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Chapter 6 - PERFORMANCE DATA) must be observed between a landing or
a rejected takeoff (RTO) and a subsequent takeoff, to ensure that a sufficient
brake energy is available to bring the airplane to a complete stop, if the
subsequent takeoff is rejected.
LIMITATIONS
DOT Approved May 30/2003 Airplane Flight Manual 02-05-01
REV 1 CSP 100-1
FUEL LIMITATIONS
APPROVED FUELS
Fuels conforming to any of the following specifications are approved for use.
Mixing of fuel types is permitted.
The maximum altitude is limited to 16 000 ft when JP-4 or JET B is used.
APPROVED FUEL ADDITIVES
Fuel additives (kerosene):
• Anti-icing additives MIL-I-27686 (0.1 to 0.15% by volume).
• Methyl cellosolve
• Biobar JF biocide (270 ppm)
• Shell ASA-3 anti-static additive
• Corrosion inhibitors: Appollo PRI-19 (0.0227 g/l), Dupont DCI-4A
(0.0227 g/l), Dupont DCI-6A (0.0227 g/l) Hitec E-515 (0.0457 g/l), Hitec
E-580 (0.0227 g/l) Nalco 5403 (0.0227 g/l), Nalco 5405 (0.0227 g/l),
Tolad 245 (0.0340 g/l).
• Anti-static additive: STADIS 450 (a), (b), (e), Sigbol (cis), TU-38101741.
FUELING
Single-point pressure refueling is limited to 55 psig (3792 hPa) and defueling
is limited to -8 psig (-552 hPa).
FUEL TRANSFER SYSTEMS
The Power and Gravity shut-off valves shall be selected off for takeoff.
CANADIAN AMERICAN BRITISH
CAN/CGSB-3.23-97 ASTM D1655-99 - JET A Def-Stan 91-91/3
CAN/CGSB-3.23-97 ASTM D1655-99 - JET A-1 Def-Stan 91-91/3
3-GP-24c MIL-DTL-5624T - JP-5 Def-Stan 91-86/2
CAN/CGSB-3.22-97 ASTM D1655-99 - JET B Def-Stan 91-88/1
CAN/CGSB-3.22-97 MIL-DTL-5624T - JP-4 Def-Stan 91-88/1
(METRIC) LIMITATIONS
02-05-02 Airplane Flight Manual DOT Approved Feb 02/2005
CSP 100-1 REV 2
(Metric)
FUEL LIMITATIONS (Cont)
USABLE FUEL LOAD
The maximum usable fuel load for each fuel tank is given below:
MINIMUM FUEL QUANTITY FOR GO-AROUND
The minimum fuel quantity for go-around is 500 lb (227 kg) per side.
MAXIMUM FUEL IMBALANCE
The maximum allowable fuel imbalance values are detailed in the Flight Crew
Operating Manual, Volume 1.
TEMPERATURE LIMITATIONS
The aircraft is prohibited from taking off if the bulk fuel temperature is
below -30 °C (-22 °F) for Jet A, and -35 °C (-31 °F) for Jet A1 and JP-5, and
-40 °C (-40 °F) for JP-4 and Jet B.
The aircraft is prohibited from taking off if the Bulk Fuel Temperature is above
50 °C (122 °F).
With wing bulk fuel temperature at 45 °C (113 °F) or above:
- the minimum fuel load for takeoff is 2800 lbs.
- with less than 1000 lbs of fuel per side, do not operate engine for more
than 30 minutes.
Pressure Refuel
Fuel Tank Fuel Mass †
Right 7075 lb 3210 kg
Left 7075 lb 3210 kg
Left & Right 14 150 lb 6420 kg
† Based on a fuel density of 6.75 lb/USG (0.809 kg/litre), rounded to the nearest
5 lb or 5 kg.
Gravity Refuel (Airplane Level)
Fuel Tank Fuel Mass †
Right 6500 lb 2950 kg
Left 6500 lb 2950 kg
Left & Right 13 000 lb 5900 kg
† Based on a fuel density of 6.75 lb/USG (0.809 kg/litre), rounded to the nearest
50 lb or 25 kg.
LIMITATIONS
DOT Approved Aug 16/2005 Airplane Flight Manual 02-06-01
REV 4 CSP 100-1
POWERPLANT LIMITATIONS
ENGINE TYPE
AS907-1-1A turbofan propulsion engines.
ENGINE OPERATION
The engine indicating system is designed to show system status with specified
colors. The limits are indicated in red.
ENGINE OPERATING LIMITS
Figure 02-06-01
LIMIT GROUND
START
AIR
START
7
IDLE MAX
REVERSE
MAXIMUM
CONTINUOUS
(CLB) 1
NORMAL
TAKEOFF
(TO) 2
APR
(MAX
POWER) 3
N1 -- -- -- 70.7%
4
95.2% 96.1% 96.1%
N2 -- -- 46.0%
min.
-- 97.2% 97.2% 98.1%
ITT 650 °C 700 °C
5
-- 928 °C 928 °C 928 °C 946 °C
OIL
TEMP -40 °C
min.
-- -- -- 138 °C max. 138 °C max.
27 °C min.6
138 °C max.
OIL
PRESS -- -- 28 psi
min.
8 8 8 8
1. Climb (CLB) equals maximum continuous thrust (MCT)
2. Normal Takeoff power is limited to 5 minutes
3. APR power (one engine inoperative) is limited to 10 minutes
4. Maximum reverse thrust is automatically reduced (ramped) commencing at 85 KIAS
5. Maximum ITT limit varies with N2 speed (400 °C when N2 <18% and ITT at start
initiation <250 °C)
6. Minimum oil temperature must be achieved before commencing takeoff. Below -30 °C
(-22 °F) the minimum oil temperature limit is 15 °C provided a fuel system icing
　
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