|
As seen in
Flying Magazine
"I
want to thank you guys again for giving me the best training available.
I feel confident that I could work for any airline in the world - guaranteed."
P.D. Sep-Oct 99 graduate
"The
Morris Family and Sheffield School have been in Aviation longer than
any other school around. My classmates who are now working as dispatchers
have told me that they know more and are better
trained than other dispatchers from other schools. Sheffield
does not in anyway just "crank-out" dispatchers; you will have to work
very hard. If you want to be a Dispatcher, go to the best school,
SHEFFIELD."
T.L.,
Sheffield Graduate, 12/2/97
|
FAA
Aircraft Dispatcher Knowledge Exam
MODEL DC-9
En Route Climb
|
OPERATING
CONDITIONS
|
W-1
|
W-2
|
W-3
|
W-4
|
W-5
|
|
CLIMB
SCHEDULE
|
LR
|
HS
|
LR
|
HS
|
HS
|
|
INITIAL
WEIGHT (X1000)
|
84
|
86
|
78
|
88
|
92
|
|
CRUISE
PRESS ALTITUDE
|
34,000
|
28,000
|
32,000
|
22,000
|
24,000
|
|
ISA
TEMPERATURE
|
ISA
|
ISA
|
ISA
|
ISA
|
ISA
|
|
AVG
WIND COMP (KTS)
|
20
HW
|
30
HW
|
10
TW
|
20
TW
|
40
HW
|
FIGURE
48 - DC-9 - En Route Climb
|
TIME,
FUEL, AND DISTANCE TO CLIMB
JT8D-1 ENGINES - NORMAL BLEED
DC-9 SERIES 10 - HIGH SPEED CLIMB SCHEDULE
CLIMB AT 320 KNOTS IAS TO 23500 FT ALTITUDE THEN CLIMB AT M .74
|
|
INITIAL
WEIGHT = 78000 POUNDS
|
|
PRES.
ALT.
FEET
|
TIME
MIN.
|
FUEL
BURNED
LB.
|
DIST.
N. MI.
|
|
0
|
0
|
0
|
0
|
|
2000
|
0.5
|
113
|
2.2
|
|
4000
|
0.9
|
227
|
4.6
|
|
6000
|
1.5
|
342
|
7.3
|
|
8000
|
2.0
|
457
|
10.2
|
|
10000
|
2.6
|
574
|
13.3
|
|
12000
|
3.2
|
693
|
16.8
|
|
14000
|
3.9
|
815
|
20.7
|
|
16000
|
4.6
|
941
|
25.0
|
|
18000
|
5.4
|
1070
|
29.9
|
|
20000
|
6.3
|
1205
|
35.4
|
|
22000
|
7.2
|
1347
|
41.7
|
|
24000
|
8.3
|
1498
|
49.0
|
|
26000
|
9.5
|
1661
|
57.6
|
|
26860
|
10.1
|
1736
|
61.8
|
|
26860
|
10.1
|
1736
|
61.8
|
|
28000
|
10.7
|
1813
|
66.2
|
|
30000
|
11.9
|
1953
|
74.6
|
|
32000
|
13.3
|
2102
|
84.2
|
|
34000
|
14.9
|
2267
|
95.4
|
|
36000
|
16.9
|
2456
|
109.2
|
|
|
INITIAL
WEIGHT = 82000 POUNDS
|
|
PRES.
ALT.
FEET
|
TIME
MIN.
|
FUEL
BURNED
LB.
|
DIST.
