A/C |
Manufacturer |
ATR |
|
ATR |
|
|
Sources: |
|
|
|
Aircraft type |
ATR 42 |
|
ATR 72 |
|
[1] |
https://www.flightglobal.com/download?ac=73559 |
|
Total number
of operating A/C |
208 |
[1] |
795 |
[1] |
[2] |
https://perma.cc/UQ5K-LGE4 |
|
Option/Variant |
42-500/-600 |
[5] |
72-212A/-600 |
[4] |
[3] |
https://www.atr-aircraft.com/wp-content/uploads/2020/07/Factsheets_-_ATR_42-600.pdf |
Engine |
No. of Engines |
2 |
[3] |
2 |
[4] |
[4] |
https://www.atr-aircraft.com/wp-content/uploads/2020/07/Factsheets_-_ATR_72-600.pdf |
Model |
PW127M |
[3] |
PW127M/N |
[4] |
[5] |
https://www.easa.europa.eu/downloads/8249/en |
|
Max. Rated
Takeoff Thrust, T_TO [kN] |
- |
|
- |
|
[6] |
https://perma.cc/J8MY-KVDC |
|
Equivalent Power, P [kW] |
1589 |
[3] |
1820 |
[4] |
|
Comments: |
|
Propeller |
568F |
[3] |
568F |
[4] |
|
¹ No further details |
|
Cabin |
Length, l_CABIN
[m] |
N/A |
|
N/A |
|
|
Max. Height,
h_CABIN [m] |
1,91 |
[3] |
1,91 |
[4] |
|
Max. Width, d_F,I
[m] |
2,57 |
[3] |
2,57 |
[4] |
|
Passenger
Compartment Volume, V_CABIN
[m³] |
N/A |
|
N/A |
|
|
Fuselage |
Height, h_F [m] |
2,63 |
[6] |
2,63 |
[2] |
|
Width, w_F [m] |
2,87 |
[6] |
2,87 |
[2] |
|
Total |
Length, l_A/C
[m] |
22,67 |
[3] |
27,17 |
[4] |
|
Span, b_W [m] |
24,57 |
[3] |
27,05 |
[4] |
|
Height, h_A/C [m] |
7,59 |
[3] |
7,65 |
[4] |
|
Landing Gear |
Track, l_T [m] |
4,1 |
[3] |
4,1 |
[4] |
|
Wheelbase, l_WB
[m] |
8,78 |
[3] |
10,77 |
[4] |
|
Wing |
Area, S_W [m²] |
54,5 |
[3] |
61 |
[4] |
|
Taper ratio,
λ_W |
N/A |
|
0,47 |
[2] |
|
1/4 Chord
Sweep, φ_25,W [°] |
N/A |
|
3,5 |
[2] |
|
Vertical Tail |
Area, S_V [m²] |
12,48 |
[6] |
N/A |
|
|
Height, b_V [m] |
4,53 |
[6] |
4,43 |
[2] |
|
Taper ratio,
λ_V |
N/A |
|
0,65 |
[2] |
|
1/4 Chord
Sweep, φ_25,V [°] |
N/A |
|
29 |
[2] |
|
Horizontal Tail |
Area, S_H [m²] |
11,73 |
[6] |
N/A |
|
|
Span, b_H [m] |
7,31 |
[6] |
7,31 |
[2] |
|
Taper Ratio,
λ_H |
N/A |
|
0,525 |
[2] |
|
1/4 Chord
Sweep, φ_25,H [°] |
N/A |
|
5,5 |
[2] |
|
Cruise |
V_MO [kt] |
300 |
[6] |
275 |
[4] |
|
M_MO [Mach] |
0,55 |
[6] |
0,55 |
[2] |
|
Cruise Speed,
M_CR [Mach] |
N/A |
|
N/A |
|
|
Max. Certified
Flight Level, h_MCR [FL] |
250 |
[6] |
250 |
[2] |
|
Cruise
Altitude, h_CR [FL] |
N/A |
|
N/A |
|
|
Fuel |
Unusable Fuel [l] |
26 |
[5] |
37 |
[5] |
|
Optional Fuel
[l] |
- |
|
- |
|
|
Max usable
fuel [l] |
5700 |
[5] |
6360 |
[5] |
|
Range |
Max. Payload, R_MPL [nm] |
N/A |
|
N/A |
|
|
Max. Pax, R_M,pax [nm] |
703 |
¹[3] |
758 |
¹[4] |
|
Max. Range, R_PLMR [nm] |
N/A |
|
N/A |
|
|
Mass |
Max.
Ramp, m_MR (MRM) [kg] |
18770 |
[5] |
23170 |
[5] |
|
Max. Take-Off, m_MTO
(MTOM) [kg] |
18600 |
[3] |
23000 |
[4] |
|
Max. Landing, m_ML (MLM)
[kg] |
18300 |
[3] |
22350 |
[4] |
|
Max. Zero Fuel, m_MZF
(MZFM) [kg] |
17000 |
[3] |
21000 |
[4] |
|
Operating Empty, m_OE
(OEM) (MZFM-MPL) [kg] |
11550 |
[3] |
13010 |
[4] |
|
Max. Payload, m_MPL (MPL) [kg] |
5300 |
[3] |
7550 |
[4] |
|
Payload at Max. Range, m_PLMR [kg] |
N/A |
|
N/A |
|
|
Cargo |
Volume, V_CARGO
[m³] |
N/A |
|
N/A |
|
|
Cargo Capacity |
- |
|
- |
|
|
Max. Pallet
Underfloor |
- |
|
- |
|
|
Seats |
Max. Seats, n_M,SEAT |
60 |
[5] |
74 |
[5] |
|
Std. Layout,
n_SEAT |
48 |
[5] |
72 |
[4] |
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