.
terrain display test pattern shows on weather radar display. Hold the test switch at least 10 seconds to test the above indications
and any additional EGPWS aural warnings. Light controls .......................................................................... As desired VHF NAV radios ........................................................... Set for departure EFIS control panel .............................................................................. Set
EHSI range selector – As desired
EHSI mode selector – MAP
Weather radar switch – OFF
Map switches – As desired
Seat ................................................................................................ Adjust Verify positive horizontal (fore and aft) seat lock. Rudder pedals ................................................................................ Adjust
Copyright . The Boeing Company. See title page for details.
NP.20.18 June 4, 2004
Normal Procedures -Amplified Procedures 737 Operations Manual
Adjust rudder pedals to permit full rudder deflection and brake application. Ensure the captain holds the nose wheel steering wheel while moving rudder pedals.
Takeoff data .............................................................................. Complete
Complete the takeoff data to include N1, V1, VR, V2, flap setting, zero fuel weight, temperature, altimeter setting, gross weight, and stabilizer trim setting and pass the data card to the captain.
Final Flight Deck Preparation – Captain and First Officer
N1 & IAS bugs ....................................................................................Set Verify N1 cursors reflect the full rated N1 value or the derated N1 value if a TAKEOFF DERATE is selected. Set V2 in the MCP IAS/Mach display and check airspeed cursors and speed tape (as
installed) indications. Set airspeed indicator markers (bugs) V1, VR,
V2 + 15, and flaps up maneuvering speed.
Engine start clearance...............................................................Obtain
The captain calls “BEFORE START CHECKLIST DOWN TO THE
LINE.” The first officer accomplishes the BEFORE START checklist down to the line. – – – – – –– – – – – – CLEARED FOR START –– – – – – – – – – –– Doors .............................................................................................Closed All exterior door annunciator lights – Extinguished Flight deck windows.....................................................................Locked
Verify the lock levers are in the locked (forward) position. Air conditioning PACK switches...................................................... OFF Start pressure ..........................................................................._____ PSI
The minimum start pressure at sea level is 30 psi. Allow .5 psi reduction for each 1000 feet above sea level. ANTI–COLLISION light switch........................................................ON
Normal Procedures -Amplified Procedures
Alerts the ground crew and tower that the flight crew is starting engines.
The captain calls “BEFORE START CHECKLIST BELOW THE LINE.”
The first officer completes the BEFORE START checklist.
Engine Start Procedure
CAPTAIN FIRST OFFICER
Announce engine start sequence. Normal starting sequence is 2, 1.
Announce “STARTING ENGINE No. ___.” Position ENGINE START switch to GRD.
Verify increase in N2 RPM.
Acknowledge first officer’s report. Verify increase in oil pressure by the time engine is stabilized at idle and announce “OIL PRESSURE RISING” when observed.
Position engine start lever to IDLE detent when: . N1 rotation is observed and . N2 RPM reaches 25% or (if 25% N2 is not achievable) . at max motoring and a minimum of 20% N2. Max motoring occurs when N2 acceleration is less than 1% in approximately 5 seconds.
Verify fuel flow and EGT indication.
At 46% N2 RPM check ENGINE Verify START VALVE OPEN light
START switch moves to OFF; if not, extinguishes. Verify ENGINE START
position start switch to OFF. switch moves to OFF and report “STARTER CUTOUT.”
Monitor N1, N2, EGT, fuel flow and oil pressure for normal indications as the engine accelerates and stabilizes at idle.
Copyright . The Boeing Company. See title page for details.
NP.20.20 June 4, 2004
Normal Procedures -Amplified Procedures 737 Operations Manual
Standard day, sea level, approximate stabilized idle indications for CFM56–3.
.
N1 RPM – 22% EGT – 475°C**
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