N. MI.
|
|
0
|
0
|
0
|
0
|
|
2000
|
0.5
|
120
|
2.4
|
|
4000
|
1.0
|
241
|
4.9
|
|
6000
|
1.5
|
363
|
7.7
|
|
8000
|
2.1
|
486
|
10.8
|
|
10000
|
2.7
|
610
|
14.2
|
|
12000
|
3.4
|
737
|
17.9
|
|
14000
|
4.1
|
868
|
22.1
|
|
16000
|
4.9
|
1002
|
26.7
|
|
18000
|
5.7
|
1141
|
31.9
|
|
20000
|
6.7
|
1286
|
37.9
|
|
22000
|
7.7
|
1439
|
44.6
|
|
24000
|
8.9
|
1602
|
52.5
|
|
26000
|
10.2
|
1780
|
61.9
|
|
26860
|
10.9
|
1863
|
66.5
|
|
26860
|
10.9
|
1863
|
66.5
|
|
28000
|
11.6
|
1948
|
71.4
|
|
30000
|
12.9
|
2104
|
80.8
|
|
32000
|
14.4
|
2274
|
91.7
|
|
34000
|
16.3
|
2464
|
104.6
|
|
36000
|
18.7
|
2693
|
121.3
|
|
|
INITIAL
WEIGHT = 80000 POUNDS
|
|
PRES.
ALT.
FEET
|
TIME
MIN.
|
FUEL
BURNED
LB.
|
DIST.
N. MI.
|
|
0
|
0
|
0
|
0
|
|
2000
|
0.5
|
117
|
2.3
|
|
4000
|
1.0
|
234
|
4.8
|
|
6000
|
1.5
|
352
|
7.5
|
|
8000
|
2.1
|
471
|
10.5
|
|
10000
|
2.7
|
592
|
13.7
|
|
12000
|
3.3
|
715
|
17.4
|
|
14000
|
4.0
|
841
|
21.4
|
|
16000
|
4.7
|
971
|
25.9
|
|
18000
|
5.6
|
1105
|
30.9
|
|
20000
|
6.5
|
1245
|
36.6
|
|
22000
|
7.5
|
1392
|
43.2
|
|
24000
|
8.6
|
1549
|
50.7
|
|
26000
|
9.9
|
1719
|
59.7
|
|
26860
|
10.5
|
1798
|
64.1
|
|
26860
|
10.5
|
1798
|
64.1
|
|
28000
|
11.1
|
1879
|
68.7
|
|
30000
|
12.4
|
2027
|
77.7
|
|
32000
|
13.8
|
2186
|
87.8
|
|
34000
|
15.6
|
2362
|
99.8
|
|
36000
|
17.7
|
2570
|
114.9
|
|
|
INITIAL
WEIGHT = 84000 POUNDS
|
|
PRES.
ALT.
FEET
|
TIME
MIN.
|
FUEL
BURNED
LB.
|
DIST.
N. MI.
|
|
0
|
0
|
0
|
0
|
|
2000
|
0.5
|
124
|
2.4
|
|
4000
|
1.0
|
248
|
5.1
|
|
6000
|
1.6
|
374
|
8.0
|
|
8000
|
2.2
|
500
|
11.1
|
|
10000
|
2.8
|
629
|
14.6
|
|
12000
|
3.5
|
760
|
18.5
|
|
14000
|
4.2
|
894
|
22.8
|
|
16000
|
5.1
|
1033
|
27.6
|
|
18000
|
5.9
|
1177
|
33.0
|
|
20000
|
6.9
|
1327
|
39.1
|
|
22000
|
8.0
|
1486
|
46.2
|
|
24000
|
9.2
|
1656
|
54.4
|
|
26000
|
10.6
|
1841
|
64.1
|
|
26860
|
11.3
|
1928
|
69.0
|
|
26860
|
11.3
|
1928
|
69.0
|
|
28000
|
12.0
|
2018
|
74.1
|
|
30000
|
13.4
|
2183
|
84.1
|
|
32000
|
15.0
|
2364
|
95.7
|
|
34000
|
17.1
|
2570
|
109.7
|
|
36000
|
19.7
|
2826
|
128.3
|
|
FIGURE
50 - Long-Range Climb Schedule
Contact
us at:
499
NW 70th Ave Suite 110
Ft. Lauderdale, FL 33317 - USA
Tel 800-843-8289, 954-581-6022
Fax 954-584-8980
email morris@sheffield.com
|
