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Limitations Flashcards

1
Q

How many required crew-members?

A

Captain and First Officer

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2
Q

Flight Manuevering Load Acceleration flaps up?

A

+2.5g to -1.0g

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3
Q

Flight manuevering load acceleration flaps down?

A

+2.0g to 0.0g

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4
Q

Runway slope for takeoff and landing?

A

+2.0% to -2.0%

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5
Q

Max takeoff tailwind component?

A

15 kts

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6
Q

Maximum landing tailwind component?

A

15 kts

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7
Q

Maximum dry runway wind limits takeoff and landings.
Maximum steady state wind velocity?
Maximum gust velocity?

A

50 kts maximum steady state
20 kts maximum gust
NOTE: Takeoff crosswinds limits are based upon the most adverse aircraft loading and assume an engine out RTO.

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8
Q

Maximum dry runway wind limits takeoff and landings. Notes about gust velocities?

A

Gust velocities are advisory; however, operations with a steady-state near the limits with higher gusts should be considered unacceptable. The captain may choose to further reduce these limits based on such factors as mels, gust velocity, runway width/length, braking action, wx phenomena, pilot currency and time in type of aircraft.

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9
Q

Takeoff crosswind chart:

A

See pic.

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10
Q

Type of aircraft operations?

A

Icing
Visual (VFR)
Instrument (IFR)
Extended over water

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11
Q

What is the max crosswind takeoff in the 700/800/900 based on braking action?

A 
Dry 700/40 kts; 800/33 kts; 900/33kts
Good 25kts (all)
Good to medium 22 kts (all)
Medium 20 kts (all) 
Medium to poor 15 kts (all)
Poor 13 kts (all)
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12
Q

What is the max landing crosswind in the 400/700?

A 
Good 40 kts
Good to medium 35 kts
Medium 25 kts
Medium to poor 17 kts
Poor 15 kts
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13
Q

What is the max crosswind for landing in the 800/900?

A 
Good 37 kts
Good to Medium 35 kts
Medium 25 kts
Medium to poor 17kts
Poor 15 kts

Note: Reduce crosswind guidelines by 5 kts on wet or contaminated runways whenever asymmetric reverse thrust is used.

Crosswind limits may be further restricted by emergency or abnormal procedures.

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14
Q

What is the max crosswind component for a sideslip only landing?

A

Sideslip only landings are not recommended with crosswind components in excess of 17 kts at Flaps 15; 20 kts at Flaps 30; or 23 kts at Flaps 40. This ensures adequate ground clearance and is based on maintaining adequate control margin.

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15
Q

What is the minimum ground time after landing on the NG if max quick turnaround weight limit is exceeded?

A

If max quick turnaround weight limit is exceeded on landing, wait at least 67 minutes after aircraft block-in, then check wheel thermal plugs to ensure they have not melted.

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16
Q

Takeoff crosswind note:

A

Gust velocities are advisory; however, operations with a steady-state component near the limits with higher gusts should be considered unacceptable. The Capt may choose to further reduce these limits based on such factors as MELs, gust velocity, rwy width/length, braking action, weather phenomena, pilot currency and time in type of aircraft.

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17
Q

Maximum flight operating latitudes (AFM/400)

A

73 * North and 60* South

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18
Q

Maximum flight operating latitudes (AFM/NG)

A

82North and 82 South, except between 80 west and 130 West longitude, when the maximum 70 North and between 120 East and 160 East, when the maximum is 60 South.

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19
Q

What is the max operating altitude for the NG?

A

41000 ft

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20
Q

What is the maximum takeoff and landing altitude?

A

8400 Ft

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21
Q

Minimum take-off and landing temperature?

A

Minus 54c

-54 degrees Celsius

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22
Q

Maximum takeoff and landing temperature?

A 
-1000 ft.   = 54c
Sea lvl.      = 54c
2000 ft.    = 50c
4000 ft.    = 46c
6000 ft.    = 42c
8000 ft.    = 38c
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23
Q

Minimum inflight temperature for (NG)

A 
Sea lvl = -62c
5000.  = -63c
15000 = -66c
25000 = -69c
35000 = -72c
41000 = -73c
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24
Q

