CHANGE PROJECT PUB

TIII 5704 – EASY ARCHITECTURE ROBUSTNESS DESIGN ISSUE) CODDE2 PAGE 1 / 2 DGT105609 CP0177-PUB DGT105609 DASSAULT AVIATION Proprietary Data These attached CODDE2 amended pages are linked with the AFM CP0177 related to TIII 5704 – EASy Architecture Robustness Design Issue The technical content of this document is approved under the authority of DOA EASA.21J.051 under change reference CP0177. Approval Date: June 28, 2021. Pending next CODDE2 revision, attached pages can be used in conjunction with CODDE2 revision 24. FILING INSTRUCTIONS Title CODDE2 Sub-sub-sections changes Removed Added Applicability CODDE2-CP0177- TIII 5704 – EASy Architecture Robustness Design Issue 04-05-05 (all pages) issue 13 04-05-05 (all pages) CP0177 04-15-10 (all pages) issue 14 04-15-10 (all pages) CP0177 Insert this page in CODDE2 before the “LIST OF ISSUES” sub-sub-section (00-00-15). Remove CODDE2 CP0177 pages when CODDE2 revision 25 is received. CHANGE PROJECT PUB GENERAL REVISIONS TIII 5704 – EASY ARCHITECTURE ROBUSTNESS DESIGN ISSUE FALCON 7X PAGE 2 / 2 CODDE2 CP0177-PUB DGT105609 DGT105609 DASSAULT AVIATION Proprietary Data INTENTIONALLY LEFT BLANK FALCON 7X EMERGENCY AND ABNORMAL OPERATIONS OPERATING TECHNIQUES OPERATING TECHNIQUES 04-05-05 CODDE2 PAGE 1 / 32 DGT105609 CP0177 DASSAULT AVIATION Proprietary Data REJECTED TAKE-OFF – Any event or failure with or without CAS jeopardizing take-off safety below V1  (1) BELOW V1  Brakes ................................................................................................................................Full braking  Power levers (All 3) ........................................................................................................................ Idle  AIRBRAKES ........................................................................................................................ AB2  (2)  Thrust reverser ................................................................................................................... As required NOTE This procedure addresses the corrective actions linked with NO TAKE OFF. TASKS AND CALL OUT TASK ALLOCATION CALL - OUT PF PM Monitor and report failures. e.g. “AMBER CAS”, “ENGINE”, “SMOKE”, “DANGER”, “RED CAS”   (1) PIC Decides and announces the Rejected Take-Off. “STOP” PF Applies full braking and sets power levers to idle. PM Sets Airbrakes handle to position 2. “AIRBRAKES 2”   (2) PF Deploys Thrust reverser. "REVERSE" PM Checks effective deployment of the thrust reverser. “DEPLOYED” PF Applies thrust reverser as required. PM Advises ATC (IAS < 60 kt). "REJECTING TAKE-OFF" or "ABORTING TAKE-OFF" PF Vacates the runway if possible (except in case of fire). TECHNICAL EXPLANATIONS Triggering event Decision to reject take-off remains the Captain’s decision according to circumstances. However, DA recommends, as a general rules, to seriously consider performing the "Rejected take-off" Operating Technique for the following reasons: - Any significant failure before V1, - Any external event jeopardizing take-off safety. Objectives of the Operating Technique The “Rejected take-off” Operating Technique leads to interrupting take-off before V1. 04-05-05 EMERGENCY AND ABNORMAL OPERATIONS OPERATING TECHNIQUES OPERATING TECHNIQUES FALCON 7X PAGE 2 / 32 CODDE2 CP0177 DGT105609 DASSAULT AVIATION Proprietary Data NOTE Any Rejected Take-Off initiated after V1 could lead to a runway overrun. Expanded explanations   (1) Below 80 kt, DA recommends performing an RTO for any failure. Above 80 kt, DA recommends performing an RTO for the following major failures or events: - Any red CAS message. - Failure not indicated by a CAS message, but that leads the crew to believe that the airplane’s handling is affected, such as a non-commanded change of trajectory, insufficient acceleration (10 % below expected acceleration), inefficient flight control command, etc. - Any external event jeopardizing take-off safety.   (2) AIRBRAKES AB2 It is necessary to manually extend the airbrakes despite automatic extension. ENGINE FAILURE AT OR AFTER V1  AT VR  Rotate the airplane with full aft stick until a positive flight path is achieved.  AT V2  Maintain V2 by pitch up and down adjustments, limited to +20° pitch attitude (no thrust adjustment).  WHEN A POSITIVE FLIGHT PATH IS ESTABLISHED  Landing gear handle .........................................................................................................................Up CAUTION If the speed achieved when the landing gear is retracted is above V2, maintain the speed attained without exceeding a limit of V2 + 10 kt. If the conditions make it impossible to maintain the speed below V2+10 with a maximum pitch attitude of 20°, let the airplane accelerate at the current flight path angle.  AT NOT LESS THAN 400 FT AAL  Level flight acceleration. NOTE Slats-Flaps may be set to SF 1 as soon as V2+10 is attained.  AT VFR:  SLATS/FLAPS handle ...................................................................................................................SF 0 FALCON 7X EMERGENCY AND ABNORMAL OPERATIONS OPERATING TECHNIQUES OPERATING TECHNIQUES 04-05-05 CODDE2 PAGE 3 / 32 DGT105609 CP0177 DASSAULT AVIATION Proprietary Data  WHEN IN CLEAN CONFIGURATION  Maintain VFTO.  5 MINUTES MAX. AFTER TAKE-OFF THRUST POWER SETTING  Power levers .....................................................................................................................................CL NOTE The published take-off performance is achieved when take-off is performed in accordance with AFM section 5. EXPANDED EXPLANATION After Take-off or Go-Around, the power lever of the operative engine is in TO position (5 minutes maximum). During this time, the airplane air conditioning system is automatically switched off. A transient white CHECK CABIN RATE CAS message can be triggered. 