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101-590010-469R3_text.fm Page 18 Tuesday, January 29, 2013 8:56 AM
TAKE-OFF WEIGHT - FLAPS APPROACH
TO ACHIEVE EU-OPS CLIMB REQUIREMENTS
ASSOCIATED CONDITIONS: EXAMPLE:
AIRPLANE........AIRBORNE PRESSURE ALTITUDE ....543O FT
POWER ..........TAKE-OFF OAT ..................28°C
FLAPS...........APPROACH
INOPERATIVE NOTE: FOR OPERATION WITH ICE TAKE-OFF WEIGHT.......12,5OO LB
PROPELLER.....FEATHERED VANES EXTENDED, NO OFF
LOADING IS REQUIRED
10000 ISA + 37°C
10,000
30°C
9000 OUTSIDE AIR TEMPERATURE
8000
7000
PRESSURE ALTITUDE ~ FEET 5000
6000
4000
3000 MAXIMUM TAKE-OFF WEIGHT
2000
1000
BLAATOOO1C
0 SL
900
9,000 0 10,000 11,000 12,000
WEIGHT ~ POUNDS
3500 4000 4500
WEIGHT ~ KILOGRAMS
Approved Performance Data
Revised: January, 2013
18 of 28 P/N 101-590010-469
