Limitations Flashcards
Maximum Operating Altitude
3.1.1.2
41,000 feet
Maximum Flight Operation Latitude
3.1.1.3
82° North and 82° South
Maximum Runway Slope
3.1.1.6.
+/- 2%
Take off & landing tail wind - Maximum
3.1.1.7
10 knots
Takeoff crosswind - Maximum
3.1.1.7
-700/-800 33 knots, -8 35 knots
Landing crosswind - Maximum
3.1.1.7
-700/-800 33 knots, -8 32 knots
Land Crosswind limit - BAR - Dry Runway
3.1.1.7
-700/-800 33 knots, -8 32 knots
Land Crosswind limit - BAR - Good
3.1.1.7
-700/-800 33 knots. -8 32 knots
Land Crosswind limit - BAR - Good to Medium
3.1.1.7
All 25 Knots
Land Crosswind limit - BAR - Medium
3.1.1.7
All 20 knots
Land Crosswind limit - BAR - Medium to Poor
3.1.1.7
All 15 knots
Land Crosswind limit - BAR - Poor
3.1.1.7
All 10 knots
Maximum Speeds
3.1.1.10
Observe Gear and flap placards
Escape Slide Retention Bar On revenue passenger flights during taxi , takeoff, and landing
3.1.1.11
Installed
Autopilot Engaged - Minimum Altitude - Takeoff
3.2.2
400 feet AGL
Autopilot Engaged - Minimum Altitude - Single channel operation during approach
3.2.2
50 feet AGL
Engine Limitations and Display Markings - Maximum and Minimum Limits
3.4.1
Red
Engine Limitations and Display Markings - Caution Limits
3.4.1
Amber
Engine Ignition - On
3.4.2
Takeoff, Landing, Operation in Heavy Rain & Ant-ice operation
Starter Duty Cycle - NG
3.4.3
2 Minutes On - 10 seconds between start attempts
Starter Duty Cycle - MAX
3.4.3
3 Minutes On - 10 seconds between start attempts
Reverse Thrust Intentional selection in flights
3.4.4
Prohibited
APU - Bleed and Electrical Load - Maximum altitude
3.4.5
10,000 feet
APU - Bleed Only - Maximum altitude
3.4.5
17,000 feet
APU - Electrical load only - Maximum altitude
3.4.5
41,000 feet
What must be avoided with a Dual Bleed light illuminated?
Thrust must be limited to idle
Wide Cut Fuels JP-4 or Jet B
3.5.1
Prohibitied
Maximum fuel tank temperature
3.5.2
49°C
Minimum fuel tank temperautre
-43° C or 3°C above the freezing point of fuel being used. Whichever is higher.
Fuel Imbalance - Allowable lateral imbalance between main and tanks 1 and 2
3.5.3
Must be scheduled to be zero
Random fuel imbalance for taxi, takeoff, flight or landing
3.5.3
Must not exceed 1,000 lbs
Maximum flap extension altitude
3.6.1
20,000 feet
Holding in icing conditions with flaps extended
3.6.1
Prohibited
Under what conditions must engine anti-ice be selected on?
When icing conditions exist or are anticipated, except during climb and cruise below -40°C SAT. Icing conditions are defined as, the ambient temperature is +10°C or below and any of the following conditions exist; Visible moisture such as clouds or fog with visibility less than 1nm, rain, snow, sleet, or ice crystals; Standing water, ice, snow, is present on ramps, taxiways, or runways.
Speedbrakes - Minimum radio altitudes for deployment in flight
3.6.2
1,000 feet
Under what conditions are reduced thrust takeoffs not permitted?
Slippery or contaminated runways, anti skid inop, when special departure procedures specify max Thrust for T/O, wind shear is present, or EEC in alternate mode
Maximum Differential
3.9.1
9.1 PSI
AUTOLAND
Maximum allowable wind speeds when landing weather minima are predicated on autoland operations?
FOM 3.2.3
Headwind 25 knots;
Tailwind 10 knots;
Maximum crosswind 20 knots; and
Autoland capability may only be used with flaps 30 or 40 and both engines
operative.
Not authorized for overweight landings.
The maximum and minimum glideslope angles are 3.25 and 2.5 degrees, respectively.
Engine Warm Up Requirement
FOM 4.5.1
(B737NG) Verify an increase in engine oil temperature before takeoff
(B737MAX) Verify engine oil temperature is at or above 31°C before takeoff
Run the engine, for at least 2 minutes (B737NG) or 3 minutes (B737MAX), using a
thrust setting normally used for taxi operations before applying takeoff thrust
