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Aircraft record

N419BT1986 Canadair CL-215-6B11(CL-215T)

Registration validUnclaimedSource: FAA, updated Oct 20, 2026

Safety record in brief:No NTSB accidents or incidents since 19829 ADs may apply9 service difficulty reports

Registration
Valid
expires Jul 31, 2028
Based in
Belgrade, MT
owner city / state
Engine
PW123AF · 2380 hp
P&W Canada
Owners
1
since 2021
NTSB events
None
since 1982
ADs may apply
9
confirm with A&P
Service reports
9
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Registered owner
Bridger Air Tanker 4 LLC
Owner type
LLC
City, state
Belgrade, MT
Certificate issued
Jul 22, 2021
Expires
Jul 31, 2028
Airworthiness
Restricted · Forest
Airworthiness date
Jul 23, 2021

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
Canadair
Model
CL-215-6B11(CL-215T)
Year
1986
Serial number
1089
Aircraft type
Fixed wing multi engine
Category
Amphibian
Certification
Type Certificated
Seats
10
Engines
2
Max takeoff weight
20,000 and over lb
Type certificate data sheet
A14EA
Mode S code
A4F5BA

Engine

Make and model
P&W Canada Pw123af
Type
Turbo-prop
Power
2380 hp

Total time and engine hours aren't public. They appear here once the owner adds logbooks.

Ownership history

Ownership history from FAA records
  1. 2021 – nowBridger Air Tanker 4 LLCBelgrade, MT · 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 (9)

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.

ADSubjectEffectiveApplies to
2023-07-10Equipment/ furnishingsJun 20, 2023Airframe (CL-215-6B11(CL-215T))
2019-25-11WingsFeb 10, 2020Airframe (CL-215-6B11(CL-215T))Certain serial numbers: CL-215-1A10 1001–1125; CL-215-6B11 1001–1125
2019-08-12Flight controlsJun 13, 2019Airframe (CL-215-6B11(CL-215T))Certain serial numbers: CL-215-6B11 1085; CL-215-6B11 1086; CL-215-6B11 1093; CL-215-6B11 1094; CL-215-6B11 1098–1101; CL-215-6B11 2076–2090. Only with: Serials 1085-1101 are CL-215T Variant; serials 2076-2090 are CL-415 Variant.
2019-02-05WingsMar 22, 2019Airframe (CL-215-6B11(CL-215T))Certain serial numbers: CL-215-1A10 1001–1125; CL-215-6B11 1056–1125
2017-17-17Hydraulic powerOct 11, 2017Airframe (CL-215-6B11(CL-215T))Certain serial numbers: CL-215-1A10 1001–1125; CL-215-6B11 1056–1125; CL-215-6B11 2001–2990
Show all 9 ADs
ADSubjectEffectiveApplies to
2017-15-14Equipment/ FurnishingsSep 5, 2017Airframe (CL-215-6B11(CL-215T))Certain serial numbers: 2001; 2002; 2005–2007; 2010; 2012–2017; 2019; …. Only with: CL-415 Variant
2013-15-08Pratt & Whitney Canada Corp. Turboprop EnginesSep 17, 2013Engine (PW123AF)Serial numbers per Table 1 of the Appendix of P&WC Service Bulletin No. PW100-72-21823, Revision 3. Only with: First-stage power turbine blade P/N 3120973-01, 3120983-01, or 3054053-01 installed with a serial number listed in the referenced SB table.
2012-26-08Pratt & Whitney Canada Corp. Turboprop EnginesFeb 15, 2013Engine (PW123AF)Serial numbers per P&WC ASB No. PW100-72-A21813 Rev 3, PW100-72-A21802 Rev 4, and PW100-72-A21798 Rev 5. Only with: Engines with propeller shafts having serial numbers listed in the referenced P&WC ASBs.
2004-20-01Pratt & Whitney Canada Models PW123, PW123B, PW123C, PW123D, PW123E, PW123AF, PW124B…Nov 5, 2004Engine (PW123AF)Only with: Mechanical fuel controls (MFCs) P/Ns 3244841-21, 3244853-17, 3244855-15, 3244857-14, 3244858-23, 3244871-5, 3244873-4, and 3244874-4 installed.

AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.

Service Difficulty Reports (9)

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.

  • Wings · angle · crackedFeb 4, 2026

    RIGHT WING IN PNL 841-20 DOUBLER BEHIND VERTICAL ANGLE HAS 3/4 INCH LONG CRACK FS 434 BL 51

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Hydraulic power · pump · failedFeb 3, 2026

    RIGHT ENGINE DRIVEN HYDRAULIC PUMP REQUIRES REPAIR OR REPLACEMENT. THE HYDRAULIC PUMP WAS REMOVED & INSTALLED IAW PSP 392 29-11-12 AND SB 215-3134.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Stabilizers · spar cap · failedJan 6, 2026

    R/H FWD HORIZONTAL STABILIZER LOWER SPAR CAP FOUND CRACKED INBOARD OF FINLET ATTACH BRACKET NDT SERVICES FOR RH HORIZONTAL STABILIZER LOWER SPAR CAP CRACK- INSPECTION OF CUT IN SPAR MADE DURING REPAIR. REFER TO 250031-28 FOR ORIGINAL REPAIR RD215-55-47. R/H LOWER SPAR CAP HFEC INSPECTION C/O BY…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 9 reports
  • Fuselage · drag angle · failedJan 6, 2026

    LEFT FWD WING TO FUSELAGE DRAG ANGLE FOUND CRACKED. LT REAR WING TO FUSELAGE DRAG ANGLE CRACKED IN RH AFT WING DOULBLER BEHIND ANGLE IS CRACK: PERFORM AN EDDY CURRENT INSPECTION TO DETECT CRACKING OF THE FUSELAGE FRAME ANGLES AT THE WING FRONT AND REAR SPAR ATTACHMENT TO THE FUSELAGE, IN…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Hydraulic power · pump · making metalSep 8, 2025

    HYDRAULIC SYSTEM FOUND CONTAMINATED WITH METAL FROM FAILED L/H ENGINE-DRIVEN HYDRAULIC PUMP.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Landing gear · switch · inoperativeMay 23, 2022

    AIRCRAFT NLG DID NOT RETRACT AFTER TAKEOFF. ABLE TO LAND WITHOUT INCIDENT. UPON INSPECTION, TECHNICIANS FOUND CENTERING SWITCH OUT OF ADJUSTMENT. TECHNICIANS CORRECTED SWITCH. AIRCRAFT MAY HAVE EXPERIENCED A LANDING GEAR OVERSPEED CONDITION SO AN INSPECTION WAS PLANNED AND CONDUCTED. OEM TECH…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Stabilizers · drag angle · crackedFeb 17, 2022

    R/H H-STAB LOWER FINLET L/H DRAG ANGLE CRACKED

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Stabilizers · drag angle · crackedFeb 17, 2022

    R/H H-STAB LOWER FINLET R/H DRAG ANGLE CRACKED.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Flight controls · switch · fodAug 31, 2021

    COMING OFF A SCOOP, FLAPS WERE SELECTED 0 FROM 10, AFTER THE SELECTOR WAS MOVED THE INDICATOR STILL SHOWED 10 FLAPS. A VISUAL INSPECTION FROM BOTH PILOTS VERIFIED THE FLAPS WERE STILL AT 10. THE ABNORMAL CHECKLIST WAS RUN AND WE PROCEEDED BACK TO KCIC FOR MAINTENANCE. ROOT CAUSE OF NON-MOVEMENT OF…

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

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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