- Registered owner
- Bridger Air Tanker 4 LLC
- Location
- Belgrade, MT
- Owner type
- LLC
- Serial number
- 1089
- Year built
- 1986
- Type
- Fixed wing multi engine
- Engine
- Turbo-prop
- Airworthiness
- Restricted, forest
- Airworthiness date
- July 23, 2021
- Certificate issued
- July 22, 2021
- Expires
- July 31, 2028
- Mode S code
- A4F5BA
Canadair CL-215-6B11(CL-215T)TCDS A14EAAirframe · Canadair CL-215-6B11(CL-215T)TCDS E20NEEngine · Pratt & Whitney Canada PW123AF
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 34
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1977 | 2 |
|---|---|
| 1994 | 1 |
| 1995 | 2 |
| 1997 | 2 |
| 1998 | 2 |
| 2002 | 1 |
| 2003 | 1 |
| 2004 | 4 |
| 2005 | 3 |
| 2006 | 1 |
| 2009 | 1 |
| 2010 | 1 |
| 2011 | 3 |
| 2012 | 3 |
| 2013 | 4 |
| 2014 | 1 |
| 2015 | 1 |
| 2017 | 2 |
| 2019 | 2 |
| 2020 | 1 |
| 2023 | 2 |
| 2025 | 1 |
| 2026 | 1 |
Airframe · Canadair CL-215-6B11(CL-215T)
AD 2026-13-02NavigationAD 2025-07-01Air Data ComputerAD 2023-07-10Equipment/furnishingsInformation bulletins that may apply · 1
Advisory, not mandatory.
Airframe · Canadair CL-215-6B11(CL-215T)
SAIB AIR-21-15R1Navigation SystemHistorical bulletins · 1
NTSB investigations
No NTSB investigations matched to N419BTMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Canadair CL-215-6B11(CL-215T) aircraft
FAA incident reports
No FAA accident or incident reports matched to N419BTMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Canadair CL-215-6B11(CL-215T) aircraft
Service difficulty reports · 9
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 4GIA8G9R0106201Angle · crackedRIGHT WING IN PNL 841-20 DOUBLER BEHIND VERTICAL ANGLE HAS 3/4 INCH LONG CRACK FS 434 BL 51SDR 4GIA2026020300201Pump · failedRIGHT ENGINE DRIVEN HYDRAULIC PUMP REQUIRES REPAIR OR REPLACEMENT. THE HYDRAULIC PUMP WAS REMOVED & INSTALLED IAW PSP 392 29-11-12 AND SB 215-3134.SDR 4GIA2026020206201Drag Angle · failedLEFT 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 SDR 4GIA202601060001Spar Cap · failedR/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 SDR 8G9R202509110001Pump · making metalHYDRAULIC SYSTEM FOUND CONTAMINATED WITH METAL FROM FAILED L/H ENGINE-DRIVEN HYDRAULIC PUMP.SDR 8G9R705DSwitch · inoperativeAIRCRAFT 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 WASDR 8G9R20220217003Drag Angle · crackedR/H H-STAB LOWER FINLET R/H DRAG ANGLE CRACKED.SDR 8G9R20220217002Drag Angle · crackedR/H H-STAB LOWER FINLET L/H DRAG ANGLE CRACKEDSDR 8G9R20210902001Switch · fodCOMING 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 MAIN
STCs that may be installed · 23
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
See all 23 STCs