- Home
- RSAF's forces
- Aircraft
Aircraft
Find out more about the roles and specifications of the aircraft that RSAF employs.
On this page
Fighters
F-15SG

F-15SG
Specifications of F-15SG
The F-15SG is an all-weather multi-role fighter. Equipped with the latest technological upgrades, it is one of the most capable and lethal multi-role aircraft in the world. Featuring the state-of-the-art cockpit and advanced avionics, including the Joint Helmet Mounted Cueing System (JHCMS), the F-15SG provides the Pilot and Weapon Systems Officer (WSO) (Fighter) with increased situational awareness, as well as enhanced air-to-air and self-defence capabilities. The aircraft is powered by two General Electric F110-GE-129 turbofan engines.
Specifications of F-15SG
Length | 63.8 ft |
Height | 18.5 ft |
Wing Span | 42.8 ft |
Performance | Maximum Speed - 2.5 Mach Service Ceiling - 60,000 ft |
Armament | M61 20 mm cannon AIM-9 air-to-air missiles AIM-120 air-to-air missiles Laser-guided bombs Maverick air-to-ground missiles |
Crew Composition | 1 Pilot 1 Weapon Systems Officer (WSO) (Fighter) |
F-16C/D/D+ Fighting Falcon

F-16C/D/D+ Fighting Falcon
Specifications of F-16C/D/D+ Fighting Falcon
The F-16 is a multi-role tactical fighter with full air-to-air and air-to-surface combat capabilities. The aircraft features modern core avionics, Common Colour Multi-Function Display (CCMFD), sophisticated radar, smart weapons compatibility and state-of-the-art navigation and targeting systems. It is powered by Pratt and Whitney F100-PW-229 turbofan engine.
Specifications of F-16C/D/D+ Fighting Falcon
Length | 15.06 m |
Height | 4.88 m |
Wing Span | 10.01 m |
Performance | Maximum Speed - 2.0 Mach Service Ceiling - 50,000 ft |
Armament | M61 20mm cannon AIM-9 air-to-air missiles AIM-120 air-to-air missiles Maverick air-to-ground missiles Laser-guided bombs |
Helicopters
AS332M/M1 Super Puma

AS332M/M1 Super Puma
Specifications of AS332M/M1 Super Puma
The AS332M/M1 Super Puma is a medium lift helicopter. It is powered by two Turbomeca Makila 1A/1A1 turbo-shaft engines. It is employed for various roles such as troop lift, Search and Rescue (SAR) operations, underslung cargo transport and VIP transport.
Specifications of AS332M/M1 Super Puma
Performance | Maximum Speed – 167 Knots Endurance – 4.5 Hours |
Crew Composition | 2 Pilots 1 Aircrew Specialist Configuration: 24 passengers or 6 stretchers and 1 medic |
CH-47D/SD Chinook

CH-47D/SD Chinook
Specifications of CH-47D/SD Chinook
Role & Specifications
The CH-47D/SD Chinook is a tandem rotor helicopter fitted with a triple hook system. It is powered by two Honeywell 55-L-714A turbo-shaft engines. The Chinook is employed for various roles such as Search and Rescue (SAR) operations, casualty evacuation, troop lift, fire-fighting, para-jumping and internal/underslung cargo transport. Besides supporting SAF’s operational requirements, the Chinooks have also been deployed for numerous Humanitarian Aid and Disaster Relief (HADR) missions.
Specifications of CH-47D/SD Chinook
Length | 30.18 m |
Height | 5.70 m |
Rotor Diameter | 18.29 m |
Performance | Maximum Speed - 170 Knots |
Crew Composition | 2 Pilots 1 Flight Engineer 1 Aircrew Specialist Configuration: 33/55 passengers or 24 stretchers and 2 medics |
AH-64D Apache Longbow

AH-64D Apache Longbow
Specifications of AH-64D Apache Longbow
The AH-64D Apache is a multi-mission helicopter, designed to fight and survive in day, night and adverse weather conditions. It is the first tandem-seat helicopter in the RSAF, with the pilot located in the rear seat and co-pilot in the front seat. The AH-64D Apache is equipped with a highly sophisticated Fire Control Radar (FCR), which gives it the ability to detect, classify, and prioritise stationary and moving targets both on the ground and in the air. The helicopter is powered by two General Electric T700-GE-701C Gas Turbine Engines, each producing 1,890 Shaft Horsepower (SHP).
Specifications of AH-64D Apache Longbow
Length | 17.73 m |
Height | 4.05 m, 4.95 m (Longbow) |
Wing Span | 5.23 m |
Performance | Maximum Speed - 158 Knots |
Armament | 30 mm M230 chain gun HYDRA 70 rockets AGM-114 hellfire missiles |
Crew Composition | 1 Pilot 1 Co-pilot/Gunner |
S-70B Seahawk

