POH Ch 3 Bold Limitations (7/9) Revision 27

Question 1

Max xwind TO and LD

Answer 1

27 Kts

Question 2

Max xwind landing CAT II

Answer 2

15 Kts

Question 3

Max headwind landing CAT II

Answer 3

16kts

Question 4

Max tailwind for TO and LD (including gusts)

Answer 4

10 Kts

Question 5

Max operating altitude 7/9

Answer 5

41,000 ft

Question 6

Except in an emergency, takeoff or landing will not be attempted whenever peak wind value exceeds:

Answer 6

50 Kts

Question 7

Max altitude for single pack operation 7/9

Answer 7

31,000 ft

Question 8

Turbulence penetration speed

Answer 8

280 KIAS/ .75 M, whichever is lower

Question 9

Max gear extension speed

Answer 9

220 KIAS

Question 10

Max gear extended speed

Answer 10

220 KIAS

Question 11

Max gear retraction speed

Answer 11

200 KIAS

Question 12

Flaps 1 VFE 7/9

Answer 12

230 KIAS

Question 13

Flaps 8 VFE

Answer 13

230 KIAS

Question 14

Flaps 20 VFE

Answer 14

220 KIAS

Question 15

Flaps 30 VFE

Answer 15

185 KIAS

Question 16

Flaps 45 VFE

Answer 16

170 KIAS

Question 17

7/9
The APU starter motor duty cycle is limited to not more than ____ starts/start attempts in ___ hour with a __ minute delay between cranking attempts.

Answer 17

3 starts
1 hour
2 minutes

Question 18

Bleed air extraction from the APU is not permitted above: (7/9)

Answer 18

25,000 ft

Question 19

With the APU door not closed or the door position is unknown: (7/9)

Answer 19

Airplane must be limited to 220 KIAS or the APU must remain in operation.

Question 20

To protect the flight compartment CRT displays, the maximum permissible time for ground operations with DC power is only:

Answer 20

5 minutes

Question 21

During all starts, do not exceed ____ for ____ after start, or until all operating indications are in the normal range, whichever is longer.

Answer 21

75% N1

2 minutes

Question 22

Operate Engines at or near idle for ___ prior to shutdown.

Answer 22

2 minutes

Question 23

Takeoff power oil pressure

Answer 23

45 PSI minimum

Question 24

After cold start, engine must ____ until oil pressure returns to normal range

Answer 24

Remain at idle

Question 25

Continuous Engine Ignition must be used during the following:

Answer 25

- takeoff and landing on contaminated runways. - takeoff with high crosswind components (15 Kts or greater). - Flight through moderate or heavier intensity rain. - Flight through moderate or easier intensity turbulence. - Flight in the vicinity of Thunderstorms.

Question 26

7/9 ground only starter cranking limits

Answer 26

Start 1- 90 sec max on followed by 10 sec off Start 2- 90 sec max on followed by 10 sec off Start 3- 90 sec max on followed by 5 min off

Question 27

During landing, maximum reverse thrust is prohibited below ____, and reverse idle should be achieved by ___.

Answer 27

75 KIAS | 60 KIAS

Question 28

(Engine operating limits due to wind direction 7/9) Within 30° on either direction of the airplane nose- no wind speed limit -OR- >30° in either direction of the airplane nose- <5 kts wind speed

Answer 28

No limitations- TOGA thrust may be applied before brakes released.

Question 29

(Engine operating limits due to wind direction 7/9) | > 30° in either direction of the airplane nose- between 5 and 30 Kts wind speed

Answer 29

Apply maximum of 75% N1 before brake release, then TOGA thrust.

Question 30

(Engine operating limits due to wind direction 7/9) | >30° in either direction of the airplane nose- > 30 Kts wind speed

Answer 30

Apply maximum of idle/ taxi thrust before brake release, then TOGA thrust.

Question 31

(7/9) if Static/Standing takeoff data is generated and wind limits prevent a Static/standing takeoff:

Answer 31

A.) winds must be entered in ACARS -OR- B.) for Aircraft with ACARS INOP, dispatch must manually insert winds into TLR data.

