Large Cabin Trijet (Legacy)
Dassault Falcon 900 (Original): Complete Specs, Performance, and Buyer's Guide (2026)
Dassault Aviation
Dassault Falcon 900 (Original): Complete Specs, Performance, and Buyer's Guide (2026)
The Dassault Falcon 900 (original variant, in production from 1986 to 1991) is Dassault's foundational large-cabin trijet and the platform that established Dassault's premier business jet positioning in the heavy-iron market. Announced in 1984, the F900 took its first flight on September 21, 1984, received certification in 1986 by French and U.S. aviation authorities, and entered service with initial deliveries in December 1986. The Falcon 900 is a development of the Falcon 50 (itself a development of the earlier Falcon 20), substantially enlarged with 5.5 ft longer fuselage, taller tail, longer wing, and 544 additional gallons of fuel allowing it to go 700 nautical miles further than its predecessor. The airframe incorporates composite materials (titanium, Kevlar, carbon fiber) for substantial weight savings while maintaining structural strength. Powered by three Garrett (later Honeywell/AlliedSignal) TFE731-5AR-1C turbofan engines (each producing 4,500 lbf of thrust, 20 kN), the Falcon 900 delivers Mach 0.84-0.87 max speed (Mach 0.85 max operating), Mach 0.80 typical cruise, 3,800-4,000 nm range (long-range mission 4,300 nm at Mach 0.75 per JetAV, max range 4,500 nm per FlyCraft), and 51,000 ft service ceiling. Cruising speed approximately 474 knots. Cabin altitude 9.3 psi differential providing sea-level cabin to 25,300 ft. The aircraft accommodates between 8 and 12 passengers standard (up to 19 maximum). Cabin: 39 ft length (excluding cockpit), 7.7 ft wide, 6.2 ft tall, 1,267 cu ft total volume. Takeoff distance 5,300 ft at sea level (8,095 ft at 5,000 ft altitude at 77°F). Crew 2. Length 20.21 m (66.3 ft), wingspan 19.33 m (63.4 ft), wing area 49.0 m². Empty weight 10,255 kg. Max takeoff weight 20,640 kg (45,500 lb). Fuel capacity 8,690 kg. Production ended 1991 with the introduction of the Falcon 900B. 177 Falcon 900 family aircraft built combined through 1999 production end. Almost all earlier Falcon 900s upgraded with -5BR engines for B-spec compliance. Pre-owned prices per Vref: $5M starting (1987 model). North America operates 69% of Falcon 900 jets, Europe 17%.
For operators wanting Dassault's foundational large-cabin trijet that established Dassault Falcon's premier business jet positioning, three-engine safety margin (overwater operations and short-field capability), composite materials airframe (titanium + Kevlar + carbon fiber for substantial weight savings), Mach 0.84-0.87 max speed, 3,800-4,000 nm intercontinental range, 51,000 ft service ceiling (industry-leading for class), and Dassault Falcon family heritage, the Falcon 900 represents Dassault's foundational large-cabin trijet platform.
Dassault Falcon 900 Specifications at a Glance
| Specification | Value |
|---|---|
| Category | Large Cabin Trijet (Legacy) |
| Production Status | Discontinued 1991 (succeeded by Falcon 900B) |
| Designation | Dassault Falcon 900 |
| Manufacturer | Dassault Aviation (France) |
| Family Heritage | Development of Falcon 50 (development of Falcon 20) |
| Announcement | 1984 |
| First Flight | September 21, 1984 |
| Certification | 1986 (French + U.S.) |
| First Delivery | December 1986 |
| Production Years | 1986 to 1991 |
| Industry Distinction | Dassault's first heavy-iron private jet |
| Industry Distinction | Foundational Dassault large-cabin trijet |
| Industry Distinction | Three-engine safety margin (overwater operations) |
| Industry Distinction | Composite airframe (titanium + Kevlar + carbon fiber) |