Maximum airspeed

A

The maximum operating limit speed shall not be exceededin any flight regime

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25
Operating speeds maximum operating limit
Observe VMO/MMO and Gear/flap placards
26
Severe turbulent penetration speed (Ng)
280 kias/.76 mach
27
Maximum Flaps speed when extended via alternate system?
Do not exceed 230 Kts when flaps are extended by alternate (stand-by) system.
28
Maximum Flap speed for flaps 1-5 all models?
250 kts | *Do not exceed 230 kts when flaps are extended by alternate (stand-by) system
29
Flaps 10 max speeds
``` 700 = 210 800/900= 210 900ER = 205 ```
30
Flaps 15 max speeds
``` 700 = 195 800/900= 200 900ER = 200 ```
31
Flaps 25 max speeds
``` 700 = 170. 800/900= 190 900ER = 195 ```
32
Flaps 30 max speeds
700=165 kts 800/900= 175 kts 900ER=180 kts
33
Flaps 40 max speeds
``` 700= 156 kts 800/900= 162 kts 900ER= 170 kts ```
34
Landing gear max speeds
``` V lo (retract) 235 kts V lo (extend) 270 kts/.82M V le (extended) 320 kts/.82 M ```
35
Landing gear max speed V lo (retract)
235 kts
36
V lo (extend) landing gear max speed
270 kts/.82M
37
V le (extended) landing gear max speed
320 kts/.82M
38
700 Max weights
Max Taxi 155,000 Max takeoff 154,500 Max landing 129,200 Max ZFW 121,700
39
800 Max weights
Max Taxi 174,700 Max takeoff 174,200 Max landing 144,000 Max ZFW 136,000
40
900 Max weights
Max Taxi 174,700 Max takeoff 174,200 Max landing 146,300** Max ZFW 140,300*** ** Max landing weight at flaps 15 (900) 144,200 lbs ***Max zero fuel weight for 737-900W is 140,690 lbs
41
900ER max weights
``` Max Taxi 188,200 Max takeoff 187,700 Max landing 157,300** Max ZFW 147,300 Max landing weight at Flaps 15 (900ER) 154,200 lbs ```
42
Max plane weights
See chart section 2.020
43
Max takeoff and landing weights further limited
Takeoff and landing weights may be further limited by center of gravity, performance, and MEL/CDL considerations. These lower limits will be annotated on the Dispatch Release unless the limit is driven by actual aircraft loading. When limited by actually loading, the reduced limit weight will be indicated on the Load Closeout.
44
Configuration Deviation List (CDL)
When operation is scheduled with certain secondary airframe and engine parts missing, the aircraft must be operated in accordance with the basic aircraft limitations, and as amended by the CDL.
45
Static Dischargers
Aircraft with blended winglets installed: The aircraft is equipped with 14 static dischargers, a maximum of 2 may be missing
46
How many static dischargers? | And how many can be missing?
On aircraft with blended winglets installed: 14 static dischargers Max of 2 can be missing
47
PAX evacuation
On revenue flights, the escape slide retention bar must be installed during taxi, takeoff, and landing. (NG) Installation of handle covers on overwing exits must be verified prior to darture, whenever PAX are carried.
48
What must be installed for PAX evacuation?
On revenue flights, the escape slide retention bar, during taxi, takeoff, and landing. On NG handle covers on overwing exits must be verified prior to departure.
49
Photoluminescent (PL) Floor Track Lighting
PL Floor Emergency Lighting must be charged for 5 minutes prioe to PAX boarding on the first flight of the day. During this period, cabin activity is limited to minor aisle traffic of crew and personnel with overhead bins closed and all cabin lighting on bright.
50
How long do PL floor track lighting need to be on for 1st flight of day?
5 mins prior to PAX boarding with all cabin lights on bright and overhead bins closed
51
Flight Deck Door
An operational check of the Flight Deck Door Access System must be accomplished once each flight day. All normal requests to enter the Flight Deck must be in accordance with established FOM procedures; any use of a door access code is considered an emergency request. The automatic access time delay is set for 60 seconds. If the 28V DC Bus 2 or the door access system is unpowered, set the FDAS switch to the OFF position and use the deadbolt to lock the door. The deadbolt position allowing access with a key is to be used on the ground only.
52
How often do you need to do an operational check of the Flight Deck Door Access System?
Once each day
53
What happens if you use a door access code on flight deck door?
It is considered an emergency. The automatic access time delay is 60 seconds.
54
How can you lock the flight deck door if it is unpowered?
Set FDAS switch to OFF position and use the deadbolt to lock door.
55
When can the deadbolt to the flight deck door be accessed with a key?
On the ground only
56
Aircell Airborne Broadband System
(Placarded Aircraft) Use of Wi-Fi devices on the Flight Deck is prohibited when engines are operating for the purpose of flight.
57
On the freighter/combi what can you not do with the Main Cargo Door open?
Cannot be towed, taxied, or jacked
58
Who needs to verify the positive locking of the cargo door from the ground?
A Flight Crewmember
59
Main Cargo Door System A and B Warning light must be extinguished prior to what?
Pushback and taxi
60
Main Cargo Door loading lights must be extinguished prior to what?
Pushback or taxi
61
What are wind limitations for the Main Cargo Door with both actuators operational?
60 kts as long as aircraft is pointed into the wind (+/-5 degrees)
62
What is the wind speed limitation for the Main Cargo Door in the sail position (80-135 degrees) with both actuators opetational?
Wind gusts up to 30 kts in either direction
63
What is the max wind speed gusts with Main cargo door in canopy position (0-80degrees) with both actuators working?
Wind gusts up to 60 kts from the right (FO side) or 50 kts from the left side ( CAptain) of the fuselage
64
Main Cargo Door Wind Limitations with one actuator failed
Ensure that all personnel remain clear of door at all times. May be opened to canopy position (0-80 degrees) with one actuator failed in wind gusts up to 10 kts
65
Air
Maximum limits are red. Maximum System Safety Relief Differential Pressure (AFM) • (NG) 9.10 psi • (400) 8.65 psi Maximum allowable cabin pressure differential for takeoff and landing: 0.125 psi (236 ft below airport pressure altitude). (AFM)
66
What is the max system safety relief differential air pressure?
NG 9.10 psi
67
What is max allowable cabin pressure differential for takeoff and landing?
O.125 psi (236 ft below airport pressure altitude)
68
Bleed Air Duct Pressure
Minimum bleed air duct pressure on the ground with engine power at idle, air conditioning packs in AUTO, and engine anti-ice OFF is 15 PSI. Minimum bleed air duct pressure in flight with engine power at takeoff, climb, or cruise power is 18 PSI. Maximum bleed air duct pressure is 60 PSI. NOTE: Report any in-flight duct pressure differentials exceeding 20 PSI to Maintenance
69
What is Minimum bleed air duct pressure on the ground with engine power at idle, air conditioning packs in AUTO, and engine anti-ice OFF?
15 psi
70
What is minimum bleed air pressure in flight with engine power at takeoff, climb, or cruise power?
18 psi
71
What is max bleed air duct pressure?
60 psi
72
What is max in-flight duct pressure differentials before reporting to MX?
60 psi

AK Limitations (8 decks)

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