PUMA FLIGHT PLANNING
FOR INFORMATION ONLY. Check max. Gross Mass.

Helicopter & Configuration

Set automatically per aircraft; toggle if the database value is wrong.

Loading

kg
kg
kg
× 7.6

Additional Equipment

Mass is added to Equipment below.

Result

BEM–
Equipment–
Crew + Pax/Cargo + Fuel–
Gross Mass–
Max. Gross Mass (9000 kg)
Calculations with MPAI closed.

Conditions

hPa
°C

Hover Ceilings (TOP)

HOGE TOP–
HIGE TOP–

OEI Ceilings

OEI Ceiling (no ICE)–
OEI Ceiling (with ICE)–
OEI HIGE–

Climb Gradient OEI (%)

2000 ft4000 ft6000 ft
no ICE–––
with ICE–––

VNE & Max Gross Mass

VNE at altitude–
Max Gross Mass — HOGE TOP–
Max Gross Mass — HIGE TOP–
ft

H/V Diagram Point A

ft
H/V Diagram Point A–
Flight rules

Route

Coordinates
Altitude

Fuel & Mass Setup

kg
kg/h
kt
°
kt
min
min
kg
kg
kg
Total distance0 NM
Total time enroute00:00
Trip fuel0 kg
Min. fuel required (trip+cont+reserve+taxi+alt)0 kg
Fuel remaining at destination–

Map

Inside Switzerland: swisstopo colour map with aviation-obstacle and military layers. Outside: OpenStreetMap. Requires internet.

Export / Import Route

For Info only — use Device in Landscape Format. This Operational Flight Plan is generated from the Nav page.
Puma — Operational Flight Plan
–
Total distance0 NM
Total time enroute00:00
Calculations with MPAI closed.
For Info only — use Device in Landscape Format. Performance is computed at each landing point's altitude and the gross mass at that point.
Puma — OFP Performance per Landing Point
QNH 1013 · ISA 0 °C
Add landing points (LZ / Heliport) on the Nav page to see performance here.