14 5 mccauley f 6 performance parte f

METRO III ICAO ANNEX 8 PART F – EN ROUTE CLIMB PERFORMANCE CONTENTS ITEM

PAGE

Single Engine Best Rate of Climb Bleed Air On ............................................................................................................................... 4F-2 Bleed Air Off ............................................................................................................................... 4F-3 Single Engine Service Ceiling Bleed Air On ............................................................................................................................... 4F-4 Bleed Air Off ............................................................................................................................... 4F-5 Two Engine Best Rate of Climb Bleed Air On ............................................................................................................................... 4F-6 Bleed Air Off ............................................................................................................................... 4F-8

FAA APPROVED: MAY 22/89 REVISED: OCT 17/94

PERFORMANCE

4F-i 4MC

METRO III ICAO ANNEX 8

THIS PAGE LEFT BLANK INTENTIONALLY

4F-ii 4MC

PERFORMANCE

MANUFACTURER'S DATA ISSUED: MAY 22/89

METRO III ICAO ANNEX 8

THIS PAGE LEFT BLANK INTENTIONALLY

FAA MANUFACTURER'S APPROVED: MAY DATA 22/89 ISSUED: MAY 22/89

PERFORMANCE

4F-1 4MC

METRO III - ICAO ANNEX 8 SINGLE

ENGINE

BEST

RATE

OF CLIMB

- BLEED

AIR ON ASSOCIATED

CONDITIONS:

POWER . . . . . . . . . . . . . . . . . . . . . . . . MAX CONTINUOUS PROPELLER . . . . . . . . . . . . . . . . . . . . FEATHERED ON INOPERATIVE ENGINE GEN LOAD ................................ .3M) AMPS BLEED AIR ..............................................

ON ENG ANTI-ICE ............... OFF (SEE NOTE) CLIMB SPEED.....SE E VYSE SCHEDULE GEAR ........................................................

UP FLAPS .......................................................

UP

60

EXAMPLE: GIVEN:

50

OAT I 10% PRESSURE ALTITUDE - 5,COO FEET GROSS WEIGHT = 13,Mx) POUNDS (5900 k@ VYSE CLIMB SPEED - 124 KIAS RATE OF CLIMB - 460 FEET PER MINUTE

OBTAIN: 40 .

NOTE REDUCE RATE OF CLIMB BY 240 WITH ENGINE ANTCICE ON.

.

MAXIMUM

30

OAT

VYSE

GROSS WEIGHT r (kg)

WITH

CLIMB

ENGINE

SPEED

FEET

ANTI-ICE

SCHEDULE

PER

ON

MINUTE

IS 5%.

(KIAS)

PRESSURE

ALTINDE

(FEET)

S.L.

5,ooo

10,ow

15,tKQ

20,000

6580 6500

132 132

130 129

130 129

130 129

130 129

6wo 5500

129 126

125 123

124 121

124 119

124 119

5ooo 4m

124 122

120 116

116 114

114 112

113 110

7

5

ia -1,000

-600

-600

-400

-200

0 200 RATE OF CLIMB (FEET

400 600 PER MINUTE)

800

1,000

1,200

1,400

FIGURE 4F-1 4F-2 4MC

PERFORMANCE

FAA APPROVED: MAY 22189

METRO III - ICAO ANNEX 8 SINGLE

ENGINE

BEST

RATE

OF CLIMB

- BLEED

AIR OFF ASSOCIATED

CCINOITIONS:

POWER . . . . . . . . . .. . . . . . . . . . . . . . MAX CONTINUOUS PROPELLER . . . . . . . . . . . . . . . . . . . . FEATHERED ON INOPERATIVE ENGINE GEN LOAD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 300 AMPS BLEED AIR . . . . . . . . . .. . . . . . .. . . . . . . . . . .. . . . . . . . . . . . . . . . OFF ENG ANTI-ICE . . . . . . . . . OFF (SEE NOTE) CLIMB SPEED . . . ..SEE V YSE SCHEDULE GEAR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP FLAPS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP

60

EXAMPLE:

40

GIVEN:

OAT - 10% PRESSURE ALTITUDE - 10,000 FEET GROSS WEIGHT - ll.tXXI POUNDS (4990 k@ VYSE CLIMB SPEED - 116 KIAS RATE OF CLIMB = 530 FEET PER MINUTE

OBTAIN:

30

,.“,I.

