DASSAULT FALCON 900B Model Guide
DASSAULT FALCON 900B · Model Guide
Overview
DASSAULT FALCON 900B is a turbofan business jet. The registry lists the Falcon 900 family (variants 900, 900EX) at up to 4330 nm range, 428 kt cruise, 51000 ft ceiling and up to 18 passengers. Variant-specific figures are not in our sources. This guide draws on the maintenance manual's airworthiness limitations and an operator's normal checklist.
- Family-level registry maxima: 4330 nm range, 428 kt cruise, 20600 kg MTOW, 18 passengers, 51000 ft ceiling. These are not 900B-specific.
- Airworthiness limits run to a design service goal of 20,000 flights/30,000 flying hours. Mandatory tasks cannot be changed or deleted.
- Ask for proof of compliance with Chapter 5-40, Revision 26 (September 2021). Non-compliance suspends the airworthiness certificate.
- Regular cargo, training, search and rescue or other non-passenger use means the aircraft is not a 'Standard Aircraft' for the fatigue program.
Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.
Reference only, not for flight. Use the current approved manual for your aircraft. See terms, section 5.
Document
Source
Copy found at sprinkle.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type ·
- Model Guide
- Year ·
- 2026
- File size ·
- 47 KB
- Copy found at ·
- sprinkle.com
What range does the DASSAULT FALCON 900B have?
Our sources give no 900B-specific figure. DASSAULT FALCON 900B belongs to a family listed at up to 4330 nm range and 428 kt cruise. Confirm the actual figure in the aircraft's flight manual.
How long is the DASSAULT FALCON 900B's design service life?
For the DASSAULT FALCON 900B, the airworthiness limitations run to a design service goal of 20,000 flights/30,000 flying hours, per Falcon 900 maintenance manual Chapter 5-40.
What is the DASSAULT FALCON 900B Model Guide?
The DASSAULT FALCON 900B Model Guide is a model guide for the DASSAULT FALCON 900B, dated 2026.
What year was the DASSAULT FALCON 900B Model Guide published?
The DASSAULT FALCON 900B Model Guide — the DASSAULT FALCON 900B model guide on file — is dated 2026.
Common. More common than 94% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the DASSAULT FALCON 900B.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
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In this document
Life-limited parts
Main and nose landing gear legs are limited to 20000 LDG each. Inboard flap screw jacks (P/N 5318-3) are overhauled at 3500 LDG and outboard at 4500 LDG. Seat safety belt assemblies have a life limit of 60 M, with a buckle spring inspection at 18 M. Eddy-current inspection of flap tracks 2 and 5 is due at 8855 FC, then every 4770 FC.
Recurring mandatory checks
The flap asymmetry detection test is due every 450 FH on aircraft with the AVIAC flap control system and every 1800 FH on those with DED. Confirm which system the aircraft has. Flight control hydraulic components get an integrity, corrosion and leak check every 4000 FH. Flap screw/nut play checks recur at 330 FH to 630 FH, depending on part number.
Operator checklist notes
The DM Air normal checklist (VER 3.1) covers APU start, 3 windshield heats, trims (5), stall tests and an oxygen mask test. Its listed climb profile is 300/.80 260/.72. Use it as a reference for what the systems should test as normal during a pre-buy flight.
Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.
Safety notes
- Failure to comply with Chapter 5-40 leads to immediate suspension of the airworthiness certificate.
- Modifications not approved by Dassault (STC, PMA) are not covered by the limitations. Non-standard aircraft need an adapted program.
- Corrosion level 2 or 3 on principal structural elements must be reported. Structure must be kept at level 1 or better.
Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.
Full document text
DASSAULT FALCON 900B Model Guide DASSAULT FALCON 900B is a turbofan business jet. The registry lists the Falcon 900 family (variants 900, 900EX) at up to 4330 nm range, 428 kt cruise, 51000 ft ceiling and up to 18 passengers. Variant-specific figures are not in our sources. This guide draws on the maintenance manual's airworthiness limitations and an operator's normal checklist. • Family-level registry maxima: 4330 nm range, 428 kt cruise, 20600 kg MTOW, 18 passengers, 51000 ft ceiling. These are not 900B-specific. • Airworthiness limits run to a design service goal of 20,000 flights/30,000 flying hours. Mandatory tasks cannot be changed or deleted. • Ask for proof of compliance with Chapter 5-40, Revision 26 (September 2021). Non-compliance suspends the airworthiness certificate. • Regular cargo, training, search and rescue or other non-passenger use means the aircraft is not a 'Standard Aircraft' for the fatigue program. Life-limited parts Main and nose landing gear legs are limited to 20000 LDG each. Inboard flap screw jacks (P/N 5318-3) are overhauled at 3500 LDG and outboard at 4500 LDG. Seat safety belt assemblies have a life limit of 60 M, with a buckle spring inspection at 18 M. Eddy-current inspection of flap tracks 2 and 5 is due at 8855 FC, then every 4770 FC. Recurring mandatory checks The flap asymmetry detection test is due every 450 FH on aircraft with the AVIAC flap control system and every 1800 FH on those with DED. Confirm which system the aircraft has. Flight control hydraulic components get an integrity, corrosion and leak check every 4000 FH. Flap screw/nut play checks recur at 330 FH to 630 FH, depending on part number. Operator checklist notes The DM Air normal checklist (VER 3.1) covers APU start, 3 windshield heats, trims (5), stall tests and an oxygen mask test. Its listed climb profile is 300/.80 260/.72. Use it as a reference for what the systems should test as normal during a pre-buy flight. Safety notes: • Failure to comply with Chapter 5-40 leads to immediate suspension of the airworthiness certificate. • Modifications not approved by Dassault (STC, PMA) are not covered by the limitations. Non-standard aircraft need an adapted program. • Corrosion level 2 or 3 on principal structural elements must be reported. Structure must be kept at level 1 or better.