04-05-05 EMERGENCY AND ABNORMAL OPERATIONS OPERATING TECHNIQUES OPERATING TECHNIQUES FALCON 7X PAGE 4 / 32 CODDE2 CP0177 DGT105609 DASSAULT AVIATION Proprietary Data TASKS AND CALL OUT TASK ALLOCATION CALL OUT PIC Announces take-off continuation. “GO” PM Announces VR. “ROTATE” PF Rotates (full aft stick) and aligns ROS with horizon. After ROS disappearance, follows FD TO guidance. PM Announces positive rate of climb. “POSITIVE RATE” PF Requests landing gear retraction. “GEAR UP” PM Retracts landing gear. Checks appropriate indication. Announces landing gear position. Sets taxi light off, and landing lights PULSE. Sets wings anti-ice as required. “GEAR IS UP” AT OR ABOVE 400FT AAL PF Requests AP ON. “AUTOPILOT ON” PM Selects AP ON. Checks FMA. Announces AP status. “AUTOPILOT IS ON” AT TAKE-OFF SAFETY ALTITUDE PM Announces take-off safety altitude. “TOSA” PF Checks aircraft is accelerating to VFT. AT VFR PM Announces when speed is greater than VFR (V2+30 kt). “ABOVE VFR” PF Requests slats / flaps retraction. “SF0” PM Retracts (one notch at a time). Checks appropriate indication and announces Slats/Flaps position. “SF CLEAN SET” AT VFT PM Announces when speed is greater than VFT. “VFT” PF Sets Max Climb Thrust on live engines. Follows SID with full automation except AT. “MAX CLIMB” WHEN CLEAR OF OBSTACLES PF Sets appropriate FD mode and speed as required. Announces vertical mode and speed. FALCON 7X EMERGENCY AND ABNORMAL OPERATIONS OPERATING TECHNIQUES OPERATING TECHNIQUES 04-05-05 CODDE2 PAGE 5 / 32 DGT105609 CP0177 DASSAULT AVIATION Proprietary Data GO AROUND – ONE ENGINE INOPERATIVE (APPROACH WITH SF 3)  TOGA pushbutton......................................................................................................................... Push  Rotate the airplane until a positive flight path is achieved.  Power levers .................................................................................................................................... TO  SLATS/FLAPS handle ...................................................................................................................SF 2  Maintain the approach speed by pitch up and down adjustments, limited to +20° pitch attitude (no thrust adjustment).  WHEN A POSITIVE FLIGHT PATH IS ESTABLISHED  Landing gear handle .........................................................................................................................Up  SLATS/FLAPS handle ...................................................................................................................SF 1  AT NOT LESS THAN 800 FT AAL  Level flight acceleration.  AT VFR:  SLATS/FLAPS handle ...................................................................................................................SF 0  WHEN IN CLEAN CONFIGURATION  Maintain VFTO.  5 MINUTES MAX. AFTER TAKE-OFF THRUST POWER SETTING  Power levers .....................................................................................................................................CL EXPANDED EXPLANATION After Take-off or Go-Around, the power lever of the operative engine is in TO position (5 minutes maximum). During this time, the airplane air conditioning system is automatically switched off. A transient white CHECK CABIN RATE CAS message can be triggered. 04-05-05 EMERGENCY AND ABNORMAL OPERATIONS OPERATING TECHNIQUES OPERATING TECHNIQUES FALCON 7X PAGE 6 / 32 CODDE2 CP0177 DGT105609 DASSAULT AVIATION Proprietary Data TASKS AND CALL OUT TASK ALLOCATION CALL-OUT PF PM Decide to go-around. “GO-AROUND SF2” PF Pushes the TOGA pushbutton. Follows the FD in LNAV-GA mode. Sets take-off thrust. PM Retracts slats flaps to SF2. Checks appropriate indication. Announces Slats/Flaps position. Checks Airbrakes are retracted. “SF 2 SET” WHEN POSITIVE RATE OF CLIMB PM Announces positive rate of climb. “POSITIVE RATE” PF Requests landing gear retraction. “GEAR UP” PM Retracts landing gear. Checks appropriate indication. Announces landing gear position. “GEAR IS UP” PF Request SF1. “SF1” PM Retracts slats flaps to SF1. Checks indication in PDU and announces Slats/Flaps position. “SF1 SET” AT OR ABOVE 400FT PF Requests AP. “AUTOPILOT ON” PM Engages AP. Confirms AP is engaged on FMA. “AUTOPILOT IS ON” AT GO-AROUND SAFETY ALTITUDE PM Announces go-around safety altitude. “GASA” PF Checks airplane is accelerating to VFT. AT VFR PM Announces when speed is greater than VFR. “ABOVE VFR” PF Requests Slats/Flaps retraction. “SF0” PM Retracts (one notch at a time) and checks appropriate indication. Announces Slats/Flaps position. “SF CLEAN SET” AT VFT PF Sets Max Climb Thrust on live engines. Follows missed approach with full automation except AT. “MAX CLIMB” WHEN CLEAR OF OBSTACLES PF Sets appropriate FD mode and speed as required. Announces vertical mode and speed. FALCON 7X EMERGENCY AND ABNORMAL OPERATIONS OPERATING TECHNIQUES OPERATING TECHNIQUES 04-05-05 CODDE2 PAGE 7 / 32 DGT105609 CP0177 DASSAULT 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.  