Limitations Flashcards
Takeoff tailwind limit
15 knots
Landing tailwind limit
10 knots
- except 15 knots at SJO and San Pedro Sula
Severe turbulent air penetration speed
280 knots / .76 Mach
Max altitude with flaps extended
20,000 feet
Speed brakes
Do not deploy in flight at altitudes less than 1,000 ft RA
3RA-3VM In flight, do not extend Speedbrake lever beyond ARMED
detent with Flaps 40 selected
Minimum altitude for autopilot
engagement for takeoff
(Minimum to engage)
400’ AGL
Minimum altitude for autopilot
engagement during approach
(Minimum to disengage)
50’ AGL
APU bleed air + electrical load max altitude in flight
10,000 feet MSL
APU bleed air max altitude
17,000 feet MSL
APU electrical load max altitude
41,000 feet MSL
Weather Radar
Avoid operation in a hangar
HF radio
Do not operate during refueling operations
Crosswind takeoff
3AA-3PX Dry …………………………………………………………………………….. 33 kts*
3RA-3VM Dry………………………………………………………………………………32 kts*
Wet …………………………………………………………………………………………….. 25 kts
Standing Water/Slush………………………………………………………………….15 kts
Snow (Wet and Dry) …………………………………………………………………… 25 kts
Compacted Snow ………………………………………………………………………. 20 kts
Ice………………………………………………………………………………………………….15 kts
Crosswind landing
3AA-3PX Dry, Good, Good to Medium (RCC 6, 5, 4)………………..33 kts*
3RA-3VM Dry, Good, Good to Medium (RCC 6, 5, 4)……………….32 kts*
Medium (RCC 3) ……………………………………………………………………….. 25 kts
Medium to Poor (RCC 2)……………………………………………………………..17 kts
Poor (RCC 1) ………………………………………………………………………………. 15 kts
Maximum Cabin Differential Pressure (system relief)
9.1 psi
Unpressurized flight
Maximum altitude for unpressurized flight, following an in flight depressurization, is 14,000 feet. This altitude may be exceeded when terrain clearance requirements dictate.
Maximum altitude when aircraft is dispatched for unpressurized flight is 10,000 feet.
Engine anti ice use
Engine anti-ice must be on during all ground and flight operations when icing conditions exist or are anticipated, except during climb and cruise when the temperature is below -40°C SAT. Engine anti-ice must be on prior to and during descent in all Icing Conditions, including temperatures below -40°C SAT.
Minimum oil quantity for engine start
3AA-3PX 12 quarts.
3RA-3VM 14 quarts.
Fuel imbalance
fuel imbalance must not exceed 1000 lbs for taxi, takeoff, flight or landing.
Fuel loading
Main tanks 1 and 2 must be full if center tank contains more than 1000 lbs.
Cat III WX
300 600/400/300
TDZ +1
Takeoff alternate distance
330 nm
HUD low visibility takeoff
<500 RVR
(2 of 3) • Touchdown: 300 RVR (75m) • Mid-field: 300 RVR (75m) • Roll-out: 300 RVR (75m)
PM “centerline”
FO takeoff/ landing mins
1600 takeoff
1800 landing
When must O2 be used
Smoke & fumes
Halon extinguisher used
Depressurization
Minimum RNP
0.10
Drift down procedure
— Disengage the autothrottle
— Thrust lever operating engine - Set to MCT
— Maximum engine out altitude - Set in MCP altitude window
— Engine out target speed* - Set in MCP IAS/MACH window
— LVL CHG - Select after aircraft decelerates to engine out target speed
PM
— Notify ATC and request altimeter setting
— Refer to QRH - “One Engine driftdown and cruise”
Disengage APP mode
- TO/GA
- Disengage autopilot AND turn off both Flight Directors
- Retune BOTH VHF navs to non ILS freq
Max holding speeds
6,000 feet or less 200
Above 6,000 to 14,000 feet 230
Above 14,000 feet 265
Maximum operating altitude
41,000 feet
Maximum Takeoff and Landing Altitude
8,400 feet
Maximum Landing Weight
NG 146,300
MAX 152,800
If the elevation of the destination airport is over_____, set the LAND ALT window to ______.
6000 feet.
Time limit between turning on APU and using it to run the AC packs
2 minutes
Time limit for turning battery off after turning off the APU
3 minutes
Wingspan
117’ 5”
RFD (Ready For Departure) conditions
Delayed engine start due to ATC ACARS entry: RFD.
Ramp congestion due to aircraft or vehicular traffic ACARS entry: RAMP DELAY or Misc 59.
De/anti icing location congestion ACARS entry: DE-ICE DELAY or Misc 59.
RVSM Altimeter Tolerances
In Flight: 200 feet
On Ground: 50 feet (elev 0 to 5000 feet)
60 feet (elev >5000 feet)
Max difference between CA or FO altimeter & elev: 75 feet
(The standby altimeter does not meet altimeter accuracy requirements of RVSM)
Engine failure on takeoff, what can you do passing 400’?
- Call ATC
- Start the APU
- Analyze the engine
Single engine go around littanies
400’: HDG SEL, APU, ATC (MAYDAY)
1000’: LVL CHANGE, Set speed
Flaps up: MCT, Checklist
