MEMORY ITEMS

Question 1

DC GEN 1+2 FAULT

Answer 1

▶ PF…………………………………….CAPT
▶ DC GEN 1 ………………………RESET
▶ DC GEN 2……………………….RESET
■ If one generator recovered
▶ DC GEN 1(2) FAULT procedure ( A24.13 ) …. APPLY
■ If no generator recovered
▶ HYD GREEN PUMP ………….OFF
▶ TRU ……………………………….ON
■ If no TRU arrow light
▶ MAX IMC FLIGHT TIME : 30 min
▶ TRU ………………………………OFF
▶ LAND ASAP

Question 2

SMOKE

Answer 2

■ If smoke/fumes in the cockpit
▶ CREW OXY MASKS.. DON / 100 %
▶ GOGGLES………………………………………….. SET
▶ CREW COMMUNICATIONS…………..ESTABLISH
▶ RECIRC FANS 1+2…………………………………..OFF
▶ AP ………………………………………………………. ON

Question 3

ENG 1(2) FIRE AT TAKEOFF

Answer 3

● WHEN AIRBORNE
▶ LDG GEAR…………………………….UP
● AT ACCELERATION ALTITUDE
▶ PWR MGT ………………. MCT

● AT VFTO						
■ If normal conditions				
▶ FLAPS.............................0
■ If icing conditions					
▶ FLAPS : MAINTAIN 15°				
▶ PL (affected ENG).................FI
▶ CL (affected ENG)..FTR THEN FUEL S.O.
▶ FIRE HANDLE (red light on)......PULL
Fire handle light remains on as long as a fire is detected.		
■ If fire persists after 10 s				
10 s delay enables airflow to decrease, which result in a better efficiency of the agent
▶ AGENT 1 (affected eng)..........DISCH
■ If fire persists after 30 s				
▶ AGENT 2 (affected eng)..........DISCH

Question 4

ENG 1(2) FIRE OR SEVERE MECHANICAL DAMAGE IN FLIGHT

Answer 4

▶ PL (affected ENG)…………………. FI
▶ CL (affected ENG)…….. FTR THEN FUEL S.O.
▶ FIRE HANDLE (affected ENG)…..PULL
Fire handle light remains on as long as a fire is detected.
■ If fire persists after 10 s
10 s delay enables airflow to decrease, which result in a better efficiency of the agent
▶ AGENT 1 (affected ENG)….DISCH
■ If fire persists after 30 s
▶ AGENT 2 (affected ENG)….DISCH

Question 5

ENG 1(2) FIRE OR SEVERE MECHANICAL DAMAGE ON GROUND

Answer 5

▶ AIRCRAFT…………………………STOP
Set PL on GI position, reverse as required
▶ BRAKE HANDLE………..PARKING
▶ CL 1+2………………………….FTR THEN FUEL S.O.
▶ FIRE HANDLE (affected ENG)..PULL
■ If fire persists
▶ AGENT 1 (affected ENG)……DISCH
■ If fire persists after 30 s
▶ AGENT 2 (affected ENG)…..DISCH

Question 6

ENG 1(2) FLAME OUT AT TAKEOFF

Answer 6

▶ AUTOFEATHER……………….CHECK
▶ UPTRIM………………………….CHECK
■ If no UPTRIM
▶ PL 1 + 2…………………..ADVANCE TO THE RAMP
● WHEN AIRBORNE
▶ LDG GEAR…………………………UP
■ If NO BLEEDS 1 + 2 FAULT
▶ BLEEDS 1 + 2………………….OFF
● AT ACCELERATION ALTITUDE
▶ ALT MODE……………………..SET
● AT VFTO
▶ PL 1+2 ………………………………..IN THE NOTCH
▶ PWR MGT ……………………..MCT
Disarm ATPCS, set maximum continuous power to remaining engine and prepare for
restart
▶ IAS …………………………… SET
■ If normal conditions
▶ SPD TGT ……………. CHECK VFTO
▶ FLAPS……………………………..0°
■ If icing conditions
▶ SPD TGT ………..CHECK VFTO ICING FLAPS 15°
▶ FLAPS : MAINTAIN 15°
▶ PL (affected eng)……………….FI
▶ CL (affected eng)…………..FTR THEN FUEL S.O.