INTERIOR LIGHTS: FASTEN BELT pushbutton .............................................................................. Push  Status light ........................................................................................................ Blue ON  Autopilot.............................................................................................................................. Disconnect  Power levers (all 3) ......................................................................................................................... Idle  AIRBRAKES .................................................................................................................................. AB2  Descent airspeed.......................................................................... MMO / VMO, smooth air conditions  Transponder ................................................................................................................................. 7700 COMMENTS: This configuration permits a high rate of descent while remaining within the MMO/VMO limits. Airbrakes may be used in all flight envelope. COMMENTS: To avoid high load factors, anticipate the level-off according to the rate of descent. Select a safe en-route altitude to continue the flight and achieve a safe landing. The amount of supplemental oxygen required shall be determined for the most critical point of the flight. TASKS AND CALL OUT TASK ALLOCATION CALL - OUT PIC Calls for Emergency Descent. “EMERGENCY DESCENT” PF Disconnects AP. PF Sets Power Levers to idle. PF Sets airbrakes handle to position 2. PF Adopts diverging heading  30 ° as required. Initiates descent to maximum appropriate speed, reducing speed if structural damage is suspected. PM Selects MEA or FL100 in ASEL. NOTE Once descent is established, AP can be reengaged in HDG and PATH modes. 04-05-05 EMERGENCY AND ABNORMAL OPERATIONS OPERATING TECHNIQUES OPERATING TECHNIQUES FALCON 7X PAGE 8 / 32 CODDE2 CP0177 DGT105609 DASSAULT AVIATION Proprietary Data TECHNICAL EXPLANATIONS Triggering event Rapid depressurization. Objectives of the Operating Technique The “EMERGENCY DESCENT” Operating Technique leads both crew members to set the airplane on the highest rate of descent. Expanded explanations None. RAPID DEPRESSURIZATION  Operating technique CREW RESPIRATORY PROTECTION procedure (section 04-05-05) .................... ............................................................................................................................................ Applied.    Operating technique EMERGENCY DESCENT procedure (section 04-05-05) ..................... Applied.   TASKS AND CALL OUT Refer to “Crew oxygen protection” (ATA35) and “Emergency Descent” Operating techniques. TECHNICAL EXPLANATIONS Triggering event The “RAPID DEPRESSURIZATION” Operating Technique must be triggered by the crew when rapid depressurization is identified, even if not annunciated by any alert through the aircraft interface. Objectives of the Operating Technique The “RAPID DEPRESSURIZATION” Operating Technique leads both crew members to wear their mask and initiate an emergency descent. Expanded explanations None. FALCON 7X EMERGENCY AND ABNORMAL OPERATIONS OPERATING TECHNIQUES OPERATING TECHNIQUES 04-05-05 CODDE2 PAGE 9 / 32 DGT105609 CP0177 DASSAULT AVIATION Proprietary Data UNWANTED DISCONNECTION OF AUTOPILOT AUTOPILOT voice warning, PDU ADI window: AP symbol flashing.  SIL pushbutton or AP quick disconnect pushbutton...................................................................... Push  Re-engage autopilot in normal flight conditions.  (1) TASKS AND CALL OUT TASK ALLOCATION CALL - OUT PF Manually flies the airplane. PF Silences the alarm.   (1) PF If necessary, requests the AP reconnection. “AP ON” PM Upon PF’s request, attempts to reengage AP and checks its effective engagement. “AP IS ON” Or “AP IS OFF” TECHNICAL EXPLANATIONS Triggering event - Aural alert "AUTOPILOT", - AP flag flashing on PDU's ADI window, - Not annunciated AP disconnection. Objectives of the Operating Technique The “AP DISCONNECTION” Operating Technique leads the PF to manually fly the airplane. Expanded explanations   (1) Silence the alarm The PF can silence the “AUTOPILOT” aural alarm using the AP/PTY pushbutton on sidestick, or the SIL pushbutton on the Guidance Panel. 04-05-05 EMERGENCY AND ABNORMAL OPERATIONS OPERATING TECHNIQUES OPERATING TECHNIQUES FALCON 7X PAGE 10 / 32 CODDE2 CP0177 DGT105609 DASSAULT AVIATION Proprietary Data UNWANTED DISCONNECTION OF AUTOTHROTTLE AUTOTHROTTLE voice warning, PDU ADI: A/T amber flashing.  AT/DISC pushbutton..................................................................................................................... Push  Try to re-engage the autothrottle.  (1)  If the re-engagement cannot be achieved:  Continue the flight without autothrottle. TASKS AND CALL OUT TASK ALLOCATION CALL - OUT PF Manually controls the throttle. PF Silences the alarm.   (1) PF If necessary, call for the AT reconnection. “AT ON” PM Upon PF’s request, attempts to reengage AT and checks its effective engagement. “AT IS ON” Or “AT IS OFF” TECHNICAL EXPLANATIONS Triggering event - Aural alert "AUTOTHROTTLE", - A/T flag flashing on PDU’s ADI window, - Unannunciated AT disconnection. Objectives of the Operating Technique The “AT disconnection” Operating Technique leads the PF to manually control the engines throttles. Expanded explanations   (1) Silence the alarm The PF can silence the "AUTOTHROTTLE" aural alarm using the AT push-button on the power levers. FALCON 7X EMERGENCY AND ABNORMAL OPERATIONS OPERATING TECHNIQUES OPERATING TECHNIQUES 04-05-05 CODDE2 PAGE 11 / 32 DGT105609 CP0177 DASSAULT AVIATION Proprietary Data OVERSPEED ALERT  AP ........................................................................................................................................ Disengage  Adjust power setting and / or path to decrease speed.  