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Diamond DA-40- 566DS
Specifications may change - Pilots should always check the POH!


Exterior

Specifications

Engine
180 Horsepower

Fuel Capacity
48.0 usable gals. (10.0GPH)

Maximum Speed TAS
140 kts (75% PWR)

Useful Load
889 lbs.
Based on 2646 MTW
MLW 2535

Max Crosswind
20kts

VA = 94-108 KIAS
VFE = 91 KIAS
VX = 64 KIAS

Airport: PAO

Tiedown: U18

Color: white/gray

Hourly Rate: $199 G1000

Year: 2006

Equip: DA-40


Basic Avionics
  • Garmin G-1000 Glass Cockpit (PFD/MFD/GPS/NAV/COMM/TX)
  • AUTOPILOT: KAP 140 Two-axis with Altitude Preselect
  • AUDIO/INTERCOM: Garmin 1347 4 Place
  • TIS: Mode S Traffic Information System
  • Terrain mapping
  • XM Aviator Light Package - METARs/TAFs/TFRs/Nexrad
>>>>> Check for Avionics Manuals <<<<<

Remarks:
48 gal useable fuel, AMSAFE airbags, constant speed prop, 100 - lb. useful load increase (to 889 lb.), extended baggage compartment (takes golf bags and skis) "Great, sturdy, forgiving plane for private or instrument training!"

Specials:
$175 c/o rate 5hr max// $189 blk rate 10 hr min



Weight and Balance

Replace sample weights with your actual weights, then click on the "Calculate" button to see the new takeoff C.G.
Pilots should always calculate the W&B on the ramp prior to takeoff using the latest data from the POH, and taking into account all circumstances including the difference between takeoff and landing fuel quantity and weight.

Empty Wt
1756.77
Empty CG
96.74
MGTW
2646
MRW
2646
MLW
2535
Item Weight Arm Moment
Empty Weight
Front Seats
Rear Seats
Baggage
Fuel (6 lbs./gal.)
Totals
   
Takeoff C.G.   
  


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