This online tool can be used to calculate the mass and balance distribution for G-ASWX
only (S/N 28-1932). The figures used in this calculator are not applicable to any other aircraft, even for
those of the same type and model. The operating envelope is defined i.a.w. US 2A13 TCDS (see CAA Product List for approval) & AFM VB-38.
Legal Disclaimer: This calculator has not been certified by any
governing body. Use at your own risk and assume all data incorrect until validated by you.
Notes:—The following aerobatic manoeuvres are permitted within the Utility Envelope:Spins, steep turns, lazy eights and chandelles.
This online tool can be used to calculate the takeoff distance required for PA-28-180 aircraft, S/N 28-1761 thru 28-3149 only. The performance data has been digitally extracted from Figure V-5 of the approved Aircraft Flight Manual VB-38 and uses interpolation to derive a result. The takeoff distance required is from rest to 50ft, with flaps up and rotation initiated at 70 KIAS.
Legal Disclaimer: This calculator has not been certified by any
governing body. Use at your own risk and assume all data incorrect until validated by you. Safety factors are taken from AFM VB-38. For more guidance on safety factors see CAA Safety Sense Leaflet 09.
Calculation Results
| Result from graph: | |
|---|---|
| Correction for grass: | N/A |
| Conversion ft to m: | x 0.3048 |
| Takeoff Run Required (TORR): | |
| Takeoff Distance Required (TODR): |
Notes:1.The takeoff run will not exceed, and has been taken as, 64% of the takeoff distance required.2.The measured takeoff distance has been factored by 1.25, to obtain the scheduled takeoff distance required, and the measured takeoff run by 1.15.3.The wind correction curves are factored so that 50% of headwinds and 150% of tailwinds are obtained. Reported winds may therefore be used directly in the graph.
Reference document AFM VB-38 Rev. 19, 1st May 1986