AIRBRAKES handle ........................................................................................................... As required NOTE Pull up maneuver engaged by FBW system should not be counteracted by the crew. TASKS AND CALL OUT TASK ALLOCATION CALL - OUT PF PM Emergency situation is identified. “OVERSPEED” PF Disconnects AP and flies the airplane manually. “I HAVE CONTROLS” PF Sets Power levers to Idle. PF Uses Airbrakes as required. PF Does not counteract pull-up maneuver engaged by the FBW system. PF Maneuver with caution. TECHNICAL EXPLANATIONS Triggering event - Aural alert VMO/MMO. Objectives of the Operating Technique The “OVERSPEED RECOVERY” Operating Technique leads the crew to reduce power levers setting to idle and, if required, to use airbrakes. Expanded explanations None. 04-05-05 EMERGENCY AND ABNORMAL OPERATIONS OPERATING TECHNIQUES OPERATING TECHNIQUES FALCON 7X PAGE 12 / 32 CODDE2 CP0177 DGT105609 DASSAULT AVIATION Proprietary Data INCONSISTENT OR UNRELIABLE FLIGHT DATA IN IPFD AND/OR HUD  Fly using SFD.  PILOT SIDE pushbutton ........................................................................................................Select LH  Monitor trajectory using INAV. INCREASE SPEED ALERT  Power setting .............................................................................................................................. Adjust  AP ........................................................................................................................................ Disengage  Path angle ..................................................................................................... Adjust to increase speed TASKS AND CALL OUT TASK ALLOCATION CALL - OUT PF PM Situation is identified. PF Adjusts power and / or path to increase speed. “I HAVE CONTROLS” TECHNICAL EXPLANATIONS Triggering event - Aural alert "INCREASE SPEED". Objectives of the Operating Technique The “INCREASE SPEED” Operating Technique leads the PF to increase the speed by adjusting power and path. Expanded explanations None. STALL "STALL" voice warning SIMULTANEOUSLY and smoothly:  Autopilot and Autothrottle ................................................................................................... Disconnect  Pitch control ........................................................................................................................ Nose down  Bank ................................................................................................................................... Wings level  Power levers .................................................................................................................................... TO  AIRBRAKES ................................................................................................................................. AB 0 FALCON 7X EMERGENCY AND ABNORMAL OPERATIONS OPERATING TECHNIQUES OPERATING TECHNIQUES 04-05-05 CODDE2 PAGE 13 / 32 DGT105609 CP0177 DASSAULT AVIATION Proprietary Data  AFTER STALL RECOVERY:  Pitch Attitude .............................................................................................................. Close to horizon  Thrust ......................................................................................................................................... Adjust TASKS AND CALL OUT TASK ALLOCATION CALL - OUT PF PM Emergency situation is identified. “I HAVE CONTROLS” PF Disconnects A/P and A/T and manually takes-over. PF Lower the nose and level the wings. PF Sets thrust to Take-Off power. PF Sets airbrakes manual handle in position 0. PF After stall recovery, adjust pitch and thrust as needed. TECHNICAL EXPLANATIONS Triggering event The “STALL RECOVERY” Operating Technique must be triggered by the crew for following reasons: - Aural alert "Stall". Objectives of the Operating Technique The “STALL RECOVERY” Operating Technique leads the crew to reduce angle of attack, by: - Reducing flight path angle (if trajectory permits). - Increasing power levers setting, Expanded explanations In case of stall warning, airbrakes will possibly auto-retract. 04-05-05 EMERGENCY AND ABNORMAL OPERATIONS OPERATING TECHNIQUES OPERATING TECHNIQUES FALCON 7X PAGE 14 / 32 CODDE2 CP0177 DGT105609 DASSAULT AVIATION Proprietary Data UNUSUAL ATTITUDE RECOVERY COMMENTS : The two following Operating Techniques are not in the Airplane Flight Manual but they provide the crew with adequate recovery techniques of nose-up and nose-down unusual attitudes. UNUSUAL ATTITUDE RECOVERY - NOSE UP  Autopilot and Autothrottle ................................................................................................... Disconnect  Power levers .................................................................................................................................... TO  Bank the aircraft by the shortest way........................................................................... 80° to 90° Bank  AIRBRAKES ................................................................................................................................. AB 0  WHEN AIRCRAFT NOSE IS CLOSE TO HORIZON:  Bank ................................................................................................................................... Wings level  Thrust ......................................................................................................................................... Adjust UNUSUAL ATTITUDE RECOVERY - NOSE DOWN  Autopilot and Autothrottle ................................................................................................... Disconnect  Power levers ................................................................................................................................... Idle  Bank ................................................................................................................................... Wings level  AIRBRAKES ....................................................................................................................... As required  Nose up pitch control ....................................................................................................Smoothly apply  WHEN AIRCRAFT NOSE IS CLOSE TO HORIZON:  AIRBRAKES ................................................................................................................................. AB 0  Thrust ......................................................................................................................................... Adjust FALCON 7X EMERGENCY AND ABNORMAL OPERATIONS OPERATING TECHNIQUES OPERATING TECHNIQUES 04-05-05 CODDE2 PAGE 15 / 32 DGT105609 CP0177 DASSAULT AVIATION Proprietary Data AIRBRAKE AUTO EXTEND FAIL – FCS: AB AUTO EXTEND FAIL  AIRBRAKES ....................................................................................................................... AB 2  (1) TASKS AND CALL OUT TASK ALLOCATION CALL - OUT PF PM Emergency situation identified. “AIRBRAKES FAIL” PM Pulls Airbrakes Manual Handle in position 2.   (1) “AIRBRAKES TWO” TECHNICAL EXPLANATIONS Triggering event - Red CAS message: FCS: AB AUTO EXTEND FAIL, - Crew identification of automatic airbrake extension failure during landing. Objectives of the Operating Technique The “AIRBRAKES AUTO EXTEND FAIL” Operating Technique leads the crew to manually extend airbrakes at landing. Expanded explanations   (1) AIRBRAKES AB2 With regard to airbrakes operation, DA recommends that it should always be performed: - By PF in flight, - By PM on ground. 04-05-05 EMERGENCY AND ABNORMAL OPERATIONS OPERATING TECHNIQUES OPERATING TECHNIQUES FALCON 7X PAGE 16 / 32 CODDE2 CP0177 DGT105609 DASSAULT AVIATION Proprietary Data AIRBRAKE AUTO RETRACT FAIL – FCS: AB AUTO RETRACT FAIL  AIRBRAKES ........................................................................................................................ AB0  (1) TASKS AND CALL OUT TASK ALLOCATION CALL - OUT PF PM Emergency situation identified. PF Retracts Airbrakes Manual Handle in position 0.   (1) “AIRBRAKES ZERO” TECHNICAL EXPLANATIONS Triggering event - Red CAS message: FCS : AB AUTO RETRACT FAIL, - Crew identification of automatic airbrakes retraction failure, during Go-Around or at high angle of attack. Objectives of the Operating Technique The “AIRBRAKE AUTO RETRACT FAIL” Operating Technique leads the crew to manually retract airbrakes if: - Airbrakes auto-retraction fails while low speed protection limit is reached, or - Engines are at Take-Off power after airbrakes have been manually extended, or - Flaps are extended while inboard airbrakes are not retracted. Expanded explanations   (1) AIRBRAKES AB0 Airbrakes operations should be performed: - By the PF in flight, - By the PM on ground. FALCON 7X EMERGENCY AND ABNORMAL OPERATIONS OPERATING TECHNIQUES OPERATING TECHNIQUES 04-05-05 CODDE2 PAGE 17 / 32 DGT105609 CP0177 DASSAULT AVIATION Proprietary Data BACK-UP "BACK-UP OPERATIVE" voice warning.  Use pitch trim for pitch control and rudder pedals for roll control.  (1) TASKS AND CALL OUT TASK ALLOCATION CALL - OUT PF PM Emergency situation identified. PF Uses pitch trim for pitch control and rudder pedals for roll control.   (1) “I HAVE CONTROLS” PF Announces when the airplane is under control.   (2) “UNDER CONTROL” TECHNICAL EXPLANATIONS Triggering event Loss of control by MFCC and SFCC, identified by the aural alert: “BACK-UPOPERATIVE”. Objectives of the Operating Technique The “BACK-UP” Operating Technique leads the crew to use pitch trim for pitch control and rudder pedals for roll control, after failure of MFCC and SFCC. Expanded explanations Transition to Back-up mode has a very low probability of occurrence and no credit is taken for it with regard to certification.   (1) Use pitch trim for pitch control and rudder pedals for roll control. The Back-Up computer allows roll control through the use of spoilers commanded by the pedals. Sidesticks are inoperative in back-up mode.   (2) Calls out ”Airplane Under control” Once the airplane trajectory is under control, the PF is able to handle communication and navigation tasks, allowing the PM to proceed with the Emergency Procedure. 04-05-05 EMERGENCY AND ABNORMAL OPERATIONS OPERATING TECHNIQUES OPERATING TECHNIQUES FALCON 7X PAGE 18 / 32 CODDE2 CP0177 DGT105609 DASSAULT AVIATION Proprietary Data DIRECT LAWS "DIRECT LAWS" voice warning  Sidesticks .................................................................................................................... Neutral position  Maneuver with caution.  (1) TASKS AND CALL OUT TASK ALLOCATION CALL - OUT PF PM Emergency situation identified. PF Releases sidestick then Maneuver with caution.   (1) “I HAVE CONTROLS” PF Announces when the airplane is under control.   (2) “UNDER CONTROL” TECHNICAL EXPLANATIONS Triggering event Loss of control by MFCC or degradation of MFCC flight control laws, identified by the aural alert: “DIRECT LAWS”. Objectives of the Operating Technique The “DIRECT LAWS” Operating Technique leads the crew to smooth the airplane maneuvers. Expanded explanations   (1) Release sidestick then Maneuver with caution Sidestick movement should be limited as Angle Of Attack, attitude and G-load protections are lost.   (2) Calls out ”Airplane Under control” Once airplane trajectory is under control, the PF is able to handle communication and navigation tasks, allowing the PM to proceed with the Emergency Procedure. FALCON 7X EMERGENCY AND ABNORMAL OPERATIONS OPERATING TECHNIQUES OPERATING TECHNIQUES 04-05-05 CODDE2 PAGE 19 / 32 DGT105609 CP0177 DASSAULT AVIATION Proprietary Data CONTROL SURFACE JAM – FCS: CONTROL SURFACE JAM  Maneuver with caution.  Maintain current speed or reduce below red tape if more restrictive, and maintain configuration. TASKS AND CALL OUT TASK ALLOCATION CALL – OUT PF PM Emergency situation identified. “CONTROL SURFACE JAM” PF Maintains current speed or reduce below red tape if more restrictive and maintains configuration. “I HAVE CONTROLS” PF Announces when the airplane is under control.   (1) “UNDER CONTROL” TECHNICAL EXPLANATIONS Triggering event Jamming of one aileron, spoiler, elevator or of the rudder, identified by the CAS message FCS: CONTROL SURFACE JAM. Expanded explanation   (1) Airplane Under control Once the airplane trajectory and configuration are under control, PF is able to handle communication and navigation tasks, allowing the PM to proceed with the Emergency Procedure. 04-05-05 EMERGENCY AND ABNORMAL OPERATIONS OPERATING TECHNIQUES OPERATING TECHNIQUES FALCON 7X PAGE 20 / 32 CODDE2 CP0177 DGT105609 DASSAULT AVIATION Proprietary Data SIDESTICK PRIORITY "XX SIDESTICK FAIL" voice warning – FCS: XX SIDESTICK FAIL, or – One sidestick jammed, – Incapacitation of one crew member, – Loss or damage of artificial feel.  Use valid sidestick to control the airplane.  On valid sidestick AP/PTY pushbutton .......................................................... Press for at least 30 sec. CAUTION Do not press AP/PTY pushbutton on jammed sidestick. COMMENTS: All pushbuttons on failed sidestick are operative. TASKS AND CALL OUT TASK ALLOCATION CALL – OUT PF PM Emergency situation identified. Pilot on affected side Requests transfer of control. “YOUR CONTROL” Pilot on non affected side Acknowledges transfer of control. “I HAVE CONTROLS” Pilot on non affected side Pushes AP/PTY pushbutton on sidestick during at least 30 seconds. Pilot on non affected side Controls the airplane with the valid sidestick. TECHNICAL EXPLANATIONS Triggering event - Mechanical Failure of one sidestick, including jam, high friction or complete or partial loss of artificial feel: this failure does not trigger any CAS message, - Hardware failure of one sidestick, indicated by red CAS message FCS: XX SIDESTICK FAIL and XX SIDESTICK FAIL aural alert, - Incapacitation of one crew member. FALCON 7X EMERGENCY AND ABNORMAL OPERATIONS OPERATING TECHNIQUES OPERATING TECHNIQUES 04-05-05 CODDE2 PAGE 21 / 32 DGT105609 CP0177 DASSAULT AVIATION Proprietary Data Objectives of the Operating Technique The “SIDESTICK PRIORITY” Operating Technique leads to having only one sidestick active. Expanded explanation None. 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 sidestick (1)  Counteract using the manual pitch trim (1)  Emergency panel: TRIM EMERG pushbutton ......................................................................... Push (2)  Status light ..................................................................................................... Amber ON  FCS: THS DEGRAD, FCS: ALTN LAWS ACTIVE and AFCS: AP FAIL appear. TASKS AND CALL OUT TASK ALLOCATION CALL – OUT PF PM Emergency situation identified. “TRIM RUNAWAY” PF Counteracts unwanted pitch effect using sidestick and manual trim control.   (1) PM Stops the pitch trim runaway by using the trim emergency pushbutton on PF’s request. TECHNICAL STATUS SYSTEM LOST AVAILABLE DFCS PITCH AUTO TRIM MANUAL PITCH TRIM DFCS NORMAL THS MOTORS BACK UP THS MOTOR DFCS NORMAL LAWS ALTERNATE LAWS AFCS AUTO PILOT X TECHNICAL EXPLANATIONS Triggering event - Pitch trim runaway not detected by the automatic protections loops, or - Pitch trim runaway triggered in manual operation. 04-05-05 EMERGENCY AND ABNORMAL OPERATIONS OPERATING TECHNIQUES OPERATING TECHNIQUES FALCON 7X PAGE 22 / 32 CODDE2 CP0177 DGT105609 DASSAULT AVIATION Proprietary Data Objectives of the Operating Technique The “PITCH TRIM RUNAWAY” leads to crew to counteract unwanted pitch effect due to pitch trim runaway. Expanded explanation   (1) Counteract pitch effect The crew must apply continuous pressure on sidestick if the airplane is not trimmed.   (2) Emergency panel: TRIM EMERG pushbutton: Push This action: - Stops any trim runaway by shutting down electrical power for THS motor 3 and 4. - Allows the crew to use the manual pitch through the THS back up motor. FALCON 7X EMERGENCY AND ABNORMAL OPERATIONS OPERATING TECHNIQUES OPERATING TECHNIQUES 04-05-05 CODDE2 PAGE 23 / 32 DGT105609 CP0177 DASSAULT AVIATION Proprietary Data RUDDER TRIM RUNAWAY Slipping tendency and roll effect  Counteract using pedals and the manual yaw trim. (1)  Crew must apply continuous pressure on pedals if airplane is not autotrimmed.  Engine differential thrust can be set to compensate a possible slipping tendency. TASKS AND CALL OUT TASK ALLOCATION CALL – OUT PF PM Emergency situation identified. “TRIM RUNAWAY” PF Counteracts slipping tendency and roll effect through pedals and yaw manual trim control.   (1) TECHNICAL EXPLANATIONS Triggering event This failure rudder trim when manually used by the crew. Objectives of the Operating Technique The “RUDDER TRIM OPERATING TECHNIQUE” leads the crew to counteract unwanted yaw effect due to rudder trim runaway. Expanded explanation   (1) Counteract slipping tendency The crew must apply continuous pressure on pedals if the airplane is not auto-trimmed. Engine differential thrust can be set to compensate a possible slipping tendency. If in Normal or Alternate Flight Control laws, the PM can attempt to reconnect the AP upon PF’s request. 