Limits Flashcards by Scott Long

Runway Slope

+- 2%

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Vmo

340

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Mmo

0.82

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Maximum Operating Altitude

41,000

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Maximum Takeoff and Landing Altitude

8,400

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Maximum Takeoff Crosswinds (flaps 1,5 dry)

35 knots

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Maximum Takeoff Crosswinds (flaps > 5, dry)

30 knots

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Maximum Takeoff Crosswind (all flaps, wet)

25 knots

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Maximum Landing Crosswind (All flaps, dry)

35 knots

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Maximum Landing Crosswind (All flaps, wet)

30 knots

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Maximum Takeoff and Landing Crosswind (all flaps, contaminated)

15 knots

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Maximum Takeoff and Landing Tailwind Componet

15 Knots

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Maximum Total Air Temperature (TAT)

55°C

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Maximum Touch and Go Crosswind Reccomendation

25 knots

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Maximum Landing Crosswind Recommendation Flaps 40

30 knots

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RVSM Maximum In-Flight Altitude Difference

200 ft

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Maximum RVSM On-The-Ground Altitude Display Difference

50 ft (sea level - 5,000)
60 ft (5,001 - 10,000)

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Maximum RVSM On-The-Ground Altitude Between Display and Field Elevation

75 ft

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IDG Load Limit During Ground Operations

41% Load requires 32% N1

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Engine Oil Minimum

Overland: 60% (12 Quarts)
Overwater: 60% (12 Quarts) or 7 Quarts plus 1 Quart per Total Flight Hour (whichever is higher)

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Minimum Oil to Arrive at Destination or Alternate

7 Quarts

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Maximum Takeoff EGT

950-965°C (3 minutes)
950°C (5 minutes) (Increases to 10 min if Engine Failure Occurs)

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Maximum Continuous EGT

925°C

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Maximum Start EGT

725°C

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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

Limits Flashcards

(63 cards)