METRO III – ICAO ANNEX 8 PART I – SUPPLEMENTAL TAKEOFF PERFORMANCE
CONTENTS ITEM
PAGE
Maximum Takeoff Weight Limitation Chart – Dry, Bleed Air Off .......................................................... 4I-1 Takeoff Speed Schedules – Dry, Bleed Air Off .................................................................................... 4I-2 Distance to Accelerate to V1 and Stop – Dry, Bleed Air Off ................................................................. 4I-9 Single Engine Takeoff Distance to 35 Foot Height – Dry, Bleed Air Off ............................................ 4I-10 Single Engine Takeoff Run Distance – Dry, Bleed Air Off ................................................................. 4I-12 Maximum Takeoff Weight Limitation Chart – Wet .............................................................................. 4I-15 Takeoff Speed Schedules – Wet ....................................................................................................... 4I-16 Distance to Accelerate to V1 and Stop – Wet .................................................................................... 4I-23 Single Engine Takeoff Distance to 35 Foot Height – Wet .................................................................. 4I-24 Single Engine Takeoff Run Distance – Wet ....................................................................................... 4I-26 Takeoff Flight Path Distance to 1500 Foot Height ............................................................................. 4I-28
FAA APPROVED: MAR 18/92
PERFORMANCE
4I-i 8AC
METRO III – ICAO ANNEX 8
THIS PAGE LEFT BLANK INTENTIONALLY
4I-ii 8AC
PERFORMANCE
MANUFACTURER'S DATA ISSUED: MAR 18/92
METRO III - ICAO ANNEX 8 MAXIMUM TAKEOFF WEIGHT LIMITATION ASSOCIATED
CHART - DRY, BLEED AIR OFF NOTE
CONDITIONS:
(DRY) POWER . . . . .. .. . . . . .. .._.._......... TAKEOFF GEN LOAD . . . . . . . . . . . . . . .._................. 300 AMPS BLEED AIR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. . .. . . . .. . .. . . OFF ENG ANTI-ICE . . . . . . . . . . . . . .. OFF (SEE NOTE) GEAR . . .. . . . .. . .. . . . .. . .. . .. . . . .. . DOWN (TAKEOFF) UP (SECOND AND THIRD SEGMENT) FLAPS . . . . . . . . . . . . . . . . . . . . . . . . . . . .. . .. . . l/4 (TAKEOFF) UP (ENROUTE)
l
l
l
REDUCE TAKEOFF WEIGHT WITH ENGINE ANTI-ICE ON. MAXIMUM
OAT
WITH
ENGINE
BY
1,125
ANTI-ICE
POUNDS
ON
(510
kg)
IS 5°C.
THIS WEIGHT IS THE MAXIMUM AT WHICH TAKEOFF CAN BE CONTINUED AFTER AN ENGINE FAILURE IS RECOGNIZED AT OR ABOVE V, .
EXAMPLE: GIVEN: OBTAIN:
OAT = 26°C PRESSURE ALTITUDE = 5,500 FEET TAKEOFF WEIGHT = 12,500 POUNDS
(1675 m) (5670 kg)
16
6
8
FAA APPROVED: MAR 18/92
FIGURE 41-l PERFORMANCE
COP
gz
TAKEOFF
SPEED
SCHEDULE
(KIAS)
- DRY, BLEED
AIR OFF -ICAUTION
lPoUNDs1
. REFER
I
‘AH! i I RLT (FT)
CIUTSIDE
---l-
S.L.
115 112 110 107 1011 102 101 101 102 103 103 103
115
z
++ 08 E 1001 i:, Ei 02 03 m 03
---I16000 15500 15000 111500
200’
115 113 110 108
105 102 101 101 102 102 103 103 103
tt
113
1211 106
111
122
103
110 112 1111 116 118 119 121
123 121 126 129 131 133 135
101 100 101 101 102 103 103
RIR
I
-10 150
16000 15500 15000 111500 111000 13500 -t13000 12500 12000 11500 11000 10500
1
. TAKEOFF IN TEMPERATURE AND ALTITUDE CONDITIONS SHOWN TO THE RIGHT OF AND ABOVE THE SOLID, STEPPED LINE IS NOT APPROVED. THE SPEEDS IN THAT AREA OF THE CHART ARE PROVIDED FOR INTERPOLATiON ONLY.
120
IS 108
3
E 101 101 m-i 102 103 103 103
111 110 112 11Y 116 118 119 121
116 113 111 108 10s 103 101
120 118 116 1111 113 111 110
FE 102 103 i-m 103
& 115
1111 113
117 i-n 120
116 120 1111 jlfJ 111 116 108 1111 113 ii2 111 101 110 100 110 101 i-i-2 101 1111 102 116 103 118 103 120
129
117
128 126 125 1211 122 122 123 125 127 130 132 134
11Y 112 109 106
129 128 126 125 123 122 121 122 124 126 129 131 1311
117 115 112 110 107 1ou 102 101
129 127 126 125 123 122 121 121 123 125 127 130 132
118 116 113 111 108 105 103
1011
101 100 100 101 102 103 103
100
100 101 102 103
101
100 100 100 101 102
-
41-l
TEMPERRTURE 10
Vl
TO FIGURE
FOR MAXIMUM
-
57
TAKEOFF
YO
I
-
I
c
V2
-
,
VP
120
120
I% 1111 113 111 109 109 109 110
!I! 1lY
117 115 ii-2 110 107 1011 102 101 100 100 101 102 103 -
120 ii8 i-z 1111 113 iii 109
118 116 113 111 1oB 105 103 101 100 100 100 101 102
120
ii6 116 -
% 109 110 in 1111 -
126 121 123 122 120 120 121 122 12Y 126 128
115 112 110 107 105 103 102 101 101 100 101
115 112 110 107 105 103 102 101 101 100 101
H 1111 113 i-i-l 109 5% 109 109 110 112
55
-
117 u 112 109 pzlJ 1OY 101 100 ml 101 102 i-m 103 -
116 1111 113 111 109 109 109 110 111 113 116
WEIGHTS.
