Q.R.H.

C-295M-BR01-1

EMERGENCY PROCEDURES C-295M BR01

SMOKE OR FIRE AT THE
GENERAL

3 SMOKE EVACUATION 4
COCKPIT OR CARGO CABIN

LANDING WITH ABNORMAL LANDING FORCED

6 9 DITCHING 11
GEAR CONFIGURATION LANDING

ENGINE FIRE OR SEVERE DAMAGE ENGINE FAILURE ABORTED

13 14 14
EMERGENCIES
ON GROUND

ON GROUND AT TAKEOFF TAKEOFF

ENGINE SHUTDOWN EMERGENCY

15 15
ON GROUND BRAKING

ELECTRICAL SMOKE OR GROUND

17 18
FIRE ON GROUND EVACUATION
ENVIRONMENTAL

O.TEMP
AIR CONDITIONING SMOKE 19 PCKG BLEED 20 20
LIGHT ON
CONTROL

EXCESSIVE CABIN
RAPID DEPRESSURIZATION 21 22
DIFFERENTIAL PRESSURE

WINDSHIELD/WINDOW DOOR
LOSS OF PRESSURIZATION 23 24 25
CRACKED UNLOCKED

PITCH TRIM
ELEVATOR MISTRIM 26 26
FLIGHT

FAILURE
AUTO

AILERON / RUDDER AUTOPILOT

27 27
MISTRIM FAILURE WARNING

DUAL DC GENERATORS
28 BUS UNTIE 30 DC GEN & BUS UNTIE 33
FAILURE
ELECTRICAL

GEN HOT 35 INVERTER FAILURE 35 BAT HOT / WARM 36

ELECTRICAL SMOKE OF
AC GEN 37 DC GEN 38 39
FIRE IN FLIGHT

ELEVATOR / AILERON / AILERON / RUDDER

40 41 41 42 42
RUDDER JAMMING FLOTATION
FLIGHT CONTROLS

PITCH / AILERON / RUDDER

42 43 43 RTCS FAILURES 43
TRIM RUNAWAY

RBS FAILURE 44 RBS HEATER FAILURE 45 ELEVATOR TRIM 45

RUDDER
45 SWRS FAILURE 46 FLAPS FAIL 46 FLAPS ASYM 47
TRIM

EP-1
Q.R.H. C-295M-BR01-1

EMERGENCY PROCEDURES C-295M BR01

FUEL

FUEL LOW 48 FUEL PRESS 50 FUEL COLD 52

HYDRA HYDRAULIC QUANTITY

HYDRAULIC HOT 53 54 HYD PRESS 55
ULIC LOSS

WING AND TAIL ENGINE PROPELLER

56 57 58
ICE AND DE-ICING FAILURE DE-ICING DE-ICE
RAIN
PROTEC
TION WINDSHIELD PITOT
59 60
HEATING HEATING
LANDING

ABNORMAL LANDING LANDING GEAR EMERGENCY ANTISKID

GEAR

61 62 63
GEAR INDICATION LOWERING FAILURE

PNEUM
ATIC
BLEED O.TEMP 65 WING OVERHEAT 65

ENGINE FIRE OR SEVERE DUAL ENGINE

67 ENGINE FLAME OUT 68 68
DAMAGE IN FLIGHT FAILURE

ENGINE SHUT-DOWN IN ENGINE RESTART IN AUTOFEATHER

69 71 72
FLIGHT FLIGHT FAILURE
POWERPLANT

LOW / HIGH OIL LOW / HIGH OIL

NL OVERSPEED 72 73 73 74 74
PRESSURE TEMPERATURE

FIRE DETECTION
EEC FAILURE 75 EPC FAILURE 77 78
SYSTEM FAILURE

UNSAFE PROPELLER POWERPLANT

78 78 IEDS FAILURE 80
BRAKE INDICATION FAILURE

DISPLAY
ACP FAILURE 81 UNIT 82 IOP FAILURE 82 ICP FAILURE 83
FAILURE

EFIS CONTROL HEADING HEADING

83 84 84 ATTITUDE FAILURE 85
AVIONIC

PANEL FAILURE FAILURE MISMATCH

ATTITUDE AIRSPEED AIRSPEED

85 IVSI FAILURE 85 85 86
MISMATCH FAILURE MISMATCH

ALTITUDE CHECK PFD AVIONIC DATA

ALTITUDE FAILURE 86 86 87 87
MISMATCH WARNING LOST

EP-2
 Q.R.H. C-295M-BR01-1

GENERAL
SMOKE OR FIRE AT THE COCKPIT OR CARGO
CABIN

1. Masks and Goggles ............................................................

............................ ON / ADJUSTED / 100% / EMERGENCY ALL
Select NORMAL Oxygen when the masks and goggles
are cleared of smoke or steam.

2. MASK Pushbutton ................................................. PRESS ALL

3. Crew status ............................................................REPORT ALL
4. Cockpit Door ............................................................ CLOSE 2
5. Recirculation and Avionics Fans ................................... OFF 2
6. Passengers Signs ........................................................... ON 2
7. Pressurization Mode selector........................................MAN 2
8. Manual Rate of Change selector ..............FULL INCREASE 2
9. Manual Cabin Altitude selector ........................................UP 2
If there is not oxygen enough for all passengers,
maximum cabin altitude of 10000 ft or MEA (whichever
higher).

10. ATC / Loadmaster................................................... NOTIFY 1/2

11. Descent .........................................................................A.R. 1

CAUTION

If any on-board inflammable material is likely to fire

dangerously, consider Cargo Jettison recommendations
in AFM section 3. Refer to "CENTER OF GRAVITY
LIMITATIONS" in Section I.

EP-3
Q.R.H. C-295M-BR01-1

12. Whether the smoke has dissipated or not, land at the

nearest suitable airport. If it is possible, apply <E.P.-4>
"SMOKE EVACUATION".

CAUTION

Bear in mind that if the fire has not been extinguished,

ramp opening might intensify it.

NOTE
If it is necessary to continue the flight for a considerable
time with the aircraft depressurized, refer to "Fixed
Oxygen System - Maximum Duration" table in "Chapter
35 - Oxygen" (Volume I - Systems Description).

SMOKE EVACUATION

1. Loadmaster ............................................................. NOTIFY 1

2. Pressurization Mode selector........................................MAN 2
3. Manual Rate of Change selector ..............FULL INCREASE 2
4. Manual Cabin Altitude selector ............................. KEEP UP 2
If there is not oxygen enough for all passengers,
maximum cabin altitude of 10000 ft or MEA (whichever
higher).

5. ATC ........................................................................ NOTIFY 2

6. Descent .........................................................................A.R. 1
A. If the smoke goes-off:

7. Restore normal operation. (END)

B. If the smoke does not go-off:

7. PRESS DUMP Switch ............................................... ON 2

8. IAS .......................................................... MAX 200 KIAS 1
EP-4
 Q.R.H. C-295M-BR01-1

9. Headphones ...................................................... ADJUST 1/2

10. RH window ........................................................... OPEN 2

NOTE
If the smoke is cargo cabin mainly located, C/M-2 will
open the cockpit door and C/M-1 will order to the
Loadmaster to open the cargo door after warning the
passengers (if any) about it.

WARNING

Before opening the cargo door, the Loadmaster must fit

his Safety Harness / Parachute.

11. Re-establish normal conditions once the smoke has

been evacuated.
12. Land at nearest suitable airport.

EP-5
Q.R.H. C-295M-BR01-1

LANDING WITH ABNORMAL LANDING GEAR

CONFIGURATION

CAUTION

In case of an emergency landing consider to eject the

flares. In order to avoid damages on ground, try to
perform the jettison above 1000 ft AGL and over a safe
zone.

1. ATC / TWR ............................................................. NOTIFY 1/2

2. Crew Briefing .......................................................... IMPART 1
3. Landing gear condition ........................................ CONFIRM 1/2
A. If the nose wheel is not locked down:

After touchdown, keep the nose up with the elevator and the trim.
Retract the flaps and use reverse thrust. Minimize the use of brakes.
Lower the nose gently onto the runway while there is still effective
elevator control.

After the nose contact, keep control with differential braking.

Continue with point 4.

B. If one main landing gear leg is not locked down:

It is recommended to land with all the landing gear up.

Nevertheless, if it is necessary to land with asymmetric main landing

gear:

– Try to consume as much fuel as possible from the side with

the insecure landing gear (XFEED and pump) without
exceeding the fuel unbalance limits.
– Once the aircraft has touched down, keep the wings levelled
as long as possible.
EP-6
 Q.R.H. C-295M-BR01-1

– Once the aircraft has banked, use both reverse thrust and
brakes on the safe leg side.
– Try to keep runway-alignment with rudder, available brakes
(without antiskid) and the nose wheel steering.
Continue with point 4.

C. If both main landing gear legs are not locked down:

It is recommended to land with all the landing gear up.

If it is nevertheless necessary to land with the landing gear insecure:

– Make initial contact with the rear landing gear fairing at an

angle of 8-10º nose up.
– Try to keep runway-alignment with rudder, available brakes
and nose wheel steering.
Continue with point 4.

D. If all the landing gear is up:

Try to keep runway-alignment with rudder and asymmetric power.

Hold the nose up as long as possible.

4. Cargo cabin and Cockpit .................................... PREPARE ALL

5. Move the centre of gravity (if required).
Before entering the circuit:

6. Vref .................................................................. CALCULATE 2

7. Passengers Signs ........................................................... ON 2
8. Crew Oxygen ........................................................... CLOSE 2
9. Landing Data ....................................................... CONFIRM 1/2
10. Exterior Lights ................................................................A.R. 1
11. Emergency and Entrance Lights ..................................... ON 2
EP-7
Q.R.H. C-295M-BR01-1

12. Altimeters / Radioaltimeter ............ ADJUST __ & X-CHECK 1/2

13. Cabin Report......................................................... RECEIVE 1/2
14. N.P. "APPROACH" ............................................. PERFORM ALL
Before landing:

15. Flaps ....................................................................... 23º (DN) 2

16. LDG GR POS C/B (U3, A3) .........................................PULL 2
17. TERR INHB, GPWS INHB and AUDIO INHB Pb ..... PRESS 2
18. Bleed switches .............................................................. OFF 2
19. PRESS DUMP Switch .................................................... ON 2
20. PSHR DSARM Pushbutton ............................................A.R. 1
21. Vref ...................................................................... MAINTAIN 1
22. N.P. "BEFORE LANDING".................................. PERFORM ALL
At 150 ft:

23. "Brace for impact" ................................................. ORDER 2

With aircraft stopped:

24. Parking Brake (if required) ..........................................SET 1

25. FFLs .....................................................DIRECTLY TO OFF 2
26. Fire Handles .......... PULL AND TURN BOTH TO DISCH 1 2
27. Fuel Pumps ................................................................. OFF 2
28. Evacuation.............................................................. ORDER 1
29. MSTR ELEC (BAT and GEN) Switches ...................... OFF 1

EP-8 Revision 1
 Q.R.H. C-295M-BR01-1

FORCED LANDING

Preparation (if time enough):

CAUTION

In case of an emergency landing consider to eject the

flares. In order to avoid damages on ground, try to
perform the jettison above 1000 ft AGL and over a safe
zone.

NOTE
Wherever possible, all passengers must sit together
leaving no spaces in between each other and at the
forward part of the cargo cabin.

