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Aircraft record

N107DU2019 C Series Aircraft Ltd Ptnrsp BD-500-1A10

Registration validUnclaimedSource: FAA, updated Oct 20, 2026

Safety record in brief:No NTSB accidents or incidents since 1982No ADs since 1998 matched40 service difficulty reports

Registration
Valid
expires Jul 31, 2027
Based in
Salt Lake City, UT
owner city / state
Owners
1
since 2020
NTSB events
None
since 1982
ADs may apply
0
confirm with A&P
Service reports
40
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Registered owner
Bank Of Utah Trustee
Owner type
Corporation
City, state
Salt Lake City, UT
Certificate issued
Jul 1, 2020
Expires
Jul 31, 2027
Airworthiness
Standard · Transport
Airworthiness date
Mar 1, 2019

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 data

Airframe

Manufacturer
C Series Aircraft Ltd Ptnrsp
Model
BD-500-1A10
Year
2019
Serial number
50026
Aircraft type
Fixed wing multi engine
Category
Land
Certification
Type Certificated
Seats
133
Engines
2
Max takeoff weight
20,000 and over lb
Type certificate data sheet
T00008NY
Mode S code
A01F13

Engine

Make and model
P & W Pw1519g
Type
Turbo-fan
Power
19,775 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
  1. 2020 – nowBank Of Utah TrusteeSalt Lake City, UT · current

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026

NTSB events (0)

No NTSB accidents or incidents found for this airframe since 1982.

Accident history for this model

ADs 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 (40)

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 oil · oil cooler · leakingJan 12, 2026

    ATB/FUMES - RETURNED TO MSP DUE TO FUMES IN THE FLIGHT DECK AND CABIN. PERFORMED HIGH POWER ENGINE RUNS WITH NO ODORS FOUND. P-TRACK DATA INDICATED APU AS LIKELY SOURCE OF ODOR. APU INSPECTION IN WORK. FOUND #2 ENGINE AIR/OIL COOLER CRACKED. SAME REPLACED. (LP# 8056530)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Air conditioning and pressurization · unknown · odorJul 12, 2025

    PRIOR TOD AT FL 340 STRONG SMELL OF BURNING ELECTRICAL. THE SMELL DISSIPATED 5 MINUTES LATER. OXYGEN MASKS WERE DEPLOYED IN THE COCKPIT. REF LP#: 1077551 FOR T/S & ODI COMPLETION. T/S PER A220 EFIM. FOUND ALL (5) AFDS DIRTY & CAKED W/ DUST. CLEANED PER AMP 31-61-01. CLEANED FLT CREW MASKS PER AMP…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · door frame · corrodedJul 10, 2025

    FWD PAX DOOR FRAME 22 HAS MULTIPLE FASTENER HOLES WITH CORROSION. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0567:5321-2009/003 00324 REPAIRED IAW PRI 627025-14 REV 0, PRI 627025-14 REV 1, PRI 627025-14 REV 2, PRI 627025-14 REV 3, AND ER/A 627025-14 REV ORIGINAL SECTION 1. (LP# 1074083)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Fuselage · door frame · corrodedJul 10, 2025

    FWD PAX DOOR FRAME 19 HAS MULTIPLE FASTENER HOLES WITH CORROSION. REPAIRED IAW PRI 627025-14 REV 0, PRI 627025-14 REV 1, PRI 627025-14 REV 2, PRI 627025-14 REV 3, AND ER/A 627025-14 REV ORIGINAL SECTION 1. (LP# 1074103)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · door frame · corrodedJul 10, 2025

    FWD SERVICE DOOR CUTOUT FASTENER HOLES FOR TRIM NUT PLATES AT FR17 AND FR20 SHOW OXIDATION. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0568:5321-2013/003 00338 REPAIRED IAW PRI 627026-14 REV 0, PRI 627026-14 REV 1, PRI 627026-14 REV 2, PRI 627026-14 REV 3, AND ER/A 627026-14 REV ORIGINAL…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · skin · corrodedJul 1, 2025

    CORROSION FOUND ON FUSELAGE SKIN FWD OF THE WASTE BOX AND FRAME 75. (P). SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0549:0500-2020/004 00354 COMPLIED WITH ER/A PRI 597330-14 REV 0, REV 1, AND FINAL ERA 597330-14AD REV A. ORIGINAL MATERIAL THICKNESS…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · seat track · corrodedJun 30, 2025

    AFT FUSELAGE SEAT TRACK CORROSION AFT OF STA 72 RBL 43.5. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0569:5321-2021/003 00303 REMOVED AND REPLACED AFT FUSELAGE SEAT TRACK PER A220 ASRP 51-77-00. (LP# 1055505)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · door sill · corrodedJun 29, 2025

    AFT CARGO LOWER SILL AFT CORNER STRIKER HAS CORROSION. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0523:5300-2012/003 00457 COMPLIED WITH PRI 626953-14 REV 0, PRI 626953-14 REV 1, PRI 626953-14 REV 2 AND FINAL ER/A 626953-14 REV ORIGINAL. SECTION I…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · door sill · corrodedJun 29, 2025

    AFT CARGO LOWER SILL FWD CORNER STRIKER HAS CORROSION. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0523:5300-2012/002 00456 COMPLIED WITH PRI 626953-14 REV 0, PRI 626953-14 REV 1, PRI 626953-14 REV 2 AND FINAL ER/A 626953-14 REV ORIGINAL. SECTION I…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · beam · corrodedJun 28, 2025

    FWD CARGO - LOWER SILL BEAM HAS CORROSION IN SCUFF PLATE ATTACH HOLES (M)(P). COMPLIED WITH ER/A 626994-14 PRI REV0, ER/A 626994-14 PRI REV 1 AND FINAL ER/A 626994-14 REV ORIGINAL SECTION I. SEE LOG # 1043585 FOR SECTION II REP. INSPECTION. COMPLIED WITH ER/A 626994-14 PRI REV0, ER/A 626994-14 PRI…

    From FAA Service Difficulty Reports; matched by N-number and serial number.

Showing the 10 most recent of 40 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

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