- Registered owner
- Bank Of Utah Trustee
- Location
- Salt Lake City, UT
- Owner type
- Corporation
- Serial number
- 49104
- Year built
- 1982
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- October 3, 2013
- Certificate issued
- October 24, 2012
- Expires
- October 31, 2028
- Mode S code
- ACB477
Mcdonnell Douglas DC-9-82(MD-82)TCDS A6WEAirframe · Mcdonnell Douglas DC-9-82(MD-82)TCDS E9NEEngine · Pratt & Whitney JT8D-217C
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 291
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 | 10 |
| 1990 | 10 |
| 1991 | 11 |
| 1992 | 13 |
| 1993 | 10 |
| 1994 | 12 |
| 1995 | 9 |
| 1996 | 14 |
| 1997 | 9 |
| 1998 | 9 |
| 1999 | 16 |
| 2000 | 11 |
| 2001 | 10 |
| 2002 | 16 |
| 2003 | 9 |
| 2004 | 10 |
| 2005 | 9 |
| 2006 | 10 |
| 2007 | 2 |
| 2008 | 6 |
| 2009 | 1 |
| 2010 | 4 |
| 2011 | 9 |
| 2012 | 2 |
| 2013 | 2 |
| 2014 | 3 |
| 2015 | 2 |
| 2016 | 2 |
| 2017 | 3 |
| 2018 | 2 |
| 2020 | 1 |
| 2021 | 1 |
| 2022 | 1 |
| 2023 | 4 |
| 2025 | 1 |
| 2026 | 2 |
Airframe · Mcdonnell Douglas DC-9-82(MD-82)
AD 2026-13-15NavigationAD 2026-13-02NavigationAD 2025-09-11Flight controlsInformation bulletins that may apply · 6
Advisory, not mandatory.
Airframe · Mcdonnell Douglas DC-9-82(MD-82)
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-217C
SAIB NE-16-22Turbine Engine Combustion Section JT8D Series Turbofan EnginesSAIB NE-10-32Turbine Engine Accessory DriveNTSB investigations
No NTSB investigations matched to N918AVMatched 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-9-82(MD-82) aircraft
FAA incident reports
No FAA accident or incident reports matched to N918AVMatched 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-9-82(MD-82) aircraft
Service difficulty reports · 15
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2CCA15072101Power Supply · inoperativeDURING SERVICE CHECK, EMERGENCY LIGHTS DID NOT ILLUMINATE AT ROWS 7 THRU 11. DURING TROUBLESHOOTING, NOTED POWER SUPPLY SMELLED BURNED. R & R POWER SUPPLY IAW AMM, OPS CHECKED GOOD.SDR 2CCA15052901918Actuator · out of adjustDURING POST MAINTENANCE VISIT ACCEPTANCE FLIGHT, DURING FLIGHT CONTROL CHECK IN EXCESS OF 250 KTS, FOUND LT RUDDER HAD NO EFFECT WHEN DEPRESSED FULLY - EITHER WITH POWER ON OR OFF. FULL RUDDER TRIM HAD NO EFFECT DEFLECTED LEFT. RT RUDDER CHECK AND TRIM OPERASDR 2CCA2015060100066Piston · out of adjustDURING POST MAINTENANCE VISIT ACCEPTANCE FLIGHT, DURING FLIGHT CONTROL CHECK IN EXCESS OF 250 KTS, FOUND LT RUDDER HAD NO EFFECT WHEN DEPRESSED FULLY - EITHER WITH POWER ON OR OFF. FULL RUDDER TRIM HAD NO EFFECT DEFLECTED LEFT. RIGHT RUDDER CHECK AND TRIM OSDR 2CCA20140311918Sensor · failedENROUTE AT FL 36.0, RECEIVED MOMENTARY RT ICE PROTECTION TEMP HIGH LIGHT. WAS ON FOR LESS THAN A SECOND. AIRFOIL ICE OFF, ENGINE ON. CABIN PRESSURE STARTED FLUCTUATING +/- 300-500 FT A MINUTE MOMENTARILLY WITH AN INTERMITTENT FLOW LIGHT. PERFORMED QRH PROCESDR 2CCA2014F00082Angle · crackedFORWARD MAIN CABIN ENTRANCE DOOR UPPER FORWARD CORNER ANGLE CRACKED.SDR 2CCA2014F00081Angle · crackedFORWARD MAIN CABIN ENTRANCE DOOR UPPER FORWARD CORNER ANGLE CRACKED.SDR 2CCA2013083003Cusp Web · corrodedDURING 60 MO SI; CORROSION FOUND AT BS 256 RT WEB MEMBRANE. CORROSION REMOVED AND REPAIR DOUBLER INSTALLED IAW SRM 53-05, FIG 131A-10.SDR 2CCA2013083002Cusp Web · corrodedCORROSION DISCOVERED AT BS 239 LT CUSP MEMBRANE. CORROSION REMOVED AND REPAIR DOUBLER, INSTALLED IAW SRM 53-05, FIG 131A-10.SDR 2CCA2013083001Tee Fitting · corrodedCORROSION FOUND IN RT AFT LAVATORY BS 1338 CUSP LINE AND LONG 18. INSTALLED CUSP TEE SLICE REPAIR AT BS 1300 - 1336 LONG 18R IAW SRM 53-05, FIG 25.SDR EE4Y2012080100266Skin · crackedLOWER FUSELAGE AT Y STA 68.5-Z13RH SECTION SKIN WITH CRACKED. THE SKIN WAS REPAIRED IAW EO COO-9-53-197-12 WITH APPROVAL. UNDER NON ROUTINE ITEM; WO:A1A163,SUBJOB:1,ITEM:303.SDR EE4Y2012072400262Angle · crackedLOWER FUSELAGE AFT CARGO COMPARTMENT BS 1155 BETWEEN LONGERON 28 AND 29 RT ANGLE CRACKED. ANGLE WAS REPLACED WITH THE SRM 51-01, PARAGRAPH 2.SDR EE4Y2012072400265Panel · crackedLT WING T/E CAVITY UPPER PANEL EDGE CRACKED AT XCW 109. THE PANEL WAS REPAIRED IAW SRM 57-09, FIG 42.SDR EE4Y2012072400264Fitting · corrodedRIGHT WING NR 3 SLAT CENTER TRACK FITTING LUGS WITH CORROSION. FITTINGS WERE REPLACED WITH THE SRM 51-01, PARA 2D.SDR EE4Y2012072400263Door · corrodedLOWER FUSELAGE AFT LAVORATORY SERVICE DOOR WITH CORROSION. SERVICE DOOR WAS REPLACED IAW SRM 51-01, PARA 2.SDR EE4Y2012072400261Support Fitting · crackedLOWER FUSELAGE RT MLG WW CEILING AREA AT Y BS 977 FLAP ACTUATOR SUPPORT FITTING WITH CRACK. FITTING WAS REPLACED IAW SRM 51-01, PARAGRAPH 2D.
STCs that may be installed · 477
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.