION Proprietary Data 

### LOCALIZER-BASED APPROACHES

The use of FMS guidance (lateral and vertical) on the final approach segment of a localizer-based approach (LOC, LOC-DME, LOC B/C, LDA, SDF, ILS, ILS-DME) is prohibited. The final part of these approaches shall be executed on LOC or LOC/GS guidance only (depending on the type of procedure). However, the FMS LNAV / VNAV can be used up to interception of the localizer. For these phases (initial approach and intermediate approach), the limitations associated with the following events ( UNABLE RNP in FMS message window, amber DGR on HSI, NAV:FMS ..-GPS 1+2 POS MISC and NAV: FMS/GPS 1+2 MONIT in CAS message) are applicable.

### FALCON Airplane Flight Manual EMERGENCY OPERATING TECHNIQUES Emergency descent 

### 2-100-50 PAGE 1 / 2

CP056

DGT105608 EASA APPROVEDDASSAULT AVIATION Proprietary Data 

### EMERGENCY DESCENT

CAUTION The following procedure assumes structural integrity of the airplane. If structural integrity is questioned: - Limit airspeed to lowest practicable value, - Avoid high maneuvering load factors.

 FASTEN BELT pushbutton ........................................................................................................... Push  Status light ......................................................................................................... Blue ON

 Autopilot

............................................................................................................................... .. Disconnect

 Power levers (all 3) ......................................................................................................... .................. Idle

 AIRBRAKES .................................................................................................................... ................. AB2

 Descent airspeed: .......................................................................... 0.85 / 320 kt, smooth air conditi ons

 ATC transponder ............................................................................................................. . Mayday code

### 2-100-50 EMERGENCY OPERATING TECHNIQUES Emergency descent 

### FALCON Airplane Flight Manual PAGE 2 / 2

CP056

DGT105608 EASA APPROVEDDASSAULT AVIATION Proprietary Data

INTENTIONALLY LEFT BLANK

### FALCON Airplane Flight Manual EMERGENCY EMERGENCY PROCEDURES

Fly by wire(A/C with M566) 

### 2-200-35A PAGE 1 / 4

CP056

A/C with M566 or SB 7X-100 DGT105608 EASA APPROVEDDASSAULT AVIATION Proprietary Data 

### MASTER + gong with 66 FCS: DIRECT LAWS ACTIVE 

### in Crew Alerting System "DIRECT LAWS" voice warning Loss of protection, autotrims and autopilot.

 Operating technique DIRECT LAWS procedure (section 2-100-15) ... ................................ Applied 

 Maneuver with caution.

CAUTION Loss of protections (low speed, high speed, G load), autotrims, autopilot.
Loss of airbrakes auto retraction and inboard slats auto retraction. Do not use AB 2 in flight while flaps are extended. Use autothrottle until Minimum Use Height.

 Airspeed ...................................................................................................... Below 260 KIAS or MI 0.80

 Manual trims ................................................................................................................. .................... Use

 FASTEN BELT pushbutton ........................................................................................................... Push  Status light ......................................................................................................... Blue ON

 A/B AUTO EXT. pushbutton ......................................................................................................... Push  Status light .................................................................................................... Amber OFF

 Maximum landing crosswind 10 kt.
 If FCS: BOTH AILERONS FAIL NOT in CAS:

 If FCS: BOTH ELEVATORS FAIL NOT in CAS:

 If FCS: MFCC FAULT NOT in CAS:

 Perform a long stabilized approach.
 APPROACH

 SLATS/FLAPS handle ........................................................................................................ SF 3

 Approach speed (zero wind) ................................. ............................................................ VREF

 Increase landing distance by 23 % (multiply by 1.23).
 AT 50 FT

 Reduce progressively flight path angle to approximately minus 1.5° at touch down.

WARNING
PILOT MUST MINIMIZE SIDE STICK INPUTS AND TRIM ACTIVITY DURING FLARE.

### 2-200-35A EMERGENCY EMERGENCY PROCEDURES

Fly by wire(A/C with M566) 

### FALCON Airplane Flight Manual PAGE 2 / 4

CP056

DGT105608 A/C with M566 or SB 7X-100

EASA APPROVEDDASSAULT AVIATION Proprietary Data  AIRPLANE ON GROUND

 Manual airbrakes only when nose gear is maintained firmly on ground.

