T-100 Integrated
Training System    T-100: MORE THAN AN AIRCRAFT
T-100: MORE THAN AN AIRCRAFT
The T-100 is a two-engine, tandem-seat, next            Key attributes include:
generation advanced jet trainer, key element of a       •	 Carefree handling capabilities throughout the flight
family of systems designed to enable student pilots        envelope
                                                        •	 ETTS for advanced Air-to-Air and Air-to-Ground training
to develop the knowledge, skills and habits required    •	 Live Virtual Constructive networking capability
of a combat aircraft pilot.                             •	 Two latest generation “0-0” capability ejection seats
                                                           complying with the stringent APT FOS requirements
The T-100 is purpose-designed for a wide range of       •	 Front and rear cockpit Head-Up Displays with 5th
                                                           generation fighters’ symbology
training missions, long-term reliability and cost-
                                                        •	 Two independent Helmet Mounted Displays (provision for)
effective operations. These characteristics – along     •	 Two Large Area Displays
with its in-service proven Integrated Training System   •	 NVG capability
                                                        •	 Comfortable environment and wide Field of View in both
(ITS) solution comprised of Simulators and Ground
                                                           cockpits
Based Training devices, include the most advanced       •	 No scheduled depot-level structural inspections
and already operational Live, Virtual, Constructive     •	 In service with the air forces of Israel, Singapore, Italy
                                                           and Poland
environment in the world – make the T-100 ITS a low-
cost, low-risk, and proven solution to train today’s    Weights
next generation military pilots.                        Ramp, Clean (2 standard pilots)	      15,870 lb (7.200 kg)
                                                        Ramp, Maximum	                        21,200 lb (9.600 kg)
The updated cockpit avionics with the latest            Powerplant
Large Area Display (LAD) and the advanced               Engines, turbofan	                    2 Honeywell/
mission management suite offered by the T-100’s         	                                     ITEC F124-GA-200
Embedded Tactical Training Simulation (ETTS),           Thrust, Maximum, SLS, ISA 	           2x6, 280 lb (2x2850 kg)
make the T-100 truly representative of the 5th          Performance
generation combat aircraft.                             Maximum level Speed, 5000 ft	         590 KTAS
                                                        Limit speed	                          572 KEAS / 0.95M
The T-100 exposes student pilots to the performance     	                                     500 KEAS / 1.15M
and handling qualities experienced in 5th generation    Rate of Climb, Max
fighters, while managing the flow of information and    (SL, 100% fuel)	                      24,000 ft/min
associated tasks to operate in a modern network         Sustained Turn Rate, Max
centric combat environment.                             (15,000 ft, 50% fuel)	                12.9 deg/s
                                                        Sustained Load Factor, Max
                                                        (SL, 50% fuel)	                       8g
                                                        Service ceiling	                      45,000 ft
                                                        Take-off Ground Run
                                                        (SL, 100% fuel, no wind, no slope)	   1,300 ft (400 m)
                                                        Landing Ground Roll
                                                        (SL, 20% fuel, no wind, no slope)	    2,150 ft (655 m)
                                                        Limit Load Factors	                   +8 / -3 g
                                                                                                                        T-100.us
MORE THAN AN AIRCRAFT
INTEGRATED TRAINING SYSTEM
INTRODUCING THE TRAINER OF THE FUTURE
The T-100 is more than just an aircraft. It’s
a turnkey solution for the U.S. Air Force’s
T-X program.
Team T-100 is comprised of CAE USA for
ground based training, Honeywell for propulsion
engines, Leonardo Aircraft’s world-class aircraft
and integrated training system and Leonardo
DRS to tie it all together. We’re proud to be the
only T-X team building a new U.S. tactical aircraft
manufacturing facility.
For years to come, the T-100 will bring high-tech
jobs in aircraft and training system production to
America. Making it the right choice not only for
our pilots, but for our country, today and in
the future.
ADVANCED JET AND LEAD-IN                               A FAMILY OF SYSTEMS FOR TRAINING
FIGHTER TRAINER
                                                       In its training role, the T-100 is conceived as the “core”
The T-100 is a twin-engine, tandem-seat, next          of a family of systems for advanced aircrew training
generation advanced jet trainer, and the central       which includes:
element of a family of systems for training designed
to allow student pilots to develop knowledge, skills   •	Aircraft with built-in Embedded Tactical Training
and practices to fly modern combat aircraft.              Simulation (ETTS)
                                                       •	Suite of flight simulators (Weapons System Trainer
The T-100 is purpose-built for a wide range of            and Operational Flight Trainer)
training capabilities, long-term reliability and       •	Academic training (Computer Aided Instruction
cost-effective operations. These characteristics –        and Computer Based Training to include Desktop
along with its proven integrated training system          Simulators)
comprised of Simulators and Ground Based               •	Mission Planning (Mission Support Station to
Training devices, including the most advanced and         support Briefing and De-briefing phases)
already operational Live, Virtual, and Constructive    •	Live, Virtual, Constructive (LVC) training
environment – make the T-100 the best solution to         environment (the ability to link flight simulators with
train today’s next generation fighter pilots.             the aircraft)
                                                       •	Training Need Analysis (TNA) and Training
The T-100 characteristics maximize teaching               Management Information System (TMIS)
effectiveness and enable flight hours to be            •	 Integrated Logistic Support
downloaded from front two-seat versions of front
line aircraft, allowing a huge saving in the Air
Force’s operational training costs, and preserves
service life on the front line fighters.