1. Loadmaster ............................................................. NOTIFY 1/2

2. ATC ........................................................................ NOTIFY 2
3. IFF (if no other code is required)...................................7700 2
4. Altimeters / Radioaltimeters .......... ADJUST __ & X-CHECK 1/2
5. Fuel Reduction / Transfer .................................. CONSIDER 1
6. Vref .................................................................. CALCULATE 1/2
7. Pressurization .........................................................ADJUST 2
8. Oxygen .......................................................... CLOSE / OFF 2
9. Cargo cabin and Cockpit .................................... PREPARE ALL
10. Exterior lights .................................................................A.R. 1
11. Emergency and Entrance Lights ..................................... ON 2
12. Cabin report .......................................................... RECEIVE 1/2
13. Final memory actions............................................. REVIEW 1/2

EP-9
Q.R.H. C-295M-BR01-1

Approach:
14. Passengers signs ........................................................... ON 2
15. Landing Gear .................................................................A.R. 2
Consider, depending on the chosen field for landing,
convenience to land with the landing gear extended or
retracted.
16. Flaps ....................................................................... 23º (DN) 2
17. CMDS ........................................................................... OFF 1
18. LDG GR POS C/B (U3, A3) ...........................................A.R. 2
19. TERR INHB, GPWS INHB and AUDIO INHB Pb ..... PRESS 2
20. Bleed switches .............................................................. OFF 2
21. PRESS DUMP Switch .................................................... ON 2
22. Last ATC Message ............................................ TRANSMIT 2
23. ELT ................................................................................. ON 2
24. PSHR DSARM ......................................................... PRESS 2
25. Vref ..................................................................... MAINTAIN 1
26. Fuel Pumps................................................................... OFF 2
27. Harness ...................................................................... LOCK 1/2
Imminent contact:

28. "Brace for impact" .................................................ORDER 2

Upon contact:

29. FFLs .....................................................DIRECTLY TO OFF 2*

30. Fire Handles ......................................................... PULLED 2

EP-10
 Q.R.H. C-295M-BR01-1

When the aircraft stops:

31. Fire Handles ............................. TURN BOTH TO DISCH 1 2
32. Evacuation..............................................................ORDER 1
33. Portable ELT........................................................ REMOVE LM
34. MSTR ELEC (BAT and GEN) Switch.......................... OFF 1

DITCHING
Preparation (if time enough)
NOTE
Wherever possible, all passengers must sit together
leaving no spaces in between each other and at the
forward part of the cargo cabin.
1. Loadmaster ............................................................. NOTIFY 1/2
2. ATC ........................................................................ NOTIFY 2
3. IFF (if no other code required) ......................................7700 2
4. Altimeters / Radio altimeter ........... ADJUST __ & X-CHECK 1/2
5. Reduction / Transfer of Fuel .............................. CONSIDER 1
6. VREF ................................................................ CALCULATE 1/2
7. Pressurization .........................................................ADJUST 2
8. Oxygen .......................................................... CLOSE / OFF 2
9. Cargo cabin and Cockpit .................................... PREPARE ALL
10. Exterior lights .................................................................A.R. 1
11. Emergency and Entrance Lights ..................................... ON 2
12. Cabin Report......................................................... RECEIVE 1/2
13. Final memory actions............................................. REVIEW 1/2
Approach:
14. Passengers signs ........................................................... ON 2

EP-11
Q.R.H. C-295M-BR01-1

15. Landing gear ............................................ UP / THREE "UP" 2

16. Flaps ....................................................................... 23º (DN) 2
17. LDG GR POS C/B (U3, A3) .........................................PULL 2
18. TERR INHB, GPWS INHB and AUDIO INHB Pb ..... PRESS 2
19. Bleed switches .............................................................. OFF 2
20. PRESS DUMP Switch .................................................... ON 2
21. Last ATC Message .....................................................SEND 2
22. ELT ................................................................................. ON 2
23. PSHR DSARM Pushbutton ...................................... PRESS 1
24. VREF (rate of descent as low as possible) ........... MAINTAIN 1
25. Fuel Pumps................................................................... OFF 2
26. Harness ...................................................................... LOCK 1/2
Imminent ditching:
27. "Brace for impact" .................................................ORDER 2
28. Nose Up Attitude........................... 10º APPROXIMATELY 1
Upon contact:
29. FFLs .....................................................DIRECTLY TO OFF 2*
30. Fire Handles ......................................................... PULLED 2
When the aircraft stops:
31. Fire Handles ............................. TURN BOTH TO DISCH 1 2
32. Evacuation..............................................................ORDER 1
33. Portable ELT........................................................ REMOVE LM
34. MSTR (BAT and GEN) Switches ................................ OFF 1

WARNING

Do not open any doors if (even partially) under water.

EP-12
 Q.R.H. C-295M-BR01-1

ON GROUND EMERGENCIES
ENGINE FIRE OR SEVERE DAMAGE ON GROUND

1. PLs (both) ........................................................................ GI 1

2. Parking Brake (with aircraft stopped) ........................SET 1
3. FFL (affected engine) .........................DIRECTLY TO OFF 2*

NOTE
Consider delaying foregoing action on non-affected
engine until airplane is safely positioned.

4. Fire Handle (affected engine)...... PULL / CHECK READY 2*

A. If all the fire indications go off:

5. Apply <E.P.-15> "ENGINE SHUTDOWN ON GROUND".

(END)
B. If any fire indication persists:

5. Fire Handle (affected engine) .......................................

............................ TURN TO DISCH 1 / CHECK EMPTY 2*
6. Clock ............................................................. RUNNING 2
B.1. If all fire indications go off before 30 seconds:

7. Apply <E.P.-15> "ENGINE SHUTDOWN ON

GROUND". (END)
B.2. If any fire indication persists after 30 seconds:

7. Fire Handle (affected engine) ..................................

.......................TURN TO DISCH 2 / CHECK EMPTY 2*
8. Bleed switches ................................................... OFF 2
9. Fuel Pumps ........................................................ OFF 1

EP-13
Q.R.H. C-295M-BR01-1

10. GPU Switch........................................................ OFF 2

11. Apply <E.P.-18> "GROUND EVACUATION".

ENGINE FAILURE AT TAKEOFF

If an engine failure occurs before reaching the decision speed at takeoff

(V1), apply <E.P.-14> "ABORTED TAKEOFF".

If an engine failure occurs above V1, the takeoff must be continued. The
corresponding procedure will not be applied until the takeoff is
complete, except in case of:

– ENGINE FIRE OR SEVERE DAMAGE or

– ENGINE FAILURE WITH AUTOFEATHER FAILURE

ABORTED TAKEOFF

1. PLs ................................................................................... GI 1

WARNING

If Take-Off is aborted due to engine fire or severe

damage, do not use reverse power.

2. Brakes .......................................................................... A.R. 1

3. Control Column.................... SLIGHT FORWARD FORCE 2
4. Corresponding Emergency Procedure .................APPLY 1/2
Once the Aircraft is stopped the corresponding
Emergency Procedure shall be applied.

EP-14
 Q.R.H. C-295M-BR01-1

ENGINE SHUTDOWN ON GROUND

1. PLs (both) ......................................................................... GI 1

2. Parking Brake (with aircraft stopped) .............................SET 1
3. FFL (affected engine) ........................... DIRECTLY TO OFF 2*
4. Fuel PUMP pushbutton (affected engine) . PRESS / CHECK 2
5. Electrical System ...................................... CHECK BUS TIE 2
6. Generator (affected engine) .......................................... OFF 2
7. Reduce electrical loads below 400A. Refer to <E.P.-28>
"DUAL DC GENERATORS FAILURE".

NOTE
Park and/or apply <E.P.-18> "GROUND
EVACUATION".

EMERGENCY BRAKING

1. Brakes Pressure ...................................................... CHECK 2

A. If pressure is available at the normal brakes accumulator:

NOTE
With 3000 PSI at the BKR PRESS Indicator, the
accumulator allows at least six normal brakes full
operations.

2. AntiSkid ................................................................... OFF 2

With the aircraft firmly grounded:

3. Normal Brakes................................ APPLY SMOOTHLY 1

EP-15
Q.R.H. C-295M-BR01-1

CAUTION

Do not pump the brakes to avoid accumulator pressure

fast discharging.

4. If there is no more pressure in the Normal Brakes

accumulator, continue with section B.
B. If there is no pressure available at the normal brakes
accumulator:

NOTE
Before using the emergency brakes, completely release
the pressure on normal brakes pedals.

NOTE
With 3000 psi at the EMER BKR PRESS indicator, the
accumulator allows at least six emergency brake full
operations, if correctly used.

NOTE
Antiskid is unavailable.

With the aircraft firmly grounded:

2. Emergency Brake ........................... APPLY SMOOTHLY 1

CAUTION

Do not pump the brakes to avoid accumulator pressure

fast discharging.

3. If there is no more pressure in the emergency brakes

accumulator, continue with section C.

EP-16
 Q.R.H. C-295M-BR01-1

C. If there is no pressure available at the normal brakes accumulator

and the emergency brakes accumulator:

2. Use reverse judiciously for braking, as well as for

directional control in conjunction with rudder control, and
if available, with nosewheel steering.

NOTE
If necessary, as braking aid, consider to retract the
landing gear.

ELECTRICAL SMOKE OR FIRE ON GROUND

1. Tower / Loadmaster / Ground Personnel ............ NOTIFY 1/2

2. MSTR ELEC BAT and GEN Switches (and GPU)...... OFF 2
3. Both PLs ........................................................................... GI 1
4. Parking Brake (with aircraft stopped) .............................SET 1
5. Both FFLs ............................................. DIRECTLY TO OFF 2
6. If necessary, apply <E.P.-18> "GROUND EVACUATION".

EP-17
Q.R.H. C-295M-BR01-1

GROUND EVACUATION

WARNING

If a hot brake is suspected or main wheel well fire

exists, use reverse trust to stop the aircraft, once the
aircraft is stopped do not use parking brake.

If a main wheel well fire exists, or if hot brakes are

suspected, chock the nose wheel only.

Do not approach the main wheel area when extreme

temperatures due to excessive braking are suspected.
All personnel other than the fire department should
evacuate the immediate area. The area on both sides of
the wheel will be cleared of personnel and equipment
for at least 300 feet. If conditions require personnel to
be close to any overheated wheel or tire assembly, the
approach should only be from the fore or aft of the
wheel area.

1. Parking Brake (with aircraft stopped) ........................SET 1

2. Tower, Loadmaster, Ground Personnel.............. NOTIFY 1/2
3. FFLs .....................................................DIRECTLY TO OFF 2
4. Both Fire Handles ..................................................... PULL 2
5. Both Fire Handles (if required) ...........TURN TO DISCH 1 2
6. Emergency Lights ......................................................... ON 2
7. PRESS DUMP switch .................................................... ON 2
8. Ramp............................................................................ A.R. 2
9. Evacuation..............................................................ORDER 1
10. MSTR ELEC BAT and GEN Switches (and GPU)...... OFF 1
11. Leave the aircraft ALL

EP-18
 Q.R.H. C-295M-BR01-1

ENVIRONMENTAL CONTROL
AIR-CONDITIONING SMOKE

1. Masks and Goggles ............................................................

............................ ON / ADJUSTED / 100% / EMERGENCY ALL
Select NORMAL Oxygen when the masks and goggles
are cleared of smoke or steam.
2. MASK Pushbutton ................................................. PRESS ALL
3. Crew status ............................................................REPORT ALL
4. Recirculation Fans ........................................................ OFF 2
5. ATC / Loadmaster................................................... NOTIFY 1/2
6. Corresponding Bleed Switch......................................... OFF 2
A. If the smoke decreases or does not increase (after 2 minutes):

The smoke was coming from the disconnected pack. If necessary,

apply <E.P.-4> "SMOKE EVACUATION". (END)

B. If the smoke continues to increase:

7. Bleed Switch previously turned off ............................ ON 2

8. Other Bleed Switch.................................................. OFF 2
B.1. If the smoke decreases or does not increase (after 2 minutes):

The smoke was coming from the disconnected pack. If

necessary, apply <E.P.-4> "SMOKE EVACUATION". (END)

B.2. If the smoke continues to increase:

9. Bleed Switch previously turned off ....................... ON 2

10. Land at the nearest suitable airport.
11. If necessary, apply <E.P.-4> "SMOKE
EVACUATION".
EP-19
Q.R.H. C-295M-BR01-1

