```PERFORMANCE B-767/300
• CURSO DE REFRESCO
PERFORMANCE DE EQUIPO B-767-300
• Instructor : Hugo Montes E.
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PERFORMANCE B-767/300
• MOTORES :
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G/E CF6-80C2B6F
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2 + 1 = 3 KTS
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SXXX
FIELD LENGTH (FT) 12000
CLEARWAY……. 1200 FT.
STOPWAY …… 1000 FT.
NORMAL V1 …. 140 KIAS
CLEARWAY MINUS STOPWAY
800 FT. - 1000 FT = - 200
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SPIM RWY 15 A/C OFF T° 30° C WIND CALM
STANDING WATER 6mm.
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SPIM RWY 15 A/C OFF T° 30° C WIND CALM
STANDING WATER 6mm.
189.4 - 22.3 = 167.1
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Maximum Reverse Thrust
Revisar Tabla a usar
No Reverse Thrust
V1 = 154-17 = 137kts
VR
=
160kts
V2 =
166kts .
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• HACER COMPARACIÒN CON OPT.
• DATOS:
MATRICULA CC-CZW-W
SPIM - RWY 15- T 30G C - WIND CALM
QNH 29.94
A/C OFF - FLAPS 5
STANDING WATER 6 m.m.
. ANTI/ICE OFF
C.G STD
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V1 (MCG) LIMIT WEIGHT .Is the maximun weight at which the airplane can accelerate to V1(MCG) speed and
still stop within the field lenght available for the reported braking action.
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SPIM
TEMPERATURE 30° C
20 KTS
LANDING WEIGHT 140,000 KGS.
VREF 30
+10 KTS
BRAKING CONF. AUTOBRAKE 3
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SPIM
TEMP. 30° C
20 KTS
LANDING WEIGHT 140,000 KGS.
VREF +10 KTS - NO REVERSES
ANTI-SKID OFF (FLAPS 30°)
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SPIM MEDIUM REPORTED BRAKING ACTI.
LANDING WEIGHT ……………….. 140,000 KGS.
VREF30 … +10 KTS TEMP….. 30° C
ANTI-SKID OFF (FLAPS 30°)
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DRIFTDOWN SPEED / LEVEL OFF ALTITUDE
LEVEL OFF
OPTIM. DRIFTDOWN
SPEED
M.C.T.
L.R.C.
Engine INOP
B
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LONG RANGE CRUISE DIVERSION FUEL AND TIME
LEVEL OFF
L.R.C.
Engine INOP
B
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PERFORMANCE B-767/300
LONG RANGE CRUISE DIVERSION FUEL AND TIME.
• Tables are provided for crews to determine the fuel and time
required to proceed to an alternate airfield with one engine
inoperative. The data is based on single engine Long Range
Cruise speed and .78/290/250 descent.
Enter with Air Distance as determined from the Ground to Air
Miles Conversion table and read Fuel and Time required at
the cruise pressure altitude. Adjust the fuel obtained for
deviation from the reference weight at checkpoint as
required by entering the Fuel Required Adjustment table
with the fuel required for the reference weight and the actual
weight at checkpoint.
Read fuel and time required for the actual weight.
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GEAR DOWN/ENGINE INOP.
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SPIM A/C 0N RWY. 15 / T° 26° C / WIND CALM
ANTI-SKID INOPERATIVE
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188,300 kgs. 22,700 kgs.
165,600 kgs.
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V1….. 158 - 31 = 127 Kts.
Vr…………………………158 Kts.
V2……………… ………..163 Kts.
188,300 kgs. 22,700 kgs.
165,600 kgs.
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• HACER COMPARACIÒN CON OPT.
• DATOS:
MATRICULA CC-CZW-W
SPIM - RWY 15- T 30G C - WIND CALM
QNH 29.94
A/C OFF - FLAPS 5
. ANTI/ICE OFF
C.G STD
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PERFORMANCE B-767/300
•
COMO PODRÁN APRECIAR EN LOS ANALISIS DE PISTA DE MEJICO POR EJEMPLO
POR LA PISTA 05L CON 20° DE OAT FLAPS 5 DA LOS SIGUIENTES PESOS Y
1. STANDARD .. 153,400 KGS.
V1 152 / VR 153 / V2 158.
2. ALTERNO 1.. 155,500 KGS.
V1 151 / VR 152 / V2 156.
3. ALTERNO 2 .. 156,200 KGS.
V1 150 / VR 151 / V2 156.
•
ASIMISMO ESTOS C.G AUTORIZADOS CORRESPONDEN A LIMITES DELANTEROS DE
20% MAC (ALT. 1 FWD CG LIMIT FOR T.O), O DEL 25% MAC ( ALT. 2 FWD CG LIMIT
FOR T.O).
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“A”
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PESO ACTUAL PARA
T.O
160,000 KGS.
MÁXIMA TEMPERATURA
ASUMIDA 50° C
V1 = 156
VR = 156
V2 = 161
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PESO ACTUAL PARA T.O
160,000 KGS.
MÁXIMA TEMPERATURA
ASUMIDA 54° C
V1 = 152
VR = 156
V2 = 161
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PERFORMANCE B-767/300
MUCHAS GRACIAS .
Hugo Montes Espinoza
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