Shimada notes

Question 1

Oxygen requirements

Answer 1

850psi lasts 2.5 hours for decompression: 0.5 Smoke

1850psi lasts 5.5 1.0

Question 2

Autoland Function

Answer 2

Approach mode Push
-3-channel arm

1500ft and LOC, GS capture

• 3 Channel engage
• ASA land 3
• FLARE/ROLLOUT ARM

500ft

• Runway alignment begin
• Crab 5, bank 2

100’
-Trim if 2 channel

50’
-FLARE ENGGE

15’
A/T retard

5ft
ROLLOUT capture
Wings level

on ground ——no, float for 2 sec

• A/T disengage Pitch mode disarm
• Pitch att 2 degrees

Question 3

Critical operation

Answer 3

Threshold speed- Vref +15kts
Touch down point - 2000ft
Transition time- 3 sec
Braking force–Most slippery + all eng reverse (to 70kts)
–Average slippery + Eng reverse idle
Reverse thrust- As above
Coefficient of length margin –1
Temp. 30 degrees for Dry/wet, 0 for snow/ice/slush

Question 4

Critical operation reverser

Answer 4

Dry Dry reverse idle
flooded All eng
Others *

Question 5

Landing climb

Answer 5

3.2%
Vref> 1.23 VS1G
Thrust available after 8 sec

Question 6

Approach climb

Answer 6

2.1%

Speed <1.4 VS1G

Question 7

Required landing distance

Answer 7

Certified = demonstrated + 67%

Wet + Certified + 15 %

Question 8

Maintenance time periods

Answer 8

A check -500 hrs
C check- 6000 hrs
Heavy Maintenance - 5 years

Question 9

Check flight performance

Answer 9

D2/F5 distance 5960’ +1400 (10kts tailwind)

Vmcg Max 113: D1 108, D2 103
Vmca Max 102: D1 99, D2 95

TO N1 100.3% Des speed econ 296kts

Climb speed: ECON 312, MAX RATE 282/.78, ANGLE 211/.77

OPTIMUM ALT 37300
MCRT/MCLT 41500
1.3G 41100
1.5G 37900

Question 10

1 ENGINE INOP Check performance

Climb segments

Answer 10

2nd segment: 4.5%, 1100fpm, 3.86nm
3rd segment: 4nm
final segment: 5.2%, 1900fpm, 4nm

Question 11

1 ENGINE INOP Check performance

Altitude capability

Answer 11

MCT LIMIT: 24600 (ISA+15)
MCRT LIMIT 24700’ (-900’ for eng anti ice on)

Inflight diversion  (183nm form RORS to ROAH @ FL210
BOF  6475lbs (10500 lbs/hr)
SPD  350 (LRC)

Driftdown
speed 217kts
Alt 30000

Question 12

Check performance

Landing field lenght (256300)

Answer 12

Dry 4700 +1100 -10kt
WetG 5500
WetNG 6200 +1300

Question 13

RORS landing distance available

Answer 13

9840

Question 14

Holding fuel

Vref30+80, 260000, ISA

Answer 14

1500ft: 8680lbs/hr
10000ft: 8300lbs/hr

Question 15

Limit speed (stick shaker/stall)

Answer 15

F up       174/159
F1           138/131
F5          126/121
F20+g    119/111
F30        118/110

Question 16

Vss while banking

Answer 16

30 degrees   1.07  Vss
40                  1.14
50                  1.25
60                  1.41
70                  1.71

Question 17

Stopping distance

Answer 17

140 kts max Auto 2700ft

150 kts 3100ft (Autobrake 2 =x2)

Question 18

Fuel dump time

Answer 18

10 000lbs =4min @ 2600lbs/min

Question 19

FPDM
Correction factor
Performance factor

Answer 19

Correction factor: Factor which corrects the amount of required fuel when fuel planning.
Performance factor: Factor which corrects the performance data stored in FMC

Question 20

Taxi fuel

Answer 20

Standard International 800lbs (15min)
Standard Domestic 500lbs (10min)
Narita 1000lbs (20min)

Question 21

Landing buffer fuel

Answer 21

loaded if route less than 1000nm
Included in Descent fuel burn:
Naha 1 min
HND 3 min

Question 22

Localizer expanded scale

Answer 22

1 dot =0.5 degrees (half of standard, 1 dot=1degree)

Question 23

GS 1 dot

Answer 23

1 dot =0.35 degree (expanded scale the same)

Question 24

EHSI full ILS mode

Answer 24

1 dot localizer = 1.25

Question 25

EHSI VOR full mode

Answer 25

1 dot = 5degree

Question 26

Plan to land at nearest suitable airport

12

Answer 26

Window damage
Cabin Altitude
Pack L+R

Engine LIM surge or stall
ENG severe damage
ENG failures
ENG oil filter, press, Temp

Volcanic ash
FIRE, APU, wheelwell, eng, cargo, eng overheat
FUEL leak and low Fuel

Hydraulic, 1 remaining
Tailstrike.

Question 27

Threshold gear and eye height

Answer 27

Gear 36’

Eye. 65’

Question 28

Blind area on landing

Answer 28

Gear to eye. 74’
Eye to aiming point 120’
Gear to aiming point 194’

Question 29

RVSM equipment

Answer 29

Two individual alt measurement devices
1 Automatic alt hold control system
1 Alt alerting system
1 SSR alt reporting transponder Mode C

Question 30

RTO policy

Answer 30

Go mindedness
Except for the occurrence of a hindrance where there is a serious doubt that the airplane can safely fly, it is safer to continue the takeoff than to reject it from a point near V1

Guidelines
Reject if thrust loss or takeoff warning that would render the aircraft unflyable

Safer not to reject for EGT or fire without thrust loss.

Tire failure or antiskid failure extremely dangerous

Criteria if high speed defined by Captain, but 80kts

Briefing
Go/no go decision based on go-mindedness
Callout of malfunction with high speed criteria
Review of RTO procedure

Only call malfunction if it requires RTO (not above 80kts)
Call eng failure only. Not which engine

Use RTO braking backup with manual

Risk of go and no go

V1 and takeoff performance standard

Question 31

Oxygen masks and smoke goggles

Answer 31

Emergency position-
when positive pressure is needed to remove contaminants

100% -
When positive pressure is not needed but Contamination exists.

N
If prolonged use is needed. When cabin alt above a certain value 100% is automatically supplied under pressure

Question 32

When to use oxygen masks

Answer 32

Cabin alt rapid depressurization
Pack off 
Volcanic ash
Smoke fire or Fumes
Cargo fire

Question 33

Oxygen duration

Answer 33

Cabin - 12 min

Cabin - ER, 22 min

Question 34

Hydroplaning speed ER

Answer 34

9/—- of 210 = 130kts

Question 35

Runway grooving

Answer 35

6mm——32mm——6mm

Question 36

Wing and stabilizer sweep

Answer 36

Wing 31.3

Stabilizer 33

Stabilizer high speed stall later.