Limits Flashcards
Runway Slope
+- 2%
Vmo
340
Mmo
0.82
Maximum Operating Altitude
41,000
Maximum Takeoff and Landing Altitude
8,400
Maximum Takeoff Crosswinds (flaps 1,5 dry)
35 knots
Maximum Takeoff Crosswinds (flaps > 5, dry)
30 knots
Maximum Takeoff Crosswind (all flaps, wet)
25 knots
Maximum Landing Crosswind (All flaps, dry)
35 knots
Maximum Landing Crosswind (All flaps, wet)
30 knots
Maximum Takeoff and Landing Crosswind (all flaps, contaminated)
15 knots
Maximum Takeoff and Landing Tailwind Componet
15 Knots
Maximum Total Air Temperature (TAT)
55°C
Maximum Touch and Go Crosswind Reccomendation
25 knots
Maximum Landing Crosswind Recommendation Flaps 40
30 knots
RVSM Maximum In-Flight Altitude Difference
200 ft
Maximum RVSM On-The-Ground Altitude Display Difference
50 ft (sea level - 5,000)
60 ft (5,001 - 10,000)
Maximum RVSM On-The-Ground Altitude Between Display and Field Elevation
75 ft
IDG Load Limit During Ground Operations
41% Load requires 32% N1
Engine Oil Minimum
Overland: 60% (12 Quarts)
Overwater: 60% (12 Quarts) or 7 Quarts plus 1 Quart per Total Flight Hour (whichever is higher)
Minimum Oil to Arrive at Destination or Alternate
7 Quarts
Maximum Takeoff EGT
950-965°C (3 minutes)
950°C (5 minutes) (Increases to 10 min if Engine Failure Occurs)
Maximum Continuous EGT
925°C
Maximum Start EGT
725°C
Maximum N1 RPM
104.7% (20 seconds)
104.0% (continuous)
Maximum N2 RPM
105%
Minimum Oil Pressure
13 psi
Maximum Oil Temperature
155°C (maximum)
140-155°C (45 minutes)
140°C (continuous)
Engine Idle Time Prior to Shutdown
3 Minutes
Maximum Start Time
2 Minutes
Time Required Between Starts
10 seconds
Maximum N2 to Engage Starter
55%
Engine Ignition for Moderate or Heavy Rain, Hail or Sleet
CONT
Engine Ignition for Severe Turbulance
FLT
Assumed Temperature Method Limits
Shall not be amused for EEC in Alternate Mode, Contaminated With Slush, Snow, Standing Water or Ice, or when Antiskid is Inoperative
Not Recommended for Potential Windshear
Reduced Thrust Takeoff Limits
Not Recommended for Potential Windshear
Shall Not Be Used for Takeoff With EEC in Alternate
EEC in Alternate for Takeoff Limits
1) Both in Alternate
2) No Fixed Derate or ATM
3) Do Not Use FMC Takeoff N1
4) Use of Autothrottle is Prohibited
AAR Airspeed Envelope
250-300 Knots
AAIR Altitude Envelope
8,000-28,000 ft
Minimum On-Station Altitude
200 ft AGL
Minimum Altitude for Seat Swaps
1,000 ft AGL
Maximum Taxi Weight
189,700 lbs
Maximum Takeoff Weight
189,200 lbs
Maximum Landing Weight
149,800 lbs
Maximum Zero Fuel Weight
141,800 lbs
Maximum Fuel Temperature
Active Feeding: 59°C
Not Feeding: 62°C
Maximum Fuel Imbalance
1,000 lbs
Minimum Fuel for Landing
6,000 lbs or 10% of Total Fuel Required (Transit+Onstation+Alternate)
Minimum Temperature for Hot Fuel Mins
38°C
Emergency On Deck Fuel
4,000 lbs
Minimum Fuel for Electric Hyd Pumps
1,675 lbs in Related Tank
APU Bleed Air and Electrical Load Maximum Altitude
10,000 ft
APU Bleed Air Maximum Altitude
17,000 ft
APU Electrical Load Maximum Altitude
41,000 ft
APU Altitude and Load Limit
32,000 ft, load must be below 68%
Icing Conditions
10°C and Visible Moisture
Minimum Altitude for Autopilot on Takeoff
400 ft
CWS Bank Angle Limit
Above 1,500 ft: 45° AOB
Below 1,500 ft: 30° AOB
Autopilot Minimum Altitude
Non-Terminal: 500ft
Approach: Minimums (50ft below DH or 50+MDA) or 100ft AGL
Turbulent Air Penetration Speed
280 knots
0.76 Mach
Maximum Hydraulic Pressure
3,500 psi
Hydraulic Quantity Limits
Minimum: 76%
Maximum: 106%
Prohibited Operations
1) Intentional spins, stalls, aerobatics, steep dives (not associated with an Emergency Descent), or maneuvers resulting in abrupt accelerations
2) Use of auto land
3) Load factor greater than 2.0 g’s with asymmetric thrust
4) Holding and on-station mission operations in icing with flaps extended
5) Use of Mission Limit Mode
6) Uninterrupted rudder deflections across the neutral position (commonly referred to as rudder reversals). Approximately zero side slip and yaw must be established at neutral position
7) Rapid rudder check or rapid release to neutral after abrupt rudder input
8) Alternating control inputs, especially in combination with large changes in pitch, roll or yaw (e.g., large sideslip angles)
9) Uninterruped rapid wheel inputs across the neutral position at roll rated greater than 10° per sec
10) Inflight aux fuel functions fwd>aft aft>fwd, except to prevent or correct a cg limit exceedence
11) Flight beyond stick shaker or initial buffet
12) Intentional single engine or simulated single engine maneuvers, except as required for FCF
13) Use of tactical fuel flow margin
