2023 Aquila A211
Single Engine Piston
FOR SALEAircraft Details
Seller reportedDescription
ENGINE:
Bombardier Rotax 912S
Cylinders 4
Rated power 100 HP 73,5 kW
Max. take off power and max. continuous power A211 95 HP 69 kW
TBO 2.000 h 15 years
PROPELLER:
MT-Propeller 2-blade constant-speed-propeller MTV-21-A/170-05, TBO 2.000 h/ 6 years
PERFORMANCE:
Max. speed 165 kts 190 mph
Max. level speed, MSL 130 kts 150 mph
75%
5.000 ft
ISA 55%
5.000 ft
ISA
Speed (TAS) 121 kts 140 mph 103 kts 118 mph
Range (+ 45 min rsv) 535 NM 615 mi. 620 NM 715 mi.
Endurance (+ 45 min rsv) 4:30 hrs 6:05 hrs
Fuel-flow 21,5 ltr/h 5.7 gph 16,6 ltr/h 4.36 gph
Stallspeed clean VS1 49 kts 56 mph
Stallspeed in landing
configuration VS0 39 kts 45 mph
Max. demonstrated crosswind 15 kts 17 mph
Rate of climb, sea level 750 ft/min 3.8 m/s
Service ceiling 14.500 ft 4.450 m
WEIGHTS & CAPACITIES:
Empty weight, typical from 500 kg from 1,102 lb
Max. takeoff weight 750 kg 1,653 lb
Useful load (at standard equipment) 250 kg 551 lb
Max. baggage weight 40 kg 88 lb
Max. wing loading 71.4 kg/m² 14.6 lb/sqft
Seats 2
Fuel capacity
100LL or Eurosuper 95 2 x 60 ltr 2 x 16 gal (US)
TAKEOFF & LANDING DISTANCES:
Takeoff distance, ground roll 250 m 820 ft
Takeoff distance over 50 ft
obstacle 430 m 1,410 ft
Landing distance, ground roll 200 m 650 ft
Landing distance over 50 ft
obstacle 500 m 1,640 ftGuide to adding images for gallery
Image dimensions width 600px x height 400px
Average size of jpg 70k
Engine
Bombardier Rotax 912S Cylinders 4 Rated power 100 HP 73,5 kW Max. take off power and max. continuous power A211 95 HP 69 kW TBO 2.000 h 15 years PROPELLER: MT-Propeller 2-blade constant-speed-propeller MTV-21-A/170-05, TBO 2.000 h/ 6 years PERFORMANCE: Max. speed 165 kts 190 mph Max. level speed, MSL 130 kts 150 mph 75% 5.000 ft ISA 55% 5.000 ft ISA Speed (TAS) 121 kts 140 mph 103 kts 118 mph Range (+ 45 min rsv) 535 NM 615 mi. 620 NM 715 mi. Endurance (+ 45 min rsv) 4:30 hrs 6:05 hrs Fuel-flow 21,5 ltr/h 5.7 gph 16,6 ltr/h 4.36 gph Stallspeed clean VS1 49 kts 56 mph Stallspeed in landing configuration VS0 39 kts 45 mph Max. demonstrated crosswind 15 kts 17 mph Rate of climb, sea level 750 ft/min 3.8 m/s Service ceiling 14.500 ft 4.450 m WEIGHTS & CAPACITIES: Empty weight, typical from 500 kg from 1,102 lb Max. takeoff weight 750 kg 1,653 lb Useful load (at standard equipment) 250 kg 551 lb Max. baggage weight 40 kg 88 lb Max. wing loading 71.4 kg/m² 14.6 lb/sqft Seats 2 Fuel capacity 100LL or Eurosuper 95 2 x 60 ltr 2 x 16 gal (US) TAKEOFF & LANDING DISTANCES: Takeoff distance, ground roll 250 m 820 ft Takeoff distance over 50 ft obstacle 430 m 1,410 ft Landing distance, ground roll 200 m 650 ft Landing distance over 50 ft obstacle 500 m 1,640 ftGuide to adding images for gallery Image dimensions width 600px x height 400px Average size of jpg 70k
Description and equipment details provided by the seller. AeroGurus does not verify seller-provided information.
Price Comparison 1 active offer
| Source | Price | Location | Listed | Days on Market | Status | Action |
|---|---|---|---|---|---|---|
|
Marco Intelisano
avpay.aero
|
Contact for Price
|
Germany | Apr 16, 2026 | — | Active |
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AeroGurus Data & Analysis
Independent data from FAA, NTSB, and market analysis
About This Aquila A211
This 2023 Aquila A211 is a single engine piston with 1 hours on the airframe.
NTSB records show 0 incidents for this airframe — a clean safety record.
Pre-Purchase Checklist
Ownership & Registration
Registration number not available.
Location & Ownership
Aircraft Location
Germany
DE
Seller reportedTitle Status
No FAA title records
Available for US-registered aircraft only
Source: FAA Aircraft Registry, FAA Civil Aviation Registry (DocIndex). Title data may be delayed. Always verify with an aviation attorney before purchase.
Safety Record
NTSB safety data coming soon.
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