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FedEx > ***767 Limits (FM 11) > Flashcards

***767 Limits (FM 11) Flashcards

1
Q

***Max Taxi Weight

A

409,000

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2
Q

***Max Take Off Weight

A

408,000

230,000 (757)

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3
Q

***Max Landing Weight

A

326,000

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4
Q

Max Single Engine Taxi Weight

A

300,000 lbs

320,000 lbs
FTM: pg 66/67

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5
Q

***Max Zero Fuel Weight

A

309,000

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6
Q

Landing CG Range

A

7-37 (22 center)

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7
Q

***Normal Taxi Speed

A

20 knots
No longer a limitation

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8
Q

***Long Strait Taxi Speed

A

30 knots
No longer a limitation

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9
Q

***Turns On A Dry Surface (other than high speed turnoffs)

A

10 knots

Turns 30° or more
No longer a limitation

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10
Q

***Differential Breaking While Turning

A

Avoid

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11
Q

Maximum Operating Speeds

A

FL290 / 338 knots / 0.86 Mach

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12
Q

***Severe Turbulent Air Penetration Speeds

A

290 knots / 0.78 Mach

Whichever is lower

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13
Q

Flap Extended Speeds

A 
1 - 250 (230)
5 - 230 (210)
15 - 210 (190)
20 - 210 (190)
25 - 180 
30 - 170
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14
Q

Max Landing Gear Ops Speeds

A

Placarded

Operating speeds - 270 / 0.82
Extended speeds - 270 / 0.82

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15
Q

***Max Tailwind

A

T/O, Landing, Autoland
15 knots

1 or 2 engines

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16
Q

***Max Autoland Headwind

A

25 knots

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17
Q

***Max Crosswind, RCC 6

A

T/O: 30 knots
Landing: 30 knots

* Sideslip only (zero crab) landings are not recommended with crosswind components in excess 26knots (767)*

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18
Q

***Max Crosswind, RCC 5 / Good

A

T/O: 25 knots
Landing: 30 knots

* Sideslip only (zero crab) landings are not recommended with crosswind components in excess 26knots (767)*

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19
Q

***Max Crosswind, RCC 4 / Good-Medium

A

T/O: 20 knots
Landing: 30 knots

* Sideslip only (zero crab) landings are not recommended with crosswind components in excess 26knots (767)*

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20
Q

***Max Crosswind, RCC 3 / Medium

A

T/O: 17 knots

Landing: 25 knots

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21
Q

***Max Crosswind, RCC 2 / Medium-Poor

A

T/O: 15 knots

Landing: 17 knots

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22
Q

***Max Crosswind, RCC 1 / Poor

A

T/O: 13 knots

Landing: 15 knots

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23
Q

***Max Crosswind, RCC 0 / Nil

A

Operations Prohibited

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24
Q

***Max Crosswind CAT II Manual Landing

A

15 knots

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25
Q

***Max Crosswind Autoland

A

25 knots

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26
Q

***Max Crosswind CAT II/III

A

15 knots

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27
Q

***Wind Limit: Wet or contaminated runways whenever asymmetric reverse thrust is used

A

Reduce landing crosswind limitations by 5 knots

Inop T/R

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28
Q

***Maximum Runway Slope

A

+/- 2%

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29
Q

***Minimum Runway Width for 180° Turn

A

146 feet / 44.6 meters

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30
Q

Maximum Depth of slush, wet snow, or standing water for takeoff

A

1/2 inch (13 mm)

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31
Q

Maximum Depth of dry snow for takeoff

A

4 inches (102 mm)

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32
Q

***Maximum Operational Altitudes

A

43,100’

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33
Q

***Maximum Takeoff and Landing Altitudes

A

9,500’

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34
Q

Max G’s

A

Flaps Up: +2.5 to -1.0

Flaps Down: +2.0 to 0.0

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35
Q

Required O2

A

1000 psi for dispatch (2 pilots only)
Non-ETOPS: 1,500 psi
ETOPS: 1,800 psi or limited to 5 occupants (@ 70° F)

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36
Q

Before use of the EVAS system

A

EVAS: Emergency Vision Assurance System

HUD must be stowed prior to deployment
Front windshield sun shields must be removed prior to deployment

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37
Q

Cargo Door Wind Limits

A

Any cargo door operation: 40 knots

Any cargo door open: 65 knots

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38
Q

Maximum Cabin Differential Pressures

A

Relief Valves: 9.1

T/O and Landing: 0.125

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39
Q

***When must Anti-Ice be used

A

OAT on the ground and for takeoff or TAT in-flight is 10° or colder
and visible moisture in any form is present

