Charter ATR 72-212A Cargo Conversion
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ATR 72-500F (ATR 72-212A(F)) payload and cargo capacity
ATR 72-212A Cargo Conversion · AT75
Aircraft information
This technical reference for ATR 72-500F (ATR 72-212A(F)) includes available capacity, performance, dimensions, and loading data.
Key figures
- Max payload
- 8,900 kg
- Cargo volume
- 75 m³
- Range at max payload
- 1,480 km
Charter
Specifications
Cargo & performance
- Max payload
- 8,900 kg
- Cargo volume
- 75 m³
- Range at max payload
- 1,480 km
- Ferry range
- 3,700 km
- Cruise speed
- 556 km/h
Dimensions
- Overall length
- 27.17 m
- Wingspan
- 27.05 m
- Main deck length
- 17.96 m
- Main deck width
- 2.26 m
- Main deck height
- 1.75 m
Cargo doors & loading notes
Main deck large cargo door (LH): approx. 294 × 180 cm
Weights
- Maximum takeoff weight (MTOW)
- 23,000 kg
- Maximum zero fuel weight (MZFW)
- 21,000 kg
- Maximum landing weight (MLW)
- 22,350 kg
- Operating empty weight (OEW)
- 12,000 kg
Aircraft
- Manufacturer
- ATR
- Aircraft family
- ATR72
- ICAO type code
- AT75
- Aircraft category
- Narrow-body freighter
- Propulsion
- Turboprop/Turboshaft
- Engines
- 2 × PW127M / PW127F depending certified series
- Recorded operational status
- Active
Airport planning
ICAO type classification
Current Doc 8643 record for AT75.
Official ICAO type-level classification mapped by the current Doc 8643 designator. Multiple aircraft variants may share one designator; this is not variant-specific operational approval.
- ICAO type designator
- AT75
- Wake turbulence category
- M
- Wingtip clearance group
- F
- Aircraft configuration
- Land Plane · 2 × Turboprop/Turboshaft
Source: ICAO · Doc 8643 — Aircraft Type Designators · Updated Sep 3, 2026
FAA airport planning characteristics
Mapped by ICAO type designator AT75. FAA source record: ATR-72-500.
FAA aircraft-type data mapped by ICAO designator. It is intended for airport planning and design; it is not variant-specific operational approval or a complete compatibility assessment.
- FAA approach category
- B
- Airplane design group
- III
- Taxiway design group
- 2A
- Reference approach speed
- 120 kt
- Tail height
- 7.65 m
- Wheelbase
- 10.76 m
- Main gear width
- 5.24 m
- Reference MTOW
- 22,800 kg
Source: FAA · Aircraft Characteristics Database (October 2024) · Download source dataset