Profiles/callouts

Front 1

Engine Failure after V1

Back 1

at approximately 1.4 EPR…
“AUTOTHROTTLES ON”

“EPR XX”

“CLAMP, 80 KNOTS, THRUST NORMAL”

“V1, ENGINE FAILURE, ROTATE, POSITIVE RATE”

“GEAR UP”

recommended technique above 400 feet AFE…

Declare an emergency. Comply with Airway Manual, Engine Out Departure Priorities.

“SET SPEED COMMAND BUG TO V2 + 20”

Hint 1

at 1000 feet AFE…

“ALTITUDE HOLD, SET SPEED COMMAND BUG TO V2 + 20” (if not already set)

at V2 + 20...

“IAS, MCT, EPR LIMIT, BANK ANGLE 25, AFTER TAKEOFF CHECKLIST, ENGINE FAILURE CHECKLIST”

recommended technique…

“AUTOPILOT ON”

Front 2

Rejected Takeoff Maneuver

Back 2

Verify actions as follows:
• Ensure throttles to IDLE
• A/T(s) disengage
• Verify reverse thrust applied.

SPD BRK lever aft.
Call "SPOILERS UP".

If SPD BRK lever not aft,
Call "SPOILERS NOT DEPLOYED."

Hint 2

Verify maximum brakes applied.

Call out any omitted action items.

Call out 80 knots.

Front 3

Localizer And ILS (G/S OUT) Approaches

Back 3

Select the VOR/ LOC mode on the FGCP.

Raw Date Monitor Intercept.

Hint 3

Observe raw data during the approach by selecting either the ARC, or ROSE mode and expanded localizer display on the PFD.

Both pilots may be in MAP mode throughout the approach except during localizer capture.

One EFIS NAV display must be in the ARC or ROSE mode during localizer capture in order to crosscheck FMS operation with navigation radio data.

Front 4

LDA Approach

Back 4

Select VOR/LOC to track inbound course.

Raw Data to Monitor Intercept.

Use vertical speed or glide slope to control descent.

Hint 4

Select VOR/LOC to track inbound course.

One pilot must be in ARC or ROSE to verify capture of correct LOC course, then may return to ND map display.

Use vertical speed or glide slope to control descent.

Front 5

VOR Approach

Back 5

Set appropriate VOR frequency and course.

Select VOR/ LOC mode on the FGCP.

Continuous Raw Date Monitoring throughout the approach by one pilot.

Hint 5

Set appropriate VOR frequency and course.

Select the VOR/ LOC mode on the FGCP.

The FD and autopilot (if engaged) will provide course guidance.

A pilot must observe raw data information for the VOR approach by using either the ARC, or ROSE mode with the RDMI selector in VOR.

One pilot may use the MAP display as a monitor for situational awareness if desired.

Front 6

NDB Approach

Back 6

Continuous Raw Data Monitoring
Select ADF to ON on the EFIS control panel.
Select the RDMI selector switch to ADF to display raw data on the RDMI.

PF set NDB course in the ILS/VOR window on the FGCP
and compare ADF blue needle with CDI course needle in either the ARC or ROSE display.

Use HDG SEL or NAV to track inbound course.
(NAV must be manually disengaged by the FAF)

Hint 6

Select ADF to ON on the EFIS control panel.

This will display the ADF needle on the ND in the ARC, ROSE and MAP modes. Select the RDMI selector switch to ADF to display raw data on the RDMI.

It is recommended that the PF set NDB course in the ILS/VOR window on the FGCP and compare ADF blue needle with CDI course needle in either the ARC or ROSE display.

Use HDG SEL or NAV to track inbound course. If NA V is used, it must be manually disengaged by the FAF.

Consider selecting approach in the FMS that resembles the NDB approach (i.e. ILS) or extending the runway for situational awareness. See the Use of MAP Display information in this chapter.

Front 7

LOC Back Course Approach

Back 7

Continuous Raw Data Monitor
SELECT Front Course

HDG Select Must be used.

Hint 7

CAUTION: Automatic flight guidance and autopilot tracking of the back course are not available. Do not arm the localizer function of the DFGS during a back course approach.

Front 8

Non-Precision Approach Briefing Items

Back 8

C - R - L - A - V - S

Configuration Point (3-5 miles FAF)
Runway (Course)
Lateral Mode
Altitude (Runway Rounded up)
Vertical Mode
Speed Intervention

Front 9

Missed Approach

Back 9

B A H A (Bank Angle, Hdg., Alt.)

