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MAD X4219 Long Shaft eVTOL Airplane Drone Motor (270KV/550KV/600KV), IP35, up to 6.8 kgf

MAD X4219 Long Shaft eVTOL Airplane Drone Motor (270KV/550KV/600KV), IP35, up to 6.8 kgf

MAD X4219 Long Shaft eVTOL Airplane Drone Motor (270KV/550KV/600KV), IP35, up to 6.8 kgf

Original price was: $133.50.Current price is: $66.75.
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Overview

MAD X4219 (Long Shaft Version) is an eVTOL airplane drone motor designed for endurance flights and demanding operating conditions. It is specified as water and dust resistant with an IP35 protection rating. The 270KV version lists 6.8 kg (6.8 kgf) maximum thrust, and the 550KV version can replace the AT4219 550KV motor.

Key Features

  • Energy Efficient / Industry Professional Edition (datasheet labeling)
  • Degree of protection: IP35
  • Centrifugal heat dissipation: YES (datasheet)
  • Recommended ESC: MAD AMPX 80A (5-14S) (datasheet)

Specifications

Motor Data (MAD X4219 IPE V1.0 datasheet)

Motor model MAD X4219 IPE V1.0
Stator TAIWAN / Anticorrosive
Motor size D:50 x 65 mm
Degree of protection IP35
Centrifugal heat dissipation YES
Propeller mounting holes D:20 M3x4 / M8 Nut
Shaft diameter IN: 6 mm
Bearing EZO 686ZZ *2 / EZO 696ZZ
Number of pole pairs 7
Varnished wire degree 180C
Magnet degree 150C
Cable length 110 mm 14# Awg(Black) silicone
Rotor balance <=5 mg
Motor balance <=10 mg
Motor mounting holes D:30 M4x4, D:56 M4x4, D:60 M4x4
Disruptive test 500 V

270KV (MAD X4219 IPE 270KV)

Banner (datasheet) ENERGY EFFICIENT 270KV / INDUSTRY PROFESSIONAL EDITION
Recommended hover thrust (datasheet) 2.0~3.0 kgf
Maximum thrust (datasheet) 6.8 kgf
Optimized weight (datasheet) 284 g
Efficiency (datasheet) >73%
RPM/V 270 KV
No load current 0.6A/20V
Motor weight 284 g
Internal resistance 50 m
Nominal voltage 12S lipo battery
Maximum current 52.8 A
Maximum power 2233 W
Maximum torque 1.9 Nm
Product boxed weight 536g (110 x 110 x 95 mm)
Recommended ESC MAD AMPX 80A (5-14S)
Recommended propellers 15×8, 16×8
UAV take-off weight 12S-16″/8kg–Quadcopter; 12kg–Hexacopter; 16kg–Octocopter
Single rotor take-off weight 2kg ~ 3kg

270KV Test Notes (datasheet)

Analytical Graph of Motor Operation definitions: I – Current, P – Input Power, – Electrical Efficiency, T – Thrust, N – Rotational Speed. Data measured with an input voltage of 48 V, at a temperature of 25C and sea level. Rotational speed adjusted by throttle.

The above data are the theoretical values when the input voltage is 48V, for reference only. In the case of room temperature of 25C and no additional cooling device, the current over 53A is non-working zone, 15-53A is short-term (about 10-30s), working zone, and below 15A is sustainable working zone. In actual use, please control the motor running time according to the working environment temperature and heat dissipation conditions.

270KV Performance Data MAD X4219 IPE 270KV / APC 15×8 / AMPX 80A (5-14S) / 12S / MAX 101C

Throttle [%] Voltage [V] Current [A] Input Power [W] Output Power [W] Torque [Nm] RPM Thrust [gf] Efficiency [%] Efficiency [gf/W]
30 44.04 1.46 63.5 45.1 0.131 3293 626 71.11 9.8
35 44.01 2.21 96.9 73.1 0.182 3843 870 75.42 8.9
40 43.98 3.2 140.1 112.2 0.244 4397 1160 80.05 8.2
45 43.95 4.23 185.3 151.4 0.299 4840 1428 81.64 7.7
50 43.9 5.56 243.6 202.2 0.365 5291 1723 82.96 7.1
55 43.85 7.25 317.5 267.1 0.442 5776 2072 84.11 6.5
60 43.78 9.29 406.0 345.7 0.528 6255 2464 85.09 6.1
65 43.69 12 523.9 449.4 0.634 6767 2928 85.73 5.6
70 43.59 14.98 652.4 561.3 0.745 7197 3403 85.99 5.2
75 43.5 17.86 776.1 668.4 0.841 7591 3776 86.06 4.9
80 43.38 21.27 922.4 790.9 0.946 7982 4192 85.71 4.5
85 43.25 25.43 1099.4 931.4 1.065 8354 4392 84.66 4.0
90 43.1 29.82 1284.6 1079.1 1.182 8719 4788 83.95 3.7
95 42.92 35.08 1505.3 1257.5 1.327 9052 5236 83.4 3.5
100 42.64 42.84 1825.8 1501.6 1.521 9428 5801 82.2 3.2