Except during climb and cruise when the temperature is below -40°C SAT (except Ice Crystals, if present it must be ON)

Visible moisture is any form of precipitation such as clouds, fog with visibility of one mile (1600m) or less, rain, snow, sleet, or ice crystals

On the ground: Snow, ice, standing water or slush

Do not use engine anti-ice when OAT or TAT is above 10°C

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40
Q

Engine Run-Ups

A

When engine anti-ice is required and the OAT is 3°C or below
60% N1 for 30 sec no less than every 30 min

Before T/O: Run-up 60% N1 for 30 sec, confirm stable engine Ops

Check that area behind the airplane is clear

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41
Q

Icing Conditions in Decent

A

Engine anti-ice must be ON prior to and during descent in icing conditions

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42
Q

***Restriction on use of Aileron Trim

A

Don’t use while Autopilot is engaged

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43
Q

***Restriction on use of FLCH

A

Do not use FLCH on final approach below 1,000 feet AFE

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44
Q

***Autopilot use at airports > 8,500’

A

Do not use the autopilot below 100’ RA
So NO Autoland

45
Q

***Autopilot min engagement altitude after T/O

A

Must not be engaged below 1,000feet AFE

46
Q

***Min Autopilot use on Approach, Coupled ILS without autoland

47
Q

***Min Autopilot use altitude on Approach, Non-precision with VNAV

A

50’ below DA
100’ below DDA

DDA is required if approach is not selectable from NAV Database

48
Q

***Min Autopilot use altitude on Approach, Non-precision with V/S

A

50’ below MDA
100’ below DDA

DDA is required if approach is not selectable from NAV Database

49
Q

***Autoland Flaps

A

Flaps 25 or 30

1 or 2 engines

50
Q

***Don’t us HF radios

A

Do not operate HF radios during refueling operations

51
Q

N1 RPM Limit

A

Low pressure rotor 117.5%

52
Q

N2 RPM Limit

A

High pressure rotor 112.5%

53
Q

***Reverse Thrust Limitation

A

Reverse thrust is for ground use only

Do not use reverse thrust to back the airplane

54
Q

Engine Starter Duty Cycle

A

5 minutes on, followed by 1/2 minute off per minute on
To monitor, CA times once the FO selects start

55
Q

Engine Starter Re-engagement speed

A

0% N2 - Recommended

0-20% N2 - Normal

56
Q

Engine Oil Limitations, Min Pressure

57
Q

APU starter duty cycle max

A

3 consecutive starts or attempts within a 60 minute period

58
Q

***Flight Control Limits

A

Avoid rapid and large movements

59
Q

***Max Flap Altitude

60
Q

***Max altimeter difference for RVSM, in-flight

61
Q

***Max altimeter difference for RVSM, on the ground

62
Q

***Max altimeter difference for RVSM, from field elevation

63
Q

Airport facility required for a HUD required T/O

A

CAT III RWY / ILS critical area protected

64
Q

When must the FPA be caged

A

T/O Ops below 500’ / 150 m RVR

65
Q

***Max x-wind for HUD required T/O

66
Q

***Max x-wind for HUD required approach beyond FAF

67
Q

***Max course offset while using the HUD

68
Q

***EFVS required approach beyond FAF, what vertical nav modes are authorized

A

VNAV or Glide Slope

69
Q

***EFVS required approach beyond FAF, what vertical nav modes are NOT authorized

A

V/S or FPA

70
Q

***HUD approach database requirement

A

Line-selectable, FMC Nav Database that provides vertical and lateral guidance

71
Q

***Conformal Approach Symbology

Not allowed on what approaches

A

N/A on CAT I ILS with offset or LDA with G/S

72
Q

North/South Latitudes

A

Nav and displays not supported at latitudes > 87°

73
Q

Required for single Ops FMC on VOR approach

A

1 pilot must have raw data on PFD/ND by FAF

74
Q

Max Fuel Temp

75
Q

***Min Fuel Temp

A

3°C above freezing point

76
Q

Number of Fuel Tanks

A

3 Total

2 Main / 1 Center

77
Q

***Main Tank Qty

A

40,000 lbs
6,000 gal

6,010 gal / 40,267 lbs

78
Q

***Center Tank Qty

A

80,000 lbs
12,000 gal

11,900 gal / 79,730 lbs

79
Q

***Total Fuel Qty

A

160,000 lbs
24,000 gal

23,920 gal / 160,264 lbs

80
Q

Don’t reset circuit breakers

A
  1. Fuel Pump

2. Fuel Pump Control

81
Q

Fuel Usage I

A

No center tank fuel

Tank-To-Engine
All main tank boost pumps ON
X-feed valve closed (for T/O and Landings)

