POH Ch 3 Bold Limitations (7/9) Revision 27 Flashcards
Max xwind TO and LD
27 Kts
Max xwind landing CAT II
15 Kts
Max headwind landing CAT II
16kts
Max tailwind for TO and LD (including gusts)
10 Kts
Max operating altitude 7/9
41,000 ft
Except in an emergency, takeoff or landing will not be attempted whenever peak wind value exceeds:
50 Kts
Max altitude for single pack operation 7/9
31,000 ft
Turbulence penetration speed
280 KIAS/ .75 M, whichever is lower
Max gear extension speed
220 KIAS
Max gear extended speed
220 KIAS
Max gear retraction speed
200 KIAS
Flaps 1 VFE 7/9
230 KIAS
Flaps 8 VFE
230 KIAS
Flaps 20 VFE
220 KIAS
Flaps 30 VFE
185 KIAS
Flaps 45 VFE
170 KIAS
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.
3 starts
1 hour
2 minutes
Bleed air extraction from the APU is not permitted above: (7/9)
25,000 ft
With the APU door not closed or the door position is unknown: (7/9)
Airplane must be limited to 220 KIAS or the APU must remain in operation.
To protect the flight compartment CRT displays, the maximum permissible time for ground operations with DC power is only:
5 minutes
During all starts, do not exceed ____ for ____ after start, or until all operating indications are in the normal range, whichever is longer.
75% N1
2 minutes
Operate Engines at or near idle for ___ prior to shutdown.
2 minutes
Takeoff power oil pressure
45 PSI minimum
After cold start, engine must ____ until oil pressure returns to normal range
Remain at idle
Continuous Engine Ignition must be used during the following:
- 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.
7/9 ground only starter cranking limits
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
During landing, maximum reverse thrust is prohibited below ____, and reverse idle should be achieved by ___.
75 KIAS
60 KIAS
(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
No limitations- TOGA thrust may be applied before brakes released.
(Engine operating limits due to wind direction 7/9)
> 30° in either direction of the airplane nose- between 5 and 30 Kts wind speed
Apply maximum of 75% N1 before brake release, then TOGA thrust.
(Engine operating limits due to wind direction 7/9)
>30° in either direction of the airplane nose- > 30 Kts wind speed
Apply maximum of idle/ taxi thrust before brake release, then TOGA thrust.
(7/9) if Static/Standing takeoff data is generated and wind limits prevent a Static/standing takeoff:
A.) winds must be entered in ACARS
-OR-
B.) for Aircraft with ACARS INOP, dispatch must manually insert winds into TLR data.
Minimum altitude for flight spoiler deployment
1,000 ft AGL
To ensure adequate maneuver margins, flight spoilers must not be extended inflight at air speeds below the recommended reference speed plus ____
17 KIAS
(7/9) max fuel imbalance
- takeoff
- All other phases of flight
- 300 lbs
- 800 lbs
Takeoff with fuel load in excess of ____ in the center tank is not permitted unless each wing tank is above ___
500 lbs
4,400 lbs
Powered cross flow and gravity cross flow must be ___
Off for takeoff
(Operating in icing conditions) TAXI condition: Temperature: IAS: Anti Ice:
- Ground contamination or visible moisture.
- OAT 10° C or Below
- N/A
- Cowl
(Operating in icing conditions) TAKEOFF condition: Temperature: IAS: Anti Ice:
- ground contamination or visible moisture
- OAT 10°C or Below- Cowl.
- OAT 5°C or below- Wing and Cowl
(Operating in icing conditions) IN FLIGHT condition: Temperature: IAS: Anti Ice:
- Visible Moisture
- From TAT 10°C to SAT -39° C
- IAS > or = 230: Cowl
- IAS <230: Wing and Cowl
(Operating in icing conditions) ICE ANNUNCIATED IN FLIGHT condition: Temperature: IAS: Anti Ice:
- On
- N/A
- N/A
- Wing and Cowl
Ground Contamination definition
Runways, ramps, or taxiways with surface snow, ice, slush, or standing water.
Visible Moisture definition
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).
If visible moisture is present below ____ with OAT ___ activate cowl anti ice for TO. If ___ activate both cowl and wing anti ice for TO.
- 400 ft AGL
- OAT 10°C
- OAT 5°C
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.
10°C (50°F)
-40°C (-40°F)
Do not hold in icing conditions with the _________.
Slats and/or flaps extended.
Taxi lights must be switched to OFF whenever the airplane is stationary in excess of ____.
10 minutes.
Minimum brake cooling time is ____, and all BTMS indicators must be _____.
15 minutes
- green and not increasing.
CAT II approaches are prohibited when the braking action is reported as less than ____.
Medium
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 ____.
- 600 ft AGL
- 400 ft AGL
- 80 ft AGL, with glide path exceptions (see POH 3.13.1)
- 110 ft AGL
Use of _______ with the flight director or autopilot coupled during approach is not permitted.
SPEED MODE (DES or IAS)
Use of ____ with the flight director or autopilot coupled during the climb and approach phases of flight is not permitted.
VNAV
Max Taxi and Ramp weight- 700
75,250 lbs
Max Taxi and Ramp weight- 900
85,000 lbs
Max TO weight- 700
75,000 lbs
Max TO weight- 900
84,500 lbs
Max landing weight- 700
67,000 lbs
Max landing weight- 900
75,100 lbs
Max ZFW- 700
62,300 lbs
Max ZFW- 900
70,750 lbs
