Presentation is loading. Please wait.

Presentation is loading. Please wait.

10/05/20151 H.M.E.1 CURSO DE REFRESCO PERFORMANCE DE EQUIPO B-767-300 Instructor : Hugo Montes E. PERFORMANCE B-767/300.

Similar presentations


Presentation on theme: "10/05/20151 H.M.E.1 CURSO DE REFRESCO PERFORMANCE DE EQUIPO B-767-300 Instructor : Hugo Montes E. PERFORMANCE B-767/300."— Presentation transcript:

1

2 10/05/20151 H.M.E.1 CURSO DE REFRESCO PERFORMANCE DE EQUIPO B Instructor : Hugo Montes E. PERFORMANCE B-767/300

3 10/05/20152 H.M.E.2 DIAPOSITIVAS PRESENTADAS A BASE: MOTORES : G/E CF6-80C2B6F PERFORMANCE B-767/300

4 10/05/20153 H.M.E.3

5 10/05/2015H.M.E = 3 KTS

6 10/05/20155 SXXX FIELD LENGTH (FT) CLEARWAY…… FT. STOPWAY …… 1000 FT. NORMAL V1 …. 140 KIAS CLEARWAY MINUS STOPWAY 800 FT FT = - 200

7 10/05/20156

8 7 H.M.E.7 SPIM RWY 15 A/C OFF T° 30° C WIND CALM STANDING WATER 6mm.

9 10/05/20158 H.M.E.8

10 10/05/20159 H.M.E.9 SPIM RWY 15 A/C OFF T° 30° C WIND CALM STANDING WATER 6mm = 167.1

11 10/05/ /05/2015H.M.E.10

12 10/05/ /05/2015H.M.E.11 Maximum Reverse Thrust No Reverse Thrust Revisar Tabla a usar V1 = = 137kts VR = 160kts V2 = 166kts.

13 10/05/2015H.M.EH.M.E.12 HACER COMPARACIÒN CON OPT. DATOS: MATRICULA CC-CZW-W SPIM - RWY 15- T 30G C - WIND CALM QNH A/C OFF - FLAPS 5 STANDING WATER 6 m.m.. ANTI/ICE OFF C.G STD

14 10/05/ /05/2015H.M.E.13

15 10/05/ /05/2015H.M.E.14

16 10/05/2015H.M.E.15 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.

17 10/05/ /05/2015H.M.E.16

18 10/05/201517

19 10/05/ /05/2015H.M.E.18

20 10/05/2015H.M.E.19

21 10/05/ /05/201520H.M.E.

22 10/05/ /05/201521H.M.E.

23 10/05/ /05/201522H.M.E.

24 10/05/ /05/2015H.M.E.23

25 10/05/ /05/2015H.M.E.24

26 10/05/ /05/2015H.M.E.25

27 10/05/ /05/2015H.M.E.26

28 10/05/ /05/2015H.M.E.27

29 10/05/ SPIM TEMPERATURE 30° C HEADWIND 20 KTS LANDING WEIGHT 140,000 KGS. VREF KTS BRAKING CONF. AUTOBRAKE 3

30 10/05/201529

31 10/05/201530

32 10/05/ SPIM TEMP. 30° C HEADWIND 20 KTS LANDING WEIGHT 140,000 KGS. VREF +10 KTS - NO REVERSES ANTI-SKID OFF (FLAPS 30°)

33 10/05/201532

34 10/05/ /05/2015H.M.E.33 SPIM MEDIUM REPORTED BRAKING ACTI. HEADWIND……………………………. 20 KTS LANDING WEIGHT ……………….. 140,000 KGS. VREF30 … +10 KTS TEMP….. 30° C ANTI-SKID OFF (FLAPS 30°)

35 10/05/ /05/2015H.M.E.34

36 10/05/ /05/2015H.M.E.35

37 10/05/ /05/2015H.M.E.36

38 10/05/ /05/2015H.M.E.37

39 10/05/ /05/2015H.M.E.38

40 10/05/201539

41 10/05/ /05/2015H.M.E.40

42 10/05/ /05/2015H.M.E.41

43 10/05/ A B M.C.T. L.R.C. Engine INOP.78/290/250 LEVEL OFF OPTIM. DRIFTDOWN SPEED DRIFTDOWN SPEED / LEVEL OFF ALTITUDE 10/05/201542H.M.E.

