Limitations

Question 1

Takeoff tailwind limit

Answer 1

15 knots

Question 2

Landing tailwind limit

Answer 2

10 knots

• except 15 knots at SJO and San Pedro Sula

Question 3

Severe turbulent air penetration speed

Answer 3

280 knots / .76 Mach

Question 4

Max altitude with flaps extended

Answer 4

20,000 feet

Question 5

Speed brakes

Answer 5

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

Question 6

Minimum altitude for autopilot
engagement for takeoff
(Minimum to engage)

Answer 6

400’ AGL

Question 7

Minimum altitude for autopilot
engagement during approach
(Minimum to disengage)

Answer 7

50’ AGL

Question 8

APU bleed air + electrical load max altitude in flight

Answer 8

10,000 feet MSL

Question 9

APU bleed air max altitude

Answer 9

17,000 feet MSL

Question 10

APU electrical load max altitude

Answer 10

41,000 feet MSL

Question 11

Weather Radar

Answer 11

Avoid operation in a hangar

Question 12

HF radio

Answer 12

Do not operate during refueling operations

Question 13

Crosswind takeoff

Answer 13

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

Question 14

Crosswind landing

Answer 14

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

Question 15

Maximum Cabin Differential Pressure (system relief)

Answer 15

9.1 psi

Question 16

Unpressurized flight

Answer 16

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.

Question 17

Engine anti ice use

Answer 17

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.

Question 18

Minimum oil quantity for engine start

Answer 18

3AA-3PX 12 quarts.

3RA-3VM 14 quarts.

Question 19

Fuel imbalance

Answer 19

fuel imbalance must not exceed 1000 lbs for taxi, takeoff, flight or landing.

Question 20

Fuel loading

Answer 20

Main tanks 1 and 2 must be full if center tank contains more than 1000 lbs.

Question 21

Cat III WX

Answer 21

300 600/400/300

TDZ +1

Question 22

Takeoff alternate distance

Answer 22

330 nm

Question 23

HUD low visibility takeoff

Answer 23

<500 RVR

(2 of 3) • Touchdown: 300 RVR (75m) • Mid-field: 300 RVR (75m) • Roll-out: 300 RVR (75m)

PM “centerline”

Question 24

FO takeoff/ landing mins

Answer 24

1600 takeoff

1800 landing

Question 25

When must O2 be used

Answer 25

Smoke & fumes Halon extinguisher used Depressurization

Question 26

Minimum RNP

Answer 26

0.10

Question 27

Drift down procedure

Answer 27

— 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”

Question 28

Disengage APP mode

Answer 28

- TO/GA - Disengage autopilot AND turn off both Flight Directors - Retune BOTH VHF navs to non ILS freq

Question 29

Max holding speeds

Answer 29

6,000 feet or less 200 Above 6,000 to 14,000 feet 230 Above 14,000 feet 265

Question 30

Maximum operating altitude

Answer 30

41,000 feet

Question 31

Maximum Takeoff and Landing Altitude

Answer 31

8,400 feet

Question 32

Maximum Landing Weight

Answer 32

NG 146,300 | MAX 152,800

Question 33

If the elevation of the destination airport is over_____, set the LAND ALT window to ______.

Answer 33

6000 feet.

Question 34

Time limit between turning on APU and using it to run the AC packs

Answer 34

2 minutes

Question 35

Time limit for turning battery off after turning off the APU

Answer 35

3 minutes

Question 36

Wingspan

Answer 36

117’ 5”

Question 37

RFD (Ready For Departure) conditions

Answer 37

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.

Question 38

RVSM Altimeter Tolerances

Answer 38

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)

Question 39

Engine failure on takeoff, what can you do passing 400’?

Answer 39

- Call ATC - Start the APU - Analyze the engine

Question 40

Single engine go around littanies

Answer 40

400’: HDG SEL, APU, ATC (MAYDAY) 1000’: LVL CHANGE, Set speed Flaps up: MCT, Checklist