PCKG BLEED

1. PCKG BLEED pushbutton ....................................... PRESS 2

A. If the "PCKG BLEED" light goes off:

2. Check that the corresponding Bleed Magnetic Indicator

is in line. The normal system conditions have been re-
established. (END)
B. If the "PCKG BLEED" light remains on:

2. Corresponding Bleed Switch ................................... OFF 2

O.TEMP LIGHT ON

1. Recirculation Fan ............................................. CHECK / ON 2

A. If the "O.TEMP" light goes off:
2. Keep flying in normal operation. (END)
B. If the "O.TEMP" light remains on:
2. Corresponding Temp. Sel. knob ...... ROTATE TO COLD 2
B.1. If the "O.TEMP" light goes off:

3. Continue with the Temperature Control in Automatic

Mode. (END)
B.2. If the "O.TEMP" light remains on:

3. O.TEMP Pushbutton ..................................... PRESS 2

B.2.1. If the "O.TEMP" light goes off:
4. Continue with the Temperature Control in Manual
Mode. (END)
B.2.2. If the "O.TEMP" light remains on:
4. Corresponding Bleed Switch ........................ OFF 2
EP-20
 Q.R.H. C-295M-BR01-1

RAPID DEPRESSURIZATION
A. If flying altitude is over 15000 ft:
1. Masks ........................................................... ON / 100% ALL
2. MASK Pushbutton ............................................ PRESS ALL
3. Crew status ...................................................... REPORT ALL
Proceed to Section B.
B. If flying altitude is below 15000 ft:

1. Passengers Signs ..................................................... ON 2

2. ATC / Loadmaster ............................................. NOTIFY 2
3. IFF (if no other code required) .................................7700 2
4. Automatic Pilot .......................................... DISENGAGE 1
5. PLs .............................................................................. FI 1
6. PRS ...................................................................... TOGA 1
7. FI SEL Pushbutton ...................................................A.R. 1
8. Descent (MAX VMO) .......................................... INITIATE 1

NOTE
Descend to 10000 ft or MEA, whichever higher.

CAUTION

If structural integrity is suspected, reduce airspeed as

much as possible (min. VREF / max. VFE). Extend flaps
23º and landing gear.

CAUTION

The Loadmaster will supply oxygen to those passengers

requiring it.

EP-21
Q.R.H. C-295M-BR01-1

EXCESSIVE CABIN DIFFERENTIAL PRESSURE

1. Pressurization Mode selector........................................MAN 2

2. Manual Rate of Change selector ..............FULL INCREASE 2
3. Manual Cabin Altitude selector ............................. KEEP UP 2
A. If it is not possible to keep the differential pressure in the green
zone:

4. Bleed Switches ........................................................ OFF 2

5. PRESS DUMP Switch (with aircraft depressurized) .. ON 2

NOTE
After landing, while reaching the parking position, open
a window. (END)

A.1. If the CABIN warning comes on:

6. Apply <E.P.-23> "LOSS OF PRESSURIZATION".

EP-22
 Q.R.H. C-295M-BR01-1

LOSS OF PRESSURIZATION

1. Masks ............................................................... ADJUSTED ALL

2. MASK Pushbutton ................................................. PRESS ALL
3. Crew status ............................................................REPORT ALL
4. Passengers Signs ........................................................... ON 2
5. ATC / Loadmaster................................................... NOTIFY 2
6. Automatic Pilot ................................................ DISENGAGE 1
7. Descent ................................................................. INITIATE 1
Descent will be performed until the CABIN annunciator
goes off or until MEA, whichever higher.

CAUTION

If structural integrity is suspected, reduce airspeed as

much as possible (min. VREF / max. VFE). Extend flaps
23º and landing gear.

CAUTION

The Loadmaster will supply oxygen to those passengers

requiring it.

8. Pressurization ...........................................................RESET 2
A. Pressurization panel "FAULT" light off:

(END)

EP-23
Q.R.H. C-295M-BR01-1

B. Pressurization panel "FAULT" light on:

9. Pressurization............................ OPERATE MANUALLY 2

NOTE
If it is not possible to maintain a Cabin Altitude lower
than 10000 ft, refer to "Fixed Oxygen System -
Maximum Duration" table in "Chapter 35 - Oxygen"
(Volume I - Systems Description).

WINDSHIELD/WINDOW CRACKED

NOTE
Both outer and inner layers are fail-safe designed,
therefore one of them can withstand the maximum
certified differential pressure.

1. Cracked layer....................................................... IDENTIFY 1/2

Identify by any possible mean if the inner layer is
cracked. A good way to identify if the inner layer is
cracked is to try to touch the crack with the finger nail or
with a pen.

A. If the inner layer is not cracked:

2. Continue flight normally. (END)

B. If the inner layer is cracked:

2. Outer layer integrity cannot be assured. Consider

landing at the nearest suitable airport.

EP-24
 Q.R.H. C-295M-BR01-1

DOOR UNLOCKED

1. Passengers Signs (No Smoke and Seat Belts)............... ON 2

A. If the crew door/ramp door light is on:

2. The aircraft will depressurize automatically. Apply <E.P.-

21> "RAPID DEPRESSURIZATION" and land at the
nearest suitable airport". (END)
B. If the emergency door/paratroops door light is on:

2. Aircraft ...................................... LEVEL AND STABILIZE 2

3. Safety Harness / Parachute....................................... FIT LM
4. Door Closed ....................................................... CHECK LM
B.1. The light goes off:

5. Continue flight normally. (END)

B.2. If the light remains on, or both door and locking device cannot
be checked:

5. Cabin Differential Pressure ..... MAINTAIN POSITIVE 2

6. Assess whether it is advisable to keep flying or land
at the nearest suitable airport. 1

EP-25
Q.R.H. C-295M-BR01-1

AUTO FLIGHT
ELEVATOR MISTRIM

1. Control Columns ...........................................HOLD FIRMLY 1/2

2. Elevator re-trim ..............................................................A.R. 1
3. If necessary, autopilot can be reengaged after manually
trimming the airplane.

PITCH TRIM FAILURE

1. Control Columns ...........................................HOLD FIRMLY 1/2

2. Elevator re-trim ..............................................................A.R. 1
3. If necessary, autopilot can be reengaged after manually
trimming the airplane.

EP-26
 Q.R.H. C-295M-BR01-1

AILERON / RUDDER MISTRIM

A. If "MISTRIM (L WING DN)" or "MISTRIM (R WING DN)" is

displayed:

1. Control Wheels ........................................HOLD FIRMLY 1/2

2. Normal Trim..............................................................A.R. 1
B. If "MISTRIM (TRIM NOSE LEFT)" or "MISTRIM (TRIM NOSE
RIGHT)" is displayed:

1. Pedals .....................................................HOLD FIRMLY 1/2

2. Normal Trim..............................................................A.R. 1

AUTOPILOT FAILURE WARNING

1. Automatic Pilot ................................. DISENGAGE / CHECK 1/2

2. Automatic Pilot ...............................................................A.R. 1/2

EP-27
Q.R.H. C-295M-BR01-1

ELECTRICAL
DUAL DC GENERATORS FAILURE

1. BAT BUS TIE Selector ................................................ OFF 2

2. Generators.................... RESET / ON (MAX 2 ATTEMPTS) 2
A. If no generator is recovered:

3. TRU Selector .............. 1 (if M.I. not in line, rotate to 2) 2

4. BAT BUS TIE Selector .............................................. ON 2
5. Hydraulic Pumps ........................................... MAN / A.R. 2
When necessary, use only the hydraulic pump
corresponding to the side where TRU is connected
(1 or 2).

6. GEN Switches (1 and 2) .......................................... OFF 2

7. Land at the nearest suitable airport. Reduce electrical
loads below 300 A. Refer to "LIST OF ELECTRICAL
LOADS" at the end of this procedure. (END)
B. If only one generator is recovered:

3. Unrecovered Generator........................................... OFF 2

4. BAT BUS TIE Selector .......................................... AUTO 2
If the BAT BUS TIE magnetic indicator is not in line,
the BUS UNTIE warning will come on. Set the BAT
BUS TIE selector to ON. If the magnetic indicator is
still not in line, set it to OFF and press the GEN BUS
TIE pushbutton.

5. Hydraulic Pumps ........................................... MAN / A.R. 2

When necessary, use only the hydraulic pump
corresponding to the operative generator (1 or 2).

EP-28
 Q.R.H. C-295M-BR01-1

6. Reduce electrical loads below 400 A. Refer to "LIST OF

ELECTRICAL LOADS" at the end of this procedure.
(END)
C. If both generators are recovered:

3. BAT BUS TIE Selector .......................................... AUTO 2

(END)

LIST OF ELECTRICAL LOADS

Hydraulic pump (#1 or #2) (under load) 60 (130) A

Windshield Heating (1) 44 A

Recirculation fan (1) 35 A

Revision 1 EP-29
Q.R.H. C-295M-BR01-1

BUS UNTIE

1. Bus bar RESET button (once only) .......................... PRESS 2

A. If the BAT-GEN magnetic indicator goes to in-line position:

Continue normal operation. (END)

B. If the BAT-GEN magnetic indicator remains in crossline position:

2. BAT BUS TIE Selector .............................................. ON 2

B.1. If the BAT BUS TIE Magnetic Indicator moves to in-line
position:

3. Reduce electrical loads to below 400 A. Refer to

"LIST OF ELECTRICAL LOADS" in <E.P.-28>
"DUAL DC GENERATORS FAILURE". (END)
B.2. If the BAT BUS TIE Magnetic Indicator does not go to in-line
position:

3. BAT BUS TIE Selector ....................................... OFF 2

4. GEN BUS TIE Pushbutton ............................ PRESS 2
5. Land at nearest suitable airport. If the battery has
been disconnected or discharged, V/UHF, windshield
and pitot heating on the affected side will not be
available. Autopilot disconnection will occur.
Consequently:
– Transfer the functions between C/M-1 and
C/M-2 if No. 1 Battery bus has failed.
– Avoid icing zones.
– Match the PL without indication with the other.

EP-30
 Q.R.H. C-295M-BR01-1

Other systems requiring special actions will have

also been lost:
– If BAT bus 1 has been lost:

CAUTION

Ice Detector has been lost. If ice conditions are

suspected, apply the next step to recover the system.

A. Inverters: Main inverter has been lost;

Apply <E.P.-35> "INVERTER FAILURE".

B. Communications: IOP 1 has been lost;

Apply <E.P. -82> "IOP FAILURE".

C. Flaps: Land with the available flaps

(according to cut-off level) with VREF+ 1kt
for each degree below 25º. Press the
EGPWS FLAP OVRD pushbutton to avoid
a nuisance warning. Refer to "LANDING
DISTANCES TABLE" to ensure that the
selected airport is landing convenient.

D. Landing Gear: Apply <E.P.-62>

"LANDING GEAR EMERGENCY
LOWERING". There is a valid landing gear
indication.

E. Trim: Only normal rudder, standby aileron

and standby elevator trims are operative.

F. Engines: The igniters in both engines are

inoperative. Then, in flight, the engines
cannot be restarted and autoignition is not
operative.

G. Hydraulic Pumps: Hydraulic pumps No. 1

and No. 3 have been lost. Use the
remaining hydraulic pump for braking.
Nose wheel steering is lost.
EP-31
Q.R.H. C-295M-BR01-1

H. EFIS: C/M-1 PFD and C/M-2 ND have

been lost. In C/M-1 side, to display PFD
information in ND, switch off PFD in EFIS
control panel.

(END)
– If BAT bus 2 has been lost:
A. Flaps: Land with the available flaps
(according to cut-off level) with VREF + 1kt
for each degree below 25º. Press the
EGPWS FLAP OVRD pushbutton to avoid
a nuisance warning. Refer to "LANDING
DISTANCES TABLE" to ensure that the
selected airport is landing convenient.

