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Aircraft record

N415BT1985 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 apply6 service difficulty reports

Registration
Valid
expires May 31, 2027
Based in
Belgrade, MT
owner city / state
Engine
PW123AF · 2380 hp
P&W Canada
Owners
1
since 2020
NTSB events
None
since 1982
ADs may apply
9
confirm with A&P
Service reports
6
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Registered owner
Bridger Air Tanker 1 LLC
Owner type
LLC
City, state
Belgrade, MT
Certificate issued
May 27, 2020
Expires
May 31, 2027
Airworthiness
Experimental · To show compliance with FAR
Airworthiness date
Jun 6, 2020

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
1985
Serial number
1081
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
A4E6DE

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. 2020 – nowBridger Air Tanker 1 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 (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.

  • Fuselage · frame · crackedApr 7, 2025

    FRAME CRACKED ALONG BOTTOM FLANGE THROUGH BOLT HOLE FOR GUST LOCK CASTING TO LIGHTNING HOLE AT FS 434 BL 0 ROOF LEVEL. CRACK MEASURES 1.5" IN LENGTH.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · skin · crackedDec 10, 2024

    A CRACK MEASURING APPROXIMATELY 3/4" LONG WAS DISCOVERED ON THE ROOF SKIN LOCATED AT FS388, LWS43, WL225 APPROXIMATELY.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Flight controls · relay · faultyApr 28, 2024

    PILOT REPORT: WHILE ON DOWNWIND FOR LANDING KBZN WE HAD THE "RUDDER AUTO REVERSION TO MANUAL MODE AND LOST ALL RUDDER HYDRAULIC PRESSURE". WE RAN THE APPROPRIATE CHECKLIST "ABNORMAL PROCEDURES" PAGE 45 OF THE 215T QRH. SYSTEM HYDRAULIC LEVELS WERE STABLE BUT RUDDER PRESSURE REMAINED ZERO. WE…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 6 reports
  • Stabilizers · drag angle · crackedFeb 17, 2022

    RH HORIZONTAL STABILIZER FINLET LOWER O/B DRAG ANGLE IS CRACKED.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Doors · wire rope · frayedMay 7, 2021

    WIRE ROPE, WAS FOUND DURING DAILY INSP TO HAVE BROKEN STRANDS AT END THAT ATTACHES TO DAMPER FITTING. REMOVED & REPLACED WITH NEW WIRE ROPE ON LT FWD DOOR ATTACH POINT. VISUAL INSP OF REMAINING 3 WIRE ROPE ASSEMBLIES SHOW EXACT WEAR & BROKEN STRANDS IN SAME LOCATION, WHICH IS RIGHT AT DAMPER…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Flight controls · bonding strap · distressedJun 13, 2020

    PIC REPORTED A RESTRICTION IN ELEVATOR CONTROL NOSE UP MOVEMENT DURING LANDING FLARE. POWER APPLIED & A GO-AROUND EXECUTED, RETURN TO BASE. MAINT CONDUCTED A VISUAL INSP OF ENTIRE ELEV CONTROL SYS, CONTROL WHEEL & ELEV MOVEMENT. NO DEFECTS. DETAILED VISUAL INSP ACCOMP. DURING DVI, A BONDING STRAP…

    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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