| Crew | 2 |
| Passengers (Standard) | 8 to 12 |
| Passengers (Maximum) | 19 |
| Engines | 3× Garrett TFE731-5AR-1C turbofans (later Honeywell/AlliedSignal) |
| Thrust per Engine | 4,500 lbf (20 kN) |
| Total Thrust | 13,500 lbf |
| Avionics | Original analog flight deck (later many upgraded) |
| Connectivity | Optional with retrofits |
| Max Speed | Mach 0.84-0.87 |
| Cruise Speed | Mach 0.80 (~474 knots) |
| Long-Range Cruise | Mach 0.75 |
| Max Range (Long-Range Mission per JetAV) | 4,300 nm (4,940 mi) |
| Max Range (Maximum per FlyCraft) | 4,500 nm (5,180 mi) |
| Initial Range Spec (per AOPA) | 3,800 nm |
| Service Ceiling | 51,000 ft (15,500 m) |
| Cabin Pressurization | 9.3 psi (sea-level cabin to 25,300 ft) |
| Cabin Length | 39 ft (excluding cockpit) |
| Cabin Width | 7.7 ft |
| Cabin Height | 6.2 ft |
| Cabin Volume | 1,267 cu ft |
| Aircraft Length | 20.21 m (66.3 ft) |
| Wingspan | 19.33 m (63.4 ft) |
| Wing Area | 49.0 m² |
| Empty Weight | 10,255 kg (22,608 lb) |
| Max Takeoff Weight | 20,640 kg (45,500 lb) |
| Fuel Capacity | 8,690 kg (19,158 lb) |
| Takeoff Distance (Sea Level) | 5,300 ft |
| Takeoff Distance (5,000 ft / 77°F) | 8,095 ft |
| Stall Speed | 158 km/h |
| Production Total (All 900 Family Through 1999) | 177 aircraft |
| Pre-Owned Price (per Vref 1987 model) | $5,000,000 starting |
| New List Price (Original) | $21,000,000 (per FlyCraft) |
| Hourly Charter Rate (per FlyCraft) | $6,300 |
| Annual Operating Cost Estimate | $1,500,000 |
| Fuel Burn | 303 GPH |
History as Dassault's Foundational Heavy-Iron Trijet
The Falcon 900 represents Dassault Aviation's strategic decision to enter the heavy-iron private jet market with substantial industry-leading capabilities.
Platform timeline:
- 1963: Falcon 20 launched (Dassault's foundational business jet)
- 1979: Falcon 50 launched (3-engine development of Falcon 20)
- 1984: Falcon 900 announced (substantially larger development of Falcon 50)
- September 21, 1984: Falcon 900 first flight
- 1986: French + U.S. certification
- December 1986: First customer deliveries
- 1986-1991: Original Falcon 900 production
- 1991: Falcon 900B introduced (successor)
- 1999: Falcon 900B production ended (succeeded by 900C and 900EX)
- Total Falcon 900 Family Production: 525 units (per Military Factory)
Per FlyCraft: "The Falcon 900 was Dassault's first foray into the heavy-iron private jet market."
Why the Falcon 900 Is Industry-Foundational
The original Falcon 900 introduced industry-defining capabilities:
1. Three-Engine Trijet Configuration
The defining Falcon 900 advantage:
- First-rate short-field capabilities: Modern positioning
- Outstanding rates of climb: Industry-leading
- Extra margin of safety for overwater work: Premium positioning
- Industry-distinct vs twin-engine large cabin: Premium
2. Composite Airframe (Titanium + Kevlar + Carbon Fiber)
- Lightweight construction: Modern engineering
- Industry-leading for era: Premium positioning
- Industry-distinct vs aluminum competitors: Modern
- Allows shorter takeoff distance: Premium positioning
- Industry-leading for era: Modern
3. 3,800-4,000 nm Range with Three Engines
- Intercontinental capability: Premium positioning
- Industry-leading for heavy-iron era: Modern
- 8-12 passenger comfort: Premium positioning
- London to central United States or middle China: Premium
4. 51,000 ft Service Ceiling
- Industry-leading for class: Premium
- Above weather + traffic: Premium positioning
- Modern operational envelope: Premium
5. Mach 0.84-0.87 Max Speed
- Industry-leading for era: Premium positioning
- Mach 0.80 typical cruise: Modern
- 474 knot cruise: Premium
