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Maximum Operating Pressure Altitude
NG - CL
- NG 41,000 feet
- CL 37,000 feet
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With engine bleed air switches ON, do not operate the air conditioning packs in _____ for _____, ______, or ________.
With engine bleed air switches ON, do not operate the air conditioning packs in HIGH for takeoff, approach, or landing
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Ice and Rain
Holding in icing conditions with flaps extended is: __________________.
Prohibited (NG only)
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Radar
Do not operate the weather radar during fueling, near fuel spills, or near people
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Electrical (2)
- 1. (NG) On the ground, limit one generator operation (engine driven) to a maximum of 215 amps
- 2. Do not remove AC power from the aircraft for at least 30 seconds after IRS shutdown
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Resetting a tripped circuit breaker in flight (2)
- 1. The in-flight reset of a tripped circuit breaker should only be accomplished when directed by the QRH. Allow approx. 2 minutes for cooling before resetting.
- 2. A tripped circuit breaker may only be reset once. Allow approx. 2 minutes cooling before resetting.
- An inflight 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.
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Power Plant
Minimum duct start pressure (CL only)
30 PSI, reducing 0.5 PSI per 1000 feet above sea level
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Maximum EGT for Ground Start
725 C
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Engine Stabilization and Cooldown (2)
- 1. Operate engines at or near idle, after rollback, for a minimum of 2 minutes prior to applying takeoff thrust.
- (Recommendation: 5 minutes on first flight of the day)
- 2. Operate engines at or near idle for a minimum of 1 minute prior to shutdown.
- (Recommendation: 3 minutes when operational conditions permit)
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Reverse Thrust
Reverse thrust is for ground use only.
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APU Altitude Limitations
NG;CL
- Operation 41,000; 35,000
- Electric Only 41,000; 35,000
- Bleed Air Only 17,000; 17,000
- Bld Air+Elec 10,000; 10,000
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Flight Controls: Speedbrakes (3)
- 1. In flight, do not extend the speedbrake lever beyond the flight detent
- 2. Do not use speedbrakes in flight below 1000 feet AGL
- 3. In flight, do not extend the speedbrakes unless the flaps are fully retracted
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Flight Controls: Flaps (2)
- 1. 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.
- 2. Do not extend flaps above 20,000 feet pressure altitude
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Fuel System - Min/Max temps
(Note)
- 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
Main tanks must be ____ if the center tank quantity is greater than ____ lbs.
(Note 7 - ______)
- Full; 1000lbs.
- Note 7- Some MEL items can override this limitation.
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Fuel Distribution Note 5
_____ lbs. may be retained in the center tank provided _____________.
The effects of balance have been considered.
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Fuel Distribution Note 6
Center tank fuel pumps must be ___ for all operations with more than _____ lbs. in the center tank.
ON; 1000 lbs.
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For ground operations, _____ tank fuel pump switches must not be positioned ____ unless the center tank fuel quantity exceeds ____ lbs. except when ________.
Center; ON; 1000 lbs; defueling or transferring fuel.
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Fuel may be transferred from tank to tank or the aircraft may be defueled with passengers onboard, provided ____.
Deplane all passengers and non-essential crew members when _____
The fuel quantity in the tank from which fuel is being taken is maintained at not less than 2000 lbs.
Deplane all passengers and non-essential crew members when defueling a tank or transferring fuel from a tank that has less than 2000 lbs. until the process has been completed and the respective fuel boost pumps are turned off.
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In the Classic, center tank fuel pump switches must be ____ when both center tank fuel pump LOW PRESSURE lights illminate.
OFF
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(NG) Corresponding center tank fuel pump switch must be positioned ____ when a LOW PRESSURE light illuminates.
OFF
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When established in level flight, both center tank pump switches should be positioned ___ if the center tank contains ____.
ON; Usable fuel.
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If the center tank is empty, both center tank fuel pump switches must be ___ when ______.
- OFF
- The first center tank fuel pump LOW PRESSURE light illuminates.
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Center tank fuel pumps must not be ____ unless:__________.
- ON
- Personnel are available on the flightdeck to monitor the LOW PRESSURE lights.
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May flight crews reset a tripped fuel quantity indicator, fuel pump, or fuel pump control circuit breaker?
NO!
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Cargo Bay Smoke Detection and Fire Suppression
- Aircraft must land within 60 minutes of initial discharge of the fire suppression system
- (8E = 195 minutes)
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TCAS (2)
- 1. Pilots are authorized to deviate from an ATC clearance to the extent necessary to comply with the TCAS II Resolution Advisory (RA)
- 2. Flight Crews must immediately respond to TCAS information (both TAs and RAs) by using the TCAS (Traffic Avoidance) guidelines located in the QRH Maneuvers chapter.
