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10. Second Pack Switch................................................................. OFF
(If COOL TURB HOT message is still displayed.)
11. Proceed to nearest suitable airport and land.
END
Quick Reference Handbook
ABNORMAL / EMERGENCY PROCEDURES REVISION 7
Page EH - 10 May 30/02
Temperature Range for Cowl Anti-Icing AFM 1-30-20
Quick Reference Handbook
REVISION 7 ABNORMAL / EMERGENCY PROCEDURES
May 30/02 Page EI - 1
Miscellaneous Index
Windshield Failure ....................................................................... EI-2
Overweight Landing .................................................................... EI-3
Ditching......................................................................................... EI-3
Emergency Airplane Evacuation ................................................ EI-6
Planned Airplane Evacuation ......................................................... EI-6
Emergency Escape Routes............................................................ EI-8
Related Topics In QRH
Landing Planning Data...............................................PC-1 thru PC-14
“G” Monitor System......................................................................EG-9
“G” Monitor Versus Airplane Gross Weight Charts....................EG-11
Quick Reference Handbook
ABNORMAL / EMERGENCY PROCEDURES REVISION 7
Page EI - 2 May 30/02
Windshield Failure AFM 4-25-10
If windshield heat failure is detected, cycle the windshield heat control
OFF, then ON. If windshield heat can not be regained, flight may be
continued, but flight into icing conditions should be avoided. If failure
involves a front window, pull appropriate circuit breaker:
• L FRONT POWER (or L FRONT POWER or L FRONT WSHLD):
CP, J-8
• R FRONT POWER (or R FRONT POWER or R FRONT WSHLD):
CP, K-8
• L SIDE PWR (or L SIDE WSHLD): CP, J-10
• R SIDE PWR (or R SIDE WSHLD): CP, K-10
Windshield crack(s):
1. Upon detection of a crack in outer heating / protective windshield
ply, immediately turn windshield heat OFF on affected panel by
pulling the appropriate circuit breaker listed above and observe
icing restrictions.
2. Upon detection of a crack in either main structural windshield ply,
a reduction of cabin pressure differential to 7.5 psi is
recommended for remainder of flight.
3. Maintain current airspeed / mach or slower for remainder of flight.
4. Refer to GIV AFM Configuration Deviation List - Appendix B for
subsequent takeoff considerations.
WARNING: IF CRACKING IS TO THE INNER GLASS PLY, IT
IS RECOMMENDED THAT THE PILOT ADJACENT TO THE
CRACK AREA WEAR EYE PROTECTION SUCH AS SMOKE
GOGGLES.
END
Quick Reference Handbook
REVISION 7 ABNORMAL / EMERGENCY PROCEDURES
May 30/02 Page EI - 3
Overweight Landing AFM 4-20-10
If landing at a weight in excess of Maximum Landing Weight is
unavoidable:
1. Plan to land on the longest available runway.
2. See Landing Planning Data (pages PC-1 thru PC-14) for landing
field length requirements.
NOTE: Data contained in Landing Planning Data for overweight landings
are predicted data and have not been verified by field performance test.
3. Minimize sink rate and crab at touchdown.
4. During landing rollout, maximum authorized reverse thrust should
be used.
5. Report overweight landing for appropriate maintenance
inspections.
CAUTION: TIRE SPEED LIMITATIONS WILL BE EXCEEDED IF
TOUCHDOWN IS MADE IN EXCESS OF 182 KNOTS GROUND SPEED.
(195 KNOTS GROUND SPEED WITH ASC 190 AND SN 1214 AND
SUBSEQUENT).
NOTE: For airplanes SN 1156 and subs., and airplanes SN 1000 through
1155 with ASC 118, the overweight landing inspection may not be
required if the recorded landing vertical acceleration is within limits. See
‘G’ Monitor System, page EG-9, for additional information.
END
Ditching AFM 4-20-20
1. No tests or actual ditching have been made. The following
procedures will improve the chances of a successful ditching.
2. Plan the descent and ditching to ensure minimum fuel remaining,
but ample fuel aboard to make controlled power-on.
3. At approximately 2000 ft., make an appraisal of sea surface
conditions and choose a ditching heading. The ditching heading
should be parallel to and on the highest crest of the dominant wave
pattern.
4. Check that all passengers have donned life vests and are
cautioned not to inflate them until they have evacuated the airplane.
Continued on next page →
Quick Reference Handbook
ABNORMAL / EMERGENCY PROCEDURES REVISION 7
Page EI - 4 May 30/02
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