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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
REV 6, Aug 30, 2005 Flight Crew Operating Manual
CSP 700−5000−6
Volume 1
02−05−5
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
WideCut
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
Flight Crew Operating Manual REV 6, Aug 30, 2005
CSP 700−5000−6
Volume 1
02−05−6
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
Fuel Recirculation must be inhibited when using wide cut or CIS fuels.
Asymmetric operation of Fuel Recirculation is prohibited during normal operation.
4. OIL
A. Oil Temperature
Minimum for starting −40°C
Minimum before accelerating above idle +20°C
Maximum Permissible +160°C
LIMITATIONS
POWER PLANT
REV 6, Aug 30, 2005 Flight Crew Operating Manual
CSP 700−5000−6
Volume 1
02−05−7
4. OIL (CONT'D)
B. Oil Pressure
See Figure 02−05−2.
Engine Oil Pressure Limits
Figure 02−05−2
C. Oil Grades
The Airplane Maintenance Manual, Chapter 51, lists the oils approved for use.
D. Oil Consumption
Maximum oil consumption, on each engine, is 0.2 litre per hour (0.21 US quarts per hour).
E. Oil Replenishment
Operation of the oil replenishment system is prohibited when the OAT £ −12 °C.
LIMITATIONS
POWER PLANT
Flight Crew Operating Manual REV 6, Aug 30, 2005
CSP 700−5000−6
Volume 1
02−05−8
5. AUTOTHROTTLE
A. TakeOff
The autothrottle must be engaged and takeoff
thrust verified prior to 60 KIAS for autothrottle
engaged takeoff.
B. Landing
Use of the autothrottle
when landing with flaps at any position other than flaps 30° is
prohibited.
6. AUXILIARY POWER UNIT
A. Type: RE 220
B. Maximum RPM: 106%
C. Maximum EGT (dependent upon altitude and OAT) :
· During start: 675 °C to 1038 °C.
· Normal operations: 613 °C to 732 °C.
D. Maximum Operating Altitude: 45,000 feet
E. Starting:
(1) Minimum ambient temperature for starting a cold soaked APU on the ground is −40 °C.
(2) The maximum number of start attempts per hour is three.
(3) Maximum Starting Altitude − 37,000 feet.
(4) Temperature − See Figure 02−04−1.
F. Bleed Air Extraction Limit:
(1) Bleed air extraction is limited to 30,000 feet.
(2) APU bleed extraction above 45 °C OAT for airconditioning
　
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