N309PXBritish Aerospace BAE JETSTREAM 3101
This N-number isn't registered right now. Below is its last known registration, canceled Sep 20, 2001.
Safety record in brief:No NTSB accidents or incidents since 1982No ADs since 1998 matched6 service difficulty reports
- Registration
- Deregistered
Registration
FAA Aircraft Registry · Oct 18, 2026- Last registered owner
- Finova Capital Corporation
- Owner type
- Corporation
- City, state
- Scottsdale, AZ
- Certificate issued
- Mar 4, 1998
- Canceled
- Sep 20, 2001
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
- British Aerospace
- Model
- BAE JETSTREAM 3101
- Serial number
- 676
- Aircraft type
- Fixed wing multi engine
- Category
- Land
- Certification
- Type Certificated
- Seats
- 19
- Engines
- 2
- Max takeoff weight
- 12,500 - 19,999 lb
- Mode S code
- A3421C
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- 1998 – 2001Finova Capital CorporationScottsdale, AZ
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 18, 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 (6)
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.
- Engine indicating · tq signal cond · failedMay 31, 1997
LEFT TORQUE AND EGT FLUCTUATION WITH SRL AND TTL ON, TTL OFF AND NO TORQUE FLUCTUATION BUT STILL EGT FLUCTUATION. SRL CAP LIGHT ILLUMINATED, STILL EGT FLUCTUATION WITH SRL TURNED OFF. REMOVED AND REPLACED LEFT SIGNAL CONDITIONER. (M)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Engine indicating · srl computer · failedMar 4, 1997
RIGHT SRL LIGHT ILLUMINATED DURING TAKEOFF ROLL AND TAKEOFF WAS ABORTED. DEFER SRL PER MEL. (M)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Engine indicating · tq indication · fluctuatedOct 20, 1996
ON TAKEOFF, LT ENG HAD ERRATIC TQ AND EGT IND. TQ FLUCTUATED FROM 100 PERCENT TO 70 PERCENT WITH EGT FLUCTUATING FROM 640 TO 500 WITH CORRESPONDING LOSS OF ENGINE PERFORMANCE LAST APPROX 5 MINUTES, THEN STABILIZED BY ITSELF APPROX 3 MINUTES LATER EGT FLUCTUATED FROM 600/200. INSPECTED EGT PIGTAIL…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 6 reportsShow fewer reports
- Engine indicating · wire harness · brokenOct 20, 1996
LEFT ENGINE EGT HAD EXTREME TEMP FLUCTUATIONS ON TAKEOFF ROLL. REMOVED AND REPLACED LEFT ENGINE EGT HARNESS BECAUSE OF DISLOCATED TERMINAL END RAN A/C OPS CHECK GOOD. (M)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Hydraulic power · hyd pump · malfunctionedAug 30, 1995
ON REPOSITION FLIGHT TO TUP LOST LEFT HYD PUMP AND RIGHT PUMP INTERMITTENT. UPON LANDING FOUND HYDRAULIC LINE RUPTURED. FOUND RUPTURED HYD PRESSURE LINE IN LEFT ENGINE NACELLE AND REPLACED LINE. REMOVED AND REPLACED LEFT AND RIGHT HYDRAULIC PUMPS AS A PRECAUTION DUE TO LOSS OF HYDRAULIC FLUID. (M)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Hydraulic power · pressure hose · rupturedAug 30, 1995
ON REPOSITION FLIGHT TO TUP, LOST LEFT HYD PUMP AND RIGHT PUMP INTERMITTENT. UPON LANDING FOUND HYDRAULIC LINE RUPTURED. FOUND RUPTURED HYD PRESSURE LINE IN LEFT ENGINE NACELLE AND REPLACED LINE. REMOVED AND REPLACED LEFT AND RIGHT HYDRAULIC PUMPS AS A PRECAUTION DUE TO LOSS OF HYDRAULIC FLUID. (M)
From FAA Service Difficulty Reports; matched by N-number and serial number.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 18, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 18, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026