“TOGA POWER, FLAPS 15”

“POSITIVE RATE”

“GEAR UP”

recommended technique…
“AUTOTHROTTLES ON, CHECK
BANK ANGLE, HEADING AND
ALTITUDE”

Hint 9

above 400 feet AGL... MAP...
“HEADING SELECT” or “NAV”
(if required)

at 1000 feet AFE or acceleration
height…

“CLIMB POWER,
SPEED COMMAND BUG 180”

at MAP altitude and maneuver speed…

“BANK ANGLE 25, AFTER TAKEOFF CHECKLIST”

Front 10

Missed Approach (Single Engine)

Back 10

B A H A (Bank Angle, Hdg., Alt.)

“TOGA POWER, FLAPS 11”
-POSITIVE RATE-

“GEAR UP”

recommended technique…
“AUTOTHROTTLES ON,
CHECK BANK ANGLE, HEADING AND ALTITUDE”

Hint 10

above 400 feet AGL... MAP...

“HEADING SELECT” or “NAV”
(if required)

at 1000 feet AFE or acceleration
height…

“ALTITUDE HOLD,
SET SPEED COMMAND BUG TO FLAPS 11 MANEUVER SPEED”

at flaps 11 maneuver speed
(flaps 15 maneuver + 10 knots)…

“IAS, MCT, EPR LIMIT, BANK
ANGLE 25, AFTER TAKEOFF
CHECKLIST”

Front 11

Emergency Evacuation

Back 11

Stop

Configure
Parking Brake Set
Spoilers Retract / Flaps 28

Shutdown

Evacuate

Front 12

Minimum Maneuvering Speeds

(1.4 to 1.5 Vs for each individual configuration)

Back 12

Flaps 5
(Flaps 15 Maneuvering + 20 knots)

Flaps 11
(Flaps 15 Maneuvering + 10 knots)

Hint 12

Flaps 15
(Flaps 15 Maneuvering)

Flaps 23
(Flaps 15 Maneuvering)

Flaps 28 or 40
(VREF + 10 knots)

Front 13

Windshear on Takeoff

Back 13

Approaching V1...

Airspeed Degradation (Identify..CALL)

AutoThrottles (Disconnect)
Power (Firewall)

Rotation.....(Call)
Above Vr.....(Max Thrust / 15 Pitch Angle)
Below Vr....(Max Thrust / 2,000 ft. remaining)

Hint 13

discretion to momentarily
Delay rotation during takeoff, allow the actual rotation speed to increase a few knots (no more than Vr + 20) to provide better performance during initial climbout.

Front 14

Windshear Escape Maneuver

Back 14

A/P, Power, A/T, Profile
(Click-Push-Push-Click-Fly)

Auto-Pilot (Disconnect)
TOGA (Push)
Power (Max...Firewall)
Auto-Throttles (Disconnect)
Profile

Hint 14

• Disconnect autopilot.
• Push either TO/GA.
• Set TO/GA power. If ground
contact is a factor, aggressively
apply maximum* thrust.
• Disconnect autothrottle(s).
• Simultaneously roll wings level and
rotate toward an initial pitch
attitude of 15°.
• Retract speedbrakes.
• Follow flight director guidance (if
available).
------------
• Do not change gear or flap
configuration until windshear is no
longer a factor.
• Monitor vertical speed and altitude.
• Do not attempt to regain lost
airspeed until windshear is no
longer a factor.

Front 15

Rapid Descent

Back 15

*Memory Items*
(Declare Emergency, Squawk 7700)

Speed - Idle - Brake - Altitude

Hint 15

Speed (IAS/MACH)
*320-340 Kias / .80-.82 Mach
*275-285 Kias / .75-.79 Mach
(Structural Damage)

IDLE (Throttles)

Speed Brake (Deploy)

Altitude (Preset/Arm)
Level Off Altitude / Speed

Front 16

PWS
Predictive Windshear

Back 16

Below 1,200' RA
Transponder ON
1 Engine Running
Right Throttle Advanced

Hint 16

CAUTION (3 miles/Not Ahead)
"MONITOR RADAR DISPLAY"

WARNING (1.5-3 miles/Ahead)
"GO AROUND, WINDSHEAR AHEAD"

Front 17

PWS
(Takeoff Inhibited)

Back 17

CAUTION Inhibited

80 KIAS - 400' RA

Hint 17

WARNING Inhibited

100 KIAS - 50' RA

Front 18

RWS
Reactive Windshear

Back 18

Below 1,500' RA
Nosegear Extension
(Takeoff)
TO
NosegearRetraction
(Touchdown Flare)

Hint 18

Alert & Guidance

CAUTION
-Increased Performance

WARNING
-Decreased Performance