16 f 10 performance standard reference parte i

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

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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

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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