Verkehrsflugzeug · Zivil · Ukraine
Antonov An-24
- 29. Oktober 1959
- Erstflug
- 1962
- Indienststellung
- Im Dienst
- Status
- 1.367
- Gebaute Exemplare
-1600.webp)
-1600.webp)
-1600.webp)
-1600.webp)
-1600.webp)
_1-1600.webp)
.jpg)
-1600.webp)
-1600.webp)
1 / 22
Die Antonov An-24 ist ein sowjetisches zweimotoriges Turboprop-Regionalverkehrsflugzeug, das am 29. Oktober 1959 zum ersten Mal flog und 1962 in Dienst ging. Für den Betrieb von notdürftigen Pisten konzipiert, wurde sie mit mehr als 1.367 gebauten Exemplaren zu einem der zahlreichsten Regionalflugzeuge des sowjetischen Blocks.
Verwandte Ereignisse
Verwandte Einträge
Kategorie
Dreiseitenansicht
Geschichte
Ende der fünfziger Jahre stützte sich der sowjetische Regionalluftverkehr noch immer auf die betagte Kolbenmotormaschine Ilyushin Il-14, und das Konstruktionsbüro Antonov erhielt den Auftrag, sie auf den Kurz- und Mittelstrecken abzulösen. Das Ergebnis war die An-24, ein Hochdecker mit zwei Ivchenko-AI-24-Turboprops, eigens für abgelegene Flugplätze und unbefestigte Pisten gedacht, wo Robustheit mehr zählte als Verfeinerung. Der Prototyp hob am 29. Oktober 1959 ab, und der Typ nahm 1962 den Betrieb auf.
Die verbreitetste Passagierversion, die An-24V, nahm 50 Passagiere bei einer dreiköpfigen Besatzung auf und bot bei voller Betankung eine maximale Reichweite von 2.400 km. Die Produktion verteilte sich auf die Werke in Kiew, Irkutsk und Ulan-Ude, und als die Hauptlinie 1976 geschlossen wurde, waren mehr als tausend Zellen fertiggestellt; die Gesamtzahl übersteigt 1.367 Exemplare. In China wurde der Entwurf als Xi'an Y-7 weiterhin in Lizenz gebaut und verlängerte so das industrielle Leben des Projekts.
Mehr als sechs Jahrzehnte nach ihrem Erstflug steht die An-24 weiterhin bei zivilen und militärischen Betreibern mehrerer Länder im Dienst, ein Zeugnis der Einfachheit und Widerstandsfähigkeit ihres Entwurfs. Ihre Zelle diente überdies als Grundlage für eine ganze Familie von Transportableitungen, die ihre Philosophie des kargen Betriebs erbten.
Varianten
| An-24 (prototypes) | An-24 | An-24T | An-24A | An-24AEW | An-24ALK | An-24A (NK-4 project) | An-24AT | An-24AT-RD | An-24AT-U | An-24B | An-24D | An-24-I | An-24-II | An-24K | An-24LL | An-24LP | An-24LR-1 'Toros' | An-24LR-2 'Nit' | An-24PRT | An-24PS | An-24R | An-24RR | An-24RT | An-24RT (retranslyator) | An-24RV | An-24ShT | An-24T (first use, project) | An-24T 'Troyanda' | An-24TV | An-24USh | An-24V | An-24VSR | |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| Erstflug | 20. Oktober 1959 | 29. Oktober 1959 | 16. November 1965 | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — |
| Luftfahrzeugtyp | Regional turboprop airliner prototype | Regional turboprop airliner | Turboprop tactical transport | Regional turboprop airliner | Turboprop airborne early warning aircraft | Turboprop navaid calibration aircraft | Projected turboprop regional airliner | Projected turboprop tactical transport | Projected turboprop tactical transport | Proyecto de avión de transporte táctico turbohélice | Regional turboprop airliner | Projected turboprop regional airliner | Regional turboprop airliner | Regional turboprop airliner | Projected turboprop regional airliner | Turboprop flying laboratory | Turboprop forest fire-fighting aircraft | Turboprop ice reconnaissance aircraft | Turboprop earth resources survey aircraft | Avión turbohélice de búsqueda y rescate | Turboprop search and rescue aircraft | Turboprop photographic reconnaissance aircraft | Turboprop NBC reconnaissance aircraft | Turboprop tactical transport | Turboprop communications relay aircraft | Regional turboprop airliner | Turboprop airborne command post | Projected turboprop tactical transport | Turboprop anti-submarine detection testbed | Turboprop freighter for export | Turboprop navigator trainer | Regional turboprop airliner | Turboprop navigation trainer |
