7ER Other Important Limitations Flashcards

1
Q

What is the max runway slope allowed?

A

+/-2%

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2
Q

What is the max takeoff and landing altitude for most of the fleet? 6815-6817?

A

8,400 feet pressure altitude
9,500 feet pressure altitude

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3
Q

Is HF radio operation allowed during refueling operations?

A

No

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4
Q

What is the 757-200 Max Landing Weight (MLW)?

A

198,000 Lbs

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5
Q

What is the 757-300 Max Landing Weight (MLW)?

A

224,000 Lbs

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6
Q

What is the 767-300 Max Landing Weight (MLW)?

A

320,000 Lbs

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7
Q

If main tanks are not full, center tank fuel on the 757-200/300 may not exceed what amount?

A

2,000 Lbs

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8
Q

If main tanks are not full, center tank fuel on the 767-300 may not exceed what amount?

A

22,000 Lbs, provided center tank weight, plus actual ZFW is less than MZFW, and CG limits are observed

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9
Q

If flying a 757 approved for landing above 8,400’ pressure altitude to an airport above 8,400’ pressure altitude, what autopilot limitation needs to be followed?

A

Do not use the autopilot below 100’ RA at airport pressure altitudes above 8,400’

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10
Q

Autoland is authorized for what flap settings only?

A

Flaps 25 or 30

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11
Q

Is an autoland approved above a ground speed of 165 knots?

A

No

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12
Q

When must CONT ignition be selected?

A

-When operating in severe turbulence*
-If moderate to heavy rain, hail or sleet is encountered

*Continuous ignition is automatically provided with the flap lever out of the “UP” position or in icing conditions when engine anti–ice is on.

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13
Q

What is the max EGT for engine start on the ground for the 757?

A

545°C at Zero seconds, decreasing linearly to 485°C at 30 seconds and thereafter. (Decrease of 2 degrees per second)

-If EGT surpasses 485°C but not 545°C, shutdown is not required. Make a logbook entry and contact maintenance prior to dispatch for further guidance.

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14
Q

For the 757, during takeoff or climb phase, EGT may increase to what temperature for 5 seconds?

A

660°C

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15
Q

For the 757, during takeoff, the EGT may increase to what temperature for 5 minutes? What about ships 6801-6823?

A

-645°C
-Ships 6801-6823: 645°C for 10 minutes in the event of loss of thrust on one engine during takeoff

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16
Q

What is the max EGT for takeoff for the 767 with P&W engines? How long is this temperature allowed?

A

-650°C
-5 minutes

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17
Q

What is the max EGT for takeoff for the 767 with GE engines? How long is this temperature allowed? Single Engine?

A

-960°C for 5 minutes
-Single Engine: 10 minutes

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18
Q

What are the engine starter duty cycle limits?

A

• Continuous for 5 minutes, followed by cool down of 30 seconds for each minute of operation
• After 2 consecutive 5-minute cycles, cool starter for 10 mins prior to each subsequent starter duty cycle

19
Q

What is the APU starter duty cycle maximum?

A

Max of 3 consecutive starts or attempts within a 60 minute period

20
Q

APU bleed air is available up to what altitude?

A

Approximately 17,000’

21
Q

On the ground, the standby altimeter must be within how many feet of the Captain’s AND First Officer’s altimeters?

A

+/-75 feet

22
Q

What is the maximum allowable in-flight difference between the Captain’s and First Officer’s altitude displays for RVSM operation?

23
Q

What is the maximum allowable on-the-ground difference between the Captain’s OR First Officer’s altitude displays AND Field Elevation for RVSM operation?

24
Q

What is the maximum allowable on-the-ground difference between the Captain’s and First Officer’s altitude displays for RVSM operation on the 757 at sea level, 5,000’, and 10,000’?

A

-S.L.: 25 Feet
-5,000’: 35 feet
-10,000’: 40 feet

25
What is the maximum allowable on-the-ground difference between the Captain’s and First Officer’s altitude displays for RVSM operation on the 767-300 at sea level, 5,000’, and 10,000’?
-S.L.: 40 Feet -5,000’: 45 feet -10,000’: 50 feet
26
Is intentional dry running of a center tank fuel pump (CTR L FUEL PUMP or CTR R FUEL PUMP message displayed on EICAS) allowed?
No, it is prohibited
27
Do we have an uncompensated Baro-VNAV system?
Yes
28
What altitude is set in the Landing Altitude Selector during preflight if the landing airport elevation is between 8,000’ and 9,500’?
Set 5,000’ during the preflight flow
29
What altitude is set in the Landing Altitude Selector during the descent procedure (Top Of Descent) if the landing airport elevation is between 8,000’ and 9,500’?
Set landing field elevation
30
What are the quick reference landing lengths? Is a 15% safety margin included?
757-200: 7,000’ 757-300: 8,500’ 767-300: 8,000’ *Yes, this includes the 15% safety margin for wet runways. Other assumptions must be met to use these numbers
31
Which 75/76 versions ARE APPROVED to use DRY takeoff data when water/slush/wet snow is less than 0.14 inches on grooved or porous friction overlay runways?
757-200 and 767-300ER
32
Which 75/76 versions ARE NOT APPROVED to use DRY takeoff data when water/slush/wet snow is less than 0.14 inches on grooved or porous friction overlay runways?
757-300
33
What is the max wing tank capacity of the 757?
14,500 Lbs or 14,900 Lbs depending on ship number. Check differences section.
34
What is the max wing tank capacity of the 767-300?
41,000 Lbs
35
What is the minimum additive to Vref?
5 Knots
36
What is the maximum additive for wind to Vref?
15 Knots
37
How much additive do we use for landing on runway 27 if the winds are 360@10 gust 20?
Half the headwind, all of the gust: Headwind = 0 Gust = 10 So add 10 knots to Vref
38
Do we maintain steady headwind additive to touchdown?
No
39
Do we maintain gust additive to touchdown?
Yes
40
What is the minimum fuel required in the main tanks in order to jettison center tank fuel?
10,300 Lbs
41
What can we do for takeoff when APU is in the condition remark section on the WDR?
Either a PACKS OFF takeoff OR APU to Pack takeoff
42
What must be done if POF is listed in the remark section on the WDR?
Must do a PACK OFF takeoff
43
If landing with gusty winds, what do you input on the LPR for knots above Vref?
You add only the gust factor for the LPR because it is maintained to touchdown