N360SZ1984 Saab-Fairchild 340A
This N-number isn't registered right now. Below is its last known registration, canceled Mar 16, 2006.
Safety record in brief:No NTSB accidents or incidents since 1982No ADs since 1998 matched7 service difficulty reports
- Registration
- Deregistered
Registration
FAA Aircraft Registry · Oct 17, 2026- Last registered owner
- Lambert Leasing INC
- Owner type
- Corporation
- City, state
- Sterling, VA
- Certificate issued
- Jul 17, 2001
- Canceled
- Mar 16, 2006
- Airworthiness
- Standard · Transport
- Airworthiness date
- Jul 19, 1984
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
- Saab-Fairchild
- Model
- 340A
- Year
- 1984
- Serial number
- 340A-006
- Aircraft type
- Fixed wing multi engine
- Category
- Land
- Certification
- Type Certificated
- Seats
- 37
- Engines
- 2
- Max takeoff weight
- 20,000 and over lb
- Mode S code
- A40DF4
Engine
- Type
- Turbo-prop
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 2001 – 2006Lambert Leasing INCSterling, VA
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 (7)
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 · swivel · crackedOct 20, 2004
FLT 7925, DURING TAXI TO RUNWAY, HYDRAULIC LIGHT ILLUMINATED, HYDRAULIC PUMP RAN CONT, HYDRAULIC QTY ON THE MAIN AND OB WENT TO 0, BIG 1800 PSI, EMERGENCY 2500 PSI. INSPECTED AND FOUND RT OB BRAKE SWIVEL TO BE CRACKED. REMOVED AND REPLACED RT BRAKE SWIVEL, LEAK CHECK GOOD, IAW M/M 32-42-35-2.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Engine · engine · malfunctionedJul 29, 2004
FLIGHT 7889 IAD-TYS. DURING CLIMBOUT OF IAD CREW REPORTED LOSS OF RT ENGINE POWER. CREW DECLARED AN EMERGENCY AND RETURNED TO IAD.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Propellers · governor · malfunctionedApr 17, 2004
AIRCRAFT ABORTED TAKE OFF WHEN THE RT POWER WOULD NOT SET. POWER LEVERS BROUGHT TO 80 PERCENT, CTOT SET TO 90 PERCENT. LT WENT TO 90 PERCENT, RT STAYED AT 80 PERCENT.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 7 reportsShow fewer reports
- Landing gear · wheel · malfunctionedMar 11, 2004
ON TAKEOFF ROLL A/C EXPERIENCED A NOSE WHEEL SHIMMY AT 65KTS. AIRCREW ABORTED TAKE-OFF AND RETURNED SAFETY TO THE GATE.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Navigation · receiver · inoperativeJan 7, 2004
ON THIS DATE 1/7/04 AT APPROXIMATELY 1745Z, FLIGHT 4649 FROM BGM-PIT DECLARED AN EMERGENCY FOR VOR SYSTEM SHOWING RED LETTERS ON EFIS SYSTEM. BOTH VOR SYSTEMS INOP.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Landing gear · control valve · wornOct 24, 2002
UPON LANDING, PILOT REPORTED BRAKES FELT WEAK ON STARBOARD SIDE. FELT OK, AIRCRAFT INSPECTED AIRCRAFT AND FERRIED FOR FURTHER INVESTIGATION. REMOVED AND REPLACED BRAKE CONTROL VALVE AND FURTHER PROBLEMS NOTED.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Doors · plate · crackedSep 12, 2002
DURING RIGGING OF THE CARGO DOOR, IT WAS NOTED BY THE MECHANIC THAT THE CARGO DOOR HANDLE SLIDE PLATE WAS CRACKED AT THE TOP LOCKING PIN HOLE. SERVICE BULLETIN 340-52-022 HAD NOT BE COMPLIED WITH. AS A CORRECTIVE ACTION, THE CARGO DOOR WAS REMOVED AND SENT OUT FOR REPAIR. (M)
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