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Page ND - 4 May 30/02
8. Autothrottle.................................. ARM / ENGAGED (IF DESIRED)
NOTE: Autothrottle will annunciate “HOLD” at approximately 60 knots
and will maintain power lever "HOLD" unless selected to another mode
after attaining 400 ft. AGL.
END
Notes
Quick Reference Handbook
REVISION 7 NORMAL PROCEDURES
May 30/02 Page NE - 1
Climb AFM 2-05-10
1. Landing Gear...............................................................................UP
2. Flaps............................................................................................UP
3. Flight Guidance Panel .............................................................. SET
4. Exterior Lights .........................................................AS REQUIRED
5. Ignition ...................................................................................... OFF
6. Ground Spoilers ....................................................................... OFF
7. BTMS / OVHT Message........................................... CHECK / OUT
NOTE: SPZ-8000 equipped airplanes SN 1156 and subs and SN 1000
through 1155 having ASC 167. For SPZ-8400 equipped airplanes, BTMS
display is incorporated in the BRAKES system page.
8. Pressurization......................................................................CHECK
9. Engine Climb Power / Autothrottle ................SET / AS REQUIRED
10. Engine Synchronizer ...............................................AS REQUIRED
11. Altimeters (3) ....................................................................................
............SET & CROSS-CHECKED (AT TRANSITION ALTITUDE)
12. APU .......................................SHUT DOWN PRIOR TO 30,000 FT
NOTE: Shut down APU prior to reaching 30,000 ft. if not required for
electrical power.
END
Cruise AFM 2-05-20
1. Power ................................................................ SET FOR CRUISE
2. Pressurization......................................................................CHECK
3. Panel Sweep ................................................................COMPLETE
NOTE: A panel sweep or a check for normal system operation and
indication should be accomplished at top-of-climb, top-of-descent, and
at regular intervals between top-of-climb and top-of-descent.
4. FMS Fuel Quantity.............................................................UPDATE
NOTE: The flight crew should perform hourly updates to the FMS fuel
quantity using data from the FQMS. On FMS PERF INT Page 5/5,
perform a delete on line select key 2L.
END
Quick Reference Handbook
NORMAL PROCEDURES REVISION 7
Page NE - 2 May 30/02
Descent AFM 2-05-30
1. Crew Briefing (VREF / Go-Around Power) ........................ BRIEFED
2. Pressurization ...........................................................................SET
CAUTION: IF ON MANUAL PRESSURE CONTROL, MONITOR
CLOSELY TO ENSURE LANDING UNPRESSURIZED WITH THE
OUTFLOW VALVE FULLY OPEN.
3. Circuit Breakers .................................................................. CHECK
4. Fuel Boost Pumps...............................................................ALL ON
5. Nose Wheel Steering ................................................................. ON
6. Parking Brake / Accumulator ..................................OFF / 3000 PSI
END
Approach - In Range AFM 2-05-40
1. Altimeters (3)....................................................................................
.................. SET & CROSS-CHECKED (AT TRANSITION LEVEL)
2. Engine Synchronizer .................................................................OFF
3. Flaps .......................................................................AS REQUIRED
4. VREF / Go-Around Power ............................................... CHECKED
5. Hydraulic Pressure.............................................................. CHECK
6. Exterior Lights .........................................................AS REQUIRED
7. Auxiliary Hydraulic Pump ....................................................ARMED
END
Before Landing AFM 2-05-50
1. Landing Gear .......................................................................DOWN
2. Crew Alerting System.......................................................... CHECK
3. Nutcracker.............................................................................. TEST
CAUTION: DO NOT ARM GROUND SPOILERS IF NUTCRACKER
SWITCH TEST IS UNSUCCESSFUL.
4. Ground Spoilers ..................................................................ARMED
Quick Reference Handbook
REVISION 7 NORMAL PROCEDURES
May 30/02 Page NE - 3
5. Flaps................................................................SET FOR LANDING
　
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