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MIL−T−5624 − JP−5 −36 °C 54 °C −46 °C
WideCut
ASTM D1655 − JET B −40 °C 43 °C −50 °C
ASTM D1655 − JP−4 −48 °C 43 °C −58 °C
LIMITATIONS
POWER PLANT
DOT Approved
REV 47, Aug 30, 2005
Airplane Flight Manual
CSP 700−1A
02−05−8
3. FUEL (CONT'D)
E. Fuels and Fuel Additives (Cont’d)
(3) BRITISH FUELS
FUEL SPEC BULK FUEL TAKE-OFF
LIMIT
BULK FUEL
FREEZING
MIN °C MAX °C POINT
Kerosene D. ENG. RD. 2494 −30 °C 54 °C −40 °C
D. ENG. RD. 2494 −37 °C 54 °C −47 °C
D. ENG. RD. 2453 −37 °C 54 °C −47 °C
D. ENG. RD. 2452 −36 °C 54 °C −46 °C
WideCut
D. ENG. RD. 2486 −40 °C 43 °C −50 °C
D. ENG. RD. 2486 −48 °C 43 °C −58 °C
(4) CIS FUELS
FUEL SPEC BULK FUEL TAKE-OFF
LIMIT
BULK FUEL
FREEZING
MIN °C MAX °C POINT
Wide−Cut TS−1 Premium −40 °C 43 °C −50 °C
RT Premium −45 °C 43 °C −55 °C
(5) CHINESE FUELS
FUEL SPEC BULK FUEL TAKE-OFF
LIMIT
BULK FUEL
FREEZING
MIN °C MAX °C POINT
Chinese
Kerosene GB 6537−94 No.3 −37 °C 54 °C −47 °C
(6) FUEL ADDITIVES
· Antiicing
additives to the latest revision of specification MIL−I−27686E or any direct
equivalent at a concentration of 0.10 to 0.15% by volume.
· Russian fuel icing inhibitors Fluid I (conforming to GOST 8313) at a maximum
concentration of 0.3% vol. and Fluid I−M (conforming to TU6−10−1458 GOST, a
mixture of GOST 8313 and GOST 2222 in equal parts by weight) at a maximum
concentration 0.3% vol.
· SOHIO Biobor JF biocide additive at a concentration not in excess of 270 parts per
million (20 parts per million elemental boron) to prevent the growth of
microorganisms.
· Stadis 450 antistatic
additive at a concentration of 5 mg/L.
LIMITATIONS
POWER PLANT
DOT Approved
REV 47, Aug 30, 2005
Airplane Flight Manual
CSP 700−1A
02−05−9
3. FUEL (CONT'D)
F. Engine Fuel Temperature
Takeoff
with engine fuel temperature indications below 5 °C is prohibited.
G. Fuel Crossfeed
Fuel crossfeed must be off for takeoff
and landing.
H. Fuel Recirculation System
On airplanes 9002 thru 9158:
Fuel Recirculation switch must be OFF for takeoff
and initial climb to altitude.
Fuel Recirculation switch must be OFF inflight
below 34,000 feet.
NOTE
FUEL RECIRC ON will be posted if the above systems limitations
are exceeded.
Effectivity:
· Airplanes 9002 thru 9114 not incorporating Service Bulletin:
· SB 700−28−036, Fuel Management and Quantity Gauging System (FMQGS) −
FMQGS Computer Change to Part No. GP546−1501−7.
NOTE
L−R FUEL RECIRC FAIL will be posted if the above systems
limitations are exceeded.
Fuel Recirculation switch must be OFF with bulk fuel temperature indication above 10 °C.
Effectivity:
· Airplanes 9002, 9004 thru 9095, 9097 thru 9114 not incorporating Service Bulletin:
· SB 700−28−044, Fuel Management and Quantity Gauging System (FMQGS) −
FMQGS Computer Change to Part No. GP546−1501−8.
or
· Airplanes 9003, 9096, 9115 thru 9132 not incorporating Service Bulletin:
· SB 700−28−045, Fuel Management and Quantity Gauging System (FMQGS) −
FMQGS Computer Change to Part No. GP546−1501−9.
Fuel Recirculation switch must be OFF with bulk fuel temperature indication above 0 °C.
NOTE
It is recommended that the system only be turned on when the
bulk fuel temperature reaches −25 °C.
Fuel Recirculation is prohibited when using wide cut or CIS fuels.
Asymmetric operation of Fuel Recirculation is prohibited during normal operation.
LIMITATIONS
POWER PLANT
DOT Approved
REV 47, Aug 30, 2005
Airplane Flight Manual
CSP 700−1A
02−05−10
4. OIL
A. Oil Temperature
Minimum for starting −40°C
Minimum before accelerating above idle +20°C
Maximum Permissible +160°C
B. Oil Pressure
See Figure 02−05−2.
Engine Oil Pressure Limits
Figure 02−05−2
C. Oil Grades
The Airplane Maintenance Manual, Chapter 12, lists the oils approved for use.
　
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