44 10/05/ /05/2015H.M.E.43

45 10/05/ A B L.R.C. Engine INOP.78/290/250 LONG RANGE CRUISE DIVERSION FUEL AND TIME.78/290/250 LEVEL OFF D C 10/05/201544H.M.E.

46 10/05/ /05/2015H.M.E.45 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. PERFORMANCE B-767/300

47 10/05/2015H.M.E.46

48 10/05/2015H.M.E.47

49 10/05/2015H.M.E.48

50 10/05/2015H.M.E.49

51 10/05/2015H.M.E.50

52 10/05/2015H.M.E.51

53 10/05/2015H.M.E.52 GEAR DOWN/ENGINE INOP.

54 10/05/2015H.M.E.53

55 10/05/ /05/2015H.M.E.54 SPIM A/C 0N RWY. 15 / T° 26° C / WIND CALM ANTI-SKID INOPERATIVE

56 10/05/ /05/2015H.M.E.55

57 10/05/ /05/2015H.M.E ,300 kgs. - 22,700 kgs. 165,600 kgs.

58 10/05/ /05/2015H.M.E.57 V1… = 127 Kts. Vr…………………………158 Kts. V2……………… ………..163 Kts. 188,300 kgs. - 22,700 kgs. 165,600 kgs.

59 10/05/2015H.M.EH.M.E.58

60 10/05/ /05/2015H.M.E.59

61

62

63

64 10/05/2015H.M.EH.M.E.63 HACER COMPARACIÒN CON OPT. DATOS: MATRICULA CC-CZW-W SPIM - RWY 15- T 30G C - WIND CALM QNH A/C OFF - FLAPS 5. ANTI/ICE OFF C.G STD

65 10/05/2015H.M.E.64

66 10/05/2015H.M.E.65

67 10/05/2015H.M.E.66

68 10/05/2015H.M.E.67

69 10/05/2015H.M.E.68

70 10/05/2015H.M.E.69

71 10/05/2015H.M.E.70

72 10/05/2015H.M.E.71

73 10/05/2015H.M.E.72

74 10/05/2015H.M.E.73

75 10/05/2015H.M.E.74

76 10/05/ /05/2015H.M.E.75

77 10/05/ /05/2015H.M.E.76 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 VELOCIDADES: 1.STANDARD.. 153,400 KGS. V1 152 / VR 153 / V ALTERNO ,500 KGS. V1 151 / VR 152 / V ALTERNO ,200 KGS. V1 150 / VR 151 / V 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). PERFORMANCE B-767/300

78 10/05/2015H.M.E.77 “A”

79 10/05/ /05/2015H.M.E.78 PESO ACTUAL PARA T.O 160,000 KGS. V1 = 156 VR = 156 V2 = 161 MÁXIMA TEMPERATURA ASUMIDA 50° C

80 10/05/ /05/2015H.M.E.79 PESO ACTUAL PARA T.O 160,000 KGS. V1 = 152 VR = 156 V2 = 161 MÁXIMA TEMPERATURA ASUMIDA 54° C

81 10/05/2015H.M.EH.M.E.80

82 10/05/2015H.M.EH.M.E.81

83 10/05/ /05/2015H.M.E.82 MUCHAS GRACIAS. Hugo Montes Espinoza PERFORMANCE B-767/300


Download ppt "10/05/20151 H.M.E.1 CURSO DE REFRESCO PERFORMANCE DE EQUIPO B-767-300 Instructor : Hugo Montes E. PERFORMANCE B-767/300."

Similar presentations


Ads by Google