04-05-05 EMERGENCY AND ABNORMAL OPERATIONS OPERATING TECHNIQUES OPERATING TECHNIQUES FALCON 7X PAGE 24 / 32 CODDE2 CP0177 DGT105609 DASSAULT AVIATION Proprietary Data TOTAL LOSS OF NORMAL BRAKING – BRAKE: BOTH SYSTEMS FAIL AIRPLANE ON GROUND  Thrust reverser ................................................................................................................... As required  Apply brake pressure slowly by gently pulling PARK BRAKE handle.  On PDU: Deceleration on dry runway .......................................................................Maintain – 0.25 g  AIRBRAKES ................................................................................................................................ AB 2 CAUTION Avoid PARK BRAKE handle cycling applications. TASKS AND CALL OUT TASK ALLOCATION CALL - OUT PF PM Emergency situation identified. “BOTH BRAKES FAIL” PF Deploys thrust reverser. “REVERSE” PM Checks effective deployment of the thrust reverser. “DEPLOY” PF Pulls Park Brake handle below first detent, to reach and maintain adequate deceleration rate (max -0.25 on a dry runway). “PARK BRAKE” PM Reads the deceleration rate on PDU. “INDICATED G” PM Pulls Airbrakes Manual Handle in position 2. “AIRBRAKES TWO” TECHNICAL EXPLANATIONS Triggering event The “TOTAL LOSS OF BRAKING” Operating Technique must be triggered by the crew for the following reasons: - Red CAS message: BRAKE: BOTH SYSTEMS FAIL confirmed by PF, - Crew identification of loss of normal braking system. Objectives of the Operating Technique The “TOTAL LOSS OF BRAKING” Operating Technique leads crew to use Park Brake rather than normal braking system. Expanded explanation None. FALCON 7X EMERGENCY AND ABNORMAL OPERATIONS OPERATING TECHNIQUES OPERATING TECHNIQUES 04-05-05 CODDE2 PAGE 25 / 32 DGT105609 CP0177 DASSAULT AVIATION Proprietary Data CREW RESPIRATORY PROTECTION "CABIN" voice warning, – smoke and unusual odors, – Rapid depressurization,  Full face masks...............................................................................................................................Don  Crew oxygen mode selector ...................................................................................................... EMGY  Yellow blinker ................................................................................................... Checked TASKS AND CALL OUT TASK ALLOCATION CALL - OUT PF PM Emergency situation identified. PF PM Don their quick donning oxygen masks and verify oxygen supply. "OXYGEN" PF PM Select “Mask” on Audio Control Panel and test communication. NOTE MIC button on the storage box should be in "MASK" position at all times. TECHNICAL EXPLANATIONS Triggering event The “CREW OXYGEN PROTECTION” Operating Technique must be triggered by the crew for the following reasons: - Rapid depressurization, - Smoke in the cockpit, - Aural alert CABIN. Objectives of the Operating Technique The “CREW OXYGEN PROTECTION” Operating Technique leads both crew members to don their mask. Expanded explanation None. 04-05-05 EMERGENCY AND ABNORMAL OPERATIONS OPERATING TECHNIQUES OPERATING TECHNIQUES FALCON 7X PAGE 26 / 32 CODDE2 CP0177 DGT105609 DASSAULT AVIATION Proprietary Data PULL UP "PULL UP" or "TERRAIN AHEAD PULL UP" or "OBSTACLE AHEAD PULL UP" voice warning – PULL UP in PDU – PULL UP in HUD  Autopilot.............................................................................................................................. Disconnect  Level the wings.  Sidestick fully aft.  Power levers .................................................................................................................................... TO  SLATS/FLAPS ............................................................................................................... SF2 maximum  Landing gear handle .........................................................................................................................Up  On HSI: GEAR symbols (all 3) ................................................................................. Out TASKS AND CALL OUT TASK ALLOCATION CALL - OUT PF PM Emergency situation is identified. PF Announces a pull-up maneuver. “PULL-UP RECOVERY” PF Disconnects AP. “I HAVE CONTROLS” PF Pulls sidestick fully aft. PF Sets Power Levers to Take Off. PF Requests SF2 if in SF3. “SF2” PM Sets SF2 on PF’s request and checks slats/flaps effective retraction. “SF2 SET” PIC Requests gear retraction as required, once risk of contact with ground has been eliminated. “GEAR UP” PM Retracts the gear on PIC’s request and checks its effective retraction. “GEAR IS UP” PF Maintains positive rate of climb until safety altitude is reached. TECHNICAL EXPLANATIONS Triggering event The “PULL UP” Operating Technique must be triggered by the crew for following cases: - Identification of possible terrain collision, without EGPWS alert, - Aural “PULL UP” alert and red PULL UP warning in the PDU, - Aural “TERRAIN AHEAD PULL UP” alert or “OBSTACLE AHEAD PULL UP” and red PULL UP warning in the PDU. FALCON 7X EMERGENCY AND ABNORMAL OPERATIONS OPERATING TECHNIQUES OPERATING TECHNIQUES 04-05-05 CODDE2 PAGE 27 / 32 DGT105609 CP0177 DASSAULT AVIATION Proprietary Data Objectives of the Operating Technique The “PULL UP” Operating Technique leads the crew to execute a pull up maneuver to avoid ground collision. Expanded explanation At night or in IMC, the procedure should be applied immediately without diagnosis. During daylight VMC, with terrain and obstacles clearly in sight, the alert may be considered as cautionary. Take positive corrective action until alert ceases or a safe trajectory in ensured. WINDSHEAR RECOVERY "WINDSHEAR WINDSHEAR WINDSHEAR" voice warning, – WINDSHEAR in PDU, – WINDSHEAR in HUD.  