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Maximum Permissible Loads on DC Electrical System - Ground
Operation - Airplanes 3040 and Subsequent and Airplanes
Incorporating Canadair Service Bulletin 601-0107
Figure 7
LIMITATIONS
Page 24
DOT Approved
Mar 10/89
44,600
DOT Approved
Apr 20/98
44,600/45,100
LIMITATIONS
Page 25
8. SYSTEMS LIMITATIONS (Cont’d)
D. FLIGHT CONTROLS − LIFT/DRAG DEVICES
(1) Flaps
En-route use of flaps is prohibited.
Flight at altitudes above 15,500 feet with flaps extended is
prohibited.
(2) Flight Spoilers
On airplanes 3001 to 3039 which do not incorporate Canadair Service
Bulletin 601-0040, Modification − Central Warning System − Flight
Spoilers, or on airplanes incorporating Canadair Service Bulletin
601-0040 (Initial issue) and Canadair Service Bulletin 601-0095,
Modification − Flight Spoiler Warning System − Elimination of
Spurious Warnings:
(a) Flight below an altitude of 700 feet agl with flight spoilers
extended and the flaps retracted is prohibited.
(b) Flight spoilers must not be extended in flight with flaps
extended.
On airplanes 3013, 3018 to 3023, 3040 and subsequent and airplanes
incorporating Canadair Service Bulletin 601-0040 (Initial issue) only
(i.e. Service Bulletin 601-0095 not incorporated) or Canadair Service
Bulletin 601-0040 (Rev. 1):
(a) Flight below an altitude of 300 feet agl with flight spoilers
extended is prohibited.
(b) To ensure adequate manoeuvre margins, flight spoilers must not
be extended in flight at airspeeds below the recommended
approach speed (refer to PERFORMANCE − LANDING) plus 10 KIAS.
(3) Ground Spoilers
On airplanes 3001 to 3059 which do not incorporate Canadair Service
Bulletin 601-0113, Modification − Ground Spoilers − Auto Deployment:
The spoiler lever must not be selected to the GROUND SPOILER position
in flight.
MODEL CL−600−2A12
AIRPLANE FLIGHT MANUAL
PSP 601−1A−1
DOT Approved
Jan 19/07
44,600/45,100
LIMITATIONS
Page 26
8. SYSTEMS LIMITATIONS (Cont’d)
E. FUEL SYSTEM
The maximum permissible fuel imbalance between the contents of the main
fuel tanks is 800 lb (363 kg).
Take-off with up to 500 lb (230 kg) of fuel in the auxiliary tank is
permitted, provided that there is at least 1500 lb (690 kg) of fuel in
each wing tank and no fuel in the tail tank (if installed).
Take-off with more than 500 lb (230 kg) of fuel in the auxiliary tank is
permitted, provided that there is at least 4400 lb (1996 kg) of fuel in
each wing tank.
Fuel remaining in a tank when the appropriate fuel quantity indicator reads
zero is not usable.
The maximum usable fuel quantities shown below are achieved by pressure
fueling and are based on maximum achievable capacity with wings level,
aircraft 1/2 nose down and a standard day conversion factor of 6.8 lb/USG.
To determine approximate maximum usable fuel quantities by gravity fueling,
　
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