6. 9.3 psi Cabin Pressurization
- Sea-level cabin to 25,300 ft: Industry-leading
- Premium positioning: Modern
- Industry-leading for era: Premium
7. Substantial Cabin (1,267 cu ft)
- 39 ft cabin length excluding cockpit: Industry-leading
- 7.7 ft cabin width: Premium
- 6.2 ft cabin height: Industry-leading for class
- 8-12 passengers standard, up to 19: Premium
8. Garrett TFE731-5AR-1C Engines
- 4,500 lbf thrust each: Standard for era
- TFE731 family proven: Modern reliability
- Three engines total: Premium safety margin
- 13,500 lbf total: Industry-leading
Cabin Interior
The Falcon 900 cabin features industry-leading large dimensions for the era:
| Cabin Measurement | Value |
|---|---|
| Cabin Length | 39 ft (excluding cockpit) |
| Cabin Width | 7.7 ft |
| Cabin Height | 6.2 ft |
| Cabin Volume | 1,267 cu ft |
| Cabin Pressurization | 9.3 psi |
| Cabin Altitude at 51,000 ft | Sea-level cabin to 25,300 ft |
Standard Configuration
- 8 to 12 Passengers Standard: Premium positioning
- Up to 19 Passengers Maximum: Premium maximum
- Forward Club Seating: Premium social
- Conference / Dining Area: Premium business
- Rear Sleeping Cabin: Premium private
- Forward Lavatory: Standard
- Aft Lavatory: Standard
- Galley: Premium dining
Cabin Features
- 39 ft cabin length (excluding cockpit): Industry-leading for class
- 6.2 ft stand-up cabin: Premium positioning
- 7.7 ft cabin width: Industry-leading
- 1,267 cu ft cabin volume: Premium
- Sea-level cabin to 25,300 ft (9.3 psi): Industry-leading
- Premium fit + finish: Dassault heritage
- Modern customization potential: Standard
- Premium luxury: Industry-leading for era
Performance
Speed and Range
| Performance Metric | Value |
|---|---|
| Max Speed | Mach 0.84-0.87 |
| Typical Cruise | Mach 0.80 (~474 knots) |
| Long-Range Cruise | Mach 0.75 |
| Max Range (Long-Range Mission per JetAV) | 4,300 nm |
| Max Range (Maximum per FlyCraft) | 4,500 nm |
| Initial Range Spec (per AOPA) | 3,800 nm |
| Service Ceiling | 51,000 ft |
Runway Performance
| Field Performance | Value |
|---|---|
| Takeoff Distance (Sea Level) | 5,300 ft |
| Takeoff Distance (5,000 ft / 77°F) | 8,095 ft |
| MTOW | 45,500 lb (20,640 kg) |
| Industry-leading short field | Premium positioning |
Typical Mission Examples
- New York to Los Angeles (~2,500 nm) - non-stop very comfortable
- Coast-to-coast U.S.: Premium positioning
- London to central United States (~4,000 nm) - non-stop close to limit
- London to middle China (~4,500 nm) - non-stop achievable
- Premium positioning: Industry-leading
Engines
Three Garrett TFE731-5AR-1C turbofan engines (later Honeywell/AlliedSignal branding), each producing 4,500 lbf of thrust (20 kN).
Key features:
- TFE731-5AR-1C family: Modern proven for era
- 4,500 lbf per engine: Premium thrust class
- 13,500 lbf total: Industry-leading three-engine
- Premium reliability: TFE731 family proven
- Industry-leading commercial heritage: Premium
- 303 GPH fuel burn: Standard for class
Avionics
Original analog flight deck (many later upgraded):
- Original 1986 analog instrumentation: Standard for era
- Many later upgraded with Honeywell Primus: Modern retrofits
- Modern integration available: Premium retrofit
- TCAS, EGPWS retrofit available: Standard
- Modern weather radar retrofit available: Premium
Operating Costs
| Cost Item | Per Hour |
|---|---|
| Fuel (303 GPH) | $2,727 to $3,030 |
| Engine Reserve (3 engines) | $900 |
| Airframe Maintenance | $1,200 |
| Insurance + Hangar | $500 |
| Crew | $800 |
| Other Variable | $200 |
| Total Direct Operating Cost (Estimated) | ~$6,300/hr (per FlyCraft charter) |
Annual operating budget estimate: $1.5M per FlyCraft.
