CEAPR DR400/135CDI User Manual

Supplement POH DR400/120D, DR400/140B,
DR400/180R, DR400/200R, DR400/RP
Page 5 - 10 Issue 3 – July 2014
CRUISE PERFORMANCE
At maximum takeoff weight 980 kg (2161 lb), in standard atmosphere.
Range and endurance calculations take into account 45 min. reserve (at
55% load) at destination.
Assumption is made that higher consumption for climb is compensated
by a cruise descent.
Range assumes no wind.
Standard Tank ............................................................... 109 liters usable
Standard and Auxiliary Tanks ....................................... 159 liters usable
Press.
Alt.
ISA conditions
Standard Tank
109 Liters
Standard and
Auxiliary Tank
159 Liters
Engine
Load
Fuel flow
[ft]
[%]
KCAS
KTAS
[l/h]
NM
Hours
NM
Hours
2000
75
108
111
21.2
496
4.5
758
6.8
2000
70
104
107
19.6
516
4.8
788
7.4
2000
65
100
103
18.1
537
5.2
821
8.0
2000
60
95
98
16.7
555
5.7
848
8.7
2000
55
88
91
15.3
562
6.2
859
9.5
2000
50
79
81
13.9
554
6.8
846
10.4
4000
75
107
114
21.2
508
4.5
776
6.8
4000
70
103
109
19.6
526
4.8
804
7.4
4000
65
99
105
18.1
548
5.2
837
8.0
4000
60
94
99
16.7
564
5.7
862
8.7
4000
55
87
92
15.3
570
6.2
871
9.5
4000
50
78
82
13.9
561
6.8
857
10.4
6000
75
107
117
21.2
520
4.5
794
6.8
6000
70
102
112
19.6
537
4.8
821
7.4
6000
65
98
107
18.1
559
5.2
854
8.0
6000
60
93
101
16.7
576
5.7
880
8.7
6000
55
85
93
15.3
579
6.2
885
9.5
6000
50
76
84
13.9
569
6.8
870
10.4
Table 5-11 Cruise performance, 2000 – 6000 ft
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CEAPR DR400/135CDI Specifications

General

Brand	CEAPR
Model	DR400/135CDI
Category	Aircrafts
Language	English