 End of procedure. 
 If FCS: MFCC FAULT in CAS:

 Airplane stabilized.

 Wait at least one minute or MFCC 1 or 2 or 3 green lighted in FCS synoptic page.

 FASTEN BELT pushbutton ................................................................................... Blue ON – Check

 Release pressure on flight controls.

 NORM FCS ENGAGE pushbutton ............................................................................................ Push

 If blue status light ENGAGE does not light:

 ST-BY FCS ENGAGE pushbutton ........................................................................................ Push

 If 66 FCS: DIRECT LAWS ACTIVE goes out:

 A/B AUTO EXT. pushbutton .................................................................................................. Push  Status light ................................................................................................ Unlighted - On

 End of procedure. 
 If 66 FCS: DIRECT LAWS ACTIVE remains on:

 Perform a long stabilized approach.
 APPROACH

 SLATS/FLAPS handle ............................................................................................................ . SF 3

 Approach speed (zero wind) ................................................................................................ VR EF

 Increase landing distance by 23 % (multiply by 1.23).
 AT 50 FT

 Reduce progressively flight path angle to approximately minus 1.5° at touch down.

WARNING
PILOT MUST MINIMIZE SIDE STICK INPUTS AND TRIM ACTIVITY DURING FLARE.

 AIRPLANE ON GROUND

 Manual airbrakes only when nose gear is maintained firmly on ground.

 End of procedure. 

### FALCON Airplane Flight Manual EMERGENCY EMERGENCY PROCEDURES

Fly by wire(A/C with M566) 

### 2-200-35A PAGE 3 / 4

CP056

A/C with M566 or SB 7X-100 DGT105608 EASA APPROVEDDASSAULT AVIATION Proprietary Data  If FCS: BOTH AILERONS FAIL in CAS:

CAUTION Roll control is accomplished only through rudder pedal inputs. Roll trim is inoperative: Use Rudder trim.

 Airplane stabilized.

 FASTEN BELT pushbutton ................................................................................... Blue ON – Check

CAUTION Be prepared to counteract roll tenden cy in case of effective FCS engage.

 Release pressure on flight controls.

 NORM FCS ENGAGE pushbutton ............................................................................................ Push

 If blue status light ENGAGE does not light:

 ST-BY FCS ENGAGE pushbutton ........................................................................................ Push

 If 66 FCS: DIRECT LAWS ACTIVE goes out:

 A/B AUTO EXT. pushbutton .................................................................................................. Push  Status light ................................................................................................ Unlighted - On

 End of procedure. 
 If 66 FCS: DIRECT LAWS ACTIVE remains on:

 Perform a long stabilized approach.
 APPROACH

 SLATS/FLAPS handle ............................................................................................................ . SF 3

 Approach speed (zero wind) ................................................................................................. VR EF

 Increase landing distance by 23 % (multiply by 1.23).
 AT 50 FT

 Reduce progressively flight path angle to approximately minus 1.5° at touch down.

WARNING PILOT MUST MINIMIZE SIDE STICK INPUTS AND TRIM ACTIVITY DURING FLARE.

 AIRPLANE ON GROUND

 Manual airbrakes only when nose gear is maintained firmly on ground.

 End of procedure. 

### 2-200-35A EMERGENCY EMERGENCY PROCEDURES

Fly by wire(A/C with M566) 

### FALCON Airplane Flight Manual PAGE 4 / 4

CP056

DGT105608 A/C with M566 or SB 7X-100

EASA APPROVEDDASSAULT AVIATION Proprietary Data  If FCS: BOTH ELEVATORS FAIL in CAS:

CAUTION

Pitch control is accomplished only through the manual pitch trim. Manual airbrakes only when nose gear is on ground.

 Airplane stabilized.

 FASTEN BELT pushbutton ................................................................................... Blue ON – Check

 Release pressure on flight controls.

 NORM FCS ENGAGE pushbutton ............................................................................................ Push

 If blue status light ENGAGE does not light:

 ST-BY FCS ENGAGE pushbutton ........................................................................................ Push

 If 66 FCS: DIRECT LAWS ACTIVE goes out:

 A/B AUTO EXT. pushbutton .................................................................................................. Push  Status light ................................................................................................ Unlighted - On

 End of procedure. 
 If 66 FCS: DIRECT LAWS ACTIVE remains on:

 Perform a long and flat stabilized approach (path angle approximately minus 1.5°).
 APPROACH

 SLATS/FLAPS handle ............................................................................................................ . SF 3

 Approach speed (zero wind) ..................................... ................................................. VREF + 20kt

 Increase landing distance by 120 % (multiply by 2.20).
 AT 50 FT

 Maintain flight path angle until touch down.