The aircraft is designed to meet the rigorous
training needs of the U.S. Air Force (USAF).
Building upon the proven technology and systems
of Leonardo’s M-346, the T-100 incorporates best-
in-class U.S. industry technology to provide USAF
with the capability it needs today to meet the
requirements of tomorrow.
MAIN FEATURES                                        AVIONICS
Airframe                                             •	 Latest generation cockpit avionics
                                                     •	Embedded GPS/Inertial navigation system and
•	Damage tolerant designed structure 25% more          Radar altimeter (EGIR)
   service life than what the USAF is asking for     •	 Two V/UHF radios
•	 Large use of composite materials                  •	 IFF transponder
                                                     •	TCAS
Engines & Fuel System                                •	Radio-Aided mode, based on TACAN and VOR/
                                                        ILS/MB
•	Two fuel efficient interchangeable modular        •	 Digital Moving Map
   Honeywell/ITEC F124-GA-200, twin-shaft,           •	 Voice command (provision for)
   turbofan engines with FADEC                       •	 Hands On Throttle And Stick (HOTAS) controls
•	An APU to provide autonomous engine               •	Two 20”X 8” Large Area Displays (LAD) in front
   start, electrical and pneumatic power (air           and rear cockpit
   conditioning)                                     •	New Digital Wave Guided Low Profile Head-Up
•	 Three internal fuel tanks                            Display (HUD)
•	Single point pressure refueling/defueling         •	 Get Home Display, for back up flight data
   system                                            •	Provision for two independent Helmet Mounted
                                                        Displays
Crew Escape                                          •	 Avionics Integrated Stores Management System
                                                     •	 Integrated central Audio Warning
•	Two latest generation “0-0” capability ejection
   seats complying with the stringent APT FOS
   requirements
Oxygen
•	 On-Board Oxygen Generator System (OBOGS)
EMBEDDED TACTICAL TRAINING
SIMULATION (ETTS)
A comprehensive in-flight ETTS suite is a key feature
of the T-100 and flight simulators and a core element
of the family of systems for advanced training.
ETTS enables the T-100 to offer the whole spectrum
of simulated training functions in flight and on the
ground and provides both students and instructors
with the following on-board simulations:
•	A tactical scenario (digital map with threats
   and targets)
•	Presence of realistic Computer Generated Forces
   (friend and foe)
•	On-board sensors (such as multimode Fire Control
   Radar, targeting pod and active/passive electronic
   countermeasures)
•	Weapons, including specific symbology and
   delivery parameters
•	Live, Virtual, Constructive capability to link aircraft
   with flight simulators
ETTS functions can support Stand Alone (flying
a single-ship mission) or Multi-Ship networked
operations, with aircraft and simulators networked
via a dedicated Training Datalink to exchange
Tactical Scenario data with other participants.
T-100: MASTER IN TRAINING
Thanks to the excellent, proven in-service, advanced
Lead-In Fighter Trainer capabilities and high
performances, the T-100 aircraft can smoothly
enable student pilots to accomplish all their training
tasks in flight.
Amongst the characteristics which make the T-100
the safest aircraft for student pilots are:
•	Carefree handling and throttle movements in the
   whole flight envelope
•	 Four channel fly-by-wire flight control system
•	 Twin engine configuration
•	 Low wing loading providing more margin for error
•	Automatic Ground Collision Avoidance System
   (Auto GCAS)
•	 Pilot Activated Recovery System (PARS)
•	Unique engine design stall/surge resistant with
   auto relight
Thanks to non-afterburning engines, its high training
endurance keeps costs down and is best tailored
to the training mission’s duration to deliberately
perform the required training syllabus objectives, in
a more effective and efficient way.