S-70B Seahawk
Specifications of S-70B Seahawk
With its state-of-the-art avionics, mission systems and cockpit, the Sikorsky S-70B Seahawk naval helicopter is one of the world’s most advanced naval helicopters. The S-70B is integrated to the Republic of Singapore Navy’s (RSN) Formidable class Stealth Frigates and operates as an integral unit in the conduct of Anti-Surface Warfare (ASuW) and Ant-Submarine Warfare (ASW) missions.
Specifications of S-70B Seahawk
Weight | 9,600 kg |
Performance | Maximum Speed - 140 Knots Endurance - 3 hours Hover Ceiling - 2,200 m |
Crew Composition | 2 Pilots 1 Tactical Coordination Officer 1 Sensor Supervisor |
Trainer
M-346

M-346
Specifications of M-346
Specifications of M-346
Overall Length | 11.49 m |
Overall Height | 4.76 m |
Wing Span | 9.72 m |
Take-off Weight | 7,400 kg (clean) |
Performance | Maximum Speed: 590 kts |
PC-21

PC-21
Specifications of PC-21
Specifications of PC-21
Overall Length | 11.232 m |
Overall Height | 3.749 m |
Wing Span | 9.108 m |
Basic Take-off Weight | 3,100 kg (Aerobatics) / |
Performance | Maximum Speed: 370 kts |
Transports
G550-Airborne Early Warning

G550-Airborne Early Warning
Specifications of G550-Airborne Early Warning
The Gulfstream 550-Airborne Early Warning (G550-AEW) replaced the E-2C to provide airborne early warning. It is powered by two Rolls Royce BR710-C4-11 turbofan engines with a rated thrust of 15,385lbs. The G550-AEW is equipped with Active Electronically Scanned Array (AESA) radar, and is able to detect, track and identify aerial targets from a longer range than its predecessor. This allows the RSAF to identify potential aerial threats early and respond decisively, in peace and war.
Specifications of G550-Airborne Early Warning
Length | 29.8 m |
Height | 8.3 m |
Wing Span | 28.5 m |
Performance | Maximum speed - 0.82 Mach Service Ceiling - 41,000 ft Endurance - 9 Hours |
Crew Composition | 2 Pilots 6 Air Warfare Officers |
A330 Multi-Role Tanker Transport

A330 Multi-Role Tanker Transport
Specifications of A330 Multi-Role Tanker Transport
The Airbus A330 Multi-Role Tanker Transport (A330-MRTT) is a next generation tanker aircraft capable of conducting Air-to-Air Refuelling (AAR) and airlift roles simultaneously. The A330-MRTT has better endurance, cargo and passenger capacity, and ability to provide more fuel to other aircraft compared to the KC-135R aerial tankers, and will replace the ageing KC-135R. Its AAR capability will allow the Republic of Singapore Air Force (RSAF) to extend the endurance of our fighter aircraft to safeguard our skies, and also enable the RSAF to be more effective and capable in meeting our operational demands. In addition, the platform provides the RSAF with greater operational flexibility and will enhance Singapore’s ability to contribute to international Humanitarian Assistance and Disaster Relief (HADR) missions and Peace Support Operations.
Air-to-Air Refuelling Capabilities. The A330-MRTT can carry 245,000 lbs (111,000 kg) of fuel for its own use or for offload to its receiver aircraft. It can refuel both drogue-refuelled and boom-refuelled platforms, which will also enhance the RSAF’s interoperability with other air forces. Additionally, the A330-MRTT is equipped with the Universal Aerial Refuelling Receptacle Slipway Installation (UARRSI), which allows it to receive fuel from another tanker aircraft. This will increase the endurance and range of the A330-MRTT to fulfil its mission during extended operations.
Airlift Capabilities. Apart from AAR operations, the A330-MRTT has the ability to carry up to 82,000 lbs (37,000 kg) of cargo or 266 personnel. This flexibility allows the aircraft to be configured expeditiously for a wide range of airlift missions. When required, the aircraft can also be equipped with medical equipment for aero-medical evacuation missions.
Aircraft Systems.
1. Avionics. The A330-MRTT is fitted with advanced avionics as well as fly-by-wire control systems featured in the civil A330 aircraft. It will also be equipped with a customised suite of military avionics.
2. Air Refuelling (AR) Systems. The AR systems are controlled from the Operator Console located in the flight deck. This arrangement facilitates pilot and operator coordination. The Aerial Refuelling Boom System (ARBS) is operated by fly-by-wire controls and electrical actuators, together with a 3-dimensional (3D) video system. The 3D video system provides the operators with a clearer and realistic visualisation of ongoing AAR operations.
Specifications of A330 Multi-Role Tanker Transport
Length | 58.8 m |
Height | 17.4 m |
Wing Span | 60.3 m |
Performance | Cruise Speed - 0.86 Mach Service Ceiling - 12.6 km Maximum Fuel Weight - 111,000 kg |
Crew Composition | Maximum Personnel Capacity - 266 personnel Maximum Cargo Capacity - 37,000 kg |
KC-135R Stratotanker

