NOTAM
Confirm
AIRCRAFT
BOEING 767-200
CF6-80A2 • PERFORMANCE TOOL
TAKEOFF
 
ARPT
RWY
COND
WIND
GUST
( TW 1 / XW 3 )
OAT
84 F
QNH
29.94 IN HG
FLAP
BRKS
NNC
REV
0 KT
LANDING WT
191,400 LBS
Exceeds Max Landing Wt (128,367 KGS)
VREF ADD:
Vref30 = 109 KT

ALL DISTANCES
M / FT Unfactored / Factored
Max Manual-926 M
Max Auto-1413 M
AB 4-1542 M
AB 3-1773 M
AB 2-1971 M
AB 1-2124 M
TAILWIND
1KT
CROSSWIND (RWY 34)
3KT
from Right
VREF
109KT
VAPP
146KT
(Vref + 5)
LDR 1971 M
0 M
3020 M
Recommended Brake Cooling Schedule
CALCULATE FROM BTMS:
REV:
AUTOBRAKE:
TAXI MILES:
ONE BRAKE DEACTIVATED:
Inflight Gear down cooldown:
GROUND COOLDOWN:
 
ARPT
RWY
COND
WIND
( CALM )
OAT
86 F
QNH
29.91 IN HG
FLAPS
PERF
ANTI-ICE
DEFECT
TOW
350,755 LBS
CG (%)
% MAC
ENG FAILURE PROCEDURE
---
---
NOISE ABATEMENT
Select procedure above

INTX
FULL
COND
DRY
WIND
030/0
(CALM)
A/C
A/ICE OFF
PERF
PACKS ON
FLAP
---
TOGW
--- KG
RTOW
--- KG
RWY/INT
---
EO ACCEL ALT
--- ft MSL
--- AGL
TRIM
---
---
LIMIT
---
ASSUMED TEMP
--- °C
N1
---
V1
---KT
VR
---KT
V2
---KT
Vref30
---KT
RUNWAY : 27
ATIS :
VABB / BOM
DRY
080/5
30
1012
FLAPS : 1
5
15
E/O PROCEDURE
MAX PERF: LIMIT TOW
(As per Takeoff Analysis)
DRY
WET
DEFECT
PACKS ON DRY
110,950KG
WIND :
080/5
( TW 5 / XW 1 )
QNH :
Low QNH 1010
-3 hPa @ -110
-330
PACKS/EAI/WAI :
PACKS ON
0
MEL:
TOTAL CORRECTIONS : =
-100
CORRECTED MTOW (RTOW) :
110,850 KG
REDUCED THRUST
ACTUAL TAKEOFF WEIGHT :
76,522KG
TOTAL CORRECTIONS (reversed) : =
+100
ASSUMED TAKEOFF WEIGHT :
76,622KG
ASSUMED TEMPERATURE USED FOR TAKEOFF
54 °C
FLAP : 5
E/O ACCEL HT : 1040'
V₁
134
V₂
134
136
Vʀᴇғ₃₀
121
Vʀᴇғ₃₀₊₄₀
161
Vʀᴇғ₃₀₊₈₀
201
TOT N1:
A/TEMP:
54 °C
RTOT N1:
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Total Defects
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IFALPA China RVSM Conversion Table
WESTBOUND 180° to 359°
RVSM airspace
40,100 38,100 36,100 34,100 32,100 30,100
IMPORTANT NOTES
  • ATC will issue the Flight Level clearance in meters.
  • Pilots shall use the China RVSM FLAS table to determine the corresponding flight level in feet.
WESTBOUND 180°-359°
Cleared
Meter FL
Select
FL in Feet
EASTBOUND 0°-179°
Westbound
Eastbound
RVSM
EASTBOUND 0° to 179°
RVSM airspace
41,100 39,100 37,100 35,100 33,100 31,100 29,100
IMPORTANT NOTES
  • The aircraft shall be flown using the flight level in FEET.
  • Pilots should be aware that due to rounding differences, the metric readout of onboard avionics will not necessarily correspond to the cleared FL in meters, however the difference will never be more than 30 meters.
Fuel Imbalance Check
lb
lb
lb
Enter fuel quantities to check

FUEL (kg)

OPERATIONAL ITEMS (kg)

CERT. LIMITS (kg)

MAIN DECK (kg) configure each column by type — A, D, or (unused) — then enter bay weight

LOWER DECK (kg) enter hold/ULD weights in kilograms

LOADSHEET SUMMARY

Traffic Load
Allowed TL
Underload
ZFW
/ —
TOW
/ —
LW
/ —
Total Loaded Idx
%MAC at TOW
Stab Trim
Lateral (Main)
Lateral (Lower)

TRIM SHEET — CURTAILED WEIGHT LIMITS live CG plot · aircraft

Avoidances — FIR / Airway / Waypoint
Performance Inputs — Fuel & Optimum FL auto-calculated
MTOW: — · MLW: —
Per-flight (payload)
AUTO MIN FUEL:
Using auto min fuel
DOW: — · MZFW: — · (edit in Loadsheet to adjust DOW)
Auto from weather
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DANGEROUS GOODS

Emergency response drill reference. Enter a UN number or search by proper shipping name.
ICAO DOC 9481 §4
Accepts 1230 or UN1230.
Emergency response only. Quantity limits are not included in this phase.
RECENT DG