B. Trim: Only standby rudder, normal aileron

and normal elevator trims are operative.
Trim indication is lost.

C. Pressurization: Automatic mode is lost,

operate manually.

D. Engines: The engines cannot be started

in-flight.

E. Hydraulic Pumps: Hydraulic pumps No.2

and No.3 have been lost. Use the
remaining hydraulic pump for landing gear
extension and normal braking (without
brake pressure, hydraulic pressure and
hydraulic quantity indications) and for
nosewheel steering.

Apply <E.P.-62> "LANDING GEAR

EMERGENCY LOWERING".

EP-32
 Q.R.H. C-295M-BR01-1

DC GEN & BUS UNTIE

1. Affected Generator ........ RESET / ON (MAX 2 ATTEMPTS) 2

A. If the "GEN" magnetic indicator goes to in-line position and the
annunciator goes off:

(END)

B. If the "GEN" magnetic indicator goes to in-line position and the

"BUS UNTIE" annunciator persists:

2. Apply <E.P.-30> "BUS UNTIE". (END)

C. If the "GEN" magnetic indicator remains at crossline position and
both annunciators persist:

2. Affected Generator .................................................. OFF 2

C.1. If the BAT BUS TIE Magnetic Indicator is at in-line position:

3. Corresponding bus RESET button ................ PRESS 2

C.1.1. If the BAT-GEN Magnetic Indicator goes to in-line position:

4. Proceed to step 7 of section C.2.2.

C.1.2. If the BAT-GEN Magnetic Indicator remains at crossline
position:

The corresponding generator bus and its associated

equipment have been lost:

– If GEN bus 1 has been lost: Engine Air Inlet De-Icing,

Fuel Indication, Windshield Wiper, propeller deicing,
AOA heater and Pack have been lost on the left side.
Front Anti-Skid, ramp operation, Weather Radar and
Wing and Tail De-Icing AUTO Mode have also been
lost.

EP-33
Q.R.H. C-295M-BR01-1

– If GEN bus 2 has been lost: Engine Air Inlet De-Icing,

Fuel Indication, Windshield Wiper, propeller deicing,
AOA heater, aux pitot and Pack have been lost on the
right side. Rear Anti-Skid, Hydraulic Pump No. 3, and
both Wing and Tail De-Ice MAN Mode have also been
lost.
4. Proceed to step 7 of section C.2.2.
C.2. If the BAT BUS TIE Magnetic Indicator is at crossline position:

3. BAT BUS TIE Selector ......................................... ON 2

C.2.1. If the BAT BUS TIE Magnetic Indicator goes to in-line
position:

4. Proceed to section C.1.2.

C.2.2. If the BAT BUS TIE Magnetic Indicator remains at crossline
position:

NOTE
The related BAT BUS has been lost. After finishing this
procedure, proceed to step 5 of section B.2. in <E.P.-
30> "BUS UNTIE".

4. BAT BUS TIE Selector.................................. OFF 2

5. GEN BUS TIE Pushbutton ....................... PRESS 2
6. Hydraulic Pumps ................................ MAN / A.R. 2
When necessary, connect only the hydraulic
pump corresponding to the operative
generator (1 or 2).

7. Reduce electrical loads below 400 A. Refer to

"LIST OF ELECTRICAL LOADS" in <E.P.-28>
"DUAL DC GENERATORS FAILURE".

EP-34
 Q.R.H. C-295M-BR01-1

GEN HOT

1. Affected Generator ....................................................... OFF 2

2. Bat Bus Tie Magnetic Indicator ...................CHECK IN LINE 2
If the BAT BUS TIE magnetic indicator is not in line, set
the selector to ON. If still not in line, set the BAT BUS
TIE selector to OFF and press the GEN BUS TIE
pushbutton.

3. Hydraulic Pumps................................................. MAN / A.R. 2

When necessary, connect only the hydraulic pump
corresponding to the operative generator (1 or 2).

4. Reduce electrical loads below 400 A. Refer to "LIST OF

ELECTRICAL LOADS" in <E.P.-28> "DUAL DC
GENERATORS FAILURE".
If the "GEN HOT" warning goes off (after a few minutes):

5. Affected Generator (once only) ........................ RESET / ON 2

6. Disconnected Electrical Loads ............................. REPLACE 2
7. Hydraulic Pumps.........................................................AUTO 2

NOTE
If the GEN HOT warning comes on again, apply the
procedure again only up to step 4.

INVERTER FAILURE

1. MAIN Inverter Pushbutton ....................................... PRESS 2

2. STBY Inverter Pushbutton ....................................... PRESS 2

EP-35
Q.R.H. C-295M-BR01-1

BAT HOT/WARM

A. "BAT HOT" warning on:

1. Affected Battery (above 150 ºF) ........................... OFF 2

(END)

B. If only "BAT WARM" warning is on:

1. Monitor the battery rate of recharge 2

B.1. If the batteries recharging rate is normal:

Monitoring the batteries rate of recharge (each 2 minutes at

least) and temperature. (END)

B.2. If the batteries rate of recharge is abnormal:

2. Affected Battery ................................................. OFF 2

3. Let the affected battery cool down for 5 minutes after
the WARM light has gone off.
4. Affected Battery ................................................... ON 2

NOTE
If the WARM light comes on again, disconnect the
affected battery for the rest of the flight.

EP-36
 Q.R.H. C-295M-BR01-1

AC GEN

NOTE
The display of the AC GEN annunciator in the IEDS,
below 70% NP is normal as the alternator is not
connected up to this value.

CAUTION

After finishing this procedure, continue monitoring the

engine of the affected AC GEN for the rest of the flight.
If smoke or sparks are detected, immediately follow up
<E.P.-15 / E.P.-69> "ENGINE SHUTDOWN".

1. Propeller (affected side) ............... CHECK UNFEATHERED 2

2. ENG AIR INLET and PROPELLER pushbutton (affected
side) ....................................... RESET (MAX 2 ATTEMPTS) 2
A. If "AC GEN" does not come on again:

3. Continue flight in normal operation.

(END)

B. If "AC GEN" and associated "P/D-ICE" and / or "E/D-ICE"

annunciators come on again:

3. Apply <E.P.-58> "PROPELLER DE-ICE" and / or

<E.P.- 57> "ENGINE DE-ICING".

NOTE
If the other AC Generator also fails and cannot be
recovered, the Distributor Valves heaters of the Wing
and Tail De-Icing system will be lost as well as the
Propeller De-Icing system.

Revision 1 EP-37
Q.R.H. C-295M-BR01-1

DC GEN

1. Affected Generator ........ RESET / ON (MAX 2 ATTEMPTS) 2

A. If the GEN magnetic indicator is in line:

Operate normally. (END)

B. If the GEN magnetic indicator is in the crossline position:

2. Affected Generator .................................................. OFF 2

3. BAT BUS TIE Selector ............................ CHECK AUTO 2
Check that the BAT BUS TIE magnetic indicator is in
line. If not in line, the IEDS BUS UNTIE annunciator
is on. Set the BAT BUS TIE Selector to ON. If still
not in line, set it to OFF and press the GEN BUS TIE
Pushbutton.

4. Hydraulic Pumps ........................................... MAN / A.R. 2

When necessary, connect only the hydraulic pump
corresponding to the operative generator (1 or 2).

5. Reduce electrical loads below 400 A. Refer to "LIST OF

ELECTRICAL LOADS" in <E.P.-28> "DUAL DC
GENERATORS FAILURE"

EP-38
 Q.R.H. C-295M-BR01-1

ELECTRICAL SMOKE OR FIRE IN FLIGHT

1. Masks and Goggles ............................................................

............................ ON / ADJUSTED / 100% / EMERGENCY ALL
Select NORMAL Oxygen when the masks and goggles
are cleared of smoke or steam.

2. MASK Pushbutton ................................................. PRESS ALL

3. Crew status ............................................................REPORT ALL
4. Recirculating Fans ........................................................ OFF 2
5. Automatic Pilot (if engaged) ............................ DISENGAGE 2
6. BAT BUS TIE Selector.................................................. OFF 2
7. BAT and GEN switches (at the pilot's choice)............... OFF 2
A. If the smoke or fire signs go out:

8. Leave the battery and generator off for the rest of the
flight. (END)
B. If the smoke or fire signs persist:

8. BAT and GEN switches disconnected ....................... ON 2

9. BAT and GEN switches (opposite side) .................. OFF 2
10. Land at the nearest suitable airport.
11. Apply <E.P.-3> "SMOKE OR FIRE AT THE COCKPIT
OR CARGO CABIN".

EP-39
Q.R.H. C-295M-BR01-1

FLIGHT CONTROL
ELEVATOR JAMMING

NOTE
If possible, maintain both flap and speed configuration
at the failure moment.

1. Automatic Pilot (if engaged) ........................ DISENGAGE 1

2. Control Columns................. FORCE AGAINST JAMMING 1/2
A. If the jamming goes out:

3. Continue normal operation. (END)

B. If the jamming persists:

3. Control Columns .................................. HOLD FIRMLY 1/2

4. PITCH Control Disengage Selector................... UNTIE 2*
5. Pilots Functions (depending on free column) .... A.R. 1/2
6. Configuration and Normal Trim ........................... A.R. PF

NOTE
Hold both Control Columns for the rest of the flight.

7. Land at nearest suitable airport with less crosswind and

turbulence, with flaps at 15º and VREF + 10 kts or at
minimum VTH, whichever higher. Press the EGPWS
FLAP OVRD pushbutton to avoid a nuisance warning.
Refer to LANDING DISTANCE TABLE.

EP-40
 Q.R.H. C-295M-BR01-1

AILERON JAMMING

1. Automatic Pilot (if engaged) ........................ DISENGAGE 1

2. IAS (if possible)............................................. MAX 150 kts 1
A. If the jamming goes out:

3. Continue normal operation. (END)

B. If the jamming persists:

3. Control Wheels ..................................... HOLD FIRMLY 1/2

4. ROLL Control Disengage Selector.................... UNTIE 2*
5. Pilots functions (depending on free column) ..... A.R. 1/2
6. Normal Trim ........................................................... A.R. PF

CAUTION

Hold both wheels during the rest of the flight. Limit bank
angle to 15º. Use the rudder as necessary.

7. Land at nearest suitable airport with less crosswind and

turbulence, with flaps at 15º and VREF + 10 kts or at
minimum VTH, whichever higher. Press the EGPWS
FLAP OVRD pushbutton to avoid a nuisance warning.
Refer to LANDING DISTANCE TABLE.

RUDDER JAMMING

1. Automatic Pilot (if engaged) ............................ DISENGAGE 1

2. Use asymmetrical power to counteract sideslip .............A.R. 1
3. Land at nearest suitable airport with less crosswind and
turbulence. Check crosswind, land on the most suitable
runway.

EP-41
Q.R.H. C-295M-BR01-1

AILERON FLOTATION

1. Automatic Pilot (if engaged) ............................ DISENGAGE 1

2. IAS ................................................................... MAX 150 kts 1
3. Hydraulic Pressure .................................................. CHECK 2
4. Flaps ..................................................................... 10º or 15º 2

WARNING

Do not use the aileron trim tabs.

5. Land at nearest suitable airport with less crosswind and

turbulence. If landing in crosswind, it is advisable that it be
on the side of the floating aileron. Use flaps at 15º and VREF
+ 10 kts or minimum VTH, whichever higher. Press the
EGPWS FLAP OVRD pushbutton to avoid a nuisance
warning. Refer to "LANDING DISTANCE TABLE".

RUDDER FLOTATION

1. Automatic Pilot (if engaged) ............................ DISENGAGE 1

2. Control with banking ......................................................A.R. 1

NOTE
Do not use the rudder trim.