Pricing
| Year/Status | Price |
|---|---|
| Pre-Owned 1987 Model (per Vref) | $5,000,000 starting |
| Pre-Owned Acquisition (per FlyCraft) | $12,000,000 to $15,000,000 |
| Pre-Owned Recent (per FlyCraft) | $7,000,000 to $9,000,000 |
| Original New List Price (per FlyCraft) | $21,000,000 |
| Hourly Charter Rate | $6,300 |
Mission Profile
Best fit profiles:
- Three-Engine Safety Operators: Premium positioning (overwater operations)
- Step-Up From Falcon 50: Substantially more cabin + range
- Entry-Level Heavy-Iron Operators: Modest acquisition cost vs modern variants
- Multi-Generational Operators: Premium positioning
- Operators Valuing Composite Airframe: Modern engineering
- 51,000 ft Operators: Industry-leading
- Operators Valuing Short-Field with Heavy Iron: Industry-distinct
- Premium Dassault Heritage Operators: Industry-leading
Less suited if:
- You need modern glass cockpit (consider Falcon 900EX with Primus 2000)
- You require 4,500+ nm range consistently (consider Falcon 900EX or LX)
- You require modern fuel efficiency (consider Falcon 900LX winglets)
- You require modern avionics certification (RVSM, ADS-B require retrofit)
Pros and Cons
What the Falcon 900 Does Well
- 3,800-4,500 nm range
- Mach 0.84-0.87 max speed
- Mach 0.80 typical cruise (~474 knots)
- 51,000 ft service ceiling (industry-leading)
- Three Garrett TFE731-5AR-1C engines (4,500 lbf each)
- 13,500 lbf total thrust
- Three-engine trijet safety margin
- Composite airframe (titanium + Kevlar + carbon fiber)
- 39 ft cabin length (excluding cockpit)
- 7.7 ft cabin width
- 6.2 ft cabin height
- 1,267 cu ft cabin volume
- 9.3 psi cabin pressurization
- Sea-level cabin to 25,300 ft
- 8-12 passengers standard (up to 19 maximum)
- 5,300 ft takeoff distance (sea level)
- 45,500 lb MTOW
- 8,690 kg fuel capacity
- $5M starting pre-owned (1987 model per Vref)
- Premium Dassault heritage
- Modern operational versatility
- Worldwide Dassault service network
- Strong residual value within legacy market
- 177 aircraft production (substantial fleet)
- North America operates 69% of fleet
- Modern customization potential
Tradeoffs to Understand
- Production ended 1991 (succeeded by 900B)
- Original analog flight deck (requires retrofits for modern compliance)
- 303 GPH fuel burn substantial
- Three-engine maintenance vs twin-engine modern alternatives
- Range less than modern Falcon 900EX (3,800-4,500 vs 4,500+ nm)
- Older avionics vs modern variants
Frequently Asked Questions
How is the Falcon 900 different from the Falcon 900B?
The Falcon 900B (1991-1999 succeeded the original Falcon 900 (1986-1991). Key improvements: more powerful TFE731-5BR-1C engines (4,750 lbf vs original 4,500 lbf), increased range, modest performance improvements. Almost all earlier Falcon 900s were upgraded with -5BR engines for B-spec compliance per AOPA.
How is the Falcon 900 different from the Falcon 50?
The Falcon 900 is a substantially enlarged development of the Falcon 50. Key differences: 5.5 ft longer fuselage, taller tail, longer wing, 544 additional gallons of fuel allowing 700 nm further range, three TFE731-5AR-1C engines (vs Falcon 50's three engines), substantially larger cabin (39 ft vs Falcon 50's smaller cabin). Both share three-engine trijet configuration and Dassault heritage.
What engines power the Falcon 900?
Three Garrett TFE731-5AR-1C turbofan engines (later Honeywell/AlliedSignal branding), each producing 4,500 lbf of thrust (20 kN). Total thrust: 13,500 lbf. Almost all earlier Falcon 900s were later upgraded with TFE731-5BR-1C engines for B-spec compliance.
How far can a Falcon 900 fly?
The Falcon 900 has a long-range mission of 4,300 nm at Mach 0.75 per JetAV (4,940 mi). Maximum range is 4,500 nm per FlyCraft. Initial range spec at launch was 3,800 nm per AOPA. This enables London to central United States (~4,000 nm) or London to middle China (~4,500 nm) non-stop.
Why is the Falcon 900 a three-engine trijet?
The trijet configuration provides three primary advantages: (1) first-rate short-field capabilities, (2) outstanding rates of climb, and (3) extra margin of safety for overwater work. The Falcon 50 (predecessor) also used three engines, and Dassault maintained this configuration as a competitive differentiator vs twin-engine large-cabin alternatives.
What's the Falcon 900's service ceiling advantage?
The Falcon 900 achieves 51,000 ft service ceiling (industry-leading for class) with 9.3 psi cabin pressurization providing sea-level cabin to 25,300 ft. This enables operation above most weather + traffic for substantially smoother flights.
When did Falcon 900 production end?
The original Falcon 900 was in production from 1986 to 1991, succeeded by the Falcon 900B (with more powerful TFE731-5BR engines). The Falcon 900B remained in production until succeeded by the 900C and 900EX. Total Falcon 900 family production reached 525 units per Military Factory.
What's the Falcon 900 pre-owned market like?
Per Vref (cited in AOPA), Falcon 900 prices start at $5M for a 1987 model. Per FlyCraft, acquisition cost typically ranges $12-15M (likely for upgraded variants with modern retrofits). Pre-owned recent transactions can be within $7-9M for early variants. Annual operating cost ~$1.5M.
Who flies Falcon 900 aircraft?
The Falcon 900 is operated by a diverse range of private owners, businesses, small airlines, and military forces worldwide. Countries including Libya, Qatar, Saudi Arabia, Bolivia, France, Germany, Italy, Japan, Malaysia, and many others have incorporated the Falcon 900 into their fleets for various purposes from VIP transport to maritime patrol. North America operates 69% of the fleet, Europe 17%. The French Transport Squadron 60 operates Falcon 900s for VIP transport of French government officials.