| Antrieb | 2 × Ivchenko AI-24 turboprops of 1,790 kW (2,400 shp) each, driving four-blade AV-72 constant-speed propellers. | 2 × Ivchenko AI-24 turboprops of 1,790 kW (2,400 shp) each, driving four-blade AV-72 constant-speed propellers. | 2 × second-series Ivchenko AI-24T turboprops of 2,103 kW (2,820 eshp) each, with water injection. | 2 × Ivchenko AI-24A turboprops of 1,900 kW (2,550 eshp) each, driving four-blade AV-72 constant-speed propellers. | 2 × Ivchenko AI-24A turboprops of 1,900 kW (2,550 eshp) each, driving four-blade AV-72 constant-speed propellers. | 2 × Ivchenko AI-24A turboprops of 1,900 kW (2,550 eshp) each, driving four-blade AV-72 constant-speed propellers. | 2 × Kuznetsov NK-4 turboprops; the version was halted when the engine was cancelled. | Coupled Isotov TV2-117DS turboprops. | Coupled Isotov TV2-117DS turboprops plus two booster turbojets podded under the outer wings. | Turbohélices acoplados Isotov TV2-117DS con tres o cinco cohetes de despegue asistido PRD-63 de propulsante sólido. | 2 × Ivchenko AI-24A turboprops of 1,900 kW (2,550 eshp) each, driving four-blade AV-72 constant-speed propellers. | 2 × Ivchenko AI-24A turboprops of 1,900 kW each plus a single RU-19 booster turbojet in the starboard nacelle. | 2 × Ivchenko AI-24A turboprops of 1,900 kW (2,550 eshp) each, driving four-blade AV-72 constant-speed propellers. | 2 × second-series Ivchenko AI-24T turboprops of 2,103 kW (2,820 eshp) each, with water injection. | No published powerplant data: the project never got past the initial idea. | 2 × Ivchenko AI-24A turboprops of 1,900 kW (2,550 eshp) each, driving four-blade AV-72 constant-speed propellers. | 2 × Ivchenko AI-24A turboprops of 1,900 kW (2,550 eshp) each plus one Tumansky RU-19A-300 auxiliary turbojet of 8.83 kN (800 kgf) in the starboard nacelle. | 2 × Ivchenko AI-24A turboprops of 1,900 kW (2,550 eshp) each, driving four-blade AV-72 constant-speed propellers. | 2 × Ivchenko AI-24A turboprops of 1,900 kW (2,550 eshp) each, driving four-blade AV-72 constant-speed propellers. | 2 × turbohélice Ivchenko AI-24T de 2.103 kW (2.820 shp equivalentes) unitarios más un turborreactor auxiliar Tumanski RU-19A-300 de 8,83 kN (800 kgf) en la góndola de estribor. | 2 × Ivchenko AI-24A turboprops of 1,900 kW (2,550 eshp) each, driving four-blade AV-72 constant-speed propellers. | 2 × Ivchenko AI-24A turboprops of 1,900 kW (2,550 eshp) each, driving four-blade AV-72 constant-speed propellers. | 2 × Ivchenko AI-24A turboprops of 1,900 kW (2,550 eshp) each, driving four-blade AV-72 constant-speed propellers. | 2 × Ivchenko AI-24T turboprops of 2,103 kW (2,820 eshp) each plus one Tumansky RU-19A-300 auxiliary turbojet of 8.83 kN (800 kgf) in the starboard nacelle. | 2 × second-series Ivchenko AI-24T turboprops of 2,103 kW (2,820 eshp) each, with water injection. | 2 × Ivchenko AI-24A turboprops of 1,900 kW (2,550 eshp) each plus one Tumansky RU-19A-300 auxiliary turbojet of 8.83 kN (800 kgf) in the starboard nacelle. | 2 × second-series Ivchenko AI-24T turboprops of 2,103 kW (2,820 eshp) each, with water injection. | No engine designation published for this first tactical transport project. | 2 × second-series Ivchenko AI-24T turboprops of 2,103 kW (2,820 eshp) each, with water injection. | 2 × second-series Ivchenko AI-24T turboprops of 2,103 kW (2,820 eshp) each, with water injection. | 2 × Ivchenko AI-24A turboprops of 1,900 kW (2,550 eshp) each, driving four-blade AV-72 constant-speed propellers. | 2 × Ivchenko AI-24A turboprops of 1,900 kW (2,550 eshp) each, driving four-blade AV-72 constant-speed propellers. Propeller diameter 3.90 m. | 2 × Ivchenko AI-24A turboprops of 1,900 kW (2,550 eshp) each, driving four-blade AV-72 constant-speed propellers. |
