Turbulent Air Penetration in severe turbulence
- 290 kts below 25 000’
- 310kts/M.84 above 25 000’ (whichever is lower)
HF and weather radar restrictions
- Don’t operate HF during refuelling
- Avoid weather radar in hangars
- Avoid when personnel within area normally enclosed by radar
Autopilot engagement limits + Glideslope + Airport elev
- Not engaged below 200’ on takeoff
- Disengage by 135’ unless Land 2 or 3
- Disengage by 100’ with Land 2 or 3 with glideslope greater than 3.25 degrees
- Disengage by 50’ below DH/MDA if glideslope greater than 3.77 degrees
- Autoland only for airports below 8400’
Autoland Wind, Slope & Flap Limits
- Max 25 kts headwind
- Max 15 kts tailwind
- Max 25 kts crosswind
- maximum glideslope 3.25 degrees
- minimum glideslope 2.5 degrees
- can be used F20, F25 or F30 with 2 or 1 eng
RVSM Operations + Altimeter differences
- Do not fly in RVSM airspace on ISFD only
- Max allowable difference before T/O Capt or F/O altimeter and field elevation is 75’
- AIP max difference is 60’
Runway slope
- +- 2%
Max takeoff and landing tailwind component
- 15 kts
Max operating altitude
- 43 100’
Max takeoff and landing altitude
- 14 000’
Weight Limitations
- max Taxi………..255 372 kg
- max Takeoff……254 692 kg
- max Landing….192 776 kg
- max ZFW……….181 436 kg
Wind limits when T/O weather minima are predicated HUD operations
- Max 25 kts headwind
- Max 15 kts tailwind
- Max 20 kts crosswind
- Max 15 kts crosswind when RV/RVR below 550m (T/O + Ldg)
Don’t use FLCH on final approach below
- 1000’ AFE
Engines - oil temp + reverse
- oil temp greater than -40 C for engine start
- intentional reverse thrust in flight prohibited
- backing with reverse thrust prohibited
Flap and flight control input restrictions
- avoid rapid and large alternating control inputs
- max flap altitude 20 000’
- takeoff only permitted in normal flight control mode
Fuel temperature -max x 3 + min
Max
- Takeoff 49 C
- Inflight TS-1 57 C
- Inflight other 65 C
Min
- Takeoff -29 C
- Inflight -42 C or 3 C above fuel freezing point
Climb Speeds - Max Angle + Max Rate
Max Angle - from FMC (approx Vimd/Flap Up/Vref30 + 80kts)
Max Rate - Vref30 + 140kt into M.84 (Max angle + 60 kts)
Aircraft Dimensions + RFF cat
Wing span - 60.1 m (197’)
Length - 62.8 m (206’)
Cat D
RFF Cat 9
ICAO code 4E
FAA Group V
ETOPS Threshold time
60 min = 413nm
Hydraulic Tests and Eng Cooldown on landing
- First 90 seconds from flap/SB up (45 sec in sup proc)
- Second takes 55 seconds after hydraulics unpowered
- wait 3 min after HYD PRESS SYS L+C+R before recording maint
- 3 min cooldown from touchdown (idle) or out of full reverse
- PECS cooldown either 10 min (APU or 2 x ext) or 22 min (1 ext) before removing power
LMC
Above 240 000kg
- No traffic LMC
- Max fuel LMC 1000kg
At or below 240 000kg
- Traffic LMC 700kg
- Fuel LMC 1000kg
Approach Tolerances
ILS and VOR/ADF
ILS/GLS
To 300’ - 1 dot normal or within expanded scale
Below 300’ - 1/2 dot normal or within expanded scale
“App Minima” or “100” - 1/2 expanded scale
- PFD/HUD expanded scale = 1/2 dot - Call “Outside limits” if exceeded
Glideslope - 1 dot
VOR/ADF
- +-5 degrees
Airspeed
- +10k to -5k
RoD - no more than 1000fpm below 1000’
Takeoff Alternate
- Required if weather below lowest useable landing minima
- A/B or C within 60 min of departure airport above Landing Minima
- A/B or C between 60 min and 180 min of departure airport above EDTO Planning minima and EDTO annotated
- Requires a +-30 min buffer
- INTER/TEMPO 30% or 40% do not need to be considered
Low Vis T/O Requirements
- Capt PF with vis below 800m
- Low Vis required below 550m
- RVR required below 350m
- At/above 200m req TDZ + Mid or end
- Below 200m req all 3 zones
- HUD required for RVR below 125m
- Max crosswind 15kts
Runup Required
3 - temp 3 degrees or less + vis moisture on apron/taxi/RW
4 - need 40%
5 - for 5 sec
6 - every 60 min
12 - max 120 min taxi
- Needs to be completed within 5 min of T/O.
- If vibration increase to 50% until vib less than 4 units
