Daher-Socata TBM 900 Pilot's Information Manual page 291

PILOT'S OPERATING HANDBOOK
CLIMB PERFORMANCE AFTER GO-AROUND
Conditions :
- Landing gear DN and flaps LDG
- IAS = 90 KIAS
Pressure
Airplane
altitude
weight
(feet)
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
Edition 0 -- October 31, 2013
Rev. 1
RATE OF CLIMB (ft/min)
ISA ISA
- 35°C - 20°C - 10°C
1550 1520 1495
1525 1485 1455
1490 1440 1410
1450 1400 1365
1410 1355 1320
RATE OF CLIMB (ft/min)
ISA ISA
- 35°C - 20°C - 10°C
1285 1245 1220
1250 1210 1180
1215 1170 1140
1175 1130 1100
1135 1090 1050
Figure 5.10.9 - CLIMB PERFORMANCE AFTER GO-AROUND
ISA ISA
ISA
+ 10°C
1465 1440
1425 1395
1380 1350
1335 1305
1285 1255
ISA ISA
ISA
+ 10°C
1195 1165
1155 1125
1110 1085
1065 1035
1015 980
SECTION 5
PERFORMANCE
ISA ISA
+ 20°C + 30°C
1410 1385
1370 1340
1320 1290
1270 1240
1215 1180
ISA ISA
+ 20°C + 30°C
1140 1115
1100 1075
1055 1020
1000 970
945 910
Page 5.10.9