Question 7

ENG 1(2) FLAME OUT IN FLIGHT

Answer 7

▶ PL (affected eng)……………………FI
■ If NH drops below 30 % (no immediate relight)
▶ CL (affected eng)…………..FTR THEN FUEL S.O.

Question 8

ENG 1+2 FLAME OUT

Answer 8

▶PF…………………………………… CAPT
▶ PL 1+2………………………………….. FI
■ If NH drops below 30 %
▶ CL 1+2………………………….FTR THEN FUEL S.O
▶ OPTIMUM SPEED……………VmHB

Question 9

EMERGENCY DESCENT

Answer 9

▶ CREW OXY MASKS…….. AS RQRD
▶ CREW COMMUNICATIONS……………..AS RQRD
▶ GOGGLES…………………….AS RQRD
▶ DESCENT………………..INITIATE
▶ PL 1+2………………………………….FI
▶ CL 1+2…………………..100% OVRD

Question 10

SEVERE ICING

Answer 10

▶ IAS : ICING BUG + 30 kt (or ICING BUG IF FLAPS 15 EXTENDED)
▶ PWR MGT …………………………MCT
▶ PL 1+2……………………….ADJUST
▶ CL 1+2………………..100% OVRD

Question 11

STALL

Answer 11

▶ CONTROL COLUMN............ PUSH
Reduce the Angle Of Attack.					 
▶ ENG PWR ......................INCREASE
■ If FLAPS 0						 
▶ FLAPS..................EXTEND TO 15	 
▶ BANK...................WINGS LEVEL

Question 12

UNRELIABLE AIRSPEED INDICATION

Answer 12

▶ AP/YD ………………………………..OFF
▶ FD …………………………………. STBY
▶ PITCH : MAINTAIN
▶ TQ : MAINTAIN
■ If at takeoff or GA below 1 500 ft
▶ PITCH………………………………..8 ° IMMEDIATELY
▶ ICING CONDITIONS……ESCAPE
Pitots obstruction may be due to the severe icing.
▶ VOLCANIC ASHES CONDITIONS……….ESCAPE
Pitots obstruction may be due to volcanic ashes.

Question 13

FLAPS UNLK

Answer 13

● Before V1
▶ TAKEOFF……………………….ABORT
● After V1
▶VR & V2 SPEED BUGS AUTOMATICALLY INCREASED
● If FLAPS UNLK during approach
▶ GO AROUND…………………PERFORM
▶VGA ……..NOT LESS THAN Vmin OPS

Question 14

PITCH CONTROL JAM AT TAKEOFF OR LANDING

Answer 14

▶ CONTROL COLUMNS ……… UNCOUPLE
▶ FREE CONTROL COLUMN ………… IDENTIFY
Only one pilot has control. He actuates only one elevator.
▶ PF…………………FREE CONTROL COLUMN SIDE

Question 15

PITCH DISCONNECT

Answer 15

▶ FREE CONTROL COLUMN(S) ……. IDENTIFY
▶ PF…….. FREE CONTROL COLUMN SIDE
▶ MAX IAS : 180 kt

Question 16

EFIS COMP

Answer 16

■ If ROL, PIT, ATT, HDG cautions appears on EFIS
▶ BOTH PFD/STBY INSTs ……….. COMPARE TO IDENTIFY AFFECTED AHRS
Standby instruments are used as a reference to identify affected EADI.
▶ ATT/HDG (affected side)….. ALTERNATE SYS
The pilot on the affected side selects the operative AHRS to supply its SGU.

Question 17

LO PITCH IN FLIGHT

Answer 17

▶ PL (affected ENG)…………………. FI

▶ CL (affected ENG)…………………… FTR THEN FUEL S.O.

Question 18

ABNORMAL PARAMETERS DURING START

Answer 18

■ If ITT tends to exceed 900 °C, or no ITT, or no NH
▶ CL (affected ENG)……….FUEL S.O.
▶ ENG START selector ……..OFF & START ABORT

Question 19

INCREASE SPEED

Answer 19

▶ IAS : ICING BUG +30kt

Question 20

PEC 1 (2) FAULT

Answer 20

■ If in short final approach (below 400 ft RA)

▶ GO-AROUND……………..PERFORM