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Maximum Landing Weight
97000 lbs
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Maximum 90° crosswind component(including gusts) for:
Rolling takeoff and landing
Static Takeoff
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Maximum headwind for Cat II/IIIa approaches
25 knots
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Maximum 90° crosswind component(including gusts) for Cat II/IIIa approaches
15 knots
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Maximum takeoff and landing tailwind component
10 knots
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Maximum operating altitude
41,000 feet
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Maximum altitude with flaps extended
20,000 feet
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Minimum runway length for LAHSO
6,000 feet
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Maximum operating airspeed
VMO
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Maximum operating Mach number
.82 (MMO)
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Turbulent airspeed (below 10,000 feet)
250 KIAS
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Turbulent airspeed (at or above 10,000 feet)
270 KIAS/.76M
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Maximum airspeed for windshield wiper operation
250 KIAS
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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
240 KIAS
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Icing Conditions are defined as.• OAT (on the ground and for takeoff) or TAT (inflight) is _____________, and visible moisture in any form is present such as clouds, fog with visibility ofone mile or less, rain, snow, sleet, and ice crystals, or when operating on ramps, taxiways or runways where surface snow, ice,standing water, or slush may be ingested by engines, or freeze on engines,nacelles, or engine sensor probes
10 °C or below
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During taxi out and takeoff, the ___________ must be set to ____ when _________ or below and icing conditions exist or are anticipated.
- MCDU TO DATASET MENU REF A/I
- ALL
- OAT is 10°C
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Maximum permissible fuel imbalance between left and right main tanks during all phases is
800 lbs
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Maximum altitude for single pack operation
31,000 feet
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Maximum Altitude with Flaps/Slats Extended
20,000 feet
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EICAS marking colors used for;
Maximum and Minimum Limitations - ____
Caution Range - ____
Normal Operating Range - ____
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Engine Starter Maximum Duty Cycle for all Starts
- 90 seconds ON (ground)
- 120 seconds ON (in flight)
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Engine Starter Minimum Rest Periods after;
1st and 2nd Starts ____
3rd thru 5th Starts ____
- 10 Seconds OFF
- 5 Minutes OFF
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Maximum reverse thrust is not permitted at airspeeds
below sixty (60) KIAS
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Below 60 KIAS _________ reverse thrust to ________.
reduce
IDLE
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APU Starter Minimum Rest Periods following;
1st and 2nd starts ___________
3rd start ___________
- 60 seconds OFF
- 5 minutes OFF
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APU Operational altitude Limits;
Start _______
Electrical _______
Bleed _______
Assist Engine Start ______
- Start 30,000 Feet
- Elec 33,000 Feet
- Bleed 15,000 Feet
- Assist 21,000 Feet
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The maximum allowable in-flight difference between Captain and FirstOfficers altitude displays for RVSM operations is
200 feet
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QRH
CABIN ALTITUDE HI / Rapid Depressurization
- 1. Oxygen Masks... Verify..ON, 100%
- 2. Captain assumes PF duties.
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QRH
Jammed Control Column - Pitch
1. ELEVATOR DISCONNECT...Confirm .... PRESS and PULL
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QRH
Jammed Control Wheel - Roll
1. AILERON DISCONNECT ...Confirm ... PRESS and PULL
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QRH
PITCH TRIM Runaway
1. AP/TRIM DISC...PRESS and HOLD
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QRH
(ROLL or YAW) TRIM Runaway
1. AP/TRIM DISC..PRESS and HOLD
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QRH
Nosewheel Steering Runaway
1. STEER DISC..Press
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QRH
Aborted Engine Start
- 1. Associated Thrust Lever .. IDLE
- 2. Associated START/STOP..STOP
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