(‘Cl 20
I
PERMISSIBLE
iii
tfi! 109 109 i-m 109 109 i-B 110 118 i-is 1111 113 i-r id 109 I 109 / 109 I 109 I i-m I 110 I -
12u 123 122 121 u 119 119 119 119 120 120 121
-
109 108 rm 107 106 105 1011 -
i-i-T 109 109 m 109 109 im 110 -
119 118 118
110 109 108 106 107 106 105
110
109
#i 108 107 106 105
EE! 109 109 109 110
118 118 118 119 119 119 120
110 109 109 108 107 106
110 glJ 109 109 109 109 108 ~ 107 109 _106 110
118 118 118 119 119 119
119 119 120 120
116 123 11Y 122 113 I _121 111 120 !,
#ii I 118 iTi% I 119 109 I 119 109 I 120 109 I 120 110 I 120
7c) D 0 D z z
m x 00
TAKEOFF
SPEED
SCHEDULE
(KIAS)
1 POUNDS
- DRY, BLEED
AIR OFF
1
* TAKEOFF IN TEMPERATURE AND ALTITUDE CONDITIONS SHOWN TO THE RIGHT OF AND ABOVE THE SOLID. STEPPED LINE IS NOT APPROVED. THE SPEEDS IN THAT AREA OF THE CHART ARE PROVIDED FOR INTERPOLATION . REFER
OUTSIDE RESS 121 T
CROSS MT I
FTI
ILBs'
.,_.
!
-30
a
...
"1
"R
"2
"50
"1
!
"R
"2
16000 116 116 120 129 116 116 120 35500 113 113 118 128 1111 1111 118 15000 111 111 116 126 112 112 116 1'4500 108 108 1111 125 109 109 1111 Itllnnnl~ncilnclllall~lll,ncl,ncl,~all~~lln~llnll~l~ll~ai~nallnnl~~~l~~~l 13500 103 103 111 122 1011 1OU 111 13000 101 101 110 122 101 101 109 100 100 111 123 100 100 110 12500 12000 101 101 113 125 100 100 111 11500 102 102 115 128 101 101 113 11000 103 103 117 130 102 102 115 10500 103 103 119 133 103 103 117 10000 103 103 120 1311 103 103 119
-I I.e”Y”
3000
-10
16000 15500 15000 111500 111000 13500
I”.,
116 1111 111 108 106 103
,“.I
116 llll 111 108 106 103
II.J
120 118 116 1111 113 111
IL.a
129 128 126 125 12Y 122
IV”
117 115 112 109 107 1011
I””
117 115 112 109 107 1011
l&cl
120 118 116 114 113 111
0
RlR
!
41-l FOR MAXIMUM
TEMPERFITURE 10
,
TO FIGURE
PERMISSIBLE
TAKEOFF
WEIGHTS.
I’CJ
!
20
110
!
"50
"1
"R
"2
"50
"1
"R
"2
"50
"1
"R
"2
"50
129 127 126 125
117 115 113 110
117 115 113 110
120 118 116 llli
129 12’ 126 12’4
119 117 1111 112
119 117 1111 112
120 118 116 1111
178) 127 125 121
118
118
118
126
IL.,
I”.
I”<
LLLI
,L.A
I”_
IYJ
IIJ
ILJ
111,111
122 121 122 123 126 128 131 133
105 102 100 100 100 101 102 103
105 102 100 100 100 101 102 103
111 109 109 110 111 113 115 117
122 120 120 121 123 125 128 130
106 1OY 102 101 100 100 101 101
106 10’4 102 101 100 100 101 101
111 109 109 109 109 110 112 1111
121 120 120 120 121 122 12Y 126
108 106 1OU 103 102 101 100 100
115 115 1111 ,,C.l,,sl,,al,~fll LlJ Al.2 108 111-?21 111 111 111 106 109 119 109 109 109 108,109 1OY 109.119..108 103 lC!s 120 107 107 109 IO.2 109 120 107 107 109 lOkJJj9 121 106 106 109 lO0 109 121 105 105 109 100 111 122 1OU 1OY 110
129 127 126 125 123 122
118 116 113 111 108 106
118 118 113 111 108 106
120 118 116 11’4 113 111
128 127 125 124 123 121
120 117 115 112 110 107
120 117 115 112 110 107
120 118 116 1111 113 111
128 128, 129 1211 122 121
116 11Y 111 109
116 1111 111 109
113 111
113 111
119 119
109 109 109
110 119 119 119
111 109 109 109 109 109 109 110
118 117 117 118 118 119 119 120
I‘rt.1LC
116 11Y 113 111
"1
"R
!
"2
l,J
1211 123 122 113 120 111
"50
121 IL” 119 118 118 119 119 119 120 120
55 I
,
"1
vR
I
110 109 109 108 107
I "2
I
110 109 109 108 107
"50
I
109 109 109 109 110
118 118 118 119 119
c)
D 0 D z z
uooo
IL3””
12000 11500 11000 10500 I 10000
5000
1tiUUU J5500 15000 111500 ,lUOOO 13500 13000 12500 12000 11500 11000 10500 10000
I””
101 101 102 103 I 103
lib 1111 111 109 106 103 101 100 101 101 102 103 103
‘“IJ
IIU
ILL
I””
I”3
ICI
101 101 102 103 103
112 1111 116 118 120
125 127 129 132 1311
100 101 101 102 I 103
LU”
100 101 101 102 103
110 112 1111 116 118
122 12U 126 129 131 I
101 100 100 101 102
101 100 100 101 102
109 120 110 122 111 123 113 125 1151128 I
102 102 101 100 101
102 102 101 100 101
109 109 109 110 112
120 IOU 104 109 119J&dw,~ua 120 103 103 109 120 107 107 121 102 102 109 120 107 107 122 101 101 109 121 106 106 12Y,101,101,110,121,105,105,110,120
116 1111 111 109 106 103 101 100 101 101 102 103 103
120 118 116 1111 113 111 109 110 112 113 115 118 119
129 127 126 125 123 122 121 122 12U 126 128 131 133
118 115 113 110 108 105 102 101 100 100 101 102 102
118 115 113 110 108 105 102 101 100 100 101 102 102
120 118 116 11’4 113 111 109 109 110 111 112 114 117
128 127 128 121 123 122 120 120 121 123 125 127 130
119 111 1111 112 109 107 1OU 102 102 101 100 101 101
119 117 1111 !12 :09 107 1011 102 102 101 100 101 101
120 118 116 1111 113 111 109 109 109 109 110 111 113
118 116 113 111 108 106 1011 103 102 102 101 100
118 116 113 111 108 106 1011 103 102 102 101 100
118 116 11’4 113 111 109 109 109 109 109 110 111
126 175 123 122 121 119 119 120 120 120 121 122
128, ;2S 27 12Y 122 121 120 120 120 121 122 12Y 126
1111 112 110 107 106 105 1011 1011 102 101
1111 112 110 107 106 105 104 1OY 102 101
1111 113 111 109 109 109 109 109 109 110
123 122 120~‘111 119 110 119 109 119 108 119 108 120 101 120 107 121 106
111 110 109 106 108 m 107 106
ii0 109 108
110 109 108
109 109 110
i~9~109~110~119 I I
118 118 119
m x 00
3
METRO III â&#x20AC;&#x201C; ICAO ANNEX 8
THIS PAGE LEFT BLANK INTENTIONALLY
4I-4 8AC
PERFORMANCE
FAA APPROVED: MAR DATA 18/92 MANUFACTURER'S ISSUED: MAR 18/92
FIGURE 41-2 (continued) PERFORMANCE
METRO III - ICAO ANNEX 8
FAA APPROVED: MAR 18/92
41-5 8AC
41-6 8AC
FAA APPROVED: MAR 18/92
METRO III - ICAO ANNEX 8
FIGURE 41-2 (continued) PERFORMANCE
2
TAKEOFF
SPEED
SCHEDULE
(KIAS)
-DRY,
BLEED
AIR OFF . TAKEOFF IN TEMPERATURE AND ALTITUDE CONDITIONS SHOWN TO THE RIGHT OF AND ABOVE THE SOLID, STEPPED LINE IS NOT APPROVED. THE SPEEDS IN THAT AREA OF THE CHART ARE PROVIDED FOR INTERWLATKIN . REFER
WJTSIDE ‘RESS LIIT
iFi’
GROSS UT 1 Iii’
I )I
I ‘11
-30 I
%I
I
I
v2~v50~
I ‘11
-10 I ‘RI
0 I v2~v5Cl~
‘11
‘RI
,
AIR
!