| Triebwerke | 2 × Ivchenko AI-24 | 2 × Ivchenko AI-24 | 2 × Ivchenko AI-24T | 2 × Ivchenko AI-24A | 2 × Ivchenko AI-24A | 2 × Ivchenko AI-24A | 2 × Kuznetsov NK-4 | 2 × Isotov TV2-117DS | 2 × Isotov TV2-117DS | 2 × Isotov TV2-117DS | 2 × Ivchenko AI-24A | 2 × Ivchenko AI-24A + Tumansky RU-19 | 2 × Ivchenko AI-24A | 2 × Ivchenko AI-24T | 2 × turboprop | 2 × Ivchenko AI-24A | 2 × Ivchenko AI-24A + Tumansky RU-19A-300 | 2 × Ivchenko AI-24A | 2 × Ivchenko AI-24A | 2 × Ivchenko AI-24T + Tumansky RU-19A-300 | 2 × Ivchenko AI-24A | 2 × Ivchenko AI-24A | 2 × Ivchenko AI-24A | 2 × Ivchenko AI-24T + Tumansky RU-19A-300 | 2 × Ivchenko AI-24T | 2 × Ivchenko AI-24A + Tumansky RU-19A-300 | 2 × Ivchenko AI-24T | 2 × turboprop | 2 × Ivchenko AI-24T | 2 × Ivchenko AI-24T | 2 × Ivchenko AI-24A | 2 × Ivchenko AI-24A | 2 × Ivchenko AI-24A |
| Leistung je Triebwerk | 2.400 hp | 2.400 hp | 2.820 hp Bester Wert dieser Zeile | 2.548 hp | 2.548 hp | 2.548 hp | — | — | — | — | 2.548 hp | 2.548 hp | 2.548 hp | 2.820 hp Bester Wert dieser Zeile | — | 2.548 hp | 2.548 hp | 2.548 hp | 2.548 hp | 2.820 hp Bester Wert dieser Zeile | 2.548 hp | 2.548 hp | 2.548 hp | 2.820 hp Bester Wert dieser Zeile | 2.820 hp Bester Wert dieser Zeile | 2.548 hp | 2.820 hp Bester Wert dieser Zeile | — | 2.820 hp Bester Wert dieser Zeile | 2.820 hp Bester Wert dieser Zeile | 2.548 hp | 2.548 hp | 2.548 hp |
| Länge | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | 23,5 m Bester Wert dieser Zeile | — | — | — | — | — | 23,5 m Bester Wert dieser Zeile | — |
| Spannweite | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | 29,2 m Bester Wert dieser Zeile | — | — | — | — | — | 29,2 m Bester Wert dieser Zeile | — |
| Höhe | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | 8,3 m Bester Wert dieser Zeile | — | — | — | — | — | 8,3 m Bester Wert dieser Zeile | — |
| Flügelfläche | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | 75 m² Bester Wert dieser Zeile | — | — | — | — | — | 75 m² Bester Wert dieser Zeile | — |
| Leermasse | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | 13.300 kg Bester Wert dieser Zeile | — | — | — | — | — | 13.300 kg Bester Wert dieser Zeile | — |
| MTOW | — | — | — | — | — | — | — | — | — | — | 21.000 kg Bester Wert dieser Zeile | — | — | — | — | — | — | — | — | — | — | — | — | — | — | 21.000 kg Bester Wert dieser Zeile | — | — | — | — | — | 21.000 kg Bester Wert dieser Zeile | — |
| Höchstgeschwindigkeit | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | 485 km/h Bester Wert dieser Zeile | — | — | — | — | — | 485 km/h Bester Wert dieser Zeile | — |
| Höhe der Höchstgeschwindigkeit | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | 6.000 m | — | — | — | — | — | 6.000 m | — |
| Reisegeschwindigkeit | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | 450 km/h Bester Wert dieser Zeile | — | — | — | — | — | 450 km/h Bester Wert dieser Zeile | — |
| Reiseflughöhe | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | 6.000 m | — | — | — | — | — | 6.000 m | — |
| Dienstgipfelhöhe | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | 8.400 m Bester Wert dieser Zeile | — | — | — | — | — | 8.400 m Bester Wert dieser Zeile | — |
| Anfängliche Steigrate | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | 7,1 m/s | — |
