TBM-700 Takeoff Performance Data

This information is non-official - copied from a generic TBM-700 Pilot's Information Manual and may ONLY be used for general information purposes. This information MAY NOT, CAN NOT, and MUST NOT be used for flight planning purposes. Only the approved Pilot's Information Manual for the specific aircraft may be used for flight planning.

WEIGHT: 5,512 lbs. (2,500kg) at 50 ft. - 91 KIAS - 105 MPH IAS
Pressure Altitude ft.	ISA -35o C		ISA -20o C		ISA -10o C		ISA
	GR	D50	GR	D50	GR	D50	GR	D50
0	787	1,280	886	1,411	951	1,493	1,017	1,591
2,000	886	1,411	984	1,558	1,066	1,657	1,132	1,772
4,000	984	1,558	1,099	1,722	1,181	1,837	1,280	1,968
6,000	1,099	1,722	1,230	1,903	1,329	2,051	1,444	2,215
8,000	1,230	1,903	1,394	2,149	1,526	2,329	1,657	2,510
Pressure Altitude ft.	ISA +10o C		ISA +20o C		ISA +30o C		ISA +37o C
	GR	D50	GR	D50	GR	D50	GR	D50
0	1,083	1,690	1,148	1,788	1,214	1,903	1,247	1,969
2,000	1,214	1,870	1,296	1,985	1,378	2,133	1,444	2,231
4,000	1,363	2,100	1,476	2,247	1,575	2,411	1,640	2,526
6,000	1,575	2,379	1,690	2,559	1,837	2,756	1,919	2,887
8,000	1,804	2,707	1,968	2,920	2,100	3,133	2,198	3,281
Associated Conditions: • Landing Gear DN and flaps TO • Np = 2,000 RPM - BLEED LO • Hard, dry and level runway • GR = Ground roll (in ft.) • D50 = Takeoff Distance in feet (clear to 50 ft.) Note: Between ISA + 30 Deg. C and ISA + 37 deg. C, it may be necessary to cut-off the Bleed in order to set TQ  = 100% during takeoff while respecting the engine limitations.  In this case, reduce power after takeoff to set the Bleed ON Corrections: • Reduce total distances of 10% every 10 kt. of headwind • Increase total distances of 30% every 10 kt. of rear wind • Other runway surfaces require the following correction factors:   Increase by 7% on hard sod   Increase by 10% on short grass   Increase by 15% on wet runway   Increase by 25% on high grass   Increase by 30% on slippery runway

WEIGHT: 6,579 lbs. (2,984kg) at 50 ft. - 94 KIAS - 108 MPH IAS
Pressure Altitude ft.	ISA -35o C		ISA -20o C		ISA -10o C		ISA
	GR	D50	GR	D50	GR	D50	GR	D50
0	1,083	1,673	1,214	1,870	1,280	2,001	1,378	2,133
2,000	1,214	1,870	1,345	2,067	1,444	2,198	1,542	2,362
4,000	1,345	2,067	1,509	2,297	1,640	2,461	1,739	2,625
6,000	1,509	2,297	1,706	2,559	1,837	2,723	1,968	2,920
8,000	1,706	2,559	1,903	2,854	2,067	3,051	2,231	3,281
Pressure Altitude ft.	ISA +10o C		ISA +20o C		ISA +30o C		ISA +37o C
	GR	D50	GR	D50	GR	D50	GR	D50
0	1,476	2,264	1,575	2,395	1,690	2,559	1,755	2,657
2,000	1,673	2,493	1,772	2,657	1,903	2,854	1,969	2,953
4,000	1,870	2,789	2,001	2,953	2,149	3,182	2,231	3,314
6,000	2,100	3,117	2,297	3,346	2,461	3,609	2,543	3,740
8,000	2,428	3,543	2,657	3,839	2,854	4,134	2,969	4,298
Associated Conditions: • Landing Gear DN and flaps TO • Np = 2,000 RPM - BLEED LO • Hard, dry and level runway • GR = Ground roll (in ft.) • D50 = Takeoff Distance in feet (clear to 50 ft.) Note: Between ISA + 30 Deg. C and ISA + 37 deg. C, it may be necessary to cut-off the Bleed in order to set TQ  = 100% during takeoff while respecting the engine limitations.  In this case, reduce power after takeoff to set the Bleed ON Corrections: • Reduce total distances of 10% every 10 kt. of headwind • Increase total distances of 30% every 10 kt. of rear wind • Other runway surfaces require the following correction factors:   Increase by 7% on hard sod   Increase by 10% on short grass   Increase by 15% on wet runway   Increase by 25% on high grass   Increase by 30% on slippery runway