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D. Oil Consumption
Maximum oil consumption, on each engine, is 0.2 litre per hour (0.21 US quarts per hour).
LIMITATIONS
POWER PLANT
DOT Approved
REV 47, Aug 30, 2005
Airplane Flight Manual
CSP 700−1A
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
DOT Approved
REV 47, Aug 30, 2005
Airplane Flight Manual
CSP 700−1A
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
DOT Approved
REV 42, Nov 26, 2004
Airplane Flight Manual
CSP 700−1A
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
DOT Approved
REV 42, Nov 26, 2004
Airplane Flight Manual
CSP 700−1A
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.
GF8206_003
Design Maneuvering Speeds
Figure 02−06−2
LIMITATIONS
OPERATING SPEEDS
DOT Approved
REV 39, Dec 01, 2003
Airplane Flight Manual
CSP 700−1A
02−06−3
1. OPERATING SPEEDS (CONT'D)
C. Slat/Flap Extended Speed
The maximum speeds at which the slats/flaps may be extended are:
· Slats extended: 225 KIAS
· Flaps to 6 degrees: 210 KIAS
· Flaps to 16 degrees: 210 KIAS
· Flaps to 30 degrees: 185 KIAS
D. Maximum Landing Gear Operating Speed
· The maximum airspeed at which it is safe to retract the landing gear is 200 KIAS.
· The maximum airspeed at which it is safe to extend the landing gear is 200 KIAS.
E. Maximum Landing Gear Extended Speed
The maximum airspeed at which the airplane may be flown with the landing gear extended is
250 KIAS / 0.7 M.
Flight at altitudes above 20,000 feet with the landing gear extended is prohibited.
F. Tire Limit Speed
The tire limit speed is 183 knots ground speed.
G. Turbulence Penetration Speed
Maximum air speed for turbulence penetration is 300 KIAS or .80 Mach, whichever is lower.
NOTE
Turbulence penetration maneuvers must be accomplished in
accordance with the procedures detailed in Flight Crew Operating
Manual Vol 1, Chapter 7; SUPPLEMENTARY PROCEDURES −
FLIGHT IN TURBULENCE.
H. Minimum Operating Limit Speed
Intentional speed reduction below the onset of stall warning, as defined by stick shaker
operation, is prohibited.
VMCG is 80 KIAS and VMCA in the takeoff
configuration is 86 KIAS.
LIMITATIONS
OPERATING SPEEDS
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