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SOCATA TBM 700 - Page 45

SOCATA TBM 700
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SECTION 2
LIMITATIONS
D.G.A.C. Approved
T B M
700 PILOTS INFORMATION MANUAL
Back to
Contents
Page 2.3.3
Rev. 7
NOTE :
Use of AVGAS to be recorded in engine module logbook.
US Specification
(US)
French Specification
(FR)
English
Specification
(UK)
NATO Code
ASTMD1655 JET A
ASTMD1655 JET A1
ASTMD1655 JET B
AIR 3405C Grade F35 DERD 2494 Issue 9
F35 without
additive
MILT5624L Amdt1
Grade JP4
AIR 3407B
DERD 2454 Issue 4
Amdt 1
F40 with
additive
MILT5624L Amdt1
Grade JP5
AIR 3404C Grade F44
DERD 2452 Issue 2
Amdt 1
F44 with
additive when
utilization
MILT83133A Amdt1
Grade JP8
AIR 3405C Grade F34
DERD 2453 Issue 4
Amdt 1
F34 with
additive S748
AIR 3404C Grade F43 DERD 2498 Issue 7
F43 without
additive
Figure 2.3.2 RECOMMENDED FUEL TYPES
(Reference : Service Bulletin P & W C. No. 14004)
PROPELLER
Number of propellers : 1
Propeller manufacturer : HARTZELL
Propeller model number : HCE4N3 / E9083S (K)
Propeller diameter :
Minimum : 90 inches (2.286 m)
Maximum : 91 inches (2.311 m)
Propeller blade setting at 30 inches station :
Low pitch : 21°
Feathering : 86°
Maximum reverse : - 11°

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