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Boeing 737 > Limitations > Flashcards

Limitations Flashcards

1
Q

Maximum Operating Altitude

A

41,000 Feet

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2
Q

Minimum Takeoff and Landing Temperature

A

-55 Degrees Celsius

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3
Q

Maximum Takeoff and Landing Temperature

A

55 Degrees Celsius

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4
Q

Maximum Takeoff and Landing Pressure Altitude

A

8,400 Feet

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5
Q

Runway Slope

A

+/- 2%

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6
Q

VMO/MMO

A

340 Knots/0.82 Mach

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7
Q

Severe Turbulence Penetration Speed

A

280 Knots/0.76 Mach

(Whichever is Less)

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8
Q

Maximum Tailwind

A

Takeoff = 15 Knots

Landing = 10 Knots

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9
Q

Maximum Crosswind

A

Takeoff = 33 Knots (3AA-3PX), 32 Knots (3RA-3VM)

Landing = 33 Knots (3AA-3PX), 32 Knots (3RA-3VM)

3AA-3VM

Flaps 15 - 15 Knots or Less

Flaps 30 - 18 Knots or Less

Flaps 40 - 21 Knots or Less

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10
Q

Manuevering Speed

A

VA is defined for evaluating aircraft structural design. At or below this speed, Boeing aircraft are capable of sustaining a single input to any set of control surfaces to their maximum available authority. These control surface inputs are to be in one axis and do not include control input reversal or oscillatory inputs.

Even at speeds below VA, transport category aircraft should be flown judicioulsy, avoaiding full or abrupt control movements.

Turbulence Penetration Speed can be used as a rough approximation for VA

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11
Q

NG Maximum Weights

(3AA-3PX)

A

Taxi: 174,700

Takeoff: 174,200

Landing: 144,000

Zero Fuel: 136,000

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12
Q

MAX 8 Maximum Weights

(3RA-3VM)

A

Taxi: 181,700

Takeoff: 181,200

Landing: 152,800

Zero Fuel: 145,400

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13
Q

Evacuation Systems

A

Any time passengers are on board, prior to aicraft movement, at least one floor level exit must be open or armed.

On revenue flights, the escape slide retention bar (girt bar) must be inserted in the brackets on all doors during taxi, takeoff, and landing.

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14
Q

Overwater Operations

A

On aircraft with 160 seats: limited to 168 seated passengers for overwater flights.

The aircraft has 169 seats (160 PAX, 2 Pilots, 1W, and 6 FAs). Life raft seating capacity is 168.

On aircraft with 172 seats: not limited for overwater flights.

The aircraft has 181 seats (172 PAX, 2 Pilots, 1W, 6 FAs). Life raft seating capacity is 193.

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15
Q

Flight Deck Door and Flight Deck Access System

A

Accomplish Pre-Flight Check (Prior to First Flight of the Day)

Use of the Access Code is considered an Emergency Access Request

If DC Bus 2 is unpowered, POWER CUTOFF Switch = OFF and deadbold = LOCKED KEY INOP

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16
Q

Air Conditioning Packs

A

Do NOT operate the packs in HIGH for takeoff, approach, or landing

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17
Q

Maximum Cabin Differential Pressure

A

9.1 PSI

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18
Q

Maximum Unpressurized Altitude

A

After an Inflight Depressurization: 14,000 Feet (can be exceeded for terrain)

Dispatch: 10,000 Feet

19
Q

Icing Condition Definition

A

OAT on the ground and for takeoff, TAT inflight

10 Degrees Celsius/50 Degrees Fahrenheit or below and:

Visible Moisture in any form is present (clouds, fog with visibility of one mile or less, rain, snow, sleet, and ice crystals)

OR

When operating on ramps, taxiways, or runways where surface snow, ice, standing water, or slush may be ingested by the engines or freeze on the engines or nacelles

20
Q

Icing Condition Ignition Use

A

Engine Ignition must be on when operating in icing conditions

21
Q

Icing Caution

A

Do not rely on airframe visual icing cues to turn engine anti-ice on. Delaying the use of engine anti-ice until ice buildup is visible from the flightdeck may result in severe engine damage.

22
Q

Engine Anti-Ice

A

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 temperatue is below -40 Degrees Celsius SAT. Engine anti-ice must be on prior to and during descent in all Icing Conditions, including temperatures below -40 Degrees Celsius SAT.

