- Registered owner
- Arctic One LLC
- Location
- Fairbanks, AK
- Owner type
- LLC
- Serial number
- 53471
- Year built
- 1996
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- May 23, 1996
- Certificate issued
- April 13, 2018
- Expires
- April 30, 2028
- Mode S code
- AD63CB
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Pratt & Whitney JT8D model are included below.
On this page
Airworthiness directives that may apply · 58
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1970 | 4 |
|---|---|
| 1971 | 2 |
| 1975 | 1 |
| 1976 | 1 |
| 1977 | 5 |
| 1978 | 1 |
| 1980 | 1 |
| 1984 | 1 |
| 1985 | 1 |
| 1986 | 2 |
| 1987 | 1 |
| 1988 | 1 |
| 1989 | 1 |
| 1990 | 1 |
| 1992 | 1 |
| 1994 | 1 |
| 1995 | 5 |
| 1996 | 2 |
| 1997 | 5 |
| 1998 | 2 |
| 1999 | 4 |
| 2000 | 3 |
| 2001 | 2 |
| 2002 | 4 |
| 2003 | 3 |
| 2005 | 4 |
| 2006 | 3 |
| 2010 | 3 |
| 2011 | 3 |
| 2015 | 1 |
| 2021 | 1 |
See all 71 ADs
Information bulletins that may apply · 8
Advisory, not mandatory.
Historical bulletins · 1
NTSB investigations
No NTSB investigations matched to N962CEMatched 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 MD 83 aircraft
FAA incident reports
No FAA accident or incident reports matched to N962CEMatched 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 MD 83 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 FXGA07302025001Duct · crackedTAIL COMPARTMENT TEMP HIGH LIGHT ILLUMINATED DURING CLIMB. FOUND RT BLEED AIR SOURCE DUCT WELD BROKEN. REMOVED AND REPLACED 13THSTAGE BLEED AIR SOURCE DUCTING BETWEEN ENGINE AND AUGMENTER VALVE IAW AMM 20-10-11. LEAK CHECK GOOD IAW AMM 71-00-00 CONFIG 4 STEP 4SDR FXGA07292025002Overheat Sensor · activatedTAIL COMPARTMENT TEMP HIGH ILLUMINATED, REPLACED R/H TAIL COMPARTMENT TEMP SENSOR IAW MD-80 AMM 36-20-02. OPERATIONAL CHECK GOODSDR FXGA07292025001Duct Clamp · leakingTAIL COMPARTMENT TEMP HIGH ILLUMINATED, FOUND #2 ENGINE BLEED AIR LEAK IN TAIL SECTION, REPLACED CLAMP IAW MD-80 AMM 20-10-11. GROUND RUN-UP OPERATIONAL CHECK GOOD.SDR FXGA20240426001Unlock Cylinder · leakingNOSE LANDING GEAR FAILED TO EXTEND WITH NORMAL MEANS, CYCLED GEAR AND NOSE GEAR EXTENDED NORMALLY. LANDED WITH NO FURTHER INCEDENTSDR FXGA2021102001None · noneLEFT PAC SUPPLY PRESSURE DROPPED TO ZERO FOLLOWED BY LOSS OF PRESSURIZATION WHILE IN CRUISE TO ANC. FOUND LOOSE CLAMP AND DUCTING FROM ACM OUTPUT.SDR FXGA20210706Liner · delaminatedON DEPARTURE #1 ENGINE COMMPRESSOR STALLS, REDUCED POWER AND RETURNED TO KLRD, UPON VISUAL INSPECTION TURBINE LINER WAS DELAMINATED FROM ENGINE TURBINE CASE.
STCs that may be installed · 28
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Engine · Pratt & Whitney JT8D series
STC SE1622GLInstallation of Ametek 8TJ124GGR1 digital mass fuel flow transmitter.STC SE482CHInstallation of Tube Processing Corporation (TPC) JT8D-200 Anti-Ice tube assemblies Part Numbers 2026-TP, 2027-TP, 2028-TP and 2029-TP and support brackets Part Number 2060-TP, 2061-TP, 2062-TP and 2063-TPSTC SE01944LAInstallation of a JET Engineering, Ltd. Turbine Exhaust Cone Mixer (TECM).