N986SA1985 Gates Learjet Corp. 35A
Safety record in brief:No NTSB accidents or incidents since 1982No ADs since 1998 matched1 service difficulty report
Registration
FAA Aircraft Registry · Oct 17, 2026- Registered owner
- N331US LLC
- Owner type
- LLC
- City, state
- Hillsboro, OR
- Certificate issued
- Mar 20, 2025
- Expires
- Mar 31, 2032
- Airworthiness
- Standard · Transport
- Airworthiness date
- Feb 16, 2006
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Airframe & engine
FAA Registry + type dataAirframe
- Manufacturer
- Gates Learjet Corp.
- Model
- 35A
- Year
- 1985
- Serial number
- 609
- Aircraft type
- Fixed wing multi engine
- Category
- Land
- Certification
- Type Certificated
- Seats
- 10
- Engines
- 2
- Max takeoff weight
- 12,500 - 19,999 lb
- Mode S code
- ADC2FF
Engine
- Make and model
- Garrett Tfe731-2b
- Type
- Turbo-fan
- Power
- 3,500 lb thrust
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 2025 – nowN331US LLCHillsboro, OR · current
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 17, 2026 · SDRs · Oct 16, 2026NTSB events (0)
No NTSB accidents or incidents found for this airframe since 1982.
Accident history for this modelADs published since 1998 that may apply (0)
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
No ADs published since 1998 matched this airframe or engine model.
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (1)
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
- Hydraulic power · hydraulic line · chafedJan 12, 2021
TWO HYDRAULIC LINES FOR THE THRUST REVERSER SYSTEM IN THE TAIL RUBBED AGAINST EACH OTHER AND CHAFED THROUGH. IT WAS CHAFED THROUGH TO POINT THAT THERE WAS PIN HOLE LEAK IN ONE LINE AND THE OTHER LINE WAS CHAFED 3/4 OF THE THROUGH. DURING A 3.5 HOUR FLIGHT ABOUT A HALF A QUART OF HYDRAULIC FLUID…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 17, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 17, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026