- Registered owner
- Treeline Helicopters Inc
- Location
- Bristol, TN
- Owner type
- Corporation
- Serial number
- 0577E
- Year built
- 2008
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Standard, normal
- Airworthiness date
- April 19, 2008
- Certificate issued
- June 12, 2026
- Expires
- June 30, 2033
- Mode S code
- AB0065
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 76
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1972 | 1 |
|---|---|
| 1973 | 1 |
| 1974 | 1 |
| 1977 | 2 |
| 1979 | 1 |
| 1980 | 1 |
| 1981 | 1 |
| 1982 | 4 |
| 1984 | 4 |
| 1986 | 2 |
| 1987 | 1 |
| 1988 | 1 |
| 1989 | 4 |
| 1990 | 6 |
| 1991 | 1 |
| 1992 | 1 |
| 1993 | 2 |
| 1994 | 1 |
| 1995 | 2 |
| 1996 | 3 |
| 1997 | 1 |
| 1998 | 3 |
| 1999 | 5 |
| 2000 | 1 |
| 2001 | 2 |
| 2002 | 1 |
| 2003 | 3 |
| 2005 | 4 |
| 2006 | 2 |
| 2007 | 2 |
| 2008 | 1 |
| 2012 | 1 |
| 2013 | 2 |
| 2015 | 1 |
| 2016 | 2 |
| 2017 | 1 |
| 2018 | 1 |
| 2019 | 1 |
| 2020 | 2 |
| 2021 | 1 |
| 2022 | 2 |
| 2023 | 1 |
| 2024 | 2 |
| 2025 | 1 |
| 2026 | 2 |
Airframe · MD Helicopters 369E
AD 2026-21-05Engine/transmission couplingAD 2026-19-01Rotorcraft flight controlAD 2025-17-11tail rotor control systemInformation bulletins that may apply · 3
Advisory, not mandatory.
Airframe · MD Helicopters 369E
SAIB AIR-21-19R1AERIAL TOW EQUIPMENT, Side Pull HookSAIB SW-12-45Garmin Model 400W/500W Series GPS-WAAS Navigation SystemEngine · Rolls-Royce 250-C20
SAIB CE-01-10Historical bulletins · 1
NTSB investigations
No NTSB investigations matched to N808JHMatched 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 MD Helicopters 369E aircraft
FAA incident reports · 1
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Service difficulty reports · 15
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DCGA202509100629Blade · dentedDURING A POST FLIGHT MAINTENANCE INSPECTION A SMALL DENT WAS DISCOVERED ON THE OUTBOARD FACE OF ONE OF THE AIRCRAFT TAIL ROTOR BLADES. PILOT REPORTED THERE WAS NO INDICATIONS OR NOISE OF ANYTHING STRIKING THE BLADE. THE BLADE DENT WAS FOUND TO BE WITHIN SERVICSDR 2023FA0000430Doubler · crackedDURING A POST FLIGHT INSPECTION, THE MECHANIC FOUND A CRACK ON THE AFT END OF THE RIGHT-HAND STATION 174 DOUBLER CONNECTING THE BOOM FAIRING AND TURTLE BACK OF THE UPPER AFT FUSELAGE.SDR 2019FA0000338Fuel Control · leakingDURING MAINTENANCE GROUND RUN CHECK OPERATIONS ENGINE FUEL WAS NOTICED COMING OUT OF THE FUEL CONTROL CASE AND LEAKING TO THE GROUND. FUEL CONTROL WAS REMOVED FOR INVESTIGATION AND A SERVICABLE UNIT INSTALLED.SDR 2019FA0000291Bladder · leakingFUEL LEAKING FROM LEFT HAND FUEL BLADDER. REPLACED BOTH LEFT AND RIGHT HAND BLADDERS.SDR 2019FA0000194Engine · making metalENGINE CHIP LIGHT ILLUMINATED WHEN ENGINE WAS BROUGHT TO FLIGHT IDLE AFTER ENGINE START UP. MAINTENANCE