270KV Performance Data MAD X4219 IPE 270KV / APC 16×8 / AMPX 80A (5-14S) / 12S / MAX 120C

Throttle [%] Voltage [V] Current [A] Input Power [W] Output Power [W] Torque [Nm] RPM Thrust [gf] Efficiency [%] Efficiency [gf/W]
30 44.03 1.75 76.5 58.5 0.173 3238 785 76.39 10.2
35 44 2.67 116.9 93.2 0.237 3764 1075 79.68 9.1
40 43.96 4.01 175.7 144.7 0.320 4317 1454 82.27 8.2
45 43.91 5.37 235.4 198.2 0.399 4747 1804 84.13 7.6
50 43.86 7.01 307.2 259.6 0.478 5183 2144 84.45 7.0
55 43.79 9.11 398.3 340.5 0.578 5630 2565 85.43 6.4
60 43.7 11.83 516.3 441.9 0.693 6088 3061 85.53 5.9
65 43.6 15.06 655.9 559.1 0.815 6553 3564 85.19 5.4
70 43.48 18.55 806.0 685.7 0.940 6964 4056 85.02 5.0
75 43.34 22.58 978.4 826.7 1.077 7330 4582 84.45 4.7
80 43.2 26.72 1153.8 966.1 1.203 7670 5044 83.66 4.4
85 43.03 31.77 1366.7 1134.7 1.354 8003 5538 82.97 4.1
90 42.84 37.17 1591.7 1296.9 1.488 8325 5982 81.42 3.8
95 42.61 43.72 1862.9 1487.6 1.652 8597 6375 79.81 3.4
100 42.3 52.8 2233.0 1723.2 1.848 8906 6819 77.13 3.1

550KV (MAD X4219 IPE 550KV)

Banner (datasheet) ENERGY EFFICIENT 550KV / INDUSTRY PROFESSIONAL EDITION
Recommended hover thrust (datasheet) 2.0~3.0 kgf
Maximum thrust (datasheet) 5.5 kgf
Optimized weight (datasheet) 286 g
Efficiency (datasheet) >73%
RPM/V 550 KV
No load current 1.5A/10V
Motor weight 286 g
Internal resistance 14.2 m
Nominal voltage 6S lipo battery
Maximum current 76.8 A
Maximum power 1498 W
Maximum torque 1.3 Nm
Product boxed weight 538g (110 x 110 x 95 mm)
Recommended ESC MAD AMPX 80A (5-14S)
Recommended propellers 15×8, 16×8
UAV take-off weight 6S-16″/8kg–Quadcopter; 12kg–Hexacopter; 16kg–Octocopter
Single rotor take-off weight 2kg ~ 3kg

550KV Test Notes (datasheet)

Analytical Graph of Motor Operation definitions: I – Current, P – Input Power, – Electrical Efficiency, T – Thrust, N – Rotational Speed. Data measured with an input voltage of 24 V, at a temperature of 25C and sea level. Rotational speed adjusted by throttle.

The above data are the theoretical values when the input voltage is 48V, for reference only. In the case of room temperature of 25C and no additional cooling device, the current over 77A is non-working zone, 27-77A is short-term (about 10-30s), working zone, and below 27A is sustainable working zone. In actual use, please control the motor running time according to the working environment temperature and heat dissipation conditions.

550KV Performance Data MAD X4219 IPE 550KV / APC 15×8 / AMPX 80A (5-14S) / 6S / MAX 89C

