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26 Cards in this Set
- Front
- Back
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Circle-to-Land Approach Maneuver
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Weather minimums are at 1000 ft ceiling and three miles visibility, unless approach chart minimums specify higher.
Use a minimum descent altitude of 1000 ft above airport elevation unless restricted to a higher altitude in the circle-to-land minimums section on the approach chart. |
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Circuit Breakers
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A tripped circuit breaker may only be reset once. Allow approximately two minutes for cooling before resetting. An in-flight reset should only be accomplished if, in the judgment of the Captain, regaining use of that system is critical to the safe conduct of the flight. Flight Deck Crews must not reset tripped fuel quantity indicator, fuel pump, or fuel pump control circuit breakers."
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TCAS
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Flight Crews must immediately respond to TCAS information (both TAs and RAs) by using the TCAS (Traffic Avoidance) guidelines located in the QRH Section P Non-Normal Maneuvers/Profiles.
Pilots are authorized to deviate from an ATC clearance to the extent necessary to comply with the TCAS II Resolution Advisory (RA)." |
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Maximum Operating Pressure Altitude
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Maximum Operating Pressure Altitude
NG…41,000 feet CL…37,000 feet |
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Bleed Air (2)
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With engine bleed air switches ON, do not operate the air conditioning packs in HIGH for takeoff, approach, or landing.
(CL) Minimum duct start pressure is 30 PSI, reducing 0.5 PSI per 1000 feet above sea level. |
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Maximum Allowable Altitude for APU
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Aircraft…NG CL
Operation…41,000 feet 35,000 feet Electric Only…41,000 feet 35,000 Bleed Air Only…17,000 feet 17,000 Bleed Air and Electric…10,000 feet 10,000 |
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Cargo Bay
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Aircraft must land within 60 minutes of initial discharge of the fire suppression system.
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Electrical Power
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NG On the ground, limit one generator operation (engine driven) to a maximum of 215 amps.
Do not remove AC power from the aircraft for at least 30 seconds after IRS shutdown. |
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Flight Controls
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Flight Controls
Do not use speedbrakes in flight below 1000 feet AGL. In flight, do not extend the speedbrake lever beyond the flight detent. In flight, do not use speedbrakes unless the flaps are fully retracted. Alternate flap duty cycle in flight is one complete cycle, then 5 minutes off. A complete cycle is movement from position 0 to 15 and back to 0. The alternate flap switch must be in the OFF position for 15 seconds before reversing the direction of flap movement. Do not extend flaps above 20,000 feet pressure altitude. |
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Fuel Temperature Limits
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Max Fuel Tank Temperature: +49*C
Min Fuel Tank Temperature: -37*C Note: Jet A freeze point is - 40*C, and other listed fuels freeze at lower temperatures. |
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Fuel Distribution (#1)
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Fuel Distribution (#1)
Main tanks must be full if the center tank quantity is greater than 1000 pounds. Note 4: 1000 pounds may be retained in the center tank provided the effects of balance have been considered. Note 5: CL Center tank fuel pumps must be ON for takeoff with more than 1000 pounds of fuel in the center tank. Note 6: Some MEL items can overridethis limitation. Note 7: NG This limitation is modified under ADs 2002-19-52 and 2002-24-51. Refer to 3.12.2 Center Tank Fuel Limitations from ADs 2002-19-52 and 2002-24-51 in this section for operational details and requirements. |
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Fuel Distribution (#2)
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Fuel Distribution (#2)
Use center tank to depletion followed by wing tank fuel. |
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Fuel Distribution (#3)
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Fuel Distribution (#3)
For ground operation, center tank fuel pump switches must not be positioned to ON unless the center tank fuel quantity exceeds 1000 pounds, except when defueling or transferring fuel. |
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Fuel Distribution (#4)
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Fuel Distribution (#4)
Center tank fuel pump switches must be positioned to OFF when both center tank fuel pump low pressure lights illuminate. Note: The limitation does not changethe existing normal procedure to turn the center tank fuel pump switches to OFF at the first indication of low pressure from either pump. |
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Fuel Distribution (#5)
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Fuel Distribution (#5)
Center tank fuel pumps must not be ON unless personnel are available on the flightdeck to monitor the low pressure lights. |
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NG AD Center Tank Fuel Limitations
At All Times |
NG AD Center Tank Fuel Limitations
At All Times The fuel pump switches must be positioned OFF at the first indication of fuel pump low pressure. |
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NG AD Center Tank Fuel Limitations
Takeoff and Initial Climb |
NG AD Center Tank Fuel Limitations
Takeoff and Initial Climb Both center tank fuel pump switches must be positioned OFF for takeoff if center tank fuel quantity is less than 5000 pounds. When center tank fuel quantity is greater than 2000 pounds, turn on both center tank fuel pump switches above 10,000 feet or after reducing the pitch attitude to accelerate to 250 knots or greater. |
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NG AD Center Tank Fuel Limitations
Climb and Cruise |
If more than 2000 pounds of fuel remain in the center tank, both center tank fuel pump switches should be repositioned ON.
Turn one center fuel pump switch OFF during climb or cruise when the center tank fuel quantity reaches approximately 2000 pounds. Open the crossfeed valve to minimize fuel imbalance. When the MASTER CAUTION and FUEL system annunciator lights illuminate, turn the remaining center tank fuel pump switch OFF without delay and close the fuel crossfeed valve. |
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NG AD Center Tank Fuel Limitations
Descent |
NG AD Center Tank Fuel Limitations
Descent • Turn one center fuel pump switch OFF at the beginning of the descent if less than 3000 pounds of fuel remain in the center tank. Open the crossfeed valve to minimize fuel imbalance. • When the MASTER CAUTION and FUEL system annunciator lights illuminate, turn the remaining center tank fuel pump switch OFF without delay and close the fuel crossfeed valve. • If an extended period of level flight is required prior to approach and landing (i.e., holding), and fuel remains in the center tank, a single center tank fuel pump switch may be positioned ON if both fuel pumps were previously turned OFF. The fuel crossfeed valve should be opened to prevent fuel imbalance. |
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Ice and Rain
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Ice and Rain
NG: Holding in icing conditions are prohibited with flaps extended. |
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What is the maximum EGT for ground start?
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725*C
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Minimum duct pressure for engine start in classic fleet?
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30 PSI, less .5 PSI per 1000' above sea level.
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Engine Shutdown Limitations
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Operate the engines at idle for at least 1 minute prior to shutdown. When possible, operate the engines at idle for 3 minutes prior to shutdown.
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Reverse Thrust
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Reverse Thrust is for ground use only.
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RADAR
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Do not operate the weather RADAR during refueling, near fuel spills or people.
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Electrical Power
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Electrical Power
• NG On the ground, limit one generator operation (engine driven) to a maximum of 215 amps. • Do not remove AC power from the aircraft for at least 30 seconds after IRS shutdown." |
