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8. APU Air .....................................................................................OFF
9. APU.........................................................................AS REQUIRED
10. Yaw Damper .............................................................................. ON
Taxi-In:
Allow one (1) minute for cool down at idle thrust on right engine prior to
shutdown.
1. APU......................................................................................START
2. AUX Power ................................................................................ ON
3. Right Converter .........................................................................OFF
4. Yaw Damper ............................................................................OFF
5. Right Engine.............................................................. SHUT DOWN
END
Battery Charging Using APU or External AC Power
1. ELECTRIC MASTER AUX PWR ............................................... ON
NOTE: Battery charging is possible using APU alternator or external AC
power only.
2. BATT 1 or BATT 2 ..................................................................... ON
NOTE: If charging of only one (1) battery is desired, pull appropriate
BATT CHGR circuit breaker on PDB. For airplanes having ASC 54, if
charging of only one (1) battery is desired, select appropriate BATT
switch ON.
3. Battery Ammeter(s) .........................................................MONITOR
NOTE: The battery chargers may use up to 34 volts for battery charging.
Maximum current for battery charging is limited to 38 amps.
END
Quick Reference Handbook
REVISION 7 NORMAL PROCEDURES
May 30/02 Page NG - 5
GIV QFE Operations AFM 2-08-80
Takeoff:
1. Set altimeters to QNH (if available). If QNH is not available, set
altimeters to achieve field elevation.
2. Perform Takeoff Initialization and verify Takeoff Data to be correct.
3. On Display Controller, manually "box" takeoff speeds.
4. Set QNH in BARO CORR window of Cabin Pressure Selector
Panel.
5. Set altimeters to QFE for takeoff.
6. During TAXI checklist, verify that DFRN PRESS does not exceed
0.30 PSID.
7. Select TERRAIN INHIBIT to ON if EGPWS equipped and Software
Level is -104 -104.
Climb:
1. When clear of traffic pattern, select AUTO V-SPEEDS on Display
Controller.
2. At transition altitude, select appropriate altimeter setting (29.92 /
1013).
3. Select TERRAIN INHIBIT to OFF.
Approach:
1. Set QFE altimeter setting when directed by ATC.
2. Set QNH in BARO CORR window of Cabin Pressure Selector
Panel.
3. Set actual Landing Field Elevation in LANDING window of Cabin
Pressure Selector Panel.
4. Set desired rate in RATE window of Cabin Pressure Selector
Panel.
5. Select TERRAIN INHIBIT to ON if EGPWS equipped and Software
Level is -104 -104.
6. Verify DFRN PRESS is less than 0.30 PSID prior to landing.
END
Quick Reference Handbook
NORMAL PROCEDURES REVISION 7
Page NG - 6 May 30/02
RNAV Approach Procedures AFM 2-08-90
1. Review the published approach.
2. Select the approach from the database and activate it.
3. Set MDA or RAD ALT value to the published DA or reference radio
altitude value.
4. When cleared for the approach, arm the LNAV mode (and VNAV
mode, if VNAV guidance is desired for the approach) on the
guidance panel. Set the altitude preselector to the touchdown zone
elevation to ensure continuous vertical guidance to the runway.
5. When within 2 miles of the FAF (Final Approach Fix), the FMS Approach
light / FMS Approach message will illuminate. This is clearance
to continue the approach to the published DA. If the FMS Approach
light / FMS Approach message does not illuminate, the approach
shall be abandoned.
6. When runway is in sight, disconnect autopilot and/or autothrottle
and land. If runway not in sight at the DA (or MDA, as appropriate),
execute the published missed approach.
END
Quick Reference Handbook
REVISION 7 NORMAL PROCEDURES
May 30/02 Page NG - 7
High Elevation Airport Operations OM 07-01-90
Flight Crew Considerations:
Use of oxygen by the flight crew while performing high-workload tasks
at high elevation airports or at field elevations for which the flight crew
is not acclimated is highly recommended.
NOTE: Examine performance data thoroughly to determine the adverse
effects of high density altitude on airplane performance.
Right Engine Start:
CAUTION: WITH THE UTILITY PUMP OFF, ONLY THE PARKING
BRAKE IS AVAILABLE TO HOLD THE AIRCRAFT. THE USE OF
CHOCKS IS RECOMMENDED.
　
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