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SOCATA TBM 700 User Manual

SOCATA TBM 700
670 pages
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January 31, 1990 - Rev. 9 Printed in FRANCEP/N : T00.DMAPIPYE
TBM 700
Versions A and B
PILOT'S
INFORMATION MANUAL
CAUTION
THIS INFORMATION MANUAL IS A NON-OFFICIAL COPY OF THE PILOT'S
OPERATING HANDBOOK AND MAY BE USED FOR GENERAL INFORMATION
PURPOSES ONLY.
IT IS NOT KEPT CURRENT AND THEREFORE CANNOT BE USED AS A SUBSTITUTE
FOR AIRWORTHINESS AUTHORITIES APPROVED MANUAL WHICH IS THE ONLY ONE
INTENDED FOR OPERATION OF THE AIRPLANE.
The content of this document is the property of SOCATA. It is supplied in confidence and
commercial security of its contents must be maintained.
It must not be used for any purpose other than that for which it is supplied, nor may
information contained in it be disclosed to unauthorized persons. It must not be reproduced
nor transmitted in any form in whole or in part without permission in writing from the owners
of the Copyright.
Information in this document is subject to change without notice.
For any information concerning this document, please contact :
SOCATA
SUPPORT CLIENT / CUSTOMER SUPPORT
AEROPORT TARBES-OSSUN-LOURDES TELEPHONE : 33 (0)5 62.41.73.00
B.P. 930 - 65009 TARBES CEDEX TELEFAX : 33 (0)5 62.41.76.54
FRANCE TELEX : 532 835 F
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SOCATA TBM 700 Specifications

General IconGeneral
ManufacturerSOCATA
ModelTBM 700
TypeSingle-engine turboprop
EnginePratt & Whitney Canada PT6A-64
Power Output700 shp
Crew1
Maximum Speed300 knots
Service Ceiling30, 000 ft (9, 144 m)
Passenger Capacity5-6
Maximum Takeoff Weight7, 394 pounds
AvionicsGarmin G1000

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