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NOTE
It is recommended that the system only be turned on when the
bulk fuel temperature reaches −25 °C.
Fuel Recirculation is prohibited when using wide cut or CIS fuels.
Asymmetric operation of Fuel Recirculation is prohibited during normal operation.
LIMITATIONS
POWER PLANT
Flight Crew Operating Manual REV 47, Aug 30, 2005
CSP 700−6
Volume 1
02−05−10
4. OIL
A. Oil Temperature
Minimum for starting −40°C
Minimum before accelerating above idle +20°C
Maximum Permissible +160°C
B. Oil Pressure
See Figure 02−05−2.
Engine Oil Pressure Limits
Figure 02−05−2
C. Oil Grades
The Airplane Maintenance Manual, Chapter 12, lists the oils approved for use.
D. Oil Consumption
Maximum oil consumption, on each engine, is 0.2 litre per hour (0.21 US quarts per hour).
LIMITATIONS
POWER PLANT
REV 47, Aug 30, 2005 Flight Crew Operating Manual
CSP 700−6
Volume 1
02−05−11
4. OIL (CONT'D)
E. Oil Replenishment
Operation of the oil replenishment system is prohibited when the OAT £ −12 °C.
5. AUTOTHROTTLE
A. TakeOff
The autothrottle must be engaged and takeoff
thrust verified prior to 60 KIAS for autothrottle
engaged takeoff.
B. Landing
Use of the autothrottle
when landing with flaps at any position other than flaps 30° is
prohibited.
6. AUXILIARY POWER UNIT
A. Type: RE 220
B. Maximum RPM: 106%
C. Maximum EGT (dependent upon altitude and OAT) :
· During start: 675 °C to 1038 °C.
· Normal operations: 613 °C to 732 °C.
D. Maximum Operating Altitude: 45,000 feet
E. Starting:
(1) Minimum ambient temperature for starting a cold soaked APU on the ground is −40 °C.
(2) The maximum number of start attempts per hour is three.
(3) Maximum Starting Altitude − 37,000 feet.
(4) Temperature − See Figure 02−04−1.
F. Bleed Air Extraction Limit:
(1) Bleed air extraction is limited to 30,000 feet.
(2) APU bleed extraction above 45 °C OAT for airconditioning
operation is prohibited.
LIMITATIONS
POWER PLANT
Flight Crew Operating Manual REV 47, Aug 30, 2005
CSP 700−6
Volume 1
02−05−12
1. OPERATING SPEEDS
A. Maximum Operating Speed and Mach Number
Maximum operating limit speeds as given in Figure 02−06−1.
GF0206_001 NEW_MMO.PLT
Maximum Operating Speed and Mach Number
Figure 02−06−1
LIMITATIONS
OPERATING SPEEDS
REV 42, Nov 26, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 1
02−06−1
1. OPERATING SPEEDS (CONT'D)
A. Maximum Operating Speed and Mach Number (Cont’d)
Effectivity:
· Airplanes 9002 thru 9094 not incorporating Service Bulletin:
· SB 700−34−020, Replacement of Micro AirData
Computer for RVSM Qualification
Requirements.
GF0206_002 mmo_afm_05_oct_98.plt
Maximum Operating Speed and Mach Number
Figure 02−06−1
LIMITATIONS
OPERATING SPEEDS
Flight Crew Operating Manual REV 42, Nov 26, 2004
CSP 700−6
Volume 1
02−06−2
1. OPERATING SPEEDS (CONT'D)
B. Design Maneuvering Speed
Full application of rudder and aileron controls as well as maneuvers that involve angles of
attack near the stall, must be confined to speeds below VA.
Values of VA are given in Figure 02−06−2, for varying pressure altitudes and airplane
weights.
NOTE: For 51,000 feet, the maneuvering ’g’ was reduced to 2.3 ’g’ due to stall limitations.
LIMITATIONS
OPERATING SPEEDS
REV 41, Jul 08, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 1
02−06−3
1. OPERATING SPEEDS (CONT'D)
B. Design Maneuvering Speed (Cont’d)
(If 43,545 kg (96,000 lb) MTOW placard is installed)
GF0206_003 gxvakm.p
Design Maneuvering Speeds
Figure 02−06−2
LIMITATIONS
OPERATING SPEEDS
Flight Crew Operating Manual REV 42, Nov 26, 2004
CSP 700−6
Volume 1
02−06−4
1. OPERATING SPEEDS (CONT'D)
B. Design Maneuvering Speed (Cont’d)
(If 44,452 kg (98,000 lb) MTOW placard is installed)
GF8206_003
Design Maneuvering Speeds
Figure 02−06−2
LIMITATIONS
OPERATING SPEEDS
REV 42, Nov 26, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 1
02−06−5
1. OPERATING SPEEDS (CONT'D)
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