KC-135R Stratotanker
Specifications of KC-135R Stratotanker
Role & Specification
The KC-135R is a long-range jet tanker which the RSAF uses for mid-air refuelling of its aircraft. The KC-135R can also undertake aero-medical evacuation and airlift missions to provide logistics support for the SAF's overseas deployments and training exercises.
Specifications of KC-135R Stratotanker
Length | 41.76 m |
Height | 32.82 m |
Wing Span | 65.02 m |
Performance | Maximum Take-off Weight - 146,283.55 kg Maximum Cruise Speed - 0.9 Mach |
Crew Composition | Pilot, Co-pilot, Navigator, Boom Operator along with one of the following: 83,000 lbs Cargo Capacity 57 passengers 6 x 463L pallets: Max 6,000 lbs per pallet Aero-Medical Evacuation (AME) |
C-130 Hercules
.jpg)
C-130 Hercules
Specifications of C-130 Hercules
The C-130 Hercules is a four-engine turboprop military transport aircraft employed by the RSAF for a wide range of missions. The RSAF C-130 Hercules has been deployed to support the SAF’s operational requirements, including numerous Humanitarian Aid and Disaster Relief (HADR) and Search and Locate (SAL) missions.
Specifications of C-130 Hercules
Length | 30.32 m |
Height | 11.81m |
Wing Span | 40.41 m |
Performance | Maximum Speed – 290 Knots Endurance - 15 Hours Service Ceiling - 29,000 ft |
Crew Composition | 2 Pilots 1 Navigator 1 Flight Engineer 1 Loadmaster Configuration: 92 Ground Troops (72 Troops if fully equipped) 64 Fully Equipped Paratroops 74 Stretchers and 2 Medics Up to 42,000 lbs of cargo for airdrops |
Fokker-50 UTA/MPA

Fokker-50 UTA/MPA
Specifications of Fokker-50 UTA/MPA
Role & Specifications
The Fokker-50 is a twin-engine propeller aircraft employed by the RSAF for a wide range of missions. Together with the Republic of Singapore Navy (RSN), the Fokker-50 provides maritime air surveillance and protects the seaward defence and sea lines of communication of Singapore. The Fokker-50 has also been deployed in numerous Humanitarian Assistance and Disaster Relief (HADR) as well as Search and Locate (SAL) missions.
Specifications of Fokker-50 UTA/MPA
Length | 25.25 m |
Wing Span | 29.0 m |
Performance | Maximum Endurance - 8 Hours Maximum Speed - 220 Knots |
Armament | Anti-ship Missiles |
Crew Composition | MPA: 2 Pilots, 3 System Operators, 1 Loadmaster UTA: 2 Pilots, 1 Loadmaster, and one of the following: 39 fully-equipped paratroopers 21 stretchers and 2 medics 50 Passengers Cargo by ground delivery |
UAV
Hermes 450 UAV

Hermes 450 UAV
Specifications of Hermes 450 UAV
Role & Specifications
The Hermes 450 is a single engine Unmanned Aerial Vehicle (UAV) with advance composite structure and optimised aerodynamics. It has long endurance to sustain operations and improved detection capability. It is also equipped with communication system that can transfer imagery in real time.
Specifications of Hermes 450 UAV
Length | 6.1 m |
Wing Span | 10.5 m |
Performance | Cruise Speed - 60 to 70 Knots Maximum Range - 100 km Endurance - More than 14 hours |
Payload | Electro-Optical/Infrared and Laser Designator |
Heron 1 UAV

Heron 1 UAV
Specifications of Heron 1 UAV
Role & Specification
The Heron 1 is a single engine Unmanned Aerial Vehicle (UAV) equipped with advance avionics and detection capabilities that improve awareness and enhance mission effectiveness. It also has long flight endurance and it features a fully Automatic Take-off and Landing (ATOL) capability.
Specifications of Heron 1 UAV
Length | 8.80 m |
Wing Span | 16.6 m |
Performance | Cruise Speed - 60 to 70 knots Maximum Range – 200 km Endurance – Up to 24 Hours |
Payload Capacity | Electro-Optical/Infrared and Laser Designator |