Question 32

Minimum altitude for flight spoiler deployment

Answer 32

1,000 ft AGL

Question 33

To ensure adequate maneuver margins, flight spoilers must not be extended inflight at air speeds below the recommended reference speed plus ____

Answer 33

17 KIAS

Question 34

(7/9) max fuel imbalance - takeoff - All other phases of flight

Answer 34

- 300 lbs | - 800 lbs

Question 35

Takeoff with fuel load in excess of ____ in the center tank is not permitted unless each wing tank is above ___

Answer 35

500 lbs | 4,400 lbs

Question 36

Powered cross flow and gravity cross flow must be ___

Answer 36

Off for takeoff

Question 37

``` (Operating in icing conditions) TAXI condition: Temperature: IAS: Anti Ice: ```

Answer 37

- Ground contamination or visible moisture. - OAT 10° C or Below - N/A - Cowl

Question 38

``` (Operating in icing conditions) TAKEOFF condition: Temperature: IAS: Anti Ice: ```

Answer 38

- ground contamination or visible moisture * OAT 10°C or Below- Cowl. * OAT 5°C or below- Wing and Cowl

Question 39

``` (Operating in icing conditions) IN FLIGHT condition: Temperature: IAS: Anti Ice: ```

Answer 39

- Visible Moisture - From TAT 10°C to SAT -39° C * IAS > or = 230: Cowl * IAS <230: Wing and Cowl

Question 40

``` (Operating in icing conditions) ICE ANNUNCIATED IN FLIGHT condition: Temperature: IAS: Anti Ice: ```

Answer 40

- On - N/A - N/A - Wing and Cowl

Question 41

Ground Contamination definition

Answer 41

Runways, ramps, or taxiways with surface snow, ice, slush, or standing water.

Question 42

Visible Moisture definition

Answer 42

Visible moisture or precipitation in any form (such as fog with vis of 1 mile or less, mist, rain, snow, sleet, and ice crystals or clouds inflight).

Question 43

If visible moisture is present below ____ with OAT ___ activate cowl anti ice for TO. If ___ activate both cowl and wing anti ice for TO.

Answer 43

- 400 ft AGL - OAT 10°C - OAT 5°C

Question 44

Icing conditions exist in flight at a TAT of ____ or below, and visible moisture in any form is encountered (such as clouds, rain, snow, sleet, or ice crystals), except when the SAT is ____ or below.

Answer 44

10°C (50°F) | -40°C (-40°F)

Question 45

Do not hold in icing conditions with the _________.

Answer 45

Slats and/or flaps extended.

Question 46

Taxi lights must be switched to OFF whenever the airplane is stationary in excess of ____.

Answer 46

10 minutes.

Question 47

Minimum brake cooling time is ____, and all BTMS indicators must be _____.

Answer 47

15 minutes | - green and not increasing.

Question 48

CAT II approaches are prohibited when the braking action is reported as less than ____.

Answer 48

Medium

Question 49

Operation with the autopilot engaged is prohibited at altitudes below ____, except when performing the following: * for VIS and non precision approaches, minimum height for autopilot is ____. * for (PAR/ILS), the minimum height for autopilot use is _____. * (900) for PAR/ILS, one engine inop min height for autopilot is ____.

Answer 49

- 600 ft AGL - 400 ft AGL - 80 ft AGL, with glide path exceptions (see POH 3.13.1) - 110 ft AGL

Question 50

Use of _______ with the flight director or autopilot coupled during approach is not permitted.

Answer 50

SPEED MODE (DES or IAS)

Question 51

Use of ____ with the flight director or autopilot coupled during the climb and approach phases of flight is not permitted.

Answer 51

VNAV

Question 52

Max Taxi and Ramp weight- 700

Answer 52

75,250 lbs

Question 53

Max Taxi and Ramp weight- 900

Answer 53

85,000 lbs

Question 54

Max TO weight- 700

Answer 54

75,000 lbs

Question 55

Max TO weight- 900

Answer 55

84,500 lbs

Question 56

Max landing weight- 700

Answer 56

67,000 lbs

Question 57

Max landing weight- 900

Answer 57

75,100 lbs

Question 58

Max ZFW- 700

Answer 58

62,300 lbs

Question 59

Max ZFW- 900

Answer 59

70,750 lbs