767 Flight Training Manual (FTM 12)

Question 1

QNE

Answer 1

29.92 inches

1013 hPa

Question 2

QNH

Answer 2

Local station barometric pressure

Question 3

QFE

Answer 3

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

Question 4

Transition Level (TL)

Answer 4

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

Going Down

Question 5

Transition Altitude (TA)

Answer 5

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

Going Up

Question 6

Transition Layer (TRL)

Answer 6

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

Question 7

Hold Time Limit (Bingo Fuel)

Answer 7

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

Question 8

Engine Severe Damage

Answer 8

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

Question 9

Systems that require coordination with ground crew before use

Answer 9

1. Hyd System Pressurization
2. Flight Control Surface Movement
3. ACFT Movement

Question 10

Radio Use

Answer 10

VHF L - ATC
VHF R - All other voice communications
VHF C - ACARS/Datalink
HF L - Primary
HF R - Secondary/ACARS/Datalink

Question 11

Electric Failure Rules

Answer 11

AC Lies

DC Dies

Question 12

Wind Additive

Answer 12

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

Question 13

When must Autothrottles be disconnected

Answer 13

Manual Landing: Prior to touchdown

Question 14

Decision Region Tolerances

Answer 14

500’ RA

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

Question 15

ASA Indications

Answer 15

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

Question 16

When can you set your Missed Approach Alt on an RNAV

Answer 16

FAF is a good place

Make sure you’re 300’ below missed approach altitude

Question 17

Decent on an RNAV approach

Answer 17

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

Question 18

After Cleared, Established and Protected

Answer 18

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)

Question 19

RNAV RNP AR considerations

Answer 19

• 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

Question 20

Min Holding Speed

Answer 20

Vref30 + 100

Question 21

How is top of decent calculated

Answer 21

Any restrictions

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

Question 22

Reasons to Abort Engine Start

Answer 22

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

Question 23

LESS THAN ALL ENGINE TAXI (LTAET) RESTRICTIONS

Answer 23

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

Question 24

Normal EICAS Messages before start

Answer 24

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

Question 25

Reject Prior to 80 knots

Answer 25

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

Question 26

Reject Above 80 knots - V1

Answer 26

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

Question 27

Tail Strike

Answer 27

8° T/O 5° Landing Try to keep less than 7.5° at all times “TAILSTRIKE” warranting at 6.5°

Question 28

Ways to reduce T/O thrust

Answer 28

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%

Question 29

Windshear Indication and Reaction

Answer 29

``` 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

Question 30

GPWS Recovery

Answer 30

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

Question 31

Max High Speed Turn-Off

Answer 31

60 knots

Question 32

Magenta “B” on the Landing Performance

Answer 32

AML entry required Req block time of (time), landed at (date and time)

Question 33

What altitude should fuel jettison be complete

Answer 33

4000’

Question 34

Required MX Write-Ups

Answer 34

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

Question 35

Pitch on Approach Pitch in the Flare

Answer 35

Approach: 2° - 4° Flare: 4° - 6°

Question 36

Flare Height Caculation

Answer 36

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