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Beechcraft Beech 95 2017 - Time, Fuel, and Distance to Climb (4200 Lb)

Beechcraft Beech 95 2017
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Selkirk College IATPL Program Manual
Beech 95 POH Effective September 1, 2005 Appendix 14 - 46
Time, Fuel, and Distance to Climb (4200 lb)
Conditions:
4200 lb
Gear and Flaps up
Power 25” x 2500 rpm to full throttle altitude, then full throttle
Mixture full rich below 5000, then leaned per schedule on fuel flow gauge
Standard temperature
Notes:
Add 2.5 gallons of fuel for engine start, taxi and takeoff allowance.
Increase time, fuel, and distance by 10% for each 10°C above standard temperature.
Distances shown are based on zero wind
Weight
Lb
Pressure
Altitude
Ft.
Temp
C
Climb
Speed
KIAS
Rate of
Climb
Fpm
From Sea Level
Time
Min
Fuel
Used
Gallons
Distance
NM.
4200
S.L,
1000
2000
3000
4000
5000
6000
7000
8000
9000
10,000
11,000
12,000
13,000
14,000
15,000
16,000
17,000
18,000
15
13
11
9
7
5
3
1
-1
-3
-5
-7
-9
-11
-13
-15
-17
-19
-21
105
105
105
105
105
101
97
93
90
89
89
88
87
87
86
85
85
84
83
1005
955
905
855
805
755
705
655
605
556
506
456
406
356
306
256
206
156
106
0
1
2
3
4
6
7
9
10
12
14
16
18
21
25
28
31
38
48
0.0
0.7
1.3
2.0
2.7
3.5
4.3
5.1
5.9
6.9
7.8
8.8
9.8
11.2
12.7
14.1
15.5
18.4
22.7
0
2
4
6
8
11
14
17
20
24
29
33
38
45
53
61
70
86
111

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