Cockpit Flows/Callouts

Question 1

Before Start Flow

Answer 1

FO:
Red Anti-Collision (Beacon) …….. ON
Electric Hydraulic Pumps ………….. ON (pressurize right system first)
Fuel Pumps …………………………………… ON (for tanks containing fuel)
APU Bleed Valve ……. …………………… OFF (if either or both Packs ON)
Pack Control Selectors ………………. OFF
APU Bleed Valve ………………………….. ON
Transponder ………………………………….. XPNDR
*Read BEFORE START checklist after CA finishes flow

CA:
Trim ………………………………………………….. Set

NOTE: Stabilizer trim settings less than (B757) 3 units or (B767) 1.50 units require the use
of manual trim levers or alternate Stabilizer Trim switches (as installed)

Flight Controls ……………………………….. Check
Lower EICAS Display ……………………. Engine
EICASE Messages …………………………. CANCEL

Question 2

After Start Flow

Answer 2

After Captain calls: “FLAPS_____, AFTER START CHECKLIST.”

FO:
FLAPS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Set
APU selector . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
ENGINE ANTI-ICE switches (if required). . . . . . ON
(B757) ISOLATION switch . . . . . . . . . . . . . . . . . . . Off
(B767) L and R ISOLATION switches . . . . . . . . . Off
PACK control selectors . . . . . . . . . . . . . . . . . . . . . . . . AUTO

CA:
RECALL. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Checked
AUTO BRAKES selector. . . . . . . . . . . . . . . . . . RTO

FO:
Reads After Start Checklist

Question 3

Delayed Engine Start

Answer 3

Starting Second Engine:
FO:
APU BLEED switch (using APU-assisted start) . . . .. . OFF
PACK control selector(s). . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
APU BLEED switch (using APU-assisted start) . . . . . . ON
(B757) ISOLATION switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
(B767) L and R ISOLATION switches . . . . . . . . . . . . . . . . . ON
ENGINE ANTI-ICE switches . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

Question 4

Before Takeoff Procedures

Answer 4

• Takeoff Briefing

- BEFORE TAKEOFF checklist (called for by CA)

Question 5

Cleared onto Runway

Answer 5

“RUNWAY ___ VERIFIED” (CA and FO)
- verify proper runway and Position

CA:
Exterior lighting. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

FO:
Transponder mode selector . . . . . . . . . . . . . . . . . . . . . . . . . . TA/RA

CA and FO:
TFC display . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Set
Weather radar . . . . . . . . . . . . . . . . . . . . . . . . . . . . On (one or both should have WXR displayed)
TERRAIN display . . . . . . . . . . . . . . . . . . . . . . . . . On (at lease one when terrain is a factor)

Question 6

Takeoff Procedure and callouts

Answer 6

PF - Advance thrust levers to 1.1 EPR (757), 70% N1 (767)
PF - Selecet N1/EPR/THR mode
“SET TAKEOFF THRUST”
PM - “THRUST SET”
- at 80 knots call “80 knots”
PF - verify 80 knots “Check”
PM - “V1”
- “Rotate”
PF - at Vr rotate to 15º and follow F/D after liftoff
PM - “V2”
- “Positive Rate”
PF - “Gear UP”
PM - “Gear UP” and position landing gear lever UP
PF - at 400’ AFE call for “HDG” (or verify LNAV captures)
- at 1000’ (NADP 2) or 1500’ (NADP 1) call for “VNAV”
- “FLAPS___” according to flap retraction schedule
PM - “FLAPS___” and position flap lever
PF - at flaps up speed “FLAPS UP AFTER TAKEOFF CHECKLIST, CLIMB 2”
PM - verify flaps up and select CLB 2, read checklist
- “AFTER TAKEOFF CHECKLIST COMPLETE

Question 7

After Takeoff Procedures

Answer 7

PF Calls “AFTER TAKEOFF CHECKLIST”

PM:
Landing gear lever . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
-Verify landing gear is up, then position landing gear lever OFF
FLAPS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP

“AFTER TAKEOFF CHECKLIST COMPLETE”

Question 8

Expected Takeoff Briefing

Answer 8

• Runway
• Flaps
• Thrust Rating
• NADP 1 or NADP 2
• MCP (Left to Right)
• EO Accel Altitude

Question 9

PF Pre-Takeoff Brief

Answer 9

• Runways
• Takeoff Flaps
• Takeoff Thrust Setting
• Planned Automation
• MCP settings and Altitude
• Altitude Constraints
• Transition Altitude
• EO Procedures

Question 10

SPACE Check

Answer 10

S----- SAFETY
    Battery Still Has Good Fluid
    1.) BATTERY switch - ON
    2.) STANDBY POWER selector – AUTO
    3.) HYDRAULIC ELECTRIC PUMP switches – OFF
        a.) (B767) HYDRAULIC DEMAND PUMP selectors - OFF
    4.) Landing Gear lever – DN
    5.) ALTERNATE FLAPS selector – NORM

P ---- POWER
    Electrical Power - Establish
    1.) Bus Tie switches – AUTO
    2.) APU selector (if desired) – START, then ON
    3.) EXTERNAL POWER switch - PUSH

A ---- ACCESSORY PANEL 
    (B767) 2 / 1 / 2
    1.) Flight Recorder switch - NORM
    2.) Service Interphone switch – OFF
        a. With PRM installed - PRM
    3.) Reserve Brakes and Steering Reset/Disable switch Guard – CLOSED
         a. Verify ISLN light extinguished
    4.) EEC MAINT switches - NORM 
    (B757) 1 / 2 / 1
    1.) Power Transfer Unit switch - OFF
    2.) Flight Recorder switch - NORM
    3.) Service Interphone switch - OFF
    4.) EEC MAINT switch - NORM (RR) No EEC Power switch

C —- CIRCUIT BREAKERS

E—– EMERGENCY EQUIPMENT & EVERYTHING ELSE

Question 11

Descent/Arrival Prep

Answer 11

“ID A B4 C”
I —- In-Range Report – Send
D — Landing Data – Request
A — ATIS (Arrival airport) – Request
B — Build approach (FMC, ILS control panel, etc.)
B — Bugs (APPROACH REF page, minimums etc.)
B — Brakes – Set autobrakes, if desired
B — Brief arrival, approach, taxi, and ABG to include “what if planning”
C — Checklist (Descent checklist)

Question 12

Non-ILS Approach

Answer 12

“LAVS/LVSA”

L — Lateral Mode
A — Altitude Window
V — Vertical Mode
S—- Speed Intervene

Question 13

After Landing Flow

Answer 13

“I Told Fred To Run Ahead”

Trigger: Clear of active runway, taxi clearance received and understood by both
crewmembers

I - - - - - ILS – Park
Told - - - Transponder – XPNDR
Fred - - - FLAPS – UP
To - - - - STAB TRIM – 4 ANU
Run - - - RADAR – Off
Ahead - - APU selector – As required