QNH—MB
970
975
980
985
990
995
1,000
IN. Hg
28.64
28.79
28.94
29.09
29.23
29.38
29.53
CORRECTION
—
FEET
+ 1,500
+ 1,350
+ 1,250
+ 1,100
+ 950
+ 800
+ 650
QNH—MB
1,005
1,010
1,015
1,020
1,025
1,030
1,035
IN. Hg
29.68
29.82
29.97
30.12
30.27
30.41
30.56
CORRECTION
—
FEET
+ 550
+ 400
+ 250
+ 100
0
– 150
– 300
TAKEOFF
Before beginning the takeoff, the MAIN AIR
VLV switches must be set to CLOSE. Check
that both MAIN AIR VALVE annunciators are
extinguished. Check that the F/DK VLV switch
is set to CLOSE. Check that the PRESSN
switch is set to AUTO.
AFTER TAKEOFF
As soon as practicable after takeoff, position
the MAIN AIR VLV switches to OPEN. Check
that MAIN AIR VALVE annunciators are ex-
tinguished. Check that the DUCT OVHT
↑
annunciator remains extinguished. Adjust the
cabin RATE of change knob to obtain the de-
sired rate of climb appropriate to the top of
climb height.
If the airplane fails to pressurize during the
climb, it may be due to an auto mode mal-
function. Select the PRESSN switch to OVRD;
this will ensure that the fan-oprated venturi,
normally operating on the ground to hold the
outflow valves open, is switched off.
In the event of cabin altitude not being con-
trolled satisfactorily by the cabin pressure con-
trol, turn the MANUAL CABIN ALTITUDE
CONTROL slightly in the INCREASE direc-
tion. The PRESSURIZATION CONTROL
lever should then be turned to the GROUND
TEST position after which the MANUAL
CABIN ALTITUDE CONTROL can be used to
attain the required cabin altitude.
DURING FLIGHT
Check that the cabin altitude and temperature
are maintained satisfactorily. Crew compart-
ment temperature may be increased indepen-
dently of the cabin by operation of the F/DK
VLV switch.
DESCENT
At the start of descent, set the cabin pressure
control according to Table 12-1 for the desti-
nation airfield. Adjust the cabin RATE of
change knob to give the desired rate of descent.
This should not exceed 300 ft/minute.
BEFORE LANDING
The cabin altitude setting for landing depends
upon the destination barometric pressure (QNH).
Apply the correction given in Table 12-1 for the
appropriate barometric pressure (QNH) to the air-
field elevation. Then set that value on the outer
scale of the CABIN CONTROLLER.
Close the main air valves before the aircraft
descends below 250 feet to reduce engine
12-7
FOR TRAINING PURPOSES ONLY
HAWKER 800 XP
PILOT TRAINING MANUAL
FlightSafety
international
Table 12-1. CABIN ALTITUDE SETTING FOR LANDING
Summary of Contents for 800 XP
Page 4: ......
Page 6: ......
Page 10: ......
Page 104: ......
Page 124: ......
Page 126: ......
Page 156: ......
Page 158: ......
Page 160: ......
Page 170: ......
Page 172: ......
Page 174: ......
Page 184: ......
Page 186: ......
Page 198: ......
Page 200: ......
Page 202: ......
Page 222: ......
Page 264: ......
Page 266: ......
Page 268: ......
Page 276: ......
Page 278: ......
Page 280: ......
Page 290: ......
Page 292: ......
Page 310: ......
Page 312: ......
Page 314: ......
Page 328: ......
Page 338: ......
Page 340: ......
Page 342: ......
Page 352: ......
Page 354: ......
Page 356: ......
Page 378: ......
Page 412: ......
Page 414: ......
Page 416: ......
Page 474: ......
Page 476: ......
Page 478: ......
Page 486: ......
Page 500: ......
Page 502: ......
Page 504: ......