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C. ELECTRICAL SYSTEMS
Unless it has been established that any AC Generator with a part number
720845, 720845A or 720845B has more than 150 operating hours:
Prior to every flight a visual inspection of the engine cowls and
drains for evidence of AC Generator oil leakage must be conducted.
If generator oil leakage is evident, generator must be replaced.
Unless it has been established that an APU Generator with a part number
720845, 720845A or 720845B has more than 150 operating hours:
Prior to every flight a visual inspection of the APU drains for
evidence of generator oil leakage must be conducted. If oil leakage
is evident, APU Generator must be replaced unless it has been
established that AC Generators with part numbers 720845, 720845A or
720845B are not installed, or if installed, both have more than 150
operating hours.
(1) Permissible Loads on AC Systems
Individual AC generator loading, as indicated by the loadmeters, must
not exceed the following values:
Altitude
(feet)
0 - 11,000
11,000 - 20,000
20,000 - 35,000
35,000 and above
L o a d Limitation
(kV
Main Generator
(each)
30
30
30
25
mi tat ion
VA)
APU Generator
CO CO
CD CD
LIMITATIONS
Page 22
DOT Approved
Oct 25/02
44,600/45,100
canadair
chanenqer
MODEL CL-600-2A12
AIRPLANE FLIGHT MANUAL
PSP 601-1A-1
8. SYSTEMS LIMITATIONS (Cont'd)
C. ELECTRICAL SYSTEMS (Cont'd)
(2) Permissible Loads on DC Systems
(a) In Flight
The maximum permissible continuous load on TRU 1 or TRU 2 is
100 amps.
The maximum permissible continuous load on TRU 3 is 50 amps.
(b) Ground Operation
Total combined loads on TRU 1 and TRU 2 must not exceed limits
shown in Figure 6 or Figure 7.
Individual loads on TRU 1 and TRU 2 must not exceed 100 amps. If
TRUs are inadvertently operated at limiting loads for periods
longer than those shown, the nose bay doors must be opened for
10 minutes minimum prior to taxi for take-off.
(3) Permissible Operating Time
During ground operation at ambient temperatures above 45°C (113°F),
operation of electrical/avionics equipment must be limited to
30 minutes unless at least one environmental control system is
operating and cabin doors closed.
DOT Approved
O c t25/0 2 ,nn LIMITATIONS
44,600/45,100 Page
canadair
chanenqer
MODEL CL-600-2A12
AIRPLANE FLIGHT MANUAL
PSP 601-1A-1
THIS PAGE INTENTIONALLY LEFT BLANK
DOT Approved
LIMITATIONS Oct 25/02
Page 22B 44,600/45,100
canadair
chaiienqier
MODEL CL-600-2A12
AIRPLANE FLIGHT MANUAL
PSP 601-1A-1
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