PITCH TRIM RUNAWAY

1. R, L ELEV Selectors guard on STBY TRIMS panel .. LIFT 1

2. R, L ELEV Selectors on STBY TRIMS panel ............. A.R. 1

EP-42
 Q.R.H. C-295M-BR01-1

AILERON TRIM RUNAWAY

1. AILERON Selector guard on STBY TRIMS Panel ........ LIFT 1

2. AILERON Selector on STBY TRIMS Panel ...................A.R. 1

RUDDER TRIM RUNAWAY

1. RUDDER Selector guard on STBY TRIMS Panel......... LIFT 1

2. RUDDER Selector on STBY TRIMS Panel ....................A.R. 1

RTCS FAILURES

A. If the "RTCS EXP" caution comes on:

1. For landing, choose a runway with less than 20 kts of
crosswind and land with flaps 15º at VREF + 10 or
minimum VTH, whichever higher. Press the EGPWS
FLAP OVRD pushbutton to avoid a nuisance warning.
Refer to "LANDING DISTANCE TABLE".
B. If the "RTCS MAN" caution comes on:

1. Continue flight normally.

B.1. If "RTCS AUTO" caution comes on:

Proceed from point 4 of section C.1.

C. If the "RTCS AUTO" caution comes on:

1. AIRSPEED SEL Selector .........................................A.R. 2

SPEED SELECTOR POSITION

Below 140 KIAS LOW

Between 140 and 200 KIAS MED

Above 200 KIAS HIGH

EP-43
Q.R.H. C-295M-BR01-1

NOTE
Avoid rudder pedals sudden or big displacements as
well as sideslip.

2. For landing, choose a runway with less than 20 kts of

crosswind and land with flaps 15º at VREF + 10 or
minimum VTH, whichever higher. Press the EGPWS
FLAP OVRD pushbutton to avoid a nuisance warning.
Refer to LANDING DISTANCE TABLE.
C.1. If the "RTCS MAN" caution comes on next:

3. AIRSPEED SEL selector..................................AUTO 2

4. Rudder travel limits (with IAS < 140 kts) ....... CHECK 1/2
5. Land with flaps 15º and VREF + 10 or minimum VTH,
whichever higher. Press the EGPWS FLAP OVRD
pushbutton to avoid a nuisance warning. Refer to
LANDING DISTANCE TABLE.

RBS FAILURE

1. ACTR Pushbutton .......................................... PRESS / OFF 2

2. IAS (until landing secured).................... MIN VREF + 35 KIAS 1

EP-44
 Q.R.H. C-295M-BR01-1

RBS HEATER FAILURE

1. STBY HEATER pushbutton ........................... PRESS / SEC 2

If the "RUD HT" caution comes on again:

2. Decrease the aircraft altitude below the icing level. If this is

not possible, make frequent Rudder movements to avoid
jamming of the actuator due to ice build up.

ELEVATOR TRIM

If the RTCS AUTO caution also comes on, all the Auto trim Modes have
been lost, along with Normal Trimming from the control columns PITCH
TRIM selectors.

1. Normal Trim ............................................................. CHECK 1

2. R, L ELEV Selectors on STBY TRIMS panel .................A.R. 1

CAUTION

Operate both elevator trim selectors symmetrically.

RUDDER TRIM

If the "RTCS AUTO" caution also displays, all the Auto trim Modes have
been lost, along with Normal Trimming from the pedestal RUDDER
TRIM selector.

1. Normal Trim ............................................................. CHECK 1

2. RUDDER Selector on STBY TRIMS Panel ....................A.R. 1

NOTE
If an engine fails at high power, the force on pedals will
be noticeably greater.

EP-45
Q.R.H. C-295M-BR01-1

SWRS FAILURE

Avoid flight conditions close to stall.

1. PSHR DSARM pushbutton ...................................... PRESS 2

If both "1 SWRS" and "2 SWRS" cautions are displayed in the IEDS:

The Stick-Pusher, both Stick-Shakers and acoustic stall warning have

been lost.

FLAPS FAIL

If the "FLAP ASYM" warning comes on at the same time, apply <E.P.-
47> "FLAPS ASYM". (END)

1. Hydraulic Pressure .................................................. CHECK 2

2. Flaps RESET switch .................................................RESET 2
A. If caution goes off:

3. Continue flight operating normally. (END)

B. If caution comes on again:

3. Flaps Lever............. ACCORDING TO THE INDICATOR 2

4. Land at the nearest suitable airport at VREF + 1kt for
each flaps degree estimated below 25º, or at minimum
VTH, whichever higher. Press the EGPWS FLAP OVRD
pushbutton to avoid a nuisance warning. Do not land
with tail wind if the flaps setting is below 15º. Refers to
LANDING DISTANCE TABLE.

EP-46
 Q.R.H. C-295M-BR01-1

FLAPS ASYM

1. Automatic Pilot (if engaged) ............................ DISENGAGE 1

2. IAS ................................................................... MAX 175 kts 1
A. If the flaps lever has been operated without hydraulic power:

3. Flaps Lever............. ACCORDING TO THE INDICATOR 2

4. FLAPS SYS C/B (U1, A5) (one attempt only) .........PULL 1
5. Hydraulic Pumps ............................................ MAN / ON 2
30 seconds after pulling out the circuit breaker:

WARNING

Be prepared for possible losses of lateral trim due to

real asymmetry.

6. FLAPS SYS C/B (U1, A5) .................................. PRESS 1

If the FLAP ASYM warning goes off, continue normal
operation.

If it does not go off, continue at Section B.

B. If the flaps lever has been operated with hydraulic power:

3. Land at the nearest suitable airport at VREF + 1kt per

flaps degree below 25º, or at minimum VTH, whichever
higher. Press the EGPWS FLAP OVRD pushbutton to
avoid a nuisance warning. Refer to LANDING
DISTANCE TABLE.

EP-47
Q.R.H. C-295M-BR01-1

FUEL
FUEL LOW

1. Corresponding Fuel PUMPS pushbutton ................. CHECK 2

2. Fuel Quantity ........................................................... CHECK 2

CAUTION

Perform periodical checking of the fuel indications.

CAUTION

In case of potential leakage, detected or not by the

crew, take every caution while using reverse thrust
during landing to prevent any potential fire.

CAUTION

Avoid sudden manoeuvres, limiting both maximum pitch

and sideslip.

The minimum fuel quantity permitted for a Baulked

Landing and the following Go Around and Landing is
180 lb (80 kg) in each main tank.

A. If a fuel leakage is suspected:

CAUTION

If the leakage is big-enough follow up <E.P.-69>

"ENGINE SHUTDOWN IN-FLIGHT".

EP-48
 Q.R.H. C-295M-BR01-1

3. Corresponding Fuel PUMPS pushbutton ........... PRESS 2

WARNING

When flying in suction mode above the altitudes stated

in the "FUEL SUCTION FEEDING ALTITUDE" table
below, be ready for a possible engine flameout.

USED FUEL Maximum Flight Altitude

JP-8 / Jet A / Jet A-1 / JP-5 13000 ft

JP-4 / Jet B 6000 ft

WARNING

Engine flameout is highly probable to occur using JP-4

or Jet B fuel types when operating in suction mode
above 13000 ft.

4. Proceed to 4 of section B.2.

B. If no fuel leakage is suspected:

3. Fuel Quantity ...................................................... CHECK 2

B.1. If crossfeed is possible:

4. X-FEED pushbutton ...................................... PRESS 2

10 seconds later:

5. Corresponding Fuel PUMPS pushbutton ...... PRESS 2

6. Land at the nearest suitable airport. (END)
B.2. If crossfeed is not possible:

4. While possible, hold a level flight attitude, monitor the

fuel quantity on the affected side and be ready for a
possible engine flameout.
5. Land at the nearest suitable airport.
EP-49
Q.R.H. C-295M-BR01-1

FUEL PRESS

CAUTION

Be ready for a possible engine flameout.

1. Corresponding Fuel PUMPS Pushbutton ................ CHECK 2

2. Fuel Quantity ........................................................... CHECK 2

CAUTION

If a fuel leakage is detected, disconnect the

corresponding fuel pump. If the leakage is big-enough
apply <E.P.-69> "ENGINE SHUTDOWN IN-FLIGHT".
(END)

CAUTION

In case of a possible fuel leakage that has not been

detected by the crew, take extreme care while using the
reverse thrust during landing to prevent any potential
fire.

3. X-FEED Pushbutton ................................................ PRESS 2

10 seconds later:

4. Corresponding Fuel PUMPS Pushbutton ................ PRESS 2

A. If the "FUEL P" warning remains on:

5. Corresponding Fuel PUMPS Pushbutton ........... PRESS 2

EP-50
 Q.R.H. C-295M-BR01-1

10 seconds later:

6. X-FEED Pushbutton ........................................... PRESS 2

If no fuel leakage is confirmed, disregard the
warning. Continue normal operation monitoring
engine parameters. (END)

B. If the "FUEL P" warning goes off:

5. X-FEED Operation ........ CONTINUE WHILE POSSIBLE

Keep on mind the maximum allowed asymmetry.
Otherwise, press the X-FEED to continue operation
using suction, taking note of both time and flight
altitude if the recommended operational altitude for
this type of operation is overcome.

WARNING

When flying in suction mode above the altitudes stated

in the "FUEL SUCTION FEEDING ALTITUDE" table
below, be ready for a possible engine flameout.

USED FUEL Maximum Flight Altitude

JP-8 / Jet A / Jet A-1 / JP-5 13000 ft

JP-4 / Jet B 6000 ft

WARNING

Engine flameout is highly probable to occur using JP-4

or Jet B fuel types when operating in suction mode
above 13000 ft.

EP-51
Q.R.H. C-295M-BR01-1

FUEL COLD

1. Fuel Temperature .................................................... CHECK 2

A. If the fuel temperature is 3ºC or above:

2. Continue normal operation monitoring both engines

operation. (END)
B. If the fuel temperature is below 3ºC:

2. Corresponding PL ......................................... ADVANCE 1

If possible, descent to warmer altitudes.

3. Check the FUEL COLD annunciator 2

If the annunciator remains on, the affected engine
indications become abnormal, apply <E.P.-69>
"ENGINE SHUTDOWN IN-FLIGHT".

EP-52
 Q.R.H. C-295M-BR01-1

HYDRAULIC
HYDRAULIC HOT

CAUTION

Complete the change of flap configuration if initiated.

1. Hydraulic Pumps.................................................. MAN/OFF 2

When the annunciator has gone out:

2. Hydraulic Pumps (one at each time) ........................ CHECK 2

NOTE
Do not use any pump which gives an overpressure
reading (yellow arc) during rest of flight.

When hydraulic pressure is necessary:

3. Hydraulic Pump Operative (only one) .................. MAN / ON 2

NOTE
Do not operate both Flaps and Landing Gear
simultaneously.

If the "HYD HOT" annunciator comes on again:

CAUTION

Complete the change of flap configuration if initiated.

4. Hydraulic Pump ................................................. MAN / OFF 2

EP-53
Q.R.H. C-295M-BR01-1

If the Hydraulic System gets out of order due to the "HYD HOT"
caution:

5. Apply <E.P.-62> "LANDING GEAR EMERGENCY

LOWERING"
6. Land at the nearest suitable airport at VREF + 1kt for each
degree the flaps are below 25º, or at minimum VTH,
whichever is higher. Press the EGPWS FLAP OVRD
pushbutton to avoid a nuisance warning. Refer to LANDING
DISTANCE TABLE.

CAUTION

Nose wheel steering will not be available.

7. Apply <E.P.-15> "EMERGENCY BRAKING"

HYDRAULIC QUANTITY LOSS

CAUTION

Complete the change of flap configuration if initiated.