‘21’501
‘11
TEMPERRTURE 10 ,
(
TO FIGURE
‘RI
, v21v5~1
‘1
1 ‘RI
,
3000
UOOO
5000
116 113 111 108 106 1OU 102 100 101 101 102 103 103 103
116 113 111 106 106 1011 102 100 1L31 101 102 103 103 103
119 118 116 115 113 112 111 110 112 ~~~ 113 115 117 119 120
129 127 126 125 12U 123 122 122 121 ~_ 126 128 130 132 131
116 1111 112 109 107 1OU 102 101 100 ~~ 101 101 102 103 103
116 1111 112 109 107 1011 102 101 100 ~~~ 101 101 102 103 103
119 118 116 115 113 112 110 110 110 112 113 115 117 119
129 127 126 125 12U 123 121 121 122 1211 126 126 130 132
117 115 112 110 108 196 103 101 100 100 100 101 102 102
117 115 112 110 108 106 103 101 100 :oo :OO 101 102 102
119 129 118 127 116 126 115 125 113 123 112 122 121 110 109 120 109 121 1101122 111 123 113 125 115 127 117 130
119 >lb 1111 112 110 107 105 103 102 101 100 100 100 101
7257 7000 6800 6600 6UO0 6200 6000 5800
116 113 111 109 106 1011 102 100
116 113 111 109 106 1011 102 100
119 118 116 115 113 112 110 110
129 128 126 125 121 123 122 122
sfinn
in0
100
iii
173
30 11800 4600
._ 102 103 103
01 -02 102 103 103
113 1111 116 118 119
125 127 129 131 133
117 114 112 110 107 105 103 LO1 ion 100 101 101 102 103
117 11U 112 110 107 105 103 101 inn 100 101 101 102 103
119 118 116 115 113 112 !lO 109 110 111 112 1111 116 117
129 127 126 125 121 122 121 121 121 123 1211 126 129 131
118 116 113 111 109 107 1011 102 101 101 100 100 101 102
118 116 113 111 !09 107 1011 102 101 101 lo0 100 101 102
119 128 1181127 116 125 115 124 113 123 112 122 110 121 109 120 1091120 1091121 110’122 1111123 113’125 115 127
7257 7000
116 1111
116 1111
119 118
129 127
118 115
118 115
119 118
128 127
107 1OU 102 100 100 101 101 102 103 103
107 1011 102 100 100 101 101 102 103 103
113 112 110 110 110 112 1111 115 117 119
12U 123 121 121 122 124 126 128 130 132
108 106 103 102 101 LOO 100 101 101 102
108 106 103 102 101 100 100 101 101 102
113 !12 110 109 109 110 111 i12 1111 116
123 122 121 120 121 122 123 125 127 129
6UO0 6200 6000 5800 I 5600 5uoo 5200 5000 U800 U600
110 107 105 103 102 101 101 100 100 101
110 107 105 103 102 :01 101 100 100 101
113 112-122 110 109 109 109 109 110 111 113
123 120 120 120 120 121 122 123 125
119
119
llb
118
1111 112 110 107 105 103 102 101 100 100 100 101
116 115 113 112 110 109 109 109 109 110 111 113
128 Izt’llS 125 12’4’113 123 122 121 120 120 120 121 122 123 126
120 117 115 113 110 108 106 1011 103 102 101 101 100 101
120 117 115 113 110 108 106 10’4 103 102 101 101 100 101
119 118 116 115 113 112 110 109 109 109 109 109 110 111
126 136 125 1211 123 121 120 120 120 120 120 121 122 12U
118
118
118
126
111 109 107 105 1011 103 102 102 101 101
111 109 107 105 1011 103 102 102 101 101,110
113 112 110 109 109 109 109 109 110
122 121 120 119 119 120 120 120 121 122
116 111 109 107 105 1OU 103 102 102 101 100
118 116 113 111 109 107 105 1011 103 102 102 101 100
TAKEOFF
WEIGHTS.