82
Q

Fuel Usage II

A

Fuel in center tank

Use center tank for all Ops until empty, then use Fuel Usage I

All boost pumps ON
X-feed valve closed

83
Q

Dry running of the center fuel tank

A

Prohibited

CTR L FUEL PUMP
CTR R FUEL PUMP

84
Q

***Max Fuel Imbalance

A

2,500 lbs (when total Main Tank is < 48,000 lbs)

1,500 lbs ( when total Main Tank is > 48,000 lbs)

85
Q

***When can the Center Tank have fuel with less than full Main Tanks

A

Center up to 22,050 lbs with < full main tanks

Provided: Center Tank fuel weight + actual zero fuel weight does not exceed max zero fuel weight / CG limits are observed

86
Q

***WX Radar, when not to use

A

Avoid Ops in hangar

87
Q 
***ACFT Dimensions
Length 
Width 
Height
Horizontal Stabilizer Width
A

180/156/52

Length: 180’3”
Width: 156’-1”
Height: 52’
Horizontal Stabilizer Width: 61’1”

88
Q

***Gear Dimensions
L/R
Nose/Main

A

L/R: 30’-6”

Nose/Main: 74’8”

89
Q

***Continuous Ignition Required

A
  1. Moderate - Heavy Rain
  2. Hail
  3. Sleet (encountered or anticipated)
90
Q

Dry Ice and APU

A

If there is dry ice,

For ground Ops:
APU - ON
Both Packs - ON

Until all cargo doors are open for 5 min, then APU and Packs may be turned off (FOM pg 312)
Don’t leave the APU on with ACFT unattended (Crew or MX)

91
Q

Engine Type/Thrust

A

GE CF6-80

60,200 lbs of thrust

92
Q

Fuel Dump Rate and Time

A

2600 lbs/min

30 min with full tanks

93
Q

Max trim tolerance between the APS output and the FMC-calculated trim setting

A

One unit or less

94
Q

Max allowable V speed tolerance between the APS output and the FMC-calculated V speed

A

1 knot

If there is a one knot difference, the FMC value takes precedence

95
Q

Aborted Engine Start (reasons)

A
  1. EGT does not increase by 25 seconds after the fuel control switch is moved to RUN.
  2. There is no N1 rotation by 30 seconds after N2 is stabilized at idle.
  3. EGT quickly nears or exceeds the start limit.
  4. The oil pressure indication is not normal by the time the engine is stabilized at idle.
96
Q

Max single engine thrust in a congested area

97
Q

Engine Warm-Up

A
  1. 3 min

2. Oil temperature must be above the bottom of the temperature scale

98
Q

Engine Cool-Down

A

3 min

Do not delay engine shutdown for a taxi that is less than 3 min

99
Q

When not to do a LTAET

A
  1. Hydraulic or electric MEL deferrals.
  2. A system that impacts braking or steering capability is not operative.
  3. Visibility less than 1,200 RVR/350m.
  4. When “FOM 10.37 Dry Ice Supplemental Procedures in Effect.”
  5. Ramp and/or taxiway slippery or contaminated.
  6. Aircraft to be deiced.
  7. During Icing conditions.
  8. Tight maneuvering required.
  9. 10-10 page restriction.
100
Q

Tail Strike Pitch Attitude

A

T/O: 8°

Landing: 5°

101
Q

Min Holding Speed

A

Vref 30 + 100

102
Q

Flaps Up Maneuvering Speed

A

Vref 30 + 80

103
Q

Max Rate of Climb

A

Vref 30 + 130

104
Q

How far is the pilot seat from the nose/main gear

A

Nose: 7.5’
Main: 82’

105
Q

Go Around Time & Fuel (Fleet Update)

A

15 min / 3100 lbs

106
Q

Cockpit Monitoring System

A

Not to be used < 10,000’

107
Q

Speedbrakes

A

Avoid use > Flaps 5 to avoid buffeting

108
Q

APU Burn

A

400 lbs/hr

FedEx (20 decks)

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