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0
KIAS
5000
10000
15000
20000
25000
30000
Windmill
Envelope
(7.2% Min. N2)
ATS Envelope
Special
AEO
Rapid
Relight
NOTE: Special All-Engine Out Rapid Relight Envelope, from 10,000 feet to S. L. and 200 to 250 KIAS.
330 KIAS
21,000 ft
8,000 ft
335 KIAS
Starter Assist Required
(Fuel in at 20% N2 min.)
25,000 ft
Airplane Flight Manual
CSP C-012 DOT Approved
REV 2A, Jul 14/04
LIMITATIONS
Power Plant
02--05--5
6. FUEL
Pending Rectification:
Centre tank fuel quantity must be monitored throughout flight.
Themaximumpermissible fuel imbalance between the contents of themain left tank and themain
right tank are given below:
S During take-off -- 136 kg (300 lb)
S All other phases of flight -- 363 kg (800 lb)
Fuel remaining in a tank when the appropriate fuel quantity indicator reads zero is not usable.
The fuel quantities below are based on 6.75 lb/perUS gal. Themaximumusable fuel load for each
fuel tank is given below:
Pressure Refueling Gravity Refueling
Left main tank 3,398 kg (7,492 lb) 3,359 kg (7,405 lb)
Right main tank 3,398 kg (7,492 lb) 3,359 kg (7,405 lb)
Centre tank 2,091 kg (4,610 lb)
Total 8,888 kg (19,595 lb) 6,718 kg (14,810 lb)
Take-offwith a fuel load in excess of 227 kg (500 lb) in the centre tank is not permitted unless each
main wing tank is above 1,996 kg (4,400 lb).
The minimum fuel quantity for go-around is 272 kg (600 lb) per wing (with the airplane level) and
assuming a maximum airplane climb attitude of 10° nose up.
Dispatch with the fuel quantity gauging system inoperative is prohibited.
A. Fuel Temperature
S Take-off with engine fuel temperature indications below 5°C (41°F) is prohibited.
S Take-off with bulk fuel temperature indications below the limits stated is prohibited.
S During flight, bulk fuel temperature must remain above the applicable bulk fuel freezing
point.
Fuel Bulk Fuel Take-off Limit Bulk Fuel Freezing Point
ASTM D 1655 JET A ---30_C --40 °C
ASTM D 1655 JET A1 ---37_C --47 °C
MIL T--5624 JP 5 ---36_C --46 °C
MIL T--83133 JP 8 ---40_C --50 °C
GB6537---94
No. 3 Jet ---37_C ---47_C
Airplane Flight Manual
CSP C-012 DOT Approved
REV 2, Feb 24/04
LIMITATIONS
Power Plant
02--05--6
B. Fuel Grades
S Fuels conforming to any of the following specifications are approved for use. Mixing of
fuels is permitted.
CANADIAN AMERICAN BRITISH ROMANIAN CHINESE
CAN 2 - 3.23 ASTM D1655
JET A DEF. STAN 2494
CAN 2 - 3.23 ASTM D1655
JET A1 DEF. STAN 2494 STAS 5639/88
TH †
GB6537---94
No. 3 Jet
-- MIL-T-83133
JP-8 DEF. STAN 2453
-- MIL-T-5624 JP-5 DEF. STAN 2452
† Fuel additives restricted to those listed in paragraph C. (below) and / or antistatic
STADIS-450 (max 3 ppm).
C. Fuel Additives
The following additives, used individually or in combination, are approved:
S Anti-icing 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.
S Anti-icing Methyl Cellosolve at concentrations of 0.10 to 0.15% by volume.
S 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 micro-organisms.
S Shell ASA-3 anti-static additive at a concentration that will provide not in excess of
300 conductivity units, which is approximately equivalent to 1 part per million.
D. Fuel Crossflow
S Powered crossflow and gravity crossflow must be off for take-off.
Airplane Flight Manual
CSP C-012 DOT Approved
REV 2, Feb 24/04
LIMITATIONS
Power Plant
02--05--7
7. OIL GRADES
NOTE
Mixing of different types of oils is prohibited.
COMPONENT MIL-L-23699
(TYPE II)
MIL-L-7808
(TYPE I) CASTROL 4000
Engines n n n
Air Turbine Starter n n n
Integrated Drive
Generator
n n n
Auxiliary Power Unit n n n
8. OIL CONSUMPTION
Maximum oil consumption, on each engine, is 189 cubic centimeter per hour (6.4 US ounces per
hour 0.05 US gallons per hour).
9. ENGINE OIL LEVEL
Engine oil levels must be checked as follows:
S The maximum duration without engine oil servicing is 36 operating hours.
S For airplane operations in excess of 36 operating hours (without engine oil tank servicing),
the engine oil level must be checked within 3 minutes to 1 hour after every engine
shutdown.
10. OIL REPLENISHMENT SYSTEM
If use of the oil replenishment system is required, then the engine(s) should be replenished
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