| Reichweite | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | 2.400 km Bester Wert dieser Zeile | — | — | — | — | — | 2.400 km Bester Wert dieser Zeile | — |
| Überführungsreichweite | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | 2.820 km | — |
| Einsatzradius | 0 km Bester Wert dieser Zeile | 0 km Bester Wert dieser Zeile | 0 km Bester Wert dieser Zeile | 0 km Bester Wert dieser Zeile | 0 km Bester Wert dieser Zeile | 0 km Bester Wert dieser Zeile | 0 km Bester Wert dieser Zeile | 0 km Bester Wert dieser Zeile | 0 km Bester Wert dieser Zeile | 0 km Bester Wert dieser Zeile | 0 km Bester Wert dieser Zeile | 0 km Bester Wert dieser Zeile | 0 km Bester Wert dieser Zeile | 0 km Bester Wert dieser Zeile | 0 km Bester Wert dieser Zeile | 0 km Bester Wert dieser Zeile | 0 km Bester Wert dieser Zeile | 0 km Bester Wert dieser Zeile | 0 km Bester Wert dieser Zeile | 0 km Bester Wert dieser Zeile | 0 km Bester Wert dieser Zeile | 0 km Bester Wert dieser Zeile | 0 km Bester Wert dieser Zeile | 0 km Bester Wert dieser Zeile | 0 km Bester Wert dieser Zeile | 0 km Bester Wert dieser Zeile | 0 km Bester Wert dieser Zeile | 0 km Bester Wert dieser Zeile | 0 km Bester Wert dieser Zeile | 0 km Bester Wert dieser Zeile | 0 km Bester Wert dieser Zeile | 0 km Bester Wert dieser Zeile | 0 km Bester Wert dieser Zeile |
| Flugdauer | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | 320 min | — |
| Bedingungen der Reichweite | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | 2,400 km with maximum fuel and about 550 km with maximum payload. | — | — | — | — | — | 2,400 km with maximum fuel (5,550 litre capacity) and about 550 km with maximum payload. | — |
| Bewaffnung | None | None | None | None | None | None | None | None | None | Ninguno | None | None | None | None | None | None | None | None | None | Ninguno | None | None | None | None | None | None | None | None | None | None | None | None | None |
| Maximale Waffenzuladung | 0 kg Bester Wert dieser Zeile | 0 kg Bester Wert dieser Zeile | 0 kg Bester Wert dieser Zeile | 0 kg Bester Wert dieser Zeile | 0 kg Bester Wert dieser Zeile | 0 kg Bester Wert dieser Zeile | 0 kg Bester Wert dieser Zeile | 0 kg Bester Wert dieser Zeile | 0 kg Bester Wert dieser Zeile | 0 kg Bester Wert dieser Zeile | 0 kg Bester Wert dieser Zeile | 0 kg Bester Wert dieser Zeile | 0 kg Bester Wert dieser Zeile | 0 kg Bester Wert dieser Zeile | 0 kg Bester Wert dieser Zeile | 0 kg Bester Wert dieser Zeile | 0 kg Bester Wert dieser Zeile | 0 kg Bester Wert dieser Zeile | 0 kg Bester Wert dieser Zeile | 0 kg Bester Wert dieser Zeile | 0 kg Bester Wert dieser Zeile | 0 kg Bester Wert dieser Zeile | 0 kg Bester Wert dieser Zeile | 0 kg Bester Wert dieser Zeile | 0 kg Bester Wert dieser Zeile | 0 kg Bester Wert dieser Zeile | 0 kg Bester Wert dieser Zeile | 0 kg Bester Wert dieser Zeile | 0 kg Bester Wert dieser Zeile | 0 kg Bester Wert dieser Zeile | 0 kg Bester Wert dieser Zeile | 0 kg Bester Wert dieser Zeile | 0 kg Bester Wert dieser Zeile |
| Nutzlast | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | 5.500 kg Bester Wert dieser Zeile | — | — | — | — | — | 5.500 kg Bester Wert dieser Zeile | — |
