- Registered owner
- Federal Dynamics Corp
- Location
- Henderson, NV
- Owner type
- Corporation
- Serial number
- 53093
- Year built
- 1993
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- June 29, 1993
- Certificate issued
- August 26, 2021
- Expires
- August 31, 2028
- Mode S code
- AAFDD3
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 · 1
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
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 · 8
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2WAA2018042501Slide · no testL1 DOOR ESCAPE SLIDE FAILED TO INFLATE DURING DEPLOYMENT PROCESS.SDR 2WAA201804240001Landing Gear · collapsedRIGHT MAIN LANDING GEAR COLLAPSED AFTER LANDING.SDR 2018F00060Clamp · unsecureTAIL COMPARTMENT TEMP HIGH WARNING LIGHT COME ON DURING CLIMB. DURING TROUBLESHOOTING, FOUND THE LT COOLING TURBINE OULET DUCT LOOSE FROM THE CLAMP, REPOSITIONED THE PNEUMATIC DUCT AND SECURED THE CLAMP, PERFORMED OPS & LEAK CHECKS, NO LEAKS NOTED IAW IAW ASDR 2WAA20171222011Clamp · looseTAIL COMPARTMENT TEMP HIGH WARNING LIGHT CAME ON DURING CLIMB. DURING TROUBLESHOOTING, FOUND THE RT COOLING TURBINE OUTLET DUCT CLAMP LOOSE. REPOSITIONED THE PNEUMATIC DUCT AND SECURED THE CLAMP. PERFORMED AN OPS & LEAK CHECK, NO LEAKS NOTED IAW AMM 21-51-01SDR 2WAA2017101900001Oven · odorWIRE BURNING ODOR AT 12000 FT, SMOKE IN FWD CABIN. TURNED OFF MASTER GALLEY POWER SWITCH, SMOKE DISSIPATED. PERFORMED A VISUAL INSPECTION AND EWIS ON MASTER GALLEY POWER SWITCH AND SURROUNDING CIRCUITRY AT OVER HEAD PANEL, AND ON EPC PANEL AND GALLEY WIRING ISDR 2WAA20160809001Link Assy · damagedGEAR DOOR OPEN LIGHT AND LEFT GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. DIVERTED. ON INSPECTION, FOUND MLG INBD LOWER LINK ASSY DAMAGED. REPLACED IAW AMM 32-32-02, OPS CHECKED SATISFACTORY IAW AMM 32-30-00.SDR 2WAA201629003Duct · failedRIGHT FIRE INDICATION AND BOTH LOOP LIGHTS ILLUMINATED DURING CLIMB OUT. ALL LIGHTS EXTINGUISHED AFTER REDUCING THRUST. OPENED NR 2 ENGINE FOUND UPPER INBD ANTI-ICE AIR TUBE RUPTURED UP TO STAGE 8 IAW AMM 75-10-02.REMOVED AND INSTALLED NR 2 ENGINE INBD UPPER SDR 2WAA20150914002Control Panel · failedBOTH HAND MIKES NOT WORKING, CAPT AND F/O. PERFORMED OPS CHECK ON CAPT SIDE IAW AMM 23-50-02, FOUND NORMAL. T/S ON F/O SIDE FOUND AUDIO CONTROL PANEL INOPERATIVE. R & R F/O AUDIO CONTROL PANEL IAW AMM 23-50-02, OPS CHECK FOUND NORMAL.
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.