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庞巴迪环球5000公务机机组操作手册 Bombardier Global-限制(9)

时间:2011-11-11 09:36来源:蓝天飞行翻译 作者:公务机
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Maximum air speed for turbulence penetration is 300 KIAS or .80 Mach, whichever is lower.
NOTE
Turbulence penetration maneuvers must be accomplished in accordance with the procedures detailed in Chapter 7; SUPPLEMENTARY PROCEDURES . FLIGHT IN TURBULENCE.
H. Minimum Operating Limit Speed
Intentional speed reduction below the onset of stall warning, as defined by stick shaker operation, is prohibited.
VMCG is 80 KIAS and VMCA in the take-off configuration is 86 KIAS.

1. MANEUVERING LOADS
A. Maneuvering Limit Load Factors
These load factors limit the permissible angles of bank in turns and the severity of pull-up and push-over maneuvers:
.
Slats / flaps retracted: .1.0 G to +2.5 G.

.
Slats / flaps extended: 0.0 G to +2.0 G.

 

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LIMITATIONS SYSTEMS
1.  SYSTEMS
A. Air-Conditioning and Pressurization
.  
Pack discharge temperatures during manual mode temperature control operations must be kept between 5 °C and 60 °C.

.  
One pack must be selected off if pack control is in manual mode.

.  
The maximum relief differential pressure is 10.73 psi.


Effectivity:
.  
Airplanes 9127 thru 9158 not incorporating Service Bulletin:

.  
SB 700.1A11.21.004, Modification . Pressurization Control . Cabin Altitude Reduction During Flight for Improved Passenger Comfort.


The maximum relief differential pressure is 10.02 psi.
.  
The maximum negative relief differential pressure is .0.5 psi.

.  
During taxi and take-off, the pressure differential must not exceed 0.1 psi.

.  
During initial landing (at touchdown), the pressure differential must not exceed 1.0 psi.

.  
Auxiliary pressurization (AUX PRESS) system operations are prohibited at altitudes greater than 41,000 feet.

.  
APU bleed extraction above 45 °C OAT for air-conditioning operation is prohibited.

.  
Use of the EMER DEPRESS switch above 15,000 feet is prohibited.

B.
Automatic Flight Control System

.  
Maximum altitude for flight with the yaw damper disengaged is 41,000 feet.

.  
The minimum autopilot engage height is 400 feet AGL.

.  
The minimum autopilot use height is:
. For a precision approach (Category I or II ILS) is 50 feet AGL, and
. For a non-precision approach is 400 feet AGL.

 

JAA Certified Airplanes
.  
The minimum autopilot use height is: . For a precision approach (Category I or II ILS) is 80 feet AGL, and . For a non-precision approach is 400 feet AGL.

.  
Use of the NAV guidance panel switch for approaches with VOR as a NAV source is prohibited.
 
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