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CONDITION/LOCATION  CALLOUT 
Takeoff  Initial Power Set Takeoff Power Set 100 Knots V1’ VR Positive Rate of Climb  PF: “AUTOTHROTTLES ON” PF: “CHECK POWER” PM: “POWER SET ___%” PM: “100 KNOTS” PM:  “V1’ ROTATE” PF or PM:  “POSITIVE RATE” PF: “GEAR UP” 
Climb  Passing Transition  PM: “_____ FEET _____ SET” 
And  Altitude 
Descent  1000 Feet Above or Below Assigned Altitude  PM: State Actual Altitude For Assigned Altitude, i.e., “SIX THOUSAND FOR SEVEN THOUSAND.” 
Approach  1000 Feet ATDZ  PM: “1000” FEET
(Except  500 Feet ATDZ  “500”
Monitored)  400 Feet ATDZ  “400”
300 Feet ATDZ  “300”
200 Feet ATDZ  “200”
100 Feet ATDZ  “100” 
IMC  100 Feet Prior to  PM: “APPROACHING MINIMUMS” 
(Except  DA(H)/DDA 
Monitored)  Reaching DA(H)/DDA Approach Lights Or Runway In Sight  PM: “MINIMUMS” PM:  “APPROACH LIGHTS IN SIGHT”          “RUNWAY IN SIGHT” 
Non-Precision  Map  PM:  “MISSED APPROACH POINT” 
Monitored Approach  1000 Feet ATDZ 500 Feet ATDZ 400 Feet ATDZ 300 Feet ATDZ 100 Feet Prior to DA(H) /DDA Landing Go-Around  CAPT: “1000” FEET “500” “400” “300” CAPT: “APPROACHING MINIMUMS, I’M GOING HEADS UP” CAPTAIN:  “I HAVE THE AIRCRAFT” F/O: “MINIMUMS, GOING AROUND” 
All IMC Approaches  50 Feet 30 Feet 20 Feet 10 Feet  PM: “50...30...20...10” 
Visual Approaches At Captain’s Discretion 
Landing Roll  80 Knots  PM: “80 KNOTS” 

SAFETY INSPECTIONS

Exterior Safety Inspection
An Exterior Safety Inspection will be conducted on all originating flights and crew changes by either the Captain or the First Officer.
Surfaces and Chocks.........................................................................CHECK

Visually check that all moveable surfaces are clear and the chocks are in
place.
Maintenance Status / Log book .......................................................CHECK

Verify maintenance status is acceptable for flight and ensure agreement
with authorized dispatch deviations if required.
Cockpit Safety Inspection
A Cockpit safety inspection will be conducted from memory by either the Captain or First Officer on any originating flight or crew change prior to establishing electrical power. If both AC and DC electrical systems are already powered when the crew arrives at the aircraft, this inspection may be omitted.
Battery Switch........................................................................................... ON
Volt / Freq Selector..................................................................BATT VOLT

Verify that the battery voltage is 25 volts or higher.
Caution:  If the battery voltage is less than 25 volts, move BATT switch to OFF. Battery must replaced.
Landing Gear Handle........................................................................ DOWN
Flap/Slat Handle ................................................................. UP / RETRACT
Speed Brake Handle ......................................................................STOWED
AUX Hydraulic Pump Switch................................................................OFF
Radar Switch...........................................................................................OFF

EXTERNAL POWER / EXTERNAL AIR

External Power Check
Battery Switch.........................................................................ON/LOCKED

Pull and move the battery switch to ON and rotate it to the horizontal/locked position. With the battery switch OFF, only the battery direct bus is powered. Turning the battery switch ON powers the battery bus, DC transfer bus, and battery direct bus.
AC Volt / Freq Selector ........................................................... BATT VOLT

Verify that the battery voltage is 25 volts or higher.
Caution:  If the battery voltage is less than 25 volts, move BATT switch to OFF.  Battery must be replaced.
Ext Pwr Available Lights ......................................................................... ON

The blue lights indicate external power is available.
Voltage/Freq................................................................................ CHECKED

Rotate the VOLT/FREQ selector to EXT PWR and check for the following
　
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