This Performance Tool is provided for reference and planning purposes only.
By using this tool, you acknowledge and agree that:
All performance calculations must be verified against approved company sources and official aircraft performance documentation.
This tool does not replace official performance manuals, flight operations procedures, or crew responsibilities.
You are solely responsible for ensuring safe flight operations and compliance with all applicable regulations.
The data provided may contain errors or inaccuracies and should never be the sole basis for operational decisions.
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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 / FTUnfactored / 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:
BTMS VALUE:
REV:
AUTOBRAKE:
TAXI MILES:
ONE BRAKE DEACTIVATED:
Inflight Gear down cooldown:
GROUND COOLDOWN:
ARPT
RWY
COND
WIND
( CALM )
OAT
86 F โ
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
--- ยฐC
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 ONDRY
110,950KG
WIND :
080/5
( TW 5 / XW 1 )
QNH :
Low QNH1010
-3 hPa @ -110
-330
PACKS/EAI/WAI :
PACKS ON
0
MEL:
TOTAL CORRECTIONS : =
-100
CORRECTED MTOW (RTOW) :
110,850KG
Max RTOW = โ KG
REDUCED THRUST
ACTUAL TAKEOFF WEIGHT :
76,522KG
TOTAL CORRECTIONS (reversed) : =
+100
ASSUMED TAKEOFF WEIGHT :
76,622KG
ASSUMED TEMPERATURE USED FOR TAKEOFF
54 ยฐC
FLAP :5
E/O ACCEL HT :1040'
Vโ
134
Vโ
134
Vส
136
Vสแดาโโ
121
Vสแดาโโโโโ
161
Vสแดาโโโโโ
201
TOT N1:
โ
A/TEMP:
54 ยฐC
RTOT N1:
โ
OPT Checklists
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Aircraft Defects
5Y-SNL
Local Only
0
Total Defects
0
Open
0
Resolved
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โ
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MEL Reference
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IFALPA China RVSM Conversion Table
WESTBOUND180ยฐ to 359ยฐ
RVSM airspace
40,10038,10036,10034,10032,10030,100
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 180ยฐ-359ยฐ
Cleared Meter FL
Select FL in Feet
EASTBOUND 0ยฐ-179ยฐ
Westbound
Eastbound
RVSM
EASTBOUND0ยฐ to 179ยฐ
RVSM airspace
41,10039,10037,10035,10033,10031,10029,100
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.
-METERS
โ
-FEET
-
Tap to close
Fuel Imbalance Check
โ
lb
lb
lb
Enter fuel quantities to check
Imbalance
โ
Limit
โ
Margin
โ
Total main
โ
Total fuel
โ
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 —