23
Q

Wing Anti-Ice

A

Do not use wing anti-ice as a substitute for ground de-icing/anti-icing and inpection procedures.

Do not operate wing anti-ice on the ground when OAT is above 10 Degrees Celsius (50 Degrees Fahrenheit).

24
Q

Autopilot Limitations

A

NA from Takeoff to 400 Feet AGL

Single Channel Approach to 50 Feet AGL

No Aileron Trim while Engaged

No Dual Channel for Approach

LVL CHG on Final Approach below 1000 Feet AFE

25
Q

HF

A

Deselect the other HF radio on all panels to prevent interference

Do Not Use during Refueling Operations

26
Q

Broadband Antenna RF

A

Must be off during de-icing, taxiing under skybridge, or in a hangar

27
Q

Engine Ignition

A

Takeoff: AUTO or CONT

Landing: AUTO or CONT

Anti-Ice: AUTO or CONT

Heavy Rain: CONT

28
Q

EEC Alternate Mode

A

Both EECs must be in Alternate Mode

3AA-3PX: 26K max Takeoff Thrust must be used (27K Max, if planned)

3RA-3VM: TO takeoff thrust must be used

Do not use FMC takeoff N1 or QRH V-Speeds

Autothrottle for Takeoff is NA

29
Q

27K Bump

A

Authorized for use by Dispatch and be only be selected if it is specified on the Load Agent generated TPS

30
Q

Reverse Thrust

A

Intentional selection of reverse thrust in flight is prohibited

31
Q

APU Bleed and Electrical Load

A

Bleed and Electrical: 10,000 Feet

Bleed: 17,000 Feet

Electrical: 41,000 Feet

32
Q

APU Bleed Valve

A

Closed When:

Ground Air is connected and Isolation Valve is Open

Engine #1 Bleed Valve is Open

Isolation Valve and Engine #2 Bleed Valves are Open

Bleed Valve may be open during engine start, but avoid engine power above idle

After 3 start attempts, 15 minute cooling period is required

33
Q

Anti-Skid

A

Operation with assumed temperature reduced takeoff thrust is NA with anti-skid INOP

34
Q

Oil Quantity

A

3AA-3PX (NG): 12 Quarts

3RA-3VM (MAX 8): 17 Quarts

35
Q

Flight Controls

A

Maximum Altitude with Flaps Extended: 20,000 Feet

Holding in Icing Conditions with Flaps Extended is NA

No Speed Brakes below 1000 Feet

Do not extend the Speed Brake Lever beyond the FLIGHT detent in flight

Avoid rapid and large alternating control inputs, including speeds below VA

36
Q

Alternate Flaps

A

Allow 15 seconds after releasing the ALTERNATE FLAPS position switch before moving the switch again to avoid damage to the motor clutch

After a complete extend/retract cycle, allow 5 minutes cooling before attempting another extension

37
Q

HUD

A

Use of the HUD with an INOP RA #1 is NA

38
Q

RVSM Altitude

A

Difference between CA and FO Altitude Displays:

In Flight: 200 Feet

Ground: 50 Feet (SL to 5000 Feet)

60 Feet (5001 to 10,000 Feet)

Difference between CA and FO Altitude Displays to Field Elevation: 75 Feet

39
Q

Air Data Inertial Reference Unit (ADIRU)

A

Alignment must not be attempted at LAT > 78 Degrees 15 Minutes

40
Q

Fuel

A

Maximum Tank Temperature: 49 Degrees Celsius

Minimum Tank Temperature: -43 Degrees Celsisus or 3 Degrees Celsius aboe the fuel freezing point temperature (whichever is higher)

Intentional running of a center tank fuel pump (low pressure light) is prohibited

41
Q

Fuel Balance

A

Must be scheduled to be balanced between Tanks 1 and 2

Random Imbalance must not exeed 1000 Pounds for Taxi, Takeoff, Flight, or Landing

Tanks 1 and 2 must be full if center take contains more than 1000 Pounds

Ballast Fuel is NA

42
Q

EGPWS

A

Do Not use Terrain Display for NAV

Authorized to Deviate from Clearance to comply with EGPWS Warning

Enhanced Function should be inhibited when the aircraft is less than 15NM from:

Runways not incorporated into the Database

Approaches that have been identified as producing false alarms

43
Q

Weather Radar

A

Do Not Operate in a hangar or within 50 feet of fueling operations, fuel spills, or people

Boeing 737 (1 decks)

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