The Bottom Line
The Dassault Falcon 900 (original variant, in production from 1986 to 1991) represents Dassault Aviation's foundational large-cabin trijet and the platform that established Dassault's premier business jet positioning in the heavy-iron private jet market. With substantial industry-defining capabilities (three-engine trijet configuration providing first-rate short-field capabilities + outstanding rates of climb + extra margin of safety for overwater work as a competitive differentiator vs twin-engine large-cabin alternatives, composite airframe construction with titanium + Kevlar + carbon fiber materials providing substantial weight savings while maintaining structural strength, 3,800-4,000 nm intercontinental range with capability for long-range missions of 4,300 nm at Mach 0.75 per JetAV with maximum range 4,500 nm per FlyCraft, Mach 0.84-0.87 max speed with Mach 0.80 typical cruise around 474 knots, 51,000 ft service ceiling industry-leading for class with 9.3 psi cabin pressurization providing sea-level cabin to 25,300 ft, substantial cabin of 39 ft length excluding cockpit + 7.7 ft width + 6.2 ft height + 1,267 cu ft volume), the Falcon 900 delivered Dassault's premier foundational heavy-iron trijet. Three Garrett TFE731-5AR-1C turbofan engines (later Honeywell/AlliedSignal branding, 4,500 lbf thrust each, 20 kN, 13,500 lbf total) provide premium reliability with three-engine safety margin. The Falcon 900 is a development of the Falcon 50 (itself a development of the earlier Falcon 20) substantially enlarged with 5.5 ft longer fuselage + taller tail + longer wing + 544 additional gallons of fuel allowing 700 nm further range than its predecessor. Announced in 1984. First flight: September 21, 1984. Certification: 1986 by French and U.S. aviation authorities. First customer deliveries: December 1986. Per FlyCraft: "The Falcon 900 was Dassault's first foray into the heavy-iron private jet market." Standard configuration accommodates 8-12 passengers (up to 19 maximum) in a cabin featuring forward club seating + conference/dining area + rear sleeping cabin + forward and aft lavatories + galley. Aircraft: 20.21 m length (66.3 ft), 19.33 m wingspan (63.4 ft), 49.0 m² wing area, 10,255 kg empty weight, 20,640 kg MTOW (45,500 lb), 8,690 kg fuel capacity (19,158 lb). Takeoff distance: 5,300 ft at sea level (8,095 ft at 5,000 ft altitude at 77°F). The Falcon 900 production ended 1991 with the introduction of the Falcon 900B (more powerful TFE731-5BR-1C engines and increased range). Almost all earlier Falcon 900s were later upgraded with -5BR engines for B-spec compliance. Total Falcon 900 family production reached 525 units per Military Factory. Pre-owned market: $5M starting (1987 model per Vref), acquisition cost typically $12-15M per FlyCraft. New original list price was $21M per FlyCraft. Hourly charter rate: $6,300. Annual operating cost estimate: $1.5M. Fuel burn: 303 GPH. Operated by private owners, businesses, small airlines, and military forces worldwide including French Transport Squadron 60 for French government VIP transport. North America operates 69% of the fleet, Europe 17%. Dassault worldwide service network continues to support the Falcon 900 platform.
Quantum Jets supports the platform across private jet charter, private jet rental, private jet card programs, aircraft purchase, jet purchase, jet sales, aircraft sales, aircraft management, jet management, private jet management, aircraft maintenance, aircraft refurbishment, fractional jet access, aircraft lease, and aircraft leasing structures.
Talk to a Quantum Jets broker for Falcon 900 market intelligence and pre-buy diligence.
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Dassault Falcon 900 (Original) Services from Quantum Jets
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Related Aircraft Guides:
- Dassault Falcon 900B: Direct Successor (1991-1999)
- Dassault Falcon 900C: Mid-Range Successor (1999-2009)
- Dassault Falcon 900EX: Long-Range Successor (1996-2009)
- Dassault Falcon 900LX: Current Production Modern Successor
- Dassault Falcon 50: Smaller Predecessor (Three-Engine Trijet)
- Dassault Falcon 50EX: Modern Falcon 50 Variant
- Dassault Falcon 2000: Twin-Engine Sibling
- Gulfstream G-IV: Direct Twin-Engine Heavy-Iron Competitor
Production of the Dassault Falcon 900 ended 1991. All acquisitions are pre-owned. Dassault Aviation provides worldwide parts/support. Specifications accurate as of 2026.