WARNING
PILOT MUST MINIMIZE SIDE STICK INPUTS AND TRIM ACTIVITY DURING FLARE.

 AIRPLANE ON GROUND

 Apply brake pressure then manually extend airbrakes at AB 2.

### FALCON Airplane Flight Manual ABNORMAL ENGINES Airstart(A/C with M566) 

### 3-200-15A PAGE 1 / 4

CP056

A/C with M566 or SB 7X-100 DGT105608 EASA APPROVEDDASSAULT AVIATION Proprietary Data 

### IN FLIGHT RELIGHT ENVELOPE: WINDMILLING

WINDMILLING RELIGHT

WARNING STARTER ASSISTED RELIGHT procedure must be applied before attempting a WINDMILLING RELIGHT.
For corresponding engine:

 Engine .. FUEL switch ........................................................................................................ ............. OFF

 Establish airplane within windmilling envelope.

### 3-200-15A ABNORMAL ENGINES Airstart(A/C with M566) 

### FALCON Airplane Flight Manual PAGE 2 / 4

CP056

DGT105608 A/C with M566 or SB 7X-100

EASA APPROVEDDASSAULT AVIATION Proprietary Data NOTE

Wait for N2 below 45 % before attempting a windmilling relight.

 BOOST .. status light .........................................................................................Unlighted - On - Check

 ANTI-ICE: ENG .. and WINGS status lights ....................................................Unlighted - Off - Check

 BLEED .. status light ............................................................................................ Amber OFF - Check

 Power lever .................................................................................................................. ....... Idle - Check

 Engine .. FUEL switch ........................................................................................................ ............... ON  On PDU .......................................................................... Green START and amber IGN

 Monitor ITT and N2.
 If engine is relighted (N2 stabilized):

 IGN annunciation ................................................................................................................. .......... Out

 START annunciation ................................................................................................................. .... Out

 Engines parameters ............................................................................................................ ..... Check
 If engine 2 is operative:

 BUS TIE pushbutton .............................................................................................................. Push  Status light .......................................................................................... Unlighted - Untied

 Release pressure on flight controls.

 NORM FCS ENGAGE pushbutton ............................................................................................ Push

 If blue status light ENGAGE does not flash:

 ST-BY FCS ENGAGE pushbutton ........................................................................................ Push

 GALLEY MASTER and CABIN MASTER pushbuttons ................................................ As required

 ANTI-ICE: ENG .. and WINGS pushbuttons ................................................................. As required

 TA/RA .........................................................................................................................

............... Select

 BLEED.. pushbutton ................................................................................................... Push to set On  Status light ................................................................................................ Unlighted - On

 WINDSHIELD HEAT: LH and RH pushbutton .......................................................... Push to set On  Status lights .............................................................................................. Unlighted - On

### FALCON Airplane Flight Manual ABNORMAL ENGINES Airstart(A/C with M566) 

### 3-200-15A PAGE 3 / 4

CP056

A/C with M566 or SB 7X-100 DGT105608 EASA APPROVEDDASSAULT AVIATION Proprietary Data 

### IN FLIGHT RELIGHT ENVELOPE: STARTER ASSIST

STARTER ASSISTED RELIGHT

NOTE If possible, wait 1 minute between engine shutdown and engine start.

 BUS TIE pushbutton ...................................................................................................................... Push  Status light ................................................................................................... Amber TIED For corresponding engine:

 Engine .. FUEL switch ........................................................................................................ ............. OFF

### 3-200-15A ABNORMAL ENGINES Airstart(A/C with M566) 

### FALCON Airplane Flight Manual PAGE 4 / 4

CP056

DGT105608 A/C with M566 or SB 7X-100

EASA APPROVEDDASSAULT AVIATION Proprietary Data  Establish airplane within starter assist envelope (below 35,000 ft).

 BOOST.. status light .........................................................................................Unlighted - On - Check

 ANTI-ICE: ENG .. and WINGS status lights .....................................................Unlighted - Off - Check

 BLEED .. status light ............................................................................................ Amber OFF - Check

 Maintain N1 above 70 % on other engines.