20 /

.

REDUCE RATE OF CLIMB BY 210 WITH ENGINE ANTI-ICE ON.

-

MAXIMUM VYSE

10 s r

GROSS WEIGHT (POUNDS)

$0

OAT WITH CLIMB

ENGINE

SPEED

ANTCICE

SCHEDULE

PRESSURE S.L.

FEET

5,oco

ALTITUDE 10,m

PER

MINUTE

ON IS 5°C. (KIAS) (FEET) 15,000

20,000

-10

-20

-30

-40

-50 7 15

gj

14

5 2 8 9 ‘,

13

5. c!! 12 5 2 i

5

11

10 0 RATE

200 OF CLIMB

400 (FEET

600 BOO PER MINUTE)

1,000

1.200

1,400

1,600

FIGURE 4F-2 FAA APPROVED: MAY 22189

PERFORMANCE

4F-3 4MC

1

METRO III - ICAO ANNEX 8 rlGLE ENGINE SERVICE CEILING - BLEED AIR ON ASSOCIATED

EXAMPLE:

CONDITIONS:

POWER.. .................. MAX CONTINUOUS PROPELLER ................ FEATHERED ON INOPERATIVE ENGINE GEN LOAD ............................ .300 AMPS BLEED AIR .......................................... ON ENG ANTI-ICE ................................... OFF CLIMB SPEED ....... (SEE FIGURE 4F-1) GEAR ....................................................

UP FLAPS ...................................................

UP

GIVEN : OAT AT 21,500 FEET = -26°C GROSS WEIGHT = 11,500 POUNDS (5215 kg) OBTAIN : SINGLE ENGINE SERVICE CEILING (ASSUMING STANDARD LAPSE RATE) = 18,500 FEET

25,000

S.L. u -60

-40

-20

0 OAT (OC)

20

40

60

FIGURE 4F-3 4F-4 4MC

PERFORMANCE

FAA APPROVED: MAY 22/89

METRO III - ICAO ANNEX 8 SINGLE

ENGINE

ASSOCIATED

SERVICE

CEILING

- BLEED

AIR OFF EXAMPLE:

CONDITIONS:

POWER.. .................. MAX CONTINUOUS PROPELLER ................ FEATHERED ON INOPERATIVE ENGINE GEN LOAD ............................ .300 AMPS BLEED AIR ........................................ OFF ENG ANTI-ICE.. ................................. OFF CLIMB SPEED ....... (SEE FIGURE 4F-2) UP GEAR ....................................................

UP FLAPS ...................................................

GIVEN : OAT AT 21,500 FEET = -26°C GROSS WEIGHT = 12,500 POUNDS (5670 kg) OBTAIN : SINGLE ENGINE SERVICE CEILING (ASSUMING STANDARD LAPSE RATE) = 19,000 FEET

25,000

-60

40

-20

0 OAT (OC)

20

40

60

FIGURE 4F-4 FAA APPROVED: MAY 22189

PERFORMANCE

4F-5 4MC

METRO III - ICAO ANNEX 8 TWO

ENGINE

BEST

RATE

OF CLIMB

- BLEED

AIR ON

ENGINE ANTI-ICE

EFFECTS

30,000

25,000

20,000

15,000

10,000

5,000

IIIIIIIIIIIII I I I I I q&j++

I

S.L. 100

200

300

400

500

RATE OF CLIMB LOSS DUE TO ENGINE ANTI-ICE (FEET PER MINUTE) VY CLIMB

SPEED

GROSS WEIGHT (POUNDS)

S.L.

5,000

10.(xX)

14,5Gu 14,000

146 145

143 142

137 136

PRESSURE

GROSS

PRESSURE

SCHEDULE ALTINDE

(KM) (FEET)

lS.c#J

2o.ooo

25,000

3O.ooO

132 131

130 126

130 126

136 126

ALTITUDE

ON

(FEET)

WEIGHT (kg)

S.L.

