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processes remove the inhibitor).
 Appollo PRI-19, at a maximum concentration of 0.0227 g/l;
 Octel DCI-4A or DCI-6A, at a maximum concentration of 0.0227 g/l;
 Hitec E-515, at a maximum concentration of 0.0457 g/l;
 Hitec E-580, at a maximum concentration of 0.0227 g/l;
 Nalco 5403 or 5405, at a maximum concentration of 0.0227 g/l;
 Tolad 245, at a maximum concentration of 0.0340 g/l.
MODEL CL−600−2A12
AIRPLANE FLIGHT MANUAL
PSP 601−1A−1
DOT Approved
Sep 11/06
44,600/45,100
LIMITATIONS
Page 12
4. POWER PLANT LIMITATIONS (Cont’d)
K. OIL GRADES
Refer to appropriate maintenance or servicing manual for approved oil
grades.
L. OIL REPLENISHMENT SYSTEM
The oil replenishment system must not be operated before fifteen (15)
minutes have elapsed after engine shutdown.
M. AUXILIARY POWER UNIT (APU) OPERATING LIMITS
On airplanes incorporating Service Bulletin 601−0568 or 601−0581:
APU type: 36-150(CL)
On airplanes not incorporating Service Bulletin 601−0568 or 601−0581:
APU type: GTCP-36-100(E)
The APU must not be operated if APU generator oil leakage is evident.
Unless it has been established that any main generator with a part number
720845, 720845A or 720845B has more than 150 operating hours, the
Auxiliary Power Unit (APU) and APU generator systems must be serviceable
for dispatch.
Maximum rpm: 110%
The APU overspeed control will automatically shutdown the APU at 107% rpm
(110% on airplanes not incorporating Service Bulletin 601−0568 or
601−0581).
Maximum EGT: 732C
Starting:
Minimum ambient temperature for starting a cold soaked APU on the ground
is −40C
The following APU start cycles are permitted:
(a) Using aircraft batteries on the ground or for normal in-flight start:
Three start attempts, each of 30 seconds continuous cranking,
followed by a 20-minute off-time, followed by two further attempts
each of 30 seconds continuous cranking.
(b) Using ground power:
Two start attempts, each of 15 seconds continuous cranking, followed
by a 20-minute off-time, followed by two further attempts each of 15
seconds continuous cranking.
If, in either case (a) or (b) a successful start is not obtained, a
further start must not be attempted for a period of at least 35 minutes.
MODEL CL−600−2A12
AIRPLANE FLIGHT MANUAL
PSP 601−1A−1
DOT Approved
Dec 21/06
44,600/45,100
LIMITATIONS
Page 13
4. POWER PLANT LIMITATIONS (Cont’d)
M. AUXILIARY POWER UNIT (APU) OPERATING LIMITS (Cont’d)
The APU RDY light must be on within 60 seconds of operating the APU start
switch.
Maximum EGT: 974C not to be exceeded under any operating conditions.
Hung start:
On airplanes not incorporating Service Bulletin 601−0568 or 601−0581:
Below 60% rpm − maximum 20 seconds
Between 60% and 95% rpm − maximum 10 seconds
On airplanes incorporating Service Bulletin 601−0568 or 601−0581:
If not greater than 30% rpm within 60 seconds
APU starting and operation is permitted within the following operating
envelope:
Airspeed: Sea level to 10,000 feet: 0 to 290 KIAS
10,000 feet to 20,000 feet: 141 KIAS to 290 KIAS
Temperature: Refer to Figure 2
Altitude: Refer to Figure 4 or 4A
Do not operate the APU in-flight if a main engine fails and engine rotor
burst damage is suspected.
In-Flight Starting:
On airplanes not incorporating Service Bulletin 601−0568 or 601−0581:
In-flight starting is guaranteed at altitudes up to 15,000 feet
and has been demonstrated at altitudes up to 20,000 feet.
On airplanes incorporating Service Bulletin 601−0568 or 601−0581:
In-flight starting is guaranteed at altitudes up to 20,000 feet.
Air Conditioning:
On airplanes not incorporating Service Bulletin 601−0568 or 601−0581:
(a) APU bleed air extraction is not permitted above 14,500 feet pressure
altitude.
(b) APU bleed air extraction is not permitted in flight whenever standby
electrical power is required from the APU.
On airplanes incorporating Service Bulletin 601−0568 or 601−0581:
(a) APU bleed air extraction is not permitted above 15,000 feet pressure
altitude.
MODEL CL−600−2A12
AIRPLANE FLIGHT MANUAL
PSP 601−1A−1
DOT Approved
Sep 11/06
44,600/45,100
LIMITATIONS
Page 14
4. POWER PLANT LIMITATIONS (Cont’d)
M. AUXILIARY POWER UNIT (APU) OPERATING LIMITS (Cont’d)
Main Engine Starting:
　
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