TOGA pushbutton........................................................................................................................ Press  On FMA: WSHR .................................................................................................. Active  Autopilot............................................................................................................. Disconnected - Check  Flight Director ............................................................................................................................. Follow  Power levers .................................................................................................................................... TO  SLATS/FLAPS .............................................................................................................. SF 2 maximum  At pilot's discretion, according to airplane height and vertical speed:  Landing gear handle .....................................................................................................................Up  On HSI: GEAR symbols (all 3) ................................................................................. Out NOTE Disregard possible amber Low Speed Cue, "increase speed" aural warning and basic mode EGPWS aural alert during windshear recovery. TASKS AND CALL OUT TASK ALLOCATION CALL - OUT PF PM Emergency situation is identified. PF PM Announce the Windshear recovery maneuver. “WINDSHEAR RECOVERY” PF Pushes TOGA to activate the WSHR mode.  (1) PF PM Check AP disconnection.  (2) PF Follows WSHR vertical guidance.  (3) PF Sets TO thrust. PF Requests SF2 if in SF3 configuration. “SF 2” PM Sets SF2 and checks effective retraction. “SF2 SET” PM Announces positive flight path. “POSITIVE PATH” 04-05-05 EMERGENCY AND ABNORMAL OPERATIONS OPERATING TECHNIQUES OPERATING TECHNIQUES FALCON 7X PAGE 28 / 32 CODDE2 CP0177 DGT105609 DASSAULT AVIATION Proprietary Data TASK ALLOCATION CALL - OUT PIC Requests landing gear retraction once risk of contact with ground has been eliminated.  (4) “GEAR UP” PM Retracts the gear on PIC’s request and checks effective retraction. “GEAR IS UP” WHEN CLEAR OF WINDSHEAR PM Announces end of windshear “END OF WINDSHEAR” PF Requests vertical and lateral FD modes, as necessary e.g. “CLIMB MODE” “LNAV MODE” PM Sets requested vertical and lateral FD modes e.g. “CLIMB MODE SET” “LNAV MODE SET” PF Confirms activation of FD lateral and vertical modes on FMA “CHECKED” PF PM Perform the AFTER TAKE-OFF do-list and check-list when convenient Resume normal operations TECHNICAL EXPLANATIONS Triggering event The WINDSHEAR RECOVERY Operating Technique must be triggered by the crew for following cases: - Aural EGPWS WINDSHEAR WINDSHEAR WINDSHEAR alert and red WINDSHEAR warning in the PDU or WINDSHEAR flag in the HUD, - Windshear identified regardless of EGPWS alerts. Objective of the Operating Technique The WINDSHEAR RECOVERY Operating Technique leads the crew to execute an escape maneuver with maximum power. Expanded explanation   (1) TOGA Pressing TOGA push-button activates the WSHR escape guidance mode.   (2) Autopilot and Autothrottle disengagement conditions: If the AP is engaged, it automatically disengages when Windshear escape guidance mode (WSHR) becomes active. It the AT is engaged, it automatically disengages when Windshear escape guidance mode (WSHR) becomes active. While the FD WSHR guidance is active, the TD commands the MAX TO Thrust.   (3) Flight Director: ASEL is inhibited by the activation of the WSHR escape guidance. When leaving the Windshear conditions, the pilot must engage another vertical mode in order to get out of the WSHR escape guidance mode with AP, ALT, CLB, VS, VNAV or TOGA pushbuttons. FALCON 7X EMERGENCY AND ABNORMAL OPERATIONS OPERATING TECHNIQUES OPERATING TECHNIQUES 04-05-05 CODDE2 PAGE 29 / 32 DGT105609 CP0177 DASSAULT AVIATION Proprietary Data   (4) Risk of ground collision is considered eliminated when the following conditions are reached: - RA greater than 500 ft, - Indicated airspeed greater than low Speed Cues, - Positive path is followed. 04-05-05 EMERGENCY AND ABNORMAL OPERATIONS OPERATING TECHNIQUES OPERATING TECHNIQUES FALCON 7X PAGE 30 / 32 CODDE2 CP0177 DGT105609 DASSAULT AVIATION Proprietary Data TCAS ALERT TCAS RA voice warning – Resolution Advisory in PDU  Autopilot.............................................................................................................................. Disconnect  TCAS RA guidance .................................................................................................................... Follow TASKS AND CALL OUT TASK ALLOCATION CALL - OUT PF PM Emergency situation is identified. PF Disconnects AP. Follows TCAS RA guidance. “TCAS, I HAVE CONTROLS” PM Looks outside in VMC. Switches the LDG lights ON. Advises ATC. “ATC CENTER”, “AIRPLANE ID”, “TCAS RA” PM When cleared of conflict, advises ATC. “ATC CENTER”, “AIRPLANE ID”, “CLEAR OF CONFLICT”, “RETURNING TO “ASSIGNED CLEARANCE” Or “CLEAR OF CONFLICT”, “ASSIGNED CLEARANCE RESUMED” PM Advises ATC in case of a contradictory clearance or instruction. “UNABLE”, “TCAS RA” TECHNICAL EXPLANATIONS Triggering event TCAS alert (Resolution Advisory) is triggered following a TCAS Traffic Advisory. Objective of the Operating Technique The TCAS ALERT Operating Technique leads the crew to follow TCAS alert guidance. Expanded explanation None.