v2~v50~
118 116 115 113 112 110 109 109 109 109 109 109 110
YO
I,,
‘
7257 7000 6600 6600 6UO0 6200 6000 5800 5600 51100 5200 5000 11800 11600
PERMISSIBLE
[‘Cl 20 ,
!,
41-l FOR MAXIMUM
126 125 lZq’115 122 121 120 119 119 120 120 120 121 122
116 1111
116 1111
116 115
1211 123
108 106 105 1011 103 103 102 101
108 106 105 1011 103 103 102 101
110 109 109 109 109 109 109 110
120 119 ii9 119 120 120 121 121
115 113 111 108 107 106 105 1011 1011 103 102
115 113 111 IDS 107 106 105 10’4 1011 103 102
115 113 ll<u 110 109 109 109 109 109 109 110
123 122 120 119 119 119 120 120 120 121
“11
1111 112 110 109 108 lU/ 106 106 105 1011
‘RI
,v2(v.50j
‘1
j ‘RI ,
115 11U 112 110 109 108 llJ/ 106 106 105 1OU
115 121 113 120 I12 120 110 119 109 118 1091111_ 109 llY’110 109 119 109 119 109 120 110 120
109 109 108 107
‘21’50 I
110 109 109 108 107
I
109 109 109 109 110
118 118 118 119 119
110 109 108 108 -lU/ 107 106 105
110 109 108 108 101 107 106 105
110 109 109 109 109 109 109 110
118 118 118 118 119 119 119 120
110 110 109 LO8
110 110 109 108
109 109 109 110
118 118 118 119
110 109 109 108 108 107 107 106
110 109 109 108 108 107 107 106
110 109 109 109 109 109 109 110
117 117 117 118 UB 119 119 119
110 110 109
110 110 109
109 109 110
llf 11E 11s
,
c)
D 0 D z z
m x 00
CD*
gz
TAKEOFF
SPEED
SCHEDULE
(KIAS)
- DRY, BLEED
AIR OFF -ICAUTION]
ptiEicE1
. TAKEOFF IN TEMPERATURE AND ALTITUDE CONDITIONS SHOWN TO THE RIGHT OF AND ABOVE THE SOLID. STEPPED LINE IS NOT APPROVED. THE SPEEDS IN THAT AREA OF THE CHART ARE PROVIDED FOR INTERPOLATION ONLY. . REFER
BUTSIDE ‘AESS RLT IF71
GROSS
-30
10
41-l FOR MAXIMUM
PERMISSISLE
TAKEOFF
I-121 20
YO
55
IKG
’
"1
“I
“R
“2
“50
“I
“R
“2
“50
117 1111 112 109 4*-l ,“I 105 102 100 100 100 101
119 116 116 115 ,I? II4 112 110 109 110 111 113
129 127 126 125 ,r),l AC.? 122 121 121 122 123 125
116 116 1111 111 ,rlo LU.3
118 116 11’4 111 trio ,“il
119 118 116 115 112 1I.J
128 127 125 124 ,331 ILJ
6200 6000 5800 5600 5’400 5200
117 1111 112 109 ,*-I ,“I 105 102 100 100 100 101
107 1011 103 102 101 100
107 1011 103 102 101 100
112 110 109 109 109 110
122 121 124SOli 120 121 121
4800 5000 4600
102 103
102 103
117 115 118
130 127 132
100 101 101
101 100 101
112 111 1111
125 123 122
"Fl
"2 "50
"1
"R
"2 "50
120 117 115 113 II, 111
120 117 115 113 I,, ‘11
119 118!126 116 115 111 11J
I& 124 331 ILJ,I
116 114 ,I?
116 11’4 4,
116 115
1211 123
108 106 iQ3 lOi? 192
108 106 1011 103 lC2 102
112 110 109 109 109 109
121 120 120 120 120 120
lfdft 106 106 105 1O’I 103
108 106 105 1011 103
110 109 109 109 109
120 119 119 119 120
100 101 100
100 101 !OO
1108122 109 121 111 123
,103 102 101
102 103 101
109 110
121 120 121
"1
"R
"2 "50
"I
“R
“2
“50
“1
“R
“2
110
111 110
‘109 110
,
VU””
.A”
IA”
107 105 103 101 100 100 101 101 102 103
6’400 6200 6000 5800 5600 5UOO 5200 5000 -11800 4600 I
107 105 103 101 100 100 101 101 102 103 I
II.,
‘LIIIIL
113 112 110 109 109 111 112 1111 116 118
123 122 121 121 121 123 121 126 129 131
I
I
AIL
110 108 105 1011 102 102 101 100 100 101 I
I
*,.n,. 7257~116~118~119~128~120~120~119~128~ ..e ....^ ,^_ ..l”“”
8000
6800 6600 6400 6200 6000 5800 5600 5400 5200 5000 4800 4600
L&I
110 108 105 1011 102 102 101 100 100 101 I
123 111 122 109 120 107 120 105 120 1011 120 103 121 103 12111021102 123 101 1211 100 I
I
_.-
_.^
.^^
II>
II,
lltl
1.2,
11,
11,
lltr
lc!b
113 110 108 106 103 102 101 100 100 101 101 102
113 110 106 106 103 102 101 100 100 101 101 102
116 115 113 112 110 109 109 110 111 112 114 116
126 129 123 122 121 120 121 121 123 125 127 129
115 113 111 109 106 104 103 103 102 101 100 100
115 113 111 109 106 104 103 103 102 101 100 100
116 115 113 112 110 109 109 109 109 :09 110 111
122 121 120 119 120 120 120 121 121 123
,
,
,
_I.
‘L1LLI-llAlXlAlU
113 112 110 109 109 109 109 110 111 112
J12 110 108 106 105 10’4 1011 103 102 101
111 113y22 113 109 112 121 107 110 120 105 109 119 107 104 109 119 103~109~120~105~105~109~119 103 109 120 1011 109 120 1011 101 110 121 103 100 110 122 102 I
I1
1
I
112 110 106 106 105 1011 1011 103 102 101
1
113 112 110 109 109 109 109 109 109 110
“50
126
107 106 105
109 108 107 106 105
110 109 109 109 109
119 119 119 119 119
109 109 109 109
109 109 109 109
109 109 109 109
116 117 117 i1E
1011 1OU 103
104 103
109 110
120 120
108 108 107
IIJO 108 107
109 110
llblll 11 119
I
7000
WEIGHTS.
