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82. EGPWS.................................................................................. TEST
83. BTMS / Selector Switch (If Installed)............................. TEST / ALL
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. No test is required
or selection available.
84. Rudder and Aileron Trim ..................................................... CHECK
85. EPR / V Speeds / AOA / Radio Altimeter ..................................SET
END
Quick Reference Handbook
REVISION 7 NORMAL PROCEDURES
May 30/02 Page NC - 5
Recommended Elevator Trim Tab Settings For Takeoff
Fuel
Loading
(Lb)
Elevator Trim Tab Position Units
29,000 11 10 9 8 7 6 5 4 3 2
28,000 11 10 9 8 7 6 5 4 3 2
27,000 11 10 9 8 7 7 6 5 4 3
26,000 12 11 10 9 8 7 6 5 4 3
25,000 12 11 10 9 8 7 6 5 4 3
24,000 12 11 10 9 8 7 6 5 4 3
23,000 12 11 10 9 8 7 6 5 4 3
22,000 12 11 10 9 8 7 6 5 4 3
21,000 12 11 10 9 8 7 6 5 4 3
20,000 12 11 10 9 8 7 6 5 4 3
19,000 12 11 10 9 8 7 6 5 4 3
18,000 12 11 10 9 8 7 6 5 4 3
17,000 12 11 10 9 8 7 6 5 3 3
16,000 12 11 10 9 8 7 6 4 3 2
15,000 12 11 10 9 8 6 5 4 3 2
14,000 12 11 10 8 7 6 5 4 3 1
13,000 12 10 9 8 7 6 5 4 2 1
12,000 11 10 9 8 7 5 4 3 2 1
11,000 11 10 9 7 6 5 4 3 1 0
10,000 11 9 8 7 6 5 3 2 1 -1
9,000 10 9 8 6 5 4 3 1 0 -2
8,000 10 8 7 6 5 3 2 1 -1 -3
7,000 9 8 7 5 4 3 1 0 -2 -4
6,000 9 7 6 5 3 2 0 -1 -2 -5
5,000 8 6 5 4 3 1 0 -2 -3 -5
4,000 7 6 5 3 2 0 -1 -3 -4 -6
3,000 7 5 4 2 1 -1 -2 -4 -5 -7
2,000 6 4 3 1 0 -2 -3 -5 -6 -8
1,000 5 3 2 0 -1 -3 -4 -6 -7 -8
36 37 38 39 40 41 42 43 44 45
Zero Fuel Center of Gravity - % MAC
NOTE: A minus sign (-) indicates nose down trim.
Before Starting Engines: Thruflight AFM 2-03-10
Perform boxed items of Before Starting Engines checklist.
END
Quick Reference Handbook
NORMAL PROCEDURES REVISION 7
Page NC - 6 May 30/02
Starting Engines AFM 2-03-20
1. Start Page ..........................................................................SELECT
NOTE: When oil temperature is -10° C or less, refer to All Weather
Operations and Procedures in the GIV Operating Manual.
2. HP Fuel Cocks .......................................................................SHUT
3. Power Levers ...........................................................................IDLE
4. GUST LOCK .............................................................................OFF
5. Beacon Switch ........................................................................... ON
6. APU Air / External Air..............ON / PRESSURE 25 PSI MINIMUM
NOTE: Normal air pressure from the APU can vary between 25 to 50
psi. APU air pressure drops during the starting cycle but should not fall
below approximately 25 psi.
7. Fuel Boost Pumps (One Each Side) .............ON / MESSAGE OUT
8. Electrical Power ...............................................CHECK (35% MAX)
NOTE: If using APU, limit APU alternator load (AC AUX PWR) to 35%
during main engine starts. At high elevation airports and/or in high
ambient temperature conditions, limit AUX AC load to 30%.
9. Engine Start Master ................................................................... ON
10. Engine Start Switch..............................................................PRESS
CAUTION: CONTINUED USE OF THE STARTER IS LIMITED TO
THREE (3) CRANK CYCLES, WITH A MAXIMUM OF THIRTY (30)
SECONDS PER CYCLE. DELAY THREE (3) MINUTES BETWEEN
START ATTEMPTS. AFTER THREE (3) CYCLES, DELAY USE OF
STARTER FOR AT LEAST FIFTEEN (15) MINUTES.
11. Start Valve and Ignition .............................................................. ON
NOTE: If IGN mnemonic is not displayed on EICAS, the start may be
salvaged by selecting AIR START IGN to ON prior to opening HP fuel
cock.
12. Positive LP RPM ................................................................. CHECK
13. HP Fuel Cock .......................................OPEN (15% HP MINIMUM)
NOTE: In high tail wind conditions, direction of rotation of LP may
initially be reversed and, if so, the HP fuel cock should not be selected to
OPEN until HP is stabilized. This ensures that LP rotation is positive.
Starts with tailwinds of up to 25 knots have been demonstrated.
NOTE: Ignition should occur within ten (10) seconds after selecting HP
fuel cock to OPEN.
Quick Reference Handbook
REVISION 7 NORMAL PROCEDURES
May 30/02 Page NC - 7
14. Start Valve and Ignition ............................................................ OFF
　
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