DOC AIRBUS | MMEL OPS PROCSpoiler 1 or 3
| 27-64-02A | Spoiler 1 or 3 |
|---|
Applicable to: -
- Flight preparation/limitations
The following
penalties may be used for takeoff and landing performance determination
if no takeoff and landing data (predetermined by using OCTOPUS program
or other equivalent program with present failure case) is available.
Takeoff performance computation:
| WARNING: | Do not use this method for
takeoff on wet or contaminated runways. |
Determine the Maximum Takeoff
Weight and associated speeds in normal conditions on dry runway.
Decrease the Maximum Takeoff Weight by 800 kg ( 1770 lb).
Decrease V1, VR, and V2 by 1 kt.
If the actual TOW is lower than the MTOW calculated using above method:
The speeds determined
without failure and associated with the actual TOW may
be retained provided they are all lower than the speeds calculated
using above method.
Check that the corrected V1 is equal to or above the minimum V1 value shown
on the RTOW chart (due to VMCG limitation).
If the corrected V1 is lower than the minimum V1:
Take this last value as V1
Further decrease the
weight by 3000 kg ( 6600 lb) per kt difference between both values.
Check that the corrected VR is equal to or above the minimum VR value shown
on the RTOW chart (due to VMCA limitation).
If the corrected VR is lower than the minimum VR:
Takeoff is not possible using this method.
Check that the corrected V2 is equal to or above the minimum V2 value shown
on the RTOW chart (due to VMCA limitation).
If the corrected V2 is lower than the minimum V2:
Takeoff is not possible using this method.
Check that the corrected V2 is equal to or above the minimum V2 due to VMU limitation. ( Refer to FCOM)
If the corrected V2 is lower than the minimum V2:
Takeoff is not possible using this method.
Landing performance computation:
Multiply the landing distances by 1.10.
- After engine start
On the HYD SD Page,
check the absence of amber data.
- For takeoff
If the above method was used for takeoff performance determination:
Perform the takeoff
using full thrust (TOGA).
| 27-64-02A | Spoiler 1 or 3 |
|---|
Applicable to: -
- Flight preparation/limitations
The following
penalties may be used for takeoff and landing performance determination
if no takeoff and landing data (predetermined by using OCTOPUS program
or other equivalent program with present failure case) is available.
Takeoff performance computation:
| WARNING: | Do not
use this method for takeoff on wet or contaminated runways. |
Determine the Maximum Takeoff
Weight and associated speeds in normal conditions on dry runway.
Decrease the Maximum Takeoff Weight by 800 kg ( 1770 lb).
Decrease V1 by 1 kt. Keep VR and V2
unchanged.
If the actual TOW is lower than the MTOW calculated using above method:
The speeds determined
without failure and associated with the actual TOW may
be retained provided they are all lower than the speeds calculated
using above method.
Check that the corrected V1 is equal to or above the minimum V1 value shown
on the RTOW chart (due to VMCG limitation).
If the corrected V1 is lower than the minimum V1:
Take this last value as V1
Further decrease the
weight by 3000 kg ( 6600 lb) per kt difference between both values.
Landing performance computation:
Multiply the landing distances by 1.05.
- After engine start
On the HYD SD Page,
check the absence of amber data.
- For takeoff
If the above method was used for takeoff performance determination:
Perform the takeoff
using full thrust (TOGA).
| 27-64-02A | Spoiler 1 or 3 |
|---|
Applicable to: -
- Flight preparation/limitations
Takeoff performance computation:
The takeoff performance must be determined by using OCTOPUS program
or other equivalent program with present failure case taken into account.
Launch PEP.
Landing
performance computation
Multiply the landing distances by 1.05.
- After engine start
On the HYD SD Page,
check the absence of amber data.
| 27-64-02A | Spoiler 1 or 3 |
|---|
Applicable to: -
- Flight Preparation/Limitations
Takeoff performance computation:
The takeoff performance must be determined
by using OCTOPUS program or other equivalent program with present
failure case taken into account.
Launch PEP.
Landing
performance computation
Multiply the landing distances by 1.10.
- After Engine Start
On the HYD SD Page,
check the absence of amber data.