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action. For additional information, refer to Chapters 5 and 31 of the GIV
Maintenance Manual.
END
Quick Reference Handbook
REVISION 7 ABNORMAL / EMERGENCY PROCEDURES
May 30/02 Page EG - 11
‘G’ Monitor Versus Airplane Gross Weight OM 2A-31-32
Quick Reference Handbook
ABNORMAL / EMERGENCY PROCEDURES REVISION 7
Page EG - 12 May 30/02
‘G’ Monitor Versus Airplane Gross Weight, ctd… OM 2A-31-32
Quick Reference Handbook
REVISION 7 ABNORMAL / EMERGENCY PROCEDURES
May 30/02 Page EH - 1
Pneumatics Index
Bleed Air / ECS System Diagram................................................. EH-2
Loss of Pressurization............................................................... EH-3
Emergency Descent Procedure ................................................ EH-3
Loss of Automatic Pressurization Control .................................... EH-4
Pressurization System - Rate Limiting ......................................... EH-5
Bleed Air System Failure.............................................................. EH-6
Air Conditioning System Shut Down or Inoperative ..................... EH-7
Air Conditioning System Airflow Hot or Uncontrollable ................ EH-8
Left or Right Cooling Turbine Hot................................................. EH-9
Temperature Range For Cowl Anti-Icing ................................... EH-10
Quick Reference Handbook
ABNORMAL / EMERGENCY PROCEDURES REVISION 7
Page EH - 2 May 30/02
Bleed Air / ECS System Diagram
Quick Reference Handbook
REVISION 7 ABNORMAL / EMERGENCY PROCEDURES
May 30/02 Page EH - 3
Loss Of Pressurization AFM 4-22-10
If cabin pressurization is lost, proceed as follows:
1. Crew Oxygen Masks ............................................................... DON
2. Emergency Descent Procedure (Page EH-3) ...................INITIATE
3. Passenger Oxygen Masks ............................MANUALLY DEPLOY
NOTE: Visually check for deployment and advise passengers to DON
masks.
END
Emergency Descent Procedure AFM 4-22-20
The following procedure assumes structural integrity of airplane.
If airplane structural integrity is in doubt, limit speed as much as
possible and avoid high maneuvering loads.
1. Power Levers ...........................................................................IDLE
2. Airspeed .................................................... ESTABLISH MMO / VMO
NOTE: An initial pitch attitude of 8° to 10° nose down is recommended
to commence descent. As speed approaches MMO / VMO, adjust pitch
attitude as necessary to avoid an overspeed condition.
3. Speed Brakes....................................................................EXTEND
4. Airspeed .......................................................MAINTAIN MMO / VMO
NOTE: It is recommended that the emergency descent be flown
manually in order to achieve maximum descent rate.
5. Transponder Code .......................................................... SET 7700
6. Air Traffic Control (ATC)..................................................... NOTIFY
7. Level Off ...........................................................................................
......15,000 FT, OR MINIMUM ENROUTE ALTITUDE, IF HIGHER
Approach and Landing:
8. Normal Approach .......................................................... PERFORM
9. Gear ..................................................................DOWN / 3 GREEN
Continued on next page →
Quick Reference Handbook
ABNORMAL / EMERGENCY PROCEDURES REVISION 7
Page EH - 4 May 30/02
Emergency Descent Procedure, ctd… AFM 4-22-20
If unable to get gear down for landing and a gear-up landing is
planned:
10. Pressurization....................................................................MANUAL
11. Outflow Valve .........................................................................OPEN
12. Airplane .................................................. LAND UNPRESSURIZED
END
Loss Of Automatic Pressurization Control AFM 3-22-30
1. AUTO / MANUAL Switch...................................................MANUAL
2. DADC Selector Switch .............OPPOSITE DADC (DADC 1 OR 2)
3. AUTO / MANUAL Switch........................................................AUTO
If automatic pressurization control is not regained:
4. AUTO / MANUAL Switch...................................................MANUAL
Manually control cabin pressure as described in GIV OM Section
2A-21-20: Pressurization System.
NOTE: When operating in manual, the rate of change should be
monitored to maintain a maximum of 500 feet per minute UP or 300 feet
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