UT
7257 _ 7000 6800 6600 ci,nn “7”” 6000
FIJI? TEMPERATURE
0
-10
TO FIGURE
122 121 120 119 119 119 120 120 121 121
113
113
122
107
109
119
10’4 104 103 102
109 109 109 110
,
,
I
I
107 106 105 105 1011
119 120 120 121
107 106 105 105 104
109 109 109 109 110
I
I
I
I
I
I
I
I
I
I
I
IIll
1
I
1
1
1
1
1
I
111 J&&Q9 108 107 106 105 105 104 103
111 108 107 106 105 105 1011 103
112 110 109 109 109 109 109 109 110
120 119 119 119 119 119 120 120 120
109 108 108 107 106 106 105
109 108 106 107 106 106 105
109 109 GUY 109 109 109 110
109 109 109 109
119 119 119 120 120
109 109 109 109
109 109 109 109
116 116 117 116
109 109 109 109 110
116 116 117 116 119
I 1
118 116 lltr’lO9 119 119 119 120
1
I
109 109 109. 109
109 109 109 109 109
I
lie 118
sm
-I rlo 0 c)
D 0 D z 2 m x 00
METRO III - ICAO ANNEX 8 DISTANCE TO ACCELERATE ASSOCIATED
TO V, AND STOP -DRY,
BLEED AIR OFF
EXAMPLE:
CONDITIONS:
GIVEN:
(DRY) POWER ............................. TAKEOFF GEN LOAD.. ............................... .300 AMPS OFF BLEED AIR. ............................................ .............. OFF (SEE NOTE) ENG ANTI-ICE.. .............. DRY, HARD SURFACE RUNWAY.. FLAPS ....................................................... 114 41-2) DECISION SPEED ........ ‘.‘I (FIGURE NOSE WHEEL STEERING.. ..O N OR OFF
OBTAIN:
l
MAXIMUM TAKEOFF WEIGHT MAY NOT THE WEIGHT DETERMINED FROM FIGURE
OAT = 15°C PRESSURE ALTITUDE = 2,000 FEET GROSS WEIGHT = 15,000 POUNDS (6805 kg) HEADWIND = 20 KNOTS RUNWAY SLOPE = 1 PERCENT (UPHILL) V , SPEED = 114 KIAS ACCELERATE -STOP DISTANCE = 4,870 FEET (1485 m)
EXCEED 41-l.
8 GROSS
INCREASE PERCENT
ACCELERATE WITH ENGINE
. MAXIMUM WEIGHT
7
OAT
WITH
- STOP ANTI-ICE ENGINE
DISTANCE ON.
ANTI-ICE
ON
BY 3.5
IS5”C.
(1000 kg)
6
5
13
OAT (OC)
FAA APPROVED: MAR 18/92
GROSS
WEIGHT
(1,000
FIGURE 41-3 PERFORMANCE
POUNDS)
WIND IKNOTS)
RUNWAY SLOPE (PERCENT)
41-9 8AC
METRO III - ICAO ANNEX 8 SINGLE
ENGINE
TAKEOFF
c
DISTANCE
MA ,XIMUM
TO 35 FOOT
HEIGHT
NOTE OAT WITH ENGINE ENGINE
ANTI-ICE
ANTI-ICE
- DRY, BLEED
AIR OFF
ON IS 5°C.
EFFECTS
(METERS) 0
50
100
150
200
8,000
7,000
6,000
5 a
4,000
2,000
1,000
S.L. 0
200
400
600
800
(FEET) INCREASE IN TAKEOFF RUN DISTANCE WITH ENGINE ANTI-ICE ON
FIGURE 41-10 8AC
41-4
PERFORMANCE
FAA APPROVED:
MAR 18/92
METRO III - ICAO ANNEX 8 SINGLE
ENGINE
TAKEOFF
ASSOCIATED
DISTANCE
TO 35 FOOT
CONDITIONS:
HEIGHT
- DRY, BLEED
AIR OFF
EXAMPLE:
POWER .. ........ ................... TAKEOFF (DRY) GEN LOAD .......... .... ....... ........... .. 300 AMPS BLEED AIR .......... .... ....... ........ ... ............. OFF ENG ANTI-ICE .. ..... ... ... OFF (SEE GRAPH) RUNWAY .. ........ ..... DRY, HARD SURFACE V1 SPEED .............................. FIGURE 41-2 VR SPEED ............................. FIGURE 41-2 V2 SPEED _.............................FIGURE 41-2 FLAPS . ......... ... .... .... ........ .......................... II4 NOSE WHEEL STEERING ....ON OR OFF
GIVEN:
OAT = 10°C PRESSURE ALTITUDE = 2,000 FEET GROSS WEIGHT = 15,000 POUNDS (6805 kg) HEADWIND = 20 KNOTS RUNWAY SLOPE = 1 PERCENT (UPHILL) OBTAIN: V1 SPEED = 113 KIAS VR SPEED = 113 KIAS V2 SPEED = 116 KIAS TAKEOFF RUN = 5,770 FEET (1760 m)
NOTE
MAXIMUM TAKEOFF WEIGHT MAY NOT EXCEED THE WEIGHT DETERMINED FROM FIGURE 41-l.
FOR TAKEOFF FIELD LENGTH DETERMINATION, SINGLE ENGINE TAKEOFF DISTANCES ARE LONGER THAN TWO ENGINE TAKEOFF DISTANCES FACTORED BY 1.15. GROSS WEIGHT (1000 kg) 7 6 5
GROSS WEIGHT (1.000 POUNDS)
OAT (OC)
FIGURE FAA APPROVED:
MAR 18/92
WIND (KNOTS)
RUNWAY SLOPE (PERCENT)
41-4 (continued)
PERFORMANCE
41-l 1 8AC
METRO III - ICAO ANNEX 8 SINGLE ENGINE TAKEOFF RUN DISTANCE-DRY, / MAXIMUM
BLEED AIR OFF
OAT WITH ENGINE NoTE/ ANTI-ICE ENGINE
ANTI-ICE
ON IS 5°C.
EFFECTS
(METERS) 50
75
100
125
150
8,000
7,000
6,000
2,000
1,000
S.L. 100
200
300
400
500
(FEET) INCREASE IN TAKEOFF RUN DISTANCE WITH ENGINE ANTI-ICE ON
41-12 8AC
FIGURE 41-5 PERFORMANCE
FAA APPROVED: MAR 18/92
METRO III - ICAO ANNEX 8 SINGLE ENGINE TAKEOFF RUN DISTANCE-DRY, ASSOCIATED
BLEED AIR OFF
CONDITIONS:
EXAMPLE:
POWER . . . . . . . . . . . . . . . . . . . .. . . . . . . .. TAKEOFF (DRY) GEN LOAD .. . .. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 300 AMPS BLEED AIR .. . .. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF ENG ANTI-ICE . . .. . . . . . . . . . OFF (SEE GRAPH) SURFACE RUNWAY . . . . . . . . . . . .._.. DRY, HARD VI SPEED .. .. . . . . . . .. . . . . . . . . . . . . . . . . . . FIGURE 41-2 VR SPEED . .. . .. . .. . . . . . . . . . . . . . . . . . . . . FIGURE 41-2 41-2 V2 SPEED . . .. . . . . .. .. . . . . . . . . . .. . . . . . . . FIGURE FLAPS . . .. . . . . . . .. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. . .. . . . .. 114 NOSE WHEEL STEERING . . ..ON OR OFF
MAXIMUM TAKEOFF WEIGHT MAY NOT THE WEIGHT DETERMINED FROM FIGURE
GIVEN:
OAT = 10°C PRESSURE ALTITUDE = 2,000 FEET GROSS WEIGHT = 15,000 POUNDS (6805 HEADWIND = 20 KNOTS RUNWAY SLOPE = 1 PERCENT (UPHILL) VI SPEED = 113 KIAS VR SPEED = 113 KIAS V2 SPEED = 116 KIAS TAKEOFF RUN = 5,090 FEET (1550 m)
OBTAIN:
kg)
EXCEED 41-l.
