- Registered owner
- Bridger Air Tanker 1 LLC
- Location
- Belgrade, MT
- Owner type
- LLC
- Serial number
- 1081
- Year built
- 1985
- Type
- Fixed wing multi engine
- Engine
- Turbo-prop
- Airworthiness
- Experimental, showing compliance
- Airworthiness date
- June 6, 2020
- Certificate issued
- May 27, 2020
- Expires
- May 31, 2027
- Mode S code
- A4E6DE
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 N415BTMatched 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 N415BTMatched 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 · 6
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 8G962025052300407Frame · crackedFRAME 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.SDR 2024FA0000950Skin · crackedA CRACK MEASURING APPROXIMATELY 3/4" LONG WAS DISCOVERED ON THE ROOF SKIN LOCATED AT FS388, LWS43, WL225 APPROXIMATELY.SDR 8G9R20240430001Relay · faultyPILOT 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 RSDR 8G9R20220217001Drag Angle · crackedRH HORIZONTAL STABILIZER FINLET LOWER O/B DRAG ANGLE IS CRACKED.SDR 2021FA0000131Wire Rope · frayedWIRE 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 SDR 2020FA0000308Bonding Strap · distressedPIC 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 IN
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