FOUND 2 FLAKES WITHIN LIMITS ON THE UPPER CHIP PLUG.A 30 MINUTE GROUND RUN WAS PERFORMED, THE PLUGS WERE INSPECTED AGAIN AND FOUND CLEAN. AIRCRAFT RETURNED SDR 2019FA0000075Blade · crackedTHE BOTTOM SKIN OF THE MAIN ROTOR BLADE HAS A 4 1/2 INCH CRACK STATING AT THE TRAILING EDGE AND PERPENDICULAR TO SPAN 57 1/4 INCHES IN FOR BLADE TIP.SDR DCGA2018FA0000398Gearbox · making metalDURING A POST MAINTENANCE OPERATIONAL CHECK FLIGHT THE MAIN ROTOR GEARBOX CHIP LIGHT ILLUMINATED. A PIECE OF METAL WAS FOUND ON THE CHIP PLUG. THE TRANSMISSION WAS REMOVED AND A SERVICABLE TRANSMISSION WAS INSTALLED.SDR 2016FA0000182Blade · delaminatedDURING ROUTINE MAINTENANCE APROXIMATELY 1" INBD FROM THE TIP ON THE TOP OF THE MAIN ROTOR BLADE, PN 500P2100-105, SN 907B A .5" X .5" DELAMINATION WAS FOUND ON THE STAINLESS STEEL L/E OF THE BLADE. THE BLADE WAS REMOVED FROME THE ACFT AT THIS TIME.SDR DCGA2015FA0000622Engine · making metalPILOT GOT AN INTERMITTENT ENGINE CHIP LIGHT INDICATION AFTER TAKEOFF AND RETURNED FOR LANDING. MAINTENANCE FOUND LIGHT EXTINGUISHED BUT FOUND METAL ON UPPER AND LOWER ENGINE CHIP PLUGS. ENGINE WAS REMOVED FROM THE ACFT FOR FURTHER INSPECTION.SDR 2015FA0000613Blade · out of balanceDURING A MAINTENANCE GROUND RUN OPERATION A HIGH LATERAL VIBRATION WAS ENCOUNTERED AND THE ACFT WAS SHUTDOWN. IT WAS DISCOVERED THAT WATER HAD ENTERED THE BLADE DURING A HEAVY RAINFALL THE NIGHT BEFORE. ATTEMPTS TO REMOVE THE WATER WERE UNSUCCESSFUL AND THE SDR DCGA2015FA0000520Engine · making metalENGINE CHIP LIGHT ILLUMINATED DURING TOUR FLIGHT. THE PILOT LANDED ACFT AND CALLED MAINTENANCE. MAINTENACE FOUND METAL FLAKE MEASURING LESS THAN .03125 ON UPPER AND LOWER ENGINE CHIP PLUGS. AFTER CLEANING THE PLUGS A 30 MINUTE GROUND RUN WAS PERFORMED AND THSDR 2015FA0000313Chip Detector · shortedPILOT RECIEVED A TAIL GEARBOX DIM CHIP LIGHT IN FLIGHT. THE PILOT PERFORMED AN UNEVENTFUL UNSCHEDULED LANDING AND CALLED MAINTENANCE. THE MECHANIC EXAMINED THE GEARBOX CHIP DETECTOR AND FOUND IT CLEAN. THE MECHANIC REPLACED AN INTERNALLY SHORTING CHIP DETESDR DCGA2015FA0000217Turbine · out of tolerancePILOT REPORTED CHIRPING NOISE FROM ENGINE AT END OF DAY SHUTDOWN. MAINTENANCE REMOVED TURBINE ASSY FOR SUSPECT N2 RUBBING.SDR DCGA2014042500280Wire · shortedPILOT REPORTED AN ENGINE CHIP LIGHT. THE CHIP LIGHT WAS EXTINGUISHED WHEN CHIP PLUGS WERE REMOVED AND CLEANED. DURING OPS CHECKS THE LIGHT CAME BACK ON. MAINTENANCE ULTIMATELY DISCOVERED A SHORTING WIRE IN THE LOWER ENGINE CHIP DETECTOR CONNECTOR. THE BAD PSDR 2010FA0000772Hub · vibrationPILOT EXPERIENCED IN FLIGHT STICK SHAKE AND UNUSUAL VIBRATION. MX SUSPECTS PROBLEM WITH DROOP RING AND FOLLOWERS ON MAIN ROTOR HUB ASSY.
STCs that may be installed · 252
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
See all 252 STCs