Daher TBM 850 vs E1000

Side-by-side specs, range, and operating costs.

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Dimensions & configuration

Representative planforms, drawn to shared scale.

Daher TBM 850
41.6 × 34.9 ft 14.3 ft tall
1× Turboprop Retractable Pressurized
E1000
43.0 × 35.8 ft 13.8 ft tall
1× Turboprop Retractable Pressurized

Mission Performance

Stall, approach, cruise, range, ceiling and climb: best values are at the top.

Mission performance specifications
Specification Daher TBM 850E1000
Stall speed 81 kt88 kt
Approach speed 85 kt95 kt
Cruise speed 320 kt333 kt
Range 1520 nm1560 nm
Service ceiling 31000 ft34000 ft
Rate of climb 2005 fpm4000 fpm
Fuel burn 81.0 gph64.0 gph

Each axis is scaled independently across the compared aircraft and printed in its own units; every vertex sits at the published figure. Higher is better on all axes: Stall, Approach and Fuel Burn are inverted (lower = higher). A missing figure breaks the line at that axis.

Flight Profile

Service ceiling, range, and climb rate.

Tap legend to isolate

Arc represents the climb-cruise-descent profile based on published service ceiling and range. Climb rate annotated on ascent. FL180 (18,000 ft) shown for reference.

Fuel Burn & Range

Range, endurance, and what the fuel costs by the hour.

Daher TBM 850 Jet A
81.0 gph
Baseline
1,520 nm range 281 gal usable 4.0 nm/gal $486 fuel/hr 3h 28m endurance
Daher TBM 850: 81.0 gallons per hour at cruise, 1,520 nautical mile published range, 3 hour 28 minute endurance, 4.0 nautical miles per gallon.
E1000 Jet A
64.0 gph
Baseline
1,560 nm range 288 gal usable 5.2 nm/gal $384 fuel/hr 4h 30m endurance
E1000: 64.0 gallons per hour at cruise, 1,560 nautical mile published range, 4 hour 30 minute endurance, 5.2 nautical miles per gallon.
Jet A range each cell = 1 hr of cruise · width scales with speed

Bars show published still-air range. Endurance is usable fuel divided by the published cruise burn. Estimates only. Always verify against the POH.

Runway Performance

Density altitude adjusted estimates

Outside Air Temp
0°F57°F115°F
Field Elevation
SL4,0008,000 ft
Density Altitude

Takeoff over 50 ft obstacle

Landing ground roll

Base distance DA penalty
Scale: 6,000 ft

FAA 10%/1,000 ft DA rule of thumb (FAA-H-8083-25B). Turboprops and jets are less sensitive in practice. Always verify against the POH.

Estimated Operating Costs

Scale:
$1,125 /hr
Baseline
Daher TBM 850: $1,125 per flight hour — fuel $486, maintenance and reserve $639.
E1000 Jet A
$950 /hr
Baseline
E1000: $950 per flight hour — fuel $384, maintenance and reserve $566.
Daher TBM 850 Turboprop
$42,000 /yr Baseline
Daher TBM 850: $42,000 per year — insurance $24,000, hangar $13,000, annual inspection $5,000.
E1000 Turboprop
$94,000 /yr Baseline
E1000: $94,000 per year — insurance $50,000, hangar $24,000, annual inspection $20,000.

Estimates only. Costs vary by location, pilot profile, and market conditions. See individual aircraft pages for source notes.

Capability & limits

Each bar stacks your selected occupants against full fuel and the aircraft's useful-load limit (the black line). The open gap between them is spare payload. Add an occupant and the gap closes; once it's gone, fuel has to give.

lb

+ lb / pax

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1
Daher TBM 850
6 / 6 seats 281 / 281 gal fuel 894 lb wet payload 2,777 lb useful 7,394 lb MTOW
E1000
6 / 6 seats 288 / 288 gal fuel 930 lb wet payload 2,860 lb useful 8,000 lb MTOW

Occupants at 190 + 30 lb each. Fuel at 6.7 lb/gal jet-A, 6.0 lb/gal avgas.

Payload-Range Map

Origin: · two fingers to move map

lb

+ lb / pax

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1

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