1. Hydraulic Pumps ............................................... MAN/OFF 2

2. Antiskid ......................................................................... OFF 2
3. Apply <E.P.-62> "LANDING GEAR EMERGENCY
LOWERING" (when necessary)
4. Land at the nearest suitable airport at VREF + 1 kt per flaps
degree below 25º, or at minimum VTH, whichever higher.
Press the EGPWS FLAP OVRD pushbutton to avoid a
nuisance warning. Refer to "LANDING DISTANCE TABLE".

EP-54
 Q.R.H. C-295M-BR01-1

CAUTION

Nose wheel steering will not be available. Antiskid will

not be available. Hydraulic pressure at normal brakes
accumulator will normally start to decrease
progressively. Hydraulic pressure at emergency brakes
accumulator will be available until being used.

5. Apply <E.P.-15> "EMERGENCY BRAKING"

HYD PRESS

A. If all three "HYD P" annunciators come on:

1. Apply <E.P.-54> "HYDRAULIC QUANTITY LOSS".

(END)
B. If one or two "HYD P" annunciators come on:

1. Operative Hydraulic Pumps ............................ MAN / ON 2

NOTE
Do not operate both Flaps and Landing Gear
simultaneously with only one Hydraulic Pump operative.

2. Affected Hydraulic Pump/s ....CHECK DISCONNECTED 2

B.1. If both Pressure and Quantity of Hydraulic Fluid are
decreasing:

3. Apply <E.P.-54> "HYDRAULIC QUANTITY LOSS".

(END)
B.2. If both Pressure and Quantity of Hydraulic Fluid remain
normal:

When hydraulic pressure is not required:

3. Hydraulic Pumps Operative ............................... OFF 2

EP-55
Q.R.H. C-295M-BR01-1

ICE AND RAIN PROTECTION

WING AND TAIL DE-ICING FAILURE

A. If the "W&T D-ICE" caution comes on with/without "W&T DGRD":

1. SOV Pushbutton (under guard) .......................... PRESS 1

NOTE
The Wing and Tail De-icing System has been lost, as
well as the Pressurization System Automatic Control.

2. Pressurization System ... OPERATE IN MANUAL MODE 2

3. Leave the icing conditions as soon as possible.
Maintain the limitations of the “MINIMUM
AIRSPEEDS IN ICE FORMATION CONDITIONS”.

With ice accretion on aircraft surfaces, landing with

23º must be performed at VREF+ 30 KIAS or at VTH+
5 KIAS, whichever is higher. The landing distances
shown in the “LANDING DISTANCE TABLE” will
increase in 35% over the corresponding values.
(END)

B. If only the "W&T DEGRD" caution comes on:

1. De-Icing Mode Selector ...........................................MAN 1

2. De-Icing Supervision Switch ................................... MON 1
3. Wing and Tail De-Icing .. OPERATE IN MANUAL MODE 1
Press each Manual De-Icing Pushbutton for 6
seconds in a sequential way leaving a 1 to 3 minutes
break, depending on the icing accretion observed
visually. (END)

EP-56
 Q.R.H. C-295M-BR01-1

B.1. If any ON light does not come on or stays permanently on:

4. Do not operate the faulty pushbutton.

5. Leave the icing conditions as soon as possible.
Maintain the limitations of the “MINIMUM
AIRSPEEDS IN ICE FORMATION
CONDITIONS”.

With ice accretion on aircraft surface, landing with

23º flaps must be performed at VREF+ 30 KIAS or
at VTH+ 5 KIAS, whichever higher. Landing
distances shown in the "LANDING DISTANCES
TABLE" will increase in 35% over the
corresponding values with 23º flaps and ice-free
aircraft.

ENGINE DE-ICING

A. If both "E/D-ICE" caution come on simultaneously with the "W&T

D-ICE" caution:

1. SOV pushbutton (under guard) .......................... PRESS 1

NOTE
The Wing and Tail De-Icing system has been lost as
well as the Pressurization Automatic Control.

2. Engine Inlet De-Icing pushbuttons (sequentially) RESET 1

NOTE
Reset first the related to one engine and make sure that
de-icing and engine operate correctly before doing the
same on the other side.

3. Leave icing conditions as soon as possible.

Maintain the limitations of the "MINIMUM
AIRSPEEDS IN ICE FORMATION CONDITIONS".
EP-57
Q.R.H. C-295M-BR01-1

With ice accretion detected on aircraft surfaces,

landing with 23º flaps must be performed at VREF+ 30
KIAS or at VTH+ 5 KIAS, whichever higher. Landing
distances shown in the "LANDING DISTANCES
TABLE" will be increased by 35% over the
corresponding values with 23º flaps and aircraft ice-
free.

4. Pressurization System ... OPERATE IN MANUAL MODE 2

A.1. If any "E/D-ICE" annunciator comes on again:

Proceed to section C.

B. If both "E/D-ICE" annunciator come on:

1. Leave icing condition as soon as possible. (END)

C. If only one "E/D-ICE" caution comes on:

1. Corresponding Engine Inlet De-Icing PushbuttonPRESS 1

2. Leave icing conditions as soon as possible.

PROPELLER DE-ICE

A. If both "1P/D-ICE" and "2P/D-ICE" come on simultaneously:

1. Propeller de-icing pushbuttons ........................... PRESS 1

2. Leave icing conditions as soon as possible. (END)
B. If only one "P/D-ICE" caution comes on:

1. Corresponding Propeller De-icing pushbutton .... PRESS 1

2. Leave icing conditions as soon as possible.
3. If excessive vibrations are denoted, feather the propeller
and, if persist, apply <E.P.-15 / E.P.-69> "ENGINE
SHUTDOWN". Do not unfeather, or restart, until leaving
Icing Conditions and visually confirm ice has gone out.

EP-58
 Q.R.H. C-295M-BR01-1

WINDSHIELD HEATING

NOTE
The crew is not required to perform any action if only
one FAIL light comes on in one WINDSHIELD
pushbutton and no WSHLD caution light is IEDS
displayed, since heating is automatically provided from
the other system.

1. L and R WINDSHIELD Pushbuttons ........................ PRESS 2

While at approach phase:

2. Vision through the glasses ....................................... CHECK ALL

A. If the vision is acceptable:

(END)

B. If the vision is not acceptable:

3. Passengers / Loadmaster ................................. NOTIFY 1

4. Aircraft ................................................. DEPRESSURIZE 2
When differential Pressure is zero:

5. Cockpit Door....................................................... CLOSE 2

6. IAS .......................................................... MAX 200 KIAS 1
7. Window ................................................................ OPEN 2

EP-59
Q.R.H. C-295M-BR01-1

PITOT HEATING

1. Corresponding PITOT pushbutton ........................... PRESS 1

Avoid icing conditions. If icing or high humidity conditions appear, the
following equipment may turn inoperative:

PITOT HEATING INOPERATIVE

REQUIRED ACTION
DISCONNECTED SYSTEMS

C/M-1 Anemometer Select ADS-2

LEFT Modes FD, IAS, ALT,
AP Disengage
ALT SEL and VS

C/M-2 Anemometer Select ADS-1

RIGHT Modes FD, IAS, ALT,
AP Disengage
ALT SEL and VS

IAS and ALT of the Use IAS, ALT

IESI (Reserve information primary
Instrument) systems

Avoid
Pressurization
climbout/descent
Automatic Control,
above 600/400 fpm
AUXILIARY Cabin Altimeter and
respectively. Apply
Differential Pressure
Pressurization
Indicator
Manual Control

Avoid flight or
VMO and Flaps
configuration close to
Overspeed Warnings
these condition

EP-60
 Q.R.H. C-295M-BR01-1

LANDING GEAR
ABNORMAL LANDING GEAR INDICATION

1. Landing gear pins on board ..................................... CHECK 2

2. IAS ................................................................... MAX 175 kts 1
3. Landing Gear Lever .................................................. DOWN 2
4. Land at nearest suitable airport.
A. If all landing gear visual indicators are green (down and locked):

5. Perform normal landing procedure. (END)

B. If one or more landing gear visual indicators are not green:

5. Apply <E.P.-62> "LANDING GEAR EMERGENCY

LOWERING" Emergency Procedure.

EP-61
Q.R.H. C-295M-BR01-1

LANDING GEAR EMERGENCY LOWERING

1. IAS ................................................................... MAX 150 kts 1

2. Lateral Safety Pin ............................. PULL AND MAINTAIN 2
3. Landing Gear Emergency Lowering Cover ................... LIFT 2
Keep the cover lifted until the end of flight.

4. Landing Gear Emergency Lowering LeverPULL FULLY

OUT 2
When all three visual viewers have been positioned (green or not):

5. Landing Gear Lever .................................................. DOWN 1/2

6. Landing Gear Lever ................................................. CHECK 1/2
A. If the landing gear lever is flashing:

One or more landing gear legs are not DOWN and LOCKED.

7. Apply <E.P.-6> "LANDING WITH ABNORMAL

LANDING GEAR CONFIGURATION". (END)
B. If the landing gear lever is not flashing:

All landing gear legs are DOWN and LOCKED.

7. LDG GR C/B (U1, A4) ............................................PULL 1

EP-62
 Q.R.H. C-295M-BR01-1

ANTISKID FAILURE

A. If only the "A-SKD DGD" caution comes on:

1. Antiskid............................................. RESET (OFF / ON) 2

A.1. If caution goes off:

Keep on normal operation. (END)

A.2. If caution remains on:

2. Antiskid .................................... KEEP CONNECTED

3. Brake smoothly to avoid wheel bursting at touch
down.

NOTE
It is not advisable to taxi with one Main Landing Gear
wheel not inflated. (END)

B. If both cautions come on simultaneously:

1. Antiskid............................................. RESET (OFF / ON) 2

B.1. If both cautions go off:

Keep on normal operation. (END)

B.2. If both cautions remain on:

Antiskid, as well as all its protections, has been lost. Use reverse
power carefully only during landing run initial phase. Once the
aircraft is firmly grounded, operate brakes smoothly and
intermittently to prevent wheels from locking. However, if both
tires on Main Landing Gear same side burst only operate brakes
at the opposite side.

EP-63
Q.R.H. C-295M-BR01-1

NOTE
Do not taxi if both tires on the Main Landing Gear same
side are not inflated.

The required landing distance depends on both braking

technique and runway conditions. This should be considered
while runway selecting for landing. See the table below for
Landing Distances without Antiskid.

LANDING DISTANCE WITHOUT ANTISKID

(SL, OAT Std. From 50 ft over threshold. No factor with reverse thrust)

LANDING DISTANCE FROM 50FT

LANDING WEIGHT (x 1000 kg)

FLAP RUNWAY
12 14 16 17 18 19 20 21 22 23.2

DRY 2720 2720 2825 2920 3000 3085 3179 3275 3375 3500
23º
WET 2965 2965 3085 3210 3310 3430 3545 3660 3790 3960

DRY 2990 2990 3105 3210 3295 3395 3500 3600 3715 3850
15º
WET 3305 3305 3450 3575 3680 3810 3960 4070 4299 4355

DRY 3125 3125 3250 3355 3445 3545 3655 3770 3885 4020
10º
WET 3470 3470 3625 3760 3885 4005 4125 4295 4425 4590

DRY 3395 3395 3525 3645 3750 3855 3965 4095 4220 4380
0º
WET 3825 3825 3980 4120 4270 4395 4525 4665 4895 5065

Correction over SL Std. OAT.

ALTITUDE: Add 50 ft. for each 1000 ft. of altitude.
OAT: Add 50 ft. for each 10ºC above 15ºC
Without Reverse: add 200 ft.

EP-64
 Q.R.H. C-295M-BR01-1

PNEUMATIC
BLEED O.TEMP

NOTE
Wait a few seconds before resetting the system.

1. BLEED O.TEMP Pushbutton ................................... PRESS 2

CAUTION

If it comes on again, do not touch the BLEED O.TEMP

pushbutton as it would open the HPSOV Valve again.