Throttle [%] Voltage [V] Current [A] Input Power [W] Output Power [W] Torque [Nm] RPM Thrust [gf] Efficiency [%] Efficiency [gf/W]
30 22.02 2.97 64.9 44.1 0.130 3243 616 67.8 9.4
35 21.98 4.31 94.2 68.1 0.173 3753 828 72.22 8.7
40 21.92 6.25 136.5 103.0 0.230 4279 1097 75.39 8.0
45 21.85 8.24 179.4 138.8 0.282 4695 1342 77.32 7.5
50 21.78 10.51 228.5 178.0 0.333 5109 1589 77.86 6.9
55 21.68 13.57 293.8 231.8 0.399 5546 1903 78.84 6.5
60 21.56 17.39 374.6 299.1 0.478 5981 2266 79.8 6.0
65 21.41 22.06 471.8 378.1 0.563 6417 2642 80.08 5.6
70 21.25 26.62 565.2 455.2 0.639 6805 2967 80.5 5.2
75 21.09 31.72 668.5 535.5 0.716 7138 3321 80.04 5.0
80 20.92 36.85 770.5 613.8 0.788 7439 3613 79.64 4.7
85 20.71 42.95 889.0 706.7 0.871 7744 3951 79.44 4.4
90 20.49 49.72 1018.0 803.0 0.956 8025 4286 78.83 4.2
95 20.24 56.62 1145.5 898.6 1.035 8288 4578 78.4 4.0
100 19.92 65.73 1308.6 1016.0 1.130 8588 4913 77.59 3.8

550KV Performance Data MAD X4219 IPE 550KV / APC 16×8 / AMPX 80A (5-14S) / 6S / MAX 98C

Throttle [%] Voltage [V] Current [A] Input Power [W] Output Power [W] Torque [Nm] RPM Thrust [gf] Efficiency [%] Efficiency [gf/W]
30 22.01 3.54 77.3 55.6 0.168 3171 759 71.91 9.7
35 21.95 5.24 114.3 85.5 0.224 3651 1024 74.72 8.9
40 21.87 7.78 169.6 131.0 0.299 4180 1372 77.14 8.1
45 21.79 10.23 222.5 173.9 0.363 4582 1655 78.13 7.4
50 21.69 13.41 290.3 228.9 0.439 4960 1987 78.53 6.8
55 21.58 17.06 367.6 290.5 0.518 5354 2331 78.99 6.3
60 21.43 21.4 458.2 363.3 0.603 5752 2707 79.24 5.9
65 21.26 26.79 569.0 450.6 0.704 6113 3135 79.15 5.5
70 21.06 32.66 687.5 540.9 0.796 6485 3522 78.62 5.1
75 20.86 38.68 806.3 632.2 0.891 6777 3935 78.34 4.9
80 20.66 44.59 920.8 714.6 0.965 7067 4202 77.5 4.6
85 20.41 51.63 1053.4 812.2 1.063 7297 4581 77.06 4.3
90 20.16 59.12 1191.2 908.7 1.152 7533 4903 76.24 4.1
95 19.88 66.91 1329.2 1002.3 1.236 7745 5174 75.36 3.9
100 19.5 76.84 1498.3 1117.1 1.335 7992 5500 74.51 3.7

600KV (MAD X4219 IPE 600KV)

Banner (datasheet) ENERGY EFFICIENT 600KV / INDUSTRY PROFESSIONAL EDITION
Recommended hover thrust (datasheet) 2.0~3.0 kgf
Maximum thrust (datasheet) 5 kgf
Optimized weight (datasheet) 285 g
Efficiency (datasheet) >76%
RPM/V 600 KV
No load current 1.6A/10V
Motor weight 285 g
Internal resistance 12.2 m
Nominal voltage 6S lipo battery
Maximum current 78.2 A
Maximum power 1505 W
Maximum torque 1.2 Nm
Product boxed weight 537g (110 x 110 x 95 mm)
Recommended ESC MAD AMPX 80A (5-14S)
Recommended propellers 14×7, 15×8
UAV take-off weight 6S-15″/8kg–Quadcopter; 12kg–Hexacopter; 16kg–Octocopter
Single rotor take-off weight 2kg ~ 3kg

600KV Test Notes (datasheet)

Analytical Graph of Motor Operation definitions: I – Current, P – Input Power, – Electrical Efficiency, T – Thrust, N – Rotational Speed. Data measured with an input voltage of 24 V, at a temperature of 25C and sea level. Rotational speed adjusted by throttle.

The above data are the theoretical values when the input voltage is 48V, for reference only. In the case of room temperature of 25C and no additional cooling device, the current over 78A is non-working zone, 27-78A is short-term (about 10-30s), working zone, and below 27A is sustainable working zone. In actual use, please control the motor running time according to the working environment temperature and heat dissipation conditions.

