Daher-Socata TBM 900 Pilot's Information Manual page 585

PILOT'S OPERATING HANDBOOK
CLIMB PERFORMANCE AFTER GO-AROUND
Conditions :
- Landing gear DN and flaps LDG
- IAS = 90 KIAS
Pressure
Airplane
altitude
weight
(feet)
SL
2000
6594 lbs
4000
(2991 kg)
6000
8000
Conditions :
- Landing gear DN and flaps LDG
- IAS = 95 KIAS
Pressure
Airplane
altitude
weight
(feet)
SL
2000
7394 lbs
4000
(3354 kg)
6000
8000
Figure 5.10.17 - CLIMB PERFORMANCE AFTER GO-AROUND
Edition 0 -- October 31, 2013
Rev. 1
RATE OF CLIMB (ft/min)
ISA ISA ISA
- 35°C - 20°C - 10°C
1635 1610 1590
1615 1580 1555
1585 1545 1525
1555 1515 1490
1520 1480 1455
RATE OF CLIMB (ft/min)
ISA ISA ISA
- 35°C - 20°C - 10°C
1350 1320 1295
1325 1290 1265
1295 1255 1235
1265 1225 1200
1230 1190 1160
FIVE--BLADED PROPELLER
ISA ISA
ISA
+ 10°C + 20°C
1565 1545 1525
1535 1510 1490
1500 1480 1455
1465 1440 1420
1430 1400 1375
ISA ISA
ISA
+ 10°C + 20°C
1275 1255 1235
1245 1225 1205
1210 1190 1165
1175 1150 1120
1135 1105 1075
SUPPLEMENT 58
ISA
+ 30°C
1505
1470
1435
1395
1345
ISA
+ 30°C
1215
1180
1140
1095
1050
Page 9.58.27