N198CJSaab-Scania SAAB 340B
This N-number isn't registered right now. Below is its last known registration, canceled Jul 30, 2019.
Safety record in brief:No NTSB accidents or incidents since 1982No ADs since 1998 matched34 service difficulty reports
- Registration
- Deregistered
Registration
FAA Aircraft Registry · Oct 20, 2026- Last registered owner
- Bank Of Utah Trustee
- Owner type
- Corporation
- City, state
- Salt Lake City, UT
- Certificate issued
- Jan 17, 2018
- Canceled
- Jul 30, 2019
- Airworthiness
- Standard · Transport
- Airworthiness date
- Dec 13, 1990
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-Scania
- Model
- SAAB 340B
- Serial number
- 340B-198
- 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
- A1861E
Engine
- Make and model
- Ge Ct7-Ser
- Type
- Turbo-prop
- Power
- 1600 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 2018 – 2019Bank Of Utah TrusteeSalt Lake City, UT
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 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 (34)
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.
- Electrical power · switch · failedMay 24, 2012
AIR TURN BACK DUE TO BOTH C/A AND F/O EFIS SCREENS INTERMITTENT DURING CLIMB-OUT. REPLACED GENERATOR SWITCH AND INSPECTED THE AVIONICS SWITCHES FOR SECURITY. ENGINE RUNS GOOD, OPS CHECKED NORMAL.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Engine indicating · cable · out of rigMar 16, 2012
RETURNED TO FIELD DUE TO TEMPERATURE AND TORQUE FLUX. RIGGED RT ENGINE CABLES. ALL CHECKS GOOD. NO PARTS NEEDED.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Power plant · warning system · activatedFeb 13, 2012
DURING TAXI CREW RECEIVED THE LEFT ENGINE INTAKE LIGHT. FLIGHT RETURNED TO GATE FOR MX.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reportsShow fewer reports
- Lights · power supply · inoperativeNov 4, 2011
AFT EMERGENCY LIGHTS WERE STAYING ON AFTER POWER IS TURNED OFF. EMERGENCY LIGHT POWER SUPPLY NR 3 WAS REMOVED AND REPLACED IN ACCORDANCE WITH WORK CARD 33-900-001 AND SYSTWM TESTED GOOD.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Doors · skin · dentedNov 1, 2011
CONTROL # 198-45: DENT IN CREW EMERGENCY ESCAPE HATCH OUTER SKIN REPAIRED IAW TD 340-52-11-01.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · skin · corrodedNov 1, 2011
CONTROL # 198-26: FUSELAGE SKIN UNDER RT ICE SHIELD NR 7 NUMEROUS AREAS OF DEEP PITTING CORROSION. COMPLETED IAW SAAB STATEMENT 340SDS-023393 AND TD 340-53-11-77.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · frame · corrodedOct 30, 2011
UPPER FLANGE OF BOTTOM FRAME AT STA 294 IS CORRODED FROM RBL 21.3 TO LBL 23.8. REFERENCE TD 340-53-11-09 AND MM 409 405419 FOR REPAIR DETAILS.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · skin · corrodedOct 30, 2011
RT FUSELAGE SKIN UNDER ICE SHIELD NR 7 HAS NUMEROUS AREAS OF MINOR TO DEEP PITTING CORROSION AND LIGHTNING EXIT HOLES PIN HOLES. REPAIR DOUBLER INSTALLED FROM FUSELAGE STA 306 TO 325.5 SL 1614 TO 1620. FOR TD340-53-11-77 AND MM-409# 404889. CONTROL # 198-26.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Wings · skin · corrodedOct 30, 2011
PREVIOUSLY INSTALLED DOUBLER REPAIR TO LT FUSELAGE NOT IN THE DAMAGE LOG. THE DOUBLER WAS FIRST INSTALLED IN OCTOBER 1997 (REF SAAB STATEMENT 72SD0721 DATED 10/27/1997) AND AGAIN 4/8/2000. REF SAAB DOC#72LKS3079 & THE PRINCIPLES OF THE SRM 53-70-10 PG 215. FIG 209. FAA FORM 337 DATED 4/8/2000 AND…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · stiffener · corrodedOct 29, 2011
FOUND DEEP CORROSION ON PREVIOUS REPAIR OF FORWARD FLIGHT DECK ENTRANCE FRAME STIFFENER TOP AT STA 225. REFERENCE TD 340-53-11-70 AND MM409# 405146 UNDER CONTROL # 198-38 FOR DETAILS OF REPAIR.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Showing the 10 most recent of 34 reports.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 20, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 20, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026