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SUPPLEMENT 58
FIVE--BLADED PROPELLER
MXCL - SPEEDS (IAS - 170 KIAS/M 0.40)
Conditions :
-
Maximum climb power TRQ = 100 %
-
Landing gear and flaps UP
-
IAS = 170 KIAS / M 0.40
-
"BLEED" switch on "AUTO" or "BLEED HI" MSG ON
Pressure
Airplane
Altitude
weight
(feet)
SL
2000
5794 lbs
4000
(2628 kg)
6000
8000
SL
2000
6594 lbs
4000
(2991 kg)
6000
8000
SL
2000
7394 lbs
4000
(3354 kg)
6000
8000
NOTE :
In SL ISA conditions, nominal Np is of 1985 RPM.
Page 9.58.20
ISA
ISA
- 20°C
- 10°C
2 420
2 390
2 385
2 355
2 345
2 315
2 305
2 270
2 260
2 225
2 075
2 050
2 045
2 015
2 010
1 985
1 975
1 940
1 930
1 900
1 800
1 775
1 770
1 745
1 735
1 710
1 705
1 670
1 660
1 635
Figure 5.10.2 - MXCL - SPEEDS (IAS - 170 KIAS/M 0.40)
PILOT'S OPERATING HANDBOOK
RATE OF CLIMB (ft/min)
ISA
ISA
+ 10°C
2 365
2 335
2 325
2 295
2 280
2 250
2 235
2 205
2 190
2 155
2 025
2 000
1 990
1 965
1 950
1 920
1 910
1 880
1 870
1 835
1 755
1 730
1 720
1 695
1 685
1 655
1 645
1 615
1 605
1 575
ISA
ISA
+ 20°C
+ 30°C
2 310
2 285
2 265
2 235
2 220
2 190
2 170
2 140
2 120
2 085
1 975
1 955
1 935
1 910
1 895
1 865
1 850
1 820
1 805
1 770
1 710
1 685
1 670
1 645
1 630
1 605
1 590
1 560
1 545
1 515
Edition 0 -- October 31, 2013
Rev. 1
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