Hello everyone,
I'm working on a file regarding calculating landing distance. Here is the data for example:
Data:
Landing Weight = 59,400 kg
Pressure altitude = 3,000 ft
Temperature = 30C
Landing configuration = FULL
Brake Mode = Manual
Approach speed = VLS + 8 kt
Slope = -0.07%
Runway Condition = Dry
Both Reversers = Yes
In Cells B2:C10 contains the data mentioned above.
In Cells C22:K32 contains the Corrections on Landing Distance for a Dry runway and similar data for Good runway in Cells C38:K48.
In Cells C36:K36 contains the calculation results based on the data in Cells B2:C20 and Cell G3 where finally Cell M36 displays the final result.
What I'm trying to do is have a formula in Cells E36:K36 that calculates the data from Cells B2:D20 with the data in Cells C22:K32. If you take a look at Cells C36:K36 for example, you can see some of the formulas I have going. I just have a little problem with Cell G36:H36 and Cell J36 in terms of coming up with the formula I need. I think the Forecast and Offset function are the ones that are going to work but not sure.
Basically, based on the result in Cell B18 and C18, I would take whichever value is higher, in this case 8 and apply the rule in Cell G25 & G27. So it should look like this if using manual brake mode with full configuration: 2 x 60 = 120. Technically 1.5 (1.5 x 60 = 90) because my higher value in Cell C18 is 8, not 10. If Cell C18 was 10, then it be 2 x 60 or if Cell C18 was 3, then the value from Cell B18 would apply which then be 1 x 60. In other words, how many per 5 kt do I have in Cell C18, 2 or 1.5??
I'm working on a file regarding calculating landing distance. Here is the data for example:
Data:
Landing Weight = 59,400 kg
Pressure altitude = 3,000 ft
Temperature = 30C
Landing configuration = FULL
Brake Mode = Manual
Approach speed = VLS + 8 kt
Slope = -0.07%
Runway Condition = Dry
Both Reversers = Yes
In Cells B2:C10 contains the data mentioned above.
In Cells C22:K32 contains the Corrections on Landing Distance for a Dry runway and similar data for Good runway in Cells C38:K48.
In Cells C36:K36 contains the calculation results based on the data in Cells B2:C20 and Cell G3 where finally Cell M36 displays the final result.
What I'm trying to do is have a formula in Cells E36:K36 that calculates the data from Cells B2:D20 with the data in Cells C22:K32. If you take a look at Cells C36:K36 for example, you can see some of the formulas I have going. I just have a little problem with Cell G36:H36 and Cell J36 in terms of coming up with the formula I need. I think the Forecast and Offset function are the ones that are going to work but not sure.
Basically, based on the result in Cell B18 and C18, I would take whichever value is higher, in this case 8 and apply the rule in Cell G25 & G27. So it should look like this if using manual brake mode with full configuration: 2 x 60 = 120. Technically 1.5 (1.5 x 60 = 90) because my higher value in Cell C18 is 8, not 10. If Cell C18 was 10, then it be 2 x 60 or if Cell C18 was 3, then the value from Cell B18 would apply which then be 1 x 60. In other words, how many per 5 kt do I have in Cell C18, 2 or 1.5??
Landing distance.xlsx | ||||||||||||||||
---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
A | B | C | D | E | F | G | H | I | J | K | L | M | N | |||
1 | ||||||||||||||||
2 | LDG weight | 59400 | Weight Correction | 6600 | kgs | |||||||||||
3 | elevation | 3000 | -660 | meters | ||||||||||||
4 | Temp | 30 | ||||||||||||||
5 | LDG CONF | Full | ||||||||||||||
6 | Brake mode | Manual | Safety Factor | |||||||||||||
7 | Slope | -0.7 | 1.15 | |||||||||||||
8 | RWY COND | Dry | ||||||||||||||
9 | Both Rev working | Yes | ||||||||||||||
10 | ||||||||||||||||
11 | ||||||||||||||||
12 | Vapp Correction | |||||||||||||||