| Ladekapazität | Six test aircraft, with the 44-seat cabin of the original design. | First production batch, with a 44-passenger cabin. | Ventral loading hatch, cargo winch and escape hatch aft of the nose gear for airborne troop transport. | 44-passenger cabin with increased interior volume. | N-019 Topaz pulse-Doppler radar fitted to the An-24A airframe. | Phototheodolite and a powerful light source to calibrate optical sensors. | — | Rear loading ramp. | Wider loading ramp than the An-24AT. | Rampa de carga más ancha y previsión para hasta tres paracaídas de frenado. | Cabin for up to 52 passengers; maximum take-off weight raised to 21,000 kg. | Stretched fuselage seating 60, strengthened structure and increased fuel capacity. | Initial export version of the An-24B, with a 50-passenger cabin. | Late export version of the An-24B, seating 50 in passenger, cargo and mixed layouts. | 18-seat civil transport. | Cabin filled with metrology instrumentation to check the airworthiness of production aircraft. | Cabin tank, optical smoke and flame detectors, flare-dispenser racks and provision to para-drop firefighters. | 'Toros' sideways-looking airborne radar either side of the lower fuselage. | Large 'Nit' sideways-looking radar pod on the side of the lower fuselage. | Cabina con equipo de salvamento y dispositivos de exploración; algunas células con esquíes o flotadores. | A single An-24B adapted for search and rescue, rejected after acceptance trials. | A single An-24A with photographic cameras; it served as testbed for the An-30 camera fit. | RR8311-100 air sampling pods low on the forward fuselage and a sensor pod on a port-side pylon. | Tactical transport like the An-24T, with the auxiliary turbojet boosting take-off and climb. | Conversion of An-24T and An-24RT airframes with relay equipment in the cargo cabin. | Up to 52 passengers four abreast (2+2) and 5,500 kg of payload. | Cabin taken up by command consoles and communications equipment for the staff. | Rejected for poor field performance and inability to load or air-drop vehicles. | Sensors in teardrop fairings either side of the forward fuselage and extra equipment in extended wing centre-section fairings. | Export freighter version of the An-24T, with the same ventral hatch. | Five training stations and four rows of seats for waiting trainees; bulged windows at each station. | Cabin for 50 passengers four abreast (2+2) and up to 5,500 kg of payload; crew of three. | A single An-24V modified to train radio communications. |
| Besatzung | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | — | 3 | — |
| Passagiere | 44 | 44 | — | 44 | — | — | — | — | — | — | 52 | 60 Bester Wert dieser Zeile | 50 | 50 | 18 | — | — | — | — | — | — | — | — | — | — | 52 | — | — | — | — | — | 50 | — |
| Gebaute Exemplare | 6 | 17 | 197 | 200 | 1 | 1 | — | — | — | — | 400 Bester Wert dieser Zeile | — | — | — | — | 1 | 3 | 2 | 1 | 11 | 1 | 1 | 4 | — | — | — | — | — | — | — | 7 | — | 1 |
Bilder
Anderswo
- Planespotters.net01 YELLOW Ukrainian Air Force Antonov An-24 ↗
- Planespotters.netUP-AN422 Southern Sky Antonov An-24B ↗
- RussianPlanes.netАнтонов Ан-24РВ UR-ELM, ООН ↗
- RussianPlanes.netАнтонов Ан-24Б UR-46416, Авиалинии Донбасса ↗
- RussianPlanes.netАнтонов Ан-24РВ RA-46695, Ямал АТК ↗
- RussianPlanes.netАнтонов Ан-24РВ UK-46623, Авиалинии Узбекистана ↗
- RussianPlanes.netАнтонов Ан-24РВ RA-46621, Алроса ↗
- RussianPlanes.netАнтонов Ан-24Б ER-AZZ, зав.н. 79901110 ↗
- RussianPlanes.netАнтонов Ан-24 СССР-46389, зав.н. 57302003 ↗
- RussianPlanes.netАнтонов Ан-24 СССР-46722, зав.н. 37300302 ↗
- AirHistory.netAntonov An-24, CU-T1236, Cubana ↗
- AirHistory.netAntonov An-24B, UN-46381, SCAT Airlines ↗
Die restlichen 10 anzeigen
- AirHistory.netAntonov An-24B aircraft photos ↗
- ABPicAntonov An-24, YV-2726P, Aerosegovia ↗
- ABPicAntonov An-24RV, UR-47313, Air Urga ↗
- ABPicAntonov An-24RV, RA-47363, Avialesoochrana ↗
- ABPicAntonov An-24RV, RA-46507, Sarit Airlines ↗
- ABPicAntonov An-24RV, CU-T1706, Cubana ↗
- ABPicAntonov An-24RV, YA-DAM, Ariana Afghan Airlines ↗
- JetPhotosAntonov An-24 aviation photos ↗
- JetPhotosAntonov An-24RV aviation photos ↗
- AirlinersGallery.comAntonov An-24 gallery ↗