5,ooa

lO.ooo

15.ooa

20,C’XJ

25,OW

30,OW

6560 6500

146 146

143 142

137 137

132 132

E

130 129

130 129

6ow 5500

144 142

140 136

135 133

130 126

125 123

125 116

125 116

5000 4500

140 139

135 133

130 126

125 124

121 119

116 114

111 106

FIGURE 4F-5 4F-6 4MC

PERFORMANCE

FAA APPROVED: MAY 22189

METRO III - ICAO ANNEX 8 TWO ENGINE BEST RATE OF CLIMB - BLEED AIR ON 60

ASSOCIATED

50

POWER .................. MAX CONTINUOUS GEN LOAD ............................ 300 AMPS BLEED AIR ......................................... ON ENG ANTI-ICE .......... OFF (SEE NOTE) CLIMB SPEED.. ..SE E Vy SCHEDULE UP GEAR ...................................................

FLAPS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP

40

CONDITIONS:

EXAMPLE: GIVEN:

30 OBTAIN:

OAT - -10% PRESSURE ALTITUDE - 15,000 FEET GROSS WEIGHT = 11.500 POUNDS (5215 kg) Vy CLIMB SPEED I 126 KIAS RATE OF CLIMB = 1,620 FEET PER MINUTE DECREASE (ANTI-ICE ON) - -335 FEET PER MINUTE 1.265 FEET PER MINUTE NET RATE OF CLIMB NOTE

MAXIMUM

OAT

WITH

ENGINE

ANT!-ICE

ON IS 5%.

-10

7

1,000

-500

0

500

1,000 RATE

FAA APPROVED: MAY 22189

1,500 OF CLIMB

2,000 (FEET

PER

2,500

3,000

3,500

4,000

4.50

MINUTE)

FIGURE 4F-5 (continued) PERFORMANCE

4F-7 4MC

METRO III - ICAO ANNEX 8 TWO

ENGINE

BEST

RATE

OF CLIMB

- BLEED

AIR OFF

ENGINE ANTI-ICE

EFFECTS

30,000

25,000

20,000

15,000

10,000

5,000

S.L. 1100

200

300

400

5( 30

RATE OF CLIMB LOSS DUE TO ENGINE ANTI-ICE ON (FEET PER MINUTE) Vy CLIMB

SPEED

SCHEDULE

(KM)

THE ENGINE ANTI-ICE EFFECT IS ONLY A POWER EFFECT ASSOCIATED WITH INCREASED BLEED AIR RATE AND DOES NOT INCLUDE THE EFFECT OF ANY ICE ACCUMULATION ON ME AIRCRAFT. REFER TO PART H OF SECTION 4 FOR PER-

GROSS WEIGHT (kg)

5000

4500

PRESSURE

ALTITUDE

S.L.

5,coo

10,coo

140 133

135 133

130

125

128

124

1 s.cGu

(FEET) 20.m

25mo

30,ooo

121 119

116 114

111 108

FIGURE 4F-8 4MC

4F-6

PERFORMANCE

FAA APPROVED:

MAY 22189

METRO III - ICAO ANNEX 8 TWO

ENGINE

BEST

RATE

OF CLIMB

- BLEED

AIR OFF

60

ASSOCIATED

CONDITIONS:

POWER .................. MAX CONTINUOUS GEN LOAD ........................... .300 AMPS BLEED AIR ....................................... OFF ENG ANTI-ICE .......... OFF (SEE NOTE) CLIMB SPEED.. ..SE E V y SCHEDULE GEAR ...................................................

UP FLAPS .................................................

UP EXAMPLE: GIVEN: OBTAIN:

OAT I -1tPC PRESSURE ALTITUDE - 15,ooO FEET GROSS WEIGHT - ll.OW POUNDS (4990 kg) Vy CLIMB SPEED - 126 KIAS RATE OF CLIMB 2,150 FEET PER MINUTE DECREASE (ANTI-ICE ON) I -325 FEET PER MINUTE NET RATE OF CLIMB 1.825 FEET PER MINUTE

MAXIMUM

OAT

WITH

ENGINE

ANTCICE

ON

IS 5°C.

7

,000

-500

0

500

1,000 RATE

1,500 OF CLIMB

2,000 (FEET

FIGURE FAA APPROVED:

MAY 22189

PER

2,500

3,000

3,500

4,000

4,5oc

MINUTE)

4F-6 (continued)

PERFORMANCE

4F-9 4MC

I

METRO III ICAO ANNEX 8

THIS PAGE LEFT BLANK INTENTIONALLY

4F-10 4MC

PERFORMANCE

MANUFACTURER'S FAA APPROVED: MAY DATA 22/89 ISSUED: MAY 22/89