De Havilland DH82a Tiger
Moth
REFERENCE
INFORMATION
NOT FOR OPERATIONAL PURPOSES
For detailed instructions on how to fly this aircraft, see the Aircraft
Information
articles in the
Maximum gross aircraft weight with full fuel |
1,825 lbs |
Aircraft
Aerobatic Weight Limit |
1,750
lbs |
Aircraft
Empty Weight |
1,127
lbs |
Crew |
2 |
Fuel
(Capacity) |
22.8 US
Gal 86
litres |
|
300
Miles |
Max Rate
Of Climb: MTOW: |
|
Service
Ceiling |
14,000ft
AMSL |
Powerplant |
1 x DH
Gipsy Major 1. |
Propeller |
Wooden
Fixed Pitch. 6ft 4 in Diameter. |
NOTE: To adjust fuel load, on the Aircraft menu, click Fuel
and Load.
Maximum Level Speed |
95 KTAS//109 MPH |
Aerobatic entry speed |
90 - 95 KIAS |
Cruise @ 2100 RPM |
80 KTAS//93MPH |
VNE - Never Exceed Speed |
148 KIAS |
VS - Stalling Speed (max weight, flaps up) |
35 KIAS |
VSO - Stalling Speed in Landing Configuration |
35 KIAS |
VX - Best Angle-of-Climb Speed (sea level) |
50 KIAS |
VY - Best Rate-of-Climb Speed (sea level) |
58 KIAS |
Best Glide Speed |
50 KIAS |
Maximum Flap Placard
Speeds
Flaps degrees |
KIAS |
Upper Wing Slat |
Automatic extension based on Angle of Attack.For Aerobatics lock slats,use the / key |
NOTE: For explanations of speeds used on this tab, see "V-speeds" in the Learning Center Glossary.