Climb Performance – Flaps TO
NOTE
Conditions:
-
Landing gear UP and flaps TO.
Table 5.10.11 - Climb Performance – Flaps TO
Airplane
weight /
IAS
Pressure
altitude
(ft)
Rate of climb (ft/min)
ISA
- 35 °C
ISA
- 20 °C
ISA
- 10 °C
ISA
ISA
+ 10 °C
ISA
+ 20 °C
ISA
+ 30 °C
6,594 lbs
(2,991 kg)
110 KIAS
SL
2,295
2,275
2,260
2,250
2,240
2,225
2,215
2,000
2,280
2,260
2,245
2,230
2,220
2,210
2,190
4,000
2,265
2,245
2,230
2,215
2,200
2,180
2,165
6,000
2,250
2,225
2,210
2,190
2,175
2,155
2,135
8,000
2,235
2,205
2,185
2,165
2,145
2,130
2,110
7,394 lbs
(3,354 kg)
115 KIAS
SL
1,985
1,965
1,955
1,940
1,930
1,915
1,900
2,000
1,970
1,950
1,940
1,925
1,910
1,890
1,875
4,000
1,955
1,935
1,920
1,900
1,885
1,865
1,850
6,000
1,940
1,910
1,895
1,875
1,860
1,840
1,825
8,000
1,915
1,890
1,870
1,850
1,835
1,815
1,795
7,615 lbs
(3,454 kg)
115 KIAS
SL
1,910
1,890
1,875
1,865
1,855
1,840
1,825
2,000
1,895
1,875
1,860
1,845
1,830
1,815
1,795
4,000
1,880
1,860
1,840
1,825
1,805
1,790
1,775
6,000
1,865
1,835
1,815
1,800
1,780
1,765
1,745
8,000
1,840
1,810
1,795
1,775
1,755
1,735
1,715
Section 5
Performance
Pilot's Information Manual
PIM TBM 960 - Edition 0
Rev. 01
Page 5.10.12
PIM - DO NOT USE FOR FLIGHT OPERATIONS
