Cessna Excel/XLS vs IAI Astra 1125

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

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Dimensions & configuration

Representative planforms, drawn to shared scale.

Cessna Excel/XLS
56 ft × 52 ft ⭥ 17 ft
2× Turbofan Retractable Pressurized
IAI Astra 1125
53 ft × 56 ft ⭥ 18 ft
2× Turbofan Retractable Pressurized

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.

Mission Performance

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

Mission performance specifications
Specification Cessna Excel/XLSIAI Astra 1125
Stall speed 89 kt106 kt
Approach speed 116 kt120 kt
Cruise speed 441 kt459 kt
Range 2100 nm2926 nm
Service ceiling 45000 ft45000 ft
Rate of climb 3790 fpm—
Fuel burn 239.0 gph215.0 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.

Fuel Burn & Range

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

Cessna Excel/XLS Jet A
239.0 gph
Baseline
2,100 nm range 1.8 nm/gal 1,006 gal usable $1,434 fuel/hr 4h 12m endurance
Cessna Excel/XLS: 239.0 gph at cruise, 2,100 nautical mile published range, 4 hour 12 minute endurance, 1.8 nautical miles per gallon.
IAI Astra 1125 Jet A
215.0 gph
Baseline
2,926 nm range 2.1 nm/gal 1,297 gal usable $1,290 fuel/hr 6h 01m endurance
IAI Astra 1125: 215.0 gph at cruise, 2,926 nautical mile published range, 6 hour 1 minute endurance, 2.1 nautical miles per gallon.
Jet A range each cell = 1 hr of cruise · width scales with speed tank-dry · at this cruise burn

Bars show published still-air range: select a cell to view cruise-hours and fuel usage. Endurance is full tank at the displayed cruise burn rate; the extra is reserve and economy margin. 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

Takeoff over 50 ft obstacle

Landing over 50 ft obstacle

Density Altitude

Monte cristo

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

Hourly direct and annual fixed costs

Scale:
Cessna Excel/XLS Jet A
$2,942 /hr
Baseline
Cessna Excel/XLS: $2,942 per flight hour — fuel $1,434, maintenance and reserve $1,508.
IAI Astra 1125 Jet A
$3,030 /hr
Baseline
IAI Astra 1125: $3,030 per flight hour — fuel $1,290, maintenance and reserve $1,740.
Cessna Excel/XLS Turbofan
$19,663 /yr Baseline
Cessna Excel/XLS: $19,663 per year — insurance withheld, hangar $17,163, annual inspection $2,500.
IAI Astra 1125 Turbofan
$0 /yr Baseline
No fixed-cost estimate available

Estimates only. Hourly direct operating cost, based on fuel price and reserves; Annual fixed costs (insurance, hangar, and inspection). Costs vary by location, pilot profile, and market conditions. See individual aircraft pages for source notes.

Capability & limits

Payload vs useful load limit

+ cargo
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1
Cessna Excel/XLS Turbofan
14 / 14 seats cargo 1,006 gal / 1,006 gal fuel 660 lbs wet payload 7,400 lbs useful 20,200 lbs MTOW
IAI Astra 1125 Turbofan
8 / 8 seats cargo 1,297 gal / 1,297 gal fuel 2,010 lbs wet payload 10,700 lbs useful 23,500 lbs MTOW

Shows selected occupants against full fuel, within the aircraft's useful-load limit. Fuel weight at 6.7 lb/gal jet-A, 6.0 lb/gal avgas; pax and luggage are 190 + 30 . Change payload weights in global settings.

Payload-Range Map

Origin: → · two fingers to move map

+ cargo
×
1

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