WING OVERHEAT

1. Engine parameters ................................................ CHECK 1/2

2. Affected PL (Crossed M. I. side) (if necessary) .RETARD 1/2
3. Clock ................................................................... RUNNING 2
A. If only one magnetic indicator is at the cross-line position:

4. Corresponding Bleed Switch ................................... OFF 2

A.1. If the "WING OVHT" warning goes off before 2 minutes:

5. Affected PL .......... OPERATE KEEPING LIGHT OFF 1

(END)

A.2. If the "WING OVHT" warning remains on after 2 minutes:

5. Bleed Magnetic Indicators ............................. CHECK 2

EP-65
Q.R.H. C-295M-BR01-1

A.2.1. If only one magnetic indicator is at the cross-line position:

6. Apply <E.P.-15 / E.P.-69> "ENGINE

SHUTDOWN"
A.2.2. If both magnetic indicators are at the cross-line position:

6. Proceed to section B.
B. If both magnetic indicators are at the cross-line position:

CAUTION

If both magnetic indicators are at the cross-line position,

Cabin pressure loss will start immediately. Get ready for
an Emergency Descent.

4. Bleed Switches ........................................................ OFF 2

After "WING OVHT" warning has gone off:

5. Left Bleed Switch....................................................... ON 2

B.1. If the "WING OVHT" warning comes on:

6. Left Bleed Switch ............................................... OFF 2

7. Right Bleed Switch ............................................... ON 2
8. Continue flight with left bleed switch off.
(END)

B.2. If the "WING OVHT" remains off:

6. Continue flight with right bleed switch off.

EP-66
 Q.R.H. C-295M-BR01-1

POWERPLANT
ENGINE FIRE OR SEVERE DAMAGE IN FLIGHT

WARNING

If performing a Continued Takeoff, wait until a positive

rate of climb is reached, operate the landing gear lever
up and wait until V2 is reached before going on with the
procedure.
1. FFL (affected engine) .........................DIRECTLY TO OFF 2*
2. Fire Handle (affected engine).............................. PULLED 2*
3. Clock ................................................................... RUNNING 2
A. If all fire indications go off before 10 seconds:

4. Land immediately in the nearest suitable airport.

5. Apply <E.P.-69> "ENGINE SHUTDOWN IN-FLIGHT".
(END)
B. If any fire indication persists after 10 seconds:

4. Fire Handle (affected engine) ........TURN TO DISCH 1 2*

B.1. If all fire indication go off before 40 seconds:

5. Land immediately in the nearest suitable airport.

6. Apply <E.P.-69> "ENGINE SHUTDOWN IN-
FLIGHT". (END)
B.2. If any fire indication persists after 40 seconds:

5. Fire Handle (affected engine) ...TURN TO DISCH 2 2*

6. Land immediately at the nearest suitable airport.
7. Apply <E.P.-69> "ENGINE SHUTDOWN IN-
FLIGHT".
EP-67
Q.R.H. C-295M-BR01-1

ENGINE FLAMEOUT

1. PL (affected engine) ....................................................... FI 1

2. FFL (affected engine, NH < 30%) .......DIRECTLY TO OFF 2*
3. Apply <E.P.-15 / E.P.-69> "ENGINE SHUTDOWN".

DUAL ENGINE FAILURE

1. Automatic Pilot (if connected) ..................... DISENGAGE 1

2. PLs ................................................................................... FI 1
3. FFLs (NH < 30%) .................................DIRECTLY TO OFF 2*
4. AOA (in clean configuration) ............................ 0.66 units 1
5. NP (both engines) ................................... CHECK NPs < 3% 2
6. ATC ........................................................................ NOTIFY 2
7. Hydraulic Pumps................................................. MAN / A.R. 2
8. Non-essential electrical loads ....................... DISCONNECT 2

CAUTION

The minimum altitude to achieve re-starting and apply

maximum power is 800 ft AGL.

WARNING

Do not restart an engine if previously has been

shutdown due to fire or severe damage.

9. Engine Starting (in BAT Mode) ........................... PERFORM 2

If neither engine starts:

10. Non-essential electrical loads ....................... DISCONNECT 2

11. Flaps (use only one hydraulic pump) .............................A.R. 2
EP-68
 Q.R.H. C-295M-BR01-1

12. Landing Gear Emergency Lowering ..............................A.R. 2

CAUTION

Do not extend the landing gear if there is no convenient

ground to land on.

ENGINE SHUTDOWN IN-FLIGHT

CAUTION

Note that if any battery is disconnected or inoperative,

the engine cannot be restarted.

1. PL (affected engine) ......................................................... FI 1

2. FFL (affected engine) ........................... DIRECTLY TO OFF 2*
3. NP (affected engine) ................................. CHECK NP < 3% 2
4. PRS Selector ................................................................ MCT 2
5. Fuel PUMP (affected engine).........................................A.R. 2*

CAUTION

If the engine shutdown is a result of the <E.P.-67>

"ENGINE FIRE OR SEVERE DAMAGE IN FLIGHT",
press-out the affected engine Fuel PUMP Pushbutton.

6. Electrical System ...................................... CHECK BUS TIE 2

7. Generator (affected engine) .......................................... OFF 2
8. Hydraulic Pumps................................................. MAN / A.R. 2
When necessary, connect only the hydraulic pump
corresponding to the operative generator (1 or 2).

9. Reduce electrical loads to below 400 A. Refer to "LIST OF

ELECTRICAL LOADS" in <E.P.-28> "DUAL DC
GENERATORS FAILURE".
EP-69
Q.R.H. C-295M-BR01-1

10. Bleed switch (affected engine) ...................................... OFF 2

A. If restarting is advisable:

WARNING

Do not restart an engine if previously shutdown due to

fire or severe damage.

11. Apply <E.P.-71> "ENGINE RESTART IN-FLIGHT".

(END)
B. If restarting is not advisable:

11. Monitor fuel imbalance. If required, apply fuel crossfeed

only if there are no fire indications.
12. Land at the nearest suitable airport with flaps at 15º and
VREF+ 15 or minimum VTH, whichever higher. Press the
EGPWS FLAP OVRD pushbutton to avoid a nuisance
warning. Refer to LANDING DISTANCE TABLE.
GO-AROUND (1 ENGINE)

1. GO-AROUND .................................................. ANNOUNCE 1

2. PL (operative engine) ..................................... MAX AUTO 1
3. Bleed switches ............................................................ OFF 2
4. Speed .......................................................... VREF + 12 KIAS 1
5. Flaps ......................................................................... T/OFF 2
6. Landing Gear (positive rate of climb) ............. RETRACT 2
7. Continue operation as if performing a normal takeoff.

EP-70
 Q.R.H. C-295M-BR01-1

ENGINE RESTART IN-FLIGHT

WARNING

Do not restart an engine if previously shutdown due to

fire or severe damage.

CAUTION

Do not attempt an engine restart in flight with the

autofeather system armed.
NOTE
Before applying this procedure, complete <E.P.-69>
"ENGINE SHUTDOWN IN-FLIGHT".
NOTE
The Engine Restart in Flight is only guaranteed within
the envelope shown in the QRD.
1. Batteries ............................................................ CHECK ON 2
2. Fuel PUMP pushbutton (affected engine) ..................... RUN 2
3. MODE SEL Selector ............................................. X-START 2
4. ENGINE SEL Selector .................... TO ENGINE STOPPED 2
5. Corresponding IGN Pushbutton .....................PRESS / ARM 2
6. Corresponding START Pushbutton ......................... PRESS 2
7. Corresponding FFL (at 10% minimum NH)............... START 2
8. Relight ................................................................ OBSERVE 1/2
A. If the engine is started successfully:

9. Oil Pressure and Temperature (affected engine) CHECK 2

10. FFL (affected engine) .............................................. RUN 2
11. PRS ..........................................................................A.R. 2
EP-71
Q.R.H. C-295M-BR01-1

12. PLs ...........................................................................A.R. 1

13. ENGINE START Panel ............................. RESTABLISH 2
14. Generator (affected engine) ....................... RESET / ON 2
15. Bleed switch (affected engine) .................................. ON 2
16. Disconnected Electrical Loads ............................ RESET 2
17. Hydraulic Pumps ................................................... AUTO 2
(END)
B. If the engine is not started successfully:

9. FFL .......................................................................... OFF 2

10. ENGINE START Panel ............................. RESTABLISH 2
11. Fuel PUMP Pushbutton (affected engine) ................A.R. 2
12. Land at the nearest suitable airport with Flaps at 15º and
VREF + 15 or minimum VTH, whichever higher. Press the
EGPWS FLAP OVRD pushbutton to avoid a nuisance
warning. Refer to "LANDING DISTANCE TABLE".

AUTOFEATHER FAILURE

1. Autofeather/APR ........................................................... OFF 2

If an engine fails:

2. FFL (affected engine) .........................DIRECTLY TO OFF 2*

3. PL (operative engine) ..... ADVANCE ABOVE MAX AUTO 1
4. Apply <E.P.-15 / E.P.-69> "ENGINE SHUTDOWN".

NL OVERSPEED

1. Corresponding PL ...............................................RETARD 1
If NLs decreasing is not possible below 106.5%, apply
<E.P.-15 / E.P.-69> "ENGINE SHUTDOWN".
EP-72
 Q.R.H. C-295M-BR01-1

LOW OIL PRESSURE

A. Oil pressure between 40 and 54 PSI (lower yellow band):

1. Corresponding PL ............................................. ADJUST 1

If reaching the green range is not possible, keep on
normal operation monitoring the oil temperature and
ITT. If abnormal indications are confirmed and power
is not required, apply <E.P.-15 / E.P.-69> "ENGINE
SHUTDOWN". (END)

B. Oil pressure below 40 PSI (lower red band):

1. If power is not required, immediately apply <E.P.-15 /

E.P.-69> "ENGINE SHUTDOWN".

HIGH OIL PRESSURE

A. Oil pressure between 66 and 100 PSI (upper yellow band):

1. PL ..................................................................... RETARD 1
If reaching the green band is not possible, keep on
normal operation monitoring both oil temperature
and ITT. If abnormal indications and/or engine
vibrations are confirmed and power is not required,
apply <E.P.-15 / E.P.-69> "ENGINE SHUTDOWN".
(END)

B. Oil pressure above 100 PSI (upper red band):

1. Reduce power if possible, and if power is not required,

immediately apply <E.P.-15 / E.P.-69> "ENGINE
SHUTDOWN".

EP-73
Q.R.H. C-295M-BR01-1

LOW OIL TEMPERATURE

CAUTION

Do not initiate the takeoff with oil temperature below 0º,

or below 45ºC in icing conditions.

1. Corresponding PL ............................................... ADVANCE 1

If it is not possible to keep the temperature above 45ºC,
avoid icing conditions.

2. If the temperature drops below –40 ºC, apply <E.P.-15 /

E.P.-69> "ENGINE SHUTDOWN".

HIGH OIL TEMPERATURE

1. Corresponding PL .................................................. RETARD 1

A. Oil temperature between 126ºC and 140ºC (upper yellow range):

2. Monitor oil pressure and any possible engine vibrations.

If the oil temperature stays in the yellow band for up
to 20 minutes and power is not required, apply
<E.P.-15 / E.P.-69> "ENGINE SHUTDOWN". (END)

If any time oil pressure oscillations and/or engine

vibrations occur, apply <E.P.-15 / E.P.-69> "ENGINE
SHUTDOWN".

B. Oil temperature above 140ºC (upper red range):

2. If power is not required, apply <E.P.-15 / E.P.-69>

"ENGINE SHUTDOWN".

EP-74
 Q.R.H. C-295M-BR01-1

EEC FAILURE

WARNING

In case of double EEC failure, apply the following

procedure to one engine and, once PL control has been
achieved, proceed with the other EEC.

CAUTION

Avoid aggressive PL handling and take a minimum of

10 second for full PL movement especially when above
10000 ft., unless there are other factors requiring the PL
to be moved more quickly.