 Engine .. FUEL switch ........................................................................................................ ............... ON

 MAN START / MOTORING ENG .. pushbutton ........................................... Push and hold (0.75 sec.)  On PDU .......................................................................... Green START and amber IGN

 Monitor ITT and N2.
 If engine is relighted (N2 stabilized):

 IGN annunciation ................................................................................................................. .......... Out

 START annunciation ................................................................................................................. ... Out

 Engines parameters ............................................................................................................ ..... Check
 If engine 2 is operative:

 BUS TIE pushbutton .............................................................................................................. Push  Status light .......................................................................................... Unlighted - Untied

 Release pressure on flight controls.

 NORM FCS ENGAGE pushbutton ............................................................................................ Push

 If blue status light ENGAGE does not flash:

 ST-BY FCS ENGAGE pushbutton ........................................................................................ Push

 GALLEY MASTER and CABIN MASTER pushbuttons ................................................ As required

 ANTI-ICE: ENG .. and WINGS pushbuttons .................................................................. As required

 TA/RA .........................................................................................................................

............... Select

 BLEED.. pushbutton ................................................................................................... Push to set On  Status light ................................................................................................ Unlighted - On

 WINDSHIELD HEAT: LH and RH pushbutton .......................................................... Push to set On  Status lights .............................................................................................. Unlighted - On
 If engine is not relighted:

 Relight engine with WINDMILLING RELIGHT procedure (section 3-200-15A). 

### FALCON Airplane Flight Manual ABNORMAL FLIGHT CONTROL Sensor or actuator malfunction(A/C with M566) 

### 3-210-10A PAGE 1 / 2

CP056

A/C with M566 or SB 7X-100 DGT105608 EASA APPROVEDDASSAULT AVIATION Proprietary Data 

### MASTER + gong with FCS: THS DEGRAD 

### in Crew Alerting System

FCS: ALTN LAWS ACTIVE and AFCS: AP FAIL messages in CAS.

 Maneuver with caution.

 Use the manual pitch trim.

 Airspeed ...................................................................................................... Below 260 KIAS or MI 0.80

 Emergency Panel: TRIM EMERG pushbutton .............................................................................. Push  Status light ...................................................................................................... Amber ON
 If the manual pitch trim is operative:

 Maximum landing crosswind ............

......................................................................................... .. 15 kt

 End of procedure. 
 If the manual pitch trim is inoperative:
 CRUISE

 Recover speed for which side stick forces are acceptable.

CAUTION SLATS/FLAPS in clean configuration is forbidden at airspeed below 160 kt.

 APPROACH

 Maximum landing crosswind ............

......................................................................................... .. 15 kt

 A/B AUTO EXT. pushbutton ..................................................................................................... Push  Status light .................................................................................................... Amber OFF

 SLATS/FLAPS handle ............................................................................................................ ..... SF 2

 Airspeed ......................................................................................................................... VREF + 25 kt

 Landing gear handle ........................................................................................................... ...... Down  On HSI: GEAR symbols (all 3) .............................................................................. Green
 If in this configuration airplane has a nose up tendency:

 SLATS/FLAPS handle ............................................................................................................ . SF 3

 Approach speed (zero wind) ................................................................................................. VR EF

 Increase landing distance by 24 % (multiply by 1.24).

CAUTION Manual airbrakes extension at landing is not authorized.

### 3-210-10A ABNORMAL FLIGHT CONTROL Sensor or actuator malfunction(A/C with M566) 

### FALCON Airplane Flight Manual PAGE 2 / 2

CP056

DGT105608 A/C with M566 or SB 7X-100

EASA APPROVEDDASSAULT AVIATION Proprietary Data  If in this configuration airplane ha s a nose down tendency or is steady:

 SLATS/FLAPS handle ............................................................................................................ . SF 2

 Approach speed (zero wind) ........................................ ............................................. VREF + 25 kt

 FMW window: Arrival POF: Landing Config tab .......................................... Select Flaps Override

 Increase landing distance by 120 % (multiply by 2.2).

CAUTION Manual airbrakes extension at landing is not authorized.

CAUTION The landing gear not extended aural warning may not sound.

NOTE This procedure incorporates the procedure for: FCS: ALTN LAWS ACTIVE

. Do not complete the procedure for FCS: ALTN LAWS ACTIVE

.