GROSS 7
WEIGHT 6
(1 COO kg) 5
2
GROSS
FAA APPROVED: MAR 18/92
WEIGHT
(1,000
FIGURE 41-5 (continued) PERFORMANCE
POUNDS)
WIND
(KNOTS)
RUNWAY SLOPE (PERCENT)
41-13 8AC
METRO III â&#x20AC;&#x201C; ICAO ANNEX 8
THIS PAGE LEFT BLANK INTENTIONALLY
4I-14 8AC
PERFORMANCE
FAA MANUFACTURER'S APPROVED: MAR DATA 18/92 ISSUED: MAR 18/92
METRO III - ICAO ANNEX 8 MAXIMUM
TAKEOFF
ASSOCIATED
WEIGHT
LIMITATION
CHART
- WET NOTE
CONDITIONS:
POWER . . . . . . . . . . . . . . . . . . . . . . . . . . .. . TAKEOFF (WET) GEN LOAD . . . . . . . . . . .. . . . . . . . . . . . . . . . . . . . . . . 300 AMPS BLEED AIR . . . . . . . . . . .. . . . . . . .. . . . . . . . . . . . . . . . . . . . . . . . . . OFF ENG ANTI-ICE . .. .. . .. . . . . . . . OFF (SEE NOTE) (TAKEOFF) GEAR . . . . . . . . . . . . . . . . . . . . . . . . . . . .. DOWN UP (SECOND AND THIRD SEGMENT) FLAPS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . l/4 (TAKEOFF) UP (ENROUTE)
l
l
l
REDUCE TAKEOFF WEIGHT WITH ENGINE ANTI-ICE ON. MAXIMUM
OAT
WITH
ENGINE
BY
1,200
ANTI-ICE
POUNDS
ON
(545
kg)
IS 5°C.
THIS WEIGHT IS THE MAXIMUM AT WHICH TAKEOFF CAN BE CONTINUED AFTER AN ENGINE FAILURE IS RECOGNIZED AT OR ABOVE V, .
EXAMPLE: GIVEN: OBTAIN:
OAT = 32°C PRESSURE ALTITUDE = 5,500 FEET TAKEOFF WEIGHT = 13,080 POUNDS
(1675 m) (5935 kg) I 17
16
11
FIGURE FAA APPROVED:
MAR
18/92
41-6
PERFORMANCE
41-15 8AC
41-16 8AC
FAA APPROVED: MAR 18/92
METRO III - ICAO ANNEX 8
FIGURE 41-7 PERFORMANCE
FAA APPROVED:
41-7 (continued)
PERFORMANCE
FIGURE
METRO III - ICAO ANNEX 8
MAR 18/92
41-17 8AC
METRO III â&#x20AC;&#x201C; ICAO ANNEX 8
THIS PAGE LEFT BLANK INTENTIONALLY
4I-18 8AC
PERFORMANCE
FAA MANUFACTURER'S APPROVED: MAR DATA 18/92 ISSUED: MAR 18/92
8
FIGURE 41-7 (continued) PERFORMANCE
METRO III - ICAO ANNEX 8
FAA APPROVED: MAR 18192
03-P
gg
TAKEOFF
SPEED
SCHEDULE
(KIAS)
-WET [CAUTION 1
I
p?iEGGq
. TAKEOFF IN TEMPERATURE AND ALTITUDE CONDITIONS SHOWN TO THE RIGHT OF AND ABOVE THE SOLID, STEPPED LINE IS NOT APPROVED. THE SPEEDS IN THAT AREA OF THE CHART ARE PROVIDED FOR INTERPOLATKIN ONLY. . REFER
r
I
1
CIUTSIDE -6
I
“R
“2
1111 111 109 107 IOY LO3
119 116 116 115 113 113
“50 130 126 127 126 125 1ZU
10
I
20
AIR
I
"R "2 "50
TEMPERRTURE 30
"1
TO FIGURE
"R
I
41-6 FOR MAXIMUM
TAKEOFF
WEIGHTS.
1.C)
I
UO
"2 "SO "1
PERMISSIBLE
“I
“I3
“2
“50
"1
"R "2 "50
110 108 107 106 104 103
115 112 110 107 105 103
119 116 116 115 113 112
129 128 127 125 12U 12U
110 108 107 106 1011 103 101 101 101 102 102 103 103 103
115 112 110 108 105 103 101 101 101 102 102 103 103 103
119 116 116 115 113 112 111 111 113 11U 116 116 119 120
129 128 126 125 124 123 123 123 125 127 129 131 133 135
110 108 107 106 1011 103 101 100 100 101 101 102 103 103
116 119 113 118 111 116 109 115 106 113 1OU 112 102 110 101 110 100 111 101 112 101 1111 102 116 103 117 103 119
129 110 127 108 126 107 125 106 12U 1011 123 103 122 101 122 100 123 100 125 100 127 101 129 101 131 102 133 102
117 115 112 110 108 105 103 101 100 100 101 101 102 102
119 118 116 115 113 112 110 109 109 110 112 113 115 117
129 127 126 125 123 122 121 121 121 122 1211 126 128 130
I
50
"1
107 106 10’4 103 101 100 100 100 100 100 101 101
"R "2 "50
11U 116 111 115 109 113 107 112 lO~,lOl 103 109 101 109 101 109 100 110 100 111 101 112 101 11U
55
"I
"R "2 "50
125 12U 123 122 120 120 121 121 123 125 127
100 100 100 100 100 100 101
105 103 102 101 101 100 100 101
110 109 109 109 109 110 111 113
121 i2026 120 121 121 123 125
112 109 107 105 103 101 101 101 102 103 103 103 103
119 116 116 115 113 112 112 112 1111 116 117 119 120 121
129 126 127 125 12U 1211 12U 125 126 128 131 132 1311 136
110 106 107 106 LOU 103 101 101 101 102 102 103 103 103
115 112 110 108 105 103 101 101 101 102 102 103 103 103
119 118 116 115 113 112 111 111 113 11U 116 118 119 121
129 128 126 125 12U 123 123 123 125 127 129 131 133 135
110 108 107 106 1011 103 101 100 100 101 102 102 103 103
116 113 111 108 106 1011 102 100 100 101 102 102 103 103
11s 118 116 115 113 112 110 110 111 113 115 116 118 120
129 128 126 125 124 123 122 122 123 125 127 129 132 133
110 108 107 106 1011 103 101 100 100 100 101 101 102 103
117 1111 112 110 107 105 103 101 100 100 101 101 102 103
119 118 116 115 113 112 110 109 110 111 112 1111 116 116
