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Flight Manual Continental Rev. 11/15/02 #41
Takeoff in Icing Conditions
Normal operating procedures limit the use of wing anti-ice to altitudes above
800 feet AGL and do not require takeoff penalties when so limited. Engine antiice
is often required on takeoff and requires a reduction of the Runway Limit
Weight and the Climb Limit Weight. If engine anti-ice is required for takeoff,
these reductions are taken by ACCULOAD and noted in LINE 9 RMKS. If
ACCULOAD is not available, reduce the Runway Limit Weight and the Climb
Limit Weight as shown in the following correction charts.
>>
FLAP ENGINE ANTI-ICE DECREMENT LB
POSITION RUNWAY CLIMB LIMIT CLIMB LIMIT
LIMIT PA £ = 8000 FT PA > 8000 FT
1, 5,OR 15 400 450 900
@
FLAP ENGINE ANTI-ICE DECREMENT LB
POSITION RUNWAY CLIMB LIMIT CLIMB LIMIT
LIMIT PA £ = 8000 FT PA > 8000 FT
5 700 375 825
15 700 325 725
BCD
FLAP ENGINE ANTI-ICE DECREMENT LB
POSITION RUNWAY CLIMB LIMIT CLIMB LIMIT
LIMIT PA £ = 8000 FT PA > 8000 FT
1, 5, OR 15 300 300 300
Note: The above corrections are not runway specific and represent the most
conservative conditions. ACCULOAD can calculate Anti-Ice
corrections for a specific runway and conditions, which may provide a
lower weight reduction. Use ACCULOAD data if available.
Sec. 5 Page 34 737
Rev. 11/15/02 #41 Continental Flight Manual
Anti-Skid Inoperative
For takeoff with the anti-skid sytem inoperative the Runway Limit Weight and
V1 for that limiting weight must be reduced to allow for the resulting adverse
effect on accelerate-stop performance. ACCULOAD will adjust the Runway
Limit weight and V speeds for the anti-skid inoperative condition. If this weight
is limiting for takeoff, it will be found on line 8 (MAX GTOW-) of the pilot
weight manifest followed by the code “R” for runway limited. ACCULOAD
will calculate proper V Speeds for the Anti-Skid inoperative condition. In the
absence of ACCULOAD, use the following procedure.
Procedure For Departures With Anti-Skid Inoperative Without
ACCULOAD:
1. Reduce the Runway Limit Weight found in the Runway Analysis by the
following amounts for the indicated series aircraft:
>>: 15,500 lbs.
@: 16,500 lbs.
B: 17,200 lbs.
C: 18,700 lbs.
D: 18,000 lbs.
2. Determine the V1 for the adjusted runway limit weight and reduce this V1
by the amount shown in the ANTI-SKID INOPERATIVE V1
DECREMENT table for the appropriate series aircraft.
3. Compare this adjusted runway limit V1 to Vmcg.
· If this V1 is equal to or greater than Vmcg then skip to step 4 below.
· If this V1 is less than Vmcg and the runway is 7900 feet or longer, then
set V1 equal to Vmcg and obtain Vr and V2 from the published V speed
charts.
· If this V1 is less than the published Vmcg and the runway is less than
7900 feet, takeoff is not authorized.
4. Compare the adjusted V1 to the actual gross weight V1 and use the lesser of
the two. Obtain Vr and V2 from the published V speed charts.
Note: If the actual gross weight V1 is used, and it is less than Vmcg, set V1
equal to Vmcg.
737 Sec. 5 Page 35
Flight Manual Continental Rev. 11/15/02 #41
>>
ANTI-SKID INOPERATIVE V1 DECREMENTS
FIELD LENGTH V1 REDUCTION - KTS
6,000
8,000
27
22
10,000
12,000
14,000
17
14
11
@
ANTI-SKID INOPERATIVE V1 DECREMENTS
FIELD LENGTH V1 REDUCTION - KTS
6,000
8,000
31
24
10,000
12,000
14,000
19
15
12
B
ANTI-SKID INOPERATIVE V1 DECREMENTS
FIELD LENGTH V1 REDUCTION - KTS
6,000
8,000
18
14
10,000
12,000
14,000
12
10
8
C
ANTI-SKID INOPERATIVE V1 DECREMENTS
FIELD LENGTH V1 REDUCTION - KTS
6,000
8,000
20
16
10,000
12,000
14,000
14
12
11
D
ANTI-SKID INOPERATIVE V1 DECREMENTS
FIELD LENGTH V1 REDUCTION - KTS
6,000
8,000
19
15
10,000
12,000
14,000
13
11
10
Sec. 5 Page 36 737
Rev. 11/15/02 #41 Continental Flight Manual
Anti-Skid Inoperative Example
Determine the proper V Speeds for the (>>) anti-skid inoperative takeoff
below:
From Runway Analysis data:
Runway Length 32R 12,001 ft.
Actual Takeoff Weight 113,850 lbs.
Runway Limit Weight 143,800 lbs.
1. Runway Limit Weight is ------------ 143,800 lbs.
Weight adjustment (>>) ----------- 15,500 lbs.
Adjusted Runway Limit Weight ---- 128,300 lbs.
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