13 | 5 KT | 1/3 headwind (excluding gust) max = 15 kt | Required Landing Distance | |||||||||||||
14 | 808.45 | |||||||||||||||
15 | ||||||||||||||||
16 | ||||||||||||||||
17 | Whichever is Higher | |||||||||||||||
18 | 5 | 8 | ||||||||||||||
19 | ||||||||||||||||
20 | ISA DEV | 21 | 2.1 | 63 | ||||||||||||
21 | ||||||||||||||||
22 | Dry | |||||||||||||||
23 | Corrections on Landing Distance | Weight | Vapp SPEED | Altitude | Temp | Slope | Reversers | |||||||||
24 | ||||||||||||||||
25 | Brake Mode | LDG CONF | Ref Dist (m) for 66T | Per 1T below 66T | Per 5kt | Per 1000ft above SL | Per 10°C above ISA | Per 1% Down Slope | Per Reverser Working | -20 | ||||||
26 | ||||||||||||||||
27 | Manual | Conf 3 | 1130 | -10 | 80 | 50 | 40 | 20 | -20 | |||||||
28 | Manual | Full | 1080 | -10 | 60 | 40 | 30 | 20 | -20 | |||||||
29 | AB MED | Conf 3 | 1420 | -10 | 100 | 50 | 50 | 10 | 0 | |||||||
30 | AB MED | Full | 1360 | -10 | 90 | 50 | 40 | 10 | 0 | |||||||
31 | AB LOW | Conf 3 | 2030 | -10 | 150 | 80 | 70 | 30 | -10 | |||||||
32 | AB LOW | Full | 1930 | -10 | 130 | 80 | 60 | 20 | -10 | |||||||
33 | ||||||||||||||||
34 | Braking Mode | LDG CONF | Ref Dist (m) for 66T | Per 1T below 66T | Per 5kt | Per 1000ft above SL | Per 10°C above ISA | Per 1% Down Slope | Per Thrust Reverser Ops | Final | ||||||
35 | result | |||||||||||||||
36 | Manual | Full | 1080 | -660 | 120 | 120 | 63 | 20 | -40 | 808.45 | ||||||
37 | ||||||||||||||||
38 | Good | |||||||||||||||
39 | Corrections on Landing Distance | Weight | Vapp SPEED | Altitude | Temp | Slope | Reversers | |||||||||
40 | ||||||||||||||||
41 | Brake Mode | LDG CONF | Ref Dist (m) for 66T | Per 1T below 66T | Per 5kt | Per 1000ft above SL | Per 10°C above ISA | Per 1% Down Slope | Per Reverser Working | |||||||
42 | ||||||||||||||||
43 | Manual | Conf 3 | 1480 | -20 | 120 | 80 | 70 | 60 | -60 | |||||||
44 | Manual | Full | 1370 | -10 | 100 | 70 | 60 | 40 | -50 | |||||||
45 | AB MED | Conf 3 | 1540 | -20 | 120 | 80 | 70 | 60 | -30 | |||||||
46 | AB MED | Full | 1420 | -10 | 110 | 70 | 60 | 40 | -10 | |||||||
47 | AB LOW | Conf 3 | 2030 | -20 | 150 | 80 | 70 | 30 | -10 | |||||||
48 | AB LOW | Full | 1930 | -10 | 130 | 80 | 60 | 20 | -10 | |||||||
49 | ||||||||||||||||
50 | Braking Mode | LDG CONF | Ref Dist (m) for 66T | Per 1T below 66T | Per 5kt | Per 1000ft above SL | Per 10°C above ISA | Per 1% Down Slope | Per Thrust Reverser Ops | Final | ||||||
51 | result | |||||||||||||||
52 | Manual | Full | 1370 | -660 | 100 | 210 | 126 | 40 | -100 | 1248.9 | ||||||
53 | ||||||||||||||||
54 | ||||||||||||||||
55 | ||||||||||||||||
Sheet3 |
Cell Formulas | ||
---|---|---|
Range | Formula | |
G2 | G2 | =66000-C2 |
G3 | G3 | =G2*F27/100 |
G14 | G14 | =M36 |
C20 | C20 | =C4-(15-2*(C3/1000)) |
D20 | D20 | =C20/10 |
F20 | F20 | =INDEX(I27:I32,MATCH(1,INDEX((C36=C43:C48)*(D36=D27:D32),0,1),0))*D20 |
M25 | M25 | =INDEX(K27:K32,MATCH(1,INDEX((C36=C43:C48)*(D36=D27:D32),0,1),0)) |
C36 | C36 | =C6 |
D36 | D36 | =C5 |
E36 | E36 | =INDEX(E27:E32,MATCH(1,INDEX((C36=C43:C48)*(D36=D27:D32),0,1),0)) |
F36 | F36 | =INDEX(F27:F32,MATCH(1,INDEX((C36=C43:C48)*(D36=D27:D32),0,1),0))*G2/100 |
H36,H52 | H36 | =H28*3 |
I36 | I36 | =INDEX(I27:I32,MATCH(1,INDEX((C36=C43:C48)*(D36=D27:D32),0,1),0))*D20 |
K36 | K36 | =IF(C9="Yes",M25*2,IF(C9="No",M25*1,0)) |
M36 | M36 | =SUM(E36:K36)*G7 |
C52 | C52 | =C6 |
D52 | D52 | =C5 |
E52 | E52 | =INDEX(E43:E48,MATCH(1,INDEX((C52=C43:C48)*(D52=D27:D32),0,1),0)) |
F52 | F52 | =INDEX(F43:F48,MATCH(1,INDEX((C36=C43:C48)*(D36=D27:D32),0,1),0))*G2/100 |
G52 | G52 | =G44 |
I52 | I52 | =INDEX(I43:I48,MATCH(1,INDEX((C36=C43:C48)*(D36=D27:D32),0,1),0))*D20 |
K52 | K52 | =K44*2 |
M52 | M52 | =SUM(E52:K52)*G7 |
Cells with Data Validation | ||
---|---|---|
Cell | Allow | Criteria |
C5 | List | =$P$2:$P$4 |
C6 | List | =$O$2:$O$5 |
C8 | List | =$Q$2:$Q$4 |
C9 | List | =$R$2:$R$4 |