129 127 126 125 121 122 121 121 121 123 125 127 129 131
110 108 107 106 1011 103 101 100 100 100 100 100 101 102
118 115 113 111 109 106 1011 102 101 100 100 100 101 102
119 118 116 115 113 112 110 109 109 109 110 112 113 115
128 127 126 12U 125 122 121 120 120 121 122 121 128 128
100 101
100 101
111 113
123 125
100 100
100 100
110 111
122 123
115 112 110 108 105 103 101 101 101 102 102 103 103 103
119 118 116 115 113 112 111 112 113 115 117 118 120 121
129 128 127 125 124 123 123 129 126 127 130 132 133 135
110 108 107 106 IOU 103 101 101 101 101 102 103 103 103
115 113 110 108 106 103 101 101 101 101 102 103 103 103
119 118 116 115 113 112 111 111 112 11U 115 117 119 120
129 128 126 125 1211 123 122 123 12’4 126 128 130 132 131
110 108 107 106 1011 103 101 100 100 101 101 102 102 103
116 1111 111 109 107 1OU 102 101 100 101 101 102 102 103
119 118 116 115 113 112 110 110 110 112 113 115 117 118
129 127 126 125 1211 123 121 121 122 1211 126 128 130 132
110 108 107 106 10’4 103 101 100 100 100 100 101 101 102
118 115 113 110 108 106 103 102 101 100 100 101 101 102
119 118 116 115 113 112 110 109 109 110 111 113 11’4 116
128 127 126 12U 123 122 121 120 121 121 123 125 127 129
107 106 1011 103 101 100 100 100 100 100 101 101
1111 112 109 107 105 103 102 101 100 100 101 101
116 115 113 112 110 109 109 109 109 110 112 1111
125 129 123 122 121 120 120 120 121 122 12U 126
103 101 100 100 100 100 100 100 100
108 106 1011 103 102 101 101 100 100
112 110 109 109 109 109 109 110 111
121 120 120 120 120 120 121 122 123
100 100 100 100 100 100
1011 103 102 101 100 100
109 109 109 109 109 110
119 120 120 120 121 122
115
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221 121 021 021 021 021 221 EZI h21 '31 921
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001 001 001 001 001 to1 EOI hot 901 LO1 801
921 h21 221 121
h2l s21 L2I 821
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101 101 001 001 101 201 EOI SO1 LO1 601 I
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fiI1 911 611
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101 101 001 001 001 001 001 101 EOI hOI $01 LO1 801 011
201 101 101 001 001 001 DC1 101 EOI nor 901 LO1 $301 011
h21 22L 12t 021 021 121 221 EZI h21 921 L2[ 821
I LII SII EII 211 011 601 601 011 211 &II SII 911 811 6II
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01 tl333tl
62 L2 s2 &2 22 12 02 12 22 EZ s2 92 L2 62
6OIlIOIlOO1
SE1 I&I jar rar ;zt 217. ?21 221 @-I hZ1 3 l21 g2J hE1 m O&I &zJ 921 h21 gJ 221 E21 w SZI 821 gi?J 621
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EE I& 62 12 S2 6;2 22 22 EC? tit s2 92 L2 6Z
-
911 811 611
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LO1 801 011
611 m 911 fiI1 gJ 111 011 011 a-7 &II gJ 911 811 gJ
021 a-f LII gJ ET1 211 01‘[ III 211 El1 Ti-7 911
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41-22 8AC
FAA APPROVED: MAR 18/92
METRO III - ICAO ANNEX 8
FIGURE 41-7 (continued) PERFORMANCE
METRO III - ICAO ANNEX 8 DISTANCE TO ACCELERATE ASSOCIATED
TO V, AND STOP -WET EXAMPLE:
CONDITIONS:
GIVEN:
POWER ............................. TAKEOFF (WET) GEN LOAD.. ............................... .300 AMPS BLEED AIR.. ........................................... OFF .............. OFF (SEE NOTE) ENG ANTI-ICE.. RUNWAY ............... DRY, HARD SURFACE II4 FLAPS ....................................................... ........ Vi (FIGURE 41-7) DECISION SPEED NOSE WHEEL STEERING....0 N OR OFF
OAT = 10°C PRESSURE ALTITUDE = 2,000 FEET GROSS WEIGHT = 15,000 POUNDS (6805 kg) HEADWIND = 20 KNOTS RUNWAY SLOPE = 1 PERCENT (UPHILL) V, SPEED = 107 KIAS ACCELERATE -STOP DISTANCE = 3,910 FEET (1190 m)
OBTAIN:
NOTE
I
I I
MAXIMUM TAKEOFF WEIGHT MAY NOT EXCEED THE WEIGHT DETERMINED FROM FIGURE 41-6.
. INCREASE PERCENT MAXIMUM
l
GROSS
WEIGHT
7
ACCELERATE WITH ENGINE OAT
(1000
6
WITH
- STOP ANTI-ICE ENGINE
DISTANCE ON.
ANTI-ICE
ON
BY 1.0
IS5”C.
kg)
5
8
1
2 OAT
(OC)
FAA APPROVED: MAR 18/92
GROSS
WEIGHT
(1,000
FIGURE 41-8 PERFORMANCE
POUNDS)
WIND
(KNOTS)
RUNWAY SLOPE (PERCENT)
41-23 8AC
METRO III - ICAO ANNEX 8 SINGLE
ENGINE
TAKEOFF
DISTANCE
I MAXIMUM
TO 35 FOOT
HEIGHT-WET
OAT WITH ENGINE NoTE/ ENGINE
ANTI-ICE
ANTI-ICE
ON
IS 5°C.