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Max headwind component for HGS AIII
25 kts.
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Max Crosswind (steady state)
35 Kts if wx 4,000+ RVR
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Max Tailwind (TO and Landing)
10 knots - incl gust
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Turbulent Air Penetration Speed At or Below 15,000 MSL
250 kt
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Turbulent Air Penetration Speed Above 15,000 MSL
280/.76 (CL .73)
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TO/LDG Operating Temperature Limits
-52 C. to +54 C.
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Max T.O. & Landing Altitude
8400 ft
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Engine Anti-ice is required:
When icing conditions exist or are anticipated, except during climb and cruise below -40 C SAT, and during descent in all icing conditions, including temps below -40 deg. C.
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Max speed with inoperative Mach Trim
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Max runway slope
Plus or minus 2%
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Minimum altitude for autopilot engagement after takeoff:
1000' AGL
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Minimum altitude for autothrottle disengagement during approach
50 ft below DA/DDA, no less than 50' AGL.
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Max Continuous EGT
NG:
CL:
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Starter Duty Cycle
- NG Normal Start:
- 2 minutes ON, 10 seconds OFF between start attempts
- CL Normal Start:
- 2 minutes ON, 20 seconds OFF.
- 2 minutes ON, 3 minutes OFF before next and each subsequent attempt.
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Minimum Engine Oil Quantity
- Flights less than 2 hours:
- NG - 60%, CL - 2 gallons
- Flights 2 hours or more:
- NG - 60%, CL - 2.5 gallons
- Flights departing a MTX station:
- NG - 70%
- CL - 3 gallons
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Captain must arrange for engine oil servicing when terminating at a non-maintenance base with:
- NG - less than 65%
- CL - less than 2.5 gallons
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APU Start Limitations
Wait 90 seconds prior to a second start attempt. Allow 5 minutes cooling before a third attempt. Do not attempt a fourth start.
Wait at least 20 seconds after APU shutdown prior to turning the battery switch OFF.
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APU Recommendations
The APU should the operated for one minute before being used as a bleed source.
CL: The APU BLEED switch should be off for at least 2 minutes before APU shutdown.
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RSVM max allowable inflight difference between Captain and FO altimeters.
200 ft
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Do not use LNAV if the message -
"UNABLE REQD NAV PERF-RNP" is active.
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When can VNAV be engaged for takeoff, initial climb, or missed approach?
When flap retraction is complete.
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VNAV Policies
VNAV use during the final approach segment is only allowed on RNAV approaches.
CL: Two operable CDUs are required for VNAV.
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Fuel Tank Quantities
- NG Mains: 8,600 lb Center: 28,800 lb
- CL: Mains: 10,000 lb Center: 15,500 lb
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Minimum fuel for the ground operation of electric hydraulic pumps is?
1675 lbs in the respective wing tank.
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Max Speed for Landing Gear
Extension:
Retraction:
Extended:
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When must Auto-Brakes be used?
(3)
- 1. On any runway that is not DRY
- 2. If the reported visibility is less than 4000 RVR or 3/4 miles
- 3. Landing with less than flaps 30 (single engine or abnormal configuration)
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When is a flaps 40 landing recommended?
- 1. Negative [bracketed] OPC stopping margin under MIN (2) for flaps 30
- 2. Reported braking action less than GOOD
- 3. Weather at or near minimums for the approach being flown
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What is MAX cabin differential for T.O. and landing?
0.125 psi
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What is normal AC frequency?
400 cps (+/- 10)
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What is normal battery voltage range?
23 - 30 volts
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What is max crosswind component for landing with less than 4000 RVR or 3/4 mile?
15 knots
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What is max crosswind component for landing with braking action reported as POOR?
10 knots
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What is normal AC voltage output?
115 volts (+/- 5)
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Regarding takeoff and landing with an inoperative thrust reverser?
- Takeoff and landing is not authorized if either thrust reverser is inoperative:
- AND the runway is contaminated with clutter
- OR the breaking action is less than good
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What is the safety relief differential pressure?
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Runway Contamination (Clutter) Limitations
On the runway: Takeoff / Landing
Water or slush
Wet snow
Dry snow
- Water or slush 1/2 inch / 1 inch
- Wet snow 1 inch / 2 inches
- Dry snow 4 inches / 6 inches
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For the -700 and CL, the maximum brake temp for turnaround is?
425 F
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For the -800, carbon brakes are limited to a fixed time of ____ minutes for ground turnaround if the maximum quick turnaround weight is exceeded.
48 minutes
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