Brainscape's Knowledge GenomeTM

Browse over 1 million classes created by top students, professors, publishers, and experts.


See full index

FedEx > 767 Flight Training Manual (FTM 11) > Flashcards

767 Flight Training Manual (FTM 11) Flashcards

1
Q

QNE

A

29.92 inches

1013 hPa

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
2
Q

QNH

A

Local station barometric pressure

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
3
Q

QFE

A

Barometric pressure that will result in a reading of zero at field elevation

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
4
Q

Transition Level (TL)

A

The lowest assignable flight level at which QNE (29.92) may be used.

Going Down

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
5
Q

Transition Altitude (TA)

A

The highest assignable altitude at which QNH (field pressure) may be used.

Going Up

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
6
Q

Transition Layer (TRL)

A

When the transition altitude (TA) and the transition level (TL) are not the same, the space between is called transition layer.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
7
Q

Hold Time Limit (Bingo Fuel)

A

Fuel To Destination 1.5
Alternate Fuel (FP/R) 7.5
FOD 10.0
Bingo 19.0

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
8
Q

Engine Severe Damage

A

No N1 Rotation
No N2 Rotation
Zero Fuel Flow
Very High EGT

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
9
Q

Systems that require coordination with ground crew before use

A
  1. Hyd System Pressurization
  2. Flight Control Surface Movement
  3. ACFT Movement
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
10
Q

Radio Use

A 
VHF L - ATC
VHF R - All other voice communications
VHF C - ACARS/Datalink
HF L - Primary
HF R - Secondary/ACARS/Datalink
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
11
Q

Electric Failure Rules

A

AC Lies

DC Dies

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
12
Q

Wind Additive

A

Autothrottles ON:
Not needed

NextGen APS:
Not needed

Autothrottles OFF:
Steady state wind:
     Headwind: 50%
     45°: 35%
     X-wind: 0%

Plus full gust (don’t use if tailwind)

Min: +5
Max: +15

Do not apply wind additives for steady tailwinds or tailwind gusts

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
13
Q

When must Autothrottles be disconnected

A

Manual Landing: Prior to touchdown

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
14
Q

Decision Region Tolerances

A

500’ RA

Loc: 1/3 dot
G/S: 1/2 dot
No sustained oscillations about the localizer or the glide slope

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
15
Q

ASA Indications

A

Land 3/Blank: CAT III, Auto-land, No DA (fail operational)

Land 2/No Land 3: CAT III, Auto-land, Required DA (Fail Passive)

Blank/No Auto-land: CAT II, No Auto-land, 1200 RVR

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
16
Q

When can you set your Missed Approach Alt on an RNAV

A

FAF is a good place

Make sure you’re 300’ below missed approach altitude

17
Q

Decent on an RNAV approach

A

Cleared: Clearance from ATC

Established: Lateral scale becomes active “case break” or within 1 NM of a point cleared to

Protected: Altitudes verified and NO Discontinuities on the legs page

18
Q

After Cleared, Established and Protected

A

LAVS
L-LNAV selected and annunciated
A-Altitude set to threshold rounded up to next 100’
V-VNAV selected and either VNAV SPD or VNAV PTH annunciated
S-Speed intervention selected and set

(if past the FAF without VNAV PTH displayed and in IMC, Go-Around)

19
Q

RNAV RNP AR considerations

A
  • Confirm FMC RAD NAV INHIBIT is “On”
  • MAX 15 kt crosswind if <4000 RVR (1200 m) or ¾ mile
  • Use published VNAV DA(H)
  • The minimum RNP value is .13
  • Prior to IAF, PF must have “TERR” displayed
  • Prior to FAF, ND/PFD display range 10 NM or less
  • Speed intervention selected and set
  • Full configured and on speed by FAF

At FAF

  • Cross check primary altimeters +/- 100’
  • Compare primary altimeters +/- 100 ft of FAF
  • In the event of missed approach, manually entered RNP values should be deleted
20
Q

Min Holding Speed

A

Vref30 + 100

21
Q

How is top of decent calculated

A

Any restrictions

If none,
30 miles from the VOR / Airport at 250/10,000’ AFE

22
Q

Reasons to Abort Engine Start

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 that the engine is stabilized at idle
23
Q

LESS THAN ALL ENGINE TAXI (LTAET) RESTRICTIONS

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

DO NOT
1. Exceed 40% N1 when operating in a congested area
2. Accomplish the flight control check or the BEFORE TAKEOFF
checklist until all engines are started and stable

  • Verify*
    1. 3 minutes warm-up time
    2. Engine oil temperature must be above the bottom of the temperature scale
24
Q

Normal EICAS Messages before start

A
  1. R ENG SHUTDOWN
  2. L ENG SHUTDOWN
  3. C HYD PRIM 2
  4. PROBE HEAT
  5. R PACK OFF
  6. L PACK OFF
25
Q

Reject Prior to 80 knots

A
  1. Activation of the Master Caution
  2. System Failure(s)
  3. Unusual Noise or Vibration
  4. Tire Failure
  5. Abnormally Slow Acceleration
  6. Takeoff Config Warning
  7. Window Opens
  8. HUD (if required)
  9. Engine Failure
  10. Fire
  11. Windshear Warning
  12. ACFT Unsafe or Unable to Fly
26
Q

Reject Above 80 knots - V1

A
  1. Engine Failure
  2. Fire
  3. Windshear Warning
  4. ACFT Unsafe or Unable to Fly
27
Q

Tail Strike

A

8° T/O
5° Landing

Try to keep less than 7.5° at all times
“TAILSTRIKE” warranting at 6.5°

28
Q

Ways to reduce T/O thrust

A
  1. Assumed Temperature Method (ATM)
  2. Fixed Derate

ATM: Wet RWY OK, contaminated NOT
Fiexed Derate: OK wet and or contaminated

Max Combined is 25%

29
Q

Windshear Indication and Reaction

A 
In Excess
15 knots indicated airspeed
500 FPM vertical speed
5 degrees pitch attitude
1 dot displacement from the glideslope
Unusual thrust lever position for a significant period of time
Windshear Immediate-Alert Warning

Before V1: Reject
After V1: Perform Windshear Escape Maneuver (Rotate no later than 2000’ RWY left)
On Approach: Perform Windshear Escape Maneuver or Normal Go-Around

30
Q

GPWS Recovery

A
  1. Disconnect Autopilot and Autothrottle
  2. Maximum Thrust
  3. Roll Wings Level / Pitch Attitude 20°
  4. Retract Speedbrakes
31
Q

Max High Speed Turn-Off

A

60 knots

32
Q

Magenta “B” on the Landing Performance

A

AML entry required

Req block time of (time), landed at (date and time)

33
Q

What altitude should fuel jettison be complete

A

4000’

34
Q

Required MX Write-Ups

A
  1. Hard Landing
  2. Over Weight Landing
  3. Hi Drag / High Side Load Event
  4. Severe Turbulence
  5. Overspeed
  6. High Energy Stop
  7. Lightning Strike
  8. Extreme Dust
  9. Tail Strike
  10. Any Event PIC Deems Appropriate
35
Q

Pitch on Approach
Pitch in the Flare

A

Approach: 2° - 4°
Flare: 4° - 6°

36
Q

Flare Height Caculation

A

Flare Height
Descent Rate ÷ 30 = Landing Flare Height
900 fpm ÷ 30’ = 30’
Simpler, drop the zero
90 ÷ 3 = 30 feet

FedEx (20 decks)

Brainscape helps you reach your goals faster, through stronger study habits.
© 2024 Bold Learning Solutions. Terms and Conditions