- Registered owner
- Arctic One LLC
- Location
- Fairbanks, AK
- Owner type
- LLC
- Serial number
- 49855
- Year built
- 1996
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- October 7, 2019
- Certificate issued
- August 10, 2018
- Expires
- August 31, 2028
- Mode S code
- AD765E
Mcdonnell Douglas DC-9-83(MD-83)TCDS A6WEAirframe · Mcdonnell Douglas DC-9-83(MD-83)TCDS E9NEEngine · Pratt & Whitney JT8D-219
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 287
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1967 | 6 |
|---|---|
| 1968 | 1 |
| 1969 | 1 |
| 1970 | 5 |
| 1971 | 5 |
| 1972 | 2 |
| 1974 | 2 |
| 1975 | 2 |
| 1976 | 1 |
| 1977 | 2 |
| 1978 | 2 |
| 1979 | 4 |
| 1980 | 1 |
| 1981 | 6 |
| 1982 | 8 |
| 1983 | 2 |
| 1984 | 3 |
| 1985 | 5 |
| 1986 | 5 |
| 1987 | 10 |
| 1988 | 9 |
| 1989 | 8 |
| 1990 | 10 |
| 1991 | 11 |
| 1992 | 13 |
| 1993 | 9 |
| 1994 | 12 |
| 1995 | 9 |
| 1996 | 14 |
| 1997 | 9 |
| 1998 | 8 |
| 1999 | 16 |
| 2000 | 11 |
| 2001 | 11 |
| 2002 | 16 |
| 2003 | 9 |
| 2004 | 10 |
| 2005 | 8 |
| 2006 | 9 |
| 2007 | 2 |
| 2008 | 5 |
| 2009 | 1 |
| 2010 | 4 |
| 2011 | 9 |
| 2012 | 2 |
| 2013 | 2 |
| 2014 | 3 |
| 2015 | 2 |
| 2016 | 3 |
| 2017 | 3 |
| 2018 | 2 |
| 2020 | 1 |
| 2021 | 1 |
| 2022 | 1 |
| 2023 | 4 |
| 2025 | 1 |
| 2026 | 2 |
Airframe · Mcdonnell Douglas DC-9-83(MD-83)
AD 2026-13-15NavigationAD 2026-13-02NavigationAD 2025-09-11Flight controlsInformation bulletins that may apply · 6
Advisory, not mandatory.
Airframe · Mcdonnell Douglas DC-9-83(MD-83)
SAIB NE-19-03Escape Slide Maintenance Tasks and Intervals - JASC 2565SAIB NM-15-03Flight ControlsSAIB NM-08-43Cabin Equipment/Furnishings - SeatsSAIB NM-06-57Reports of damage to airplanes and to property on the ground caused by blue or clear ice falling from airplanes.Engine · Pratt & Whitney JT8D-219
SAIB NE-16-22Turbine Engine Combustion Section JT8D Series Turbofan EnginesSAIB NE-10-32Turbine Engine Accessory DriveNTSB investigations
No NTSB investigations matched to N967CEMatched 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 Mcdonnell Douglas DC-9-83(MD-83) aircraft
FAA incident reports
No FAA accident or incident reports matched to N967CEMatched 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 Mcdonnell Douglas DC-9-83(MD-83) 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 FXGA202301142301None · noneMAIN CARGO DOOR AFT SEAL DEPRESSOR PERMANENT REPAIR REFERENCE AEI TICKET 21004 R00 (002) STEP 1.2. TO REPAIR DAMAGE TO MAIN CARGO DOOR AFT SEAL DEPRESSOR. CUTOUT EXISTING SEAL DEPRESSOR DAMAGES SECTION AT AEO PROPOSED CUTOUT LINES AS PER ATTACHED (967 MCD #3)SDR FXGA202211172230None · noneFUSELAGE SKIN GOUGED AT F/STA 463, STR 21L. TO REPAIR A DEEP GOUGE ON FUSELAGE SKIN. PERFORM SKIN REPAIR PER AEI EO 20455.SDR FXGA202201102141None · noneR/H HORIZONTAL STAB FAIRING CRACKED. REPAIR OF CRACK IN R/H HORIZONTAL STAB TO VERT STAB FAIRING. REPAIR HORIZONTAL STAB FAIRINGS PER ENGINEERING DRAWING NR-0014.SDR FXGA202201102140None · noneL/H HORIZONTAL STAB FAIRING CRACKED. REPAIR OF CRACK IN L/H HOIZONTAL STAB TO VERT STAB FAIRING. REPAIR HORIZONTAL STAB FAIRINGS PER ENGINEERING DRAWING NR-0014.SDR FXGA20201026Control Cable · bindingGEAR HANDLE STUCK IN UP POSITION, UNABLE TO LOWER THE GEAR IN BET ON FINAL APPROACH RWY 19. RETURN TO ANC, UNABLE TO LOWER THE FLAPS IN LANDING IN ANC, UNTIL 5 MILE FINAL, THEN THEY STARTED WORKING AGAIN. DECLARED EMERGENCY IN ANC PERFORMED EMERGENCY GEAR ESDR FXGA2019121141980Barrel Nut · corrodedHORIZONTAL STAB BARREL L/H #N55 AND #N56 SRM CORROSION REPAIR. REPAIR OF CORROSION IN THE L/H HORIZONTAL STAB BARREL NUT HOLES #N55 AND #N56. REPAIR OF BARREL NUT HOLES PER SRM 55-03 REAMED TO MIN .060" OVERSIZE AND INSERT OF BUSHING, DTA MAINTENANCE REQUIREMSDR FXGA201905211975Nose Cowl · crackedRIGHT ENGINE NOSE COWL INLET LE RING HAS CRACK @ THE 9 O'CLOCK POSITION. TO CUT OUT AND REPAIR DAMAGED RT ENGINE NOSE COWL INLET LE RING. TO CUT OUT AND REPAIR DMAMAGED RT ENGINE NOSE COWL INLET LE RING IAW SRM 54-04A FIGURE 5.SDR FXGA201905171941Skin · dentedFUSELAGE DENT AT F/STA 1228 STINGER 23L. TO REPAIR AN OUT OF LIMITS DENT AT F/STA 1228 STINGER 23L. REFORM DENT AND PERFORM REPAIR PER SRM 53-04-2 FIGURE 2 SHEET 2. THIS REQUIRES RE-INSPECTION PER 53-04-2 PARA D.SDR FXGA201904251935Skin · gougedFS 1228 FUSELAGE SKIN GOUGE & DENTED BELOW 23L. BLEND OUT REQUIRES REPAIR WITHOUT DAMAGE REMOVAL. FS 1228 FUSELAGE SKIN GOUGE & DENTED BELOW 23L, BLEN OUT REQUIRES REPAIR WITHOUT DAMAGE REMOVAL IAW 54-04-2 FIG 2. REPAIR REQUIRES RE-INSPECTION @ 8,000 CYCLES
STCs that may be installed · 439
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.