Shimada notes Flashcards
Oxygen requirements
850psi lasts 2.5 hours for decompression: 0.5 Smoke
1850psi lasts 5.5 1.0
Autoland Function
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
Critical operation
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
Critical operation reverser
Dry Dry reverse idle
flooded All eng
Others *
Landing climb
3.2%
Vref> 1.23 VS1G
Thrust available after 8 sec
Approach climb
2.1%
Speed <1.4 VS1G
Required landing distance
Certified = demonstrated + 67%
Wet + Certified + 15 %
Maintenance time periods
A check -500 hrs
C check- 6000 hrs
Heavy Maintenance - 5 years
Check flight performance
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
1 ENGINE INOP Check performance
Climb segments
2nd segment: 4.5%, 1100fpm, 3.86nm
3rd segment: 4nm
final segment: 5.2%, 1900fpm, 4nm
1 ENGINE INOP Check performance
Altitude capability
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
Check performance
Landing field lenght (256300)
Dry 4700 +1100 -10kt
WetG 5500
WetNG 6200 +1300
RORS landing distance available
9840
Holding fuel
Vref30+80, 260000, ISA
1500ft: 8680lbs/hr
10000ft: 8300lbs/hr
Limit speed (stick shaker/stall)
F up 174/159 F1 138/131 F5 126/121 F20+g 119/111 F30 118/110
Vss while banking
30 degrees 1.07 Vss 40 1.14 50 1.25 60 1.41 70 1.71
Stopping distance
140 kts max Auto 2700ft
150 kts 3100ft (Autobrake 2 =x2)
Fuel dump time
10 000lbs =4min @ 2600lbs/min
FPDM
Correction factor
Performance factor
Correction factor: Factor which corrects the amount of required fuel when fuel planning.
Performance factor: Factor which corrects the performance data stored in FMC
Taxi fuel
Standard International 800lbs (15min)
Standard Domestic 500lbs (10min)
Narita 1000lbs (20min)
Landing buffer fuel
loaded if route less than 1000nm
Included in Descent fuel burn:
Naha 1 min
HND 3 min
Localizer expanded scale
1 dot =0.5 degrees (half of standard, 1 dot=1degree)
GS 1 dot
1 dot =0.35 degree (expanded scale the same)
EHSI full ILS mode
1 dot localizer = 1.25
EHSI VOR full mode
1 dot = 5degree
Plan to land at nearest suitable airport
12
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.
Threshold gear and eye height
Gear 36’
Eye. 65’
Blind area on landing
Gear to eye. 74’
Eye to aiming point 120’
Gear to aiming point 194’
RVSM equipment
Two individual alt measurement devices
1 Automatic alt hold control system
1 Alt alerting system
1 SSR alt reporting transponder Mode C
RTO policy
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
Oxygen masks and smoke goggles
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
When to use oxygen masks
Cabin alt rapid depressurization Pack off Volcanic ash Smoke fire or Fumes Cargo fire
Oxygen duration
Cabin - 12 min
Cabin - ER, 22 min
Hydroplaning speed ER
9/—- of 210 = 130kts
Runway grooving
6mm——32mm——6mm
Wing and stabilizer sweep
Wing 31.3
Stabilizer 33
Stabilizer high speed stall later.