600KV Performance Data MAD X4219 IPE 600KV / APC 14×7 / AMPX 80A (5-14S) / 6S / MAX 81C

Throttle [%] Voltage [V] Current [A] Input Power [W] Output Power [W] Torque [Nm] RPM Thrust [gf] Efficiency [%] Efficiency [gf/W]
30 21.85 2.64 57.2 43.1 0.114 3611 545 75.19 9.4
35 21.8 4.02 86.9 67.7 0.153 4221 750 77.81 8.6
40 21.76 5.43 117.8 93.4 0.190 4702 947 79.29 8.0
45 21.7 7.29 157.7 126.4 0.234 5168 1171 80.13 7.4
50 21.62 9.52 205.5 168.3 0.285 5649 1413 81.85 6.9
55 21.53 12.43 267.2 220.5 0.341 6170 1712 82.46 6.4
60 21.41 16.09 343.9 286.6 0.408 6704 2041 83.29 5.9
65 21.27 20.22 429.7 358.7 0.478 7172 2378 83.44 5.5
70 21.12 24.58 518.6 433.9 0.546 7592 2686 83.61 5.2
75 20.96 29.39 615.6 512.1 0.614 7970 3009 83.14 4.9
80 20.79 34.42 715.1 592.4 0.680 8326 3301 82.81 4.6
85 20.58 40.51 833.4 687.5 0.758 8657 3660 82.45 4.4
90 20.37 46.52 947.2 777.7 0.826 8992 3895 82.06 4.1
95 20.12 53.87 1083.1 880.2 0.907 9264 4153 81.2 3.8
100 19.78 63.64 1258.3 1011.9 1.007 9598 4425 80.36 3.5

600KV Performance Data MAD X4219 IPE 600KV / APC 15×8 / AMPX 80A (5-14S) / 6S / MAX 97C

Throttle [%] Voltage [V] Current [A] Input Power [W] Output Power [W] Torque [Nm] RPM Thrust [gf] Efficiency [%] Efficiency [gf/W]
30 21.84 3.7 80.4 53.4 0.147 3472 699 66.41 8.6
35 21.77 5.54 120.2 85.9 0.202 4073 959 71.43 7.9
40 21.71 7.66 165.8 123.1 0.258 4562 1229 74.2 7.4
45 21.62 10.22 220.6 169.3 0.323 5003 1523 76.69 6.9
50 21.52 13.12 281.9 219.9 0.386 5443 1812 77.96 6.4
55 21.4 16.94 361.9 285.3 0.461 5916 2166 78.79 6.0
60 21.24 21.77 461.9 366.9 0.549 6387 2550 79.36 5.5
65 21.07 27.11 570.6 453.9 0.638 6799 2943 79.51 5.2
70 20.87 32.68 681.5 541.5 0.721 7171 3310 79.4 4.9
75 20.67 38.65 798.5 631.3 0.804 7497 3651 79 4.6
80 20.45 45.08 921.8 723.1 0.886 7792 3989 78.4 4.3
85 20.22 52.06 1052.2 820.8 0.969 8086 4293 77.96 4.1
90 19.93 60.3 1201.3 926.7 1.064 8314 4388 77.09 3.7
95 19.63 68.38 1342.1 1026.3 1.148 8541 4689 76.42 3.5
100 19.26 78.17 1505.0 1146.5 1.240 8830 4952 76.13 3.3

Whats Included

  • Propeller plate *1
  • Prop Adapter *1
  • X-Mount *1
  • 40mm Bullet Connector *3
  • Heat Shrinkable Tube*3
  • Motor Screws, M4*10mm *4
  • Prop Adapter Screws, M3*8mm *4
  • X-Mount Installation Screw, M4*10mm *4
  • M8 Nut Propeller Screws
  • Sticker*2

Applications

  • eVTOL aircraft and fixed-wing/VTOL UAV propulsion
  • Single-rotor or multirotor platforms (see take-off weight guidance in specifications)

For compatibility questions (KV selection, propeller pairing, ESC choice) or after-sales support, contact https://rcdrone.top/ or email [email protected].

Details

The MAD X4219 270KV long shaft motor is rated for 12S use and lists key details like 284 g weight, >73% efficiency, and thrust curves for setup planning.

MAD X4219 270KV long-shaft eVTOL motor documentation includes detailed mounting dimensions plus 12S test data with an APC 15×8 prop and 80A ESC guidance.

MAD X4219 motor documentation includes thrust, current, RPM, and efficiency test data to help choose a prop and battery setup.

The MAD X4219 eVTOL drone motor includes a 600KV rating and a spec table with prop test data to help match your setup.

MAD X4219 test data lists thrust, RPM, current, and power across throttle levels for a 6S configuration.

The MAD X4219 long shaft eVTOL drone motor includes performance curves, dimensions, and wiring details to support motor selection and mounting.

The MAD X4219 long-shaft motor is labeled 550KV and 286g, with the included performance graph and tables for setup reference.

The MAD X4219 long-shaft motor is listed at 600KV with a 285g weight and efficiency over 76% on the included spec sheet.

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