### FALCON Airplane Flight Manual NORMAL BEFORE TAXI Before park brake is released 

### 4-110-05 PAGE 1 / 6

CP056

DGT105608 EASA APPROVEDDASSAULT AVIATION Proprietary Data 

### BEFORE PARK BRAKE IS RELEASED

NOTE For the first flight of the day COCKPIT CHECK must start from an electrical power off condition.
Before APU is started, safety area must be verified, nav lights must be turned on.
Before engines are started, park brake must be set, safety area must be verified, anticol red lights must be turned on.
Before park brake is released, following actions must be performed:

 Verifications of cabin and cockpit fire extinguishers and smoke hoods.

 Closure of all doors,

 Verification of Cargo and loose items,

 Verification of cockpit lights, including emergency panel.

 Verification of rain repellent level,

 Verification of hydraulic, and oxygen quantities,

 Verification of circuit breaker status,

 Verification of extinction of all “emergency panel” lights,

 Verification of tire pressure,

 Verification of no smoking and fasten seat belts signs,

 Verification of the accessibility of emergency handles for RAT and gear free fall extension,

 Verification of crew seat adjustment, rudder pedals and fa stening of crew seat belts,

 Verification of CCD pilot and copilot, outer position must be checked after verification,

 Test of Fire Control Panel  ,  Test of hydraulic Backup pump  ,  Test of RAT  ,  Test of emergency lights  ,  Test of windshield heat  ,  Test of cockpit oxygen masks  ,  Test of conditioning system  ,  Test of Anti Ice  ,  Verification that flight controls move freely up to full deflection of the stick,

NOTE Flight controls verification must be done without any other verification in progress and one axis after the other.

### 4-110-05 NORMAL BEFORE TAXI Before park brake is released 

### FALCON Airplane Flight Manual PAGE 2 / 6

CP056

DGT105608 EASA APPROVEDDASSAULT AVIATION Proprietary Data  Test of Airbrakes  ,
 Test of TRIM EMERG pushbutton  ,  Test of FCS  ,  Setting of ELT in AUTO position,

 Activation of fasten seat belt sign.
MEL when applicable must be checked for all failures indicated by CAS messages in CAS window or status page, as well as for failures identified by the crew independently of CAS messages.  FIRE CONTROL PANEL TEST This test must be performed before starting the APU or the first engine once status page has been checked. Initial conditions: - After LH and RH INIT performed, LH and UP DU available. Test description: - 1. Overhead panel: depress FIRE TEST, maintain, and check: - white CAS message FIRE: TEST IN PROGRESS is displayed. - illumination of all fire control panel and the throttles lights - 2. If amber CAS message FIRE: TEST FAIL is displayed: it must be determined which item has failed before entering MEL.

 HYDRAULIC BACKUP PUMP TEST This test must be performed before each flight. Initial conditions: - 1. Airplane on ground, - 2. Engine 1 running. Test description: - 1. Overhead panel: set BACKUP pump to ON , - 2. Check hydraulic # B pressure to 2900 PSI - 3. If pressure does not increase it must be determined which item has failed before entering MEL, - 4. Overhead panel: set BACKUP pump to AUTO.

 RAT TEST This test must be performed before each flight. Initial conditions: - 1. Electrical initialization completed. Test description: - 1. Synoptic / test page: select RAT soft key until white CAS message RAT: TEST IN PROGRESS is displayed. - 2. If amber CAS message RAT: TEST FAIL is displayed: it must be determined which item has failed before entering MEL.

