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SIDE PANELS:
32. Radar Controls..............................................................................AS REQUIRED
33. ICS Panels .....................................................................................AS REQUIRED
34. Oxygen Systems ..............................................................................ON / CHECK
35. Oxygen Masks ..............................................................................................TEST
36. Cockpit Lights...............................................................................AS REQUIRED
37. Warning Lights ..........................................................................................CHECK
38. RH Radio Rack Fan .....................................................................................AUTO
39. ISDU............................................................................................................CHECK
40. Tone Generator .............................................................................................TEST
NOTE:
For SPZ-8400 equipped aircraft, the Tone Generator
test is performed using the pilot’s Display Controller
TEST menu. Selecting TONE results in the test tone,
and a Klaxon™ (high-low, high-low) gear unsafe tone.
While in the test mode, the pilot can adjust tone
generator volume. Minimum tone volume is 80. The
test is completed by selecting the RETURN prompt to
return to the TEST menu.
41. Landing Gear Emergency Reset .................................................IN / SAFETIED
42. Emergency Gear Handle ..............................................................IN / SAFETIED
43. Cockpit Voice Recorder............................................................................CHECK
44. Flight Data Recorder ......................................................................................SET
45. Non-essential Static Source (If Installed) ......................................................ON
46. Emergency Flap Handle.......................................................................NEUTRAL
47. Emergency Flap Switch...................................................NORMAL / GUARDED
48. Smoke Detector ............................................................................................TEST
For airplanes SN 1000 through 1155 with ASC 157 and/or airplanes SN 1000 and
subsequent with ASC 268.
49. RH R/R Fan Indicator ..................................................................................AUTO
For airplanes SN 1156 and subsequent.
OPERATING MANUAL
03-03-00 EXPANDED NORMAL PROCEDURES
Page 2
May 30/02
Revision 7
INSTRUMENT PANELS:
50. Clocks ........................................................................................................CHECK
51. Display Controllers ...................................................................................CHECK
52. EFIS................................................................................................................TEST
53. EICAS.............................................................................................................TEST
54. IRSs .....................................................................................................NAV / TEST
55. ELWS Loadmeter ...............................................................................TEST / OFF
NOTE:
If the ELWS (loadmeter) is used for dispatch, refer to
GIV Airplane Flight Manual Appendix C:
OPERATIONAL PROCEDURES WITH CONVERTER
/ ALTERNATOR INOPERATIVE - ELWS INSTALLED.
Selecting ELWS loadmeter ON causes spurious
warnings unless the EPMP panel is properly
configured for ELWS use.
56. Standby Engine Instruments......................................................................AUTO
NOTE:
Check static indications with EICAS indications on first
flight of day.
57. Guidance Controller .................................................................................CHECK
58. Thrust Reverser Lights ............................................................................CHECK
A. REV ARM................................................................................................ON
B. REV Unlock / Deploy...........................................................................OUT
NOTE:
If either of both Unlock or Deploy lights are ON,
maintenance is required before flight.
59. Standby Attitude Indicator..................................................................UNCAGED
60. Standby Warning Lights Panel ......................................................AS DESIRED
NOTE:
Standby Warning Lights Panel is not installed on SPZ-
8400 equipped aircraft.
61. Fuel Quantity (Normal and Standby)..........................................................TEST
　
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