EFFECTS
(METERS) 0
50
100
150
200
8,000
7,000
6,000
F 5,000 ! E 2 5 4,000 Q k! 2 z g 3,000
2,000
1,000
S.L. 0
200
400 FEET)
600
800
INCREASE IN TAKEOFF RUN DISTANCE WITH ENGINE ANTI-ICE ON
FIGURE 41-24 8AC
41-9
PERFORMANCE
FAA APPROVED:
MAR 18/92
METRO 111 ICAO ANNEX 8 SINGLE ENGINE TAKEOFF DISTANCE TO 35 FOOT HEIGHT - WET ASSOCIATED
EXAMPLE:
CONDITIONS:
............................. TAKEOFF (WET) POWER GEN LOAD ................................. .300 AMPS OFF BLEED AIR.. ........................................... ENG ANTI-ICE ............. OFF (SEE GRAPH) RUNWAY ............... DRY, HARD SURFACE FIGURE 41-7 V 1 SPEED .............................. ........................... FIGURE 41-7 VR SPEED.. V7 SPEED .............................. FIGURE 41-7 FliPS . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . . .. . .. . .. . . . . . . .. . . . . . l/4 NOSE WHEEL STEERING .. ..ON OR OFF
GIVEN:
OBTAIN:
/
FOR TAKEOFF FIELD LENGTH ENGINE TAKEOFF DISTANCES ENGINE TAKEOFF DISTANCES
EXCEED 41-6. GROSS
WEIGHT
7
(OC)
GROSS
FIGURE FAA APPROVED:
MAR 18/92
(1000
6
WEIGHT
kg)
NOTE
I
MAXIMUM TAKEOFF WEIGHT MAY NOT THE WEIGHT DETERMINED ‘FROM FIGURE
OAT
OAT = 10°C PRESSURE ALTITUDE = 2,000 FEET GROSS WEIGHT = 15.000 POUNDS (6605 HEADWIND = 20 KNOTS RUNWAY SLOPE = 1 PERCENT (UPHILL) V1 SPEED = 107 KIAS VR SPEED = 110 KIAS V2 SPEED = 116 KIAS TAKEOFF RUN = 5,550 FEET (1690 m)
DETERMINATION, SINGLE ARE LONGER THAN TWO FACTORED BY 1.15.
kg) 5
(1,000
POUNDS)
WIND
(KNOTS)
RUNWAY SLOPE (PERCENT)
41-9 (continued)
PERFORMANCE
41-25 8AC
METRO III - ICAO ANNEX 8 SINGLE
ENGINE
TAKEOFF
RUN DISTANCE-WET NOTE OAT WITH ENGINE
MAXIMUM
ENGINE
ANTI-ICE
ANTI-ICE
ON
IS 5°C.
EFFECTS
(METERS) 0
100
50
150
8,000
6,000
2,000
1,000
S.L. 0
200
400
600
(FEET) INCREASE IN TAKEOFF RUN DISTANCE WITH ENGINE ANTI-ICE ON
FIGURE 41-26 8AC
41-l 0
PERFORMANCE
FAA APPROVED:
MAR 18/92
-METRO SINGLE
ENGINE ASSOCIATED
III - ICAO ANNEX 8 TAKEOFF
RUN DISTANCE
-WET EXAMPLE:
CONDITIONS:
POWER . . .. . . . . . . . . . . . . . . . . . . . . . . . . . TAKEOFF (WET) GEN LOAD . . . . .. . . . . . . .. . .. .. . . . . .. .. . . . . . . . 300 AMPS BLEED AIR . . . . . . . . . . . . .. . . . . . . . . . .. .. . .. . . . .. . .. . . . . . . . OFF ENG ANTI-ICE . . . . .. .. . . . . . OFF (SEE GRAPH) SURFACE RUNWAY .. .. . . . . .. .. . . . . DRY, HARD V 1 SPEED . . . . . . . . . . . . . . . . . . . . . . .. . . . . .. FIGURE 41-7 41-7 VR SPEED . . . . . . . . . . . .._................ FIGURE 41-7 Vp SPEED . . . . . . . . . . . . . . . . . . . . . . .. . . . . . . FIGURE FLAPS . . . . . . . . . . . . .. . . . . . . . . .. . .. .. . .. . .. . .. . . . . . . .. . . . . . . . . . l/4 NOSE WHEEL STEERING . . ..ON OR OFF
MAXIMUM TAKEOFF WEIGHT MAY NOT THE WEIGHT DETERMINED FROM FIGURE
GIVEN:
OBTAIN:
7
GROSS
FIGURE FAA APPROVED:
MAR 18/92
kg)
EXCEED 41-6. GROSS
OAT (“C)
OAT = 10% PRESSURE ALTITUDE = 2,000 FEET GROSS WEIGHT = 15,000 POUNDS (6805 HEADWIND = 20 KNOTS RUNWAY SLOPE = 1 PERCENT (UPHILL) VI SPEED = 107 KIAS VR SPEED = 110 KIAS V2 SPEED = 116 KIAS TAKEOFF RUN = 4,840 FEET (1475 m)
WEIGHT
(1000
kg)
‘6
WEIGHT
5
(1,000
POUNDS)
WIND
(KNOTS)
RUNWAY SLOPE (PERCENT)
41-l 0 (continued)
PERFORMANCE
41-27 8AC
METRO III – ICAO ANNEX 8 TAKEOFF FLIGHT PATH DISTANCE TO 1500 FOOT HEIGHT – WET
TWO ENGINE TAKEOFF WITH ENGINE FAILURE RECOGNIZED AT V1 , FLAPS 1/4
AFTER TAKEOFF, GEAR IS RETRACTED
MAINTAIN V 2 CLIMB TO 400 FEET WITH 1/4 FLAPS
ACCELERATE TO V YSE , RETRACT FLAPS AT V 2 +5 KNOTS AND FEATHER INOPERATIVE PROPELLER
VYSE
V2
400 FT
V2 VR
SINGLE ENGINE TAKEOFF DISTANCE TO 35 FOOT HEIGHT (FIGURE 4I-4 OR 4I-9)
4I-28 8AC
REDUCE POWER TO MCP AND CONTINUE CLIMB TO 1,500 FEET END OF FLIGHT PATH
START OF TAKEOFF ROLL
An estimate of the horizontal distance required to clear an obstacle up to 1,500 feet above the runway, or the required climb gradient to clear an obstacle along the takeoff flight path, may be obtained by using Figures 4D-6 through 4D-10 and Figure 4I-4 (Dry, Bleed Air Off) or Figures 4E-6 through 4D-10 and Figure 4I-9 (Wet). The takeoff flight path is as follows:
1,500 FEET
35 FT
SECOND SEGMENT CLIMB (PART D OR E)
SECOND SEGMENT ACCELERATION (PART D OR E)
PERFORMANCE
THIRD SEGMENT CLIMB (PART D OR E)
FAA APPROVED: MAR 18/92