### FALCON Airplane Flight Manual NORMAL BEFORE TAXI Before park brake is released 

### 4-110-05 PAGE 3 / 6

CP056

DGT105608 EASA APPROVEDDASSAULT AVIATION Proprietary Data  EMERGENCY LIGHTS TEST This test must be performed before each flight. Initial conditions: - 1. Always available. Test description - 1. Overhead panel: set EMERG LIGHTS on ON position. - 2. Check correct illumination of the emergency lights in the cockpit and the cabin.  WINDSHIELD HEAT TEST This test must be performed before each flight. Initial conditions: - 1. Airplane on ground Test description: - 1. Synoptic / test page: select WSHIELD soft key until white CAS message WSHIELD: TEST IN PROGRESS is displayed - 2. If amber CAS message WSHIELD: TEST FAIL is displayed: it must be determined which item has failed before entering MEL.  COCKPIT OXYGEN MASK TEST This test must be performed before each flight. Initial conditions: - 1. Crew stowage box switch must be ON - 2. Essential buses must be connected. Test description: - 1. Crew stowage box rotary switch on Normal position then press to test - 2. Yellow blinker is displayed within 4 sec. - 3. Repeat sequence on EMERG and 100% position - 4. If Yellow blinker is not displayed: it must be determined which item has failed before entering MEL.  CONDITIONING SYSTEM TEST This test must be performed before the first take-off of the day. Initial conditions: - 1. Airplane on ground - 2. APU running, BLEED auto or ENG 1 running, N2 > 60% and ENG 2 running, N2 > 60%. - 3. Air conditioning mode: NORMAL, or PAX OFF, or CREW OFF. Test description: - 1. Synoptic / test page : select COND soft key until white CAS message COND: TEST IN PROGRESS is displayed - 2. After 15sec, when white CAS message COND: TEST WAITING EMER is displayed select EMERG mode.

### 4-110-05 NORMAL BEFORE TAXI Before park brake is released 

### FALCON Airplane Flight Manual PAGE 4 / 6

CP056

DGT105608 EASA APPROVEDDASSAULT AVIATION Proprietary Data - 3. After 20sec, when white CAS message COND: TEST WAITING NORM is displayed select NORMAL mode. - 4. If amber CAS message COND: TEST FAILED is displayed: it must be determined which item has failed before entering MEL.  TEST OF ANTI ICE This test must be performed before each flight. Initial conditions: - 1. TLA at idle. Test description: - 1. ANTI-ICE: ENG1, ENG2 and ENG3 pushbuttons set to ON, - 2. Wait for 20 seconds, - 3. Check of absence of any A/I: ENG .. XX PRESS message in crew alerting system, - 4. ANTI-ICE: ENG1, ENG2 and ENG3 pushbuttons set to off.  AIRBRAKES TEST This test must be performed before each flight. Initial conditions: - 1. Airplane on ground and after verification of flight controls - 2. Hydraulic pressure established. Test description: - 1. Extend airbrakes to AB 1 then AB 2 position then AB 0. - 2. Check proper operation of airbrakes and absence of CAS message.  TRIM EMERG TEST This test must be performed before each flight. Initial conditions: - 1. Airplane on ground, flaps SF0 position, before TRIM EMERG test - 2. Park brake is ON - 3. All engines running - 4.Side stick released. Test description: - 1. Emergency panel: Set TRIM EMERG pushbutton to ON - 2. Select manual pitch trim until amber FCS: THS DEGRAD , FCS: NO DISPATCH , FCS: ALTN LAWS ACTIVE , AFCS: AP FAIL CAS messages are displayed. - 3. Check in FCS synoptic page that THS can be moved up and down by using manual pitch trim control - 4. Set THS 0° nose, release the manual pitch trim and check the THS does not move in FCS synoptic page. - 5. Emergency panel: Set TRIM EMERG pushbutton to OFF - 6. Overhead Panel: Select FCS ENGAGE and check amber FCS: THS DEGRAD , FCS: NO DISPATCH , FCS: ALTN LAWS ACTIVE , AFCS: AP FAIL CAS messages disappear.

### FALCON Airplane Flight Manual NORMAL BEFORE TAXI Before park brake is released 

### 4-110-05 PAGE 5 / 6

CP056

DGT105608 EASA APPROVEDDASSAULT AVIATION Proprietary Data  FCS TEST This test must be performed before each flight. Initial conditions: - 1. Airplane on ground, THS at rest, slats not ex tended and after verification of flight controls and test of airbrakes - 2. Park brake is On, - 3. All engines running, - 4. Sidestick released. Test description: - 1. Synoptic / test page: select FCS soft key until white CAS message FCS: TEST IN PROGRESS is displayed, - 2. Test is completed when white CAS message FCS: TEST IN PROGRESS goes out, - 3. If amber CAS message FCS: TEST FAIL is displayed: it must be determined which item has failed before entering MEL.

### 4-110-05 NORMAL BEFORE TAXI Before park brake is released 

### FALCON Airplane Flight Manual PAGE 6 / 6

CP056

DGT105608 EASA APPROVEDDASSAULT AVIATION Proprietary Data

INTENTIONALLY LEFT BLANK