HIGH PERFORMING AIRCRAFT                               THE BEST SOLUTION FOR THE MOST
                                                       DEMANDING AIR FORCES
The T-100 exposes student pilots to the agility
and flight characteristics experienced in the front    The T-100 is an evolution of the proven, in-service
line 5th generation fighters, and exposes the          Leonardo M-346 that has won the most important
student pilot to the flow of information required to   international tenders and has been selected
easily manage a modern network centric combat          by some of the most demanding Air Forces in
environment.                                           the world, beating the most advanced training
                                                       aircraft available on the market, delivering first
Key attributes include:                                class training and operational capabilities, while
•	 Full controllability at High Angle of Attack        keeping operating costs low. The M-346 is in
•	 High rate of climb                                  service with the Israeli, Singaporean, Italian and
•	High speed and maneuverability, even with one       Polish Air Forces.
   engine inoperative
•	 Sustained high G maneuvers
•	 High thrust to weight ratio
•	 High-end, net-centric communication suite
•	 Full network capable LVC environment
Israel: “The new trainers [M-346 Lavi] have provided       Italy: “The T-346 has striking performance: the
manifold advantages and take [pilot] training much         generous thrust, the roll rate and, in general, the
more forward. It has met all our expectations and          high stability at all speeds. The strength of the
more. The aspects of the flight performance, its           ‘346’ is surely the ETTS, the integrated simulation
specifications, the capabilities it has, the savings in    platform, which allows you to play a variety of
jet fuel, the safety from it being dual-engine, it has     sensors such as radar, targeting pod, [and] a suite
redundancy in almost every system on the plane. We         of electronic countermeasures, to name a few.
are very, very, very satisfied.”                           All these sensors can be employed with other
                                                           aircraft of the same type as if they were real and,
Lt. Col. Tal, Heyl Ha’Avir (Israeli Air Force) in charge   at the same time, also interacting with ground
of M-346 Lavi operations                                   simulators to re-create an environment typical of
July 21, 2016 – The Times of Israel                        that of the latest generation combat aircraft.”
                                                           Lt. Col. “Sossi”, instructor pilot of 61° Stormo,
                                                           Italian Air Force
                                                           March 2016 – Combat Aircraft Magazine
Italy: “The T-346 is not just an aircraft in its own     Poland: “The M-346 aircraft really is the best, and
right, but part of an integrated system that is a real   at the same time the most economical solution,
revolution compared to the past. The ground element      compared to the current system. Since training will
of the IPTS [Integrated Pilot Training System]           be cheaper, this means more savings for the Polish
employs modern simulation systems [that enable           Air Force. But what is more interesting about this
us to] ‘download’ a good slice of the activities that    project, is the fact that we could become a training
were previously carried out at the OCU and that          center for other countries in the future. We have
were previously conducted in flight, thereby bringing    such capabilities, thanks to the school in Dęblin.”
substantial savings.’
                                                         Bartosz Kownacki, Vice-minister of
Col. Paolo Tarantino, Commander of the 61° Stormo,       National Defense
Italian Air Force                                        June 8, 2016 – “Nasz Dziennik” Polish newspaper
March 2016 – Combat Aircraft Magazine
                                                      T-100 CHARACTERISTICS
On-Condition and Condition Monitoring
maintenance for equipment and systems. Two            Dimensions
level maintenance concept (Organizational and
                                                      Wing span                                        31.90 ft (9.72 m)
Intermediate) for aircraft, equipment and systems.
Structural depot level maintenance is not required.   Length                                           37.70 ft (11.49 m)
Health & Usage Monitoring System (HUMS)               Height                                           16.11 ft (4.91 m)
enables monitoring of on-board equipment and          Wing Area                                        253.2 ft² (23.52 m²)
data collection, in addition to airframe structural
                                                      Weights
health (S-HUMS). The Ground Support System
allows a rapid assessment of the aircraft systems     Ramp, Clean (2 standard pilots)                  15,870 lb (7200 kg)
status, reducing troubleshooting, scheduled and       Ramp, Maximum                                    21,200 lb (9600 kg)
unscheduled maintenance activities.                   Wing Loading
                                                      At Take-Off Weight, Clean                        62.7 lb/ft²
                                                      Powerplant
                                                      Engines, Turbofan                                2 Honeywell/ITEC F124-GA-200
                                                      Thrust, Maximum, SLS, ISA                        2x6,280 lb (2x2850 kg)
                                                      Fuel, Usable
                                                      Internal (wings and fuselage)                    3,350 lb (1520 kg)
                                                      Performance
                                                      Maximum Level Speed, 5000 ft                     590 KTAS
                                                      Limit Speed                                      572 KEAS / 0.95M /
                                                                                                       500 KEAS / 1.15M
                                                      Stall Speed (landing conf., 20% fuel)            97 KCAS
                                                      Thrust Over Weight Ratio (SL, 100%)              0.79
                                                      Rate of Climb, Max (SL, 100% fuel)               24,000 ft/min
                                                      Sustained Turn Rate, Max (15,000 ft, 50% fuel)   12.9 deg/s
                                                      Sustained Load Factor, Max (SL, 50% fuel)        8g
                                                      Service Ceiling                                  45,000 ft
                                                      Take-off Ground Run                              1,300 ft (400 m)
                                                      (SL, 100% fuel, no wind, no slope)
                                                      Landing Ground Roll                              2,150 ft (655 m)
                                                      (SL, 20% fuel, no wind, no slope)
                                                      Limit Load Factors                               +8 / -3 g
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