107 Aircraft Limitations Flashcards

1
Q

Basic Operating Weight (BOW)

A

104,500lbs

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2
Q

Maximum Zero Fuel Weight (MZFW)

A

136,000 lbs
*May be reduced w/ abnormal fuel distribution

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3
Q

Maximum Landing Weight w/ 40 degree Flaps

A

142,500 lbs

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4
Q

Maximum Landing Weight w/ 30 degree flaps

A

154,500 lbs

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5
Q

Maximum Takeoff Weight (Brake Release)

A

172,700 lbs
* no matter what pressure altitude

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6
Q

Maximum Ramp (Taxi) Weight

A

173,000 lbs

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7
Q

Maximum Pressure Altitude

A

8,400 ft

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8
Q

Minimum Pressure Altitude:

A

None; however if PA < -1,000 us performance data for -1,000

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9
Q

If PA = -1,000 to 2,500 ft then …

A

-54 C / -65 F
49 C / 120 F

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10
Q

If PA = 8,400 ft, then …

A

-54 C / -65F
38 C / 100F

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11
Q

Cross wind limitations

A

29kts max = takeoff
29kts max = CAT I
10kts max = CAT II

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12
Q

Max standing water, Slush (SLR), or Wet Snow (WSR):

A

Takeoff = 1/2 inch
Landing = 1 inch

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13
Q

Maximum Dry Snow (usually OAT < - 1 C)

A

Takeoff = 4 inches
Landing = 6 Inches

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14
Q

Fuel Requirements: Reserves

A

Domestic:
45 mins (normal cruise) = 6,800lbs

Flag:
30 min holding (1500’) = 5,800lbs
10% en route = 8300lbs / hr

Flag (no authorized alt.):
2 hrs @ normal cruise speed/fuel flow = 18,000’s (9000 lbs / hr)

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15
Q

Fuel Requirements: Additional

A

Missed approach fuel = 1,200 lbs (dispatch without an alternate)

Taxi fuel (12 min average) at 50lbs/min = 600lbs

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16
Q

Thrust Limitations

A

Takeoff Thrust (5 mins) = 14,000lbs
Max continuous Thrust = 12,600lbs
Max cruise thrust = 11,000lbs

17
Q

Fuel loading rules

A
  1. Distribute fuel equally between all 3 tanks.
  2. 1 or 3 shall not exceed quantity in tank 2 by more than 2000lbs
  3. Fuel in tanks 1 and 3 must not differ by more than 1000lbs
18
Q

When operating at the maximum zero fuel weight…

A

The fuel weight in each tank must be essentially equal unless tanks 1 and 3 are full

19
Q

When operating at less than maximum zero fuel weight with 1 and 3 not full…

A

Fuel in tank 2 must not exceed the fuel weight in 1 or 3 by more than the difference between the Max ZFW and the actual ZFW for each flight