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Gear up
PNF
PF
Landing gear lever up and EICAS indicates 3 white
UP lights on Gear up – Indicated PNF
At V2 + 10 to 15 KIAS Speed mode PF
When speed mode is engaged on FCP Speed mode – set PNF
At 320 feet AGL, minimum Autopilot – On PF
When autopilot is engaged Autopilot – set PNF
Conditions for flaps retraction are fulfilled Flaps up PF
When EICAS indicates flaps at zero degrees Flaps up – Indicated PNF
Conditions for reduction to climb thrust are fulfilled Climb thrust,
After Take-off Check PF
When climb thrust is set Climb thrust - set PNF
When AFTER TAKE-OFF CHECK is completed After Take-off Check –
Complete PNF
NORMAL PROCEDURES
Standard Callouts
Vol. 1 04−03−1
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
3. CALLOUTS DURING CLIMB
CONDITION CALL CREW
MEMBER
Passing transition altitude Transition altitude PNF
1,000 feet before reaching clearance altitude or flight
level 1,000 feet to go PNF
4. CALLOUTS DURING DESCENT
CONDITION CALL CREW
MEMBER
1000 feet before reaching clearance level or altitude 1000 feet to go PNF
Passing transition level Transition level PNF
5. CALLOUTS DURING APPROACH
CONDITION CALL CREW
MEMBER
Conditions for initial flaps extension are fulfilled Flaps 20 PF
When EICAS indicates flaps at 20 degrees Flaps 20 – Indicated PNF
When localizer course bar starts to move from full
scale deflection Localizer alive PNF
When glideslope pointer starts to move downward Glideslope alive PNF
NORMAL PROCEDURES
Standard Callouts
Vol. 1 04−03−2
REV 67, Mar 19/07
CL−604 Operating Manual
PSP 604−6
6. CALLOUTS DURING APPROACH AND LANDING
CONDITION CALL CREW
MEMBER
When at the appropriate segment of the approach Gear down,
Before Landing Check PF
When landing gear is down and EICAS indicates 3
green DN lights on Gear down – 3 greens PNF
When BEFORE LANDING CHECK is completed Before Landing Check –
Complete PNF
Conditions for flaps extension to 30 degrees/45
degrees are fulfilled Flaps 30/45 PF
When EICAS indicates flaps at 30 or 45 Flaps 30/45 – Indicated PNF
At final approach fix (FAF) Final approach fix (by
name) Both
If maximum localizer deviation is exceeded Localizer PNF
If maximum glideslope deviation is exceeded Glide path PNF
If maximum speed deviation is exceeded Speed PNF
If maximum descent rate is exceeded Sink rate PNF
If maximum altitude deviation is exceeded Altitude PNF
At 500 AGL (Precision approaches) 500 feet AGL PNF
At 100 feet above decision height (DH) or decision
altitude (DA) 100 above Decision PNF
At decision height (DH) or decision altitude (DA) Decision PNF
At 100 feet above Minimum Descent Altitude (MDA) 100 above MDA PNF
At Minimum Descent Altitude (MDA) Minimums PNF
At Missed Approach Point (MAP) Missed approach point PNF
At the MAP or DH/DA, when visual reference is
established Landing PF
At pilot’s decision to become PF I have control Pilot
At minimum height for autopilot use, if still engaged Autopilot – disengage PNF
NORMAL PROCEDURES
Standard Callouts
Vol. 1 04−03−3
REV 67, Mar 19/07
CL−604 Operating Manual
PSP 604−6
7. CALLOUTS DURING GO-AROUND
CONDITION CALL CREW
MEMBER
At the MAP or DH/DA and the runway is not in sight
or at any instance when a go-around is called for Go-Around PF
While advancing the thrust levers to the vertical
position Go-Around thrust PF
When Go-Around thrust is set Go-Around thrust – set PNF
While achieving G/A attitude and thrust Flaps 20 PF
When EICAS indicates flaps at 20 degrees Flaps 20 – Indicated PNF
When positive rate of climb is attained Positive rate
Gear up
PNF
PF
EICAS indicates 3 white UP lights on Gear up – Indicated PNF
8. CALLOUTS DURING LANDING ROLL
CONDITION CALL CREW
MEMBER
EICAS status page L and R REV ARMED advisory
message is on at 70 knots Two greens PNF
When Pilot wants to take control I have control Pilot
NORMAL PROCEDURES
Standard Callouts
Vol. 1 04−03−4
REV 67, Mar 19/07
CL−604 Operating Manual
PSP 604−6
1. AIRPLANE PREPARATION
A. General
Before power (electrical, hydraulic or pneumatic) can be safely applied to the airplane, the
external safety inspection must be made, either by qualified technical/maintenance ground
staff or by the pilot. Once power has been applied to the airplane, the pilot performs the
　
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