1. Corresponding PL ............................................................. FI 1

CAUTION

Do not try reset EEC if the PL is not in FI position.

2. Corresponding EEC ..................................................RESET 2

A. If the "1, 2 EEC" caution does not come on again:

3. Keep flying in normal operation. (END)

EP-75
Q.R.H. C-295M-BR01-1

B. If the "1, 2 EEC" caution comes on again:

3. PRS Selector ........................................................ TOGA 2

4. Corresponding EEC ................................ DISCONNECT 2

CAUTION

The EEC disconnection means both autoignition and

APR have been lost. The RBS function can be
degraded.

5. Corresponding PL ....................................................A.R. 1

CAUTION

Reverse power on the affected engine will be degraded

(asymmetric reverse power).

NOTE
If the affected engine parameters cannot be maintained
within the operational limits, apply <E.P.-15 / E.P.-69>
"ENGINE SHUTDOWN".

NOTE
Once landed, if propeller brake is required, do not
exceed the NH limits on graph on the page LD-10 for
propeller brake operation with the EEC disconnected.

EP-76
 Q.R.H. C-295M-BR01-1

EPC FAILURE

1. PRS Selector ............................................................. TOGA 2

2. Corresponding EPC (once only) ...............................RESET 2
A. If the "1, 2 EPC" caution does not come on again:

3. Keep flying in normal operation. (END)

B. If the "1, 2 EPC" caution comes on again:

3. Corresponding EPC ................................ DISCONNECT 2

CAUTION

If OSG is not able enough to keep the propeller NP in

flight at 103 ±1% , it will operate the fuel control to keep
the propeller NP at 106% (red band). Even so, the flight
can be on in this status ("GET HOME" CAPABILITY).

At Landing:

CAUTION

Do not use reverse thrust on the affected side. Take

extreme caution while using reverse thrust on the
opposite side.

After Landing and While Taxiing:

4. FFL (affected engine) .......................................... START 2

EP-77
Q.R.H. C-295M-BR01-1

FIRE DETECTION SYSTEM FAILURE

1. Land at nearest suitable airport.

UNSAFE PROPELLER BRAKE

1. Left FFL ...............................................DIRECTLY TO OFF 2*

2. Propeller Brake (if connected) ...................... DISCONNECT 2
3. Apply <E.P.-15 / E.P.-69> "ENGINE SHUTDOWN".

POWER PLANT INDICATION FAILURE

A. The TQ, NH or NP indication box flashes:

Keep flying in normal operation. (END)

B. Fluctuations not displayed at the remaining parameters or the

numerical indication displays flashing dashes:

B.1. If the affected reading is TQ, NH, ITT or NP:

1. SWP Pushbutton ........................................... PRESS 2

B.1.1. If the anomaly goes out:

Keep flying while monitoring both engines readings. (END)

B.1.2. If the anomaly persists:

2. SWP Pushbutton ..................................... PRESS 2

3. Corresponding PL ............................... EQUALIZE 1
Keep flying monitoring regularly the
indications of the same engine. (END)

EP-78
 Q.R.H. C-295M-BR01-1

B.2. If the affected indication is any other:

Keep flying monitoring regularly the indications of the same

engine. (END)

C. "FUEL FLOW" with reading failure:

The Fuel Used reading will also be incorrect. Keep flying while
taking the remaining fuel indications as a reference. (END)

D. Abnormal TQ, ITT, NP, NH or fuel flow readings from both

engines simultaneously:

1. SWP pushbutton ................................................ PRESS 2

D.1. If the anomaly goes out:

Keep flying while monitoring both engines parameters. (END)

D.2. If the anomaly persists:

2. SWP pushbutton ........................................... PRESS 2

3. Both PLs .............................................................A.R. 1
(END)

E. Both vertical scale and TQ cursor flashing:

1. Corresponding PL ............................................. ADJUST 1

2. Corresponding EEC ............................................ RESET 2
E.1. If the flashing goes off:

Keep flying in normal operation. (END)

E.2. If the flashing persists:

Avoid sharp changes in the PL position above 10000 ft.

EP-79
Q.R.H. C-295M-BR01-1

IEDS FAILURE

1. TST pushbutton ....................................................... PRESS 2

NOTE
Press and hold the IEDS TST pushbutton until the test
ends.

2. "BIT STATUS" message .......................................... CHECK 2

A. If the BIT result is "PASSED":

3. SWP pushbutton ................................................ PRESS 2

A.1. If the anomaly goes off:

4. IEDS operation is still under suspect. Keep flying in

this condition. (END)
A.2. If the anomaly persists:

4. SWP pushbutton ........................................... PRESS 2

5. C Pushbutton ................................................ PRESS 2
Keep flying using the unaffected display in
Composite Mode. (END)

B. If the BIT result is "FAILED":

3. C Pushbutton...................................................... PRESS 2
Continue flight using the unaffected display in
Composite Mode.

EP-80
 Q.R.H. C-295M-BR01-1

AVIONIC SYSTEM FAILURES

ACP FAILURE

NOTE
If C/M-3 ACP or FR10 ACP not responding or
communication is not possible through one of these
ACPs, proceed to step 2 of section B.
NOTE
In case of ACP power drop, the ACP backlight will be
removed and control will be disabled.
NOTE
In case of REU failure, related ACP normal operation is
lost.
1. EMG pushbutton ....................................... PRESS / CHECK 1/2
A. If EMG pushbutton light is on:

Integrated audio control system is already in emergency mode.

2. Communications................................................. CHECK 1/2
A.1. If communication is possible:

Continue operation in emergency mode.

(END)
A.2. If communication is not possible:

Proceed to step 2 of section B.

B. If EMG pushbutton light is off:
2. Affected ACP C/B ............................................. OUT / IN 1/2
NOTE
This step will reset the failed ACP. If communications
through failed ACP is not possible, failed ACP is lost.
EP-81
Q.R.H. C-295M-BR01-1

DISPLAY UNIT FAILURE

A. In case of PFD or ND failure:

1. Corresponding Bright Selector ................................ OFF 1/2

2. Corresponding Bright Selector (after some minutes) . ON 1/2
If the display has been reset correctly. (END)

If the display does not reset, set the selector back to

OFF. (END)

B. White "DU HOT" annunciator displayed:

1. Bright Selector ....................... REDUCE TO A MINIMUM 1/2

If the annunciation changes to amber, the display will
disconnect automatically.

NOTE
If the display is not required, leave it off for a while to
reduce its temperature.

IOP FAILURE

A. If all the NAV/COM indications are lost (except RA and DF):

The "MASTER" IOP is failed.

1. RAD PRCSR Selector .....................................................

................................... SELECT THE OPERATIVE SIDE 1/2
Continue flying with the operative side indications.
(END)

B. If DH values and speed marks on the corresponding side are lost:

The "SLAVE" IOP is failed.

1. Continue flying with the operative side indications 1/2

EP-82 Revision 1
 Q.R.H. C-295M-BR01-1

ICP FAILURE

Loss of Altitude Indication, DH and IAS Marks.

1. ADS selector .................... SELECT THE OPERATIVE SIDE 1/2

NOTE
Barometric correction will be controlled with the ICP of
the selected side.

EFIS CONTROL PANEL FAILURE

Both PFD and ND associated to the failed EFCP change to the

following fix modes:

– PFD/ND Bright in 50%

– IMG BRT Radar bright relation in 1/1
– RANGE in 40 NM
– ND FORMAT display mode in ROSE
– IMG radar mode in W X ON
– TCAS mode in AUTO
– ND OR orientation mode in HEADING UP
– If the failure is at the pilot's side: ADF 1 in needle 1 and VOR 2 in
needle 2
– If the failure is at the copilot's side: VOR 1 in needle 1 and ADF 2 in
needle 2

EP-83
Q.R.H. C-295M-BR01-1

HEADING FAILURE

NOTE
The AP is automatically disengaged.

1. AHRS Selector................. SELECT THE OPERATIVE SIDE 1/2

2. HSI/SEL Selector ............. SELECT THE OPERATIVE SIDE 1/2
If AHRS1 is the one failed: TCAS, WXR, left FD and left
AP fail.

If AHRS2 is the one failed: WXR, right FD and right AP

fail.

If both AHRS are failed: TCAS, WXR, FD, AP and

EGPWS fail.

HEADING MISMATCH

1. Invalid Heading Source........................................ IDENTIFY 1/2

WARNING

When the compass is used, ensure that the windshield

heating is off.
2. GYROSCOPIC COMPASS.... SYNCHRONIZE MANUALLY 1/2
A. If synchronizing is successful:
(END)
B. If synchronizing is not successful:
3. AHRS Selector ................................................................
..................... SELECT THE VALID HEADING SOURCE 1/2
The WXR fails.

EP-84 Revision 2
 Q.R.H. C-295M-BR01-1

ATTITUDE FAILURE

NOTE
The AP is automatically disengaged.

1. AHRS Selector................. SELECT THE OPERATIVE SIDE 1/2

2. HSI/SEL Selector ............. SELECT THE OPERATIVE SIDE 1/2
If AHRS1 is the one failed: TCAS (intruders not
displayed), left FD and left AP fail.
If AHRS2 is the one failed: WXR, right FD and right AP
fail.
If both AHRS are failed: TCAS (intruders not displayed),
WXR, FD, AP and EGPWS fail.

ATTITUDE MISMATCH

NOTE
The AP is automatically disengaged, and the WXR fails.

1. Invalid Attitude Source ......................................... IDENTIFY 1/2

2. AHRS selector . SELECT THE VALID ATTITUDE SOURCE 1/2

IVSI FAILURE

1. Continue the flight with the operative side indications 1/2

AIRSPEED FAILURE

NOTE
The AP is automatically disengaged.

1. ADS selector .................... SELECT THE OPERATIVE SIDE 1/2

Revision 1 EP-85
Q.R.H. C-295M-BR01-1

AIRSPEED MISMATCH

NOTE
The AP is automatically disengaged.

1. ADS selector ................................................................. 1 - 2 1/2

2. ADS selector .................... SELECT THE OPERATIVE SIDE 1/2

NOTE
Barometric correction will be controlled with the ICP of
the selected side.

WARNING

Pilots must be aware of standby airspeed indication

error when flying with sideslip.

ALTITUDE FAILURE

NOTE
The AP is automatically disengaged.

1. ADS selector .................... SELECT THE OPERATIVE SIDE 1/2

ALTITUDE MISMATCH

NOTE
The AP is automatically disengaged.

1. ADS selector ................................................................. 1 - 2 1/2

2. ADS selector .................... SELECT THE OPERATIVE SIDE 1/2

EP-86 Revision 1
 Q.R.H. C-295M-BR01-1

NOTE
Barometric correction will be controlled with the ICP of
the selected side.

WARNING

Pilots must be aware of the standby altitude indication

error when flying with sideslip.

CHECK PFD WARNING

1. Displays ................................................................... CHECK 1/2

2. Bright selector on the corresponding PFD .................... OFF 1/2

AVIONIC DATA LOST

A. If EFIS is lost:

Wait until IOP PBIT finishes.

1. EFIS parameters .........................................RE-SELECT 1/2

(END)

B. If FMS is lost:

Wait until FMS2 and MCDUs PBIT finish.

1. FMS1 fail messages ........................................................

............................ RESET ALL (EXCEPT CROSSTALK) 1
2. FMS1 CTK key ................................................... PRESS 1
(END)

C. If IRS/GPS is lost:

Wait 10-15 minutes until IRS/GPS2 alignment procedure finishes.

(END)
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Q.R.H. C-295M-BR01-1

D. If navigation is lost:

Wait until IOP and MCDUs PBIT finish. (END)

E. If AFCS is lost:

Wait until AFCS PBIT finishes.

1. Flight Director Mode/Automatic Pilot ........................ A.R. 1

EP-88 Revision 1